Document ID: EPA-HQ-OAR-2002-0030-0217
Agency: epa
Document Type: Supporting & Related Material
Title: 
Posted Date: 2005-05-20T04:00Z

Introduction
ICAO
ENGINE
EXHAUST
EMISSIONS
DATA
BANK
SUBSONIC
ENGINES
Introduction
This
workbook
contains
a
combined
version
of
the
ICAO
Exhaust
Emissions
Data
Bank
There
are
five
worksheets.
The
first
sheet
is
the
Introduction
sheet,
which
is
this
sheet.

A
record
of
the
issue
number
and
changes
to
the
databank
is
held
in
Record
of
Changes.

The
Record
of
Changes
sheet
is
followed
by
a
background
description
of
the
databank
(
Background).

The
Data
spreadsheet
contains
all
the
data
for
all
the
engines
with
one
engine
per
row.
Engines
are
grouped
by
manufacturer.

In
this
version
the
engines
of
each
manufacturer
are
grouped
alphabetically
so
that
for
each
engine
e.
g.
PW4056,
all
versions
appear
together.

Column
Description
describes
the
contents
of
each
column
in
the
Data
worksheet.

Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Introduction,
Page
1
of
149
Record
of
Changes
Issue
Date
Detail
of
Changes
17­
Mar­
04
Issue
12
implemented
on
Website.

9­
Mar­
04
New
engine
data
added,
CFM56
5C2/
P,
5C3/
P,
5C4/
P,
5B8/
P,
5B9/
P,
5B9/
2P
1CM006
engine
identification
changed
from
CFM56­
3C
(
rerated)
to
CFM56­
3C­
1
(
rerated)
1CM004,
005,
006
­
additional
note,
number
4,
added.

27­
Feb­
04
New
engine
data,
PW306A,
PW306B,
PW308A,
PW308C
added.

23­
Dec­
03
New
engine
data
added
BR700­
710­
C4­
11
28­
Nov­
03
Issue
11
implemented
on
Website.

27­
Nov­
03
New
engine
data
added
­
Tay
611­
8C
11
2­
Sep­
03
Correction
to
engine
identifier
for
UID
1RR001,
M54H
corrected
to
M45H
Correction
to
data
for
engines
UID's
3GE067
to
3GE079
to
include
note
showing
idle
data
calculated
at
normal
idle
setting
rather
than
7%.
1­
Sep­
03
New
engine
data
added
­
CF34­
8C1
Block
1
10
19­
May­
03
Issue
10
implemented
on
Website.
No
new
data
at
this
time.
12­
Feb­
03
Data
in
columns
CR
and
CS
changed
to
date
format
(
previously
a
mixture
of
date
and
text
formats).
4­
Feb­
03
New
engine
data
added
­
CF34­
8C5,
­
8E2,
­
8E5,
­
8E5A1
New
engine
data
added
­
CFM56­
5B7/
P
CF6­
80E
series
UID
No's
2GE050,
2GE051
and
4GE081
not
currently
produced
with
low
emissions
combustor
(
1862M39),
marked
as
out
of
production.
28­
Nov­
02
New
engine
data
added
­
AE3007
family,
20
new
entries.

9
31­
Jul­
02
New
engine
data
added
­
Trent
556­
61
with
Phase
5
tiled
combustor
17­
Jul­
02
New
engine
data
added
­
GE90­
76B,
­
77B,
­
85B,
­
90B,
­
94B
with
turbomachinery
incorporating
3D
aero
2­
Jul­
02
Further
format
changes.
No
new
data
at
this
time.
27­
Mar­
02
Rolls­
Royce
Corporation
AE3007C1
added
8
19­
Dec­
01
New
engine
data
added
­
GE90­
76B
27­
Nov­
01
New
engine
data
added
­
CF34­
3B,
CF34­
8C1,
CF6­
80E1A3
Changes
to
background
notes,
column
descriptions
and
data
base
format
(
data
requirements
and
associated
data)

7
14­
Nov­
00
New
engine
data
added
­
PW4098
27­
Oct­
00
New
engine
data
added
­
PW4168
with
TALON
II
combustor.

6
2­
May­
00
New
engine
data
added
­
PW4X58
with
TALON
II
combustor.

5
29­
Feb­
00
New
engine
data
added
­
Trent
895
New
engine
data
added
­
RB211­
535E4
and
­
535E4B
with
phase
5
combustor
4
31­
Dec­
99
New
engine
data
added
­
AE3007A,
AE3007A1
series
(
A1,
A1/
1,
A1/
2)
New
engine
data
added
­
PW2037
and
PW2040
­
revised
to
add
second
engine
test
New
engine
data
added
­
BR700­
710A1­
10,
­
710A2­
20.

3
16­
Nov­
99
New
engine
data
added
­
BR700­
715A1­
30,
­
715B1­
30
and
715C1­
30
with
improved
fuel
injectors.
New
engine
data
added
­
JT8D­
217,
­
217A,
­
217C,
­
219
with
E­
Kit
combustors.

2
8­
Feb­
99
Engine
UID
2PW062,
CO
idle
EI
and
Dp/
Foo
average
were
reversed.
This
has
been
corrected.
New
engine
data
added.
Spey
555,
standard
fuel
pump.
RB211­
524G­
T
and
­
524
H­
T,
BR700­
715A1­
30,
­
715B1­
30
and
­
715C1­
30
New
engine
data
added.
CFM56­
5A4,
­
5A5.
CFM56­
5B2/
2P,
­
5B3/
2P
CFM56­
7B20/
2,
­
7B22/
2,
­
7B24/
2,
­
7B26/
2,
­
7B27/
2.
CF6­
80E1A4
standard
combustor,
CF6­
80E1A4
low
emissions
combustor
PW4168A
1
10­
Mar­
98
First
full
issue
of
the
databank
on
the
internet
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Record
of
Changes,
Page
2
of
150
Background
Double
click
on
the
icon
to
open
the
file
in
Microsoft
Word.

Databank
supporting
text
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Background,
Page
3
of
150
Data
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
A
B
C
D
E
F
G
UID
Engine
Combustor
Eng
B/
P
Press
Rated
No
Identification
Description
Type
Ratio
Ratio
Output
kN
Allied
Signal
1AS001
TFE731­
2­
2B
TF
2.64
13.9
15.6
1AS002
TFE731­
3
TF
2.64
14.3
16.5
Allison
Engine
Company
/
Rolls­
Royce
Corporation
4AL003
AE3007A
TF
5.23
18.08
33.73
4AL002
AE3007A1
series
TF
4.76
17.81
33.73
3AL001
AE3007C
TF
5.3
16.2
28.6
6AL004
AE3007C1
TF
5.1
16.6
31.5
6AL005
AE3007A1
Type
1
TF
4.77
17.97
34.91
6AL006
AE3007A1
Type
2
TF
4.77
17.97
34.91
6AL007
AE3007A1
Type
3
(
reduced
emissions)
TF
4.77
17.97
34.91
6AL008
AE3007A1/
1
Type
1
TF
4.77
17.9
34.74
6AL009
AE3007A1/
1
Type
2
TF
4.77
17.9
34.74
6AL010
AE3007A1/
1
Type
3
(
reduced
emissions)
TF
4.77
17.9
34.74
6AL011
AE3007A1/
3
Type
1
TF
4.81
17.22
33.05
6AL012
AE3007A1/
3
Type
2
TF
4.81
17.22
33.05
6AL013
AE3007A1/
3
Type
3
(
reduced
emissions)
TF
4.81
17.22
33.05
6AL014
AE3007A1P
Type
1
TF
4.77
17.9
34.74
6AL015
AE3007A1P
Type
2
TF
4.77
17.9
34.74
6AL016
AE3007A1P
Type
3
(
reduced
emissions)
TF
4.77
17.9
34.74
6AL017
AE3007A3
Type
1
TF
4.72
17.2
33
6AL018
AE3007A3
Type
2
TF
4.72
17.2
33
6AL019
AE3007A3
Type
3
(
reduced
emissions)
TF
4.72
17.2
33
6AL020
AE3007A1E
Type
3
TF
4.72
19.06
37.16
6AL021
AE3007C
Type
1
TF
5.2
15.8
29.62
6AL022
AE3007C
Type
2
TF
5.2
15.8
29.62
6AL023
AE3007C1
Type
1
TF
5.1
16.58
31.46
6AL024
AE3007C1
Type
2
TF
5.1
16.58
31.46
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
H
I
J
K
L
M
N
O
P
Q
R
S
T
U
UID
Data
Superseded
Data
No
PR
C
R
superseded
by
NME
DTEPS
Other
Corr
as
Out
of
Date
Out
of
Date
UID
No
Annex
16
Production
Service
1AS001
x
­
­
­
­
x
­
­
­
x
­
­
­

1AS002
x
­
­
­
­
x
­
­
­
x
­
­
­

4AL003
­
x
­
­
­
­
x
­
x
­
­
­
­

4AL002
­
x
­
x
­
­
x
­
x
­
­
­
­

3AL001
­
x
­
x
­
­
x
­
x
­
­
­
­

6AL004
­
x
­
x
6AL023
­
x
­
x
­
­
­
­

6AL005
­
­
x
­
­
­
x
­
x
­
­
­
­

6AL006
­
x
­
­
­
­
x
­
x
­
­
­
­

6AL007
­
x
­
­
­
­
x
­
x
­
­
­
­

6AL008
­
x
­
­
­
­
x
­
x
­
­
­
­

6AL009
­
x
­
­
­
­
x
­
x
­
­
­
­

6AL010
­
x
­
­
­
­
x
­
x
­
­
­
­

6AL011
­
x
­
­
­
­
x
­
x
­
­
­
­

6AL012
­
x
­
­
­
­
x
­
x
­
­
­
­

6AL013
­
x
­
­
­
­
x
­
x
­
­
­
­

6AL014
­
x
­
­
­
­
x
­
x
­
­
­
­

6AL015
­
x
­
­
­
­
x
­
x
­
­
­
­

6AL016
­
x
­
­
­
­
x
­
x
­
­
­
­

6AL017
­
x
­
­
­
­
x
­
x
­
­
­
­

6AL018
­
x
­
­
­
­
x
­
x
­
­
­
­

6AL019
­
x
­
­
­
­
x
­
x
­
­
­
­

6AL020
­
x
­
­
­
­
x
­
x
­
­
­
­

6AL021
­
x
­
­
­
­
x
­
x
­
­
­
­

6AL022
­
x
­
­
­
­
x
­
x
­
­
­
­

6AL023
­
x
­
­
­
­
x
­
x
­
­
­
­

6AL024
­
x
­
­
­
­
x
­
x
­
­
­
­

­­­­­­­­
Data
Status­­­­­­­­
­­­­­­­­­­
Current
Engine
Status
­­­­­­­­­­

­­­­­­
Test
Engine
Status­­­­­­

Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
V
W
X
Y
Z
AA
AB
AC
AD
AE
AF
AG
AH
UID
Characteristic
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
%
of
Total
mass
Reg
limit
(
g)

1AS001
0.114
0.128
4.26
20.04
3
3
53.4
­
50­
58
62.3
317.8
823
1AS002
0.062
0.072
1.41
9.04
4
4
24.0
­
19­
25
27.4
139.7
393
4AL003
0.25
0.29
0.64
2.51
3
2
6.65
­
­
8.7
44.1
226
4AL002
0.26
0.30
0.72
3.10
3
2
8.33
­
­
10.8
55.3
279
3AL001
0.29
0.33
0.83
5.84
3
2
13.46
­
­
17.5
89.3
387
6AL004
0.24
0.28
0.66
4.84
3
2
10.95
­
­
14.25
55.9
346
6AL005
0.221
0.257
0.655
3.818
3
2
8.78
­
­
11.42
58.3
307
6AL006
0
0
0.18
5.04
3
1
10.51
­
­
16.19
82.6
367
6AL007
0.03
0.03
0.03
3.85
3
1
8.01
­
­
12.34
63.0
279
6AL008
0.222
0.258
0.658
3.92
3
2
9.01
­
­
11.72
59.8
313
6AL009
0
0
0.18
5.1
3
1
10.67
­
­
16.43
83.8
370
6AL010
0.03
0.03
0.03
3.88
3
1
8.08
­
­
12.44
63.5
280
6AL011
0.233
0.269
0.689
4.64
3
2
10.8
­
­
14.05
71.7
357
6AL012
0
0
0.21
5.23
3
1
11.25
­
­
17.33
88.4
372
6AL013
0.03
0.03
0.03
3.81
3
1
8.15
­
­
12.55
64.0
269
6AL014
0.222
0.258
0.658
3.85
3
2
8.88
­
­
11.55
58.9
308
6AL015
0
0
0.19
5.06
3
1
10.61
­
­
16.34
83.4
368
6AL016
0.03
0.03
0.03
3.86
3
1
8.06
­
­
12.41
63.3
280
6AL017
0.233
0.27
0.69
4.705
3
2
10.93
­
­
14.22
72.6
361
6AL018
0
0
0.23
5.65
3
1
12.14
­
­
18.7
95.4
401
6AL019
0.03
0.03
0.03
4.1
3
1
8.75
­
­
13.48
68.8
289
6AL020
0.03
0.03
0.03
3.52
3
1
7.1
­
­
10.93
55.8
264
6AL021
0.254
0.291
0.696
4.953
3
2
10.79
­
­
14.04
71.6
320
6AL022
0
0.01
0.23
5.75
3
1
11.59
­
­
17.85
91.1
344
6AL023
0.24
0.277
0.661
4.837
3
2
10.95
­
­
14.25
72.7
344
6AL024
0
0.01
0.21
5.88
3
1
12.36
­
­
19.04
97.1
389
­­­­­­­­­­­­­­­­
EI
HC­­­­­­­­­­­­­­
­­­
Number
­­­
­­­­­­­­­­­­­­­
Dp/
Foo
(
HC)­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­
­­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­­­­­

Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
AI
AJ
AK
AL
AM
AN
AO
AP
AQ
AR
AS
AT
AU
UID
Characteristic
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
%
of
Total
mass
Reg
limit
(
g)

1AS001
1.394
2.03
22.38
58.6
3
3
169.4
­
161­
177
183.2
155.3
2612
1AS002
1.13
1.62
15.56
47.7
4
4
137.7
­
133­
147
147.3
124.8
2254
4AL003
0.75
0.92
3.28
17.35
3
2
43.15
­
­
49.2
41.7
1468
4AL002
0.79
0.97
3.80
22.43
3
2
57.03
­
­
65.0
55.1
1910
3AL001
0.97
1.19
4.5
29.88
3
2
68
­
­
77.5
65.7
1964
6AL004
0.87
1.07
3.96
26.04
3
2
58.61
­
­
66.78
56.6
1850
6AL005
0.77
0.96
3.91
23.73
3
2
53.38
­
­
60.82
51.5
1865
6AL006
0.12
0.01
1.36
32.59
3
1
68.2
­
­
83.71
70.9
2383
6AL007
0.75
0.56
6.72
39.91
3
1
88.38
­
­
108.48
91.9
3088
6AL008
0.77
0.97
3.93
23.95
3
2
53.94
­
­
61.46
52.1
1874
6AL009
0
0
1.4
32.84
3
1
68.8
­
­
84.45
71.6
2389
6AL010
0.74
0.55
6.8
40.07
3
1
88.9
­
­
109.12
92.5
3088
6AL011
0.83
1.03
4.21
25.58
3
2
59.1
­
­
67.34
57.1
1954
6AL012
0
0
1.83
32.4
3
1
70.08
­
­
86.02
72.9
2317
6AL013
0.5
0.5
7.62
38.47
3
1
88.3
­
­
108.38
91.8
2919
6AL014
0.77
0.97
3.93
23.8
3
2
53.75
­
­
61.24
51.9
1867
6AL015
0
0
1.51
32.68
3
1
68.7
­
­
84.33
71.5
2386
6AL016
0.74
0.55
6.79
39.97
3
1
88.88
­
­
109.1
92.5
3087
6AL017
0.83
1.03
4.22
25.73
3
2
59.41
­
­
67.69
57.4
1960
6AL018
0
0
2
34.86
3
1
75.39
­
­
92.54
78.4
2488
6AL019
0.5
0.5
7.65
41.29
3
1
94.25
­
­
115.69
98.0
3111
6AL020
0.77
0.64
5.63
37.97
3
1
81.18
­
­
99.64
84.4
3018
6AL021
0.94
1.16
4.28
26.32
3
2
57.18
­
­
65.15
55.2
1695
6AL022
0
0
2.02
35.07
3
1
71.08
­
­
87.25
73.9
2108
6AL023
0.87
1.07
3.96
26.04
3
2
58.61
­
­
66.78
56.6
1842
6AL024
0
0
1.62
36.04
3
1
76
­
­
93.29
79.1
2389
­­­­­­­­­­­­­­­­­
EI
CO­­­­­­­­­­­­­­­­­
­­­­­­
Number­­­­­
­­­­­­­­­­­­­­­
Dp/
Foo
(
CO)­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­­­

Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
AV
AW
AX
AY
AZ
BA
BB
BC
BD
BE
BF
BG
BH
BI
BJ
UID
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
Original
CAEP
2
CAEP
4
Total
mass
(
g)

1AS001
15.25
13.08
5.90
2.82
3
3
40.5
­
39­
43
42.9
63.3
79.1
75.8
630
1AS002
19.15
16.02
6.92
3.72
4
4
51.4
­
47­
55
54.0
78.7
98.4
94.7
845
4AL003
20.54
17.47
7.79
3.83
3
2
46.30
­
­
50.9
66.8
83.6
85.6
1563
4AL002
19.78
16.84
7.22
3.52
3
2
44.61
­
­
49.1
64.9
81.1
83.1
1502
3AL001
16.92
14.56
6.63
3.24
3
2
34.73
­
­
38.2
52.8
66.0
66.4
991
6AL004
17.90
15.35
7.05
3.37
3
2
37.36
­
­
41.08
56.1
70.2
71.3
1175
6AL005
19.66
16.63
7.1
3.47
3
2
41.71
­
­
45.87
60.4
75.5
77.6
1456
6AL006
22.41
19.58
7.2
3.19
3
1
46.02
­
­
53.34
70.2
87.8
90.3
1607
6AL007
16.17
14.07
7.13
4.17
3
1
38.49
­
­
44.62
58.8
73.4
75.5
1344
6AL008
19.57
16.55
7.07
3.46
3
2
41.53
­
­
45.67
60.3
75.3
77.4
1442
6AL009
22.31
19.49
7.16
3.19
3
1
45.84
­
­
53.14
70.1
87.6
90.1
1592
6AL010
16.10
14.01
7.12
4.17
3
1
38.38
­
­
44.49
58.7
73.4
75.4
1333
6AL011
18.55
15.81
6.83
3.39
3
2
39.93
­
­
43.91
59.0
73.7
75.4
1319
6AL012
21.26
18.62
6.84
3.29
3
1
44.34
­
­
51.4
69.0
86.3
88.2
1465
6AL013
15.42
13.49
6.93
4.27
3
1
37.66
­
­
43.65
58.6
73.3
74.9
1245
6AL014
19.57
16.56
7.07
3.47
3
2
41.57
­
­
45.71
60.3
75.4
77.9
1444
6AL015
22.02
19.16
6.89
3.19
3
1
45.12
­
­
52.3
69.0
86.2
88.3
1567
6AL016
16.10
14.01
7.12
4.17
3
1
38.41
­
­
44.52
58.7
73.4
75.2
1334
6AL017
18.52
15.79
6.83
3.38
3
2
39.87
­
­
43.84
58.9
73.7
75.3
1316
6AL018
20.93
18.27
6.56
3.18
3
1
43.31
­
­
50.2
67.5
84.3
86.2
1429
6AL019
15.40
13.48
6.93
4.12
3
1
37.32
­
­
43.26
58.1
72.7
74.3
1232
6AL020
17.17
14.91
7.42
4.26
3
1
40.38
­
­
46.81
59.9
74.9
77.6
1501
6AL021
16.88
14.57
6.78
3.36
3
2
35.47
­
­
39
54.5
68.1
68.8
1050
6AL022
19.36
17.01
6.62
3.2
3
1
38.83
­
­
45.01
62.9
78.6
79.4
1150
6AL023
17.90
15.35
7.05
3.37
3
2
37.36
­
­
41.08
56.2
70.2
71.4
1175
6AL024
20.20
17.6
6.71
3.14
3
1
40.16
­
­
46.55
63.6
79.5
80.9
1262
­­­­
Number­­­­­

­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­
EI
NOx­­­­­­­­­­­­­­
­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­
Dp/
Foo
(
NOx)­­­­­­­­­­­­­­
Characteristic
as
%
of
standards
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
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aviation_
emissions_
databank
Data
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3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
BK
BL
BM
BN
BO
BP
BQ
BR
BS
BT
BU
BV
UID
Characteristic
No
T/
O
C/
O
App
Idle
Test
Eng
Max
Sigma
Range
Characteristic
%
of
Reg
limit
1AS001
­
­
­
­
­
­
­
­
­
­
­

1AS002
­
­
­
­
­
­
­
­
­
­
­

4AL003
1
0
0
0
3
2
1
­
­
1.2
3.7
4AL002
1
0
0
0
3
2
1
­
­
1.2
3.7
3AL001
1
0
0
0
3
2
1
­
­
1.2
3.6
6AL004
1.00
0.00
0.00
0.00
3
2
1.00
­
­
1.17
3.6
6AL005
1.00
0.01
0.01
0.01
3
2
1.00
­
­
1.17
3.7
6AL006
0.01
0.01
0.01
0.01
3
1
0.01
­
­
0.01
0.0
6AL007
0.01
0.01
0.01
0.01
3
1
0.01
­
­
0.01
0.0
6AL008
1.00
0.01
0.01
0.01
3
2
1.00
­
­
1.17
3.7
6AL009
0.01
0.01
0.01
0.01
3
1
0.01
­
­
0.01
0.0
6AL010
0.01
0.01
0.01
0.01
3
1
0.01
­
­
0.01
0.0
6AL011
1.00
0.01
0.01
0.01
3
2
1.00
­
­
1.17
3.6
6AL012
0.01
0.01
0.01
0.01
3
1
0.01
­
­
0.01
0.0
6AL013
0.01
0.01
0.01
0.01
3
1
0.01
­
­
0.01
0.0
6AL014
1.00
0.01
0.01
0.01
3
2
1.00
­
­
1.17
3.7
6AL015
0.01
0.01
0.01
0.01
3
1
0.01
­
­
0.01
0.0
6AL016
0.01
0.01
0.01
0.01
3
1
0.01
­
­
0.01
0.0
6AL017
1.00
0.01
0.01
0.01
3
2
1.00
­
­
1.17
3.6
6AL018
0.01
0.01
0.01
0.01
3
1
0.01
­
­
0.01
0.0
6AL019
<.
01
<.
01
<.
01
<.
01
3
1
<.
01
­
­
0.01
0.0
6AL020
0.01
0.01
0.01
0.01
3
1
0.01
­
­
0.01
0.0
6AL021
1.00
0.01
0.01
0.01
3
2
0.00
­
­
1.17
3.5
6AL022
0.01
0.01
0.01
0.01
3
1
0.01
­
­
0.01
0.0
6AL023
1.00
0.01
0.01
0.01
3
2
1.00
­
­
1.17
3.6
6AL024
0.01
0.01
0.01
0.01
3
1
0.01
­
­
0.01
0.0
­­­­­­­­­­­­­­
Smoke
Number­­­­­­­­­­­­­

­­­­­­­­­­­­­
Smoke
Number­­­­­­­­­­­­­
­­­­
Number­­­­

Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
BW
BX
BY
BZ
CA
CB
CC
CD
CE
UID
Fuel
per
No
Spec
H/
C
Arom
T/
O
C/
O
App
Idle
LTO
cycle
Ratio
%
(
kg)

1AS001
ASTM
D1655­
73T
­
17
0.205
0.173
0.067
0.024
85
1AS002
ASTM
D1655­
73T
­
17
0.225
0.186
0.072
0.026
92
4AL003
Jet
A/
JP­
8
1.899
16.5
0.377
0.315
0.117
0.049
162
4AL002
Jet
A/
JP­
8
1.899
16.5
0.380
0.319
0.117
0.050
164
3AL001
Jet­
A/
JP­
8
1.899
16.5
0.28
0.234
0.091
0.039
125
6AL004
Jet
A
/
JP8
1.899
16.5
0.322
0.269
0.099
0.042
138
6AL005
Jet
A
1.9
16
­
20
0.3826
0.318
0.113
0.0461
157
6AL006
Jet
A
1.9
16
­
20
0.3826
0.318
0.113
0.0461
157
6AL007
Jet
A
1.9
16
­
20
0.3826
0.318
0.113
0.0461
157
6AL008
Jet
A
1.9
16
­
20
0.3805
0.3163
0.1125
0.0459
156
6AL009
Jet
A
1.9
16
­
20
0.3805
0.3163
0.1125
0.0459
156
6AL010
Jet
A
1.9
16
­
20
0.3805
0.3163
0.1125
0.0459
156
6AL011
Jet
A
1.9
16
­
20
0.3589
0.2999
0.1077
0.0449
151
6AL012
Jet
A
1.9
16
­
20
0.3589
0.2999
0.1077
0.0449
151
6AL013
Jet
A
1.9
16
­
20
0.3589
0.2999
0.1077
0.0449
151
6AL014
Jet
A
1.9
16
­
20
0.3806
0.3163
0.1126
0.046
157
6AL015
Jet
A
1.9
16
­
20
0.3806
0.3163
0.1126
0.046
157
6AL016
Jet
A
1.9
16
­
20
0.3806
0.3163
0.1126
0.046
157
6AL017
Jet
A
1.9
16
­
20
0.3583
0.2995
0.1076
0.0448
150
6AL018
Jet
A
1.9
16
­
20
0.3583
0.2995
0.1076
0.0448
150
6AL019
Jet
A
1.9
16
­
20
0.3583
0.2995
0.1076
0.0448
150
6AL020
Jet
A
1.9
16
­
20
0.4122
0.3425
0.12
0.0475
165
6AL021
Jet
A
1.9
16
­
20
0.301
0.2527
0.0943
0.0377
127
6AL022
Jet
A
1.9
16
­
20
0.301
0.2527
0.0943
0.0377
127
6AL023
Jet
A
1.9
16
­
20
0.3222
0.2689
0.0991
0.0418
138
6AL024
Jet
A
1.9
16
­
20
0.3222
0.2689
0.0991
0.0418
138
­­­­­­­­­­­­­­­­­
Fuel
Flow­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­(
kg/
sec)­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­­­­­
Fuel­­­­­­­­­­­­­­­­­­­­­­­

Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
CF
CG
CH
CI
CJ
CK
CL
CM
UID
No
Baro
Temp
Humidity
kW
@
Power
%
CF
@
Power
kPa
K
kg/
kg
1AS001
0
­
0
­
96.7­
98.1
285
­
288
.0066­.
0087
1AS002
0
­
0
­
97.0­
97.3
294
­
313
.0039­.
0073
4AL003
0
­
0
­
101.3
288
0.0063
4AL002
0
­
0
­
101.3
288
0.0063
3AL001
0
­
0
­
101.3
288
0.0063
6AL004
0
­
0
­
101.3
288
0.0063
6AL005
0
­
0
­

6AL006
0
­
0
­
99.6
­
99.7
297
­
301
0.0115
­
0.0141
6AL007
0
­
0
­
98.9
­
99.0
291
­
301
0.009
­
0.012
6AL008
0
­
0
­

6AL009
0
­
0
­
99.6
­
99.7
297
­
301
0.0115
­
0.0141
6AL010
0
­
0
­
98.9
­
99.0
291
­
301
0.009
­
0.012
6AL011
0
­
0
­

6AL012
0
­
0
­
99.6
­
99.7
297
­
301
0.0115
­
0.0141
6AL013
0
­
0
­
98.9
­
99.0
291
­
301
0.009
­
0.012
6AL014
0
­
0
­

6AL015
0
­
0
­
99.6
­
99.7
297
­
301
0.0115
­
0.0141
6AL016
0
­
0
­
98.9
­
99.0
291
­
301
0.009
­
0.012
6AL017
0
­
0
­

6AL018
0
­
0
­
99.6
­
99.7
297
­
301
0.0115
­
0.0141
6AL019
0
­
0
­
98.9
­
99.0
291
­
301
0.009
­
0.012
6AL020
0
­
0
­
98.9
­
99.0
291
­
301
0.009
­
0.012
6AL021
0
­
0
­

6AL022
0
­
0
­
99.6
­
99.7
297
­
301
0.0115
­
0.0141
6AL023
0
­
0
­

6AL024
0
­
0
­
99.6
­
99.7
297
­
301
0.0115
­
0.0141
­­­­­­­­­­­­­­­­­­­
Ambient­­­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­
Loads­­­­­­­­­­­­­­­­­­­

Power
Extraction
­­­
Stage
Bleed­­­

Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
CN
CO
CP
CQ
CR
CS
UID
­­­
Test
Dates­­­

No
Manufacturer
Test
Organisation
Test
Location
From
To
1AS001
Allied
Signal
Allied
Signal
Phoenix
Dec­
75
Apr­
76
1AS002
Allied
Signal
Allied
Signal
Phoenix
Feb­
76
Aug­
76
4AL003
Allison
Engine
Company
Allison
Engine
Company
Indianapolis,
Indiana,
USA
3­
Mar­
94
19­
Apr­
95
4AL002
Allison
Engine
Company
Allison
Engine
Company
Indianapolis,
Indiana,
USA
3­
Mar­
94
19­
Apr­
95
3AL001
Allison
Engine
Company
Allison
Engine
Company
Indianapolis,
Indiana,
USA
3­
Mar­
94
19­
Apr­
95
6AL004
Rolls­
Royce
Corporation
Rolls­
Royce
Corporation
Indianapolis,
Indiana,
USA
3­
Mar­
94
19­
Apr­
95
6AL005
Rolls­
Royce
Corporation
Rolls­
Royce
Corporation
Indianapolis,
Indiana,
USA
3­
Mar­
94
19­
Apr­
95
6AL006
Rolls­
Royce
Corporation
Rolls­
Royce
Corporation
Indianapolis,
Indiana,
USA
28­
Aug­
02
29­
Aug­
02
6AL007
Rolls­
Royce
Corporation
Rolls­
Royce
Corporation
Indianapolis,
Indiana,
USA
9­
Jun­
01
11­
Jun­
01
6AL008
Rolls­
Royce
Corporation
Rolls­
Royce
Corporation
Indianapolis,
Indiana,
USA
3­
Mar­
94
19­
Apr­
95
6AL009
Rolls­
Royce
Corporation
Rolls­
Royce
Corporation
Indianapolis,
Indiana,
USA
28­
Aug­
02
29­
Aug­
02
6AL010
Rolls­
Royce
Corporation
Rolls­
Royce
Corporation
Indianapolis,
Indiana,
USA
9­
Jun­
01
11­
Jun­
01
6AL011
Rolls­
Royce
Corporation
Rolls­
Royce
Corporation
Indianapolis,
Indiana,
USA
3­
Mar­
94
19­
Apr­
95
6AL012
Rolls­
Royce
Corporation
Rolls­
Royce
Corporation
Indianapolis,
Indiana,
USA
28­
Aug­
02
29­
Aug­
02
6AL013
Rolls­
Royce
Corporation
Rolls­
Royce
Corporation
Indianapolis,
Indiana,
USA
9­
Jun­
01
11­
Jun­
01
6AL014
Rolls­
Royce
Corporation
Rolls­
Royce
Corporation
Indianapolis,
Indiana,
USA
3­
Mar­
94
19­
Apr­
95
6AL015
Rolls­
Royce
Corporation
Rolls­
Royce
Corporation
Indianapolis,
Indiana,
USA
28­
Aug­
02
29­
Aug­
02
6AL016
Rolls­
Royce
Corporation
Rolls­
Royce
Corporation
Indianapolis,
Indiana,
USA
9­
Jun­
01
11­
Jun­
01
6AL017
Rolls­
Royce
Corporation
Rolls­
Royce
Corporation
Indianapolis,
Indiana,
USA
3­
Mar­
94
19­
Apr­
95
6AL018
Rolls­
Royce
Corporation
Rolls­
Royce
Corporation
Indianapolis,
Indiana,
USA
28­
Aug­
02
29­
Aug­
02
6AL019
Rolls­
Royce
Corporation
Rolls­
Royce
Corporation
Indianapolis,
Indiana,
USA
9­
Jun­
01
11­
Jun­
01
6AL020
Rolls­
Royce
Corporation
Rolls­
Royce
Corporation
Indianapolis,
Indiana,
USA
9­
Jun­
01
11­
Jun­
01
6AL021
Rolls­
Royce
Corporation
Rolls­
Royce
Corporation
Indianapolis,
Indiana,
USA
3­
Mar­
94
19­
Apr­
95
6AL022
Rolls­
Royce
Corporation
Rolls­
Royce
Corporation
Indianapolis,
Indiana,
USA
28­
Aug­
02
29­
Aug­
02
6AL023
Rolls­
Royce
Corporation
Rolls­
Royce
Corporation
Indianapolis,
Indiana,
USA
3­
Mar­
94
19­
Apr­
95
6AL024
Rolls­
Royce
Corporation
Rolls­
Royce
Corporation
Indianapolis,
Indiana,
USA
28­
Aug­
02
29­
Aug­
02
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
CT
CU
UID
No
Remarks
1AS001
Not
required
to
meet
GASEOUS
regulations
1AS002
Not
required
to
meet
GASEOUS
regulations
4AL003
4AL002
For
AE3007A1,
A1/
1,
A1/
2
3AL001
6AL004
Results
based
on
Rolls
Royce
report
EDR
15171B
6AL005
1.
For
effectivity
see
Rolls­
Royce
Notice
to
Operators
No.
AE3007A­
076
2.
Results
are
based
on
Rolls­
Royce
report
EDR
15171B
3.
AE3007A1
data
i
6AL006
1.
For
effectivity
see
Rolls­
Royce
Notice
to
Operators
No.
AE3007A­
076
2.
Data
in
this
form
for
AE3007A1
egines
fitted
with
PAB
fuel
nozzles
3.
Resu
6AL007
1.
For
effectivity
see
Rolls­
Royce
Notice
to
Operators
No.
AE3007A­
076
2.
Data
in
this
form
for
AE3007A1
engine
fitted
with
reduced
emissions
comb
6AL008
1.
For
effectivity
see
Rolls­
Royce
Notice
to
Operators
No.
AE3007A­
076
2.
Results
based
on
Rolls­
Royce
report
EDR
15171B
6AL009
1.
For
effectivity
see
Rolls­
Royce
Notice
to
Operators
No.
AE3007A­
076
2.
Data
in
this
form
for
A3007A1/
1
fitted
with
PAB
fuel
nozzles
3.
Results
bas
6AL010
1.
For
effectivity
see
Rolls­
Royce
Notice
to
Operators
No.
AE3007A­
076
2.
Data
in
this
form
for
AE3007A1/
1
engine
fitted
with
reduced
emissions
com
6AL011
1.
For
effectivity
see
Rolls­
Royce
Notice
to
Operators
No.
AE3007A­
076
2.
Results
based
on
Rolls­
Royce
report
EDR
15171B
6AL012
1.
For
effectivity
see
Rolls­
Royce
Notice
to
Operators
No.
AE3007A­
076
2.
Data
in
this
form
for
AE3007A1/
3
engine
fitted
with
PAB
fuel
nozzles
3.
Re
6AL013
1.
For
effectivity
see
Rolls­
Royce
Notice
to
Operators
No.
AE3007A­
076
2.
Data
in
this
form
for
AE3007A1/
3
engine
fitted
with
reduced
emissions
com
6AL014
1.
For
effectivity
see
Rolls­
Royce
Notice
to
Operators
No.
AE3007A­
076
2.
Results
based
on
Rolls­
Royce
report
EDR
15171B
6AL015
1.
For
effectivity
see
Rolls­
Royce
Notice
to
Operators
No.
AE3007A­
076
2.
Data
in
this
form
for
AE3007A1P
engine
fitted
with
PAB
fuel
nozzles
3.
Re
6AL016
1.
For
effectivity
see
Rolls­
Royce
Notice
to
Operators
No.
AE3007A­
076
2.
Data
in
this
form
for
AE3007A1P
engine
fitted
with
reduced
emissions
com
6AL017
1.
For
effectivity
see
Rolls­
Royce
Notice
to
Operators
No.
AE3007A­
076
2.
Results
based
on
Rolls­
Royce
report
EDR
15171B
6AL018
1.
For
effectivity
see
Rolls­
Royce
Notice
to
Operators
No.
AE3007A­
076
2.
Data
in
this
form
for
AE3007A3
engine
fitted
with
PAB
fuel
nozzles
3.
Resu
6AL019
1.
For
effectivity
see
Rolls­
Royce
Notice
to
Operators
No.
AE3007A­
076
2.
Data
in
this
form
for
AE3007A3
engine
fitted
with
reduced
emissions
comb
6AL020
1.
For
effectivity
see
Rolls­
Royce
Notice
to
Operators
No.
AE3007A­
076
2.
Data
in
this
form
for
AE3007A1E
engine
fitted
with
reduced
emissions
com
6AL021
1.
For
effectivity
see
Rolls­
Royce
Notice
to
Operators
No.
AE3007A­
076
2.
Results
based
on
Rolls­
Royce
report
EDR
15171B
6AL022
1.
For
effectivity
see
Rolls­
Royce
Notice
to
Operators
No.
AE3007A­
076
2.
Data
in
this
form
for
AE3007C
engine
fitted
with
PAB
fuel
nozzles
3.
Resul
6AL023
1.
For
effectivity
see
Rolls­
Royce
Notice
to
Operators
No.
AE3007A­
076
2.
Results
based
of
Rolls­
Royce
report
EDR
15171B
6AL024
1.
For
effectivity
see
Rolls­
Royce
Notice
to
Operators
No.
AE3007A­
076
2.
Data
in
this
form
for
AE3007C1
engine
fitted
with
PAB
fuel
nozzles
3.
Resu
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
CV
CW
CX
CY
CZ
DA
DB
DC
DD
DE
DF
DG
DH
a
in
this
report
replace
data
reported
in
ICAO
databank
under
ID
No.
4AL002,
Rev
9
sults
based
on
Rolls­
Royce
report
EDR
19972
bustor
and
PAB
fuel
nozzles
3.
Results
based
on
Rolls­
Royce
report
EDR
19587
ased
on
Rolls­
Royce
report
EDR
19972
mbustor
&
PAB
fuel
nozzles
3.
Results
based
on
Rolls­
Royce
report
EDR
19587
Results
based
on
Rolls­
Royce
report
EDR
19972
mbustor
&
PAB
fuel
nozzles
3.
Results
based
on
Rolls­
Royce
report
EDR
19587
esults
based
on
Roll­
Royce
report
EDR
19972
mbustor
&
PAB
fuel
nozzles
3.
Results
based
on
Rolls­
Royce
report
EDR
19587
sults
based
on
Rolls­
Royce
report
EDR
19972
bustor
&
PAB
fuel
nozzles
3.
Results
based
on
Rolls­
Royce
report
EDR
19587
mbustor
&
PAB
fuel
nozzles
3.
Results
based
on
Rolls­
Royce
report
EDR
19587
ults
based
on
Rolls­
Royce
report
EDR
19972
sults
based
on
Rolls­
Royce
report
EDR
19972
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
DI
DJ
DK
DL
DM
DN
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
A
B
C
D
E
F
G
UID
Engine
Combustor
Eng
B/
P
Press
Rated
No
Identification
Description
Type
Ratio
Ratio
Output
kN
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
AO
'
Aviadgatel'

1AA001
D­
30
(
Il
series)
MTF
0.85
18.4
66.64
1AA002
D­
30KP­
2
MTF
2.2
19.45
117.6
1AA003
D­
30KU
MTF
2.35
17.4
112.7
1AA004
D­
30KU­
154
MTF
2.3
17
107.5
1AA005
PS­
90A
MTF
5
30.85
156.9
BMW
Roll­
Royce
3BR001
BR700­
710A1­
10
TF
4.2
24.31
65.61
4BR008
BR700­
710A1­
10
TF
4.20
24.23
65.61
4BR009
BR700­
710A2­
20
TF
4.19
24.16
65.61
6BR010
BR700­
710­
C4­
11
Annular
TF
4.05
24.95
68.77
4BR002
BR700­
715A1­
30
TF
4.66
28.98
84.16
4BR005
BR700­
715A1­
30
Improved
fuel
injector
TF
4.68
28.75
83.23
4BR003
BR700­
715B1­
30
TF
4.60
30.47
89.68
4BR006
BR700­
715B1­
30
Improved
fuel
injector
TF
4.60
30.58
89.68
4BR004
BR700­
715C1­
30
TF
4.55
32.01
95.33
4BR007
BR700­
715C1­
30
Improved
fuel
injector
TF
4.54
32.15
95.33
CFM
International
1CM001
CFM56­
2A
series
TF
6
25.2
106.76
1CM002
CFM56­
2B­
1
TF
6
23.5
97.86
1CM003
CFM56­
2­
C5
TF
6
23.5
97.86
1CM004
CFM56­
3­
B1
TF
5.1
22.44
89.41
1CM005
CFM56­
3B­
2
TF
5.1
24.10
98.30
1CM006
CFM56­
3C­
1
(
Rerated)
TF
5.1
21.3
82.29
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
H
I
J
K
L
M
N
O
P
Q
R
S
T
U
UID
Data
Superseded
Data
No
PR
C
R
superseded
by
NME
DTEPS
Other
Corr
as
Out
of
Date
Out
of
Date
UID
No
Annex
16
Production
Service
­­­­­­­­
Data
Status­­­­­­­­
­­­­­­­­­­
Current
Engine
Status
­­­­­­­­­­

­­­­­­
Test
Engine
Status­­­­­­

36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
1AA001
­
­
x
­
­
­
­
x
­
x
­
­
­

1AA002
­
­
x
­
­
­
­
x
­
x
­
­
­

1AA003
­
­
x
­
­
­
­
x
­
x
­
­
­

1AA004
­
­
x
­
­
­
­
x
­
x
­
­
­

1AA005
­
x
­
­
­
x
­
­
x
x
­
­
­

3BR001
­
x
­
­
­
­
x
­
x
x
­
­
­

4BR008
­
x
­
­
­
­
x
­
x
­
­
­
­

4BR009
­
x
­
­
­
­
x
­
x
­
­
­
­

6BR010
­
x
­
­
­
­
x
­
x
­
­
­
­

4BR002
­
x
­
­
­
­
x
­
x
x
­
­
­

4BR005
­
x
­
­
­
­
x
­
x
­
­
­
­

4BR003
­
x
­
­
­
­
x
­
x
x
­
­
­

4BR006
­
x
­
­
­
­
x
­
x
­
­
­
­

4BR004
­
x
­
­
­
­
x
­
x
x
­
­
­

4BR007
­
x
­
­
­
­
x
­
x
­
­
­
­

1CM001
­
x
­
­
­
x
­
­
x
x
­
­
­

1CM002
­
x
­
­
­
x
­
­
x
x
­
­
­

1CM003
­
x
­
­
­
x
­
­
x
x
­
­
­

1CM004
­
­
x
­
­
x
­
­
x
x
­
­
­

1CM005
­
­
x
­
­
x
­
­
x
x
­
­
­

1CM006
­
­
x
­
­
x
­
­
x
x
­
­
­

Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
V
W
X
Y
Z
AA
AB
AC
AD
AE
AF
AG
AH
UID
Characteristic
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
%
of
Total
mass
Reg
limit
(
g)

­­­­­­­­­­­­­­­­
EI
HC­­­­­­­­­­­­­­
­­­
Number
­­­
­­­­­­­­­­­­­­­
Dp/
Foo
(
HC)­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­
­­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­­­­­

36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
1AA001
0.12
0.14
1.50
43.60
2
1
134.9
­
­
207.8
1060.0
8992
1AA002
0.7
0.8
2.7
13.3
7
4
41.4
8.6
­
47.2
241.0
4874
1AA003
0.3
0.4
1.2
10.5
5
5
33.3
6.55
­
37.4
191.0
3753
1AA004
0.4
0.5
1.9
12.7
2
2
40.8
5.0
­
53.1
270.9
4389
1AA005
0.12
0.12
0.20
0.30
3
1
0.9
­
­
1.4
7.1
138
3BR001
0
0.03
0.04
1.98
3
1
4.29
­
3.83­
5.03
6.6
33.7
279
4BR008
0.02
0.02
0.05
1.09
3
1
2.37
­
2.13­
2.63
3.7
18.6
156
4BR009
0.02
0.02
0.05
1.12
3
1
2.44
­
2.19­
2.70
3.8
19.2
160
6BR010
0.02
0.02
0.05
2.29
3
1
4.36
­
4.19
­
4.47
6.7
34.2
301
4BR002
0.00
0.02
0.01
0.21
3
1
0.39
­
0.32­
0.47
0.6
3.1
34
4BR005
0.05
0.06
0.02
0.11
3
1
0.32
­
0.03­
0.66
0.5
2.5
25
4BR003
0.00
0.01
0.00
0.17
3
1
0.30
­
0.24­
0.37
0.5
2.3
27
4BR006
0.03
0.06
0.02
0.07
3
1
0.23
­
0.03­
0.45
0.4
1.8
20
4BR004
0.00
0.00
0.00
0.14
3
1
0.23
­
0.17­
0.29
0.4
1.8
22
4BR007
0.01
0.06
0.02
0.06
3
1
0.18
­
0.02­
0.34
0.3
1.4
18
1CM001
0.04
0.04
0.08
1.13
3
1
2.26
0.41
1.82­
2.63
3.5
17.8
242
1CM002
0.04
0.05
0.08
1.83
3
1
3.87
0.41
3.40­
4.15
6.0
30.4
378
1CM003
0.04
0.05
0.08
1.83
3
1
3.87
0.41
3.40­
4.15
6.0
30.4
378
1CM004
0.04
0.05
0.08
2.28
3
1
4.67
0.53
4.17­
5.22
7.2
36.7
418
1CM005
0.036
0.047
0.073
1.75
3
1
3.44
0.37
3.01­
3.67
5.3
27.0
337
1CM006
0.05
0.05
0.08
2.86
3
1
6.18
1.05
5.47­
7.38
9.5
48.6
507
Filename
DCTM_
ARP.
xls
Printed
on
5/
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05
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website
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aviation_
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Data
1
2
3
AI
AJ
AK
AL
AM
AN
AO
AP
AQ
AR
AS
AT
AU
UID
Characteristic
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
%
of
Total
mass
Reg
limit
(
g)

­­­­­­­­­­­­­­­­­
EI
CO­­­­­­­­­­­­­­­­­
­­­­­­
Number­­­­­
­­­­­­­­­­­­­­­
Dp/
Foo
(
CO)­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­­­

36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
1AA001
2.7
3.2
14.5
60.3
2
1
209.9
­
­
257.6
218.3
13989
1AA002
2.2
2.8
15.4
62.4
7
4
195.0
11.1
­
208.6
176.8
22932
1AA003
2.8
3.7
11.8
54.0
5
5
180.5
33.4
­
191.7
162.5
20341
1AA004
3.0
3.6
18.2
77.7
2
2
257.0
21.8
­
292.8
248.1
27627
1AA005
0.35
0.40
0.90
6.90
3
1
13.6
­
­
16.7
14.1
2123
3BR001
0.52
0.66
4.24
26.09
3
1
59.85
­
57.89­
63.69
73.5
62.3
3913
4BR008
1.04
0.93
4.78
27.82
3
1
64.26
­
63.75­
65.02
78.9
66.8
4212
4BR009
1.04
0.93
4.81
28.00
3
1
64.82
­
64.31­
65.59
79.6
67.4
4239
6BR010
1.04
0.92
4.92
31.57
3
1
64.37
­
63.78­
64.19
79.0
67.0
4449
4BR002
0.78
0.75
3.76
16.27
3
1
32.64
­
31.93­
33.86
40.1
33.9
2753
4BR005
0.66
0.63
4.05
19.72
3
1
40.83
­
40.21­
41.37
50.1
42.5
3390
4BR003
0.78
0.76
3.38
15.56
3
1
30.08
­
29.44­
31.21
36.9
31.3
2693
4BR006
0.72
0.63
3.59
18.60
3
1
36.85
­
36.28­
37.42
45.2
38.3
3300
4BR004
0.75
0.78
3.06
14.86
3
1
27.77
­
27.22­
28.85
34.1
28.9
2655
4BR007
0.80
0.64
3.23
17.85
3
1
34.04
­
33.51­
34.63
41.8
35.4
3236
1CM001
0.9
0.9
3.4
23.5
3
1
48.5
2.5
47.0­
51.4
59.5
50.5
5176
1CM002
0.9
0.9
4.2
30.7
3
1
67.2
4.1
63.5­
71.7
82.5
69.9
6578
1CM003
0.9
0.9
4.2
30.7
3
1
67.2
4.1
63.5­
71.7
82.5
69.9
6578
1CM004
0.9
0.95
3.8
34.4
3
1
72.9
5.1
68.5­
78.5
89.5
75.8
6517
1CM005
0.9
0.9
3.4
30.1
3
1
61.0
3.8
57.6­
65.1
74.9
63.5
5988
1CM006
0.9
1.0
4.2
38.1
3
1
85.2
6.4
79.7­
92.2
104.6
88.6
7002
Filename
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ARP.
xls
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Data
1
2
3
AV
AW
AX
AY
AZ
BA
BB
BC
BD
BE
BF
BG
BH
BI
BJ
UID
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
Original
CAEP
2
CAEP
4
Total
mass
(
g)

­­­­
Number­­­­­

­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­
EI
NOx­­­­­­­­­­­­­­
­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­
Dp/
Foo
(
NOx)­­­­­­­­­­­­­­
Characteristic
as
%
of
standards
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
1AA001
19.1
16.3
7.0
3.6
2
1
65.1
­
­
75.5
98.3
122.8
141.9
4338
1AA002
16.5
13.5
6.3
3.3
7
4
47.1
6.6
­
49.5
62.7
78.4
98.8
5510
1AA003
16.3
12.6
5.1
2.7
5
5
41.9
3.15
­
43.8
58.6
73.2
93.5
4720
1AA004
14.5
11.6
5.1
2.9
2
2
36.7
2.5
­
40.4
54.5
68.2
87.4
4000
1AA005
37.0
31.5
11.8
5.8
3
1
74.2
­
­
86.0
84.6
105.7
125.2
11648
3BR001
17.07
13.93
8.20
4.00
3
1
39.32
­
38.09­
40.51
45.6
51.5
64.3
72.6
2576
4BR008
18.79
15.07
7.68
4.69
3
1
42.52
­
41.84­
42.94
49.3
55.7
69.7
78.6
2790
4BR009
18.73
15.03
7.67
4.67
3
1
42.49
­
41.81­
42.91
49.3
55.8
69.7
78.7
2784
6BR010
19.52
15.43
7.71
4.5
3
1
41.41
­
40.63­
41.90
48.0
53.4
66.7
76.0
2850
4BR002
23.97
18.65
11.19
5.37
3
1
47.54
­
47.19­
48.08
55.1
56.3
70.3
82.9
4002
4BR005
20.97
16.43
8.75
3.95
3
1
40.17
­
39.09­
41.16
46.6
47.8
59.7
70.3
3340
4BR003
27.21
20.34
11.38
5.54
3
1
51.10
­
50.79­
51.54
59.2
58.7
73.3
87.2
4583
4BR006
24.28
18.27
9.01
4.14
3
1
44.14
­
43.00­
45.23
51.2
50.6
63.2
75.1
3958
4BR004
31.39
22.41
11.55
5.72
3
1
55.71
­
55.26­
56.04
64.6
62.1
77.6
90.9
5314
4BR007
27.92
20.05
9.23
4.28
3
1
48.13
­
46.96­
49.29
55.8
53.5
66.9
78.2
4588
1CM001
20.4
17.3
8.7
4.3
3
1
42.8
0.8
42.3­
43.7
49.6
54.9
68.6
83.6
4571
1CM002
18.5
16.0
8.2
4.0
3
1
39.9
0.6
39.4­
40.5
46.3
53.2
66.5
81.7
3906
1CM003
18.5
16.0
8.2
4.0
3
1
39.9
0.6
39.4­
40.5
46.3
53.2
66.5
81.7
3906
1CM004
17.7
15.5
8.3
3.9
3
1
40.3
0.8
39.6­
41.2
46.7
55.0
68.8
85.1
3595
1CM005
19.4
16.7
8.7
4.1
3
1
42.9
0.81
42.4­
43.9
49.7
56.4
70.5
86.4
4213
1CM006
16.6
14.7
8.0
3.8
3
1
39.0
0.78
38.2­
40.0
45.2
54.7
68.4
82.9
3210
Filename
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ARP.
xls
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aviation_
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Data
1
2
3
BK
BL
BM
BN
BO
BP
BQ
BR
BS
BT
BU
BV
UID
Characteristic
No
T/
O
C/
O
App
Idle
Test
Eng
Max
Sigma
Range
Characteristic
%
of
Reg
limit
­­­­­­­­­­­­­­
Smoke
Number­­­­­­­­­­­­­

­­­­­­­­­­­­­
Smoke
Number­­­­­­­­­­­­­
­­­­
Number­­­­

36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
1AA001
33
35
27
8
1
1
35
­
­
45.1
170.3
1AA002
17.5
19.5
16.0
6.5
1
1
19.5
­
­
25.1
110.9
1AA003
­
­
­
­
1
1
22.9
­
­
29.5
128.7
1AA004
­
­
­
­
­
­
­
­
­
­
­

1AA005
­
­
­
­
3
1
13
­
­
16.7
80.0
3BR001
11.03
8.69
0
0.17
3
1
11.03
­
10.18­
11.87
14.2
53.4
4BR008
13.99
11.92
0.29
0.56
3
1
13.99
­
12.64­
15.18
18.0
67.8
4BR009
13.96
11.87
0.27
0.57
3
1
13.96
­
12.60­
15.15
18.0
67.6
6BR010
14.34
12.36
0.35
0.45
3
1
14.34
­
13.08­
14.37
18.46
70.4
4BR002
3.24
2.73
0.97
0.91
3
1
3.24
­
3.04­
3.40
4.2
16.8
4BR005
4.33
3.96
0.77
0.11
3
1
4.33
­
3.85­
4.74
5.6
22.4
4BR003
3.55
2.90
1.03
0.89
3
1
3.55
­
3.24­
3.80
4.6
18.9
4BR006
4.56
4.13
0.96
0.07
3
1
4.56
­
4.16­
5.00
5.9
24.1
4BR004
3.98
3.09
1.09
0.87
3
1
3.98
­
3.61­
4.26
5.1
21.3
4BR007
4.86
4.26
1.12
0.04
3
1
4.86
­
4.62­
5.28
6.3
26.1
1CM001
7.9
4.2
2.5
2.0
3
1
7.9
0.6
7.3­
8.5
10.2
43.7
1CM002
6.0
3.0
2.6
2.2
3
1
6.0
0.8
5.4­
6.9
7.7
32.4
1CM003
6.0
3.0
2.6
2.2
3
1
6.0
0.8
5.4­
6.9
7.7
32.4
1CM004
4.0
2.5
2.5
2.2
3
1
4.0
0.6
3.4­
4.5
5.1
21.1
1CM005
6.0
3.0
2.5
2.2
3
1
6.0
0.8
5.4­
6.9
7.7
32.5
1CM006
3.0
2.4
2.5
2.1
3
1
3.0
0.4
2.5­
3.2
3.9
15.5
Filename
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xls
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aviation_
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Data
1
2
3
BW
BX
BY
BZ
CA
CB
CC
CD
CE
UID
Fuel
per
No
Spec
H/
C
Arom
T/
O
C/
O
App
Idle
LTO
cycle
Ratio
%
(
kg)

­­­­­­­­­­­­­­­­­
Fuel
Flow­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­(
kg/
sec)­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­­­­­
Fuel­­­­­­­­­­­­­­­­­­­­­­­

36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
1AA001
TS­
1
2
19.3
1.150
0.975
0.350
0.130
464
1AA002
TS­
1
2
19
1.67
1.42
0.49
0.210
703
1AA003
TS­
1
2
18.6
1.520
1.300
0.500
0.215
691
1AA004
TS­
1
2
18
1.420
1.100
0.420
0.207
629
1AA005
TS­
1
2
19
1.739
1.431
0.489
0.178
657
3BR001
AVTUR
1.94
16.5
0.707
0.588
0.220
0.089
299
4BR008
AVTUR
1.89­
1.92
16.4­
18.0
0.713
0.594
0.214
0.089
299
4BR009
AVTUR
1.89­
1.92
16.4­
18.0
0.714
0.595
0.214
0.089
299
6BR010
AVTUR
1.89
16.4
­
18.0
0.747
0.617
0.215
0.083
294
4BR002
AVTUR
1.89
17.7
0.836
0.690
0.245
0.096
335
4BR005
AVTUR
1.93
16.6
0.831
0.686
0.240
0.100
339
4BR003
AVTUR
1.89
17.7
0.905
0.743
0.259
0.098
351
4BR006
AVTUR
1.93
16.6
0.910
0.750
0.257
0.103
360
4BR004
AVTUR
1.89
17.7
0.980
0.799
0.273
0.101
370
4BR007
AVTUR
1.93
16.6
0.984
0.805
0.272
0.105
377
1CM001
Jet
A
1.93
16.0
1.114
0.911
0.318
0.130
446
1CM002
Jet
A
1.93
16.0
0.985
0.819
0.311
0.128
424
1CM003
Jet
A
1.93
16.0
0.985
0.819
0.311
0.128
424
1CM004
Jet
A
1.93
16.0
0.946
0.792
0.290
0.114
392
1CM005
Jet
A
1.93
16.0
1.056
0.878
0.314
0.119
421
1CM006
Jet
A
1.93
16.0
0.872
0.732
0.273
0.111
372
Filename
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ARP.
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05
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aviation_
emissions_
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Data
1
2
3
CF
CG
CH
CI
CJ
CK
CL
CM
UID
No
Baro
Temp
Humidity
kW
@
Power
%
CF
@
Power
kPa
K
kg/
kg
­­­­­­­­­­­­­­­­­­­
Ambient­­­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­
Loads­­­­­­­­­­­­­­­­­­­

Power
Extraction
­­­
Stage
Bleed­­­

36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
1AA001
0
­
0
­
103
293
.01048
1AA002
0
­
0
­
102.7­
103.1
284
­
289
.00748
1AA003
0
­
0
­
102.6­
102.7
292
­
294
.00788
1AA004
0
­
0
­
102.3­
102.6
289
­
291
.01119
1AA005
0
­
0
­
102.9­
104
281
­
285
.00348­.
00607
3BR001
0
­
0
­
101.5­
102.1
291.2­
300.3
.0074­.
0087
4BR008
0
­
0
­
100.9­
101.2
282.9­
286.7
.0064­.
0087
4BR009
0
­
0
­
100.9­
101.2
282.9­
286.7
.0064­.
0087
6BR010
0
­
0
­
100.9
­
101.2
282.9
­
286.7
0.0064
­
0.0087
4BR002
0
­
0
­
101.3­
101.9
288.8­
294.4
0.0066­.
0079
4BR005
0
­
0
­
100.9­
101.3
294.4­
297.2
.0072­.
0075
4BR003
0
­
0
­
101.3­
101.9
288.8­
294.4
0.0066­.
0079
4BR006
0
­
0
­
100.9­
101.3
294.4­
297.2
.0072­.
0075
4BR004
0
­
0
­
101.3­
101.9
288.8­
294.4
0.0066­.
0079
4BR007
0
­
0
­
100.9­
101.3
294.4­
297.2
.0072­.
0075
1CM001
0
­
0
­
95.98­
97.49
279
­
286
.002­.
009
1CM002
0
­
0
­
95.98­
97.49
279
­
286
.002­.
009
1CM003
0
­
0
­
95.98­
97.49
279
­
286
.002­.
009
1CM004
0
­
0
­
95.98­
97.49
279
­
286
.002­.
009
1CM005
0
­
0
­
95.98­
97.49
279
­
286
.002­.
009
1CM006
0
­
0
­
95.98­
97.49
279
­
286
.002­.
009
Filename
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ARP.
xls
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05
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aviation_
emissions_
databank
Data
1
2
3
CN
CO
CP
CQ
CR
CS
UID
­­­
Test
Dates­­­

No
Manufacturer
Test
Organisation
Test
Location
From
To
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
1AA001
AO
'
Aviadgatel'
State
Inst
for
Civ
Aviation
Sheremetjevo,
Moscow
3­
Aug­
90
­

1AA002
AO
'
Aviadgatel'
State
Inst
for
Civ
Aviation
Sheremetjevo,
Moscow
28­
Jun­
90
­

1AA003
AO
'
Aviadgatel'
State
Inst
for
Civ
Aviation
Sheremetjevo,
Moscow
19­
Jul­
89
­

1AA004
AO
'
Aviadgatel'
State
Inst
for
Civ
Aviation
Sheremetjevo,
Moscow
4­
Jul­
89
­

1AA005
AO
'
Aviadgatel'
AO
'
Aviadgatel'
Perm
City
17­
Apr­
89
18­
Apr­
89
3BR001
BMW
Rolls­
Royce
GmbH
BMW
Rolls­
Royce
GmbH
BMW
Rolls­
Royce
GmbH,
Dahlewitz,
German
5­
Jun­
96
6­
Jun­
96
4BR008
BMW
Rolls­
Royce
GmbH
BMW
Rolls­
Royce
GmbH
BMW
Rolls­
Royce
GmbH,
Dahlewitz,
German
19­
Oct­
96
20­
Oct­
96
4BR009
BMW
Rolls­
Royce
GmbH
BMW
Rolls­
Royce
GmbH
BMW
Rolls­
Royce
GmbH,
Dahlewitz,
German
19­
Oct­
96
20­
Oct­
96
6BR010
Rolls­
Royce
Rolls­
Royce
Dahlewitz
19­
Oct­
96
20­
Oct­
96
4BR002
BMW
Rolls­
Royce
GmbH
BMW
Rolls­
Royce
GmbH
BMW
Rolls­
Royce
GmbH,
Dahlewitz,
German
7­
May­
98
8­
May­
98
4BR005
BMW
Rolls­
Royce
GmbH
BMW
Rolls­
Royce
GmbH
BMW
Rolls­
Royce
GmbH,
Dahlewitz,
German
29­
Jun­
99
4BR003
BMW
Rolls­
Royce
GmbH
BMW
Rolls­
Royce
GmbH
BMW
Rolls­
Royce
GmbH,
Dahlewitz,
German
7­
May­
98
8­
May­
98
4BR006
BMW
Rolls­
Royce
GmbH
BMW
Rolls­
Royce
GmbH
BMW
Rolls­
Royce
GmbH,
Dahlewitz,
German
29­
Jun­
99
4BR004
BMW
Rolls­
Royce
GmbH
BMW
Rolls­
Royce
GmbH
BMW
Rolls­
Royce
GmbH,
Dahlewitz,
German
7­
May­
98
8­
May­
98
4BR007
BMW
Rolls­
Royce
GmbH
BMW
Rolls­
Royce
GmbH
BMW
Rolls­
Royce
GmbH,
Dahlewitz,
German
29­
Jun­
99
1CM001
CFMI
CFM56
Evaluation
Engineering
Peebles
Site
IVD
11­
Nov­
83
14­
Nov­
83
1CM002
CFMI
CFM56
Evaluation
Engineering
Peebles
Site
IVD
11­
Nov­
83
14­
Nov­
83
1CM003
CFMI
CFM56
Evaluation
Engineering
Peebles
Site
IVD
11­
Nov­
83
14­
Nov­
83
1CM004
CFMI
CFM56
Evaluation
Engineering
Peebles
Site
IVD
11­
Nov­
83
14­
Nov­
83
1CM005
CFMI
CFM56
Evaluation
Engineering
Peebles
Site
IVD
11­
Nov­
83
14­
Nov­
83
1CM006
CFMI
CFM56
Evaluation
Engineering
Peebles
Site
IVD
11­
Nov­
83
14­
Nov­
83
Filename
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ARP.
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Data
1
2
3
CT
CU
UID
No
Remarks
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
1AA001
1.
Data
obtained
on
aircraft
(
Tu­
134B)
2.
In­
service
engine(
s),
tested
after
overhaul
1AA002
1.
Data
obtained
on
aircraft
(
Il­
76TD)
2.
In­
service
engine(
s),
tested
before
overhaul
1AA003
1.
Data
obtained
on
aircraft
(
Il­
62M)
2.
In­
service
engine(
s),
tested
after
overhaul
1AA004
1.
Data
obtained
on
aircraft
(
Tu­
154M)
2.
In­
service
engine(
s),
tested
before
overhaul
1AA005
For
aircraft
Il­
96
and
Tu­
204
3BR001
Data
from
certification
report
E­
TR403/
96­(
FR)
ISS02
4BR008
1.
Data
from
Certification
report
E­
TR825/
96­(
FR)
ISS01.
2.
For
Gulfstream
V
application
4BR009
1.
Data
from
Certification
report
E­
TR853/
96­(
FR)
ISS01.
2.
For
Canadair
Global
Express
application
6BR010
1.
Certification
report
E­
TR554/
01
­
(
FR)
­
01
2.
For
Gulfstream
G550
appliaction
4BR002
Data
from
Certification
Report
E­
TR484/
98
(
FR)
ISS00
4BR005
1.
Data
from
certification
report
E­
TR346/
99
(
FR)
ISS00.
2.
Incorporating
improved
fuel
injector.

4BR003
Data
from
Certification
Report
E­
TR484/
98
(
FR)
ISS00
4BR006
1.
Data
from
certification
report
E­
TR346/
99
(
FR)
ISS00.
2.
Incorporating
improved
fuel
injector.

4BR004
Data
from
Certification
Report
E­
TR484/
98
(
FR)
ISS00
4BR007
1.
Data
from
certification
report
E­
TR346/
99
(
FR)
ISS00.
2.
Incorporating
improved
fuel
injector.

1CM001
1.
Ref
GE
Report
R83AEB631.
2.
Engine
S/
N
692441.
3.
Applicable
to
CFM56­
2A2
and
­
2A3.

1CM002
1.
Ref
GE
Report
R83AEB631.
2.
Engine
S/
N
692441.

1CM003
1.
Ref
GE
Report
R83AEB631.
2.
Engine
S/
N
692441.

1CM004
1.
Ref
GE
Report
R84AEB245.
2.
Engine
S/
N
692441.
3.
Revised
based
on
3/
89
production
cycle.
4.
Data
also
apply
to
CFM56­
3C­
1
and
­
3B­
2
engines
rerated
to
89.4
kN
(
20,100
Lb)
thrust
for
B737­
300
aircraft.

1CM005
1.
Ref
GE
Report
R84AEB245.
2.
Engine
S/
N
692441.
3.
Revised
based
on
3/
89
production
cycle.
4.
Data
also
apply
to
CFM56­
3C­
1
engines
rerated
to
98.3
kN
(
22,100
Lb.)
thrust
for
B737­
300
and
­
400
aircraft.

1CM006
1.
Ref
GE
Report
R84AEB579.
2.
Engine
S/
N
692441.
3.
Revised
based
on
3/
89
production
status
cycle.
4.
Data
also
apply
to
CFM56­
3­
B1
engines
rerated
to
82.3
kN
(
18,500
Lb.)
thrust
for
B737­
500
aircraft.

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ARP.
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Data
1
2
3
CV
CW
CX
CY
CZ
DA
DB
DC
DD
DE
DF
DG
DH
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
Filename
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ARP.
xls
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Data
1
2
3
DI
DJ
DK
DL
DM
DN
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
Filename
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ARP.
xls
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Data
1
2
3
A
B
C
D
E
F
G
UID
Engine
Combustor
Eng
B/
P
Press
Rated
No
Identification
Description
Type
Ratio
Ratio
Output
kN
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
1CM007
CFM56­
3C­
1
TF
5.1
25.5
104.60
1CM008
CFM56­
5­
A1
TF
6.0
26.6
111.2
1CM009
CFM56­
5A3
TF
6.0
27.9
117.88
4CM035
CFM56­
5A4
TF
6
23.8
97.89
4CM036
CFM56­
5A5
TF
6
25.1
104.53
2CM012
CFM56­
5B1
TF
5.7
30.2
133.45
2CM016
CFM56­
5B1/
2
DAC
TF
5.7
30.2
133.45
3CM020
CFM56­
5B1/
2P
DAC­
II
TF
5.7
30.5
133.5
3CM023
CFM56­
5B1/
P
TF
5.7
30.47
133.45
2CM013
CFM56­
5B2
TF
5.6
31.3
137.9
2CM017
CFM56­
5B2/
2
DAC
TF
5.7
31.2
137.9
4CM037
CFM56­
5B2/
2P
DAC­
II
TF
5.6
31.6
137.9
3CM024
CFM56­
5B2/
P
TF
5.6
31.57
137.90
4CM038
CFM56­
5B3/
2P
DAC­
II
TF
5.6
32.8
142.4
3CM025
CFM56­
5B3/
P
TF
5.6
32.78
142.35
2CM014
CFM56­
5B4
TF
5.9
27.1
117.9
2CM018
CFM56­
5B4/
2
DAC
TF
5.7
27.1
117.9
3CM021
CFM56­
5B4/
2P
DAC­
II
TF
5.9
27.7
120.1
3CM026
CFM56­
5B4/
P
TF
5.9
27.69
120.11
3CM027
CFM56­
5B5/
P
TF
5.9
23.33
97.89
2CM019
CFM56­
5B6/
2
DAC
TF
5.7
24.8
104.5
3CM022
CFM56­
5B6/
2P
DAC­
II
TF
6.0
24.6
104.5
3CM028
CFM56­
5B6/
P
TF
6.0
24.64
104.53
6CM044
CFM56­
5B7/
P
TF
5.9
27.69
120.11
7CM048
CFM56­
5B8/
P
SAC
TF
5.9
22.6
94.7
7CM050
CFM56­
5B9/
2P
DAC
TF
5.9
24.4
102.2
7CM049
CFM56­
5B9/
P
SAC
TF
5.9
24.0
102.2
1CM010
CFM56­
5C2
TF
6.8
28.8
138.78
7CM045
CFM56­
5C2/
P
SAC
MTF
6.8
28.2
137.61
1CM011
CFM56­
5C3
TF
6.7
29.9
144.57
7CM046
CFM56­
5C3/
P
SAC
MTF
6.7
29.2
143.33
2CM015
CFM56­
5C4
TF
6.6
31.15
151.25
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Data
1
2
3
H
I
J
K
L
M
N
O
P
Q
R
S
T
U
UID
Data
Superseded
Data
No
PR
C
R
superseded
by
NME
DTEPS
Other
Corr
as
Out
of
Date
Out
of
Date
UID
No
Annex
16
Production
Service
­­­­­­­­
Data
Status­­­­­­­­
­­­­­­­­­­
Current
Engine
Status
­­­­­­­­­­

­­­­­­
Test
Engine
Status­­­­­­

65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
1CM007
­
­
x
­
­
x
­
­
x
x
­
­
­

1CM008
­
­
x
­
­
x
­
­
x
­
­
­
­

1CM009
­
x
­
­
­
x
­
­
x
­
­
­
­

4CM035
­
x
­
­
­
x
­
­
x
­
­
­
­

4CM036
­
x
­
­
­
x
­
­
x
­
­
­
­

2CM012
­
x
­
­
­
x
­
­
x
x
­
­
­

2CM016
­
x
­
­
­
x
­
­
x
x
­
­
­

2CM020
­
x
­
­
­
­
x
­
x
­
­
­
­

3CM023
­
x
­
­
­
x
­
­
x
­
­
­
­

2CM013
­
x
­
­
­
x
­
­
x
x
­
­
­

2CM017
­
x
­
­
­
x
­
­
x
x
­
­
­

4CM037
­
x
­
­
­
­
x
­
x
­
­
­
­

3CM024
­
x
­
­
­
x
­
­
x
­
­
­
­

4CM038
­
x
­
­
­
­
x
­
x
­
­
­
­

3CM025
­
x
­
­
­
x
­
­
x
­
­
­
­

2CM014
­
x
­
­
­
x
­
­
x
x
­
­
­

2CM018
­
x
­
­
­
x
­
­
x
x
­
­
­

2CM021
­
x
­
­
­
­
x
­
x
­
­
­
­

3CM026
­
x
­
­
­
x
­
­
x
­
­
­
­

3CM027
­
x
­
­
­
x
­
­
x
­
­
­
­

2CM019
­
x
­
­
­
x
­
­
x
x
­
­
­

2CM022
­
x
­
­
­
­
x
­
x
­
­
­
­

3CM028
­
x
­
­
­
x
­
­
x
­
­
­
­

6CM044
­
x
­
­
­
x
­
­
x
­
­
­
­

7CM048
­
x
­
­
­
x
­
­
x
­
­
­
­

7CM050
­
x
­
­
­
­
x
­
x
­
­
­
­

7CM049
­
x
­
­
­
x
­
­
x
­
­
­
­

1CM010
­
x
­
­
­
x
­
­
x
­
­
­
­

7CM045
­
x
­
­
­
x
­
­
x
­
­
­
­

1CM011
­
x
­
­
­
x
­
­
x
­
­
­
­

7CM046
­
x
­
­
­
x
­
­
x
­
­
­
­

2CM015
­
x
­
­
­
x
­
­
x
­
­
­
­

Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
V
W
X
Y
Z
AA
AB
AC
AD
AE
AF
AG
AH
UID
Characteristic
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
%
of
Total
mass
Reg
limit
(
g)

­­­­­­­­­­­­­­­­
EI
HC­­­­­­­­­­­­­­
­­­
Number
­­­
­­­­­­­­­­­­­­­
Dp/
Foo
(
HC)­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­
­­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­­­­­

65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
1CM007
0.03
0.04
0.07
1.42
3
1
2.76
0.38
2.33­
3.06
4.3
21.7
287
1CM008
0.23
0.23
0.40
1.4
3
1
2.6
0.5
2.3­
3.2
4.0
20.4
285
1CM009
0.2
0.2
0.3
1.3
3
1
2.3
0.5
1.8­
2.8
3.5
18.1
268
4CM035
0.23
0.23
0.50
1.75
3
1
3.3
­
­
5.1
25.9
322
4CM036
0.23
0.23
0.45
1.53
3
1
2.8
­
­
4.3
22.0
297
2CM012
0.10
0.10
0.12
3.21
3
1
4.60
0.29
4.28­
4.86
7.1
36.1
617
2CM016
0.1
0.1
9.1
1.7
3
2
8.7
­
8.1­
9.4
11.3
57.7
1168
3CM020
0.1
0.1
3.7
2.9
4
2
6.8
­
6.2­
7.4
8.8
44.9
891
3CM023
0.10
0.20
0.50
3.70
3
1
5.29
­
­
8.2
41.8
710
2CM013
0.10
0.10
0.12
3.04
3
1
4.31
0.24
4.05­
4.53
6.6
33.9
596
2CM017
0.1
0.1
8.4
1.7
3
2
8.1
­
7.9­
8.9
10.5
53.6
1128
4CM037
0.1
0.1
3.3
2.7
4
2
6.13
­
5.6­
6.7
8.0
40.7
877
3CM024
0.10
0.20
0.50
3.60
3
1
5.13
­
­
7.9
40.3
712
4CM038
0.1
0.1
2.9
2.5
4
2
5.57
­
5.1­
6.0
7.3
37.0
807
3CM025
0.10
0.20
0.50
3.50
3
1
5.00
­
­
7.7
39.3
708
2CM014
0.10
0.10
0.13
3.87
3
1
5.70
0.40
5.26­
6.04
8.8
44.8
674
2CM018
0.1
0.1
11.4
2.2
3
2
11.2
­
10.4­
12.0
14.6
74.5
1350
3CM021
0.1
0.2
5.3
3.6
4
2
9.2
­
8.2­
10.1
12.0
61.2
1136
3CM026
0.20
0.20
0.50
4.60
3
1
6.77
­
­
10.4
53.1
818
3CM027
0.20
0.20
0.70
6.20
3
1
9.96
­
­
15.3
78.1
980
2CM019
0.1
0.2
0.2
3.4
9
4
5.84
­
4.58­
8.45
6.7
34.0
630
3CM022
0.2
0.2
0.4
4.6
4
2
7.9
­
7.6­
8.2
10.3
52.6
849
3CM028
0.20
0.20
0.60
5.50
3
1
8.61
­
­
13.3
67.9
901
6CM044
0.20
0.20
0.50
4.60
3
1
6.77
­
­
10.4
53.2
818
7CM048
0.1
0.1
0.9
6.5
3
1
10.8
­
­
16.6
84.7
1023
7CM050
0.2
0.3
0.4
4.4
4.00
2
7.6
­
7.4
­
7.8
9.9
50.5
789
7CM049
0.1
0.1
0.8
5.9
3
1
9.4
­
­
14.4
73.5
970
1CM010
0.008
0.008
0.082
5.68
3
1
7.56
0.59
6.90­
8.01
11.6
59.4
1050
7CM045
0
0
0
5.8
3
1
7.2
­
­
11.1
56.6
986
1CM011
0.008
0.008
0.074
5.35
3
1
7.00
0.49
6.45­
7.41
10.8
55.0
1012
7CM046
0
0
0
5.4
3
1
6.6
­
­
10.2
52.0
943
2CM015
0.008
0.008
0.065
5.00
3
1
6.40
0.44
5.95­
6.83
9.9
50.5
975
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
AI
AJ
AK
AL
AM
AN
AO
AP
AQ
AR
AS
AT
AU
UID
Characteristic
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
%
of
Total
mass
Reg
limit
(
g)

­­­­­­­­­­­­­­­­­
EI
CO­­­­­­­­­­­­­­­­­
­­­­­­
Number­­­­­
­­­­­­­­­­­­­­­
Dp/
Foo
(
CO)­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­­­

65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
1CM007
0.9
0.9
3.1
26.8
3
1
53.5
2.85
51.2­
56.7
65.7
55.7
5591
1CM008
0.9
0.9
2.5
17.6
3
1
27.9
0.7
27.0­
28.4
34.2
29.0
3093
1CM009
0.9
0.9
2.4
16.2
3
1
25.1
0.6
24.2­
25.5
30.8
26.1
2968
4CM035
1.1
1.1
3.1
20.3
3
1
34.1
­
­
41.9
35.5
3352
4CM036
1.1
1.1
2.8
18.5
3
1
30.3
­
­
37.2
31.5
3175
2CM012
0.50
0.50
1.57
28.40
3
1
40.5
0.34
40.1­
40.8
49.7
42.1
5423
2CM016
0.6
2.5
38.4
34.0
3
2
79.5
­
73.9­
85.2
90.6
76.8
10641
3CM020
0.8
1.9
23.1
36.5
4
2
70.5
­
66.2­
74.7
80.3
68.1
9197
3CM023
0.90
0.90
2.00
19.80
3
1
28.05
­
­
34.4
29.2
3738
2CM013
0.50
0.50
1.40
27.40
3
1
38.6
0.21
38.3­
38.7
47.4
40.2
5319
2CM017
0.4
1.7
35.8
33.7
3
2
75.4
­
70.0­
80.9
85.9
72.8
10404
4CM037
0.7
1.6
21.4
35.5
4
2
66.47
­
62.6­
70.3
75.7
64.2
9478
3CM024
0.80
0.90
1.90
19.50
3
1
27.18
­
­
33.4
28.3
3776
4CM038
0.6
1.3
19.9
34.5
4
2
62.79
­
59.3­
66.3
71.5
60.6
9141
3CM025
0.80
0.90
1.70
19.20
3
1
26.48
­
­
32.5
27.5
3777
2CM014
0.50
0.50
2.33
31.90
3
1
47.3
0.38
47.0­
47.7
58.1
49.2
5595
2CM018
1.6
4.9
43.8
37.1
3
2
93.5
­
87.6­
99.3
106.5
90.3
11234
3CM021
1.4
3.6
29.1
40.1
4
2
84.7
­
79.0­
90.4
96.5
81.8
10400
3CM026
0.90
0.90
2.30
23.40
3
1
34.30
­
­
42.1
35.7
4123
3CM027
0.90
1.00
3.40
30.00
3
1
48.31
­
­
59.3
50.3
4743
2CM019
4.48
12.18
17.75
46.10
9
4
103.35
­
97.66­
109.78
110.6
93.7
10842
3CM022
3.1
7.4
21.5
44.8
4
2
96.7
­
95.2­
98.2
110.2
93.4
10205
3CM028
0.90
1.00
2.90
27.70
3
1
43.27
­
­
53.1
45.0
4525
6CM044
0.90
0.90
2.30
23.40
3
1
34.33
­
­
42.1
35.7
4123
7CM048
0.8
0.8
3.9
32.9
3
1
54.4
­
­
66.8
56.6
5176
7CM050
2.9
8.1
21
44.1
4
2
94.3
­
92.9
­
95.8
107.5
91.1
9687
7CM049
0.8
0.8
3.7
30.4
3
1
48.7
­
­
59.7
50.6
5012
1CM010
0.93
0.80
1.75
34.0
3
1
47.2
1.71
45.4­
48.8
57.9
49.1
6546
7CM045
0.8
0.7
2.1
35.1
3
1
45.7
­
­
56.2
47.6
6278
1CM011
0.98
0.82
1.57
32.6
3
1
44.5
1.69
42.7­
46.1
54.6
46.3
6436
7CM046
0.8
0.7
1.9
33.4
3
1
42.8
­
­
52.6
44.6
6142
2CM015
1.00
0.85
1.40
30.93
3
1
41.6
1.37
39.7­
42.4
51.1
43.3
6308
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
AV
AW
AX
AY
AZ
BA
BB
BC
BD
BE
BF
BG
BH
BI
BJ
UID
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
Original
CAEP
2
CAEP
4
Total
mass
(
g)

­­­­
Number­­­­­

­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­
EI
NOx­­­­­­­­­­­­­­
­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­
Dp/
Foo
(
NOx)­­­­­­­­­­­­­­
Characteristic
as
%
of
standards
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
1CM007
20.7
17.8
9.1
4.3
3
1
45.8
0.82
45.3­
46.8
53.1
58.3
72.9
88.8
4810
1CM008
24.6
19.6
8.0
4.0
3
1
40.5
0.6
39.9­
40.9
46.9
50.4
63.0
76.3
4506
1CM009
26.4
21.1
8.3
4.1
3
1
43.4
0.7
42.7­
44.2
50.3
52.5
65.6
79.0
5110
4CM035
22.64
19.11
8.51
4.04
3
1
39.3
­
­
45.6
52.0
65.0
79.8
3851
4CM036
24.79
19.98
8.94
4.29
3
1
41.8
­
­
48.5
53.7
67.1
81.9
4367
2CM012
35.1
27.2
10.8
4.6
3
1
58.4
0.7
58.0­
59.2
67.7
67.4
84.3
100.4
7783
2CM016
27.75
14.91
7.02
4.73
3
2
39.8
­
38.8­
40.8
43.8
43.6
54.5
65.0
5314
3CM020
23.3
16.4
7.3
4.1
4
2
37.9
­
37.5­
38.3
41.7
41.3
51.6
61.3
5024
3CM023
33.00
26.20
10.70
4.50
3
1
53.38
­
­
61.9
61.3
76.7
91.1
7112
2CM013
37.8
28.5
11.0
4.7
3
1
61.5
0.5
61.2­
62.2
71.3
69.5
86.9
102.4
8485
2CM017
29.57
15.86
7.24
4.82
3
2
41.8
­
40.7­
42.8
46.0
44.9
56.2
66.3
5756
4CM037
29.4
17.5
7.6
4.2
4
2
42.12
­
41.4­
42.9
46.3
44.9
56.1
66.0
5844
3CM024
35.10
27.40
10.90
4.60
3
1
56.00
­
­
64.9
62.9
78.7
92.5
7723
4CM038
32.0
18.6
7.8
4.3
4
2
44.93
­
44.3­
45.5
49.4
46.8
58.5
68.1
6420
3CM025
37.30
28.50
11.20
4.70
3
1
58.81
­
­
68.2
64.6
80.8
94.0
8360
2CM014
28.7
23.3
10.0
4.3
3
1
49.7
0.5
49.3­
50.2
57.6
61.1
76.4
92.4
5861
2CM018
16.61
12.58
6.13
4.49
3
2
31.5
­
31.0­
31.9
34.6
36.7
45.9
55.5
3783
3CM021
18.4
13.6
6.5
3.9
4
2
31.7
­
31.1­
32.4
34.9
36.6
45.7
55.1
3847
3CM026
28.00
23.20
10.00
4.30
3
1
47.06
­
­
54.6
57.2
71.6
86.3
5641
3CM027
21.90
18.50
8.70
3.80
3
1
38.23
­
­
44.3
51.1
63.9
78.6
3732
2CM019
13.51
10.41
10.32
3.90
9
4
30.2
­
29.37­
31.42
31.7
35.4
44.2
54.0
3158
3CM022
14.2
11.0
8.7
3.6
4
2
28.8
­
28.4­
29.2
31.7
35.5
44.4
54.3
3020
3CM028
23.60
19.60
9.20
4.00
3
1
40.49
­
­
46.9
52.5
65.7
80.3
4232
6CM044
28.00
23.20
10.00
4.30
3
1
47.06
­
­
54.6
57.2
71.5
86.2
5641
7CM048
19.7
16.7
8.4
3.4
3
1
35.4
­
­
41.0
48.1
60.2
74.4
3358
7CM050
13.9
10.7
7.6
3.2
4
2
26.9
­
26.5
­
27.2
29.5
33.2
41.5
51
2754
7CM049
21.4
17.9
8.8
3.6
3
1
37.9
­
­
43.9
49.9
62.4
76.5
3875
1CM010
32.6
25.8
10.0
4.19
3
1
50.9
0.04
50.89­
50.96
59.0
60.5
75.6
90.7
7077
7CM045
29.7
23.8
9.3
3.9
3
1
45.4
­
­
52.6
54.6
68.2
82.1
6240
1CM011
34.7
27.1
10.4
4.26
3
1
53.8
0.22
53.5­
53.9
62.4
62.5
78.1
93.3
7770
7CM046
31.6
25.1
9.6
4.0
3
1
47.8
­
­
55.4
56.3
70.4
84.3
6858
2CM015
37.67
29.05
10.67
4.28
3
1
57.5
0.33
57.2­
57.9
66.7
65.2
81.5
96.2
8702
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
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website
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aviation_
emissions_
databank
Data
1
2
3
BK
BL
BM
BN
BO
BP
BQ
BR
BS
BT
BU
BV
UID
Characteristic
No
T/
O
C/
O
App
Idle
Test
Eng
Max
Sigma
Range
Characteristic
%
of
Reg
limit
­­­­­­­­­­­­­­
Smoke
Number­­­­­­­­­­­­­

­­­­­­­­­­­­­
Smoke
Number­­­­­­­­­­­­­
­­­­
Number­­­­

65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
1CM007
7.7
3.9
2.5
2.3
3
1
7.7
0.76
6.8­
8.3
9.9
42.4
1CM008
15.8
14.0
4.4
2.3
3
1
15.8
2.00
13.5­
17.3
20.3
88.5
1CM009
16.8
14.6
4.8
2.7
3
1
16.8
2.0
14.6­
18.8
21.6
95.6
4CM035
13.9
­
­
­
3
1
13.9
­
­
17.9
75.1
4CM036
14.3
­
­
­
3
1
14.3
­
­
18.4
78.7
2CM012
8.6
10.5
0
0
3
1
10.5
1.4
8.9­
11.4
13.5
61.7
2CM016
­
­
­
­
3
2
4.75
­
4.5­
5.0
5.6
25.6
3CM020
0.5
0.3
0.5
2.1
4
2
2.1
­
2.0­
2.3
2.5
11.4
3CM023
­
­
­
­
3
1
5.4
­
­
7.0
32.0
2CM013
8.2
10.1
0
0
3
1
10.1
1.3
8.6­
11.0
13.0
60.0
2CM017
­
­
­
­
3
2
4.75
­
4.5­
5.0
5.6
25.8
4CM037
0.5
0.3
0.5
2.2
4
2
2.15
­
2.0­
2.3
2.5
11.6
3CM024
­
­
­
­
3
1
5.4
­
­
7.0
32.3
4CM038
0.5
0.3
0.5
2.3
4
2
2.25
­
2.1­
2.4
2.6
12.3
3CM025
­
­
­
­
3
1
5.4
­
­
7.0
32.6
2CM014
10.0
11.7
0
0
3
1
11.7
1.3
10.2­
12.7
15.1
66.7
2CM018
­
­
­
­
3
2
4.75
­
4.5­
5.0
5.6
24.8
3CM021
0.3
0.3
0.5
2.0
4
2
2.0
­
1.8­
2.2
2.3
10.2
3CM026
­
­
­
­
3
1
5.4
­
­
7.0
31.1
3CM027
­
­
­
­
3
1
5.4
­
­
7.0
29.4
2CM019
­
­
­
­
9
4
3.7
­
3.1­
4.2
4.0
17.1
3CM022
0.3
0.3
6.7
1.8
4
2
6.7
­
6.2­
7.1
7.9
33.8
3CM028
­
­
­
­
3
1
5.4
­
­
7.0
29.9
6CM044
­
­
­
­
3
1
5.4
­
­
6.9
30.7
7CM048
5.4
­
­
­
3
1
5.4
­
­
6.9
28.7
7CM050
6.6
­
­
­
4
2
6.6
­
­
7.8
33.1
7CM049
5.4
­
­
­
3
1
5.4
­
­
6.9
29.3
1CM010
11.1
8.5
1.0
1.1
3
1
11.1
1.6
9.3­
12.1
14.3
66.0
7CM045
10.7
­
­
­
3
1
10.7
­
­
13.8
63.6
1CM011
11.8
9.1
1.0
1.1
3
1
11.8
1.6
9.9­
12.8
15.2
71.0
7CM046
11.6
­
­
­
3
1
11.6
­
­
14.9
69.5
2CM015
12.58
9.80
1.03
1.10
3
1
12.6
1.4
10.7­
13.6
16.2
76.7
Filename
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ARP.
xls
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Data
1
2
3
BW
BX
BY
BZ
CA
CB
CC
CD
CE
UID
Fuel
per
No
Spec
H/
C
Arom
T/
O
C/
O
App
Idle
LTO
cycle
Ratio
%
(
kg)

­­­­­­­­­­­­­­­­­
Fuel
Flow­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­(
kg/
sec)­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­­­­­
Fuel­­­­­­­­­­­­­­­­­­­­­­­

65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
1CM007
Jet
A
1.93
16.0
1.154
0.954
0.336
0.124
448
1CM008
Jet
A
1.95
18.0
1.051
0.862
0.291
0.1011
385
1CM009
Jet
A
1.95
18.0
1.131
0.925
0.307
0.1044
406
4CM035
Jet
A
1.95
18
0.897
0.74
0.261
0.095
346
4CM036
Jet
A
1.95
18
0.972
0.799
0.276
0.098
365
2CM012
Jet
A
1.93
16.8
1.359
1.113
0.364
0.117
474
2CM016
Jet
A
1.93
16.8
1.345
1.104
0.369
0.129
492
3CM020
Jet
A
1.93
17.33
1.32
1.07
0.37
0.12
473
3CM023
Jet
A
1.92
19.0
1.295
1.058
0.345
0.11
448
2CM013
Jet
A
1.93
16.8
1.426
1.158
0.376
0.119
489
2CM017
Jet
A
1.93
16.8
1.406
1.132
0.377
0.131
503
4CM037
Jet
A
1.93
17.33
1.39
1.11
0.39
0.13
501
3CM024
Jet
A
1.92
19.0
1.361
1.099
0.356
0.113
464
4CM038
Jet
A
1.93
17.33
1.47
1.15
0.4
0.13
512
3CM025
Jet
A
1.92
19.0
1.430
1.141
0.366
0.115
478
2CM014
Jet
A
1.93
16.8
1.166
0.961
0.326
0.107
421
2CM018
Jet
A
1.93
16.8
1.180
0.975
0.335
0.121
447
3CM021
Jet
A
1.93
17.33
1.14
0.95
0.34
0.12
442
3CM026
Jet
A
1.92
19.0
1.132
0.935
0.312
0.104
408
3CM027
Jet
A
1.92
19.0
0.891
0.742
0.260
0.094
344
2CM019
Jet
A
1.92
18.1
0.998
0.827
0.315
0.111
400
3CM022
Jet
A
1.93
17.33
0.970
0.81
0.31
0.11
394
3CM028
Jet
A
1.92
19.0
0.961
0.799
0.275
0.097
363
6CM044
Jet
A
1.92
19.0
1.132
0.935
0.312
0.104
408
7CM048
Jet
A
1.92
19
0.875
0.729
0.262
0.094
342
7CM050
Jet
A
1.93
17.33
0.961
0.799
0.296
0.105
381
7CM049
Jet
A
1.92
19
0.954
0.794
0.280
0.098
365
1CM010
Jet
A
1.95
17.3
1.308
1.076
0.3558
0.1175
466
7CM045
Jet
A
1.95
17.3
1.252
1.035
0.342
0.109
441
1CM011
Jet
A
1.95
17.3
1.373
1.131
0.370
0.1203
483
7CM046
Jet
A
1.95
17.3
1.316
1.085
0.355
0.112
458
2CM015
Jet
A
1.95
17.3
1.456
1.195
0.386
0.124
505
Filename
DCTM_
ARP.
xls
Printed
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05
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aviation_
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Data
1
2
3
CF
CG
CH
CI
CJ
CK
CL
CM
UID
No
Baro
Temp
Humidity
kW
@
Power
%
CF
@
Power
kPa
K
kg/
kg
­­­­­­­­­­­­­­­­­­­
Ambient­­­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­
Loads­­­­­­­­­­­­­­­­­­­

Power
Extraction
­­­
Stage
Bleed­­­

65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
1CM007
0
­
0
­
95.98­
97.49
279
­
286
.002­.
009
1CM008
0
­
0
­
94.70­
95.60
280
­
291
.0026­.
0034
1CM009
0
­
0
­
94.70­
95.60
280
­
291
.0026­.
0034
4CM035
0
­
0
­
94.70­
95.60
280­
291
.0026­.
0034
4CM036
0
­
0
­
94.70­
95.60
280­
291
.0026­.
0034
2CM012
0
­
0
­
97.49
­
98.18
283.4
­
293.9
.0067
­
.0076
2CM016
0
­
0
­
100.67­
101.01
293­
299
.0114­.
0129
3CM020
0
­
0
­
98.5­
99.74
284.6­
292.4
.0081­.
0115
3CM023
0
­
0
­
98.2­
99.6
281.5­
283.6
.0065­.
0075
2CM013
0
­
0
­
97.49
­
98.18
283.4
­
293.9
.0067
­
.0076
2CM017
0
­
0
­
100.67­
101.01
293­
299
.0114­.
0129
4CM037
0
­
0
­
98.5­
99.74
284.6­
292.4
.0081­.
0115
3CM024
0
­
0
­
98.2­
99.6
281.5­
283.6
.0065­.
0075
4CM038
0
­
0
­
98.5­
99.74
284.6­
292.4
.0081­.
0115
3CM025
0
­
0
­
98.2­
99.6
281.5­
283.6
.0065­.
0075
2CM014
0
­
0
­
97.49
­
98.18
283.4
­
293.9
.0067
­
.0076
2CM018
0
­
0
­
100.67­
101.01
293­
299
.0114­.
0129
3CM021
0
­
0
­
98.5­
99.74
284.6­
292.4
.0081­.
0115
3CM026
0
­
0
­
98.2­
99.6
281.5­
283.6
.0065­.
0075
3CM027
0
­
0
­
98.2­
99.6
281.5­
283.6
.0065­.
0075
2CM019
0
­
0
­
99.29­
101.01
288­
298
.0100­.
0146
3CM022
0
­
0
­
98.5­
99.74
284.6­
292.4
.0081­.
0115
3CM028
0
­
0
­
98.2­
99.6
281.5­
283.6
.0065­.
0075
6CM044
0
­
0
­
98.2
­
99.6
281.5
­
283.6
.0065
­
.0075
7CM048
0
­
0
­
98.2
­
99.6
281.5
­
283.6
0.0065
­
0.0075
7CM050
0
­
0
­
98.5
­
99.74
284.6
­
292.4
0.0081
­
0.0115
7CM049
0
­
0
­
98.2
­
99.6
281.5
­
283.6
0.0065
­
0.0075
1CM010
0
­
0
­
97.77­
98.11
286
­
295
.0061­.
0074
7CM045
0
­
0
­
97.77
­
98.11
286
­
295
0.0061
­
0.0074
1CM011
0
­
0
­
97.77­
98.11
286
­
295
.0061­.
0074
7CM046
0
­
0
­
97.77
­
98.11
286
­
295
0.0061
­
0.0074
2CM015
0
­
0
­
97.77­
98.11
286
­
295
.0061­.
0074
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
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aviation_
emissions_
databank
Data
1
2
3
CN
CO
CP
CQ
CR
CS
UID
­­­
Test
Dates­­­

No
Manufacturer
Test
Organisation
Test
Location
From
To
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
1CM007
CFMI
CFM56
Evaluation
Engineering
Peebles
Site
IVD
11­
Nov­
83
14­
Nov­
83
1CM008
CFMI
CFM56
Evaluation
Engineering
Peebles
Site
IIIC
19­
Nov­
86
20­
Nov­
86
1CM009
CFMI
CFM56
Evaluation
Engineering
Peebles
Site
IIIC
19­
Nov­
86
20­
Nov­
86
4CM035
CFMI
CFM56
Evaluation
Engineering
Peebles
Site
IIIC
19­
Nov­
86
20­
Nov­
86
4CM036
CFMI
CFM56
Evaluation
Engineering
Peebles
Site
IIIC
19­
Nov­
86
20­
Nov­
86
2CM012
CFMI
CFM56
Evaluation
Engineering
Peebles
Site
IIIB
7­
Oct­
92
8­
Oct­
92
2CM016
CFMI
CFM56
Evaluation
Engineering
PTO
Site
IIIC
15­
Jun­
94
1­
Jul­
94
3CM020
CFM
International
GEAE
Peebles
Testing
Facility
+
Techspace
APeebles
Ohio,
USE
+
Liers,
Belgium
Aug­
96
Sep­
96
3CM023
GE
CFM56­
5B
Eval
Engineering
Techspace­
Aero
Facility,
Liege,
Belgium
Nov­
95
2CM013
CFMI
CFM56
Evaluation
Engineering
Peebles
Site
IIIB
7­
Oct­
92
8­
Oct­
92
2CM017
CFMI
CFM56
Evaluation
Engineering
PTO
Site
IIIC
15­
Jun­
94
1­
Jul­
94
4CM037
CFM
International
GEAE
Peebles
Testing
Facility
+
Techspace
APeebles,
Ohio,
USA
+
Liers,
Belgium
Aug­
96
Sep­
96
3CM024
GE
CFM56­
5B
Eval
Engineering
Techspace­
Aero
Facility,
Liege,
Belgium
Nov­
95
4CM038
CFM
International
GEAE
Peebles
Testing
Facility
+
Techspace
APeebles,
Ohio,
USA
+
Liers,
Belgium
Aug­
96
Sep­
96
3CM025
GE
CFM56­
5B
Eval
Engineering
Techspace­
Aero
Facility,
Liege,
Belgium
Nov­
95
2CM014
CFMI
CFM56
Evaluation
Engineering
Peebles
Site
IIIB
7­
Oct­
92
8­
Oct­
92
2CM018
CFMI
CFM56
Evaluation
Engineering
PTO
Site
IIIC
15­
Jun­
94
1­
Jul­
94
3CM021
CFM
International
GEAE
Peebles
Testing
Facility
+
Techspace
APeebles
Ohio,
USE
+
Liers,
Belgium
Aug­
96
Sep­
96
3CM026
GE
CFM56­
5B
Eval
Engineering
Techspace­
Aero
Facility,
Liege,
Belgium
Nov­
95
3CM027
GE
CFM56­
5B
Eval
Engineering
Techspace­
Aero
Facility,
Liege,
Belgium
Nov­
95
2CM019
CFMI
SNECMA,
Villaroche,
France
Techspace
Aero,
Liege,
Belgium
19­
Jun­
95
28­
Jul­
95
3CM022
CFM
International
GEAE
Peebles
Testing
Facility
+
Techspace
APeebles
Ohio,
USE
+
Liers,
Belgium
Aug­
96
Sep­
96
3CM028
GE
CFM56­
5B
Eval
Engineering
Techspace­
Aero
Facility,
Liege,
Belgium
Nov­
95
6CM044
GE
CFM56­
5B
Eval
Engineering
Techspace­
Aero,
Liege,
Belgium
Nov­
95
Nov­
95
7CM048
CFM
International
CFM56
Evaluation
Engineering
Techspace
Aero,
Liege,
Belgium
Nov­
95
Nov­
95
7CM050
CFM
International
CFM56
Evaluation
Engineering
GEAE
PTO
and
Techspace
Aero,
Liege,
Belgi
1­
Aug­
96
30­
Sep­
96
7CM049
CFM
International
CFM56
Evaluation
Engineering
Techspace
Aero,
Liege,
Belgium
13
Non
95
Nov­
95
1CM010
CFMI
CFM56
Evaluation
Engineering
PTO
Site
IVD
4­
Jun­
91
5­
Jun­
91
7CM045
CFM
International
CFM56
Evaluation
Engineering
PTO
Site
IV­
D
4­
Jun­
91
5­
Jun­
91
1CM011
CFMI
CFM56
Evaluation
Engineering
PTO
Site
IVD
4­
Jun­
91
5­
Jun­
91
7CM046
CFM
International
CFM56
Evaluation
Engineering
PTO
Site
IV­
D
Jun­
91
Jun­
91
2CM015
CFMI
CFM56
Evaluation
Engineering
PTO
Site
IVD
4­
Jun­
91
5­
Jun­
91
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
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QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
CT
CU
UID
No
Remarks
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
1CM007
1.
Ref
GE
Report
R84AEB579.
2.
Engine
S/
N
692441.
3.
Revised
based
on
3/
89
production
status
cycle.

1CM008
1.
Ref
GE
Report
R87AEB368.
2.
Engine
S/
N
730002/
2.
3.
Data
revised
and
corrected
April
93.

1CM009
1.
Ref
GE
Reports
R89AEB316
and
R87AEB386.
2.
Engine
S/
N
730002/
2.

4CM035
1.
Ref
GE
Reports
R89AEB316
and
R87AEB386
2.
Engine
S/
N
730002/
2
4CM036
1.
Ref
GE
Reports
R89AEB316
and
R87AEB386
2.
Engine
S/
N
730002/
2
2CM012
1.
Ref
GE
Report
R92AEB262.
2.
Engine
S/
N
779101
2CM016
1.
Ref
GE
Report
CR­
797/
2.
2.
Engine
S/
N
779131/
001
&
779132/
001
3.
DAC
combustor
3CM020
DAC­
II
Combustor
P/
N
1968M99G04
3CM023
1.
FAA
Certification
Report
CR­
797/
P,
June
95.
2.
Engine
S/
N
779­
194/
1
2CM013
1.
Ref
GE
Report
R92AEB262.
2.
Engine
S/
N
779101
2CM017
1.
Ref
GE
Report
CR­
797/
2.
2.
Engine
S/
N
779131/
001
&
779132/
001
3.
DAC
combustor
4CM037
DAC­
II
Combustor
P/
N
1968M99G04
3CM024
1.
FAA
Certification
Report
CR­
797/
P,
June
95.
2.
Engine
S/
N
779­
194/
1
4CM038
DAC­
II
Combustor
P/
N
1968M99G04
3CM025
1.
FAA
Certification
Report
CR­
797/
P,
June
95.
2.
Engine
S/
N
779­
194/
1
2CM014
1.
Ref
GE
Report
R92AEB262.
2.
Engine
S/
N
779101
2CM018
1.
Ref
GE
Report
CR­
797/
2.
2.
Engine
S/
N
779131/
001
&
779132/
001
3.
DAC
combustor
3CM021
DAC­
II
Combustor
P/
N
1968M99G04
3CM026
1.
FAA
Certification
Report
CR­
797/
P,
June
95.
2.
Engine
S/
N
779­
194/
1
3CM027
1.
FAA
Certification
Report
CR­
797/
P,
June
95.
2.
Engine
S/
N
779­
194/
1
2CM019
1.
Ref
GE
Report
CR­
797/
2
Supplement
1.
2.
Engine
S/
N
779172/
001,
779174/
001,
779175/
001,
&
779178/
001
3.
DAC
combustor
3CM022
DAC­
II
Combustor
P/
N
1968M99G04
3CM028
1.
FAA
Certification
Report
CR­
797/
P,
June
95.
2.
Engine
S/
N
779­
194/
1
6CM044
1.
FAA
Certification
Report
CR0797/
P,
June
95.
2.
Engine
S/
N
779­
194/
1
7CM048
1.
FAA
Certificiaction
Report
CR
0797/
P,
June
1995
and
Certification
Report
CR­
700
S3,
October
2001
2.
Engine
S/
N
779­
194/
1
7CM050
1.
FAA
Certification
Report
CR­
700
S3,
October
2001
2.
DAC­
II
combustor
P/
N
196M99G04
7CM049
1.
FAA
Certifiaction
Report
CR
0797/
P,
June
1995
and
Certification
Report
CR­
700
S3,
October
2001
2.
Engine
S/
N
779­
194/
1
1CM010
1.
Ref
GE
Report
R91AEB471.
2.
Engine
S/
N
740­
105.

7CM045
1.
Ref
GE
Report
R91AEB471
and
FAA
Certification
Report
CR­
897/
P,
July
2003
2.
Engine
S/
N
740/
105
1CM011
1.
Ref
GE
Report
R91AEB471.
2.
Engine
S/
N
740­
105.

7CM046
1.
Ref
GE
Report
R91AEB471
and
FAA
Certification
Report
CR­
897/
P,
July
2003
2.
Engine
S/
N
740­
105
2CM015
1.
Ref
GE
Report
R91AEB471
2.
Engine
S/
N
740­
105
Filename
DCTM_
ARP.
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aviation_
emissions_
databank
Data
1
2
3
CV
CW
CX
CY
CZ
DA
DB
DC
DD
DE
DF
DG
DH
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
Engine
S/
N
779­
194/
1
0
0
DAC­
II
Combustor
P/
N
1
0
0
Engine
S/
N
779­
194/
P
0
0
Engine
S/
N
740­
105
0
0
Ebgine
S/
N
740­
105
0
0
Filename
DCTM_
ARP.
xls
Printed
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Data
1
2
3
DI
DJ
DK
DL
DM
DN
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
Filename
DCTM_
ARP.
xls
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Data
1
2
3
A
B
C
D
E
F
G
UID
Engine
Combustor
Eng
B/
P
Press
Rated
No
Identification
Description
Type
Ratio
Ratio
Output
kN
97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
7CM047
CFM56­
5C4/
P
SAC
MTF
6.6
30.5
149.9
3CM029
CFM56­
7B18
TF
5.5
21.59
86.74
3CM030
CFM56­
7B20
TF
5.4
22.61
91.63
4CM039
CFM56­
7B20/
2
TF
5.4
22.77
91.63
3CM031
CFM56­
7B22
TF
5.3
24.41
100.97
4CM040
CFM56­
7B22/
2
TF
5.3
24.61
100.97
3CM032
CFM56­
7B24
TF
5.2
25.78
107.65
4CM041
CFM56­
7B24/
2
TF
5.2
25.95
107.65
3CM033
CFM56­
7B26
TF
5.1
27.61
116.99
4CM042
CFM56­
7B26/
2
TF
5.1
27.80
116.99
3CM034
CFM56­
7B27
TF
5.0
28.63
121.44
4CM043
CFM56­
7B27/
2
TF
5.0
28.84
121.44
General
Electric
1GE034
CF34­
3A
LEC
II
TF
6.25
19.7
41.01
1GE035
CF34­
3A1
LEC
II
TF
6.25
19.7
41.01
5GE084
CF34­
3B
TF
6.25
19.3
41.01
5GE083
CF34­
8C1
TF
5.13
23.03
56.36
6GE096
CF34­
8C1
Block
1
LEC
TF
5.13
22.15
56.36
6GE092
CF34­
8C5
LEC
TF
5.13
23.09
59.42
6GE093
CF34­
8E2
LEC
TF
5.13
21.71
55.19
6GE094
CF34­
8E5
LEC
TF
5.13
23.18
59.68
6GE095
CF34­
8E5A1
LEC
TF
5.13
24.12
62.49
3GE067
CF6­
45A
Low
emissions
fuel
nozzle
TF
4.3
25.38
202.8
1GE005
CF6­
45A2
TF
4.3
25.9
202.8
3GE068
CF6­
45A2
Low
emissions
fuel
nozzle
TF
4.3
25.38
202.8
3GE069
CF6­
50A
Low
emissions
fuel
nozzle
TF
4.3
26.88
215.3
1GE006
CF6­
50C
TF
4.3
28.8
224.2
3GE070
CF6­
50C
Low
emissions
fuel
nozzle
TF
4.3
27.76
224.2
3GE073
CF6­
50C1
Low
emissions
fuel
nozzle
TF
4.3
28.44
230.4
1GE007
CF6­
50C1,
­
C2
TF
4.3
29.8
230.4
Filename
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ARP.
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Data
1
2
3
H
I
J
K
L
M
N
O
P
Q
R
S
T
U
UID
Data
Superseded
Data
No
PR
C
R
superseded
by
NME
DTEPS
Other
Corr
as
Out
of
Date
Out
of
Date
UID
No
Annex
16
Production
Service
­­­­­­­­
Data
Status­­­­­­­­
­­­­­­­­­­
Current
Engine
Status
­­­­­­­­­­

­­­­­­
Test
Engine
Status­­­­­­

97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
7CM047
­
x
­
­
­
x
­
­
x
­
­
­
­

3CM029
­
x
­
­
­
x
­
­
x
­
­
­
­

3CM030
­
x
­
­
­
x
­
­
x
­
­
­
­

4CM039
­
x
­
­
­
x
­
­
x
­
­
­
­

3CM031
­
x
­
­
­
x
­
­
x
­
­
­
­

4CM040
­
x
­
­
­
x
­
­
x
­
­
­
­

3CM032
­
x
­
­
­
x
­
­
x
­
­
­
­

4CM041
­
x
­
­
­
x
­
­
x
­
­
­
­

3CM033
­
x
­
­
­
x
­
­
x
­
­
­
­

4CM042
­
x
­
­
­
x
­
­
x
­
­
­
­

3CM034
­
x
­
­
­
x
­
­
x
­
­
­
­

4CM043
­
x
­
­
­
x
­
­
x
­
­
­
­

1GE034
­
x
­
­
­
x
­
­
x
­
­
­
­

1GE035
­
x
­
­
­
x
­
­
x
­
­
­
­

5GE084
­
x
­
­
­
x
­
­
x
­
­
­
­

5GE083
­
x
­
­
­
x
­
­
x
­
­
­
­

6GE096
­
x
­
­
­
x
­
­
x
­
­
­
­

6GE092
­
x
­
­
­
x
­
­
x
­
­
­
­

6GE093
­
x
­
­
­
x
­
­
x
­
­
­
­

6GE094
­
x
­
­
­
x
­
­
x
­
­
­
­

6GE095
­
x
­
­
­
x
­
­
x
­
­
­
­

3GE067
­
x
­
­
­
x
­
­
x
x
­
­
­

1GE005
x
­
­
­
­
x
­
­
x
x
­
­
­

3GE068
­
x
­
­
­
x
­
­
x
x
­
­
­

3GE069
­
x
­
­
­
x
­
­
x
x
­
­
­

1GE006
x
­
­
­
­
x
­
­
x
x
­
­
­

3GE070
­
x
­
­
­
x
­
­
x
x
­
­
­

3GE073
­
x
­
­
­
x
­
­
x
x
­
­
­

1GE007
x
­
­
­
­
x
­
­
x
x
­
­
­

Filename
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Data
1
2
3
V
W
X
Y
Z
AA
AB
AC
AD
AE
AF
AG
AH
UID
Characteristic
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
%
of
Total
mass
Reg
limit
(
g)

­­­­­­­­­­­­­­­­
EI
HC­­­­­­­­­­­­­­
­­­
Number
­­­
­­­­­­­­­­­­­­­
Dp/
Foo
(
HC)­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­
­­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­­­­­

97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
7CM047
0
0
0
5.0
3
1
6
­
­
9.3
47.4
897
3CM029
0.10
0.10
0.10
3.50
3
1
6.32
­
­
9.7
49.5
549
3CM030
0.10
0.10
0.10
3.10
3
1
5.44
­
­
8.4
42.9
504
4CM039
0.07
0.23
0.36
8.11
3
3
14.61
­
13.8­
15.9
17.0
86.9
1340
3CM031
0.10
0.10
0.10
2.50
3
1
4.22
­
­
6.4
32.7
432
4CM040
0.06
0.10
6.06
7.26
3
3
16.31
­
14.6­
18.2
19.0
97.1
1643
3CM032
0.10
0.10
0.10
2.40
3
1
3.91
­
­
6.0
30.6
432
4CM041
0.05
0.07
6.01
6.55
3
3
14.66
­
13.4­
15.9
17.1
87.2
1576
3CM033
0.10
0.10
0.10
1.90
3
1
3.06
­
­
4.7
24.0
361
4CM042
0.03
0.06
4.73
5.88
3
3
12.21
­
11.1­
13.4
14.2
72.7
1425
3CM034
0.10
0.10
0.10
1.70
3
1
2.76
­
­
4.3
21.9
335
4CM043
0.05
0.06
4.21
5.56
3
3
11.21
­
10.1­
12.3
13.1
66.7
1363
1GE034
0.06
0.06
0.13
3.95
3
1
7.63
0.20
7.41­
7.78
11.8
60.0
313
1GE035
0.06
0.06
0.13
3.95
3
1
7.63
0.20
7.41­
7.78
11.8
60.0
313
5GE084
0.06
0.05
0.13
4.69
3
1
8.9
­
­
13.7
69.9
366
5GE083
0.02
0.02
0.06
0.08
3
1
0.20
0.00
0.2
­
0.2
0.3
1.5
13
6GE096
0.02
0.03
0.07
0.13
3
1
0.30
­
0.3
­
0.4
0.5
2.6
20
6GE092
0.02
0.02
0.06
0.13
3
1
0.31
­
­
0.5
2.6
18
6GE093
0.02
0.03
0.07
0.16
3
1
0.38
­
­
0.6
3.1
21
6GE094
0.02
0.02
0.06
0.13
3
1
0.31
­
­
0.5
2.6
18
6GE095
0.02
0.02
0.06
0.13
3
1
0.29
­
­
0.4
2.0
18
3GE067
0.09
0.14
0.35
2.72*
3
1
3.88
0.14
3.76­
4.04
6.0
30.6
780
1GE005
0.7
0.7
1.1
26.0
6
6
39.7
3.8
­
44.2
225.3
8485
3GE068
0.09
0.14
0.35
2.72*
3
1
3.88
0.14
3.76­
4.04
6.0
30.6
780
3GE069
0.15
0.14
0.31
2.72*
3
1
3.66
0.14
3.53­
3.81
5.6
28.6
785
1GE006
0.6
0.7
1.0
23.0
6
6
35.2
3.8
­
39.2
199.8
7998
3GE070
0.14
0.14
0.29
2.72*
3
1
3.47
0.09
3.38­
3.56
5.3
27.0
784
3GE073
0.14
0.15
0.28
2.72*
3
1
3.42
0.15
3.28­
3.58
5.3
27.0
788
1GE007
0.6
0.7
1.0
21.8
6
6
33.5
3.8
­
37.3
190.1
7715
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Data
1
2
3
AI
AJ
AK
AL
AM
AN
AO
AP
AQ
AR
AS
AT
AU
UID
Characteristic
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
%
of
Total
mass
Reg
limit
(
g)

­­­­­­­­­­­­­­­­­
EI
CO­­­­­­­­­­­­­­­­­
­­­­­­
Number­­­­­
­­­­­­­­­­­­­­­
Dp/
Foo
(
CO)­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­­­

97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
7CM047
0.8
0.7
1.6
31.6
3
1
39.9
­
­
48.9
41.4
5964
3CM029
0.60
0.40
3.60
28.30
3
1
52.45
­
­
64.4
54.6
4566
3CM030
0.60
0.50
3.20
25.90
3
1
47.21
­
­
58.0
49.2
4324
4CM039
4.26
11.38
11.37
49.71
3
3
108.63
­
102.1­
114.9
117.5
99.6
9963
3CM031
0.50
0.60
2.50
22.80
3
1
39.58
­
­
48.6
41.2
4002
4CM040
2.18
6.58
30.87
45.35
3
3
104.18
­
96.9­
111.7
112.7
95.5
10492
3CM032
0.40
0.60
2.20
22.00
3
1
37.11
­
­
45.6
38.6
3998
4CM041
1.38
4.30
30.32
42.72
3
3
94.03
­
88.4­
100.0
101.7
86.2
10117
3CM033
0.20
0.60
1.60
18.80
3
1
30.33
­
­
37.2
31.5
3533
4CM042
0.77
2.51
26.07
39.93
3
3
81.39
­
77.1­
85.9
88.0
74.6
9495
3CM034
0.20
0.50
1.40
17.90
3
1
28.30
­
­
34.7
29.4
3436
4CM043
0.54
1.97
24.28
38.73
3
3
76.46
­
72.7­
80.4
82.7
70.1
9291
1GE034
0
0
1.9
42.6
3
1
81.8
3.25
79.2­
85.5
100.4
85.1
3350
1GE035
0
0
1.9
42.6
3
1
81.8
3.25
79.2­
85.5
100.4
85.1
3350
5GE084
0
0
1.88
47.59
3
1
89.7
­
­
110.1
93.3
3683
5GE083
0.41
0.50
2.91
24.92
3
1
51.30
1.04
50.1
­
52.0
63.0
53.4
2845
6GE096
0.59
0.57
4.67
19.73
3
1
42.80
­
41.5
­
44.5
52.5
44.5
2406
6GE092
0.64
0.57
4.24
18.25
3
1
34.86
­
­
42.8
36.3
2070
6GE093
0.59
0.58
4.52
20.01
3
1
39.28
­
­
48.2
40.8
2169
6GE094
0.64
0.57
4.23
18.16
3
1
34.62
­
­
42.5
36.0
2065
6GE095
0.71
0.57
4.05
17.3
3
1
32.43
­
­
39.8
33.7
2027
3GE067
0.43
0.54
5.01
24.04*
3
1
34.43
0.56
33.90­
34.38
42.3
35.8
6980
1GE005
0.5
0.5
7.5
66.0
6
6
102.0
4.6
­
107.7
91.3
21798
3GE068
0.43
0.54
5.01
24.04*
3
1
34.43
0.56
33.90­
34.38
42.3
35.8
6980
3GE069
0.43
0.49
4.35
24.04*
3
1
32.16
0.50
31.72­
32.71
39.5
33.5
6920
1GE006
0.5
0.5
5.2
62.3
6
6
95.1
4.6
­
100.5
85.1
21583
3GE070
0.44
0.46
3.99
24.04*
3
1
30.73
0.48
30.32­
31.25
37.7
31.9
6883
3GE073
0.45
0.45
3.71
24.04*
3
1
29.80
0.44
29.42­
30.28
36.6
31.0
6863
1GE007
0.5
0.5
4.3
61.8
6
6
93.7
4.6
­
99.0
83.9
21591
Filename
DCTM_
ARP.
xls
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Data
1
2
3
AV
AW
AX
AY
AZ
BA
BB
BC
BD
BE
BF
BG
BH
BI
BJ
UID
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
Original
CAEP
2
CAEP
4
Total
mass
(
g)

­­­­
Number­­­­­

­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­
EI
NOx­­­­­­­­­­­­­­
­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­
Dp/
Foo
(
NOx)­­­­­­­­­­­­­­
Characteristic
as
%
of
standards
97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
7CM047
34.1
26.7
9.9
4.1
3
1
50.9
­
­
59.0
58.4
73.0
86.8
7641
3CM029
19.20
16.60
9.10
4.30
3
1
39.99
­
­
46.4
55.8
69.7
85.8
3472
3CM030
20.50
17.40
9.50
4.30
3
1
41.83
­
­
48.5
56.9
71.1
87.9
3829
4CM039
13.25
10.81
9.39
3.75
3
3
30.58
­
30.4­
30.8
32.4
37.9
47.3
58.4
2802
3CM031
23.10
19.00
10.00
4.50
3
1
45.16
­
­
52.4
59.0
73.7
90.3
4560
4CM040
15.08
12.16
6.37
3.94
3
3
30.63
­
30.4­
30.9
32.4
36.4
45.4
55.6
3091
3CM032
25.30
20.50
10.10
4.40
3
1
47.83
­
­
55.4
60.5
75.6
92.0
5149
4CM041
16.63
13.23
6.72
4.08
3
3
32.86
­
32.7­
33.2
34.8
37.9
47.3
57.5
3534
3CM033
28.80
22.50
10.80
4.70
3
1
52.64
­
­
62.2
65.3
81.7
98.5
6149
4CM042
19.20
14.77
7.26
4.27
3
3
36.24
­
36.0­
36.8
38.4
40.2
50.2
60.5
4233
3CM034
30.90
23.70
11.00
4.80
3
1
55.27
­
­
64.1
65.9
82.4
98.9
6719
4CM043
20.81
15.59
7.53
4.36
3
3
38.23
­
37.9­
38.8
40.5
41.5
51.8
62.2
4648
1GE034
11.61
10.14
6.86
3.82
3
1
27.8
1.61
26.0­
29.0
32.2
40.6
50.7
53.2
1137
1GE035
11.61
10.14
6.86
3.82
3
1
27.8
1.61
26.0­
29.0
32.2
40.6
50.7
53.2
1137
5GE084
11.28
9.68
6.63
3.72
3
1
26.3
­
­
30.5
38.8
48.5
50.9
1078
5GE083
14.67
12.82
11.10
4.31
3
1
37.20
0.74
36.6
­
38.0
43.1
50.1
62.6
68.7
2120
6GE096
13.82
12.00
9.85
4.03
3
1
35.20
­
35.0
­
35.7
40.9
48.5
60.6
71.3
1956
6GE092
14.69
12.6
10.75
4.6
3
1
37.12
­
­
43.0
49.9
62.4
69.2
2205
6GE093
13.6
11.82
10.29
4.45
3
1
35.14
­
­
40.7
48.8
61.0
66.9
1939
6GE094
14.77
12.65
10.77
4.61
3
1
37.25
­
­
43.2
50.0
62.5
69.4
2222
6GE095
15.81
13.15
11.06
4.7
3
1
38.71
­
­
44.9
50.9
63.6
71.1
2419
3GE067
25.45
21.61
9.36
3.4*
3
1
44.90
2.94
42.69­
48.24
52.0
57.3
71.6
87.2
9105
1GE005
31.0
26.2
8.4
3.3
6
6
54.3
0.5
­
56.5
61.6
77.0
93.5
10819
3GE068
25.45
21.61
9.36
3.4*
3
1
44.90
2.94
42.69­
48.24
52.0
57.3
71.6
87.2
9105
3GE069
27.17
23.27
9.72
3.4*
3
1
47.86
2.96
45.72­
51.24
55.5
59.2
74.0
89.5
10286
1GE006
35.0
29.0
9.4
3.5
6
6
60.2
0.5
­
62.7
64.2
80.3
96.3
13436
3GE070
28.03
24.30
10.09
3.4*
3
1
49.59
2.93
47.66­
52.96
57.5
60.2
75.2
90.7
11116
3GE073
28.97
25.50
10.16
3.4*
3
1
51.58
2.80
49.71­
54.80
59.8
61.7
77.2
92.7
11884
1GE007
36.3
29.7
9.5
3.6
6
6
61.8
0.5
­
64.3
64.6
80.7
96.5
14247
Filename
DCTM_
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xls
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Data
1
2
3
BK
BL
BM
BN
BO
BP
BQ
BR
BS
BT
BU
BV
UID
Characteristic
No
T/
O
C/
O
App
Idle
Test
Eng
Max
Sigma
Range
Characteristic
%
of
Reg
limit
­­­­­­­­­­­­­­
Smoke
Number­­­­­­­­­­­­­

­­­­­­­­­­­­­
Smoke
Number­­­­­­­­­­­­­
­­­­
Number­­­­

97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
7CM047
12
­
­
­
3
1
12
­
­
15.4
72.7
3CM029
­
­
­
­
3
1
10.7
­
­
13.8
56.1
3CM030
­
­
­
­
3
1
11.4
­
­
14.7
60.6
4CM039
­
­
­
­
3
3
1.52
­
0
­
3.4
1.7
6.9
3CM031
­
­
­
­
3
1
12.0
­
­
15.4
65.2
4CM040
­
­
­
­
3
3
0.69
­
0.1­
1.8
0.8
3.2
3CM032
­
­
­
­
3
1
12.6
­
­
16.2
69.8
4CM041
­
­
­
­
3
3
0.65
­
0.2­
1.5
0.7
3.1
3CM033
­
­
­
­
3
1
14.7
­
­
18.9
83.4
4CM042
­
­
­
­
3
3
0.71
­
0.3­
1.6
0.7
3.1
3CM034
­
­
­
­
3
1
15.7
­
­
20.2
90.0
4CM043
­
­
­
­
3
3
0.75
­
0.3­
1.6
0.8
3.7
1GE034
21.9
9.2
3.1
3.1
3
1
21.9
0.25
21.7­
22.2
28.2
93.3
1GE035
21.9
9.2
3.1
3.1
3
1
21.9
0.25
21.7­
22.2
28.2
93.3
5GE084
18.3
9.2
3.1
3.1
3
1
18.3
­
­
23.6
78.1
5GE083
5.33
1.48
0
0
3
1
5.33
1.0
4.6
­
6.5
6.9
24.9
6GE096
5.20
1.25
0.00
0.00
3
1
5.20
­
2.5
­
7.2
6.7
24.2
6GE092
8.32
2.52
0
0
3
1
8.32
­
­
10.7
39.2
6GE093
4.58
0.96
0
0
3
1
4.58
­
­
5.9
21.2
6GE094
8.63
2.64
0
0
3
1
8.63
­
­
11.1
40.7
6GE095
13.64
3.9
0
0
3
1
13.64
­
­
17.6
65.4
3GE067
11.61
11.98
1.25
1.4*
3
1
12.52
1.79
10.68­
14.00
16.1
82.6
1GE005
2.9
2.2
2.9
4.6
6
6
4.6
1.5
­
4.9
25.2
3GE068
11.61
11.98
1.25
1.4*
3
1
12.52
1.79
10.68­
14.00
16.1
82.6
3GE069
11.53
12.03
1.49
1.4*
3
1
12.52
1.79
10.68­
14.00
16.1
83.9
1GE006
3.9
2.6
2.8
4.5
6
6
4.5
1.5
­
4.8
25.3
3GE070
11.41
11.83
1.61
1.4*
3
1
12.52
1.79
10.68­
14.00
16.1
84.9
3GE073
10.95
11.72
1.62
1.4*
3
1
12.52
1.79
10.68­
14.00
16.1
85.5
1GE007
4.1
2.7
2.7
4.5
6
6
4.5
1.5
­
4.8
25.5
Filename
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Data
1
2
3
BW
BX
BY
BZ
CA
CB
CC
CD
CE
UID
Fuel
per
No
Spec
H/
C
Arom
T/
O
C/
O
App
Idle
LTO
cycle
Ratio
%
(
kg)

­­­­­­­­­­­­­­­­­
Fuel
Flow­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­(
kg/
sec)­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­­­­­
Fuel­­­­­­­­­­­­­­­­­­­­­­­

97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
7CM047
Jet
A
1.95
17.3
1.395
1.143
0.370
0.115
478
3CM029
Jet
A
1.86­
1.97
16.9­
17.7
0.854
0.714
0.260
0.097
344
3CM030
Jet
A
1.86­
1.97
16.9­
17.7
0.913
0.761
0.274
0.100
361
4CM039
Jet
A
1.93­
1.94
18.0­
19.2
0.903
0.754
0.278
0.102
363
3CM031
Jet
A
1.86­
1.97
16.9­
17.7
1.021
0.844
0.298
0.105
390
4CM040
Jet
A
1.93­
1.94
18.0­
19.2
1.008
0.837
0.303
0.105
389
3CM032
Jet
A
1.86­
1.97
16.9­
17.7
1.103
0.910
0.316
0.109
412
4CM041
Jet
A
1.93­
1.94
18.0­
19.2
1.089
0.902
0.313
0.109
410
3CM033
Jet
A
1.86­
1.97
16.9­
17.7
1.221
0.999
0.338
0.113
441
4CM042
Jet
A
1.93­
1.94
18.0­
19.2
1.203
0.989
0.334
0.113
438
3CM034
Jet
A
1.86­
1.97
16.9­
17.7
1.284
1.043
0.349
0.116
456
4CM043
Jet
A
1.93­
1.94
18.0­
19.2
1.265
1.033
0.351
0.115
453
1GE034
JP­
5
1.92
20.3
0.4070
0.3343
0.1190
0.0496
167
1GE035
JP­
5
1.92
20.3
0.4070
0.3343
0.1190
0.0496
167
5GE084
Jet
A
1.92
20.30
0.3991
0.3288
0.1160
0.0489
164
5GE083
Jet
A
1.93
16.87
0.6042
0.4941
0.1681
0.0690
239
6GE096
Jet
A
1.937
18
0.6080
0.4790
0.1702
0.0703
239
6GE092
Jet
A
1.937
18
0.6481
0.5297
0.1793
0.0643
240
6GE093
Jet
A
1.937
18
0.5906
0.4850
0.1680
0.0620
226
6GE094
Jet
A
1.937
18
0.6518
0.5326
0.1800
0.0644
241
6GE095
Jet
A
1.937
18
0.6914
0.5632
0.1876
0.066
251
3GE067
Jet
A
1.935
16.3
2.027
1.663
0.592
0.163
701
1GE005
Jet
A
1.92
17.1
2.058
1.716
0.583
0.200
765
3GE068
Jet
A
1.935
16.3
2.027
1.663
0.592
0.163
701
3GE069
Jet
A
1.935
16.3
2.168
1.787
0.625
0.163
731
1GE006
Jet
A
1.92
17.1
2.379
1.915
0.643
0.212
838
3GE070
Jet
A
1.935
16.3
2.281
1.875
0.641
0.163
751
3GE073
Jet
A
1.935
16.3
2.361
1.940
0.663
0.163
769
1GE007
Jet
A
1.92
17.1
2.487
1.975
0.660
0.215
859
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
CF
CG
CH
CI
CJ
CK
CL
CM
UID
No
Baro
Temp
Humidity
kW
@
Power
%
CF
@
Power
kPa
K
kg/
kg
­­­­­­­­­­­­­­­­­­­
Ambient­­­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­
Loads­­­­­­­­­­­­­­­­­­­

Power
Extraction
­­­
Stage
Bleed­­­

97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
7CM047
0
­
0
­
97.77
­
98.11
286
­
295
0.0061
­
0.0074
3CM029
0
­
0
­
97.8­
98.0
294­
297
.0100­.
0157
3CM030
0
­
0
­
97.8­
98.0
294­
297
.0100­.
0157
4CM039
0
­
0
­
97.9­
98.0
292.8­
296.7
.00814­.
0131
3CM031
0
­
0
­
97.8­
98.0
294­
297
.0100­.
0157
4CM040
0
­
0
­
97.9­
98.0
292.8­
296.7
.00814­.
0131
3CM032
0
­
0
­
97.8­
98.0
294­
297
.0100­.
0157
4CM041
0
­
0
­
97.9­
98.0
292.8­
296.7
.00814­.
0131
3CM033
0
­
0
­
97.8­
98.0
294­
297
.0100­.
0157
4CM042
0
­
0
­
97.9­
98.0
292.8­
296.7
.00814­.
0131
3CM034
0
­
0
­
97.8­
98.0
294­
297
.0100­.
0157
4CM043
0
­
0
­
97.9­
98.0
292.8­
296.7
.00814­.
0131
1GE034
0
­
0
­
101.6­
102.9
275.5­
281.1
.0016­.
0039
1GE035
0
­
0
­
101.6­
102.9
275.5­
281.1
.0016­.
0039
5GE084
0
­
0
­
101.6­
102.9
275.5­
281.1
.0016­.
0039
5GE083
0
­
0
­
96.87
­
97.62
287
­
296.4
.0056
­
.00656
6GE096
0
­
0
­
97.1
­
98.1
284
­
292
0.00470
­
0.00727
6GE092
0
­
0
­
97.1
­
98.1
284
­
292
.00470
­
.00727
6GE093
0
­
0
­
97.1
­
98.1
284
­
292
.00470
­
.00727
6GE094
0
­
0
­
97.1
­
98.1
284
­
292
.00470
­
.00727
6GE095
0
­
0
­
97.1
­
98.1
284
­
292
.00470
­
.00727
3GE067
0
­
0
­
97.73­
97.91
292.3­
301.3
.0127­.
0216
1GE005
0
­
0
­
98.3­
100.4
270
­
296
.0027­.
0103
3GE068
0
­
0
­
97.73­
97.91
292.3­
301.3
.0127­.
0216
3GE069
0
­
0
­
97.73­
97.91
292.3­
301.3
.0127­.
0216
1GE006
0
­
0
­
98.3­
100.4
270
­
296
.0027­.
0103
3GE070
0
­
0
­
97.73­
97.91
292.3­
301.3
.0127­.
0216
3GE073
0
­
0
­
97.73­
97.91
292.3­
301.3
.0127­.
0216
1GE007
0
­
0
­
98.3­
100.4
270
­
296
.0027­.
0103
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
CN
CO
CP
CQ
CR
CS
UID
­­­
Test
Dates­­­

No
Manufacturer
Test
Organisation
Test
Location
From
To
97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
7CM047
CFM
International
CFM56
Evaluation
Engineering
PTO
Site
IV­
D
Jun­
91
Jun­
91
3CM029
GE
CFM56­
7B
Eval
Engineering
Peebles
Test
Operation,
Peebles,
Ohio,
USA
Jul­
96
3CM030
GE
CFM56­
7B
Eval
Engineering
Peebles
Test
Operation,
Peebles,
Ohio,
USA
Jul­
96
4CM039
GE
CFM56­
7B
Eval
Engineering
Peebles
Test
Operation
(
PTO)
Peebles,
OH
30­
Aug­
97
12­
Sep­
97
3CM031
GE
CFM56­
7B
Eval
Engineering
Peebles
Test
Operation,
Peebles,
Ohio,
USA
Jul­
96
4CM040
GE
CFM56­
7B
Eval
Engineering
Peebles
Test
Operation
(
PTO)
Peebles,
OH
30­
Aug­
97
12­
Sep­
97
3CM032
GE
CFM56­
7B
Eval
Engineering
Peebles
Test
Operation,
Peebles,
Ohio,
USA
Jul­
96
4CM041
GE
CFM56­
7B
Eval
Engineering
Peebles
Test
Operation
(
PTO)
Peebles,
OH
30­
Aug­
97
12­
Sep­
97
3CM033
GE
CFM56­
7B
Eval
Engineering
Peebles
Test
Operation,
Peebles,
Ohio,
USA
Jul­
96
4CM042
GE
CFM56­
7B
Eval
Engineering
Peebles
Test
Operation
(
PTO)
Peebles,
OH
30­
Aug­
97
12­
Sep­
97
3CM034
GE
CFM56­
7B
Eval
Engineering
Peebles
Test
Operation,
Peebles,
Ohio,
USA
Jul­
96
4CM043
GE
CFM56­
7B
Eval
Engineering
Peebles
Test
Operation
(
PTO)
Peebles,
OH
30­
Aug­
97
12­
Sep­
97
1GE034
GE
Aircraft
Engines
GE
Aircraft
Engines,
Lynn,
MA
Lynn
Cell
121
21­
Mar­
91
23­
Mar­
91
1GE035
GE
Aircraft
Engines
GE
Aircraft
Engines,
Lynn,
MA
Lynn
Cell
121
21­
Mar­
91
23­
Mar­
91
5GE084
GE
GE
Aircraft
Engines,
Lynn,
MA
Lynn
Cell
121
21­
Mar­
91
25­
Mar­
91
5GE083
GE
Peebles
Test
Opeation
Peebles,
Ohio
6GE096
GE
Aircraft
Engines
Peebles
Test
Operation
Peebles,
Ohio
27­
Jan­
02
28­
Jan­
02
6GE092
GE
Aircraft
Engines
Peebles
Test
Operation
Peebles,
Ohio
27­
Jan­
02
28­
Jan­
02
6GE093
GE
Aircraft
Engines
Peebles
Test
Organisation
Peebles,
Ohio
27­
Jan­
02
28­
Jan­
02
6GE094
GE
Aircraft
Engines
Peebles
Test
Organisation
Peebles,
Ohio
27­
Jan­
02
28­
Jan­
02
6GE095
GE
Aircraft
Engines
Peebles
Test
Organisation
Peebles,
Ohio
27­
Jan­
02
28­
Jan­
02
3GE067
GE
GE
Development/
Production
Test
Operation
Site
IVD,
Peebles,
Ohio
28­
Jul­
87
29­
Jul­
87
1GE005
GE
Aircraft
Engines
Production
Engine
Test
Production
Test
Cells
M34
&
M35
12­
Oct­
79
5­
Dec­
79
3GE068
GE
GE
Development/
Production
Test
Operation
Site
IVD,
Peebles,
Ohio
28­
Jul­
87
29­
Jul­
87
3GE069
GE
GE
Development/
Production
Test
Operation
Site
IVD,
Peebles,
Ohio
28­
Jul­
87
29­
Jul­
87
1GE006
GE
Aircraft
Engines
Production
Engine
Test
Production
Test
Cells
M34
&
M35
12­
Oct­
79
5­
Dec­
79
3GE070
GE
GE
Development/
Production
Test
Operation
Site
IVD,
Peebles,
Ohio
28­
Jul­
87
29­
Jul­
87
3GE073
GE
GE
Development/
Production
Test
Operation
Site
IVD,
Peebles,
Ohio
28­
Jul­
87
29­
Jul­
87
1GE007
GE
Aircraft
Engines
Production
Engine
Test
Production
Test
Cells
M34
&
M35
12­
Oct­
79
5­
Dec­
79
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
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for
latest
version
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aviation_
emissions_
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Data
1
2
3
CT
CU
UID
No
Remarks
97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
7CM047
1.
Ref
GE
Report
R91AEB471
and
FAA
Certification
Report
CR­
897/
P,
July
2003
2.
Engine
S/
N
740­
105
3.
Data
also
applies
to
CFM56­
5C4/
1P
3CM029
1.
FAA
Certification
Report
CR­
997,
Dec
96.
2.
Engine
S/
N
874­
101/
01
3CM030
1.
FAA
Certification
Report
CR­
997,
Dec
96.
2.
Engine
S/
N
874­
101/
01
4CM039
1.
FAA
Certification
Report
CR­
997/
2,
14
Nov
97
2.
Engine
S/
N
874­
136/
01,
874­
141/
01,
874­
146/
01
3CM031
1.
FAA
Certification
Report
CR­
997,
Dec
96.
2.
Engine
S/
N
874­
101/
01
4CM040
1.
FAA
Certification
Report
CR­
997/
2,
14
Nov
97
2.
Engine
S/
N
874­
136/
01,
874­
141/
01,
874­
146/
01
3CM032
1.
FAA
Certification
Report
CR­
997,
Dec
96.
2.
Engine
S/
N
874­
101/
01
4CM041
1.
FAA
Certification
Report
CR­
997/
2,
14
Nov
97
2.
Engine
S/
N
874­
136/
01,
874­
141/
01,
874­
146/
01
3CM033
1.
FAA
Certification
Report
CR­
997,
Dec
96.
2.
Engine
S/
N
874­
101/
01
4CM042
1.
FAA
Certification
Report
CR­
997/
2,
14
Nov
97
2.
Engine
S/
N
874­
136/
01,
874­
141/
01,
874­
146/
01
3CM034
1.
FAA
Certification
Report
CR­
997,
Dec
96.
2.
Engine
S/
N
874­
101/
01
4CM043
1.
FAA
Certification
Report
CR­
997/
2,
14
Nov
97
2.
Engine
S/
N
874­
136/
01,
874­
141/
01,
874­
146/
01
1GE034
1.
Ref
GE
Report
R91AEB051
(
1/
92
rev).
2.
Engine
S/
N
807­
005.
3.
LEC
II
combustor.

1GE035
1.
Ref
GE
Report
R91AEB051
(
1/
92
rev).
2.
Engine
S/
N
807­
005.
3.
LEC
II
combustor.

5GE084
1.
Ref.
GE
Report
R95AEB012
2.
Engine
S/
N
807­
005
5GE083
1.
Ref.
GE
Report
R99AEB031.
2.
Engine
S/
S
965202.

6GE096
1.
GE
Report
R2001AE078
2.
Engine
S/
N
193111
6GE092
1.
GE
Report
R2001AE078
2.
Engine
S/
N
193111
3.
LEC
combustor
6GE093
1.
GE
Report
R2001AE078
2.
Engine
S/
N
193111
3.
LEC
combustor
6GE094
1.
GE
Report
R2001AE078
2.
Engine
S/
N
193111
3.
LEC
combustor
6GE095
1.
GE
Report
R2001AE078
2.
Engine
S/
N
193111
3.
LEC
combustor
3GE067
1.
Engine
equipped
with
low
emissions
fuel
nozzle
config.
2.
GE
Report
R87AEB559.
3.
Engine
530375/
001.
4.
Asterisked
idle
emissions
calculate
1GE005
Ref
Report
no
FAA­
EE­
80­
27
(
GE
Report
R80AEG420)

3GE068
1.
Engine
equipped
with
low
emissions
fuel
nozzle
config.
2.
GE
Report
R87AEB559.
3.
Engine
530375/
001.
4.
Asterisked
idle
emissions
calculate
3GE069
1.
Engine
equipped
with
low
emissions
fuel
nozzle
config.
2.
GE
Report
R87AEB559.
3.
Engine
530375/
001.
4.
Asterisked
idle
emissions
calculate
1GE006
Ref
Report
no
FAA­
EE­
80­
27
(
GE
Report
R80AEG420)

3GE070
1.
Engine
equipped
with
low
emissions
fuel
nozzle
config.
2.
GE
Report
R87AEB559.
3.
Engine
530375/
001.
4.
Asterisked
idle
emissions
calculate
3GE073
1.
Engine
equipped
with
low
emissions
fuel
nozzle
config.
2.
GE
Report
R87AEB559.
3.
Engine
530375/
001.
4.
Asterisked
idle
emissions
calculate
1GE007
Ref
Report
no
FAA­
EE­
80­
27
(
GE
Report
R80AEG420)

Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
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aviation_
emissions_
databank
Data
1
2
3
CV
CW
CX
CY
CZ
DA
DB
DC
DD
DE
DF
DG
DH
97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
Engine
S/
N
740­
105
Data
also
a
0
ted
at
normal
idle
setting
rather
than
7%.

ted
at
normal
idle
setting
rather
than
7%.

ted
at
normal
idle
setting
rather
than
7%.

ted
at
normal
idle
setting
rather
than
7%.

ted
at
normal
idle
setting
rather
than
7%.

Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
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aviation_
emissions_
databank
Data
1
2
3
DI
DJ
DK
DL
DM
DN
97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
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QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
A
B
C
D
E
F
G
UID
Engine
Combustor
Eng
B/
P
Press
Rated
No
Identification
Description
Type
Ratio
Ratio
Output
kN
129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
145
146
147
148
149
150
151
152
153
154
155
156
157
158
159
160
3GE074
CF6­
50C2
Low
emissions
fuel
nozzle
TF
4.3
28.44
230.4
3GE078
CF6­
50C2B
Low
emissions
fuel
nozzle
TF
4.3
29.06
236.7
1GE008
CF6­
50C2R
TF
4.3
28.8
224.2
3GE072
CF6­
50C2R
Low
emissions
fuel
nozzle
TF
4.3
27.76
224.2
3GE071
CF6­
50CA
Low
emissions
fuel
nozzle
TF
4.3
27.76
224.2
3GE075
CF6­
50E
Low
emissions
fuel
nozzle
TF
4.3
28.44
230.4
3GE076
CF6­
50E1
Low
emissions
fuel
nozzle
TF
4.3
28.44
230.4
1GE009
CF6­
50E2
TF
4.3
29.8
230.4
3GE077
CF6­
50E2
Low
emissions
fuel
nozzle
TF
4.3
28.44
230.4
3GE079
CF6­
50E2B
Low
emissions
fuel
nozzle
TF
4.3
29.06
236.7
1GE001
CF6­
6D
TF
5.9
24.7
174.8
1GE002
CF6­
6D1A
TF
5.9
25.4
181.9
1GE003
CF6­
6K
TF
5.9
24.7
174.8
1GE004
CF6­
6K2
TF
5.9
25.4
181.9
1GE010
CF6­
80A
TF
5
29.0
208.8
1GE011
CF6­
80A1
TF
5
29.0
209.0
1GE012
CF6­
80A2
TF
5
30.1
216.5
1GE013
CF6­
80A3
TF
5
30.1
217.8
1GE014
CF6­
80C2A1
TF
5.1
30.96
257.4
2GE036
CF6­
80C2A1
1862M39
TF
5.1
30.53
257.40
1GE015
CF6­
80C2A2
TF
5.1
28
233.35
1GE016
CF6­
80C2A2
TF
5.1
28.0
233.35
2GE037
CF6­
80C2A2
1862M39
TF
5.1
27.79
233.35
1GE017
CF6­
80C2A3
TF
5.1
31.64
262.22
1GE018
CF6­
80C2A3
TF
5.1
31.64
262.22
2GE038
CF6­
80C2A3
1862M39
TF
5.1
31.09
262.22
1GE019
CF6­
80C2A5
TF
5.1
31.58
267.3
1GE020
CF6­
80C2A5
TF
5.1
31.58
267.3
2GE039
CF6­
80C2A5
1862M39
TF
5.1
31.66
267.34
3GE056
CF6­
80C2A5F
1862M39
TF
5.1
32.88
271.88
1GE021
CF6­
80C2A8
TF
5.1
31.0
257.4
2GE040
CF6­
80C2A8
1862M39
TF
5.1
30.45
257.37
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
H
I
J
K
L
M
N
O
P
Q
R
S
T
U
UID
Data
Superseded
Data
No
PR
C
R
superseded
by
NME
DTEPS
Other
Corr
as
Out
of
Date
Out
of
Date
UID
No
Annex
16
Production
Service
­­­­­­­­
Data
Status­­­­­­­­
­­­­­­­­­­
Current
Engine
Status
­­­­­­­­­­

­­­­­­
Test
Engine
Status­­­­­­

129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
145
146
147
148
149
150
151
152
153
154
155
156
157
158
159
160
3GE074
­
x
­
­
­
x
­
­
x
x
­
­
­

3GE078
­
x
­
­
­
x
­
­
x
x
­
­
­

1GE008
x
­
­
­
­
x
­
­
x
x
­
­
­

3GE072
­
x
­
­
­
x
­
­
x
x
­
­
­

3GE071
­
x
­
­
­
x
­
­
x
x
­
­
­

3GE075
­
x
­
­
­
x
­
­
x
x
­
­
­

3GE076
­
x
­
­
­
x
­
­
x
x
­
­
­

1GE009
x
­
­
­
­
x
­
­
x
x
­
­
­

3GE077
­
x
­
­
­
x
­
­
x
x
­
­
­

3GE079
­
x
­
­
­
x
­
­
x
x
­
­
­

1GE001
x
­
­
­
­
x
­
­
x
x
­
­
­

1GE002
x
­
­
­
­
x
­
­
x
x
­
­
­

1GE003
x
­
­
­
­
x
­
­
x
x
­
­
­

1GE004
x
­
­
­
­
x
­
­
x
x
­
­
­

1GE010
x
­
­
­
­
x
­
­
x
x
­
­
­

1GE011
x
­
­
­
­
x
­
­
x
x
­
­
­

1GE012
x
­
­
­
­
x
­
­
x
x
­
­
­

1GE013
x
­
­
­
­
x
­
­
x
x
­
­
­

1GE014
­
x
­
­
­
x
­
­
x
x
­
­
­

2GE036
­
x
­
­
­
x
­
­
x
­
­
­
­

1GE015
­
x
­
x
1GE016
x
­
­
x
x
­
­
­

1GE016
­
­
x
­
­
x
­
­
x
x
­
­
­

2GE037
­
x
­
­
­
x
­
­
x
­
­
­
­

1GE017
­
x
­
x
1GE018
x
­
­
x
x
­
­
­

1GE018
­
­
x
­
­
x
­
­
x
x
­
­
­

2GE038
­
x
­
­
­
x
­
­
x
­
­
­
­

1GE019
­
x
­
x
1GE020
x
­
­
x
x
­
­
­

1GE020
­
­
x
­
­
x
­
­
x
x
­
­
­

2GE039
­
x
­
­
­
x
­
­
x
­
­
­
­

3GE056
­
x
­
­
­
x
­
­
x
­
­
­
­

1GE021
­
x
­
­
­
x
­
­
x
x
­
­
­

2GE040
­
x
­
­
­
x
­
­
x
­
­
­
­

Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
V
W
X
Y
Z
AA
AB
AC
AD
AE
AF
AG
AH
UID
Characteristic
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
%
of
Total
mass
Reg
limit
(
g)

­­­­­­­­­­­­­­­­
EI
HC­­­­­­­­­­­­­­
­­­
Number
­­­
­­­­­­­­­­­­­­­
Dp/
Foo
(
HC)­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­
­­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­­­­­

129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
145
146
147
148
149
150
151
152
153
154
155
156
157
158
159
160
3GE074
0.14
0.15
0.28
2.72*
3
1
3.42
0.15
3.28­
3.58
5.3
27.0
788
3GE078
0.13
0.15
0.26
2.72*
3
1
3.33
0.15
3.19­
3.48
5.1
26.0
786
1GE008
0.6
0.7
1.0
23.0
6
6
35.2
3.8
­
39.2
199.8
7998
3GE072
0.14
0.14
0.29
2.72*
3
1
3.47
0.09
3.38­
3.56
5.3
27.0
784
3GE071
0.14
0.14
0.29
2.72*
3
1
3.47
0.09
3.38­
3.56
5.3
27.0
784
3GE075
0.14
0.15
0.28
2.72*
3
1
3.42
0.15
3.28­
3.58
5.3
27.0
788
3GE076
0.14
0.15
0.28
2.72*
3
1
3.42
0.15
3.28­
3.58
5.3
27.0
788
1GE009
0.6
0.7
1.0
21.8
6
6
33.5
3.8
­
37.3
190.1
7715
3GE077
0.14
0.15
0.28
2.72*
3
1
3.42
0.15
3.28­
3.58
5.3
27.0
788
3GE079
0.13
0.15
0.26
2.72*
3
1
3.33
0.15
3.19­
3.48
5.1
26.0
786
1GE001
0.3
0.3
0.7
21.0
7
7
33.3
3.5
­
36.7
187.4
5821
1GE002
0.3
0.3
0.6
19.9
7
7
30.9
3.5
­
34.1
173.9
5617
1GE003
0.3
0.3
0.7
21.0
7
7
33.3
3.5
­
36.7
187.4
5821
1GE004
0.3
0.3
0.6
19.9
7
7
30.9
3.5
­
34.1
173.9
5617
1GE010
0.29
0.29
0.47
6.29
3
1
7.84
0.95
7.17­
8.93
12.1
61.7
1636
1GE011
0.29
0.29
0.47
6.29
3
1
7.83
0.95
7.16­
8.92
12.1
61.7
1636
1GE012
0.30
0.37
0.45
6.28
3
1
7.58
0.96
6.91­
8.69
11.7
59.7
1659
1GE013
0.30
0.37
0.45
6.28
3
1
7.53
0.96
6.87­
8.64
11.6
59.2
1659
1GE014
0.08
0.09
0.20
9.19
3
2
11.32
1.27
10.24­
12.65
14.7
75.2
2915
2GE036
0.05
0.05
0.12
1.59
4
2
2.07
0.234
1.94­
2.45
2.7
13.7
536
1GE015
0.14
0.11
0.25
10.74
3
2
13.86
1.25
12.42­
14.60
18.0
92.0
3239
1GE016
0.08
0.10
0.23
10.48
3
2
13.50
1.25
12.42­
14.60
17.6
89.6
3152
2GE037
0.05
0.05
0.12
1.90
4
2
2.58
0.293
2.37­
2.99
3.4
17.1
602
1GE017
0.08
0.10
0.21
9.21
3
2
11.30
1.29
9.85­
12.32
14.7
75.0
2970
1GE018
0.06
0.08
0.19
8.94
3
2
10.94
1.29
9.85­
12.32
14.2
72.6
2874
2GE038
0.04
0.05
0.11
1.54
4
2
1.99
0.22
1.85­
2.34
2.6
13.2
523
1GE019
0.07
0.08
0.20
8.99
3
2
11.12
1.30
10.02­
12.49
14.5
73.8
2966
1GE020
0.07
0.08
0.20
8.99
3
2
11.12
1.30
10.02­
12.49
14.5
73.8
2966
2GE039
0.04
0.05
0.11
1.48
4
2
1.90
0.209
1.76­
2.24
2.5
12.6
509
3GE056
0.05
0.04
0.11
1.18
4
2
1.63
­
­
2.1
10.7
440
1GE021
0.08
0.09
0.20
9.2
3
2
11.6
1.31
10.52­
13.00
15.1
77.0
3005
2GE040
0.05
0.05
0.12
1.59
4
2
2.08
0.233
1.94­
2.45
2.7
13.8
536
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
AI
AJ
AK
AL
AM
AN
AO
AP
AQ
AR
AS
AT
AU
UID
Characteristic
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
%
of
Total
mass
Reg
limit
(
g)

­­­­­­­­­­­­­­­­­
EI
CO­­­­­­­­­­­­­­­­­
­­­­­­
Number­­­­­
­­­­­­­­­­­­­­­
Dp/
Foo
(
CO)­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­­­

129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
145
146
147
148
149
150
151
152
153
154
155
156
157
158
159
160
3GE074
0.45
0.45
3.71
24.04*
3
1
29.80
0.44
29.42­
30.28
36.6
31.0
6863
3GE078
0.46
0.44
3.42
24.04*
3
1
28.88
0.407
28.50­
29.31
35.4
30.0
6823
1GE008
0.5
0.5
5.2
62.3
6
6
95.1
4.6
­
100.5
85.1
21583
3GE072
0.44
0.46
3.99
24.04*
3
1
30.73
0.48
30.32­
31.25
37.7
31.9
6883
3GE071
0.44
0.46
3.99
24.04*
3
1
30.73
0.48
30.32­
31.25
37.7
31.9
6883
3GE075
0.45
0.45
3.71
24.04*
3
1
29.80
0.44
29.42­
30.28
36.6
31.0
6863
3GE076
0.45
0.45
3.71
24.04*
3
1
29.80
0.44
29.42­
30.28
36.6
31.0
6863
1GE009
0.5
0.5
4.3
61.8
6
6
93.7
4.6
­
99.0
83.9
21591
3GE077
0.45
0.45
3.71
24.04*
3
1
29.80
0.44
29.42­
30.28
36.6
31.0
6863
3GE079
0.46
0.44
3.42
24.04*
3
1
28.88
0.407
28.50­
29.31
35.4
30.0
6823
1GE001
0.5
0.5
6.5
54.2
7
7
88.7
6.9
­
93.3
79.1
15496
1GE002
0.5
0.5
5.5
52.0
7
7
82.8
6.9
­
87.1
73.8
15066
1GE003
0.5
0.5
6.5
54.2
7
7
88.7
6.9
­
93.3
79.1
15496
1GE004
0.5
0.5
5.5
52.0
7
7
82.8
6.9
­
87.1
73.8
15066
1GE010
1.0
1.1
3.1
28.2
3
1
35.5
0.4
35.0­
35.9
43.6
36.9
7407
1GE011
1.0
1.1
3.1
28.2
3
1
35.5
0.4
35.0­
35.9
43.6
36.9
7407
1GE012
1.0
1.1
2.8
28.2
3
1
34.2
0.4
33.8­
34.5
42.0
35.6
7398
1GE013
1.0
1.1
2.8
28.2
3
1
34.0
0.4
33.6­
34.3
41.7
35.3
7398
1GE014
0.56
0.54
2.19
42.24
3
2
53.04
3.04
50.41­
55.78
60.4
51.2
13643
2GE036
0.05
0.04
2.05
19.76
4
2
25.37
1.18
24.3­
27.1
28.9
24.5
6532
1GE015
0.58
0.56
3.04
46.65
3
2
61.53
3.08
57.97­
63.34
70.1
59.4
14358
1GE016
0.57
0.55
2.94
46.01
3
2
60.64
3.08
57.97­
63.34
69.1
58.6
14152
2GE037
0.04
0.05
2.56
21.97
4
2
29.81
1.33
28.7­
31.5
34.0
28.8
6958
1GE017
0.59
0.57
2.15
42.18
3
2
52.67
3.03
49.18­
54.56
60.0
50.9
13838
1GE018
0.58
0.56
2.07
41.51
3
2
51.80
3.03
49.18­
54.56
59.0
50.0
13611
2GE038
0.06
0.04
1.98
19.32
4
2
24.58
1.19
23.4­
26.3
28.0
23.7
6450
1GE019
0.52
0.52
1.93
41.65
3
2
52.35
3.03
49.73­
55.20
59.6
50.5
13967
1GE020
0.52
0.52
1.93
41.65
3
2
52.35
3.03
49.73­
55.20
59.6
50.5
13967
2GE039
0.06
0.04
1.91
18.89
4
2
23.78
1.96
22.6­
25.5
27.1
23.0
6367
3GE056
0.05
0.04
1.92
16.96
4
2
22.68
­
­
25.8
21.9
6156
1GE021
0.52
0.52
2.05
42.3
3
2
54.4
3.09
51.75­
57.31
62.0
52.5
14039
2GE040
0.05
0.04
2.05
19.76
4
2
25.35
1.18
24.3­
27.1
28.9
24.5
6532
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
AV
AW
AX
AY
AZ
BA
BB
BC
BD
BE
BF
BG
BH
BI
BJ
UID
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
Original
CAEP
2
CAEP
4
Total
mass
(
g)

­­­­
Number­­­­­

­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­
EI
NOx­­­­­­­­­­­­­­
­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­
Dp/
Foo
(
NOx)­­­­­­­­­­­­­­
Characteristic
as
%
of
standards
129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
145
146
147
148
149
150
151
152
153
154
155
156
157
158
159
160
3GE074
28.97
25.50
10.16
3.4*
3
1
51.58
2.80
49.71­
54.80
59.8
61.7
77.2
92.7
11884
3GE078
29.59
26.34
10.49
3.4*
3
1
52.87
2.73
51.06­
56.10
61.3
62.5
78.1
93.6
12482
1GE008
35.0
29.0
9.4
3.5
6
6
60.2
0.5
­
62.7
64.2
80.3
96.3
13436
3GE072
28.03
24.30
10.09
3.4*
3
1
49.59
2.93
47.66­
52.96
57.5
60.2
75.2
90.7
11116
3GE071
28.03
24.30
10.09
3.4*
3
1
49.59
2.93
47.66­
52.96
57.5
60.2
75.2
90.7
11116
3GE075
28.97
25.50
10.16
3.4*
3
1
51.58
2.80
49.71­
54.80
59.8
61.7
77.2
92.7
11884
3GE076
28.97
25.50
10.16
3.4*
3
1
51.58
2.80
49.71­
54.80
59.8
61.7
77.2
92.7
11884
1GE009
36.3
29.7
9.5
3.6
6
6
61.8
0.5
­
64.3
64.6
80.7
96.5
14247
3GE077
28.97
25.50
10.16
3.4*
3
1
51.58
2.80
49.71­
54.80
59.8
61.7
77.2
92.7
11884
3GE079
29.59
26.34
10.49
3.4*
3
1
52.87
2.73
51.06­
56.10
61.3
62.5
78.1
93.6
12482
1GE001
40.0
32.6
11.4
4.5
7
7
66.4
2.3
­
68.9
77.1
96.4
117.8
11611
1GE002
41.6
33.9
11.8
4.6
7
7
69.0
2.3
­
71.6
78.9
98.6
120.1
12549
1GE003
40.0
32.6
11.4
4.5
7
7
66.4
2.3
­
68.9
77.1
96.4
117.8
11611
1GE004
41.6
33.9
11.8
4.6
7
7
69.0
2.3
­
71.6
78.9
98.6
120.1
12549
1GE010
29.8
25.6
10.3
3.4
3
1
53.1
3.0
49.6­
55.4
61.6
62.9
78.6
94.2
11066
1GE011
29.8
25.6
10.3
3.4
3
1
53.0
3.0
49.6­
55.3
61.4
62.7
78.3
93.9
11066
1GE012
29.6
26.6
10.8
3.4
3
1
55.5
2.9
52.4­
58.1
64.3
64.2
80.2
95.7
11878
1GE013
29.6
26.6
10.8
3.4
3
1
55.2
2.9
52.1­
57.7
64.0
63.9
79.8
95.2
11878
1GE014
32.22
24.85
9.76
3.99
3
2
48.12
0.53
47.41­
48.43
52.9
51.9
64.9
76.8
12382
2GE036
26.55
20.45
12.43
4.68
4
2
44.72
0.31
44.3­
45.0
49.2
48.7
60.8
72.3
11514
1GE015
27.90
20.71
9.52
3.91
3
2
41.70
0.42
41.31­
42.14
45.9
47.8
59.7
71.9
9729
1GE016
27.93
20.69
9.44
3.95
3
2
41.68
0.42
41.31­
42.14
45.8
47.7
59.7
71.8
9728
2GE037
22.35
18.37
11.86
4.49
4
2
40.01
0.236
39.7­
40.3
44.0
46.0
57.5
69.3
9339
1GE017
34.44
25.45
10.01
3.96
3
2
49.91
0.40
49.63­
50.42
54.9
53.1
66.4
78.1
13090
1GE018
34.50
25.46
9.93
3.92
3
2
49.84
0.44
49.63­
50.42
54.8
53.1
66.3
78.0
13074
2GE038
27.68
21.05
12.48
4.72
4
2
46.03
0.56
45.5­
46.8
50.6
49.5
61.9
73.2
12074
1GE019
30.85
22.86
9.11
3.79
3
2
46.31
2.16
44.62­
48.92
50.9
49.4
61.7
72.6
12353
1GE020
34.38
22.86
9.11
3.79
3
2
49.25
2.23
46.22­
49.73
54.2
52.5
65.6
77.2
12735
2GE039
28.57
21.69
12.53
4.76
4
2
47.28
0.5
46.7­
47.9
52.0
50.3
62.9
73.9
12640
3GE056
28.11
21.27
12.64
4.90
4
2
47.07
­
­
51.8
49.0
61.2
71.2
12796
1GE021
33.5
22.0
9.0
3.7
3
2
45.8
1.75
44.33­
47.72
50.4
49.4
61.7
73.0
11797
2GE040
26.42
20.45
12.43
4.68
4
2
44.63
0.312
44.2­
44.9
49.1
48.6
60.8
72.3
11491
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
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aviation_
emissions_
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Data
1
2
3
BK
BL
BM
BN
BO
BP
BQ
BR
BS
BT
BU
BV
UID
Characteristic
No
T/
O
C/
O
App
Idle
Test
Eng
Max
Sigma
Range
Characteristic
%
of
Reg
limit
­­­­­­­­­­­­­­
Smoke
Number­­­­­­­­­­­­­

­­­­­­­­­­­­­
Smoke
Number­­­­­­­­­­­­­
­­­­
Number­­­­

129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
145
146
147
148
149
150
151
152
153
154
155
156
157
158
159
160
3GE074
10.95
11.72
1.62
1.4*
3
1
12.52
1.79
10.68­
14.00
16.1
85.5
3GE078
11.17
11.62
1.58
1.4*
3
1
12.52
1.79
10.68­
14.00
16.1
86.1
1GE008
3.9
2.6
2.8
4.5
6
6
4.5
1.5
­
4.8
25.3
3GE072
11.41
11.83
1.61
1.4*
3
1
12.52
1.79
10.68­
14.00
16.1
84.9
3GE071
11.41
11.83
1.61
1.4*
3
1
12.52
1.79
10.68­
14.00
16.1
84.9
3GE075
10.95
11.72
1.62
1.4*
3
1
12.52
1.79
10.68­
14.00
16.1
85.5
3GE076
10.95
11.72
1.62
1.4*
3
1
12.52
1.79
10.68­
14.00
16.1
85.5
1GE009
4.1
2.7
2.7
4.5
6
6
4.5
1.5
­
4.8
25.5
3GE077
10.95
11.72
1.62
1.4*
3
1
12.52
1.79
10.68­
14.00
16.1
85.5
3GE079
11.17
11.62
1.58
1.4*
3
1
12.52
1.79
10.68­
14.00
16.1
86.1
1GE001
4
3
3
4
7
7
4
2.2
­
4.3
20.9
1GE002
4
3
3
4
7
7
­
2.2
­
­

1GE003
4
3
3
4
7
7
4
2.2
­
4.3
20.9
1GE004
4
3
3
4
7
7
­
2.2
­
­

1GE010
12
10
2
2
1
1
12
­
­
15.6
80.6
1GE011
12
10
2
2
1
1
12
­
­
15.6
80.7
1GE012
12
10
2
2
1
1
12
­
­
15.6
81.4
1GE013
12
10
2
2
1
1
12
­
­
15.6
81.6
1GE014
8.2
­
­
­
3
2
8.2
1.2
6.0­
8.2
9.6
52.6
2GE036
7.0
4.7
0.0
0.0
4
2
7.0
0.74
6.1­
7.8
8.2
44.9
1GE015
6.5
­
­
­
3
2
6.5
1.0
5.4­
7.3
7.6
40.6
1GE016
6.5
­
­
­
3
2
6.5
1.0
5.4­
7.3
7.6
40.6
2GE037
5.8
3.2
0.0
0.0
4
2
5.8
0.63
5.1­
6.6
6.8
36.2
1GE017
7.8
­
­
­
3
2
7.8
1.3
6.3­
8.6
9.1
50.3
1GE018
7.8
­
­
­
3
2
7.8
1.3
6.3­
8.6
9.1
50.3
2GE038
6.9
5.0
0.0
0.0
4
2
6.9
0.91
5.8­
8.0
8.1
44.5
1GE019
7.8
­
­
­
3
2
7.8
1.3
6.1­
8.4
9.1
50.6
1GE020
7.8
­
­
­
3
2
7.8
1.3
6.1­
8.4
9.1
50.6
2GE039
6.94
5.36
0.0
0.0
4
2
6.9
0.91
5.9­
8.2
8.1
44.8
3GE056
7.4
5.2
0
0
4
2
7.4
­
­
8.7
48.3
1GE021
8.2
­
­
­
3
2
8.2
­
­
9.6
52.6
2GE040
6.97
4.70
0.0
0.0
4
2
7.0
0.739
6.0­
7.8
8.2
44.9
Filename
DCTM_
ARP.
xls
Printed
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emissions_
databank
Data
1
2
3
BW
BX
BY
BZ
CA
CB
CC
CD
CE
UID
Fuel
per
No
Spec
H/
C
Arom
T/
O
C/
O
App
Idle
LTO
cycle
Ratio
%
(
kg)

­­­­­­­­­­­­­­­­­
Fuel
Flow­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­(
kg/
sec)­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­­­­­
Fuel­­­­­­­­­­­­­­­­­­­­­­­

129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
145
146
147
148
149
150
151
152
153
154
155
156
157
158
159
160
3GE074
Jet
A
1.935
16.3
2.361
1.940
0.663
0.163
769
3GE078
Jet
A
1.935
16.3
2.410
1.997
0.667
0.163
779
1GE008
Jet
A
1.92
17.1
2.379
1.915
0.643
0.212
838
3GE072
Jet
A
1.935
16.3
2.281
1.875
0.641
0.163
751
3GE071
Jet
A
1.935
16.3
2.281
1.875
0.641
0.163
751
3GE075
Jet
A
1.935
16.3
2.361
1.940
0.663
0.163
769
3GE076
Jet
A
1.935
16.3
2.361
1.940
0.663
0.163
769
1GE009
Jet
A
1.92
17.1
2.487
1.975
0.660
0.215
859
3GE077
Jet
A
1.935
16.3
2.361
1.940
0.663
0.163
769
3GE079
Jet
A
1.935
16.3
2.410
1.997
0.667
0.163
779
1GE001
Jet
A
1.93
18.7
1.736
1.431
0.4839
0.1728
648
1GE002
Jet
A
1.93
18.7
1.812
1.502
0.494
0.176
667
1GE003
Jet
A
1.93
18.7
1.736
1.431
0.4839
0.1728
648
1GE004
Jet
A
1.93
18.7
1.812
1.502
0.494
0.176
667
1GE010
Jet
A
1.93
17.1
2.145
1.795
0.615
0.150
709
1GE011
Jet
A
1.93
17.1
2.145
1.795
0.615
0.150
709
1GE012
Jet
A
1.93
17.1
2.254
1.885
0.641
0.150
731
1GE013
Jet
A
1.93
17.1
2.254
1.885
0.641
0.150
731
1GE014
Jet
A
1.94
15.3
2.400
1.953
0.636
0.199
822
2GE036
Jet
A
1.94
15.3
2.453
1.989
0.651
0.201
835
1GE015
Jet
A
1.94
15.3
2.117
1.745
0.580
0.189
753
1GE016
Jet
A
1.94
15.3
2.117
1.745
0.580
0.189
753
2GE037
Jet
A
1.94
15.3
2.152
1.771
0.590
0.192
765
1GE017
Jet
A
1.94
15.3
2.457
2.003
0.649
0.202
838
1GE018
Jet
A
1.94
15.3
2.457
2.003
0.649
0.202
838
2GE038
Jet
A
1.94
15.3
2.516
2.041
0.662
0.203
851
1GE019
Jet
A
1.94
15.3
2.581
2.082
0.687
0.207
871
1GE020
Jet
A
1.94
15.3
2.581
2.082
0.687
0.207
871
2GE039
Jet
A
1.94
15.3
2.580
2.096
0.672
0.205
866
3GE056
Jet
A
1.94
15.3
2.630
2.106
0.691
0.22
897
1GE021
Jet
A
1.94
15.3
2.507
1.953
0.655
0.205
840
2GE040
Jet
A
1.94
15.3
2.444
1.989
0.651
0.201
835
Filename
DCTM_
ARP.
xls
Printed
on
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Check
website
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Data
1
2
3
CF
CG
CH
CI
CJ
CK
CL
CM
UID
No
Baro
Temp
Humidity
kW
@
Power
%
CF
@
Power
kPa
K
kg/
kg
­­­­­­­­­­­­­­­­­­­
Ambient­­­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­
Loads­­­­­­­­­­­­­­­­­­­

Power
Extraction
­­­
Stage
Bleed­­­

129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
145
146
147
148
149
150
151
152
153
154
155
156
157
158
159
160
3GE074
0
­
0
­
97.73­
97.91
292.3­
301.3
.0127­.
0216
3GE078
0
­
0
­
97.73­
97.91
292.3­
301.3
.0127­.
0216
1GE008
0
­
0
­
98.3­
100.4
270
­
296
.0027­.
0103
3GE072
0
­
0
­
97.73­
97.91
292.3­
301.3
.0127­.
0216
3GE071
0
­
0
­
97.73­
97.91
292.3­
301.3
.0127­.
0216
3GE075
0
­
0
­
97.73­
97.91
292.3­
301.3
.0127­.
0216
3GE076
0
­
0
­
97.73­
97.91
292.3­
301.3
.0127­.
0216
1GE009
0
­
0
­
98.3­
100.4
270
­
296
.0027­.
0103
3GE077
0
­
0
­
97.73­
97.91
292.3­
301.3
.0127­.
0216
3GE079
0
­
0
­
97.73­
97.91
292.3­
301.3
.0127­.
0216
1GE001
0
­
0
­
99.15­
100.46
280
­
301
.003­.
015
1GE002
0
­
0
­
99.15­
100.46
280
­
301
.003­.
015
1GE003
0
­
0
­
99.15­
100.46
280
­
301
.003­.
015
1GE004
0
­
0
­
99.15­
100.46
280
­
301
.003­.
015
1GE010
0
­
0
­
99.08­
99.78
275
­
277
.002
1GE011
0
­
0
­
99.08­
99.78
275
­
277
.002
1GE012
0
­
0
­
99.08­
99.78
275
­
277
.002
1GE013
0
­
0
­
99.08­
99.78
275
­
277
.002
1GE014
0
­
0
­
97.40­
97.82
287
­
296
.0084­.
0140
2GE036
0
­
0
­
97.61­
98.15
279­
293
.00457­.
00743
1GE015
0
­
0
­
97.40­
97.82
287
­
296
.0084­.
0140
1GE016
0
­
0
­
97.40­
97.82
287
­
296
.0084­.
0140
2GE037
0
­
0
­
97.61­
98.15
279­
293
.00457­.
00743
1GE017
0
­
0
­
97.40­
97.82
287
­
296
.0084­.
0140
1GE018
0
­
0
­
97.40­
97.82
287
­
296
.0084­.
0140
2GE038
0
­
0
­
97.61­
98.15
279­
293
.00457­.
00743
1GE019
0
­
0
­
97.40­
97.82
287
­
296
.0084­.
0140
1GE020
0
­
0
­
97.40­
97.82
287
­
296
.0084­.
0140
2GE039
0
­
0
­
97.61­
98.15
279­
293
.00457­.
00743
3GE056
0
­
0
­
97.61­
98.15
279­
293
.0046­.
0074
1GE021
0
­
0
­
97.40­
97.82
287
­
296
.0084­.
0140
2GE040
0
­
0
­
97.61­
98.15
279­
293
.00457­.
00743
Filename
DCTM_
ARP.
xls
Printed
on
5/
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05
Check
website
for
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aviation_
emissions_
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Data
1
2
3
CN
CO
CP
CQ
CR
CS
UID
­­­
Test
Dates­­­

No
Manufacturer
Test
Organisation
Test
Location
From
To
129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
145
146
147
148
149
150
151
152
153
154
155
156
157
158
159
160
3GE074
GE
GE
Development/
Production
Test
Operation
Site
IVD,
Peebles,
Ohio
28­
Jul­
87
29­
Jul­
87
3GE078
GE
GE
Development/
Production
Test
Operation
Site
IVD,
Peebles,
Ohio
28­
Jul­
87
29­
Jul­
87
1GE008
GE
Aircraft
Engines
Production
Engine
Test
Production
Test
Cells
M34
&
M35
12­
Oct­
79
5­
Dec­
79
3GE072
GE
GE
Development/
Production
Test
Operation
Site
IVD,
Peebles,
Ohio
28­
Jul­
87
29­
Jul­
87
3GE071
GE
GE
Development/
Production
Test
Operation
Site
IVD,
Peebles,
Ohio
28­
Jul­
87
29­
Jul­
87
3GE075
GE
GE
Development/
Production
Test
Operation
Site
IVD,
Peebles,
Ohio
28­
Jul­
87
29­
Jul­
87
3GE076
GE
GE
Development/
Production
Test
Operation
Site
IVD,
Peebles,
Ohio
28­
Jul­
87
29­
Jul­
87
1GE009
GE
Aircraft
Engines
Production
Engine
Test
Production
Test
Cells
M34
&
M35
12­
Oct­
79
5­
Dec­
79
3GE077
GE
GE
Development/
Production
Test
Operation
Site
IVD,
Peebles,
Ohio
28­
Jul­
87
29­
Jul­
87
3GE079
GE
GE
Development/
Production
Test
Operation
Site
IVD,
Peebles,
Ohio
28­
Jul­
87
29­
Jul­
87
1GE001
GE
Aircraft
Engines
Production
Engine
Test
Production
Test
Cells
M34
&
M35
16­
Aug­
79
19­
Nov­
79
1GE002
GE
Aircraft
Engines
Production
Engine
Test
Production
Test
Cells
M34
&
M35
16­
Aug­
79
19­
Nov­
79
1GE003
GE
Aircraft
Engines
Production
Engine
Test
Production
Test
Cells
M34
&
M35
16­
Aug­
79
19­
Nov­
79
1GE004
GE
Aircraft
Engines
Production
Engine
Test
Production
Test
Cells
M34
&
M35
16­
Aug­
79
19­
Nov­
79
1GE010
GE
Aircraft
Engines
Production
Engine
Test
Production
Test
Cells
M35
11­
Nov­
83
12­
Nov­
83
1GE011
GE
Aircraft
Engines
Production
Engine
Test
Production
Test
Cells
M35
11­
Nov­
83
12­
Nov­
83
1GE012
GE
Aircraft
Engines
Production
Engine
Test
Production
Test
Cells
M35
11­
Nov­
83
12­
Nov­
83
1GE013
GE
Aircraft
Engines
Production
Engine
Test
Production
Test
Cells
M35
11­
Nov­
83
12­
Nov­
83
1GE014
GE
Aircraft
Engines
CF6
Evaluation
Engineering
Site
IIIC,
PTO,
Peebles,
Ohio
29­
May­
85
3­
Jun­
85
2GE036
GE
CF6
Eval
Engineering
Site
IIIB,
PTO
Peebles
13­
Jan­
95
17­
Jan­
95
1GE015
GE
Aircraft
Engines
CF6
Evaluation
Engineering
Site
IIIC,
PTO,
Peebles,
Ohio
29­
May­
85
3­
Jun­
85
1GE016
GE
Aircraft
Engines
CF6
Evaluation
Engineering
Site
IIIC,
PTO,
Peebles,
Ohio
29­
May­
85
3­
Jun­
85
2GE037
GE
CF6
Eval
Engineering
Site
IIIB,
PTO
Peebles
13­
Jan­
95
17­
Jan­
95
1GE017
GE
Aircraft
Engines
CF6
Evaluation
Engineering
Site
IIIC,
PTO,
Peebles,
Ohio
29­
May­
85
3­
Jun­
85
1GE018
GE
Aircraft
Engines
CF6
Evaluation
Engineering
Site
IIIC,
PTO,
Peebles,
Ohio
29­
May­
85
3­
Jun­
85
2GE038
GE
CF6
Eval
Engineering
Site
IIIB,
PTO
Peebles
13­
Jan­
95
17­
Jan­
95
1GE019
GE
Aircraft
Engines
CF6
Evaluation
Engineering
Site
IIIC,
PTO,
Peebles,
Ohio
29­
May­
85
3­
Jun­
85
1GE020
GE
Aircraft
Engines
CF6
Evaluation
Engineering
Site
IIIC,
PTO,
Peebles,
Ohio
29­
May­
85
3­
Jun­
85
2GE039
GE
CF6
Eval
Engineering
Site
IIIB,
PTO
Peebles
13­
Jan­
95
17­
Jan­
95
3GE056
GE
CF6
Ecval
Engineering
Site
IIIB,
PTO,
Peebles,
Ohio,
USA
13­
Jan­
95
17­
Jan­
95
1GE021
GE
Aircraft
Engines
CF6
Evaluation
Engineering
Site
IIIC,
PTO,
Peebles,
Ohio
29­
May­
85
3­
Jun­
85
2GE040
GE
CF6
Eval
Engineering
Site
IIIB,
PTO
Peebles
13­
Jan­
95
17­
Jan­
95
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
CT
CU
UID
No
Remarks
129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
145
146
147
148
149
150
151
152
153
154
155
156
157
158
159
160
3GE074
1.
Engine
equipped
with
low
emissions
fuel
nozzle
config.
2.
GE
Report
R87AEB559.
3.
Engine
530375/
001.
4.
Asterisked
idle
emissions
calculate
3GE078
1.
Engine
equipped
with
low
emissions
fuel
nozzle
config.
2.
GE
Report
R87AEB559.
3.
Engine
530375/
001.
4.
Asterisked
idle
emissions
calculate
1GE008
Ref
Report
no
FAA­
EE­
80­
27
(
GE
Report
R80AEG420)

3GE072
1.
Engine
equipped
with
low
emissions
fuel
nozzle
config.
2.
GE
Report
R87AEB559.
3.
Engine
530375/
001.
4.
Asterisked
idle
emissions
calculate
3GE071
1.
Engine
equipped
with
low
emissions
fuel
nozzle
config.
2.
GE
Report
R87AEB559.
3.
Engine
530375/
001.
4.
Asterisked
idle
emissions
calculate
3GE075
1.
Engine
equipped
with
low
emissions
fuel
nozzle
config.
2.
GE
Report
R87AEB559.
3.
Engine
530375/
001.
4.
Asterisked
idle
emissions
calculate
3GE076
1.
Engine
equipped
with
low
emissions
fuel
nozzle
config.
2.
GE
Report
R87AEB559.
3.
Engine
530375/
001.
4.
Asterisked
idle
emissions
calculate
1GE009
Ref
Report
no
FAA­
EE­
80­
27
(
GE
Report
R80AEG420)

3GE077
1.
Engine
equipped
with
low
emissions
fuel
nozzle
config.
2.
GE
Report
R87AEB559.
3.
Engine
530375/
001.
4.
Asterisked
idle
emissions
calculate
3GE079
1.
Engine
equipped
with
low
emissions
fuel
nozzle
config.
2.
GE
Report
R87AEB559.
3.
Engine
530375/
001.
4.
Asterisked
idle
emissions
calculate
1GE001
Ref
Report
no
FAA­
EE­
80­
27
(
GE
Report
R80AEG420)

1GE002
Ref
Report
no
FAA­
EE­
80­
27
(
GE
Report
R80AEG420)

1GE003
Ref
Report
no
FAA­
EE­
80­
27
(
GE
Report
R80AEG420)

1GE004
Ref
Report
no
FAA­
EE­
80­
27
(
GE
Report
R80AEG420)

1GE010
1.
Ref
GE
Report
no
R83AEB635.
2.
Engine
S/
N
580214.
3.
Smoke
from
Engine
S/
N
580005,
report
R81AEG513.
4.
With
approval
of
US
FAA,
idle
p
1GE011
1.
Ref
GE
Report
no
R83AEB635.
2.
Engine
S/
N
580214.
3.
Smoke
from
Engine
S/
N
580005,
report
R81AEG513.
4.
With
approval
of
US
FAA,
idle
p
1GE012
1.
Ref
GE
Report
no
R83AEB635.
2.
Engine
S/
N
580214.
3.
Smoke
from
Engine
S/
N
580005,
report
R81AEG513.
4.
With
approval
of
US
FAA,
idle
p
1GE013
1.
Ref
GE
Report
no
R83AEB635.
2.
Engine
S/
N
580214.
3.
Smoke
from
Engine
S/
N
580005,
report
R81AEG513.
4.
With
approval
of
US
FAA,
idle
p
1GE014
1.
Ref
GE
Report
R84AEB152.
2.
Engine
S/
N's
690105
and
690005/
2.

2GE036
1.
Ref
GE
report
TM95­
17.
2.
Engine
S/
N
704/
233
&
704/
234
3.
1862M39
combustor
1GE015
1.
Ref
GE
Report
R85AEB486.
2.
Engine
S/
N's
690105
and
690005/
2.

1GE016
1.
Ref
GE
Report
R85AEB486.
2.
Engine
S/
N's
690105
and
690005/
2.

2GE037
1.
Ref
GE
report
TM95­
17.
2.
Engine
S/
N
704/
233
&
704/
234
3.
1862M39
combustor
1GE017
1.
Ref
GE
Report
R86AEB143.
2.
Engine
S/
N's
690105
and
690005/
2.

1GE018
1.
Ref
GE
Report
R86AEB143.
2.
Engine
S/
N's
690105
and
690005/
2.

2GE038
1.
Ref
GE
report
TM95­
17.
2.
Engine
S/
N
704/
233
&
704/
234
3.
1862M39
combustor
1GE019
1.
Ref
GE
Report
R84AEB152.
2.
Engine
S/
N's
690105
and
690005/
2.

1GE020
1.
Ref
GE
Report
R84AEB152.
2.
Engine
S/
N's
690105
and
690005/
2.

2GE039
1.
Ref
GE
report
TM95­
17.
2.
Engine
S/
N
704/
233
&
704/
234
3.
1862M39
combustor
3GE056
1.
GE
Report
TM95­
17.
2.
Engine
S/
N
704/
223
&
704/
234
3.
1862M39
combustor
1GE021
1.
Ref
GE
Report
R90AEB379.
Engine
S/
N's
690105
and
690005/
2.

2GE040
1.
Ref
GE
report
TM95­
17.
2.
Engine
S/
N
704/
233
&
704/
234
3.
1862M39
combustor
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
CV
CW
CX
CY
CZ
DA
DB
DC
DD
DE
DF
DG
DH
129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
145
146
147
148
149
150
151
152
153
154
155
156
157
158
159
160
ted
at
normal
idle
setting
rather
than
7%.

ted
at
normal
idle
setting
rather
than
7%.

ted
at
normal
idle
setting
rather
than
7%.

ted
at
normal
idle
setting
rather
than
7%.

ted
at
normal
idle
setting
rather
than
7%.

ted
at
normal
idle
setting
rather
than
7%.

ted
at
normal
idle
setting
rather
than
7%.

ted
at
normal
idle
setting
rather
than
7%.

e
power
data
were
only
acquired
at
the
engine
design
setting
of
3.69%.

e
power
data
were
only
acquired
at
the
engine
design
setting
of
3.69%.

e
power
data
were
only
acquired
at
the
engine
design
setting
of
3.69%.

e
power
data
were
only
acquired
at
the
engine
design
setting
of
3.69%.

Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
DI
DJ
DK
DL
DM
DN
129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
145
146
147
148
149
150
151
152
153
154
155
156
157
158
159
160
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
A
B
C
D
E
F
G
UID
Engine
Combustor
Eng
B/
P
Press
Rated
No
Identification
Description
Type
Ratio
Ratio
Output
kN
161
162
163
164
165
166
167
168
169
170
171
172
173
174
175
176
177
178
179
180
181
182
183
184
185
186
187
188
189
190
191
192
1GE022
CF6­
80C2B1
TF
5.1
30.08
249.0
2GE041
CF6­
80C2B1
1862M39
TF
5.1
29.53
249.01
1GE023
CF6­
80C2B1F
TF
5.1
30.13
254.3
1GE024
CF6­
80C2B1F
TF
5.1
30.13
254.3
2GE045
CF6­
80C2B1F
1862M39
TF
5.1
30.13
254.26
1GE025
CF6­
80C2B2
TF
5.1
27.74
231.1
2GE042
CF6­
80C2B2
1862M39
TF
5.1
27.53
231.08
1GE026
CF6­
80C2B2F
TF
5.1
27.52
231.35
2GE046
CF6­
80C2B2F
1862M39
TF
5.1
27.6
231.35
1GE027
CF6­
80C2B4
TF
5.1
30.36
254.35
2GE043
CF6­
80C2B4
1862M39
TF
5.1
30.14
254.35
1GE028
CF6­
80C2B4F
TF
5.1
30.17
254.79
2GE047
CF6­
80C2B4F
1862M39
TF
5.1
30.22
254.79
3GE057
CF6­
80C2B5F
1862M39
TF
5.1
32.82
272.53
1GE029
CF6­
80C2B6
TF
5.1
31.56
267.2
2GE044
CF6­
80C2B6
1862M39
TF
5.1
31.66
267.20
1GE030
CF6­
80C2B6F
TF
5.1
31.79
267.03
2GE048
CF6­
80C2B6F
1862M39
TF
5.1
31.72
267.03
2GE054
CF6­
80C2B7F
TF
5.1
31.79
267.03
2GE055
CF6­
80C2B7F
1862M39
TF
5.1
31.72
267.03
3GE058
CF6­
80C2B8FA
1862M39
TF
5.1
31.71
267.02
1GE031
CF6­
80C2D1F
TF
5.1
32.86
269.96
2GE049
CF6­
80C2D1F
1862M39
TF
5.1
32.05
269.96
1GE032
CF6­
80E1A1
TF
5.1
32.44
281.5
2GE050
CF6­
80E1A1
1862M39
TF
5.1
32.46
281.53
1GE033
CF6­
80E1A2
TF
5.1
33.08
287.0
2GE051
CF6­
80E1A2
1862M39
TF
5.1
33.1
287.04
5GE085
CF6­
80E1A3
Standard
TF
5.1
35.7
304.8
4GE080
CF6­
80E1A4
Standard
TF
5.1
34.5
297.44
4GE081
CF6­
80E1A4
Low
emissions
TF
5.1
34.5
297.44
2GE052
GE90­
76B
DAC
I
TF
8.5
35.30
360.62
3GE062
GE90­
76B
DAC
II
TF
8.59
35.1
360.62
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
H
I
J
K
L
M
N
O
P
Q
R
S
T
U
UID
Data
Superseded
Data
No
PR
C
R
superseded
by
NME
DTEPS
Other
Corr
as
Out
of
Date
Out
of
Date
UID
No
Annex
16
Production
Service
­­­­­­­­
Data
Status­­­­­­­­
­­­­­­­­­­
Current
Engine
Status
­­­­­­­­­­

­­­­­­
Test
Engine
Status­­­­­­

161
162
163
164
165
166
167
168
169
170
171
172
173
174
175
176
177
178
179
180
181
182
183
184
185
186
187
188
189
190
191
192
1GE022
­
x
­
­
­
x
­
­
x
x
­
­
­

2GE041
­
x
­
­
­
x
­
­
x
­
­
­
­

1GE023
­
x
­
x
1GE024
x
­
­
x
x
­
­
­

1GE024
­
­
x
­
­
x
­
­
x
x
­
­
­

2GE045
­
x
­
­
­
x
­
­
x
­
­
­
­

1GE025
­
x
­
­
­
x
­
­
x
x
­
­
­

2GE042
­
x
­
­
­
x
­
­
x
­
­
­
­

1GE026
­
x
­
­
­
x
­
­
x
x
­
­
­

2GE046
­
x
­
­
­
x
­
­
x
­
­
­
­

1GE027
­
x
­
­
­
x
­
­
x
x
­
­
­

2GE043
­
x
­
­
­
x
­
­
x
­
­
­
­

1GE028
­
x
­
­
­
x
­
­
x
x
­
­
­

2GE047
­
x
­
­
­
x
­
­
x
­
­
­
­

3GE057
­
x
­
­
­
x
­
­
x
­
­
­
­

1GE029
­
x
­
­
­
x
­
­
x
x
­
­
­

2GE044
­
x
­
­
­
x
­
­
x
­
­
­
­

1GE030
­
x
­
­
­
x
­
­
x
x
­
­
­

2GE048
­
x
­
­
­
x
­
­
x
­
­
­
­

2GE054
­
x
­
­
­
x
­
­
x
x
­
­
­

2GE055
­
x
­
­
­
x
­
­
x
­
­
­
­

3GE058
­
x
­
­
­
x
­
­
x
­
­
­
­

1GE031
­
x
­
­
­
x
­
­
x
x
­
­
­

2GE049
­
x
­
­
­
x
­
­
x
­
­
­
­

1GE032
­
x
­
­
­
x
­
­
x
­
­
­
­

2GE050
­
x
­
­
­
x
­
­
x
x
­
­
­

1GE033
­
x
­
­
­
x
­
­
x
­
­
­
­

2GE051
­
x
­
­
­
x
­
­
x
x
­
­
­

5GE085
­
x
­
­
­
x
­
­
x
­
­
­
­

4GE080
­
x
­
­
­
x
­
­
x
­
­
­
­

4GE081
­
x
­
­
­
x
­
­
x
x
­
­
­

2GE052
­
­
x
­
­
x
­
­
x
x
­
­
­

3GE062
­
x
­
­
­
x
­
­
x
­
­
­
­

Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
V
W
X
Y
Z
AA
AB
AC
AD
AE
AF
AG
AH
UID
Characteristic
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
%
of
Total
mass
Reg
limit
(
g)

­­­­­­­­­­­­­­­­
EI
HC­­­­­­­­­­­­­­
­­­
Number
­­­
­­­­­­­­­­­­­­­
Dp/
Foo
(
HC)­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­
­­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­­­­­

161
162
163
164
165
166
167
168
169
170
171
172
173
174
175
176
177
178
179
180
181
182
183
184
185
186
187
188
189
190
191
192
1GE022
0.08
0.09
0.21
9.46
3
2
11.89
1.31
10.77­
13.2
15.5
78.9
2953
2GE041
0.05
0.05
0.12
1.71
4
2
2.25
0.22
2.12­
2.65
2.9
14.9
561
1GE023
0.08
0.09
0.20
9.68
3
2
12.43
1.30
11.31­
13.70
16.2
82.5
3157
1GE024
0.08
0.09
0.20
9.88
3
2
12.30
1.25
11.22­
13.48
16.0
81.7
3127
2GE045
0.05
0.05
0.11
1.54
4
2
2.01
0.223
1.87­
2.36
2.6
13.3
513
1GE025
0.08
0.10
0.22
11.17
3
2
14.75
1.25
13.68­
16.01
19.2
97.9
3407
2GE042
0.05
0.05
0.12
1.97
4
2
2.67
0.34
2.43­
3.15
3.5
17.7
617
1GE026
0.08
0.09
0.23
11.80
3
2
14.99
1.24
13.96­
16.37
19.5
99.5
3467
2GE046
0.05
0.05
0.12
1.86
4
2
2.49
0.279
2.3­
2.89
3.2
16.5
579
1GE027
0.08
0.09
0.21
9.74
3
2
12.15
1.27
11.05­
13.37
15.8
80.7
3088
2GE043
0.05
0.05
0.12
1.59
4
2
2.10
0.235
1.96­
2.48
2.7
13.9
535
1GE028
0.08
0.09
0.20
10.37
3
2
12.47
1.19
11.44­
13.52
16.2
82.8
3176
2GE047
0.05
0.05
0.11
1.54
4
2
2.00
0.223
1.86­
2.36
2.6
13.3
513
3GE057
0.05
0.05
0.11
1.31
4
2
1.67
­
­
2.2
11.2
459
1GE029
0.07
0.08
0.20
8.99
3
2
11.12
1.30
10.02­
12.49
14.5
73.8
2966
2GE044
0.04
0.05
0.11
1.48
4
2
1.90
0.209
1.76­
2.24
2.5
12.6
509
1GE030
0.07
0.08
0.19
9.74
3
2
11.40
1.19
10.37­
12.53
14.8
75.7
3041
2GE048
0.05
0.05
0.11
1.43
4
2
1.83
0.207
1.68­
2.16
2.4
12.1
490
2GE054
0.07
0.08
0.19
9.74
3
2
11.4
1.19
10.37­
12.53
14.8
75.5
3041
2GE055
0.05
0.05
0.11
1.43
4
2
1.83
0.207
1.68­
2.16
2.4
12.1
490
3GE058
0.05
0.05
0.11
1.41
4
2
1.83
­
­
2.4
12.2
489
1GE031
0.07
0.08
0.20
9.03
3
2
10.46
1.21
9.43­
11.73
13.6
69.4
2822
2GE049
0.04
0.05
0.11
1.38
4
2
1.76
0.196
1.62­
2.07
2.3
11.7
478
1GE032
0.05
0.07
0.14
9.68
3
2
12.07
5.0
7.5­
16.4
15.7
80.1
3463
2GE050
0.05
0.04
0.11
1.30
4
2
1.76
0.186
1.44­
1.88
2.3
11.7
494
1GE033
0.05
0.07
0.14
9.37
3
2
11.78
4.8
7.4­
16.0
15.3
78.2
3384
2GE051
0.04
0.04
0.11
1.25
4
2
1.68
0.187
1.36­
1.80
2.2
11.2
480
5GE085
0.07
0.07
0.18
9.53
11
6
11.28
­
­
12.6
64.3
3438
4GE080
0.06
0.07
0.18
10.35
3
2
12.52
­
­
16.3
83.1
3726
4GE081
0.04
0.04
0.09
0.92
7
3
1.20
­
­
1.4
7.1
359
2GE052
0.07
0.06
0.67
3.42
3
3
4.78
­
4.18­
5.28
5.6
28.5
1753
3GE062
0.04
0.04
0.07
0.57
5
3
0.77
­
0.45­
1.08
0.9
4.6
279
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
AI
AJ
AK
AL
AM
AN
AO
AP
AQ
AR
AS
AT
AU
UID
Characteristic
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
%
of
Total
mass
Reg
limit
(
g)

­­­­­­­­­­­­­­­­­
EI
CO­­­­­­­­­­­­­­­­­
­­­­­­
Number­­­­­
­­­­­­­­­­­­­­­
Dp/
Foo
(
CO)­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­­­

161
162
163
164
165
166
167
168
169
170
171
172
173
174
175
176
177
178
179
180
181
182
183
184
185
186
187
188
189
190
191
192
1GE022
0.58
0.55
2.37
43.22
3
2
55.35
2.97
52.78­
57.98
63.1
53.4
13757
2GE041
0.04
0.04
2.18
20.62
4
2
26.85
1.19
25.9­
28.6
30.6
25.9
6681
1GE023
0.52
0.52
2.19
43.71
3
2
57.09
3.10
54.41­
59.98
65.0
55.1
14493
1GE024
0.52
0.52
2.21
44.32
3
2
56.09
3.00
53.51­
58.88
63.9
54.2
14270
2GE045
0.04
0.04
2.13
19.23
4
2
24.78
1.19
23.7­
26.5
28.2
23.9
6317
1GE025
0.57
0.55
2.65
48.02
3
2
64.67
2.94
62.12­
67.28
73.7
62.4
14929
2GE042
0.04
0.05
2.61
22.41
4
2
30.46
1.48
29.3­
32.4
34.7
29.4
7024
1GE026
0.52
0.52
2.93
49.75
3
2
64.51
2.89
62.01­
67.13
73.5
62.3
14928
2GE046
0.04
0.06
2.64
21.56
4
2
29.00
1.3
27.9­
30.7
33.0
28.0
6717
1GE027
0.56
0.54
2.33
43.91
3
2
55.86
3.05
53.22­
58.61
63.6
53.9
14193
2GE043
0.05
0.04
2.12
19.76
4
2
25.68
1.2
24.6­
27.4
29.3
24.8
6538
1GE028
0.52
0.52
2.21
45.74
3
2
55.95
2.85
53.49­
58.62
63.7
54.0
14251
2GE047
0.04
0.04
2.13
19.23
4
2
24.73
1.19
23.6­
26.5
28.2
23.9
6317
3GE057
0.05
0.04
1.83
17.45
4
2
21.75
­
­
24.8
21.0
5931
1GE029
0.52
0.52
1.93
41.66
3
2
52.36
3.03
49.74­
55.21
59.7
50.6
13970
2GE044
0.06
0.04
1.91
18.89
4
2
23.80
1.196
22.6­
25.5
27.1
23.0
6367
1GE030
0.52
0.52
1.92
43.89
3
2
52.18
2.80
49.76­
54.85
59.5
50.4
13931
2GE048
0.05
0.04
1.93
18.42
4
2
23.04
1.19
21.9­
24.7
26.3
22.2
6166
2GE054
0.52
0.52
1.92
43.89
3
2
52.18
2.8
49.76­
54.85
59.5
50.4
13931
2GE055
0.05
0.04
1.93
18.42
4
2
23.04
1.19
21.9­
24.7
26.3
22.2
6166
3GE058
0.05
0.04
1.97
18.27
4
2
23.19
­
­
26.4
22.4
6185
1GE031
0.52
0.52
1.94
41.78
3
2
49.21
2.83
46.76­
51.89
56.1
47.5
13279
2GE049
0.05
0.04
1.90
18.02
4
2
22.53
1.21
21.3­
24.2
25.7
21.8
6093
1GE032
0.38
0.34
1.70
43.24
3
2
54.36
8.8
46.7­
62.3
61.9
52.5
15678
2GE050
0.05
0.04
1.92
17.64
4
2
23.32
1.24
19.8­
22.7
26.6
22.5
6565
1GE033
0.38
0.34
1.61
42.67
3
2
54.29
6.2
46.3­
57.3
61.9
52.4
15602
2GE051
0.05
0.04
1.85
17.37
4
2
22.71
1.30
19.0­
22.0
25.9
21.9
6517
5GE085
0.34
0.31
1.23
37.02
11
6
44.20
­
­
46.7
39.6
13473
4GE080
0.34
0.3
1.33
38.09
3
2
46.58
­
­
53.1
45.0
13860
4GE081
0.04
0.02
1.44
15.05
7
3
18.81
­
­
20.3
17.2
5598
2GE052
0.09
0.13
5.80
40.35
3
3
54.66
­
52.1­
56.4
59.1
50.1
20020
3GE062
0.15
0.17
1.32
15.41
5
3
19.55
­
17.1­
21.6
21.1
17.9
7048
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
AV
AW
AX
AY
AZ
BA
BB
BC
BD
BE
BF
BG
BH
BI
BJ
UID
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
Original
CAEP
2
CAEP
4
Total
mass
(
g)

­­­­
Number­­­­­

­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­
EI
NOx­­­­­­­­­­­­­­
­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­
Dp/
Foo
(
NOx)­­­­­­­­­­­­­­
Characteristic
as
%
of
standards
161
162
163
164
165
166
167
168
169
170
171
172
173
174
175
176
177
178
179
180
181
182
183
184
185
186
187
188
189
190
191
192
1GE022
28.11
21.26
8.83
3.73
3
2
41.79
2.02
40.17­
44.18
46.0
45.9
57.3
68.4
10400
2GE041
24.93
19.68
12.32
4.60
4
2
43.05
0.276
42.7­
43.3
47.3
47.8
59.7
71.5
10719
1GE023
28.06
21.34
8.97
3.74
3
2
42.17
2.02
40.58­
44.60
46.4
46.3
57.8
68.9
10718
1GE024
27.73
21.07
9.00
3.78
3
2
41.38
1.98
39.83­
43.77
45.5
45.4
56.7
67.7
10528
2GE045
24.94
19.72
12.47
4.73
4
2
43.69
0.3
43.3­
44.0
48.0
47.9
59.9
71.4
11113
1GE025
23.89
18.65
8.77
3.70
3
2
38.08
1.84
36.70­
40.37
41.9
43.9
54.8
66.1
8796
2GE042
22.02
18.25
11.79
4.45
4
2
39.70
0.234
39.4­
40.0
43.7
45.9
57.4
69.2
9169
1GE026
23.56
18.32
8.54
3.64
3
2
36.14
1.70
34.80­
36.75
39.7
41.8
52.3
63.0
8361
2GE046
21.55
18.09
11.80
4.52
4
2
39.73
0.24
39.5­
40.1
43.7
45.9
57.4
69.2
9192
1GE027
29.20
21.80
8.90
3.67
3
2
44.08
2.12
42.30­
46.38
48.5
48.1
60.2
71.6
11211
2GE043
25.93
20.17
12.37
4.68
4
2
44.12
0.304
43.7­
44.4
48.5
48.4
60.5
72.1
11226
1GE028
28.72
21.32
8.88
3.71
3
2
41.73
1.90
40.25­
44.03
45.9
45.7
57.2
68.1
10635
2GE047
25.08
19.72
12.47
4.73
4
2
43.70
0.29
43.3­
44.0
48.1
47.8
59.8
71.3
11137
3GE057
28.58
21.76
12.74
4.91
4
2
48.22
­
­
53.0
50.2
62.7
73.0
13142
1GE029
30.81
22.94
9.11
3.79
3
2
46.26
2.16
44.57­
48.88
50.9
49.3
61.7
72.5
12362
2GE044
28.57
21.69
12.53
4.76
4
2
47.30
0.5
46.7­
47.9
52.0
50.3
62.9
74.0
12640
1GE030
32.16
23.09
9.06
3.75
3
2
45.43
1.98
43.90­
47.85
50.0
48.2
60.3
70.8
12134
2GE048
27.38
21.05
12.63
4.81
4
2
46.51
0.351
46.0­
46.8
51.1
49.4
61.8
72.6
12420
2GE054
32.16
23.09
9.06
3.75
3
2
45.43
1.98
43.90­
47.85
50.0
48.3
60.3
70.8
12134
2GE055
27.38
21.05
12.63
4.81
4
2
46.51
0.351
46.0­
46.8
51.1
49.4
61.8
72.6
12420
3GE058
26.90
20.85
12.63
4.83
4
2
46.43
­
­
51.1
49.4
61.8
72.6
12400
1GE031
32.65
24.02
9.16
3.80
3
2
47.10
2.16
45.47­
49.65
51.8
49.0
61.2
71.2
12714
2GE049
28.12
21.30
12.66
4.85
4
2
47.13
0.581
46.5­
47.9
51.8
49.8
62.2
72.9
12724
1GE032
37.87
27.11
9.84
4.47
3
2
53.74
1.1
52.4­
54.5
59.1
56.3
70.4
82.2
15429
2GE050
27.59
21.44
12.61
4.87
4
2
47.00
0.383
45.0­
45.8
51.7
49.3
61.6
71.9
13232
1GE033
39.29
28.02
9.91
4.53
3
2
56.44
1.3
54.7­
57.3
62.1
58.5
73.1
84.8
16203
2GE051
28.72
22.01
12.66
4.88
4
2
48.07
0.574
45.1­
46.4
52.9
49.8
62.2
72.2
13796
5GE085
45.63
31.74
10.29
4.69
11
6
63.15
­
­
65.8
59.1
73.8
83.9
19254
4GE080
43.15
30.3
10.13
4.62
3
2
60.69
­
­
66.7
61.2
76.5
87.8
18055
4GE081
31.28
23.54
12.66
4.77
7
3
50.52
­
­
53.5
49.1
61.4
70.4
15027
2GE052
44.86
35.39
12.68
5.88
3
3
59.11
­
58.0­
61.0
62.6
56.6
70.8
80.7
21342
3GE062
40.11
31.59
15.55
5.43
5
3
54.58
­
50.5­
57.3
57.8
52.5
65.6
74.9
19680
Filename
DCTM_
ARP.
xls
Printed
on
5/
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05
Check
website
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aviation_
emissions_
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Data
1
2
3
BK
BL
BM
BN
BO
BP
BQ
BR
BS
BT
BU
BV
UID
Characteristic
No
T/
O
C/
O
App
Idle
Test
Eng
Max
Sigma
Range
Characteristic
%
of
Reg
limit
­­­­­­­­­­­­­­
Smoke
Number­­­­­­­­­­­­­

­­­­­­­­­­­­­
Smoke
Number­­­­­­­­­­­­­
­­­­
Number­­­­

161
162
163
164
165
166
167
168
169
170
171
172
173
174
175
176
177
178
179
180
181
182
183
184
185
186
187
188
189
190
191
192
1GE022
7.1
­
­
­
3
2
7.1
1.1
5.7­
7.6
8.3
45.2
2GE041
6.7
4.2
0.0
0.0
4
2
6.7
0.525
6.3­
7.5
7.9
42.6
1GE023
7.1
­
­
­
3
2
7.1
1.1
5.7­
7.5
8.3
45.4
1GE024
7.1
­
­
­
3
2
7.1
1.1
5.7­
7.5
8.3
45.4
2GE045
6.9
4.5
0.0
0.0
4
2
6.9
0.62
6.2­
7.7
8.1
44.1
1GE025
5.8
­
­
­
3
2
5.8
0.95
4.6­
6.3
6.8
36.1
2GE042
5.6
3.1
0.0
0.0
4
2
5.6
0.608
5.0­
6.4
6.6
34.9
1GE026
7.5
3.6
2.4
2.5
3
2
5.7
1.0
4.4­
6.1
6.7
35.5
2GE046
5.7
3.1
0.0
0.0
4
2
5.7
0.61
5.0­
6.4
6.7
35.5
1GE027
7.2
­
­
­
3
2
7.2
1.1
5.8­
7.7
8.4
46.1
2GE043
6.9
4.5
0.0
0.0
4
2
6.9
0.624
6.2­
7.7
8.1
44.2
1GE028
7.3
4.7
2.3
2.3
3
2
7.3
1.1
5.9­
7.8
8.6
46.7
2GE047
6.9
4.5
0.0
0.0
4
2
6.9
0.64
6.2­
7.7
8.1
44.2
3GE057
7.4
5.2
0
0
4
2
7.4
­
­
8.7
48.4
1GE029
7.8
­
­
­
3
2
7.8
1.3
6.1­
8.4
9.1
50.6
2GE044
6.9
5.4
0.0
0.0
4
2
6.9
0.914
5.9­
8.2
8.1
44.8
1GE030
8.2
5.4
2.3
3.4
3
2
8.2
1.4
6.3­
8.9
9.6
53.2
2GE048
6.9
5.3
0.0
0.0
4
2
6.9
0.915
5.9­
8.2
8.1
44.7
2GE054
8.2
5.4
2.3
3.40
3
2
8.20
1.4
6.3­
8.9
9.6
53.1
2GE055
6.9
5.3
0.0
0.0
4
2
6.9
0.915
5.9­
8.2
8.1
44.7
3GE058
7.2
5.2
0
0
4
2
7.2
­
­
8.4
46.4
1GE031
8.2
5.6
2.3
3.5
3
2
8.2
1.4
6.35­
8.85
9.6
53.3
2GE049
7.0
5.5
0.0
0.0
4
2
7.0
0.908
6.1­
8.3
8.2
45.5
1GE032
9.7
6.9
0
0
3
2
9.7
2.7
7.4­
12.3
11.4
63.8
2GE050
6.9
6.2
0.0
0.0
4
2
6.9
1.07
6.5­
8.7
8.1
45.4
1GE033
9.9
7.2
0
0
3
2
9.9
2.8
7.5­
12.7
11.6
65.5
2GE051
6.8
6.5
0.0
0.0
4
2
6.8
1.26
6.1­
8.9
8.0
44.9
5GE085
10.1
8.6
0.0
0.0
11
6
10.1
­
­
10.8
61.9
4GE080
10.09
8.06
0
0
3
2
10.09
­
­
11.8
67.4
4GE081
5.9
5.5
0
0
7
3
5.9
­
­
6.5
37.0
2GE052
<
3
<
3
<
3
9.90
3
3
10.22
­
9.4­
10.2
11.2
67.5
3GE062
­
­
­
­
5
3
0.5
­
0.0­
1.93
0.6
3.6
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
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version
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aviation_
emissions_
databank
Data
1
2
3
BW
BX
BY
BZ
CA
CB
CC
CD
CE
UID
Fuel
per
No
Spec
H/
C
Arom
T/
O
C/
O
App
Idle
LTO
cycle
Ratio
%
(
kg)

­­­­­­­­­­­­­­­­­
Fuel
Flow­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­(
kg/
sec)­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­­­­­
Fuel­­­­­­­­­­­­­­­­­­­­­­­

161
162
163
164
165
166
167
168
169
170
171
172
173
174
175
176
177
178
179
180
181
182
183
184
185
186
187
188
189
190
191
192
1GE022
Jet
A
1.94
15.3
2.285
1.873
0.616
0.196
797
2GE041
Jet
A
1.94
15.3
2.340
1.922
0.630
0.197
811
1GE023
Jet
A
1.94
15.3
2.353
1.913
0.632
0.205
823
1GE024
Jet
A
1.94
15.3
2.341
1.901
0.621
0.199
809
2GE045
Jet
A
1.94
15.3
2.422
1.983
0.650
0.199
830
1GE025
Jet
A
1.94
15.3
2.131
1.761
0.577
0.192
760
2GE042
Jet
A
1.94
15.3
2.124
1.756
0.585
0.190
758
1GE026
Jet
A
1.94
15.3
2.071
1.702
0.5585
0.1852
735
2GE046
Jet
A
1.94
15.3
2.148
1.777
0.593
0.188
760
1GE027
Jet
A
1.94
15.3
2.430
1.982
0.650
0.199
830
2GE043
Jet
A
1.94
15.3
2.409
1.965
0.641
0.201
828
1GE028
Jet
A
1.94
15.3
2.359
1.907
0.6138
0.1926
799
2GE047
Jet
A
1.94
15.3
2.432
1.983
0.650
0.199
830
3GE057
Jet
A
1.94
15.3
2.685
2.162
0.697
0.206
887
1GE029
Jet
A
1.94
15.3
2.579
2.081
0.686
0.207
871
2GE044
Jet
A
1.94
15.3
2.580
2.096
0.672
0.205
866
1GE030
Jet
A
1.94
15.3
2.540
2.020
0.643
0.1963
834
2GE048
Jet
A
1.94
15.3
2.594
2.104
0.682
0.203
867
2GE054
Jet
A
1.94
15.3
2.54
2.02
0.64
0.20
834
2GE055
Jet
A
1.94
15.3
2.594
2.104
0.682
0.203
867
3GE058
Jet
A
1.94
15.3
2.605
2.117
0.688
0.205
874
1GE031
Jet
A
1.94
15.3
2.596
2.065
0.657
0.196
845
2GE049
Jet
A
1.94
15.3
2.629
2.126
0.688
0.205
876
1GE032
Jet
A
1.89
16.4
2.702
2.199
0.714
0.226
928
2GE050
Jet
A
1.94
15.3
2.702
2.199
0.714
0.226
928
1GE033
Jet
A
1.89
16.4
2.767
2.245
0.724
0.228
942
2GE051
Jet
A
1.94
15.3
2.767
2.245
0.724
0.228
942
5GE085
Jet
A
1.94
15.3
2.989
2.387
0.755
0.227
976
4GE080
Jet
A
1.94
15.3
2.904
2.337
0.744
0.227
963
4GE081
Jet
A
1.94
15.3
2.904
2.337
0.744
0.227
963
2GE052
Jet
A
1.91­
1.92
15.9­
18.6
2.83
2.33
0.78
0.30
1082
3GE062
Jet
A
1.91­
1.94
18.1­
19.3
2.824
2.311
0.781
0.280
1048
Filename
DCTM_
ARP.
xls
Printed
on
5/
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05
Check
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aviation_
emissions_
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Data
1
2
3
CF
CG
CH
CI
CJ
CK
CL
CM
UID
No
Baro
Temp
Humidity
kW
@
Power
%
CF
@
Power
kPa
K
kg/
kg
­­­­­­­­­­­­­­­­­­­
Ambient­­­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­
Loads­­­­­­­­­­­­­­­­­­­

Power
Extraction
­­­
Stage
Bleed­­­

161
162
163
164
165
166
167
168
169
170
171
172
173
174
175
176
177
178
179
180
181
182
183
184
185
186
187
188
189
190
191
192
1GE022
0
­
0
­
97.40­
97.82
287
­
296
.0084­.
0140
2GE041
0
­
0
­
97.61­
98.15
279­
293
.00457­.
00743
1GE023
0
­
0
­
97.40­
97.82
287
­
296
.0084­.
0140
1GE024
0
­
0
­
97.40­
97.82
287
­
296
.0084­.
0140
2GE045
0
­
0
­
97.61­
98.15
279­
293
.00457­.
00743
1GE025
0
­
0
­
97.40­
97.82
287
­
296
.0084­.
0140
2GE042
0
­
0
­
97.61­
98.15
279­
293
.00457­.
00743
1GE026
0
­
0
­
97.40­
97.82
287
­
296
.0084­.
0140
2GE046
0
­
0
­
97.61­
98.15
279­
293
.00457­.
00743
1GE027
0
­
0
­
97.40­
97.82
287
­
296
.0084­.
0140
2GE043
0
­
0
­
97.61­
98.15
279­
293
.00457­.
00743
1GE028
0
­
0
­
97.40­
97.82
287
­
296
.0084­.
0140
2GE047
0
­
0
­
97.61­
98.15
279­
293
.00457­.
00743
3GE057
0
­
0
­
97.61­
98.15
279­
293
.0046­.
0074
1GE029
0
­
0
­
97.40­
97.82
287
­
296
.0084­.
0140
2GE044
0
­
0
­
97.61­
98.15
279­
293
.00457­.
00743
1GE030
0
­
0
­
97.40­
97.82
287
­
296
.0084­.
0140
2GE048
0
­
0
­
97.61­
98.15
279­
293
.00457­.
00743
2GE054
0
­
0
­
97.40­
97.82
287­
296
.0084­.
0140
2GE055
0
­
0
­
97.61­
98.15
279­
293
.00457­.
00743
3GE058
0
­
0
­
97.61­
98.15
279­
293
.0046­.
0074
1GE031
0
­
0
­
97.40­
97.82
287
­
296
.0084­.
0140
2GE049
0
­
0
­
97.61­
98.15
279­
293
.00457­.
00743
1GE032
0
­
0
­
97.66­
97.99
292
­
296
.012­.
015
2GE050
0
­
0
­
97.61­
98.15
279­
293
.00457­.
00743
1GE033
0
­
0
­
97.66­
97.99
292
­
296
.012­.
015
2GE051
0
­
0
­
97.61­
98.15
279­
293
.00457­.
00743
5GE085
0
­
0
­
97.61
­
98.15
279
­
293
.00457
­
.00743
4GE080
0
­
0
­
97.61­
98.15
279­
293
.00457­.
00743
4GE081
0
­
0
­
97.61­
98.15
279­
293
.00457­.
00743
2GE052
0
­
0
­
97.38­
98.59
274­
299
.001­.
00726
3GE062
0
­
0
­
97.52­
98.62
283­
301
.0036­.
0151
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
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version
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aviation_
emissions_
databank
Data
1
2
3
CN
CO
CP
CQ
CR
CS
UID
­­­
Test
Dates­­­

No
Manufacturer
Test
Organisation
Test
Location
From
To
161
162
163
164
165
166
167
168
169
170
171
172
173
174
175
176
177
178
179
180
181
182
183
184
185
186
187
188
189
190
191
192
1GE022
GE
Aircraft
Engines
CF6
Evaluation
Engineering
Site
IIIC,
PTO,
Peebles,
Ohio
29­
May­
85
3­
Jun­
85
2GE041
GE
CF6
Eval
Engineering
Site
IIIB,
PTO
Peebles
13­
Jan­
95
17­
Jan­
95
1GE023
GE
Aircraft
Engines
CF6
Evaluation
Engineering
Site
IIIC,
PTO,
Peebles,
Ohio
29­
May­
85
3­
Jun­
85
1GE024
GE
Aircraft
Engines
CF6
Evaluation
Engineering
Site
IIIC,
PTO,
Peebles,
Ohio
29­
May­
85
3­
Jun­
85
2GE045
GE
CF6
Eval
Engineering
Site
IIIB,
PTO
Peebles
13­
Jan­
95
17­
Jan­
95
1GE025
GE
Aircraft
Engines
CF6
Evaluation
Engineering
Site
IIIC,
PTO,
Peebles,
Ohio
29­
May­
85
3­
Jun­
85
2GE042
GE
CF6
Eval
Engineering
Site
IIIB,
PTO
Peebles
13­
Jan­
95
17­
Jan­
95
1GE026
GE
Aircraft
Engines
CF6
Evaluation
Engineering
Site
IIIC,
PTO,
Peebles,
Ohio
29­
May­
85
3­
Jun­
85
2GE046
GE
CF6
Eval
Engineering
Site
IIIB,
PTO
Peebles
13­
Jan­
95
17­
Jan­
95
1GE027
GE
Aircraft
Engines
CF6
Evaluation
Engineering
Site
IIIC,
PTO,
Peebles,
Ohio
29­
May­
85
3­
Jun­
85
2GE043
GE
CF6
Eval
Engineering
Site
IIIB,
PTO
Peebles
13­
Jan­
95
17­
Jan­
95
1GE028
GE
Aircraft
Engines
CF6
Evaluation
Engineering
Site
IIIC,
PTO,
Peebles,
Ohio
29­
May­
85
3­
Jun­
85
2GE047
GE
CF6
Eval
Engineering
Site
IIIB,
PTO
Peebles
13­
Jan­
95
17­
Jan­
95
3GE057
GE
CF6
Ecval
Engineering
Site
IIIB,
PTO,
Peebles,
Ohio,
USA
13­
Jan­
95
17­
Jan­
95
1GE029
GE
Aircraft
Engines
CF6
Evaluation
Engineering
Site
IIIC,
PTO,
Peebles,
Ohio
29­
May­
85
3­
Jun­
85
2GE044
GE
CF6
Eval
Engineering
Site
IIIB,
PTO
Peebles
13­
Jan­
95
17­
Jan­
95
1GE030
GE
Aircraft
Engines
CF6
Evaluation
Engineering
Site
IIIC,
PTO,
Peebles,
Ohio
29­
May­
85
3­
Jun­
85
2GE048
GE
CF6
Eval
Engineering
Site
IIIB,
PTO
Peebles
13­
Jan­
95
17­
Jan­
95
2GE054
GE
Aircraft
Engines
CF6
Evaluation
Engineering
Site
IIIC,
PTO,
Peebles,
Ohio
29­
May­
85
3­
Jun­
85
2GE055
GE
CF6
Eval
Engineering
Site
IIIB,
PTO
Peebles
13­
Jan­
95
17­
Jan­
95
3GE058
GE
CF6
Ecval
Engineering
Site
IIIB,
PTO,
Peebles,
Ohio,
USA
13­
Jan­
95
17­
Jan­
95
1GE031
GE
Aircraft
Engines
CF6
Evaluation
Engineering
Site
IIIC,
PTO,
Peebles,
Ohio
29­
May­
85
3­
Jun­
85
2GE049
GE
CF6
Eval
Engineering
Site
IIIB,
PTO
Peebles
13­
Jan­
95
17­
Jan­
95
1GE032
GE
Aircraft
Engines
CF6
Evaluation
Engineering
Sites
IIIC
&
IIID,
Peebles
Test
Facility
8­
Jun­
92
4­
Aug­
92
2GE050
GE
CF6
Eval
Engineering
Site
IIIB,
PTO
Peebles
13­
Jan­
95
17­
Jan­
95
1GE033
GE
Aircraft
Engines
CF6
Evaluation
Engineering
Sites
IIIC
&
IIID,
Peebles
Test
Facility
8­
Jun­
92
4­
Aug­
92
2GE051
GE
CF6
Eval
Engineering
Site
IIIB,
PTO
Peebles
13­
Jan­
95
17­
Jan­
95
5GE085
GE
CF6
Eval
Engineering
Site
IIIB,
PTO
Peebles
13­
Jan­
95
17­
Jan­
95
4GE080
GE
CF6
Evaluation
Engineering
Site
IIIB,
PTO,
Ohio
13­
Jan­
95
17­
Jan­
95
4GE081
GE
CF6
Evaluation
Engineering
Site
IIIB,
PTO,
Ohio
13­
Jan­
96
16­
Mar­
96
2GE052
GE
GE90
Eval
Engineering
Site
IVD
and
6,
PTO,
Peebles
24­
Feb­
95
28­
Jul­
95
3GE062
GE
GE90
Eval
Engineering
Site
IIID,
PTO,
Peebles,
Ohio,
USA
24­
Apr­
97
19­
Jun­
97
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
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for
latest
version
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aviation_
emissions_
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Data
1
2
3
CT
CU
UID
No
Remarks
161
162
163
164
165
166
167
168
169
170
171
172
173
174
175
176
177
178
179
180
181
182
183
184
185
186
187
188
189
190
191
192
1GE022
1.
Ref
GE
Report
R84AEB152,
Addendum
1
(
Dec
1986).
2.
Engine
S/
N's
690105
and
690005/
2.

2GE041
1.
Ref
GE
report
TM95­
17.
2.
Engine
S/
N
704/
233
&
704/
234
3.
1862M39
combustor
1GE023
1.
Ref
GE
Report
R84AEB152.
2.
Engine
S/
N's
690105
and
690005/
2.

1GE024
1.
Ref
GE
Report
R87AEB208
Rev
A.
(
Jan
88).
2.
Engine
S/
N's
690105
and
690005/
2.

2GE045
1.
Ref
GE
report
TM95­
17.
2.
Engine
S/
N
704/
233
&
704/
234
3.
1862M39
combustor
1GE025
1.
Ref
GE
Report
R86AEB589.
2.
Engine
S/
N's
690105
and
690005/
2.

2GE042
1.
Ref
GE
report
TM95­
17.
2.
Engine
S/
N
704/
233
&
704/
234
3.
1862M39
combustor
1GE026
1.
Ref
GE
Report
R88AEB277.
2.
Engine
S/
N's
690105
and
690005/
2.

2GE046
1.
Ref
GE
report
TM95­
17.
2.
Engine
S/
N
704/
233
&
704/
234
3.
1862M39
combustor
1GE027
1.
Ref
GE
Reports
R84AEB152
and
R86AEB144
(
Rev
Aug
86).
2.
Engine
S/
N's
690105
and
690005/
2.

2GE043
1.
Ref
GE
report
TM95­
17.
2.
Engine
S/
N
704/
233
&
704/
234
3.
1862M39
combustor
1GE028
1.
Ref
GE
Report
R88AEB277.
2.
Engine
S/
N's
690105
and
690005/
2.

2GE047
1.
Ref
GE
report
TM95­
17.
2.
Engine
S/
N
704/
233
&
704/
234
3.
1862M39
combustor
3GE057
1.
GE
Report
TM95­
17.
2.
Engine
S/
N
704/
223
&
704/
234
3.
1862M39
combustor
1GE029
1.
Ref
GE
Report
R86AEB160.
2.
Engine
S/
N's
690105
and
690005/
2.

2GE044
1.
Ref
GE
report
TM95­
17.
2.
Engine
S/
N
704/
233
&
704/
234
3.
1862M39
combustor
1GE030
1.
Ref
GE
Report
R88AEB277.
2.
Engine
S/
N's
690105
and
690005/
2.

2GE048
1.
Ref
GE
report
TM95­
17.
2.
Engine
S/
N
704/
233
&
704/
234
3.
1862M39
combustor
2GE054
1.
Ref
GE
Report
R88AEB277.
2.
Engine
S/
N's
690105
and
690005/
2.

2GE055
1.
Ref
GE
report
TM95­
17.
2.
Engine
S/
N
704/
233
&
704/
234
3.
1862M39
combustor
3GE058
1.
GE
Report
TM95­
17.
2.
Engine
S/
N
704/
223
&
704/
234
3.
1862M39
combustor
1GE031
1.
Ref
GE
Report
R88AEB266
Rev
A
(
Jan
91).
2.
Engine
S/
N's
690105
and
690005/
2.

2GE049
1.
Ref
GE
report
TM95­
17.
2.
Engine
S/
N
704/
233
&
704/
234
3.
1862M39
combustor
1GE032
1.
Ref
GE
Report
R90AEB188.
2.
Engine
S/
N's
810­
101/
1
and
810­
104/
1.

2GE050
1.
Ref
GE
report
TM95­
17.
2.
Engine
S/
N
704/
233
&
704/
234
3.
1862M39
combustor
1GE033
1.
Ref
GE
Report
R90AEB188.
2.
Engine
S/
N's
810­
101/
1
and
810­
104/
1.

2GE051
1.
Ref
GE
report
TM95­
17.
2.
Engine
S/
N
704/
233
&
704/
234
3.
1862M39
combustor
5GE085
1.
Ref.
GE
Reports
R84AEB152,
R90AEB188,
R95AEB272­
2
2.
Standard
combustor
4GE080
1.
GE
Report
TM95­
17.
2.
Engine
S/
N
704/
233
&
704/
234
3.
Standard
combustor
4GE081
1.
Ref
GE
Report
TM95­
17
&
GEAE
R95AEB272­
2.
2.
Engine
S/
N
704/
233,
704/
234
&
704/
378
3.
Low
emissions
combustor
2GE052
1.
Ref
GE
Report
TM95­
45.
2.
Engine
S/
N
900­
108,
900­
111
&
900­
114.
3.
Post
certification/
as
delivered
to
service.
4.
Smoke
<
3
below
meas.
capa
3GE062
1.
GE
Report
R96AEB292.
2.
Engine
S/
S
900­
173,
900­
166
&
900­
167
3.
DAC
II
combustor
Filename
DCTM_
ARP.
xls
Printed
on
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aviation_
emissions_
databank
Data
1
2
3
CV
CW
CX
CY
CZ
DA
DB
DC
DD
DE
DF
DG
DH
161
162
163
164
165
166
167
168
169
170
171
172
173
174
175
176
177
178
179
180
181
182
183
184
185
186
187
188
189
190
191
192
pability.
5.
DAC
I
combustor
Filename
DCTM_
ARP.
xls
Printed
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aviation_
emissions_
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Data
1
2
3
DI
DJ
DK
DL
DM
DN
161
162
163
164
165
166
167
168
169
170
171
172
173
174
175
176
177
178
179
180
181
182
183
184
185
186
187
188
189
190
191
192
Filename
DCTM_
ARP.
xls
Printed
on
5/
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05
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aviation_
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Data
1
2
3
A
B
C
D
E
F
G
UID
Engine
Combustor
Eng
B/
P
Press
Rated
No
Identification
Description
Type
Ratio
Ratio
Output
kN
193
194
195
196
197
198
199
200
201
202
203
204
205
206
207
208
209
210
211
212
213
214
215
216
217
218
219
220
221
222
223
224
5GE086
GE90­
76B
TF
8.53
34.88
360.6
6GE087
GE90­
76B
DAC
II
TF
8.53
34.88
360.6
3GE059
GE90­
77B
DAC
I
TF
8.6
35.2
363.42
3GE063
GE90­
77B
DAC
II
TF
8.58
35.3
363.42
6GE088
GE90­
77B
DAC
II
TF
8.52
35.11
363.4
2GE053
GE90­
85B
DAC
I
TF
8.4
38.10
395.31
3GE064
GE90­
85B
DAC
II
TF
8.44
38.0
395.31
6GE089
GE90­
85B
DAC
II
TF
8.41
37.7
395.3
3GE060
GE90­
90B
DAC
I
TF
8.4
39.7
418.13
3GE065
GE90­
90B
DAC
II
TF
8.36
39.8
418.13
6GE090
GE90­
90B
DAC
II
TF
8.36
39.38
418.1
3GE061
GE90­
92B
DAC
I
TF
8.4
40.4
426.72
3GE066
GE90­
92B
DAC
II
TF
8.33
40.6
426.72
6GE091
GE90­
94B
DAC
II
TF
8.33
40.53
432.8
International
Aero
Engines
1IA001
V2500­
A1
TF
5.3
29.8
111.2
3IA006
V2522­
A5
TF
4.88
25.6
102.66
3IA007
V2524­
A5
TF
4.81
26.9
109.06
1IA002
V2525­
D5
TF
4.82
27.2
111.2
1IA003
V2527­
A5
TF
4.82
27.2
111.2
1IA004
V2528­
D5
TF
4.66
30.0
124.5
1IA005
V2530­
A5
TF
4.54
32.1
133.4
3IA008
V2533­
A5
TF
4.46
33.44
140.56
KKBM
1KK001
NK­
8­
2U
MTF
1.24
10.8
103
1KK002
NK­
8­
2U
MTF
1.24
10.8
103
Filename
DCTM_
ARP.
xls
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Data
1
2
3
H
I
J
K
L
M
N
O
P
Q
R
S
T
U
UID
Data
Superseded
Data
No
PR
C
R
superseded
by
NME
DTEPS
Other
Corr
as
Out
of
Date
Out
of
Date
UID
No
Annex
16
Production
Service
­­­­­­­­
Data
Status­­­­­­­­
­­­­­­­­­­
Current
Engine
Status
­­­­­­­­­­

­­­­­­
Test
Engine
Status­­­­­­

193
194
195
196
197
198
199
200
201
202
203
204
205
206
207
208
209
210
211
212
213
214
215
216
217
218
219
220
221
222
223
224
5GE086
­
­
­
x
­
­
x
­
­
­
­

6GE087
­
x
­
­
­
x
­
­
x
­
­
­
­

3GE059
­
x
­
­
­
x
­
­
x
x
­
­
­

3GE063
­
x
­
­
­
x
­
­
x
­
­
­
­

6GE088
­
x
­
­
­
x
­
­
x
­
­
­
­

2GE053
­
­
x
­
­
x
­
­
x
x
­
­
­

3GE064
­
x
­
­
­
x
­
­
x
­
­
­
­

6GE089
­
x
­
­
­
x
­
­
x
­
­
­
­

3GE060
­
x
­
­
­
x
­
­
x
x
­
­
­

3GE065
­
x
­
­
­
x
­
­
x
­
­
­
­

6GE090
­
x
­
­
­
x
­
­
x
­
­
­
­

3GE061
­
x
­
­
­
x
­
­
x
x
­
­
­

3GE066
­
x
­
­
­
x
­
­
x
­
­
­
­

6GE091
­
x
­
­
­
x
­
­
x
­
­
­
­

1IA001
­
x
­
­
­
x
­
­
x
x
­
­
­

3IA006
­
x
­
­
­
x
­
­
x
­
­
­
­

3IA007
­
x
­
­
­
x
­
­
x
­
­
­
­

1IA002
­
x
­
­
­
x
­
­
x
­
­
­
­

1IA003
­
x
­
­
­
x
­
­
x
­
­
­
­

1IA004
­
x
­
­
­
x
­
­
x
­
­
­
­

1IA005
­
x
­
­
­
x
­
­
x
­
­
­
­

3IA008
­
x
­
­
­
x
­
­
x
­
­
­
­

1KK001
­
­
x
­
­
­
­
x
­
x
­
­
­

1KK002
­
­
x
­
­
­
­
x
­
­
­
­
­

Filename
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Data
1
2
3
V
W
X
Y
Z
AA
AB
AC
AD
AE
AF
AG
AH
UID
Characteristic
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
%
of
Total
mass
Reg
limit
(
g)

­­­­­­­­­­­­­­­­
EI
HC­­­­­­­­­­­­­­
­­­
Number
­­­
­­­­­­­­­­­­­­­
Dp/
Foo
(
HC)­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­
­­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­­­­­

193
194
195
196
197
198
199
200
201
202
203
204
205
206
207
208
209
210
211
212
213
214
215
216
217
218
219
220
221
222
223
224
5GE086
0.04
0.03
0.06
0.52
3
1
0.68
0.058
0.061
­
0.071
1.1
5.4
241
6GE087
0.04
0.03
0.06
0.52
3
1
0.68
0.058
0.61­
0.71
1.1
5.4
241
3GE059
0.07
0.06
0.80
3.83
3
3
5.33
­
4.58­
5.92
6.2
31.6
1938
3GE063
0.04
0.04
0.07
0.56
5
3
0.75
­
0.44­
1.07
0.9
4.6
276
6GE088
0.04
0.03
0.06
0.52
3
1
0.67
0.056
0.60­
0.70
1.0
5.3
243
2GE053
0.08
0.07
1.52
3.05
3
3
4.52
­
4.27­
4.79
5.3
26.9
1772
3GE064
0.04
0.04
0.07
0.45
5
3
0.60
­
0.30­
0.92
0.7
3.6
238
6GE089
0.04
0.03
0.05
0.46
3
1
0.58
0.041
0.53­
0.61
0.9
4.5
228
3GE060
0.08
0.07
1.34
2.77
3
3
4.01
­
3.82­
4.22
4.7
24.0
1674
3GE065
0.04
0.04
0.07
0.39
5
3
0.52
­
0.25­
0.84
0.6
3.1
218
6GE090
0.04
0.04
0.05
0.43
3
1
0.54
0.036
0.49­
0.56
0.8
4.2
226
3GE061
0.09
0.07
1.17
2.64
3
3
3.74
­
3.58­
3.94
4.4
22.4
1594
3GE066
0.04
0.04
0.07
0.37
5
3
0.50
­
0.24­
0.81
0.6
3.1
212
6GE091
0.04
0.04
0.05
0.41
3
1
0.51
0.035
0.47­
0.53
0.8
4.0
221
1IA001
0.10
0.11
0.15
0.22
3
1
0.65
­
­
1.0
5.1
73
3IA006
0.041
0.041
0.062
0.103
3
1
0.29
­
­
0.5
2.3
30
3IA007
0.042
0.042
0.061
0.100
3
1
0.28
­
­
0.4
2.2
31
1IA002
0.041
0.041
0.061
0.105
3
1
0.29
­
­
0.4
2.3
32
1IA003
0.041
0.041
0.061
0.105
3
1
0.29
­
­
0.4
2.3
32
1IA004
0.043
0.041
0.058
0.102
3
1
0.27
­
­
0.4
2.1
34
1IA005
0.045
0.041
0.056
0.100
3
1
0.26
­
­
0.4
2.0
35
3IA008
0.047
0.043
0.052
0.100
3
1
0.25
­
­
0.4
2.0
35
1KK001
0.45
0.55
5.00
103.80
2
2
388.2
­
­
505.1
2577.2
39677
1KK002
2.0
2.0
2.6
32.0
2
1
117.1
­
­
180.3
920.1
11824
Filename
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ARP.
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Data
1
2
3
AI
AJ
AK
AL
AM
AN
AO
AP
AQ
AR
AS
AT
AU
UID
Characteristic
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
%
of
Total
mass
Reg
limit
(
g)

­­­­­­­­­­­­­­­­­
EI
CO­­­­­­­­­­­­­­­­­
­­­­­­
Number­­­­­
­­­­­­­­­­­­­­­
Dp/
Foo
(
CO)­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­­­

193
194
195
196
197
198
199
200
201
202
203
204
205
206
207
208
209
210
211
212
213
214
215
216
217
218
219
220
221
222
223
224
5GE086
0.12
0.15
1.58
15.66
3
1
19.08
0.476
18.53
­
19.39
23.4
19.8
6871
6GE087
0.12
0.15
1.58
15.66
3
1
19.08
0.476
18.53­
19.39
23.4
19.8
6871
3GE059
0.09
0.13
6.39
43.32
3
3
58.21
­
55.7­
60.1
63.0
53.4
21173
3GE063
0.15
0.17
1.30
15.26
5
3
19.28
­
16.9­
21.3
20.9
17.7
7005
6GE088
0.12
0.15
1.55
15.52
3
1
18.85
0.47
18.30­
19.15
23.1
19.6
6858
2GE053
0.08
0.12
25.35
37.83
3
3
58.54
­
55.8­
60.2
63.3
53.7
22928
3GE064
0.15
0.16
1.10
13.67
5
3
16.51
­
14.4­
18.4
17.9
15.2
6526
6GE089
0.12
0.13
1.30
14.10
3
1
16.47
0.414
16.00­
16.75
20.2
17.1
6522
3GE060
0.08
0.11
23.48
35.79
3
3
53.84
­
51.0­
55.7
58.2
49.3
22509
3GE065
0.15
0.15
0.98
12.70
5
3
14.91
­
13.0­
16.7
16.1
13.6
6231
6GE090
0.12
0.13
1.16
13.21
3
1
15.05
0.379
14.62­
15.31
18.5
15.7
6305
3GE061
0.08
0.10
21.87
34.70
3
3
51.31
­
48.4­
53.3
55.5
47.0
21891
3GE066
0.15
0.15
0.94
12.35
5
3
14.40
­
12.5­
16.1
15.6
13.2
6142
6GE091
0.12
0.12
1.07
12.69
3
1
14.24
0.358
13.83­
14.49
17.5
14.8
6156
1IA001
0.55
0.55
0.77
7.76
3
1
14.8
­
­
18.2
15.4
1656
3IA006
0.57
0.67
2.60
13.42
3
1
26.90
­
­
33.0
28.0
2760
3IA007
0.54
0.63
2.37
12.64
3
1
24.80
­
­
30.4
25.8
2708
1IA002
0.53
0.62
2.44
12.43
3
1
24.9
­
­
30.6
25.9
2764
1IA003
0.53
0.62
2.44
12.43
3
1
24.9
­
­
30.6
25.9
2764
1IA004
0.47
0.56
2.03
11.53
3
1
21.5
­
­
26.4
22.4
2680
1IA005
0.45
0.52
1.81
10.95
3
1
19.7
­
­
24.2
20.5
2620
3IA008
0.463
0.515
1.65
9.317
3
1
16.00
­
­
19.6
16.6
2241
1KK001
5.5
6.0
21.0
116.0
2
2
466.9
­
­
532.0
450.8
47684
1KK002
5.0
6.0
13.0
64.0
2
1
248.5
­
­
305.0
258.5
25102
Filename
DCTM_
ARP.
xls
Printed
on
5/
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05
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website
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latest
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aviation_
emissions_
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Data
1
2
3
AV
AW
AX
AY
AZ
BA
BB
BC
BD
BE
BF
BG
BH
BI
BJ
UID
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
Original
CAEP
2
CAEP
4
Total
mass
(
g)

­­­­
Number­­­­­

­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­
EI
NOx­­­­­­­­­­­­­­
­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­
Dp/
Foo
(
NOx)­­­­­­­­­­­­­­
Characteristic
as
%
of
standards
193
194
195
196
197
198
199
200
201
202
203
204
205
206
207
208
209
210
211
212
213
214
215
216
217
218
219
220
221
222
223
224
5GE086
40.41
31.77
15.09
5.64
3
1
53.80
0.185
53.61
­
53.98
62.4
56.8
71.0
81.2
19393
6GE087
40.41
31.77
15.09
5.64
3
1
53.80
0.185
53.61­
53.98
62.4
56.8
71.0
81.2
19394
3GE059
45.53
35.68
12.46
5.73
3
3
58.62
­
57.5­
60.5
62.1
56.3
70.3
80.2
21308
3GE063
40.65
31.89
15.64
5.45
5
3
55.03
­
51.0­
57.9
58.3
52.7
65.9
75.1
19995
6GE088
40.91
32.09
15.19
5.66
3
1
54.33
0.187
54.14­
54.52
63.0
57.1
71.4
81.5
19743
2GE053
52.01
40.27
10.30
6.01
3
3
65.08
­
63.8­
67.5
68.9
59.3
74.2
82.8
25703
3GE064
47.28
35.70
16.73
5.69
5
3
61.92
­
57.9­
65.3
65.6
56.6
70.7
79.0
24478
6GE089
47.25
36.17
16.24
5.86
3
1
61.15
0.227
60.90­
61.33
70.9
61.5
76.8
86.1
24177
3GE060
57.34
43.92
10.62
6.11
3
3
70.42
­
69.1­
73.0
74.6
62.5
78.1
86.3
29448
3GE065
53.21
39.13
17.47
5.86
5
3
68.08
­
64.1­
71.9
72.1
60.3
75.4
83.3
28459
6GE090
52.48
39.50
16.94
6.00
3
1
66.78
0.259
66.48­
66.95
77.4
65.2
81.5
90.3
27923
3GE061
59.56
45.41
10.89
6.17
3
3
73.05
­
71.7­
75.7
77.4
64.1
80.1
88.2
31175
3GE066
55.90
40.51
17.74
5.92
5
3
70.71
­
66.8­
74.7
74.9
61.8
77.2
84.9
30172
6GE091
56.41
41.74
17.38
6.09
3
1
70.76
0.278
70.43­
70.92
83.2
68.7
85.9
94.5
30617
1IA001
37.13
30.82
13.45
5.91
3
1
69.3
­
­
80.3
80.7
100.8
120.5
7716
3IA006
24.5
20.8
8.7
4.5
3
1
46
­
­
53.3
58.5
73.1
88.9
4720
3IA007
26.2
22
9
4.7
3
1
48.4
­
­
56.1
59.8
74.8
90.4
5278
1IA002
26.5
22.3
8.9
4.7
3
1
48.5
­
­
56.2
59.6
74.4
89.9
5382
1IA003
26.5
22.3
8.9
4.7
3
1
48.5
­
­
56.2
59.6
74.4
89.9
5382
1IA004
30.5
25.1
9.6
4.9
3
1
53.7
­
­
62.2
62.2
77.8
92.9
6686
1IA005
33.8
27.1
10.1
5.0
3
1
58.0
­
­
67.2
64.5
80.7
94.4
7732
3IA008
36.48
28.67
10.83
5.24
3
1
61.6
­
­
71.4
66.8
83.5
96.6
8646
1KK001
13.9
12.9
5.4
2.7
2
2
44.6
­
­
49.0
79.6
99.5
135.2
4776
1KK002
­
­
­
­
­
­
­
­
­
­

Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
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latest
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aviation_
emissions_
databank
Data
1
2
3
BK
BL
BM
BN
BO
BP
BQ
BR
BS
BT
BU
BV
UID
Characteristic
No
T/
O
C/
O
App
Idle
Test
Eng
Max
Sigma
Range
Characteristic
%
of
Reg
limit
­­­­­­­­­­­­­­
Smoke
Number­­­­­­­­­­­­­

­­­­­­­­­­­­­
Smoke
Number­­­­­­­­­­­­­
­­­­
Number­­­­

193
194
195
196
197
198
199
200
201
202
203
204
205
206
207
208
209
210
211
212
213
214
215
216
217
218
219
220
221
222
223
224
5GE086
2.8
1.8
2.9
2.5
3
1
2.9
0.358
2.59
­
3.23
3.7
22.2
6GE087
2.8
1.8
2.9
2.5
3
1
2.9
0.358
2.59­
3.23
3.7
22.4
3GE059
0
0
0
9.84
3
3
10.2
­
9.4­
10.2
11.2
67.4
3GE063
­
­
­
­
5
3
0.5
­
0.0­
1.92
0.6
3.6
6GE088
2.9
1.8
2.9
2.5
3
1
2.9
0.391
2.60­
3.31
3.7
22.4
2GE053
<
3
<
3
<
3
9.60
3
3
9.80
­
9.2­
9.8
10.8
66.4
3GE064
­
­
­
­
5
3
0.5
­
0.0­
1.92
0.6
3.7
6GE089
3.3
2.4
3
2.5
3
1
3.3
0.648
2.73­
4.01
4.2
26.1
3GE060
0
0
0
9.4
3
3
9.5
­
9.0­
9.5
10.5
65.6
3GE065
­
­
­
­
5
3
0.5
­
0.0­
2.03
0.6
3.8
6GE090
3.6
2.7
3.2
2.5
3
1
3.6
0.713
2.83­
4.25
4.6
28.9
3GE061
0
0
0
9.3
3
3
9.5
­
8.9­
9.5
10.5
66.0
3GE066
­
­
­
­
5
3
0.5
­
0.0­
2.07
0.6
3.8
6GE091
3.7
2.9
3.2
2.5
3
1
3.7
0.726
2.89­
4.29
4.8
30.0
1IA001
­
­
­
­
3
1
3.5
­
­
4.5
19.6
3IA006
­
­
­
­
3
1
9
­
­
11.6
49.4
3IA007
­
­
­
­
3
1
9
­
­
11.6
50.2
1IA002
­
­
­
­
3
1
9.0
­
­
11.6
50.4
1IA003
­
­
­
­
3
1
9.0
­
­
11.6
50.4
1IA004
­
­
­
­
3
1
9.0
­
­
11.6
52.0
1IA005
­
­
­
­
3
1
9.0
­
­
11.6
53.0
3IA008
­
­
­
­
3
1
9
­
­
11.6
53.8
1KK001
­
­
­
­
­
­
23.5
­
­
30.2
128.8
1KK002
­
­
­
­
­
­
­
­
­
­

Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
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aviation_
emissions_
databank
Data
1
2
3
BW
BX
BY
BZ
CA
CB
CC
CD
CE
UID
Fuel
per
No
Spec
H/
C
Arom
T/
O
C/
O
App
Idle
LTO
cycle
Ratio
%
(
kg)

­­­­­­­­­­­­­­­­­
Fuel
Flow­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­(
kg/
sec)­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­­­­­
Fuel­­­­­­­­­­­­­­­­­­­­­­­

193
194
195
196
197
198
199
200
201
202
203
204
205
206
207
208
209
210
211
212
213
214
215
216
217
218
219
220
221
222
223
224
5GE086
Jet
A
1.92
17.4
2.781
2.280
0.763
0.267
1017
6GE087
Jet
A
1.92
17.4
2.781
2.280
0.763
0.267
1017
3GE059
Jet
A
1.94
17.2
2.837
2.321
0.774
0.295
1071
3GE063
Jet
A
1.91­
1.94
18.1­
19.3
2.832
2.332
0.787
0.281
1054
6GE088
Jet
A
1.92
17.4
2.806
2.301
0.768
0.269
1026
2GE053
Jet
A
1.91­
1.92
15.9­
18.6
3.19
2.60
0.85
0.30
1149
3GE064
Jet
A
1.91­
1.94
18.1­
19.3
3.169
2.583
0.852
0.292
1134
6GE089
Jet
A
1.92
17.4
3.115
2.55
0.832
0.282
1107
3GE060
Jet
A
1.94
17.2
3.419
2.756
0.884
0.313
1208
3GE065
Jet
A
1.91­
1.94
18.1­
19.3
3.414
2.772
0.899
0.3
1193
6GE090
Jet
A
1.92
17.4
3.348
2.733
0.878
0.291
1166
3GE061
Jet
A
1.94
17.2
3.523
2.830
0.902
0.316
1231
3GE066
Jet
A
1.91­
1.94
18.1­
19.3
3.515
2.844
0.917
0.304
1217
6GE091
Jet
A
1.92
17.4
3.514
2.848
0.908
0.296
1203
1IA001
Jet
A
­
­
1.113
0.924
0.334
0.124
442
3IA006
Jet
A
­
­
0.971
0.817
0.311
0.118
407
3IA007
Jet
A
­
­
1.042
0.868
0.328
0.123
429
1IA002
Jet
A
­
­
1.053
0.880
0.319
0.128
437
1IA003
Jet
A
­
­
1.053
0.880
0.319
0.128
437
1IA004
Jet
A
­
­
1.209
0.996
0.353
0.134
476
1IA005
Jet
A
­
­
1.331
1.077
0.377
0.138
504
3IA008
Jet
A
­
­
1.426
1.1447
0.3901
0.1363
517
1KK001
TS­
1
2
19
1.75
1.17
0.58
0.24
742
1KK002
TS­
1
2
18
1.75
1.33
0.55
0.22
724
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
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aviation_
emissions_
databank
Data
1
2
3
CF
CG
CH
CI
CJ
CK
CL
CM
UID
No
Baro
Temp
Humidity
kW
@
Power
%
CF
@
Power
kPa
K
kg/
kg
­­­­­­­­­­­­­­­­­­­
Ambient­­­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­
Loads­­­­­­­­­­­­­­­­­­­

Power
Extraction
­­­
Stage
Bleed­­­

193
194
195
196
197
198
199
200
201
202
203
204
205
206
207
208
209
210
211
212
213
214
215
216
217
218
219
220
221
222
223
224
5GE086
0
­
0
­
97.3
­
98.2
279.1
­
281.6
.0022
­
.0064
6GE087
0
­
0
­
97.3
­
98.2
279.1
­
281.6
.0022
­
.0064
3GE059
0
­
0
­
97.38­
98.59
274­
299
.001­.
0073
3GE063
0
­
0
­
97.52­
98.62
283­
301
.0036­.
0151
6GE088
0
­
0
­
97.3
­
98.2
279.1
­
281.6
.0022
­
.0064
2GE053
0
­
0
­
97.38­
98.59
274­
299
.001­.
00726
3GE064
0
­
0
­
97.52­
98.62
283­
301
.0036­.
0151
6GE089
0
­
0
­
97.3
­
98.2
279.1
­
281.6
.0022
­
.0064
3GE060
0
­
0
­
97.38­
98.59
274­
299
.001­.
0073
3GE065
0
­
0
­
97.52­
98.62
283­
301
.0036­.
0151
6GE090
0
­
0
­
97.3
­
98.2
279.1
­
281.6
.0022
­
.0064
3GE061
0
­
0
­
97.38­
98.59
274­
299
.001­.
0073
3GE066
0
­
0
­
97.52­
98.62
283­
301
.0036­.
0151
6GE091
0
­
0
­
97.3
­
98.2
279.1
­
281.6
.0022
­
.0064
1IA001
0
­
4.5
7%
101.3
286
0.0048
3IA006
0
­
6.2%/
5.5%
7%/
30%
101.0­
101.8
288­
296
.0086­.
0114
3IA007
0
­
6.2%/
5.5%
7%/
30%
101.0­
101.8
288­
296
.0086­.
0114
1IA002
0
­
4.5
7%
101.0­
101.8
288
­
296
.0086­.
0114
1IA003
0
­
4.5
7%
101.0­
101.8
288
­
296
.0086­.
0114
1IA004
0
­
4.5
7%
101.0­
101.8
288
­
296
.0086­.
0114
1IA005
0
­
4.5
7%
101.0­
101.8
288
­
296
.0086­.
0114
3IA008
0
­
4.5
7
101.0­
101.8
288­
296
.0086­.
0114
1KK001
0
­
0
­
102.6
300
0.00876
1KK002
0
­
0
­
102.7
293
.00905
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
CN
CO
CP
CQ
CR
CS
UID
­­­
Test
Dates­­­

No
Manufacturer
Test
Organisation
Test
Location
From
To
193
194
195
196
197
198
199
200
201
202
203
204
205
206
207
208
209
210
211
212
213
214
215
216
217
218
219
220
221
222
223
224
5GE086
GE
GE90
Eval
Engineering
Site
IIID,
PTO,
Peebles,
Ohio,
USA
9­
Jan­
00
12­
Jan­
00
6GE087
GE
GE90
Eval
Engineering
Site
IIID,
PTO,
Peebles,
OH
9­
Jan­
00
12­
Jan­
00
3GE059
GE
GE90
Eval
Engineering
Site
IVD
&
6,
PTO,
Peebles,
Ohio,
USA
24­
Feb­
95
28­
Jul­
95
3GE063
GE
GE90
Eval
Engineering
Site
IIID,
PTO,
Peebles,
Ohio,
USA
24­
Apr­
97
19­
Jun­
97
6GE088
GE
GE90
Eval
Engineering
Site
IIID,
PTO,
Peebles,
OH
9­
Jan­
00
12­
Jan­
00
2GE053
GE
GE90
Eval
Engineering
Site
IVD
and
6,
PTO,
Peebles
24­
Feb­
95
28­
Jul­
95
3GE064
GE
GE90
Eval
Engineering
Site
IIID,
PTO,
Peebles,
Ohio,
USA
24­
Apr­
97
19­
Jun­
97
6GE089
GE
GE90
Eval
Engineering
Site
IIID,
PTO,
Peebles,
OH
9­
Jan­
00
12­
Jan­
00
3GE060
GE
GE90
Eval
Engineering
Site
IVD
&
6,
PTO,
Peebles,
Ohio,
USA
24­
Feb­
95
28­
Jul­
95
3GE065
GE
GE90
Eval
Engineering
Site
IIID,
PTO,
Peebles,
Ohio,
USA
24­
Apr­
97
19­
Jun­
97
6GE090
GE
GE90
Eval
Engineering
Site
IIID,
PTO,
Peebles,
OH
9­
Jan­
00
12­
Jan­
00
3GE061
GE
GE90
Eval
Engineering
Site
IVD
&
6,
PTO,
Peebles,
Ohio,
USA
24­
Feb­
95
28­
Jul­
95
3GE066
GE
GE90
Eval
Engineering
Site
IIID,
PTO,
Peebles,
Ohio,
USA
24­
Apr­
97
19­
Jun­
97
6GE091
GE
GE90
Eval
Engineering
Site
IIID,
PTO,
Peebles,
OH
9­
Jan­
00
12­
Jan­
00
1IA001
International
Aero
Engines
Pratt
&
Whitney
East
Hartford,
CT,
USA
2­
Jun­
88
2­
Jun­
88
3IA006
International
Aero
Engines
Pratt
&
Whitney
East
Hartford,
CT,
USA
12­
Aug­
92
13­
Aug­
92
3IA007
International
Aero
Engines
Pratt
&
Whitney
East
Hartford,
CT,
USA
12­
Aug­
92
13­
Aug­
92
1IA002
International
Aero
Engines
Pratt
&
Whitney
East
Hartford,
CT,
USA
12­
Aug­
92
13­
Aug­
92
1IA003
International
Aero
Engines
Pratt
&
Whitney
East
Hartford,
CT,
USA
12­
Aug­
92
13­
Aug­
92
1IA004
International
Aero
Engines
Pratt
&
Whitney
East
Hartford,
CT,
USA
12­
Aug­
92
13­
Aug­
92
1IA005
International
Aero
Engines
Pratt
&
Whitney
East
Hartford,
CT,
USA
12­
Aug­
92
13­
Aug­
92
3IA008
International
Aero
Engines
Pratt
&
Whitney
East
Hartford,
CT,
USA
12­
Aug­
92
13­
Aug­
92
1KK001
KKBM
State
Inst
for
Civ
Aviation
Sheremetjevo,
Moscow
12­
Jul­
89
­

1KK002
KKBM
State
Inst
for
Civ
Aviation
Sheremetjevo,
Moscow
14­
Jun­
90
­

Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
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version
www.
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com/
aviation_
emissions_
databank
Data
1
2
3
CT
CU
UID
No
Remarks
193
194
195
196
197
198
199
200
201
202
203
204
205
206
207
208
209
210
211
212
213
214
215
216
217
218
219
220
221
222
223
224
5GE086
1.
GE
Report
R97AEB298
2.
Engine
S/
N
900326
6GE087
1.
Ref.
GE
Report
R97AEB298,
2.
Engine
S/
N
900326
3.
Turbomachinery
incorporating
3D
aero
3GE059
1.
GE
Report
TM95­
17.
2.
Engine
S/
N
704/
223
&
704/
234
3.
DAC
I
combustor
3GE063
1.
GE
Report
R96AEB292.
2.
Engine
S/
S
900­
173,
900­
166
&
900­
167
3.
DAC
II
combustor
6GE088
1.
Ref.
GE
Report
R97AEB298,
2.
Engine
S/
N
900326
3.
Turbomachinery
incorporating
3D
aero
2GE053
1.
Ref
GE
Report
TM95­
45.
2.
Engine
S/
N
900­
108,
900­
111
&
900­
114.
3.
Post
certification/
as
delivered
to
service.
4.
Smoke
<
3
below
meas.
capa
3GE064
1.
GE
Report
R96AEB292.
2.
Engine
S/
S
900­
173,
900­
166
&
900­
167
3.
DAC
II
combustor
6GE089
1.
Ref.
GE
Report
R97AEB298,
2.
Engine
S/
N
900326
3.
Turbomachinery
incorporating
3D
aero
3GE060
1.
GE
Report
TM95­
17.
2.
Engine
S/
N
704/
223
&
704/
234
3.
DAC
I
combustor
3GE065
1.
GE
Report
R96AEB292.
2.
Engine
S/
S
900­
173,
900­
166
&
900­
167
3.
DAC
II
combustor
6GE090
1.
Ref.
GE
Report
R97AEB298,
2.
Engine
S/
N
900326
3.
Turbomachinery
incorporating
3D
aero
3GE061
1.
GE
Report
TM95­
17.
2.
Engine
S/
N
704/
223
&
704/
234
3.
DAC
I
combustor
3GE066
1.
GE
Report
R96AEB292.
2.
Engine
S/
S
900­
173,
900­
166
&
900­
167
3.
DAC
II
combustor
6GE091
1.
Ref.
GE
Report
R97AEB298,
2.
Engine
S/
N
900326
3.
Turbomachinery
incorporating
3D
aero
1IA001
V2500
renamed
V2500­
A1
3IA006
­

3IA007
­

1IA002
­

1IA003
­

1IA004
­

1IA005
­

3IA008
­

1KK001
1.
Data
obtained
on
aircraft
(
Tu­
154A)
2.
In­
service
engine(
s),
tested
after
overhaul
1KK002
1.
Data
obtained
on
aircraft
(
Tu­
154A)
2.
In­
service
engine(
s),
tested
after
overhaul
Filename
DCTM_
ARP.
xls
Printed
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5/
20/
05
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for
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version
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aviation_
emissions_
databank
Data
1
2
3
CV
CW
CX
CY
CZ
DA
DB
DC
DD
DE
DF
DG
DH
193
194
195
196
197
198
199
200
201
202
203
204
205
206
207
208
209
210
211
212
213
214
215
216
217
218
219
220
221
222
223
224
pability.
5.
DAC
I
combustor
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
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version
www.
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aviation_
emissions_
databank
Data
1
2
3
DI
DJ
DK
DL
DM
DN
193
194
195
196
197
198
199
200
201
202
203
204
205
206
207
208
209
210
211
212
213
214
215
216
217
218
219
220
221
222
223
224
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
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for
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www.
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aviation_
emissions_
databank
Data
1
2
3
A
B
C
D
E
F
G
UID
Engine
Combustor
Eng
B/
P
Press
Rated
No
Identification
Description
Type
Ratio
Ratio
Output
kN
225
226
227
228
229
230
231
232
233
234
235
236
237
238
239
240
241
242
243
244
245
246
247
248
249
250
251
252
253
254
255
256
1KK003
NK­
86
MTF
1.33
13.4
127.53
1KK004
NK­
86A
MTF
1.13
13.2
130.47
1KK005
NK­
86MA
MTF
1.13
13.2
130.47
Pratt
&
Whitney
Aircraft
Group
1PW035
JT15D­
1
series
TF
3.3
9.76
9.79
1PW036
JT15D­
4
series
TF
2.68
10.1
11.12
1PW037
JT15D­
5,
­
5A,
­
5B
TF
2.1
12.3
12.90
1PW038
JT15D­
5C
TF
2.1
13.3
14.19
1PW001
JT3D­
3B
TF
1.4
13.6
80.06
1PW003
JT3D­
7
series
Smoke
fix
14­
70KC
TF
1.4
13.4
84.52
1PW002
JT3D­
7
series
14­
57D
TF
1.4
13.4
84.52
1PW008
JT8D­
11
MTF
1.00
17.17
66.72
1PW010
JT8D­
15
Reduced
emissions
MTF
1.03
16.81
68.94
1PW009
JT8D­
15
Smoke
fix
MTF
1.03
16.81
68.94
1PW011
JT8D­
15A
MTF
1.08
16.45
68.94
1PW013
JT8D­
17
Reduced
emissions
MTF
1.02
17.01
71.17
1PW012
JT8D­
17
Smoke
fix
MTF
1.01
17.01
71.17
1PW014
JT8D­
17A
MTF
1.05
16.87
71.17
1PW015
JT8D­
17AR
MTF
0.96
17.28
77.42
1PW016
JT8D­
17R
MTF
0.97
18.24
77.42
1PW017
JT8D­
209
MTF
1.80
18.30
85.60
4PW068
JT8D­
217
Environmental
Kit
(
E_
Kit)
MTF
1.73
19.66
92.74
1PW018
JT8D­
217
series
MTF
1.73
19.66
92.74
4PW069
JT8D­
217A
Environmental
Kit
(
E_
Kit)
MTF
1.73
19.66
92.74
4PW070
JT8D­
217C
Environmental
Kit
(
E_
Kit)
MTF
1.70
19.05
92.74
4PW071
JT8D­
219
Environmental
Kit
(
E_
Kit)
MTF
1.70
20.27
96.52
1PW019
JT8D­
219
MTF
1.70
20.27
96.52
1PW005
JT8D­
7
series
Reduced
emissions
MTF
1.05
15.82
62.27
1PW004
JT8D­
7
series
Smoke
fix
MTF
1.05
15.82
62.27
1PW007
JT8D­
9
series
Reduced
emissions
MTF
1.04
15.88
64.5
Filename
DCTM_
ARP.
xls
Printed
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5/
20/
05
Check
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for
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aviation_
emissions_
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Data
1
2
3
H
I
J
K
L
M
N
O
P
Q
R
S
T
U
UID
Data
Superseded
Data
No
PR
C
R
superseded
by
NME
DTEPS
Other
Corr
as
Out
of
Date
Out
of
Date
UID
No
Annex
16
Production
Service
­­­­­­­­
Data
Status­­­­­­­­
­­­­­­­­­­
Current
Engine
Status
­­­­­­­­­­

­­­­­­
Test
Engine
Status­­­­­­

225
226
227
228
229
230
231
232
233
234
235
236
237
238
239
240
241
242
243
244
245
246
247
248
249
250
251
252
253
254
255
256
1KK003
­
­
x
­
­
­
­
x
­
x
­
­
­

1KK004
­
­
x
­
­
­
­
x
x
x
­
­
­

1KK005
­
x
­
­
­
x
­
­
x
­
­
­
­

1PW035
x
­
­
­
­
­
x
­
x
x
­
­
­

1PW036
x
­
­
­
­
­
x
­
x
x
­
­
­

1PW037
­
x
­
­
­
­
x
­
x
x
­
­
­

1PW038
­
x
­
­
­
­
x
­
x
x
­
­
­

1PW001
x
­
­
­
­
­
x
­
x
x
­
­
­

1PW003
x
­
­
­
­
­
x
­
x
x
­
­
­

1PW002
x
­
­
­
­
­
x
­
x
x
­
­
­

1PW008
x
­
­
­
­
x
­
­
x
x
­
­
­

1PW010
­
x
­
­
­
­
x
­
x
x
­
­
­

1PW009
x
­
­
­
­
x
­
­
x
x
­
­
­

1PW011
­
x
­
­
­
­
x
­
x
x
­
­
­

1PW013
­
x
­
­
­
­
x
­
x
x
­
­
­

1PW012
x
­
­
­
­
x
­
­
x
x
­
­
­

1PW014
­
x
­
­
­
­
x
­
x
x
­
­
­

1PW015
­
x
­
­
­
­
x
­
x
x
­
­
­

1PW016
­
x
­
­
­
­
x
­
x
x
­
­
­

1PW017
­
x
­
­
­
­
x
­
x
x
­
­
­

4PW068
­
x
­
­
­
­
x
­
x
x
­
­
­

1PW018
­
x
­
­
­
­
x
­
x
x
­
­
­

4PW069
­
x
­
­
­
­
x
­
x
x
­
­
­

4PW070
­
x
­
­
­
­
x
­
x
­
­
­
­

4PW071
­
x
­
­
­
­
x
­
x
­
­
­
­

1PW019
­
x
­
­
­
­
x
­
x
x
­
­
­

1PW005
­
x
­
­
­
­
x
­
x
x
­
­
­

1PW004
x
­
­
­
­
­
­
x
x
x
­
­
­

1PW007
­
x
­
­
­
­
x
­
x
x
­
­
­

Filename
DCTM_
ARP.
xls
Printed
on
5/
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05
Check
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aviation_
emissions_
databank
Data
1
2
3
V
W
X
Y
Z
AA
AB
AC
AD
AE
AF
AG
AH
UID
Characteristic
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
%
of
Total
mass
Reg
limit
(
g)

­­­­­­­­­­­­­­­­
EI
HC­­­­­­­­­­­­­­
­­­
Number
­­­
­­­­­­­­­­­­­­­
Dp/
Foo
(
HC)­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­
­­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­­­­­

225
226
227
228
229
230
231
232
233
234
235
236
237
238
239
240
241
242
243
244
245
246
247
248
249
250
251
252
253
254
255
256
1KK003
0.5
0.6
1.2
52.0
3
3
135
­
­
157.5
803.5
17379
1KK004
0.2
0.2
2.2
15.3
2
1
45.2
­
­
69.6
355.2
5988
1KK005
0.16
0.13
0.30
4.60
7
5
13.5
3.7
8.7­
17.1
15.2
77.4
1773
1PW035
0.01
0.01
4.43
50.5
1
1
190.65
­
­
293.6
1498.1
1866
1PW036
0.09
0.19
5.15
40.0
1
1
152.83
­
­
235.4
1200.9
1706
1PW037
0
1.3
11.7
119.1
1
1
479.8
­
­
738.9
3769.9
5715
1PW038
0
0.67
16.0
96.67
1
1
312.8
­
­
481.7
2457.7
4439
1PW001
4.0
2.0
4.0
112.0
­
2
303.9
­
­
395.4
2017.6
24363
1PW003
­
­
­
­
­
­
143.0
­
­
220.2
1123.7
1PW002
0.50
0.40
2.10
123.00
­
­
293.9
­
­
452.6
2309.4
24838
1PW008
0.40
0.45
1.4
10.0
14
13
36.8
­
­
39.5
201.6
2455
1PW010
0.24
0.28
0.55
1.46
8
3
6.1
­
­
7.1
36.3
428
1PW009
0.25
0.25
1.65
11.0
8
7
39.3
­
­
43.4
221.2
2713
1PW011
0.25
0.33
0.65
1.86
7
2
7.2
­
­
9.4
47.8
497
1PW013
0.22
0.27
0.52
1.25
8
3
5.3
­
­
6.2
31.5
379
1PW012
0.69
0.79
1.96
10.2
8
7
37.2
9.3
­
41.0
209.4
2646
1PW014
0.25
0.30
0.64
6.6
7
2
6.6
­
­
8.6
43.8
1543
1PW015
0.21
0.27
0.55
1.33
8
3
5.2
­
­
6.1
31.0
403
1PW016
0.21
0.27
0.53
0.95
8
3
4.2
­
­
4.9
25.0
329
1PW017
0.35
0.50
1.69
4.03
3
1
12.2
­
­
18.8
95.9
1047
4PW068
0.00
0.00
0.00
0.00
3
1
0.00
­
­
0.0
0.0
0
1PW018
0.28
0.43
1.60
3.33
3
1
10.1
­
­
15.6
79.4
937
4PW069
0.00
0.00
0.00
0.00
3
1
0.00
­
­
0.0
0.0
0
4PW070
0.00
0.00
0.00
0.00
3
1
0.00
­
­
0.0
0.0
0
4PW071
0.00
0.00
0.00
0.00
3
1
0.00
­
­
0.0
0.0
0
1PW019
0.27
0.42
1.59
3.48
3
1
9.9
­
­
15.2
77.8
951
1PW005
0.25
0.25
0.4
3.8
7
2
13.2
­
­
17.2
87.6
830
1PW004
0.4
0.5
1.6
10.6
14
13
37.2
­
­
39.9
203.8
2315
1PW007
0.15
0.18
0.60
3.12
7
2
11.1
­
­
14.4
73.7
713
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
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aviation_
emissions_
databank
Data
1
2
3
AI
AJ
AK
AL
AM
AN
AO
AP
AQ
AR
AS
AT
AU
UID
Characteristic
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
%
of
Total
mass
Reg
limit
(
g)

­­­­­­­­­­­­­­­­­
EI
CO­­­­­­­­­­­­­­­­­
­­­­­­
Number­­­­­
­­­­­­­­­­­­­­­
Dp/
Foo
(
CO)­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­­­

225
226
227
228
229
230
231
232
233
234
235
236
237
238
239
240
241
242
243
244
245
246
247
248
249
250
251
252
253
254
255
256
1KK003
3.9
4.2
9.3
54.4
3
3
158.2
­
­
171.1
145.0
20396
1KK004
1.8
2.2
7.8
38.0
2
1
120.7
­
­
148.2
125.6
15703
1KK005
1.55
1.90
5.90
29.80
7
5
94.6
22.5
61.3­
113
100.5
85.1
12334
1PW035
2.65
3.50
40.5
132
1
1
541.97
­
­
665.2
563.8
5306
1PW036
2.1
3.18
32
97
1
1
401.30
­
­
492.6
417.4
4478
1PW037
0
1.15
38.6
119.2
1
1
476.1
­
­
584.4
495.3
6142
1PW038
2.52
4.18
49.24
124.60
1
1
443.1
­
­
543.9
460.9
6288
1PW001
1.5
2.8
24.5
98.0
­
2
288.1
­
­
328.2
278.2
23092
1PW003
­
­
­
­
­
­
187.0
­
­
229.5
194.5
1PW002
0.89
1.90
19.50
138.99
­
­
353.5
­
­
433.9
367.7
29880
1PW008
1.2
1.9
9.4
35.0
14
13
134.7
­
­
139.8
118.4
8983
1PW010
1.03
1.15
2.77
11.0
8
3
42.6
­
­
46.1
39.0
2955
1PW009
0.7
1.0
9.6
35.2
8
7
130.6
­
­
137.4
116.4
9054
1PW011
1.08
1.2
2.9
12.93
8
3
46.8
­
­
50.6
42.9
3177
1PW013
0.95
1.10
2.67
10.46
8
3
39.4
­
­
42.6
36.1
2826
1PW012
0.74
1.00
8.54
31.00
8
7
112.5
12.4
­
118.3
100.3
8005
1PW014
1.07
1.16
2.88
12.46
8
3
43.8
­
­
47.4
40.1
3147
1PW015
0.93
1.08
2.68
10.7
8
3
37.2
­
­
40.2
34.1
2898
1PW016
0.95
1.03
2.54
9.43
8
3
34.8
­
­
37.6
31.9
2716
1PW017
1.03
1.4
4.37
14.1
3
1
40.6
­
­
49.8
42.2
3476
4PW068
0.42
0.47
3.54
15.31
3
1
39.8
­
­
48.9
41.4
3693
1PW018
0.80
1.23
4.17
12.27
3
1
34.8
­
­
42.7
36.2
3229
4PW069
0.42
0.47
3.54
15.31
3
1
39.8
­
­
48.9
41.4
3693
4PW070
0.42
0.49
3.79
17.89
3
1
45.8
­
­
56.2
47.6
4244
4PW071
0.42
0.46
3.57
17.19
3
1
41.7
­
­
51.2
43.4
4021
1PW019
0.73
1.20
4.07
12.63
3
1
33.5
­
­
41.1
34.8
3234
1PW005
0.9
1.1
2.2
14.3
7
2
50.9
­
­
52.9
44.8
3186
1PW004
1.5
2.0
10.5
35.5
14
13
130.9
­
­
135.8
115.1
8147
1PW007
1.04
1.11
2.14
14.14
7
2
50.2
­
­
57.2
48.5
3241
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
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website
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version
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aviation_
emissions_
databank
Data
1
2
3
AV
AW
AX
AY
AZ
BA
BB
BC
BD
BE
BF
BG
BH
BI
BJ
UID
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
Original
CAEP
2
CAEP
4
Total
mass
(
g)

­­­­
Number­­­­­

­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­
EI
NOx­­­­­­­­­­­­­­
­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­
Dp/
Foo
(
NOx)­­­­­­­­­­­­­­
Characteristic
as
%
of
standards
225
226
227
228
229
230
231
232
233
234
235
236
237
238
239
240
241
242
243
244
245
246
247
248
249
250
251
252
253
254
255
256
1KK003
12.8
12.1
5.1
2.7
3
3
41.3
­
­
43.7
65.5
81.9
108.2
5440
1KK004
15.7
12.4
5.8
3.1
2
1
46.1
­
­
53.4
80.5
100.6
133.2
6106
1KK005
13.0
9.4
3.9
2.3
4
4
35.5
2.3
32­
40.1
37.3
56.2
70.2
93.0
4633
1PW035
7.6
6.77
3.44
1.75
1
1
26.85
­
­
31.1
52.3
65.4
60.8
263
1PW036
9.23
8.56
5.29
2.63
1
1
36.77
­
­
42.6
70.8
88.5
82.9
409
1PW037
11.13
10.08
4.93
1.66
1
1
37.3
­
­
43.2
66.9
83.6
79.2
481
1PW038
9.93
9.79
5.23
1.08
1
1
32.0
­
­
37.1
55.7
69.6
66.4
454
1PW001
12.1
9.9
4.8
2.5
­
2
34.3
­
­
37.7
56.1
70.2
88.3
2740
1PW003
­
­
­
­
­
­
51.5
­
­
59.7
89.4
111.7
144.0
1PW002
12.69
9.59
5.30
2.20
­
­
34.4
­
­
39.9
59.7
74.6
96.2
2909
1PW008
18.9
14.6
5.8
2.75
14
13
56.1
­
­
57.6
77.5
96.9
112.6
3740
1PW010
19.4
15.1
6.9
3.2
5
2
59.6
­
­
65.5
89.0
111.3
130.7
4144
1PW009
19.1
15.0
5.9
3.0
8
7
57.9
­
­
60.1
81.6
102.0
119.9
3989
1PW011
18.1
13.9
6.6
3.1
5
2
51.4
­
­
56.5
77.5
96.9
114.0
3648
1PW013
20.6
15.7
8.0
3.2
5
2
63.7
­
­
70.0
94.6
118.3
140.1
4559
1PW012
19.20
15.23
6.10
3.3
8
7
60.2
7.2
­
62.5
84.4
105.5
125.0
4283
1PW014
19.1
14.3
6.7
3.2
5
2
55.1
­
­
60.6
82.2
102.7
121.7
3935
1PW015
24.5
16.0
8.0
3.2
5
2
64.6
­
­
71.0
95.3
119.1
144.6
5039
1PW016
25.3
17.6
8.4
3.3
5
2
72.3
­
­
79.5
104.0
129.9
156.9
5623
1PW017
22.8
19.0
8.8
3.5
3
1
59.3
­
­
68.7
89.7
112.2
140.1
5075
4PW068
17.54
13.54
7.66
4.57
3
1
49.4
­
­
57.3
72.2
90.3
113.6
4582
1PW018
25.7
20.6
9.1
3.7
3
1
64.6
­
­
74.9
94.4
118.0
148.4
5985
4PW069
17.54
13.54
7.66
4.57
3
1
49.4
­
­
57.3
72.2
90.3
113.6
4582
4PW070
16.49
13.02
7.65
4.05
3
1
45.5
­
­
52.7
67.5
84.3
106.5
4216
4PW071
18.72
13.73
7.65
4.16
3
1
47.7
­
­
55.3
68.7
85.8
107.5
4604
1PW019
27.0
20.8
9.13
3.6
3
1
63.3
­
­
73.4
91.1
113.9
142.7
6106
1PW005
17.2
14.0
6.3
3.15
4
2
52.3
­
­
57.5
80.3
100.3
115.1
3281
1PW004
17.1
13.5
5.5
2.7
14
13
49.5
­
­
50.9
71.0
88.7
101.8
3078
1PW007
19.3
14.5
6.0
2.9
4
2
54.2
­
­
59.6
83.1
103.8
120.2
3488
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
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version
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aviation_
emissions_
databank
Data
1
2
3
BK
BL
BM
BN
BO
BP
BQ
BR
BS
BT
BU
BV
UID
Characteristic
No
T/
O
C/
O
App
Idle
Test
Eng
Max
Sigma
Range
Characteristic
%
of
Reg
limit
­­­­­­­­­­­­­­
Smoke
Number­­­­­­­­­­­­­

­­­­­­­­­­­­­
Smoke
Number­­­­­­­­­­­­­
­­­­
Number­­­­

225
226
227
228
229
230
231
232
233
234
235
236
237
238
239
240
241
242
243
244
245
246
247
248
249
250
251
252
253
254
255
256
1KK003
­
­
­
­
1
1
22.1
­
­
28.4
128.5
1KK004
­
­
­
­
10
­
­
­
­
­

1KK005
­
­
­
­
10
7
9.9
2.9
6­
16
10.5
47.8
1PW035
15
­
­
­
1
1
15
­
­
19.3
43.2
1PW036
14.1
­
­
­
1
1
14.1
­
­
18.1
42.0
1PW037
18.5
­
­
­
1
1
18.5
­
­
24.1
58.1
1PW038
17.1
15.1
­
­
2
2
17.1
2.23
15.5­
17.1
20.1
49.7
1PW001
­
­
­
­
­
2
54.5
­
­
63.9
254.1
1PW003
­
­
­
­
­
­
18
­
­
23.2
93.5
1PW002
­
­
­
­
­
­
52
­
­
66.9
270.0
1PW008
­
­
­
­
14
13
23
­
­
24.0
90.9
1PW010
15.7
­
­
­
5
3
15.7
­
­
17.3
65.9
1PW009
­
­
­
­
8
7
23.8
­
­
25.3
96.6
1PW011
15.7
­
­
­
4
3
15.7
­
­
17.3
65.9
1PW013
16.8
­
­
­
5
3
16.8
­
­
18.5
71.1
1PW012
­
­
­
­
8
7
24
3
­
25.5
98.2
1PW014
16.8
­
­
­
5
3
16.8
­
­
18.5
71.1
1PW015
19.6
­
­
­
5
3
19.6
­
­
21.6
84.9
1PW016
19.6
­
­
­
5
3
19.6
­
­
21.6
84.9
1PW017
11.1
­
­
­
3
1
11.1
­
­
14.3
57.8
4PW068
6.1
­
­
­
3
1
6.1
­
­
7.9
32.7
1PW018
13.2
­
­
­
3
1
13.3
­
­
17.1
70.8
4PW069
6.1
­
­
­
3
1
6.1
­
­
7.9
32.7
4PW070
6.1
­
­
­
3
1
6.1
­
­
7.9
32.7
4PW071
6.9
­
­
­
3
1
6.9
­
­
8.9
37.2
1PW019
14.3
­
­
­
3
1
14.5
­
­
18.7
78.1
1PW005
9.5
­
­
­
4
2
9.5
­
­
11.1
41.3
1PW004
22.2
­
­
­
14
13
22.2
­
­
23.2
86.1
1PW007
10.1
­
­
­
4
2
10.1
­
­
11.8
44.4
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
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aviation_
emissions_
databank
Data
1
2
3
BW
BX
BY
BZ
CA
CB
CC
CD
CE
UID
Fuel
per
No
Spec
H/
C
Arom
T/
O
C/
O
App
Idle
LTO
cycle
Ratio
%
(
kg)

­­­­­­­­­­­­­­­­­
Fuel
Flow­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­(
kg/
sec)­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­­­­­
Fuel­­­­­­­­­­­­­­­­­­­­­­­

225
226
227
228
229
230
231
232
233
234
235
236
237
238
239
240
241
242
243
244
245
246
247
248
249
250
251
252
253
254
255
256
1KK003
TS­
1
2
18.5
2.40
1.60
0.58
0.21
779
1KK004
TS­
1
2
19
2.050
1.700
0.600
0.235
821
1KK005
TS­
1
2
18.6
2.050
1.700
0.600
0.235
821
1PW035
Jet
A­
1
1.85
<
20
0.148
0.124
0.051
0.023
71
1PW036
Jet
A­
1
1.85
<
20
0.1697
0.143
0.059
0.0261
81
1PW037
Jet
A­
1
1.85
­
0.2054
0.1727
0.0660
0.0296
93
1PW038
Jet
A­
1
1.85
­
0.2151
0.1802
0.0678
0.0276
92
1PW001
Jet
A
­
­
1.174
0.932
0.346
0.135
466
1PW003
Jet
A
­
­
1.254
1.032
0.389
0.128
482
1PW002
Jet
A
­
­
1.254
1.032
0.389
0.128
482
1PW008
Jet
A
­
­
1.121
0.9136
0.3339
0.1455
475
1PW010
Jet
A
­
­
1.178
0.9450
0.3402
0.1477
486
1PW009
Jet
A
­
­
1.178
0.9450
0.3403
0.1477
486
1PW011
Jet
A
­
­
1.115
0.8955
0.3120
0.1372
454
1PW013
Jet
A
­
­
1.245
0.9970
0.3540
0.1474
499
1PW012
Jet
A
1.89
­
1.245
0.997
0.354
0.147
498
1PW014
Jet
A
­
­
1.173
0.9344
0.3304
0.1401
470
1PW015
Jet
A
­
­
1.365
1.047
0.3574
0.1477
512
1PW016
Jet
A
­
­
1.417
1.103
0.3755
0.1550
537
1PW017
Jet
A
­
19.2
1.191
0.9828
0.3592
0.1303
469
4PW068
Jet
A
­
18
1.320
1.078
0.3833
0.1372
504
1PW018
Jet
A
­
­
1.320
1.078
0.3833
0.1372
504
4PW069
Jet
A
­
18
1.320
1.078
0.3833
0.1372
504
4PW070
Jet
A
­
18
1.282
1.045
0.363
0.137
493
4PW071
Jet
A
­
18
1.354
1.085
0.3817
0.1344
501
1PW019
Jet
A
­
19.2
1.354
1.085
0.3817
0.1344
501
1PW005
Jet
A
­
­
0.9892
0.8113
0.2861
0.1291
419
1PW004
Jet
A
­
­
0.9892
0.8113
0.2861
0.1291
419
1PW007
Jet
A
­
­
1.040
0.8453
0.2977
0.1323
433
Filename
DCTM_
ARP.
xls
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on
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20/
05
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for
latest
version
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aviation_
emissions_
databank
Data
1
2
3
CF
CG
CH
CI
CJ
CK
CL
CM
UID
No
Baro
Temp
Humidity
kW
@
Power
%
CF
@
Power
kPa
K
kg/
kg
­­­­­­­­­­­­­­­­­­­
Ambient­­­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­
Loads­­­­­­­­­­­­­­­­­­­

Power
Extraction
­­­
Stage
Bleed­­­

225
226
227
228
229
230
231
232
233
234
235
236
237
238
239
240
241
242
243
244
245
246
247
248
249
250
251
252
253
254
255
256
1KK003
0
­
0
­
102.7­
103.0
290
­
291
.00915
1KK004
0
­
0
­
102.3
270
.00238
1KK005
0
­
0
­
101.2­
102.4
260
­
298
.00079­.
0200
1PW035
0
­
0
­
100.526
290
0.0079
1PW036
0
­
0
­
103.146
257
0.0015
1PW037
0
­
0
­
99.42
280.3
.0036
1PW038
0
­
0
­
101.7
300
.010
1PW001
0
­
0
­
­
­
­

1PW003
0
­
0
­
­
­
­

1PW002
0
­
0
­
­
­
­

1PW008
0
­
0
­
­
262
­
300
­

1PW010
0
­
0
­
­
266
­
297
­

1PW009
0
­
0
­
­
269
­
302
­

1PW011
0
­
0
­
­
266
­
297
­

1PW013
0
­
0
­
­
266
­
297
­

1PW012
0
­
0
­
­
269
­
303
0.0029­
0.0093
1PW014
0
­
0
­
­
266
­
297
­

1PW015
0
­
0
­
­
266
­
297
­

1PW016
0
­
0
­
­
266
­
297
­

1PW017
0
­
0
­
­
275
­
288
­

4PW068
0
­
0
­
98.8­
103.1
271
­
281
.0009
­
.0047
1PW018
0
­
0
­
­
275
­
288
­

4PW069
0
­
0
­
98.8­
103.1
271
­
281
.0009
­
.0047
4PW070
0
­
0
­
98.8­
103.1
271
­
281
.0009
­
.0047
4PW071
0
­
0
­
98.8­
103.1
271
­
281
.0009
­
.0047
1PW019
0
­
0
­
­
275
­
288
­

1PW005
0
­
0
­
­
270
­
311
­

1PW004
0
­
0
­
100­
102
262
­
300
0.0005­
0.0123
1PW007
0
­
0
­
­
270
­
311
­

Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
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aviation_
emissions_
databank
Data
1
2
3
CN
CO
CP
CQ
CR
CS
UID
­­­
Test
Dates­­­

No
Manufacturer
Test
Organisation
Test
Location
From
To
225
226
227
228
229
230
231
232
233
234
235
236
237
238
239
240
241
242
243
244
245
246
247
248
249
250
251
252
253
254
255
256
1KK003
KKBM
State
Inst
for
Civ
Aviation
Sheremetjevo,
Moscow
15­
Jun­
89
­

1KK004
KKBM
KKBM
Samara
City
4­
Oct­
87
­

1KK005
KKBM
KKBM
Samara
City
18­
Jul­
87
20­
Jan­
90
1PW035
Pratt
&
Whitney
(
Canada)
Pratt
&
Whitney
(
Canada)
Longueuil,
Quebec
17­
Aug­
77
­

1PW036
Pratt
&
Whitney
(
Canada)
Pratt
&
Whitney
(
Canada)
Longueuil,
Quebec
1­
Feb­
73
­

1PW037
Pratt
&
Whitney
(
Canada)
Pratt
&
Whitney
(
Canada)
Longueuil,
Quebec
16­
Apr­
93
22­
Apr­
93
1PW038
Pratt
&
Whitney
(
Canada)
Pratt
&
Whitney
(
Canada)
Longueuil,
Quebec
13­
Jul­
93
13­
Jul­
93
1PW001
Pratt
&
Whitney
P&
WA
East
Hartford,
CT,
USA.
8­
Mar­
72
12­
Sep­
74
1PW003
Pratt
&
Whitney
P&
WA
East
Hartford,
CT,
USA.
­
­

1PW002
Pratt
&
Whitney
P&
WA
East
Hartford,
CT,
USA.
­
­

1PW008
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
26­
Feb­
80
18­
Jun­
80
1PW010
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
7­
Dec­
79
19­
Jun­
80
1PW009
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
Apr­
76
Mar­
77
1PW011
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
7­
Dec­
79
19­
Jun­
80
1PW013
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
7­
Dec­
79
19­
Jun­
80
1PW012
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
Apr­
76
Mar­
77
1PW014
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
7­
Dec­
79
19­
Jun­
80
1PW015
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
7­
Dec­
79
19­
Jun­
80
1PW016
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
7­
Dec­
79
19­
Jun­
80
1PW017
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
7­
Nov­
83
30­
Nov­
83
4PW068
Pratt
&
Whitney
P&
WA
East
Hartford,
CT
24­
Feb­
99
2­
Mar­
99
1PW018
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
7­
Nov­
83
30­
Nov­
83
4PW069
Pratt
&
Whitney
P&
WA
East
Hartford,
CT
24­
Feb­
99
2­
Mar­
99
4PW070
Pratt
&
Whitney
P&
WA
East
Hartford,
CT
24­
Feb­
99
2­
Mar­
99
4PW071
Pratt
&
Whitney
P&
WA
East
Hartford,
CT
24­
Feb­
99
2­
Mar­
99
1PW019
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
7­
Nov­
83
30­
Nov­
83
1PW005
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
26­
Feb­
80
18­
Jun­
80
1PW004
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
Apr­
76
Mar­
77
1PW007
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
26­
Feb­
80
18­
Jun­
80
Filename
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ARP.
xls
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Data
1
2
3
CT
CU
UID
No
Remarks
225
226
227
228
229
230
231
232
233
234
235
236
237
238
239
240
241
242
243
244
245
246
247
248
249
250
251
252
253
254
255
256
1KK003
1.
Data
obtained
on
aircraft
(
Il­
86)
2.
In­
service
engine(
s),
tested
after
overhaul
1KK004
1.
For
Il­
86
aircraft.
2.
In­
service
engine(
s),
tested
before
overhaul.

1KK005
1.
NK­
86A
with
modified
combustor.
2.
For
IL­
86
aircraft.

1PW035
1.
Not
required
to
meet
GASEOUS
emissions
regulations.
2.
Applicable
to
JT15D­
1,
­
1A,
­
1B.

1PW036
1.
Not
required
to
meet
GASEOUS
emissions
regulations.
2.
Applicable
to
JT15D­
4,
­
4B,
­
4C,
­
4D
1PW037
1.
Not
required
to
meet
GASEOUS
emissions
regulations.

1PW038
1.
Not
required
to
meet
GASEOUS
emissions
regulations.

1PW001
Emissions
data
estimated
from
JT3D­
7
engines
using
JT3D­
3B
performance
data.

1PW003
1.
Smoke
fix
combustor
14­
70KC.
2.
Applicable
to
JT3D­
7,
­
7A.

1PW002
1.
Combustor
14­
57D.
2.
Applicable
to
JT3D­
7,
­
7A
1PW008
Reduced
Emissions
Combustor
incorporated
1/
1/
84
1PW010
Reduced
Emissions
Combustor
incorporated
1/
1/
84
1PW009
Smoke
fix
combustor
in
production
prior
to
1/
1/
84
1PW011
Reduced
Emissions
Combustor
incorporated
1/
1/
84
1PW013
Reduced
emissions
combustor
incorporated
1/
1/
84
1PW012
Smoke
fix
combustor
in
production
prior
to
1/
1/
84
1PW014
Reduced
emissions
combustor
incorporated
1/
1/
84
1PW015
Reduced
emissions
combustor
incorporated
1/
1/
84
1PW016
Reduced
emissions
combustor
incorporated
1/
1/
84
1PW017
1.
All
measurements
by
traverse.
2.
SCH
46­
16B
combustor.

4PW068
Environmental
Kit
(
E­
Kit)
Combustor
and
Fuel
Nozzles,
incorporated
5/
99
1PW018
1.
All
measurements
by
traverse.
2.
SCH
46­
16B
combustor.
3.
Applicable
to
JT8D­
217,
­
217A,
­
217C.

4PW069
Environmental
Kit
(
E­
Kit)
Combustor
and
Fuel
Nozzles,
incorporated
5/
99
4PW070
Environmental
Kit
(
E­
Kit)
Combustor
and
Fuel
Nozzles,
incorporated
5/
99
4PW071
Environmental
Kit
(
E­
Kit)
Combustor
and
Fuel
Nozzles,
incorporated
5/
99
1PW019
1.
All
measurements
by
traverse.
2.
SCH
46­
16B
combustor.

1PW005
1.
Reduced
emissions
combustor.
2.
Applicable
to
JT8D­
7,
­
7A,
­
7B.

1PW004
1.
Smoke
fix
combustor
in
production
prior
to
1/
1/
84.
2.
Applicable
to
JT8D­
7,
­
7A,
­
7B.
3.
Tests
performed
on
in­
service
engine(
s).

1PW007
1.
Reduced
Emissions
Combustor
incorporated
1/
1/
84.
2.
Applicable
to
JT8D­
9,
­
9A.

Filename
DCTM_
ARP.
xls
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Data
1
2
3
CV
CW
CX
CY
CZ
DA
DB
DC
DD
DE
DF
DG
DH
225
226
227
228
229
230
231
232
233
234
235
236
237
238
239
240
241
242
243
244
245
246
247
248
249
250
251
252
253
254
255
256
Filename
DCTM_
ARP.
xls
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05
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Data
1
2
3
DI
DJ
DK
DL
DM
DN
225
226
227
228
229
230
231
232
233
234
235
236
237
238
239
240
241
242
243
244
245
246
247
248
249
250
251
252
253
254
255
256
Filename
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ARP.
xls
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Data
1
2
3
A
B
C
D
E
F
G
UID
Engine
Combustor
Eng
B/
P
Press
Rated
No
Identification
Description
Type
Ratio
Ratio
Output
kN
257
258
259
260
261
262
263
264
265
266
267
268
269
270
271
272
273
274
275
276
277
278
279
280
281
282
283
284
285
286
287
288
1PW006
JT8D­
9
series
Smoke
fix
MTF
1.04
15.88
64.5
1PW031
JT9D­
20
TF
­
20.3
205.3
1PW032
JT9D­
20J
TF
5.1
23.5
222.4
1PW033
JT9D­
59A
TF
4.9
24.5
235.8
1PW020
JT9D­
7
TF
­
21.5
202.4
1PW034
JT9D­
70A
TF
4.9
24.5
235.8
1PW021
JT9D­
7A
TF
­
20.3
205.3
1PW022
JT9D­
7F
Mod
V
TF
5.1
22.8
213.5
1PW023
JT9D­
7F
Mod
VI
TF
5.1
22.8
213.5
1PW024
JT9D­
7J
TF
5.1
23.5
222.4
1PW025
JT9D­
7Q
TF
4.9
24.5
235.75
1PW026
JT9D­
7R4D,
­
7R4D1
TF
5.0
23.40
213.5
1PW027
JT9D­
7R4E,
­
7R4E1
TF
5.0
24.2
222.4
1PW028
JT9D­
7R4E4,
­
E1(
H)
TF
5.0
24.2
222.41
1PW029
JT9D­
7R4G2
TF
4.8
26.3
243.5
1PW030
JT9D­
7R4H1
TF
4.8
26.7
249.1
1PW039
PW2037
TF
6.04
26.9
167.25
4PW072
PW2037
TF
5.71
26.7
166.35
1PW040
PW2040
TF
­
27.94
181.76
4PW073
PW2040
TF
5.54
29.4
182.02
7PW077
PW306A
Annular
TF
4.5
20
26.87
7PW078
PW306B
Annular
TF
4.5
20
26.91
7PW079
PW308A
Annular
TF
4.1
20.4
30.71
7PW080
PW308C
Annular
TF
4.1
20.7
31.15
1PW042
PW4056
Reduced
emissions
TF
4.7
29.3
249.1
1PW041
PW4056
TF
4.7
29.3
252.4
1PW043
PW4060
Reduced
emissions
TF
4.5
32.4
266.9
2PW060
PW4074
TF
6.8
32.2
333.2
3PW063
PW4074D
TF
6.7
31.76
333.2
2PW061
PW4077
TF
6.7
33.2
343.0
3PW064
PW4077D
TF
6.6
32.83
343.0
2PW062
PW4084
TF
6.4
36.2
369.6
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Data
1
2
3
H
I
J
K
L
M
N
O
P
Q
R
S
T
U
UID
Data
Superseded
Data
No
PR
C
R
superseded
by
NME
DTEPS
Other
Corr
as
Out
of
Date
Out
of
Date
UID
No
Annex
16
Production
Service
­­­­­­­­
Data
Status­­­­­­­­
­­­­­­­­­­
Current
Engine
Status
­­­­­­­­­­

­­­­­­
Test
Engine
Status­­­­­­

257
258
259
260
261
262
263
264
265
266
267
268
269
270
271
272
273
274
275
276
277
278
279
280
281
282
283
284
285
286
287
288
1PW006
x
­
­
­
­
x
­
­
x
x
­
­
­

1PW031
x
­
­
­
­
­
­
x
x
x
­
­
­

1PW032
x
­
­
­
­
­
x
­
x
x
­
­
­

1PW033
x
­
­
­
­
x
­
­
x
x
­
­
­

1PW020
x
­
­
­
­
­
­
x
x
x
­
­
­

1PW034
x
­
­
­
­
x
­
­
x
x
­
­
­

1PW021
x
­
­
­
­
­
­
x
x
x
­
­
­

1PW022
x
­
­
­
­
x
­
­
x
x
­
­
­

1PW023
x
­
­
­
­
­
x
­
x
x
­
­
­

1PW024
x
­
­
­
­
­
x
­
x
x
­
­
­

1PW025
x
­
­
­
­
x
­
­
x
x
­
­
­

1PW026
­
x
­
­
­
­
x
­
x
x
­
­
­

1PW027
­
x
­
­
­
­
x
­
x
x
­
­
­

1PW028
­
x
­
­
­
­
x
­
x
x
­
­
­

1PW029
­
x
­
­
­
­
x
­
x
x
­
­
­

1PW030
­
x
­
­
­
­
x
­
x
x
­
­
­

1PW039
­
x
­
x
4PW072
x
­
­
x
x
­
­
­

4PW072
­
­
x
­
­
x
­
­
x
­
­
­
­

1PW040
­
x
­
x
4PW073
x
­
­
x
x
­
­
­

4PW073
­
­
x
­
­
x
­
­
x
­
­
­
­

7PW077
­
x
­
­
­
­
x
­
x
­
­
­
­

7PW078
­
x
­
­
­
­
x
­
x
­
­
­
­

7PW079
­
x
­
­
­
­
x
­
x
­
­
­
­

7PW080
­
x
­
­
­
­
x
­
x
­
­
­
­

1PW042
­
x
­
­
­
x
­
­
x
x
­
­
­

1PW041
­
x
­
­
­
x
­
­
x
x
­
­
­

1PW043
­
x
­
­
­
x
­
­
x
x
­
­
­

2PW060
­
x
­
­
­
­
x
­
x
­
­
­
­

3PW063
­
x
­
­
­
x
­
­
x
x
­
­
­

2PW061
­
x
­
­
­
­
x
­
x
­
­
­
­

3PW064
­
x
­
­
­
x
­
­
x
­
­
­
­

2PW062
­
x
­
­
­
­
x
­
x
­
­
­
­

Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
V
W
X
Y
Z
AA
AB
AC
AD
AE
AF
AG
AH
UID
Characteristic
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
%
of
Total
mass
Reg
limit
(
g)

­­­­­­­­­­­­­­­­
EI
HC­­­­­­­­­­­­­­
­­­
Number
­­­
­­­­­­­­­­­­­­­
Dp/
Foo
(
HC)­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­
­­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­­­­­

257
258
259
260
261
262
263
264
265
266
267
268
269
270
271
272
273
274
275
276
277
278
279
280
281
282
283
284
285
286
287
288
1PW006
0.47
0.47
1.73
10.00
14
13
35.0
8.4
­
37.6
191.7
2256
1PW031
0.1
0.1
1.3
36.1
10
10
59
­
­
64.0
326.6
12108
1PW032
0
0
0.5
24.5
1
1
42.0
­
­
64.7
330.1
9178
1PW033
0.2
0.2
0.3
12.0
2
2
20.0
2.4
­
26.0
132.8
4559
1PW020
0.1
0.1
1.3
36.5
10
10
60.0
12.2
37.7­
69.3
65.1
332.1
12179
1PW034
0.2
0.2
0.3
12.0
2
2
20.0
2.4
­
26.0
132.8
4559
1PW021
0.1
0.1
1.3
36.1
10
10
59
­
­
64.0
326.6
12108
1PW022
0.3
0.3
0.5
26.0
7
7
43.6
5.9
­
48.1
245.4
9055
1PW023
0
0
0.6
25.9
1
1
45.5
­
­
70.1
357.7
9464
1PW024
0
0
0.5
24.5
1
1
42.0
­
­
64.7
330.1
9178
1PW025
0.2
0.2
0.3
12.0
2
2
20.0
2.4
­
26.0
132.8
4559
1PW026
0.15
0.12
0.13
1.25
7
6
2.2
­
­
2.4
12.5
464
1PW027
0.16
0.13
0.13
1.11
7
6
2.1
­
­
2.3
11.9
447
1PW028
0.15
0.13
0.22
3.35
6
5
5.7
­
­
6.4
32.7
1231
1PW029
0.15
0.14
0.18
1.55
6
5
2.6
­
­
2.9
14.9
620
1PW030
0.15
0.14
0.18
1.48
6
5
2.7
­
­
3.0
15.5
651
1PW039
0.05
0.06
0.21
2.26
3
1
3.16
­
­
4.9
24.8
530
4PW072
0.02
0.02
0.11
1.92
4
2
2.8
­
­
3.6
18.4
472
1PW040
0.026
0.035
0.18
2.25
3
1
3.3
­
­
5.1
25.9
574
4PW073
0.01
0.02
0.10
1.65
4
2
2.3
­
­
3.0
15.3
426
7PW077
0
0
0.00
4.36
3
3
10.6
­
6.3
­
13.7
12.4
63.3
287
7PW078
0
0
0.00
4.36
3
3
10.6
­
6.3
­
13.7
12.4
63.3
287
7PW079
0
0
0.02
6.62
3
3
14.98
­
14.4
­
15.88
17.5
89.3
460
7PW080
0.09
0.1
0.14
5.94
3
3
13.63
­
12.5
­
15.2
15.9
81.1
425
1PW042
0.06
0.01
0.13
1.92
3
1
2.6
­
­
4.0
20.4
652
1PW041
0.11
0.17
0.25
0.66
3
1
1.2
­
­
1.8
9.4
288
1PW043
0.10
0.03
0.14
1.66
3
1
2.2
­
­
3.4
17.3
595
2PW060
0.1
0.1
0.2
3.2
3
1
3.7
­
­
5.7
29.1
1220
3PW063
0.03
0.05
0.08
5.07
3
1
5.76
­
­
8.9
45.4
1926
2PW061
0.1
0.1
0.2
3.0
3
1
3.4
­
­
5.2
26.5
1170
3PW064
0.03
0.04
0.07
4.66
3
1
5.26
­
­
8.1
41.3
1805
2PW062
0.1
0.1
0.2
2.7
3
1
2.9
­
­
4.5
23.0
1111
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
AI
AJ
AK
AL
AM
AN
AO
AP
AQ
AR
AS
AT
AU
UID
Characteristic
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
%
of
Total
mass
Reg
limit
(
g)

­­­­­­­­­­­­­­­­­
EI
CO­­­­­­­­­­­­­­­­­
­­­­­­
Number­­­­­
­­­­­­­­­­­­­­­
Dp/
Foo
(
CO)­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­­­

257
258
259
260
261
262
263
264
265
266
267
268
269
270
271
272
273
274
275
276
277
278
279
280
281
282
283
284
285
286
287
288
1PW006
1.24
1.66
9.43
34.5
14
13
124.3
11.2
­
129.0
109.3
8018
1PW031
0
0
7.6
83.6
10
10
139.6
­
­
145.6
123.4
28647
1PW032
0.9
0.9
5.5
66.7
1
1
118.9
­
­
145.9
123.6
25974
1PW033
0.2
0.2
1.7
53.0
­
­
87.7
5.9
­
107.6
91.2
19946
1PW020
0
0
7.8
84.1
10
10
141.8
22.3
100.6­
170.6
147.9
125.3
28691
1PW034
0.2
0.2
1.7
53.0
­
­
87.7
5.9
­
107.6
91.2
19946
1PW021
0
0
7.6
83.6
10
10
139.6
­
­
145.6
123.4
28647
1PW022
0.4
0.4
2.9
54.0
7
7
91.4
5.9
­
96.1
81.5
19012
1PW023
0.9
0.9
5.8
68.6
1
1
125.1
­
­
153.6
130.2
25989
1PW024
0.9
0.9
5.5
66.7
1
1
118.9
­
­
145.9
123.6
25974
1PW025
0.2
0.2
1.7
53.0
­
­
87.7
5.9
­
107.6
91.2
19946
1PW026
0.51
0.48
1.36
8.84
7
6
15.3
­
­
16.2
13.7
3231
1PW027
0.57
0.53
1.23
8.27
7
6
14.9
­
­
15.7
13.3
3215
1PW028
0.67
0.67
1.46
16.0
6
5
27.4
­
­
29.1
24.7
5952
1PW029
0.74
0.63
1.40
11.82
6
5
19.5
­
­
20.7
17.6
4582
1PW030
0.74
0.63
1.39
11.63
6
5
20.4
­
­
21.7
18.4
4938
1PW039
0.40
0.41
2.30
23.10
3
1
32.0
­
­
39.3
33.3
5396
4PW072
0.33
0.34
1.95
22.36
4
2
33.6
­
­
38.3
32.5
5597
1PW040
0.4
0.4
2.0
25.1
3
1
35.2
­
­
43.2
36.6
6412
4PW073
0.32
0.41
1.42
19.95
4
2
28.6
­
­
32.6
27.6
5219
7PW077
2.27
2.51
7.11
36.35
3
3
99.4
­
87.0
­
120.3
107.5
91.1
2677
7PW078
2.27
2.51
7.11
36.35
3
3
99.4
­
87.0
­
120.3
107.5
91.1
2677
7PW079
0.83
1.06
4.08
38.21
3
3
92.08
­
87.17
­
98.01
99.6
84.4
2828
7PW080
0.81
0.97
5.23
42.3
3
3
101.54
­
99.0
­
105.9
109.8
93.1
3163
1PW042
0.44
0.57
2.00
21.86
3
1
30.5
­
­
37.4
31.7
7597
1PW041
0.08
0.14
0.90
11.60
3
1
14.2
­
­
17.4
14.8
3587
1PW043
0.37
0.51
1.78
20.32
3
1
27.1
­
­
33.3
28.2
7234
2PW060
0.1
0.1
0.4
21.0
3
1
22.9
­
­
28.1
23.8
7589
3PW063
0.23
0.25
0.64
34.34
3
1
39.05
­
­
47.9
40.6
13036
2PW061
0.1
0.1
0.4
20.2
3
1
21.7
­
­
26.6
22.5
7434
3PW064
0.22
0.25
0.60
32.62
3
1
36.83
­
­
45.2
38.3
12648
2PW062
0.1
0.1
0.4
18.73
3
1
19.50
­
­
23.0
19.5
7205
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
AV
AW
AX
AY
AZ
BA
BB
BC
BD
BE
BF
BG
BH
BI
BJ
UID
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
Original
CAEP
2
CAEP
4
Total
mass
(
g)

­­­­
Number­­­­­

­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­
EI
NOx­­­­­­­­­­­­­­
­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­
Dp/
Foo
(
NOx)­­­­­­­­­­­­­­
Characteristic
as
%
of
standards
257
258
259
260
261
262
263
264
265
266
267
268
269
270
271
272
273
274
275
276
277
278
279
280
281
282
283
284
285
286
287
288
1PW006
17.92
14.21
5.64
2.90
14
14
52.3
5.7
­
53.7
74.8
93.5
108.3
3370
1PW031
38.7
28.5
7.6
3.1
10
10
59.9
­
­
61.8
76.7
95.8
120.0
12291
1PW032
44.9
34.9
9.4
3.3
1
1
68.7
­
­
79.6
91.5
114.4
140.6
15885
1PW033
31.6
25.6
7.8
3.0
­
­
54.4
3.0
­
63.1
70.9
88.6
108.3
12381
1PW020
37.9
27.7
7.6
3.1
10
10
58.8
6.9
46.6­
66.1
60.7
73.1
91.3
113.6
11892
1PW034
31.6
25.6
7.8
3.0
­
­
54.4
3.0
­
63.1
70.9
88.6
108.3
12381
1PW021
38.7
28.5
7.6
3.1
10
10
59.9
­
­
61.8
76.7
95.8
120.0
12291
1PW022
46.0
34.4
7.8
3.1
7
7
69.4
4.0
­
72.0
84.2
105.2
129.8
14424
1PW023
41.7
31.5
9.1
3.2
1
1
63.1
­
­
73.1
85.4
106.7
131.8
13703
1PW024
44.9
34.9
9.4
3.3
1
1
68.7
­
­
79.6
91.5
114.4
140.6
15885
1PW025
31.6
25.6
7.8
3.0
­
­
54.4
3.0
­
63.1
70.9
88.6
108.3
12381
1PW026
38.5
30.0
9.8
4.1
6
5
61.9
­
­
64.7
74.5
93.2
114.6
13067
1PW027
41.6
34.2
10.4
4.1
6
5
67.3
­
­
70.3
79.6
99.5
121.9
14527
1PW028
36.9
29.7
8.5
3.5
6
5
60.3
­
­
63.0
71.3
89.1
109.2
13117
1PW029
41.3
29.5
8.8
3.8
6
5
60.5
­
­
63.2
68.3
85.4
103.5
14253
1PW030
45.2
30.0
8.9
3.8
6
5
65.2
­
­
68.2
73.0
91.2
110.4
15683
1PW039
31.1
24.8
10.3
4.4
3
1
48.1
­
­
55.8
59.4
74.3
89.9
8107
4PW072
29.41
23.96
9.77
4.1
4
2
48.8
­
­
53.7
57.5
71.9
87.0
8120
1PW040
34.3
27.3
10.6
4.2
3
1
55.1
­
­
63.9
66.6
83.3
100.3
10025
4PW073
35.04
26.62
10.49
4.37
4
2
54.9
­
­
60.4
61.1
76.4
91.5
9989
7PW077
20.08
19.26
11.87
4.26
3
3
55.6
­
52.7
­
58.0
58.9
73.6
92.0
92.1
1497
7PW078
20.08
19.26
11.87
4.26
3
3
55.6
­
52.7
­
58.0
58.9
73.6
92.0
92.1
1497
7PW079
16.74
14.06
8.03
3.65
3
3
42.33
­
41.21
­
42.94
44.8
55.4
69.3
70.2
1300
7PW080
18.45
15.99
7.83
3.63
3
3
45.38
­
45.0
­
45.92
48.1
59.1
73.9
74.9
1414
1PW042
28.1
22.9
11.6
4.8
3
1
48.1
­
­
55.8
56.5
70.7
84.6
11987
1PW041
32.5
24.6
11.6
5.0
3
1
51.7
­
­
59.9
60.8
76.0
91.0
13043
1PW043
32.8
24.7
12.0
4.9
3
1
52.7
­
­
61.1
58.3
72.9
85.1
14097
2PW060
38.1
31.5
11.0
4.2
3
1
54.2
­
­
62.8
60.2
75.2
88.0
18078
3PW063
42.35
34.48
11.88
3.81
3
1
59.93
­
­
69.5
67.1
83.9
98.6
19971
2PW061
39.8
32.5
11.3
4.2
3
1
56.3
­
­
65.3
61.4
76.7
89.0
19299
3PW064
44.74
35.82
12.10
3.83
3
1
62.76
­
­
72.8
68.9
86.1
100.2
21528
2PW062
45.0
35.5
12.0
4.4
3
1
62.8
­
­
72.8
64.8
81.0
91.7
23229
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
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aviation_
emissions_
databank
Data
1
2
3
BK
BL
BM
BN
BO
BP
BQ
BR
BS
BT
BU
BV
UID
Characteristic
No
T/
O
C/
O
App
Idle
Test
Eng
Max
Sigma
Range
Characteristic
%
of
Reg
limit
­­­­­­­­­­­­­­
Smoke
Number­­­­­­­­­­­­­

­­­­­­­­­­­­­
Smoke
Number­­­­­­­­­­­­­
­­­­
Number­­­­

257
258
259
260
261
262
263
264
265
266
267
268
269
270
271
272
273
274
275
276
277
278
279
280
281
282
283
284
285
286
287
288
1PW006
­
­
­
­
14
14
23
2
­
24.0
90.0
1PW031
12.3
9.5
2.5
0.7
10
10
12.3
­
­
14.5
74.4
1PW032
­
­
­
­
­
­
16.0
­
­
20.8
109.4
1PW033
­
­
­
­
­
­
8
1
­
10.3
55.0
1PW020
11.9
9.0
2.5
0.7
10
10
11.9
5.5
1.7­
21.4
14.0
71.7
1PW034
­
­
­
­
­
­
8
1
­
10.3
55.0
1PW021
12.3
9.5
2.5
0.7
10
10
12.3
­
­
14.5
74.4
1PW022
­
­
­
­
7
7
4
1
­
4.3
22.1
1PW023
16.0
­
­
­
­
­
16.0
­
­
20.8
108.2
1PW024
­
­
­
­
­
­
16.0
­
­
20.8
109.4
1PW025
­
­
­
­
­
­
8
1
­
10.3
55.0
1PW026
4.6
­
­
­
5
4
4.6
­
­
5.0
26.0
1PW027
5.0
­
­
­
5
4
5.0
­
­
5.4
28.5
1PW028
4.3
­
­
­
3
3
4.3
­
­
4.7
24.9
1PW029
6.8
­
­
­
3
3
6.8
­
­
7.5
40.3
1PW030
7.6
­
­
­
3
3
7.6
­
­
8.4
45.4
1PW039
­
­
­
­
3
1
11.4
­
­
14.7
71.4
4PW072
­
­
­
­
4
2
10.5
­
­
12.3
59.7
1PW040
­
­
­
­
3
1
11.8
­
­
15.2
75.6
4PW073
­
­
­
­
4
2
10.7
­
­
12.5
62.2
7PW077
­
­
­
­
3
3
3.9
­
3.0
­
5.1
4.3
12.7
7PW078
­
­
­
­
3
3
3.9
­
3.0
­
5.1
4.3
12.7
7PW079
­
­
­
­
3
3
15.1
­
15.0
­
15.3
17.1
52.3
7PW080
­
­
­
­
3
3
7.6
­
5.3
­
9.4
8.3
25.5
1PW042
7.8
­
­
­
3
1
7.8
­
­
10.0
54.5
1PW041
14.3
­
­
­
3
1
14.3
­
­
18.4
100.2
1PW043
8.3
­
­
­
3
1
8.3
­
­
10.7
59.1
2PW060
6.4
­
­
­
3
1
6.4
­
­
8.2
48.2
3PW063
­
­
­
­
3
1
3.38
­
­
4.4
25.9
2PW061
7.4
­
­
­
3
1
7.4
­
­
9.5
56.3
3PW064
­
­
­
­
3
1
3.76
­
­
4.8
28.4
2PW062
10.5
­
­
­
3
1
10.5
­
­
13.5
81.6
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
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aviation_
emissions_
databank
Data
1
2
3
BW
BX
BY
BZ
CA
CB
CC
CD
CE
UID
Fuel
per
No
Spec
H/
C
Arom
T/
O
C/
O
App
Idle
LTO
cycle
Ratio
%
(
kg)

­­­­­­­­­­­­­­­­­
Fuel
Flow­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­(
kg/
sec)­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­­­­­
Fuel­­­­­­­­­­­­­­­­­­­­­­­

257
258
259
260
261
262
263
264
265
266
267
268
269
270
271
272
273
274
275
276
277
278
279
280
281
282
283
284
285
286
287
288
1PW006
Jet
A
1.89
­
1.040
0.846
0.298
0.132
433
1PW031
DERD2494
­
­
2.099
1.789
0.619
0.211
802
1PW032
Jet
A
­
­
2.315
1.902
0.679
0.238
883
1PW033
Jet
A
1.89
­
2.4419
1.9996
0.6804
0.2370
900
1PW020
DERD2494
­
­
2.083
1.764
0.609
0.210
794
1PW034
Jet
A
1.89
­
2.4419
1.9996
0.6804
0.2370
900
1PW021
DERD2494
­
­
2.099
1.789
0.619
0.211
802
1PW022
Jet
A
1.89
­
2.1672
1.7640
0.6237
0.2190
815
1PW023
Jet
A
­
­
2.161
1.779
0.624
0.232
837
1PW024
Jet
A
­
­
2.315
1.902
0.679
0.238
883
1PW025
Jet
A
1.89
­
2.4419
1.9996
0.6804
0.2370
900
1PW026
Jet
A
­
­
2.055
1.678
0.7593
0.2054
810
1PW027
Jet
A
­
­
2.118
1.724
0.6529
0.2210
818
1PW028
Jet
A
­
­
2.218
1.829
0.6400
0.2205
832
1PW029
Jet
A
­
­
2.429
1.880
0.6590
0.2239
858
1PW030
Jet
A
­
­
2.512
1.999
0.7227
0.2454
926
1PW039
Jet
A
­
­
1.538
1.266
0.399
0.141
547
4PW072
Jet
A
­
­
1.571
1.307
0.458
0.152
586
1PW040
Jet
A
­
­
1.761
1.448
0.493
0.155
625
4PW073
Jet
A
­
­
1.752
1.445
0.496
0.159
631
7PW077
Jet
A­
1
1.85
­
1.87
20.0
­
22.5
0.3171
0.2641
0.0974
0.0422
137
7PW078
Jet
A­
1
1.85
­
1.87
20.0
­
22.5
0.3171
0.2641
0.0974
0.0422
137
7PW079
Jet
A­
1
1.85
­
1.87
19.5
­
21.5
0.3604
0.2991
0.1235
0.0445
154
7PW080
Jet
A­
1
1.85
­
1.86
19.8
­
21.4
0.3669
0.3047
0.1237
0.0448
155
1PW042
Jet
A
1.88
19.7
2.342
1.93
0.658
0.208
836
1PW041
Jet
A
1.87
19.7
2.449
1.981
0.647
0.188
813
1PW043
Jet
A
1.88
19.7
2.647
2.085
0.703
0.213
887
2PW060
Jet
A
1.92
20.3
2.899
2.368
0.795
0.228
981
3PW063
Jet
A
­
­
2.949
2.416
0.81
0.239
1010
2PW061
Jet
A
1.92
20.3
3.019
2.452
0.816
0.232
1008
3PW064
Jet
A
­
­
3.082
2.507
0.835
0.244
1041
2PW062
Jet
A
1.92
20.3
3.411
2.689
0.875
0.242
1086
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
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aviation_
emissions_
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Data
1
2
3
CF
CG
CH
CI
CJ
CK
CL
CM
UID
No
Baro
Temp
Humidity
kW
@
Power
%
CF
@
Power
kPa
K
kg/
kg
­­­­­­­­­­­­­­­­­­­
Ambient­­­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­
Loads­­­­­­­­­­­­­­­­­­­

Power
Extraction
­­­
Stage
Bleed­­­

257
258
259
260
261
262
263
264
265
266
267
268
269
270
271
272
273
274
275
276
277
278
279
280
281
282
283
284
285
286
287
288
1PW006
0
­
0
­
100­
102
262­
300
0.0005­
0.0123
1PW031
0
­
0
­
97.9­
101.7
276
­
300
0.0030­
0.0149
1PW032
0
­
0
­
­
­
­

1PW033
0
­
0
­
97­
100
280
­
285
0.0029­
0.0050
1PW020
0
­
0
­
97.9­
101.7
276
­
300
0.0030­
0.0149
1PW034
0
­
0
­
97­
100
280
­
285
0.0029­
0.0050
1PW021
0
­
0
­
97.9­
101.7
276
­
300
0.0030­
0.0149
1PW022
0
­
0
­
99­
103
266
­
290
0.0007­
0.0068
1PW023
0
­
0
­
­
­
­

1PW024
0
­
0
­
­
­
­

1PW025
0
­
0
­
97­
100
280
­
285
0.0029­
0.0050
1PW026
0
­
0
­
­
276
­
304
­

1PW027
0
­
0
­
­
276
­
304
­

1PW028
0
­
0
­
­
271
­
299
­

1PW029
0
­
0
­
­
271
­
299
­

1PW030
0
­
0
­
­
271
­
299
­

1PW039
0
­
0
­
100.94
298
­

4PW072
0
­
0
­
100.61
­
100.94
283.4
­
298.2
.007
­
.008
1PW040
0
­
0
­
100.94
298
­

4PW073
0
­
0
­
100.61
­
100.94
283.4
­
298.2
.007
­
.008
7PW077
0
­
0
­
98.39
­
99.49
284
­
300
0.0054
­
0.0144
7PW078
0
­
0
­
98.39
­
99.49
284
­
300
0.0054
­
0.0144
7PW079
0
­
0
­
99.42
­
103.00
280
­
296
0.0028
­
0.0090
7PW080
0
­
0
­
98.94
­
100.73
296
­
301
0.0088
­
0.0122
1PW042
0
­
0
­
100.2
299
0.010
1PW041
0
­
0
­
101.63
290
0.00053
1PW043
0
­
0
­
100.2
299
0.010
2PW060
0
­
0
­
101.3
288
0.0063
3PW063
0
­
0
­
101.06­
101.56
292.8­
302.6
.0097­.
0112
2PW061
0
­
0
­
101.3
288
0.0063
3PW064
0
­
0
­
101.06­
101.56
292.8­
302.6
.0097­.
0112
2PW062
0
­
0
­
101.3
288
0.0063
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
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version
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aviation_
emissions_
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Data
1
2
3
CN
CO
CP
CQ
CR
CS
UID
­­­
Test
Dates­­­

No
Manufacturer
Test
Organisation
Test
Location
From
To
257
258
259
260
261
262
263
264
265
266
267
268
269
270
271
272
273
274
275
276
277
278
279
280
281
282
283
284
285
286
287
288
1PW006
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
Apr­
76
Mar­
77
1PW031
Pratt
&
Whitney
NGTE,
Pyestock,
UK
British
Airways
Engine
Overhaul
Ltd,
Wales
Mar­
76
Jul­
77
1PW032
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
16­
Sep­
80
­

1PW033
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
Apr­
76
Apr­
76
1PW020
Pratt
&
Whitney
NGTE,
Pyestock,
UK
British
Airways
Engine
Overhaul
Ltd,
Wales
Mar­
76
Jul­
77
1PW034
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
Apr­
76
Apr­
76
1PW021
Pratt
&
Whitney
NGTE,
Pyestock,
UK
British
Airways
Engine
Overhaul
Ltd,
Wales
Mar­
76
Jul­
77
1PW022
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
Nov­
75
Dec­
75
1PW023
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
16­
Sep­
80
­

1PW024
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
16­
Sep­
80
­

1PW025
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
Apr­
76
Apr­
76
1PW026
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
6­
Mar­
80
3­
Nov­
81
1PW027
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
6­
Mar­
80
3­
Nov­
81
1PW028
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
26­
Oct­
81
10­
Apr­
83
1PW029
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
26­
Oct­
81
10­
Sep­
83
1PW030
Pratt
&
Whitney
P&
WA
E
Hartford,
CT,
USA
26­
Oct­
81
10­
Sep­
83
1PW039
Pratt
&
Whitney
P&
WA
X­
8
Stand,
PWA,
East
Hartford,
CT
8­
Aug­
83
10­
Aug­
83
4PW072
Pratt
&
Whitney
P&
WA
East
Hartford,
CT
8­
Aug­
83
20­
Nov­
98
1PW040
Pratt
&
Whitney
­
­
8­
Aug­
83
10­
Aug­
83
4PW073
Pratt
&
Whitney
P&
WA
East
Hartford,
CT
8­
Aug­
83
20­
Nov­
98
7PW077
Pratt
&
Whitney
Canada
Inc.
PW306
Development
Engineering
Mississauga,
Ontario,
Canada
8­
May­
00
20­
Jul­
00
7PW078
Pratt
&
Whitnet
Canada
Inc.
PE306
Development
Engineering
Mississauga,
Ontario,
Canada
8­
May­
00
20­
Jul­
00
7PW079
Pratt
&
Whitney
Canada
Inc
PW308
Development
Engineering
Mississauga,
Ontario,
Canada
15­
Apr­
00
5­
Sep­
00
7PW080
Pratt
&
Whitney
Canada
Inc.
PW308
Development
Engineering
Mississauga,
Ontario,
Canada
7­
Aug­
01
31­
Aug­
01
1PW042
Pratt
&
Whitney
­
­
17­
Aug­
87
23­
Aug­
87
1PW041
Pratt
&
Whitney
Pratt
&
Whitney
P7
Stand,
P&
W,
Middletown,
CT
14­
May­
86
14­
May­
86
1PW043
Pratt
&
Whitney
­
­
17­
Aug­
87
23­
Aug­
87
2PW060
Pratt
and
Whitney
Pratt
and
Whitney
East
Hartford,
Ct,
USA
26­
Apr­
94
2­
May­
94
3PW063
Pratt
&
Whitney
Pratt
&
Whitney
East
Hartford,
Conn,
USA
15­
Jun­
96
16­
Jun­
96
2PW061
Pratt
and
Whitney
Pratt
and
Whitney
East
Hartford,
Ct,
USA
26­
Apr­
94
2­
May­
94
3PW064
Pratt
&
Whitney
Pratt
&
Whitney
East
Hartford,
Conn,
USA
15­
Jun­
96
16­
Jun­
96
2PW062
Pratt
and
Whitney
Pratt
and
Whitney
East
Hartford,
Ct,
USA
26­
Apr­
94
2­
May­
94
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
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version
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aviation_
emissions_
databank
Data
1
2
3
CT
CU
UID
No
Remarks
257
258
259
260
261
262
263
264
265
266
267
268
269
270
271
272
273
274
275
276
277
278
279
280
281
282
283
284
285
286
287
288
1PW006
1.
Smoke
fix
combustor
in
production
prior
to
1/
1/
84.
2.
Applicable
to
JT8D­
9,
­
9A.

1PW031
1.
Emissions
estimated
from
JT9D­
7
engines
using
JT9D­
7A
performance
data.
2.
Tests
performed
on
in­
service
engine(
s),
after
overhaul.

1PW032
­

1PW033
­

1PW020
Tests
performed
on
in­
service
engine(
s),
after
overhaul.

1PW034
­

1PW021
1.
Emissions
estimated
from
JT9D­
7
engines
using
JT9D­
7A
performance
data.
2.
Tests
performed
on
in­
service
engine(
s),
after
overhaul.

1PW022
Mod
V
combustor
1PW023
Mod
VI
combustor
1PW024
­

1PW025
­

1PW026
­

1PW027
­

1PW028
­

1PW029
­

1PW030
­

1PW039
­

4PW072
Revision
to
add
second
engine
test.

1PW040
­

4PW073
Revision
to
add
second
engine
test.

7PW077
1,
P&
WC
EC
C2264A
2,
Engines
E9541/
02,
E9402/
37,
E9403/
74
7PW078
1,
P&
WC
EC
C2264A
2,
Engines
E9541/
02,
E9402/
37,
E9403/
74
7PW079
1,
P&
WC
ER
3967
2,
Engines
E9608/
01,
E9606/
04,
E9609/
01
7PW080
1,
P&
WC
ER
5080
2,
Engines
E9633/
01,
E9631/
07,
CF0001/
03
1PW042
Data
from
X698­
5
with
reduced
smoke
combustor.

1PW041
­

1PW043
Data
from
X698­
5
with
reduced
smoke
combustor.

2PW060
Data
from
X832­
4
3PW063
Data
from
Report
PWA­
6678
2PW061
Data
from
X832­
4
3PW064
Data
from
Report
PWA­
6678
2PW062
Data
from
X832­
4
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
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version
www.
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com/
aviation_
emissions_
databank
Data
1
2
3
CV
CW
CX
CY
CZ
DA
DB
DC
DD
DE
DF
DG
DH
257
258
259
260
261
262
263
264
265
266
267
268
269
270
271
272
273
274
275
276
277
278
279
280
281
282
283
284
285
286
287
288
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
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version
www.
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com/
aviation_
emissions_
databank
Data
1
2
3
DI
DJ
DK
DL
DM
DN
257
258
259
260
261
262
263
264
265
266
267
268
269
270
271
272
273
274
275
276
277
278
279
280
281
282
283
284
285
286
287
288
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
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website
for
latest
version
www.
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aviation_
emissions_
databank
Data
1
2
3
A
B
C
D
E
F
G
UID
Engine
Combustor
Eng
B/
P
Press
Rated
No
Identification
Description
Type
Ratio
Ratio
Output
kN
289
290
291
292
293
294
295
296
297
298
299
300
301
302
303
304
305
306
307
308
309
310
311
312
313
314
315
316
317
318
319
320
3PW065
PW4084D
TF
6.3
36.36
369.6
3PW066
PW4090
TF
6.1
39.16
395.0
5PW076
PW4098
TF
­
41.37
424.1
1PW045
PW4152
Reduced
smoke
TF
4.9
26.9
231.27
1PW044
PW4152
TF
4.9
26.9
231.3
1PW047
PW4156
Reduced
smoke
TF
4.7
29.3
249.1
1PW046
PW4156
TF
4.7
29.3
252.4
1PW048
PW4158
Reduced
smoke
TF
4.6
30.7
258.0
1PW049
PW4164
Floatwall
TF
5.2
31.24
284.68
1PW050
PW4168
Floatwall
TF
5.1
33.10
302.48
5PW075
PW4168
Talon
II
TF
5.1
31.84
302.5
4PW067
PW4168A
Floatwall
TF
5.1
33.1
302.48
1PW051
PW4256
TF
4.7
29.3
252.4
1PW052
PW4460
Reduced
smoke
TF
4.5
32.4
266.9
1PW053
PW4x50
Phase
3
TF
5.0
25.39
222.4
1PW054
PW4x52
Phase
3
TF
5.0
26.32
231.3
1PW055
PW4x56
Phase
3
TF
4.8
28.37
249.1
1PW056
PW4x58
Phase
3
TF
4.8
29.49
258.0
5PW074
PW4X58
Talon
II
TF
4.8
28.41
258.0
1PW057
PW4x60
Phase
3
TF
4.7
30.68
266.9
1PW059
PW4x62
Phase
3
TF
4.6
31.91
275.8
1PW058
PW4x62
Reduced
smoke
TF
4.4
33.4
275.8
Rolls­
Royce
Ltd
1RR001
M45H­
01
TF
3.0
16.5
32.4
1RR002
RB211­
22B
Package
1
TF
4.7
25.0
182.5
1RR003
RB211­
22B
Package
1
TF
4.7
25.0
182.5
1RR004
RB211­
524B
series
Package
1
TF
4.5
28.0
218.5
1RR005
RB211­
524B
series
Phase
2
TF
4.5
28.4
218.5
1RR006
RB211­
524C2
Package
1
TF
4.5
29.1
224.8
1RR007
RB211­
524D4
Package
1
TF
4.3
29.7
231.3
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
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aviation_
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Data
1
2
3
H
I
J
K
L
M
N
O
P
Q
R
S
T
U
UID
Data
Superseded
Data
No
PR
C
R
superseded
by
NME
DTEPS
Other
Corr
as
Out
of
Date
Out
of
Date
UID
No
Annex
16
Production
Service
­­­­­­­­
Data
Status­­­­­­­­
­­­­­­­­­­
Current
Engine
Status
­­­­­­­­­­

­­­­­­
Test
Engine
Status­­­­­­

289
290
291
292
293
294
295
296
297
298
299
300
301
302
303
304
305
306
307
308
309
310
311
312
313
314
315
316
317
318
319
320
3PW065
­
x
­
­
­
x
­
­
x
­
­
­
­

3PW066
­
x
­
­
­
x
­
­
x
­
­
­
­

5PW076
­
x
­
­
­
­
x
­
x
­
­
­
­

1PW045
­
x
­
­
­
x
­
­
x
x
­
­
­

1PW044
­
x
­
­
­
x
­
­
x
x
­
­
­

1PW047
­
x
­
­
­
x
­
­
x
x
­
­
­

1PW046
­
x
­
­
­
x
­
­
x
x
­
­
­

1PW048
­
x
­
­
­
x
­
­
x
x
­
­
­

1PW049
­
x
­
­
­
­
x
­
x
­
­
­
­

1PW050
­
x
­
­
­
­
x
­
x
­
­
­
­

5PW075
­
x
­
­
­
­
x
­
x
­
­
­
­

4PW067
­
x
­
­
­
­
x
­
x
­
­
­
­

1PW051
­
x
­
­
­
x
­
­
x
x
­
­
­

1PW052
­
x
­
­
­
x
­
­
x
x
­
­
­

1PW053
­
x
­
­
­
­
x
­
x
x
­
­
­

1PW054
­
x
­
­
­
­
x
­
x
­
­
­
­

1PW055
­
x
­
­
­
­
x
­
x
­
­
­
­

1PW056
­
x
­
­
­
­
x
­
x
­
­
­
­

5PW074
­
x
­
­
­
­
x
­
x
­
­
­
­

1PW057
­
x
­
­
­
­
x
­
x
­
­
­
­

1PW059
­
x
­
­
­
­
x
­
x
­
­
­
­

1PW058
­
x
­
­
­
x
­
­
x
x
­
­
­

1RR001
x
­
­
­
­
­
x
­
x
x
­
­
­

1RR002
x
­
­
­
­
x
­
­
x
x
­
­
­

1RR003
x
­
­
­
­
x
x
x
­
­
­

1RR004
x
­
­
­
­
x
­
­
x
x
­
­
­

1RR005
­
x
­
­
­
­
x
­
x
x
­
­
­

1RR006
x
­
­
­
­
­
x
­
x
x
­
­
­

1RR007
x
­
­
­
­
­
x
­
x
x
­
­
­

Filename
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ARP.
xls
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emissions_
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Data
1
2
3
V
W
X
Y
Z
AA
AB
AC
AD
AE
AF
AG
AH
UID
Characteristic
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
%
of
Total
mass
Reg
limit
(
g)

­­­­­­­­­­­­­­­­
EI
HC­­­­­­­­­­­­­­
­­­
Number
­­­
­­­­­­­­­­­­­­­
Dp/
Foo
(
HC)­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­
­­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­­­­­

289
290
291
292
293
294
295
296
297
298
299
300
301
302
303
304
305
306
307
308
309
310
311
312
313
314
315
316
317
318
319
320
3PW065
0.03
0.03
0.06
3.29
3
1
3.66
­
­
5.6
28.6
1353
3PW066
0.03
0.03
0.06
2.30
3
1
2.52
­
­
3.9
19.9
992
5PW076
0.00
0.00
0.00
0.00
3
1
0.00
­
­
0.0
0.0
0
1PW045
0.03
0.01
0.13
2.24
3
1
3.2
­
­
4.9
25.1
734
1PW044
0.13
0.16
0.15
0.74
3
1
1.3
­
­
2.0
10.2
275
1PW047
0.06
0.01
0.13
1.92
3
1
2.6
­
­
4.0
20.4
652
1PW046
0.11
0.17
0.25
0.66
3
1
1.2
­
­
1.8
9.4
288
1PW048
0.09
0.02
0.14
1.78
3
1
2.4
­
­
3.7
18.9
623
1PW049
0.03
0.04
0.16
4.46
3
1
5.3
­
­
8.2
41.6
1505
1PW050
0.03
0.04
0.15
3.29
3
1
3.9
­
­
6.0
30.6
1179
5PW075
0.0
0.0
0.0
0.2
3
1
0.3
­
­
0.5
2.3
78
4PW067
0.03
0.04
0.15
3.29
3
1
3.9
­
­
6.0
30.6
1179
1PW051
0.11
0.17
0.25
0.66
3
1
1.2
­
­
1.8
9.4
288
1PW052
0.10
0.03
0.14
1.66
3
1
2.2
­
­
3.4
17.3
595
1PW053
0.09
0.10
0.19
6.80
3
1
9.5
­
­
14.6
74.6
2104
1PW054
0.08
0.10
0.17
6.02
3
1
8.3
­
­
12.8
65.2
1914
1PW055
0.08
0.09
0.16
4.75
3
1
6.4
­
­
9.9
50.3
1597
1PW056
0.08
0.09
0.15
4.29
3
1
5.7
­
­
8.8
44.8
1481
5PW074
0.0
0.0
0.0
1.7
3
1
2.2
­
­
3.4
17.3
562
1PW057
0.08
0.08
0.15
3.73
3
1
5.0
­
­
7.7
39.3
1324
1PW059
0.08
0.08
0.15
3.26
3
1
4.3
­
­
6.6
33.8
1192
1PW058
0.10
0.06
0.14
1.53
3
1
2.0
­
­
3.1
15.7
571
1RR001
*
0.74
7.4
59.5
5
5
162.4
87.5
81.0­
293.4
182.6
931.6
1RR002
0.36
0.39
7.73
65.37
4
3
132.8
8.23
122­
140
154.9
790.4
29381
1RR003
0.15
0.25
5.96
67.75
7
7
134.8
5.6
169.8­
204.1
148.7
758.7
24653
1RR004
0.52
0.40
4.98
50.60
4
3
106.3
6.61
97.7­
112.0
124.0
632.7
22453
1RR005
0.39
0.26
0.70
1.95
3
1
4.25
0.1
4.2­
4.4
6.5
33.4
934
1RR006
0.0
0.22
4.42
54.2
­
­
116.5
­
­
179.4
915.4
26209
1RR007
0.0
0.42
4.80
46.46
3
3
97.8
­
­
114.1
582.1
22707
Filename
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ARP.
xls
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Data
1
2
3
AI
AJ
AK
AL
AM
AN
AO
AP
AQ
AR
AS
AT
AU
UID
Characteristic
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
%
of
Total
mass
Reg
limit
(
g)

­­­­­­­­­­­­­­­­­
EI
CO­­­­­­­­­­­­­­­­­
­­­­­­
Number­­­­­
­­­­­­­­­­­­­­­
Dp/
Foo
(
CO)­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­­­

289
290
291
292
293
294
295
296
297
298
299
300
301
302
303
304
305
306
307
308
309
310
311
312
313
314
315
316
317
318
319
320
3PW065
0.18
0.24
0.48
25.74
3
1
28.60
­
­
35.1
29.7
10579
3PW066
0.19
0.23
0.44
20.63
3
1
22.38
­
­
27.5
23.3
8848
5PW076
0.160
0.210
0.700
6.480
3
1
8.35
­
­
10.2
8.6
3543
1PW045
0.5
0.62
2.29
23.67
3
1
34.8
­
­
42.7
36.2
8023
1PW044
0.12
0.17
1.09
12.76
3
1
17.0
­
­
20.9
17.7
3729
1PW047
0.44
0.57
2.00
21.86
3
1
30.5
­
­
37.4
31.7
7597
1PW046
0.08
0.14
0.90
11.60
3
1
14.2
­
­
17.4
14.8
3587
1PW048
0.40
0.54
1.88
20.99
3
1
28.7
­
­
35.2
29.9
7401
1PW049
0.69
0.79
1.86
26.67
3
1
33.0
­
­
40.5
34.3
9377
1PW050
0.72
0.74
1.75
23.51
3
1
28.9
­
­
35.5
30.1
8754
5PW075
0.1
0.2
2.4
15.9
3
1
22.3
­
­
27.4
23.2
6741
4PW067
0.72
0.74
1.75
23.51
3
1
28.9
­
­
35.5
30.1
8754
1PW051
0.08
0.14
0.90
11.60
3
1
14.2
­
­
17.4
14.8
3587
1PW052
0.37
0.51
1.78
20.32
3
1
27.1
­
­
33.3
28.2
7234
1PW053
0.53
0.62
2.33
36.91
3
1
52.2
­
­
64.1
54.3
11619
1PW054
0.52
0.60
2.15
34.54
3
1
48.2
­
­
59.2
50.1
11164
1PW055
0.48
0.56
1.89
29.96
3
1
41.0
­
­
50.3
42.6
10202
1PW056
0.44
0.53
1.82
28.08
3
1
38.0
­
­
46.6
39.5
9806
5PW074
0.2
0.3
3.8
24.3
3
1
33.9
­
­
41.6
35.3
8741
1PW057
0.40
0.52
1.74
25.83
3
1
34.7
­
­
42.6
36.1
9257
1PW059
0.38
0.51
1.68
23.96
3
1
31.9
­
­
39.2
33.2
8811
1PW058
0.35
0.49
1.69
19.51
3
1
25.6
­
­
31.4
26.6
7080
1RR001
6.2
7.9
51
178.4
5
5
526.0
99.5
374.3­
633.8
558.6
473.4
17101
1RR002
2.48
4.14
26.38
93.17
4
3
205.3
8.01
197­
212
222.0
188.2
44799
1RR003
0.78
1.68
20.65
88.99
7
7
188.5
13.1
169.8­
204.1
198.3
168.0
34445
1RR004
1.83
2.82
20.0
82.2
4
3
182.9
7.15
175.6­
189
197.8
167.6
39110
1RR005
0.70
0.33
1.56
12.39
3
1
22.9
0.68
22.3­
23.6
28.1
23.8
5018
1RR006
0.66
1.63
18.9
81.0
­
­
185.4
­
­
227.6
192.9
41768
1RR007
0.51
1.18
16.9
73.8
3
3
163.4
­
­
176.7
149.7
37907
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
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aviation_
emissions_
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Data
1
2
3
AV
AW
AX
AY
AZ
BA
BB
BC
BD
BE
BF
BG
BH
BI
BJ
UID
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
Original
CAEP
2
CAEP
4
Total
mass
(
g)

­­­­
Number­­­­­

­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­
EI
NOx­­­­­­­­­­­­­­
­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­
Dp/
Foo
(
NOx)­­­­­­­­­­­­­­
Characteristic
as
%
of
standards
289
290
291
292
293
294
295
296
297
298
299
300
301
302
303
304
305
306
307
308
309
310
311
312
313
314
315
316
317
318
319
320
3PW065
53.02
39.47
12.70
4.08
3
1
72.14
­
­
83.6
74.2
92.7
104.9
26662
3PW066
61.00
42.80
13.19
4.29
3
1
80.08
­
­
92.8
78.4
98.0
108.8
31629
5PW076
51.29
36.45
14.89
7.78
3
1
76.1
­
­
88.2
71.9
89.8
98.3
32265
1PW045
25.3
21.1
11.1
4.8
3
1
45.0
­
­
52.2
55.6
69.5
84.1
10381
1PW044
26.9
22.7
11.1
4.9
3
1
46.7
­
­
54.1
57.7
72.1
87.3
10741
1PW047
28.1
22.9
11.6
4.8
3
1
48.1
­
­
55.8
56.5
70.7
84.6
11987
1PW046
32.5
24.6
11.6
5.0
3
1
51.7
­
­
59.9
60.8
76.0
91.0
13043
1PW048
30.2
23.7
11.8
4.8
3
1
50.2
­
­
58.2
57.4
71.7
85.1
12928
1PW049
38.57
31.66
14.10
4.03
3
1
60.5
­
­
70.1
68.4
85.5
100.9
17232
1PW050
42.39
33.91
14.66
4.15
3
1
65.2
­
­
75.6
71.2
89.0
103.2
19704
5PW075
26.9
20.2
12.1
5.2
3
1
46.0
­
­
53.3
51.4
64.3
75.4
13936
4PW067
42.39
33.91
14.66
4.15
3
1
65.2
­
­
75.6
71.2
89.0
103.3
19704
1PW051
32.5
24.6
11.6
5.0
3
1
51.7
­
­
59.9
60.8
76.0
91.0
13043
1PW052
32.8
24.7
12.0
4.9
3
1
52.7
­
­
61.1
58.3
72.9
86.2
14097
1PW053
25.69
21.77
11.13
3.69
3
1
43.5
­
­
50.4
55.5
69.4
84.6
9681
1PW054
27.02
22.54
11.41
3.77
3
1
45.2
­
­
52.4
56.6
70.7
85.7
10449
1PW055
30.44
24.24
11.97
3.93
3
1
49.2
­
­
57.0
59.0
73.7
88.6
12246
1PW056
32.51
25.22
12.25
3.99
3
1
51.6
­
­
59.8
60.4
75.5
90.4
13305
5PW074
22.5
18.0
11.1
4.3
3
1
39.9
­
­
46.3
47.8
59.8
71.8
10297
1PW057
34.89
26.34
12.53
4.07
3
1
54.4
­
­
63.1
62.2
77.8
92.2
14505
1PW059
37.65
27.55
12.78
4.14
3
1
57.5
­
­
66.7
64.2
80.2
94.1
15864
1PW058
36.3
25.7
12.2
4.9
3
1
56.0
­
­
64.9
60.8
76.0
88.0
15470
1RR001
11.5
9.3
3.6
1.5
5
5
31.2
3.8
26.4­
35.9
32.6
44.7
55.8
57.0
1001
1RR002
34.32
25.63
8.05
2.70
4
3
54.3
4.4
48­
57
57.5
63.9
79.9
97.5
10142
1RR003
37.33
26.89
8.18
2.86
7
7
57.8
3.1
52.2­
60.7
60.0
66.7
83.3
101.7
10545
1RR004
47.0
33.0
9.75
3.53
4
3
73.9
6.0
64.9­
77.6
78.3
81.5
101.9
122.7
16270
1RR005
52.3
38.2
9.8
4.2
3
1
77.3
0.8
76.5­
78.1
89.6
92.6
115.7
139.0
16935
1RR006
41.9
32.3
10.4
3.37
­
­
72.9
­
­
84.5
86.1
107.6
128.9
16401
1RR007
56.9
41.0
9.65
4.11
3
3
88.6
­
­
93.8
94.4
118.0
141.0
20514
Filename
DCTM_
ARP.
xls
Printed
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5/
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05
Check
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aviation_
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Data
1
2
3
BK
BL
BM
BN
BO
BP
BQ
BR
BS
BT
BU
BV
UID
Characteristic
No
T/
O
C/
O
App
Idle
Test
Eng
Max
Sigma
Range
Characteristic
%
of
Reg
limit
­­­­­­­­­­­­­­
Smoke
Number­­­­­­­­­­­­­

­­­­­­­­­­­­­
Smoke
Number­­­­­­­­­­­­­
­­­­
Number­­­­

289
290
291
292
293
294
295
296
297
298
299
300
301
302
303
304
305
306
307
308
309
310
311
312
313
314
315
316
317
318
319
320
3PW065
­
­
­
­
3
1
5.36
­
­
6.9
41.7
3PW066
­
­
­
­
3
1
7.12
­
­
9.2
56.6
5PW076
­
­
­
­
3
1
9.3
­
­
12.0
75.3
1PW045
7.0
­
­
­
3
1
7.0
­
­
9.0
47.9
1PW044
12.7
­
­
­
3
1
12.7
­
­
16.3
86.9
1PW047
7.8
­
­
­
3
1
7.8
­
­
10.0
54.5
1PW046
14.3
­
­
­
3
1
14.3
­
­
18.4
100.2
1PW048
8.1
­
­
­
3
1
8.1
­
­
10.4
57.1
1PW049
3.3
­
­
­
3
1
3.3
­
­
4.2
23.9
1PW050
4.0
­
­
­
3
1
4.0
­
­
5.1
29.5
5PW075
­
­
­
­
3
1
12.7
­
­
16.4
93.5
4PW067
4.0
­
­
­
3
1
4.0
­
­
5.1
29.2
1PW051
14.3
­
­
­
3
1
14.3
­
­
18.4
100.2
1PW052
8.3
­
­
­
3
1
8.3
­
­
10.7
59.1
1PW053
6.8
­
­
­
3
1
6.8
­
­
8.8
46.0
1PW054
7.3
­
­
­
3
1
7.3
­
­
9.4
50.0
1PW055
8.5
­
­
­
3
1
8.5
­
­
10.9
59.4
1PW056
9.1
­
­
­
3
1
9.1
­
­
11.7
64.2
5PW074
­
­
­
­
3
1
11.6
­
­
14.9
81.6
1PW057
9.6
­
­
­
3
1
9.6
­
­
12.4
68.3
1PW059
10.1
­
­
­
3
1
10.1
­
­
13.0
72.5
1PW058
8.4
­
­
­
3
1
8.4
­
­
10.8
60.3
1RR001
46.3
38.4
10.9
2.7
5
5
46.3
3.87
42­
54.5
49.8
154.5
1RR002
14.7
12.9
8.0
3.1
1
1
14.7
­
­
18.9
94.3
1RR003
7
7
22.6
6.5
14.6­
33.4
24.0
119.7
1RR004
17.9
13.5
2.7
0.9
4
3
17.9
0.5
17.3­
18.4
19.7
103.0
1RR005
­
­
­
­
3
1
12.3
0.2
12.1­
12.6
15.8
82.9
1RR006
­
­
­
­
­
­
14.5
­
­
18.7
98.4
1RR007
­
­
­
­
3
3
12.2
­
­
13.4
71.2
Filename
DCTM_
ARP.
xls
Printed
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Data
1
2
3
BW
BX
BY
BZ
CA
CB
CC
CD
CE
UID
Fuel
per
No
Spec
H/
C
Arom
T/
O
C/
O
App
Idle
LTO
cycle
Ratio
%
(
kg)

­­­­­­­­­­­­­­­­­
Fuel
Flow­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­(
kg/
sec)­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­­­­­
Fuel­­­­­­­­­­­­­­­­­­­­­­­

289
290
291
292
293
294
295
296
297
298
299
300
301
302
303
304
305
306
307
308
309
310
311
312
313
314
315
316
317
318
319
320
3PW065
Jet
A
­
­
3.511
2.771
0.907
0.258
1133
3PW066
Jet
A
­
­
3.898
2.977
0.957
0.268
1204
5PW076
Jet
A
1.9
15.5
4.138
3.245
1.075
0.321
1361
1PW045
Jet
A
1.88
19.7
2.129
1.783
0.613
0.203
789
1PW044
Jet
A
1.87
19.7
2.177
1.785
0.593
0.177
745
1PW047
Jet
A
1.88
19.7
2.342
1.93
0.658
0.208
836
1PW046
Jet
A
1.87
19.7
2.449
1.981
0.647
0.188
813
1PW048
Jet
A
1.88
19.7
2.481
2.004
0.682
0.211
862
1PW049
Jet
A
1.89
21.85
2.626
2.179
0.754
0.210
906
1PW050
Jet
A
1.89
21.85
2.836
2.327
0.798
0.221
963
5PW075
Jet
A
1.94
15.5
2.884
2.363
0.809
0.25
1017
4PW067
Jet
A
1.89
21.85
2.836
2.327
0.798
0.221
963
1PW051
Jet
A
1.87
19.7
2.449
1.981
0.647
0.188
813
1PW052
Jet
A
1.88
19.7
2.647
2.085
0.703
0.213
887
1PW053
Jet
A
1.91
21.0
2.027
1.683
0.579
0.193
747
1PW054
Jet
A
1.91
21.0
2.127
1.757
0.600
0.198
774
1PW055
Jet
A
1.91
21.0
2.351
1.912
0.643
0.208
830
1PW056
Jet
A
1.91
21.0
2.482
1.993
0.665
0.213
859
5PW074
Jet
A
1.9
20.6
2.496
1.999
0.663
0.212
859
1PW057
Jet
A
1.91
21.0
2.623
2.075
0.686
0.218
889
1PW059
Jet
A
1.91
21.0
2.767
2.166
0.708
0.223
920
1PW058
Jet
A
1.88
19.7
2.858
2.161
0.725
0.217
918
1RR001
DERD
2494
1.94
19
0.498
0.416
0.146
0.053
194
1RR002
DERD
2494
1.94
20
1.866
1.542
0.553
0.277
847
1RR003
DERD
2494
1.877
1.546
0.566
0.225
770
1RR004
DERD
2494
1.94
20
2.383
1.939
0.693
0.272
947
1RR005
AVTUR
1.91
20
2.21
1.79
0.63
0.24
855
1RR006
AVTUR
1.91
20
2.48
2.02
0.74
0.30
1016
1RR007
AVTUR
1.91
20
2.51
2.01
0.74
0.30
1016
Filename
DCTM_
ARP.
xls
Printed
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5/
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05
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aviation_
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Data
1
2
3
CF
CG
CH
CI
CJ
CK
CL
CM
UID
No
Baro
Temp
Humidity
kW
@
Power
%
CF
@
Power
kPa
K
kg/
kg
­­­­­­­­­­­­­­­­­­­
Ambient­­­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­
Loads­­­­­­­­­­­­­­­­­­­

Power
Extraction
­­­
Stage
Bleed­­­

289
290
291
292
293
294
295
296
297
298
299
300
301
302
303
304
305
306
307
308
309
310
311
312
313
314
315
316
317
318
319
320
3PW065
0
­
0
­
101.06­
101.56
292.8­
302.6
.0097­.
0112
3PW066
0
­
0
­
101.06­
101.56
292.8­
302.6
.0097­.
0112
5PW076
0
­
0
­
101.7
­
102.5
284
­
289
.00274
­
.00608
1PW045
0
­
0
­
100.2
299
.010
1PW044
0
­
0
­
101.63
290
0.00053
1PW047
0
­
0
­
100.2
299
0.010
1PW046
0
­
0
­
101.63
290
0.00053
1PW048
0
­
0
­
100.2
299
0.010
1PW049
0
­
0
­
101.3
273.5
.0018
1PW050
0
­
0
­
101.3
273.5
.0018
5PW075
0
­
0
­
101.4
­
102.3
279
­
282
.00210
­
.00355
4PW067
0
­
0
­
101.3
273.5
0.0018
1PW051
0
­
0
­
101.63
290
0.00053
1PW052
0
­
0
­
100.2
299
0.010
1PW053
0
­
0
­
102.0
270
.0015
1PW054
0
­
0
­
102.0
270
.0015
1PW055
0
­
0
­
102.0
270
.0015
1PW056
0
­
0
­
102.0
270
.0015
5PW074
0
­
0
­
100.0
­
101.3
277
­
281
.00268
­
.00342
1PW057
0
­
0
­
102.0
270
.0015
1PW059
0
­
0
­
102.0
270
.0015
1PW058
0
­
0
­
100.2
299
0.010
1RR001
0
­
6
7%
98.6­
102.1
281
­
293
0.00456­
0.00749
1RR002
0
­
0
­
99.3­
100.3
287
­
291
0.008
1RR003
0
­
0
­
99.6­
102.2
275
­
287
.0033­.
0077
1RR004
0
­
0
­
99.3­
100.3
287
­
291
0.008
1RR005
0
­
0
­
103
283
­
286
0.005
1RR006
0
­
0
­
102
288
0.005
1RR007
0
­
0
­
101
277
0.006
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
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aviation_
emissions_
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Data
1
2
3
CN
CO
CP
CQ
CR
CS
UID
­­­
Test
Dates­­­

No
Manufacturer
Test
Organisation
Test
Location
From
To
289
290
291
292
293
294
295
296
297
298
299
300
301
302
303
304
305
306
307
308
309
310
311
312
313
314
315
316
317
318
319
320
3PW065
Pratt
&
Whitney
Pratt
&
Whitney
East
Hartford,
Conn,
USA
15­
Jun­
96
16­
Jun­
96
3PW066
Pratt
&
Whitney
Pratt
&
Whitney
East
Hartford,
Conn,
USA
15­
Jun­
96
16­
Jun­
96
5PW076
Pratt
and
Whitney
Pratt
and
Whitney
East
Hartford,
Conn.
USA
3­
Jan­
98
4­
Jan­
98
1PW045
Pratt
&
Whitney
­
­
17­
Aug­
87
23­
Aug­
87
1PW044
Pratt
&
Whitney
Pratt&
Whitney
P7
Stand,
P&
W,
Middletown,
CT
14­
May­
86
14­
May­
86
1PW047
Pratt
&
Whitney
­
­
17­
Aug­
87
23­
Aug­
87
1PW046
Pratt
&
Whitney
Pratt
&
Whitney
P7
Stand,
P&
W,
Middletown,
CT
14­
May­
86
14­
May­
86
1PW048
Pratt
&
Whitney
­
­
17­
Aug­
87
23­
Aug­
87
1PW049
Pratt
&
Whitney
Pratt
&
Whitney
East
Hartford,
CT
14­
Feb­
93
17­
Feb­
93
1PW050
Pratt
&
Whitney
Pratt
&
Whitney
East
Hartford,
CT
14­
Feb­
93
17­
Feb­
93
5PW075
Pratt
and
Whitney
Pratt
and
Whitney
East
Hartford,
Conn.
USA
10­
Apr­
00
4PW067
Pratt
&
Whitney
Pratt
&
Whitney
East
Hartford,
CT
14­
Feb­
93
17­
Feb­
93
1PW051
Pratt
&
Whitney
Pratt
&
Whitney
P7
Stand,
P&
W,
Middletown,
CT
14­
May­
86
14­
May­
86
1PW052
Pratt
&
Whitney
­
­
17­
Aug­
87
23­
Aug­
87
1PW053
Pratt
&
Whitney
Pratt
&
Whitney
Middletown,
CT
15­
Jan­
93
19­
Jan­
93
1PW054
Pratt
&
Whitney
Pratt
&
Whitney
Middletown,
CT
15­
Jan­
93
19­
Jan­
93
1PW055
Pratt
&
Whitney
Pratt
&
Whitney
Middletown,
CT
15­
Jan­
93
19­
Jan­
93
1PW056
Pratt
&
Whitney
Pratt
&
Whitney
Middletown,
CT
15­
Jan­
93
19­
Jan­
93
5PW074
Pratt
and
Whitney
Pratt
and
Whitney
East
Hartford,
Conn.
USA
3­
Nov­
99
4­
Nov­
99
1PW057
Pratt
&
Whitney
Pratt
&
Whitney
Middletown,
CT
15­
Jan­
93
19­
Jan­
93
1PW059
Pratt
&
Whitney
Pratt
&
Whitney
Middletown,
CT
15­
Jan­
93
19­
Jan­
93
1PW058
Pratt
&
Whitney
­
­
17­
Aug­
87
23­
Aug­
87
1RR001
Rolls
Royce
Ltd
Rolls
Royce
Ltd
Bristol
1971
1977
1RR002
Rolls
Royce
Ltd
Rolls
Royce
Ltd
Derby
Jun­
79
Aug­
79
1RR003
Rolls
Royce
Ltd
NGTE,
Pyestock,
UK
British
Airways
Test
Facility,
Heathrow
Mar­
79
Apr­
80
1RR004
Rolls
Royce
Ltd
Rolls
Royce
Ltd
Derby
Jun­
79
Aug­
79
1RR005
Rolls
Royce
Ltd
Rolls
Royce
Ltd
SINFIN­
Derby
Sep­
86
Sep­
86
1RR006
Rolls
Royce
Ltd
Rolls
Royce
Ltd
SINFIN­
Derby
Sep­
86
­

1RR007
Rolls
Royce
Ltd
Rolls
Royce
Ltd
SINFIN­
Derby
Nov­
82
­

Filename
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aviation_
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Data
1
2
3
CT
CU
UID
No
Remarks
289
290
291
292
293
294
295
296
297
298
299
300
301
302
303
304
305
306
307
308
309
310
311
312
313
314
315
316
317
318
319
320
3PW065
Data
from
Report
PWA­
6678
3PW066
Data
from
Report
PWA­
6678
5PW076
1.
Data
from
Report
PWA­
6726­
01
1PW045
Data
from
X698­
5
with
reduced
smoke
combustor.

1PW044
­

1PW047
Data
from
X698­
5
with
reduced
smoke
combustor.

1PW046
­

1PW048
Data
from
X698­
5
with
reduced
smoke
combustor.

1PW049
Data
from
X821­
3
with
Floatwall
Combustor
1PW050
Data
from
X821­
3
with
Floatwall
Combustor
5PW075
1.
Data
from
Report
PWA­
7138.
2.
TALON
II
Combustor
4PW067
Data
from
X821­
3
with
Floatwall
Combustor
1PW051
­

1PW052
Data
from
X698­
5
with
reduced
smoke
combustor.

1PW053
Data
from
X693­
20
with
Phase
3
reduced
pressure
loss
combustor
1PW054
Data
from
X693­
20
with
Phase
3
reduced
pressure
loss
combustor
1PW055
Data
from
X693­
20
with
Phase
3
reduced
pressure
loss
combustor
1PW056
Data
from
X693­
20
with
Phase
3
reduced
pressure
loss
combustor
5PW074
1.
Data
from
Report
PWA­
7312.
2.
TALON
II
Combustor
1PW057
Data
from
X693­
20
with
Phase
3
reduced
pressure
loss
combustor
1PW059
Data
from
X693­
20
with
Phase
3
reduced
pressure
loss
combustor
1PW058
Data
from
X698­
5
with
reduced
smoke
combustor.

1RR001
Stage
bleed
on
2
engines
1RR002
Package
1
combustor.

1RR003
1.
Package
1
combustor.
2.
Tests
performed
on
in­
service
engine(
s),
after
overhaul.

1RR004
1.
Package
1
Combustor.
2.
Applicable
to
RB211­
524B,
B2,
B3,
B4.

1RR005
1.
Data
from
certification
report
CRR60515.
2.
Phase
2
combustor.
3.
Applicable
to
engines
manufactured
after
Feb
87.
4.
Applicable
to
RB211­
524B
1RR006
Package
1
combustor
1RR007
Package
1
combustor
Filename
DCTM_
ARP.
xls
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Data
1
2
3
CV
CW
CX
CY
CZ
DA
DB
DC
DD
DE
DF
DG
DH
289
290
291
292
293
294
295
296
297
298
299
300
301
302
303
304
305
306
307
308
309
310
311
312
313
314
315
316
317
318
319
320
4B,
B2,
B3,
B4.

Filename
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ARP.
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Data
1
2
3
DI
DJ
DK
DL
DM
DN
289
290
291
292
293
294
295
296
297
298
299
300
301
302
303
304
305
306
307
308
309
310
311
312
313
314
315
316
317
318
319
320
Filename
DCTM_
ARP.
xls
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on
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05
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Data
1
2
3
A
B
C
D
E
F
G
UID
Engine
Combustor
Eng
B/
P
Press
Rated
No
Identification
Description
Type
Ratio
Ratio
Output
kN
321
322
323
324
325
326
327
328
329
330
331
332
333
334
335
336
337
338
339
340
341
342
343
344
345
346
347
348
349
350
351
352
1RR008
RB211­
524D4
Phase
2
TF
4.3
30.22
231.3
1RR009
RB211­
524G
MTF
4.25
32.1
253
1RR010
RB211­
524G
MTF
4.25
32.1
253
4RR036
RB211­
524G­
T
MTF
4.25
32.1
253
1RR011
RB211­
524H
MTF
4.2
34.0
264.4
4RR037
RB211­
524H­
T
MTF
4.2
34.0
264
1RR012
RB211­
535C
TF
4.5
21.5
163.3
1RR013
RB211­
535E4
TF
4.1
25.4
176.1
1RR014
RB211­
535E4
TF
4.1
25.4
176.1
3RR028
RB211­
535E4
TF
4.1
25.8
178.4
5RR038
RB211­
535E4
Phase
5
MTF
4.1
26.0
178.4
3RR034
RB211­
535E4B
TF
4.1
27.65
191.73
5RR039
RB211­
535E4B
Phase
5
MTF
4.1
27.9
191.7
4RR035
Spey
555
Transply
IIF
MTF
1.0
15.9
44
1RR015
SPEY
Mk511
MTF
0.64
19.9
50.7
1RR016
SPEY
Mk511
Transply
IIH
MTF
0.64
18.7
50.7
1RR017
SPEY
Mk555
MTF
1.0
16.1
43.8
1RR018
SPEY
Mk555
Transply
IIF
MTF
1.0
15.9
44
3RR031
TAY
650
Pedhead
MTF
3.0
15.9
67.2
3RR032
TAY
651
Pedhead
MTF
3.0
16.4
68.5
3RR033
TAY
651
Transply
MTF
3.0
16.4
68.5
1RR019
TAY
Mk611­
8
MTF
3.0
16.1
61.6
6RR042
TAY
611­
8C
Transply
IIJ
TF
3.2
15.75
61.61
1RR020
TAY
Mk620­
15
MTF
3.0
16.1
61.6
1RR021
TAY
Mk650­
15
MTF
3.0
16.4
67.2
6RR041
Trent
556­
61
Phase
5
tiled
TF
7.5
36.71
261.5
2RR022
Trent
768
TF
5.15
34.04
298.7
3RR029
Trent
768
Improved
traverse
TF
5.15
34
300.3
2RR023
Trent
772
TF
5.03
35.79
315.9
3RR030
Trent
772
Improved
traverse
TF
5.03
35.8
316.3
2RR024
Trent
875
TF
6.08
35.42
351.85
2RR025
Trent
877
TF
6.02
36.30
361.64
Filename
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Data
1
2
3
H
I
J
K
L
M
N
O
P
Q
R
S
T
U
UID
Data
Superseded
Data
No
PR
C
R
superseded
by
NME
DTEPS
Other
Corr
as
Out
of
Date
Out
of
Date
UID
No
Annex
16
Production
Service
­­­­­­­­
Data
Status­­­­­­­­
­­­­­­­­­­
Current
Engine
Status
­­­­­­­­­­

­­­­­­
Test
Engine
Status­­­­­­

321
322
323
324
325
326
327
328
329
330
331
332
333
334
335
336
337
338
339
340
341
342
343
344
345
346
347
348
349
350
351
352
1RR008
­
x
­
­
­
­
x
­
x
x
­
­
­

1RR009
­
x
­
x
1RR010
­
x
­
x
x
­
­
­

1RR010
­
­
x
­
­
­
x
­
x
x
­
­
­

4RR036
­
x
­
­
­
­
x
­
x
­
­
­
­

1RR011
­
­
­
­
­
­
x
­
x
x
­
­
­

4RR037
­
x
­
­
­
­
x
­
x
­
­
­
­

1RR012
­
x
­
­
­
x
­
­
x
x
­
­
­

1RR013
­
x
­
x
1RR014
­
x
­
x
x
­
­
­

1RR014
­
­
x
x
3RR028
­
x
­
x
x
­
­
­

3RR028
­
­
x
­
­
­
x
­
x
x
­
­
­

5RR038
­
x
­
­
­
­
x
­
x
­
­
­
­

3RR034
­
­
x
­
­
­
x
­
x
x
­
­
­

5RR039
­
x
­
­
­
­
x
­
x
­
­
­
­

4RR035
­
x
­
­
­
­
x
­
x
x
­
­
­

1RR015
x
­
­
­
­
x
x
­
x
x
­
­
­

1RR016
­
x
­
­
­
­
x
­
x
x
­
­
­

1RR017
x
­
­
­
­
­
x
­
x
x
­
­
­

1RR018
­
x
­
­
­
x
x
­
x
­
­
­
­

3RR031
­
x
­
­
­
­
x
­
x
­
­
­
­

3RR032
­
x
­
­
­
­
x
­
x
­
­
­
­

3RR033
­
x
­
­
­
­
x
­
x
x
­
­
­

1RR019
­
x
­
­
­
x
­
­
x
­
­
­
­

6RR042
­
x
­
­
­
­
x
­
x
­
­
­
­

1RR020
­
x
­
­
­
x
­
­
x
x
­
­
­

1RR021
­
x
­
­
­
­
x
­
x
x
­
­
­

6RR041
­
x
­
­
­
x
­
­
x
­
­
­
­

2RR022
­
x
­
­
­
x
­
­
x
x
­
x
­

3RR029
­
x
­
­
­
­
x
­
x
­
­
­
­

2RR023
­
x
­
­
­
x
­
­
x
x
­
x
­

3RR030
­
x
­
­
­
­
x
­
x
­
­
­
­

2RR024
­
x
­
­
­
­
x
­
x
­
­
­
­

2RR025
­
x
­
­
­
­
x
­
x
­
­
­
­

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Data
1
2
3
V
W
X
Y
Z
AA
AB
AC
AD
AE
AF
AG
AH
UID
Characteristic
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
%
of
Total
mass
Reg
limit
(
g)

­­­­­­­­­­­­­­­­
EI
HC­­­­­­­­­­­­­­
­­­
Number
­­­
­­­­­­­­­­­­­­­
Dp/
Foo
(
HC)­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­
­­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­­­­­

321
322
323
324
325
326
327
328
329
330
331
332
333
334
335
336
337
338
339
340
341
342
343
344
345
346
347
348
349
350
351
352
1RR008
0.59
0.26
0.70
1.41
3
1
3.44
0.08
3.3­
3.5
5.3
27.0
805
1RR009
2.28
1.46
1.14
3.28
3
1
8.62
0.34
8.24­
8.92
13.3
67.7
2174
1RR010
0.39
0.27
0.37
0.89
3
2
2.14
0.28
1.87­
2.44
2.8
14.2
540
4RR036
0.00
0.03
0.00
3.95
3
1
6.24
­
5.29­
7.11
9.6
49.0
1610
1RR011
0.34
0.33
0.36
0.74
3
2
1.93
0.28
1.61­
2.14
2.5
12.8
495
4RR037
0
0.02
0
3.31
3
1
5.17
­
4.39­
5.89
8.0
40.6
1348
1RR012
0.25
0.14
0.44
1.44
3
3
3.4
0.4
3.0­
3.8
4.0
20.2
552
1RR013
0.69
0.94
1.33
2.85
5
2
7.12
0.45
6.6­
7.7
9.3
47.3
1268
1RR014
0.04
0.01
0.04
1.00
3
1
1.69
0.09
1.59­
1.77
2.6
13.3
307
3RR028
0
0.01
0.04
0.37
3
1
0.6
­
0.57­
0.66
0.9
4.6
111
5RR038
0.03
0.00
0.04
0.27
3
1
0.46
­
0.32
­
0.7
0.7
3.6
83
3RR034
0.01
0.00
0.03
0.28
3
1
0.45
­
0.41­
0.49
0.7
3.6
88
5RR039
0.07
0.00
0.05
0.14
3
1
0.28
­
0.16
­
0.54
0.4
2.2
54
4RR035
0.15
0.22
0.33
3.41
3
1
12.54
­
10.4­
15.9
19.3
98.5
552
1RR015
0.98
1.32
7.23
56.73
15
14
217
82.8
109­
360
232.4
1185.5
11179
1RR016
0.09
0.12
0.18
3.69
3
2
15.0
1.9
12.9­
16.8
19.5
99.6
758
1RR017
0.88
1.60
6.97
92.74
2
2
392
82.1
334­
450
510.1
2602.5
17160
1RR018
0.29
0.15
0.29
1.86
3
3
7.1
2.2
5.8­
9.7
8.3
42.3
315
3RR031
0.11
0.22
0.11
1.23
1
1
3.90
­
3.90
6.0
30.6
261
3RR032
0.09
0.19
0.12
1.32
1
1
4.08
­
4.08
6.3
32.1
276
3RR033
0.56
0.37
0.85
3.1
4
2
10.2
­
9.9­
10.4
13.3
67.9
689
1RR019
0.8
0.3
0.9
3.4
6
2
10.7
1.4
9.11­
12.97
13.9
71.0
684
6RR042
0.02
0
0
1.11
3
1
2.96
0
2.56­
3.37
4.6
23.2
182.4404
1RR020
0.8
0.3
0.9
3.4
6
2
10.7
1.4
9.11­
12.97
13.9
71.0
684
1RR021
0.37
0.41
0.88
3.29
4
2
10.7
0.63
10.2­
11.1
13.9
71.0
717
6RR041
0
0
0
0.1
4
2
0.1
0.14
0
­
0.2
0.2
1.0
36
2RR022
0.25
0.38
0.84
1.08
3
1
2.52
­
1.53
­
3.52
3.9
19.8
752
3RR029
0
0.01
0.01
1.89
3
1
2.7
­
2.29­
3.13
4.2
21.4
801
2RR023
0.33
0.35
0.81
0.97
3
1
2.29
­
1.23
­
3.18
3.5
18.0
735
3RR030
0
0
0.01
1.46
3
1
2.06
­
1.74­
2.37
3.2
16.3
640
2RR024
0
0
0
1.78
3
1
2.20
­
1.85­
2.52
3.4
17.3
778
2RR025
0
0
0
1.55
3
1
1.90
­
1.60­
2.18
2.9
14.9
677
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
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aviation_
emissions_
databank
Data
1
2
3
AI
AJ
AK
AL
AM
AN
AO
AP
AQ
AR
AS
AT
AU
UID
Characteristic
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
%
of
Total
mass
Reg
limit
(
g)

­­­­­­­­­­­­­­­­­
EI
CO­­­­­­­­­­­­­­­­­
­­­­­­
Number­­­­­
­­­­­­­­­­­­­­­
Dp/
Foo
(
CO)­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­­­

321
322
323
324
325
326
327
328
329
330
331
332
333
334
335
336
337
338
339
340
341
342
343
344
345
346
347
348
349
350
351
352
1RR008
1.24
0.34
1.56
9.30
3
1
18.07
0.64
17.6­
18.8
22.2
18.8
4223
1RR009
0.59
0.43
1.01
13.74
3
1
23.49
0.34
23.13­
23.81
28.8
24.4
5926
1RR010
0.59
0.43
1.01
13.74
3
1
23.49
0.34
23.13­
23.81
28.8
24.4
5926
4RR036
0.16
0.14
1.17
28.82
3
1
46.37
­
43.60­
50.58
56.9
48.2
11954
1RR011
0.87
0.38
0.99
11.75
3
1
19.35
0.37
18.9­
19.6
23.8
20.1
5143
4RR037
0.18
0.14
1.05
26.17
3
1
41.67
­
39.21­
45.02
51.2
43.3
10871
1RR012
0.70
0.27
0.48
18.79
3
3
37.3
2.6
35.5­
40.3
40.3
34.2
6030
1RR013
1.01
1.23
1.71
15.44
5
2
28.6
3.5
24.6­
33.4
32.6
27.6
5134
1RR014
1.01
1.23
1.71
15.44
5
2
28.6
3.5
24.6­
33.4
32.6
27.6
5134
3RR028
0.77
0.5
1.14
13.31
3
1
22.3
­
22.0­
22.6
27.4
23.2
4040
5RR038
0.26
0.29
2.72
20.33
3
1
33.6
­
33.3
­
33.8
41.2
34.9
6126
3RR034
0.94
0.60
1.05
11.76
3
1
19.67
­
19.35­
19.92
24.1
20.5
3837
5RR039
0.33
0.26
2.43
18.24
3
1
29.7
­
29.45
­
29.91
36.5
30.9
5812
4RR035
1.54
2.08
5.78
31.16
3
1
118.08
­
116.5­
120.0
144.9
122.8
5203
1RR015
1.81
2.06
20.30
97.96
15
14
382
66.5
233­
522
395.8
335.4
19810
1RR016
0.12
0.63
2.65
31.77
3
2
128.9
8.3
119.5­
135.3
146.9
124.5
6536
1RR017
0.44
0.0
22.22
88.23
2
2
388
148.9
283­
493
442.1
374.6
17026
1RR018
0.3
0.7
3.7
29.3
3
3
106.3
16.3
88.7­
120.8
115.0
97.4
4648
3RR031
0.69
0.48
1.76
22.36
4
1
65.16
­
62.4­
67.9
80.0
67.8
4361
3RR032
0.75
0.51
1.64
23.26
4
1
66.93
­
64.2­
69.8
82.2
69.6
4532
3RR033
1.68
1.93
6.11
32.68
4
2
99.7
­
91.6­
107.8
113.6
96.3
6744
1RR019
0.7
0.8
3.9
24.1
6
2
69.3
4.1
65.5­
74.8
79.0
66.9
4440
6RR042
1.12
1.27
4.99
28.55
3
1
82.78
0
78.58­
86.04
101.6
86.1
5103
1RR020
0.7
0.8
3.9
24.1
6
2
69.3
4.1
65.5­
74.8
79.0
66.9
4440
1RR021
1.74
2.01
6.54
33.77
4
2
102.9
11.8
94.6­
111.3
117.2
99.4
6921
6RR041
0.02
0.25
0.46
10.3
4
2
14.6
0.99
13.9
­
15.3
16.6
14.1
3826
2RR022
0.18
0.13
0.86
10.52
3
1
15.10
­
13.83­
15.92
18.5
15.7
4496
3RR029
0.18
0.15
1.02
20.22
3
1
29.7
­
27.6­
31.4
36.5
30.9
8786
2RR023
0.18
0.15
0.78
9.36
3
1
13.32
­
12.29­
14.00
16.4
13.9
4175
3RR030
0.2
0.16
0.89
17.94
3
1
26
­
24.2­
27.4
31.9
27.0
8099
2RR024
0.19
0.16
0.86
19.66
3
1
24.93
­
23.17­
26.31
30.6
25.9
8848
2RR025
0.20
0.16
0.80
18.42
3
1
23.26
­
21.62­
24.46
28.6
24.2
8302
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
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aviation_
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Data
1
2
3
AV
AW
AX
AY
AZ
BA
BB
BC
BD
BE
BF
BG
BH
BI
BJ
UID
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
Original
CAEP
2
CAEP
4
Total
mass
(
g)

­­­­
Number­­­­­

­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­
EI
NOx­­­­­­­­­­­­­­
­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­
Dp/
Foo
(
NOx)­­­­­­­­­­­­­­
Characteristic
as
%
of
standards
321
322
323
324
325
326
327
328
329
330
331
332
333
334
335
336
337
338
339
340
341
342
343
344
345
346
347
348
349
350
351
352
1RR008
59.35
43.01
10.63
4.41
3
1
86.54
0.55
85.9­
86.9
100.3
99.9
124.8
148.7
20124
1RR009
58.71
40.54
9.56
4.63
3
1
83.57
1.39
82.34­
85.08
96.9
93.0
116.2
136.1
21075
1RR010
58.71
40.54
9.56
4.63
3
1
83.57
1.39
82.34­
85.08
96.9
93.0
116.2
136.1
21075
4RR036
28.43
21.80
9.68
4.00
3
1
49.42
­
48.0­
50.3
57.3
55.0
68.7
80.5
12513
1RR011
65.84
46.31
10.26
4.78
3
1
92.83
1.79
91.1­
94.6
107.6
99.6
124.5
143.5
24501
4RR037
31.19
23.19
9.91
4.16
3
1
53.09
­
51.6­
54.1
61.5
57.0
71.2
82.1
13995
1RR012
33.71
24.89
6.37
3.44
3
3
57.0
2.0
54.1­
58.7
60.4
72.7
90.9
113.1
9277
1RR013
52.7
36.2
7.5
4.3
5
2
76.9
1.3
75.0­
78.9
84.6
93.1
116.4
141.8
13633
1RR014
52.7
36.2
7.5
4.3
5
2
76.9
1.3
75.0­
78.9
84.6
93.1
116.4
141.8
13633
3RR028
44.88
32.06
6.78
3.46
3
1
65.6
­
64.4­
66.9
76.0
83.0
103.7
126.1
11714
5RR038
22.31
17.56
8.38
4.4
3
1
41.8
­
40.3
­
43.6
48.5
52.7
65.8
80.0
7492
3RR034
54.46
36.82
7.35
3.52
3
1
76.97
­
75.9­
77.9
89.2
93.6
117.0
141.0
14791
5RR039
25.88
19.3
8.65
4.58
3
1
46.4
­
44.9
­
48.0
53.8
56.1
70.2
84.5
8927
4RR035
17.33
13.06
5.05
2.23
3
1
49.02
­
46.7­
52.8
56.8
79.1
98.9
105.5
2160
1RR015
23.27
19.18
7.94
1.48
14
13
69.1
7.39
52.5­
81.4
71.0
89.0
111.2
120.6
3513
1RR016
22.7
17.3
7.2
3.6
3
2
73.0
4.8
67.8­
77.2
80.3
103.7
129.6
140.9
3701
1RR017
18.92
14.64
5.92
1.83
2
2
50.75
12.48
41.9­
59.6
55.8
77.3
96.6
102.9
2354
1RR018
21.9
16.5
6.8
3.7
3
3
65.5
1.7
64.5­
67.5
69.4
96.6
120.8
128.8
2880
3RR031
16.45
12.94
5.26
2.50
4
1
38.75
­
38.1­
39.5
44.9
62.6
78.2
91.6
2591
3RR032
17.56
13.77
5.42
2.52
4
1
40.45
­
39.7­
41.1
46.9
64.4
80.5
94.6
2760
3RR033
20.31
17.13
4.77
1.72
4
2
43.9
­
40.9­
46.8
48.3
66.3
82.9
97.4
2990
1RR019
21.1
16.8
5.7
2.5
6
2
45.6
0.7
44.9­
46.7
50.1
69.5
86.8
99.2
2814
6RR042
18.42
15.01
5.6
2.76
3
1
41.59
0
40.99­
41.92
48.2
67.4
84.3
96.6
2562
1RR020
21.1
16.8
5.7
2.5
6
2
45.6
0.7
44.9­
46.7
50.1
69.5
86.8
99.2
2814
1RR021
19.81
16.47
4.55
1.70
4
2
42.8
3.92
40.2­
45.6
47.1
64.6
80.8
94.4
2875
6RR041
44.91
32.76
11.78
6.19
4
2
61.1
0.42
60.8
­
61.4
67.2
59.2
74.1
83.6
16113
2RR022
39.11
30.01
10.34
5.60
3
1
62.52
­
62.1
­
62.8
72.5
67.1
83.8
96.5
18672
3RR029
31.25
24.66
10.01
4.52
3
1
52.2
­
51.0­
53.1
60.5
56.0
70.0
80.7
15658
2RR023
43.60
32.66
10.68
5.74
3
1
68.09
­
67.7
­
68.4
78.9
70.7
88.4
100.4
21462
3RR030
34.38
26.44
10.3
4.71
3
1
56.3
­
55.0­
57.4
65.3
58.5
73.1
83.1
17784
2RR024
33.32
26.55
10.43
4.64
3
1
49.88
­
48.7­
50.8
57.8
52.2
65.2
74.3
17575
2RR025
34.76
27.59
10.59
4.75
3
1
51.82
­
50.5­
52.8
60.1
53.3
66.7
75.5
18736
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
www.
QinetiQ.
com/
aviation_
emissions_
databank
Data
1
2
3
BK
BL
BM
BN
BO
BP
BQ
BR
BS
BT
BU
BV
UID
Characteristic
No
T/
O
C/
O
App
Idle
Test
Eng
Max
Sigma
Range
Characteristic
%
of
Reg
limit
­­­­­­­­­­­­­­
Smoke
Number­­­­­­­­­­­­­

­­­­­­­­­­­­­
Smoke
Number­­­­­­­­­­­­­
­­­­
Number­­­­

321
322
323
324
325
326
327
328
329
330
331
332
333
334
335
336
337
338
339
340
341
342
343
344
345
346
347
348
349
350
351
352
1RR008
­
­
­
­
3
1
12.3
0.31
12.1­
12.7
15.8
84.2
1RR009
­
­
­
­
3
1
3.9
0.37
3.7­
4.3
5.0
27.3
1RR010
­
­
­
­
3
1
3.9
0.37
3.7­
4.3
5.0
27.3
4RR036
­
­
­
­
3
1
5.34
­
4.7­
6.0
6.9
37.4
1RR011
­
­
­
­
3
1
3.9
0.37
3.7­
4.3
5.0
27.7
4RR037
­
­
­
­
3
1
5.34
­
4.7­
6.0
6.9
37.9
1RR012
­
­
­
­
­
3
8.0
3.0
4.6­
10.1
8.8
42.5
1RR013
­
­
­
­
5
2
1.7
0.3
1.5­
2.3
2.0
9.8
1RR014
­
­
­
­
5
2
1.7
0.3
1.5­
2.3
2.0
9.8
3RR028
­
­
­
­
3
1
1.8
­
1.5­
2.2
2.3
11.4
5RR038
­
­
­
­
3
1
7.3
­
6.9
­
7.9
9.4
46.5
3RR034
­
­
­
­
3
1
1.84
­
1.5­
2.2
2.4
12.1
5RR039
­
­
­
­
3
1
7.3
­
6.9
­
7.9
9.4
47.5
4RR035
­
­
­
­
3
1
27.97
­
26.9­
28.8
36.0
121.5
1RR015
66.2
<
66.2
<
66.2
<
66.2
10
10
66.2
7.2
50.4­
71.3
77.9
273.1
1RR016
­
­
­
­
3
2
21.9
3.1
19.9­
25.4
25.7
90.1
1RR017
N/
A
N/
A
N/
A
N/
A
N/
A
N/
A
N/
A
N/
A
N/
A
­

1RR018
­
­
­
­
3
3
25.8
1.7
24.0­
27.4
28.4
95.7
3RR031
­
­
­
­
4
1
9.87
­
9.3­
10.4
12.7
48.1
3RR032
­
­
­
­
4
1
9.87
­
9.3­
10.4
12.7
48.4
3RR033
­
­
­
­
4
2
17.5
­
16.1­
18.9
20.5
78.1
1RR019
­
­
­
­
6
2
21.3
1.6
18.9­
22.8
25.0
92.4
6RR042
3.93
2.24
0.23
0.13
3
1
3.93
0
3.53­
4.35
5.06
18.7
1RR020
­
­
­
­
6
2
21.3
1.6
18.9­
22.8
25.0
92.4
1RR021
­
­
­
­
4
2
17.6
1.98
16.2­
19.0
20.6
78.2
6RR041
2.24
2.09
1.02
0.76
4
2
3.1
1.13
2.3
­
3.9
3.7
20.3
2RR022
­
­
­
­
3
1
1.26
­
1.1
­
1.5
1.6
9.2
3RR029
­
­
­
­
3
1
2
­
1.6­
2.5
2.6
14.8
2RR023
­
­
­
­
3
1
1.26
­
1.1
­
1.5
1.6
9.4
3RR030
­
­
­
­
3
1
2
­
1.6­
2.5
2.6
15.1
2RR024
­
­
­
­
3
1
5.34
­
4.7­
6.0
6.9
41.0
2RR025
­
­
­
­
3
1
5.34
­
4.7­
6.0
6.9
41.3
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
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for
latest
version
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aviation_
emissions_
databank
Data
1
2
3
BW
BX
BY
BZ
CA
CB
CC
CD
CE
UID
Fuel
per
No
Spec
H/
C
Arom
T/
O
C/
O
App
Idle
LTO
cycle
Ratio
%
(
kg)

­­­­­­­­­­­­­­­­­
Fuel
Flow­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­(
kg/
sec)­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­­­­­
Fuel­­­­­­­­­­­­­­­­­­­­­­­

321
322
323
324
325
326
327
328
329
330
331
332
333
334
335
336
337
338
339
340
341
342
343
344
345
346
347
348
349
350
351
352
1RR008
AVTUR
1.91
20
2.34
1.91
0.65
0.26
912
1RR009
AVTUR
1.91
20
2.62
2.08
0.70
0.26
958
1RR010
AVTUR
1.91
20
2.62
2.08
0.70
0.26
958
4RR036
AVTUR
1.95
16
2.62
2.10
0.74
0.26
970
1RR011
AVTUR
1.91
20
2.73
2.17
0.71
0.26
977
4RR037
AVTUR
1.95
16
2.81
2.22
0.77
0.26
1001
1RR012
AVTUR
1.91
20
1.80
1.47
0.54
0.20
711
1RR013
AVTUR
1.91
20
1.86
1.51
0.57
0.19
711
1RR014
AVTUR
1.91
20
1.86
1.51
0.57
0.19
711
3RR028
AVTUR
1.9
18.2
1.86
1.51
0.52
0.18
683
5RR038
AVTUR
1.931
17.6
1.85
1.5
0.52
0.18
681
3RR034
AVTUR
1.90
18.2
2.08
1.65
0.55
0.19
734
5RR039
AVTUR
1.931
17.6
2.07
1.64
0.55
0.19
732
4RR035
AVTUR
1.87­
1.95
15­
20
0.735
0.593
0.221
0.0964
313
1RR015
DERD
2494
1.94
20
0.889
0.726
0.279
0.119
386
1RR016
DERD
2494
1.91
20
0.891
0.726
0.278
0.127
398
1RR017
DERD
2494
1.94
20
0.720
0.589
0.222
0.115
341
1RR018
DERD
2494
1.91
20
0.735
0.592
0.221
0.096
312
3RR031
AVTUR
1.95
16.1
0.86
0.71
0.25
0.12
377
3RR032
AVTUR
1.95
16.1
0.87
0.72
0.26
0.12
381
3RR033
AVTUR
1.91
20
0.87
0.72
0.26
0.12
381
1RR019
AVTUR
1.91
20
0.76
0.63
0.23
0.11
342
6RR042
­
1.986
17.5
0.741
0.612
0.241
0.105
334
1RR020
AVTUR
1.91
20
0.76
0.63
0.23
0.11
342
1RR021
AVTUR
1.91
20
0.874
0.715
0.254
0.119
378
6RR041
­
1.97
17.6
2.24
1.83
0.62
0.23
843
2RR022
AVTUR
1.94
16
2.94
2.42
0.80
0.26
1041
3RR029
AVTUR
1.95
16
2.97
2.43
0.81
0.27
1061
2RR023
AVTUR
1.94
16
3.15
2.58
0.84
0.27
1096
3RR030
AVTUR
1.95
16
3.2
2.58
0.85
0.28
1116
2RR024
AVTUR
1.95
16
3.10
2.57
0.88
0.28
1117
2RR025
AVTUR
1.95
16
3.21
2.66
0.90
0.28
1139
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
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Data
1
2
3
CF
CG
CH
CI
CJ
CK
CL
CM
UID
No
Baro
Temp
Humidity
kW
@
Power
%
CF
@
Power
kPa
K
kg/
kg
­­­­­­­­­­­­­­­­­­­
Ambient­­­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­
Loads­­­­­­­­­­­­­­­­­­­

Power
Extraction
­­­
Stage
Bleed­­­

321
322
323
324
325
326
327
328
329
330
331
332
333
334
335
336
337
338
339
340
341
342
343
344
345
346
347
348
349
350
351
352
1RR008
0
­
0
­
103
283
­
286
0.005
1RR009
0
­
0
­
101
283
­
286
0.006
1RR010
0
­
0
­
101
283
­
286
0.006
4RR036
0
­
0
­
100.2
287
.0053­.
0089
1RR011
0
­
0
­
101
283
­
286
0.006
4RR037
0
­
0
­
100.2
287
.0053­.
0089
1RR012
0
­
0
­
­
281
­
287
0.004­
0.005
1RR013
0
­
0
­
100.8­
101.2
285
­
298
0.0058­
0.0087
1RR014
0
­
0
­
100.8­
101.2
285
­
298
0.0058­
0.0087
3RR028
0
­
0
­
98.8
282
0.0037
5RR038
0
­
0
­
100.7
­
101.2
281
­
287
.0058
­
.0064
3RR034
0
­
0
­
98.8
282
0.0037
5RR039
0
­
0
­
100.7
­
101.2
281
­
287
.0058
­
.0064
4RR035
0
­
0
­
100.2
287
.0068­.
0088
1RR015
0
­
0
­
­
­
0.0035­
0.0126
1RR016
0
­
0
­
99­
102
285
­
289
0.006­
0.009
1RR017
0
­
0
­
102
279
N/
A
1RR018
0
­
0
­
99­
102
280
­
290
0.006­
0.010
3RR031
0
­
0
­
­
283
.0068­.
0081
3RR032
0
­
0
­
­
283
.0068­.
0081
3RR033
0
­
0
­
99­
101
280­
289
.005­.
008
1RR019
0
­
0
­
100
288
0.005
6RR042
0
­
0
­
99.9
­
100
281.4
­
282.7
0.00475
1RR020
0
­
0
­
100
288
0.005
1RR021
0
­
0
­
99­
101
280
­
289
.005­.
008
6RR041
0
­
0
­
100.04
­
102.91
275.5
­
280.3
0.0038
­
0.0062
2RR022
0
­
0
­
100.6
293
.0073
­
.0084
3RR029
0
­
0
­
100.2
287
.0053­.
0089
2RR023
0
­
0
­
100.6
293
.0073
­
.0084
3RR030
0
­
0
­
100.2
287
.0053­.
0089
2RR024
0
­
0
­
100.2
287
.00527
­
.00886
2RR025
0
­
0
­
100.2
287
.00527
­
.00886
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
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www.
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aviation_
emissions_
databank
Data
1
2
3
CN
CO
CP
CQ
CR
CS
UID
­­­
Test
Dates­­­

No
Manufacturer
Test
Organisation
Test
Location
From
To
321
322
323
324
325
326
327
328
329
330
331
332
333
334
335
336
337
338
339
340
341
342
343
344
345
346
347
348
349
350
351
352
1RR008
Rolls
Royce
Ltd
Rolls
Royce
Ltd
SINFIN­
Derby
Sep­
86
Sep­
86
1RR009
Rolls
Royce
Ltd
Rolls
Royce
Ltd
SINFIN­
Derby
Apr­
87
May­
87
1RR010
Rolls
Royce
Ltd
Rolls
Royce
Ltd
SINFIN­
Derby
Apr­
87
Oct­
92
4RR036
Rolls­
Royce
plc
Rolls­
Royce
plc
SINFIN,
Derby
Sep­
94
1RR011
Rolls
Royce
Ltd
Rolls
Royce
Ltd
SINFIN­
Derby
Apr­
87
Oct­
92
4RR037
Rolls­
Royce
plc
Rolls­
Royce
plc
SINFIN,
Derby
Sep­
94
1RR012
Rolls
Royce
Ltd
Rolls
Royce
Ltd
SINFIN­
Derby
Apr­
84
May­
84
1RR013
Rolls
Royce
Ltd
Rolls
Royce
Ltd
SINFIN­
Derby
2­
Jul­
84
25­
Oct­
84
1RR014
Rolls
Royce
Ltd
Rolls
Royce
Ltd
SINFIN­
Derby
2­
Jul­
84
Apr­
91
3RR028
Rolls
Royce
plc
Rolls
Royce
plc
SINFIN,
Derby
Apr­
91
­

5RR038
Rolls­
Royce
plc
Rolls­
Royce
plc
Hucknall
May­
99
3RR034
Rolls
Royce
plc
Rolls
Royce
plc
SINFIN,
Derby
Apr­
91
­

5RR039
Rolls­
Royce
plc
Rolls­
Royce
plc
Hucknall
May­
99
4RR035
Rolls­
Royce
plc
Rolls­
Royce
plc
SINFIN,
Derby
1987
1RR015
Rolls
Royce
Ltd
Rolls
Royce
Ltd
Derby
1970
1975
1RR016
Rolls
Royce
Ltd
Rolls
Royce
Ltd
Derby
Sep­
84
Aug­
85
1RR017
Rolls
Royce
Ltd
Rolls
Royce
Ltd
Derby
1973
1975
1RR018
Rolls
Royce
Ltd
­
­
Aug­
83
Nov­
84
3RR031
Rolls
Royce
plc
Rolls
Royce
plc
SINFIN,
Derby
Jun­
97
3RR032
Rolls
Royce
plc
Rolls
Royce
plc
SINFIN,
Derby
Jun­
97
3RR033
Rolls
Royce
plc
Rolls
Royce
plc
SINFIN,
Derby
Mar­
88
Oct­
89
1RR019
Rolls
Royce
Ltd
­
­
Oct­
86
Nov­
86
6RR042
Rolls­
Royce
Rolls­
Royce
Dahlewitz
21­
Jan­
02
22­
Jan­
02
1RR020
Rolls
Royce
Ltd
­
­
Oct­
86
Nov­
86
1RR021
Rolls
Royce
Ltd
Rolls
Royce
Ltd
Derby
Mar­
88
Oct­
89
6RR041
Rolls
Royce
Rolls
Royce
Derby
7­
Jan­
02
18­
Jan­
02
2RR022
Rolls
Royce
plc
Rolls
Royce
plc
SINFIN,
Derby
Jul­
94
­

3RR029
Rolls
Royce
plc
Rolls
Royce
plc
SINFIN,
Derby
Sep­
94
­

2RR023
Rolls
Royce
plc
Rolls
Royce
plc
SINFIN,
Derby
Jul­
94
­

3RR030
Rolls
Royce
plc
Rolls
Royce
plc
SINFIN,
Derby
Sep­
94
­

2RR024
Rolls
Royce
plc
Rolls
Royce
plc
SINFIN,
Derby
Sep­
94
­

2RR025
Rolls
Royce
plc
Rolls
Royce
plc
SINFIN,
Derby
Sep­
94
­

Filename
DCTM_
ARP.
xls
Printed
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05
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aviation_
emissions_
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Data
1
2
3
CT
CU
UID
No
Remarks
321
322
323
324
325
326
327
328
329
330
331
332
333
334
335
336
337
338
339
340
341
342
343
344
345
346
347
348
349
350
351
352
1RR008
1.
Data
from
certification
report
CRR60515.
2.
Phase
2
combustor.
3.
Applicable
to
engines
manufactured
after
Feb
87.

1RR009
Data
from
certification
report
CRR60560
1RR010
HC
data
remeasured.

4RR036
Data
from
Certification
Report
DNS38044
1RR011
­

4RR037
Data
from
Certification
Report
DNS38044
1RR012
Data
from
certification
report
CRR58085
1RR013
Ref
RR
report
CRR58095
1RR014
HC
data
remeasured.

3RR028
Data
from
Certification
Report
DNS21233
5RR038
1.
Data
from
certification
report
DNS63281.
2.
Phase
5
combustor
3RR034
Data
from
Certification
Report
DNS21233
5RR039
1.
Data
from
certification
report
DNS63281.
2.
Phase
5
combustor
4RR035
1.
Ref
RR
report
CRR10165
2.
Transply
IIF
combustors
with
standard
fuel
pump
1RR015
­

1RR016
1.
Data
from
RR
report
CRR10149.
2.
Transply
IIH
combustors.

1RR017
­

1RR018
1.
Ref
RR
report
CRR10145.
2.
Transply
IIF
combustors
with
H.
P.
fuel
pump.

3RR031
Pedhead
combustor
3RR032
Pedhead
combustor
3RR033
Transply
combustor
1RR019
Data
from
certification
report
CRR19019
6RR042
1.
Certification
report
E­
TR164/
02
2.
New
airspray
fuel
injector
1RR020
Data
from
certification
report
CRR19019
1RR021
Data
from
certification
report
CRR19057
6RR041
1.
Certification
report
DNS
85728
2.
Phase
5
tiled
combustor
2RR022
Data
from
certification
report
DNS
12859
3RR029
1.
Data
from
certification
report
DNS
19234.
2.
Improved
traverse
combustor.

2RR023
Data
from
certification
report
DNS
12859
3RR030
1.
Data
from
certification
report
DNS
19234.
2.
Improved
traverse
combustor.

2RR024
Data
from
certification
report
DNS
14445
2RR025
Data
from
certification
report
DNS
14445
Filename
DCTM_
ARP.
xls
Printed
on
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05
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aviation_
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Data
1
2
3
CV
CW
CX
CY
CZ
DA
DB
DC
DD
DE
DF
DG
DH
321
322
323
324
325
326
327
328
329
330
331
332
333
334
335
336
337
338
339
340
341
342
343
344
345
346
347
348
349
350
351
352
New
airspray
fuel
injector
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
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aviation_
emissions_
databank
Data
1
2
3
DI
DJ
DK
DL
DM
DN
321
322
323
324
325
326
327
328
329
330
331
332
333
334
335
336
337
338
339
340
341
342
343
344
345
346
347
348
349
350
351
352
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
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website
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aviation_
emissions_
databank
Data
1
2
3
A
B
C
D
E
F
G
UID
Engine
Combustor
Eng
B/
P
Press
Rated
No
Identification
Description
Type
Ratio
Ratio
Output
kN
353
354
355
356
357
358
359
360
361
362
363
364
365
366
2RR026
Trent
884
TF
5.87
38.96
390.10
2RR027
Trent
892
TF
5.7
41.38
411.48
5RR040
Trent
895
TF
5.7
41.52
413.05
Textron
Lycoming
1TL001
ALF
502L­
2
TF
5.1
13.15
33.4
1TL002
ALF
502R­
3
TF
5.7
11.4
29.8
1TL003
ALF
502R­
5
TF
5.6
12.0
31.0
1TL004
LF507­
1F,
­
1H
TF
5.1
13.0
31.0
ZMKB
1ZM001
D­
36
TF
5
19.9
63.765
Filename
DCTM_
ARP.
xls
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05
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aviation_
emissions_
databank
Data
1
2
3
H
I
J
K
L
M
N
O
P
Q
R
S
T
U
UID
Data
Superseded
Data
No
PR
C
R
superseded
by
NME
DTEPS
Other
Corr
as
Out
of
Date
Out
of
Date
UID
No
Annex
16
Production
Service
­­­­­­­­
Data
Status­­­­­­­­
­­­­­­­­­­
Current
Engine
Status
­­­­­­­­­­

­­­­­­
Test
Engine
Status­­­­­­

353
354
355
356
357
358
359
360
361
362
363
364
365
366
2RR026
­
x
­
­
­
­
x
­
x
­
­
­
­

2RR027
­
x
­
­
­
­
x
­
x
­
­
­
­

5RR040
­
x
­
­
­
­
x
­
x
­
­
­
­

1TL001
­
x
­
­
­
x
­
­
x
x
­
­
­

1TL002
­
x
­
­
­
x
­
­
x
x
­
­
­

1TL003
­
x
­
­
­
x
­
­
x
x
­
­
­

1TL004
­
x
­
­
­
x
­
­
x
­
­
­
­

1ZM001
­
x
­
­
­
x
­
­
x
x
­
­
­

Filename
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ARP.
xls
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Data
1
2
3
V
W
X
Y
Z
AA
AB
AC
AD
AE
AF
AG
AH
UID
Characteristic
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
%
of
Total
mass
Reg
limit
(
g)

­­­­­­­­­­­­­­­­
EI
HC­­­­­­­­­­­­­­
­­­
Number
­­­
­­­­­­­­­­­­­­­
Dp/
Foo
(
HC)­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­
­­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­­­­­

353
354
355
356
357
358
359
360
361
362
363
364
365
366
2RR026
0
0
0
1.00
3
1
1.21
­
1.03­
1.40
1.9
9.5
484
2RR027
0.01
0
0
0.7
3
1
0.79
­
0.67­
0.93
1.2
6.1
329
5RR040
0.02
0.00
0.00
0.89
3
1
1.10
­
0.95
­
1.24
1.7
8.6
462
1TL001
0.02
0.023
0.183
6.65
3
3
15.3
2.59
13.2­
18.2
17.8
90.8
501
1TL002
0.056
0.053
0.287
6.51
3
3
15.0
3.25
11.9­
18.4
17.5
89.3
449
1TL003
0.060
0.053
0.217
5.39
3
3
11.7
­
­
13.6
69.4
351
1TL004
0.01
0.01
0.12
4.72
3
1
10.8
­
­
16.7
85.2
337
1ZM001
0
0
0
5.4
7
3
12
0.8
11.2­
13
14.0
71.4
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ARP.
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aviation_
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Data
1
2
3
AI
AJ
AK
AL
AM
AN
AO
AP
AQ
AR
AS
AT
AU
UID
Characteristic
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
%
of
Total
mass
Reg
limit
(
g)

­­­­­­­­­­­­­­­­­
EI
CO­­­­­­­­­­­­­­­­­
­­­­­­
Number­­­­­
­­­­­­­­­­­­­­­
Dp/
Foo
(
CO)­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­­­

353
354
355
356
357
358
359
360
361
362
363
364
365
366
2RR026
0.24
0.18
0.65
15.19
3
1
19.02
­
17.64­
19.78
23.4
19.8
7602
2RR027
0.28
0.2
0.57
13.07
3
1
15.34
­
13.98­
16.27
18.8
15.9
6381
5RR040
0.27
0.19
0.54
14.71
3
1
18.80
­
17.71
­
19.67
23.1
19.6
7834
1TL001
0.40
0.30
3.97
45.63
3
3
107.3
6.47
101.5­
114.3
116.1
98.4
3527
1TL002
0.433
0.500
8.43
44.67
3
3
109.0
10.62
100.2­
120.8
117.9
99.9
3244
1TL003
0.300
0.250
7.10
40.93
3
3
90.4
­
­
97.8
82.9
2796
1TL004
0.20
0.30
4.43
37.83
3
1
90.10
­
­
110.6
93.7
2803
1ZM001
0.5
0.4
2.7
20.7
7
3
48.8
3
46.2­
52
52.8
44.7
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Data
1
2
3
AV
AW
AX
AY
AZ
BA
BB
BC
BD
BE
BF
BG
BH
BI
BJ
UID
LTO
No
T/
O
C/
O
App
Idle
Test
Eng
Average
Sigma
Range
Characteristic
Original
CAEP
2
CAEP
4
Total
mass
(
g)

­­­­
Number­­­­­

­­­­­­­­­­­­­­­­(
g/
kg)­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­
EI
NOx­­­­­­­­­­­­­­
­­­­­­­­­­­­­­­­­­­(
g/
kN)­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­
Dp/
Foo
(
NOx)­­­­­­­­­­­­­­
Characteristic
as
%
of
standards
353
354
355
356
357
358
359
360
361
362
363
364
365
366
2RR026
40.05
30.63
11.07
5.04
3
1
58.00
­
56.5­
59.2
67.2
57.0
71.3
79.2
22687
2RR027
45.7
33.3
11.58
5.33
3
1
64.05
­
62.2­
65.6
74.2
60.4
75.6
82.7
26405
5RR040
47.79
34.29
11.39
5.11
3
1
67.81
­
65.76
­
69.5
78.6
63.9
79.9
87.3
28029
1TL001
13.43
12.03
6.47
3.38
3
3
35.2
3.50
32.7­
39.2
37.2
56.1
70.1
72.0
1173
1TL002
11.20
9.94
6.15
3.30
3
3
30.7
0.795
29.9­
31.45
32.5
51.8
64.7
65.5
915
1TL003
13.35
10.56
6.6
3.78
3
3
32.9
­
­
34.8
54.4
68.0
69.1
1017
1TL004
14.52
12.02
6.39
3.28
3
1
34.9
­
­
40.4
61.2
76.5
77.8
1086
1ZM001
26
22
9
5.5
7
3
56.3
2.5
54.5­
59
59.6
74.7
93.4
106.2
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Data
1
2
3
BK
BL
BM
BN
BO
BP
BQ
BR
BS
BT
BU
BV
UID
Characteristic
No
T/
O
C/
O
App
Idle
Test
Eng
Max
Sigma
Range
Characteristic
%
of
Reg
limit
­­­­­­­­­­­­­­
Smoke
Number­­­­­­­­­­­­­

­­­­­­­­­­­­­
Smoke
Number­­­­­­­­­­­­­
­­­­
Number­­­­

353
354
355
356
357
358
359
360
361
362
363
364
365
366
2RR026
­
­
­
­
3
1
5.34
­
4.7­
6.0
6.9
42.1
2RR027
­
­
­
­
3
1
5.34
­
4.7­
6.0
6.9
42.8
5RR040
­
­
­
­
3
1
5.34
­
4.7
­
6.0
6.9
42.8
1TL001
8.3
12.7
8.7
2.9
3
3
11.4
2.91
8.1­
13.5
12.5
39.1
1TL002
12.63
12.00
5.47
2.133
3
3
13.0
2.39
10.2­
14.4
14.3
43.4
1TL003
13.5
12.7
5.7
2.3
3
3
15.4
­
­
16.9
51.8
1TL004
10.3
10.2
6.9
6.8
3
1
10.60
­
­
13.6
41.7
1ZM001
14.8
­
­
­
3
2
14.8
­
­
17.4
64.8
Filename
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ARP.
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Data
1
2
3
BW
BX
BY
BZ
CA
CB
CC
CD
CE
UID
Fuel
per
No
Spec
H/
C
Arom
T/
O
C/
O
App
Idle
LTO
cycle
Ratio
%
(
kg)

­­­­­­­­­­­­­­­­­
Fuel
Flow­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­(
kg/
sec)­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­­­­­
Fuel­­­­­­­­­­­­­­­­­­­­­­­

353
354
355
356
357
358
359
360
361
362
363
364
365
366
2RR026
AVTUR
1.95
16
3.56
2.89
0.97
0.31
1247
2RR027
AVTUR
1.95
16
3.91
3.10
1.00
0.30
1281
5RR040
AVTUR
1.95
16
4.03
3.19
1.05
0.33
1357
1TL001
.81
1.925
19.7
0.3999
0.3236
0.1172
0.0477
162
1TL002
.81
1.925
19.7
0.3476
0.2880
0.1027
0.0432
145
1TL003
.81
1.925
19.7
0.3581
0.2955
0.1034
0.0408
143
1TL004
.81
1.925
19.7
0.3578
0.2961
0.1083
0.0453
151
1ZM001
RT
1.95
18.5
0.634
0.533
0.211
­

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Data
1
2
3
CF
CG
CH
CI
CJ
CK
CL
CM
UID
No
Baro
Temp
Humidity
kW
@
Power
%
CF
@
Power
kPa
K
kg/
kg
­­­­­­­­­­­­­­­­­­­
Ambient­­­­­­­­­­­­­­­­­­­­­

­­­­­­­­­­­­­­­­­­­
Loads­­­­­­­­­­­­­­­­­­­

Power
Extraction
­­­
Stage
Bleed­­­

353
354
355
356
357
358
359
360
361
362
363
364
365
366
2RR026
0
­
0
­
100.2
287
.00527
­
.00886
2RR027
0
­
0
­
100.2
287
.00527
­
.00886
5RR040
0
­
0
­
100.2
287
.0053
­
.0089
1TL001
0
­
20
9.49kN
101.7
290
­
300
0.0094­
0.0184
1TL002
0
­
20
8.41kN
101.3­
102.4
288
­
293
0.0088­
0.0108
1TL003
0
­
20
8.81kN
101.3­
102.4
288
­
293
0.0088­
0.0108
1TL004
0
­
20
9.41kN
101.3­
102.4
276
­
280
0.0023­
0.0038
1ZM001
0
­
0
­
99.9­
101.5
268
­
295
0.0017­
0.0083
Filename
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ARP.
xls
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Data
1
2
3
CN
CO
CP
CQ
CR
CS
UID
­­­
Test
Dates­­­

No
Manufacturer
Test
Organisation
Test
Location
From
To
353
354
355
356
357
358
359
360
361
362
363
364
365
366
2RR026
Rolls
Royce
plc
Rolls
Royce
plc
SINFIN,
Derby
Sep­
94
­

2RR027
Rolls
Royce
plc
Rolls
Royce
plc
SINFIN,
Derby
Sep­
94
­

5RR040
Rolls­
Royce
plc
Rolls­
Royce
plc
SINFIN,
Derby
Sep­
94
1TL001
Textron
Lycoming
Textron
Lycoming
Stratford,
CT
26­
Jul­
82
21­
Sep­
82
1TL002
Textron
Lycoming
Textron
Lycoming
Stratford,
CT
7­
Sep­
82
20­
Sep­
82
1TL003
Textron
Lycoming
Textron
Lycoming
Stratford,
CT
26­
Jul­
82
21­
Sep­
82
1TL004
Textron
Lycoming
Textron
Lycoming
Stratford,
CT
19­
Dec­
90
20­
Dec­
90
1ZM001
ZMKB
ZMKB
Zaporoje
17­
May­
84
10­
Dec­
84
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Data
1
2
3
CT
CU
UID
No
Remarks
353
354
355
356
357
358
359
360
361
362
363
364
365
366
2RR026
Data
from
certification
report
DNS
14445
2RR027
Data
from
certification
report
DNS
30699
5RR040
1.
Data
from
certification
report
DNS59304
1TL001
1TL002
1TL003
Calculated
using
L­
2
and
R­
3
data
+
L5
performance
1TL004
1ZM001
­

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ARP.
xls
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Data
1
2
3
CV
CW
CX
CY
CZ
DA
DB
DC
DD
DE
DF
DG
DH
353
354
355
356
357
358
359
360
361
362
363
364
365
366
Filename
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ARP.
xls
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Data
1
2
3
DI
DJ
DK
DL
DM
DN
353
354
355
356
357
358
359
360
361
362
363
364
365
366
Filename
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ARP.
xls
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Column
Description
Column
Heading
Full
Description
if
different
from
heading
A
UID
No
Unique
Identification
Number
B
Engine
Identification
C
Combustor
Type
of
combustor
where
more
than
one
type
available
on
an
engine.

D
Eng
Type
Engine
type.
TF
=
turbofan,
MTF
=
mixed
turbofan
E
B/
P
ratio
Bypass
ratio
F
Press
ratio
Engine
pressure
ratio
G
Rated
Output,
kN
Engine
maximum
rated
thrust,
in
kilonewtons
H
UID
No
Unique
Identification
Number
I
Data
type
­
PR
Data
generated
prior
to
regulations
being
applied
J
Data
Type
­
C
Certification
data
K
Data
Type
­
R
Data
revised
by
manufacturer
after
initial
submission.

L
Data
superseded
Data
for
which
a
revised
set
has
been
supplied
(
data
row
shaded
mid­
grey)

M
Superseded
by
UID
NO
UID
of
data
which
replaced
the
superseded
data
N
Data
source
­
NME
Data
from
newly
manufactured
engines
O
Data
Source
­
DTEPS
Data
from
dedicated
test
engines
to
production
standards
P
Other
Data
from
engines
other
than
NME
or
DTEPS.
See
remarks
on
engine
data
sheet.

Q
Data
corr
as
Annex
16
The
emissions
data
has
been
corrected
according
to
ICAO
Annex
16,
Vol
2,
Part
III,
Appendix
3.

R
Out
of
production
Engine
which
the
manufacturer
has
confirmed
is
no
longer
produced
(
data
row
shaded
light
grey)

S
Date
Date
on
which
the
engine
ceased
to
be
produced
T
Out
of
service
Engine
which
the
manufacturer
has
confirmed
is
no
longer
in
service
(
data
row
shaded
very
dark
grey)

U
Date
Date
on
which
the
engine
ceased
to
be
in
service
V
UID
No
Unique
Identification
Number
W
EI
HC
T/
O
Hydrocarbon
emission
index
(
g/
kg)
at
take
off
condition
X
EI
HC
C/
O
Hydrocarbon
emission
index
(
g/
kg)
at
climb
out
condition
Y
EI
HC
App
Hydrocarbon
emission
index
(
g/
kg)
at
approach
condition
Z
EI
HC
Idle
Hydrocarbon
emission
index
(
g/
kg)
at
idle
condition
AA
Number
test
Number
of
tests
done
for
hydrocarbon
AB
Number
eng
Number
of
engines
tested
for
hydrocarbon
AC
Dp/
Foo
(
HC)
average
Hydrocarbon
Dp/
Foo
(
g/
kN)
average
AD
Dp/
Foo
(
HC)
Sigma
Hydrocarbon
Dp/
Foo
(
g/
kN)
standard
deviation
AE
Dp/
Foo
(
HC)
range
Hydrocarbon
Dp/
Foo
(
g/
kN)
range
AF
Dp/
Foo
(
HC)
Characteristic
Hydrocarbon
characteristic
Dp/
Foo
value
AG
Characteristic
%
of
Reg
limit
The
characteristic
Dp/
Foo
value
expressed
as
a
percentage
of
the
regulatory
limit.

AH
LTO
total
mass
(
g)
The
total
mass
of
hydrocarbons
emitted
during
the
LTO
cycle
(
sum
of
time
in
mode
x
fuel
flow
x
average
EI
at
each
of
the
four
power
settings).

AI
UID
No
Unique
Identification
Number
AJ
EI
CO
T/
O
Carbon
Monoxide
emission
index
(
g/
kg)
at
take
off
condition
AK
EI
CO
C/
O
Carbon
Monoxide
emission
index
(
g/
kg)
at
climb
out
condition
AL
EI
CO
App
Carbon
Monoxide
emission
index
(
g/
kg)
at
approach
condition
AM
EI
CO
Idle
Carbon
Monoxide
emission
index
(
g/
kg)
at
idle
condition
AN
Number
test
Number
of
tests
done
for
carbon
monoxide
AO
Number
eng
Number
of
engines
tested
for
carbon
monoxide
AP
Dp/
Foo
(
CO)
Average
Carbon
monoxide
Dp/
Foo
(
g/
kN)
average
AQ
Dp/
Foo
(
CO)
Sigma
Carbon
monoxide
Dp/
Foo
(
g/
kN)
standard
deviation
AR
Dp/
Foo
(
CO)
range
Carbon
monoxide
Dp/
Foo
(
g/
kN)
range
AS
Dp/
Foo
(
CO)
characteristic
Carbon
monoxide
characteristic
Dp/
Foo
value
AT
Characteristic
%
of
Reg
limit
The
characteristic
Dp/
Foo
value
expressed
as
a
percentage
of
the
regulatory
limit.

AU
LTO
total
mass
(
g)
The
total
mass
of
carbon
monoxide
emitted
during
the
LTO
cycle
(
sum
of
time
in
mode
x
fuel
flow
x
average
EI
at
each
of
the
four
power
settings).

AV
UID
No
Unique
Identification
Number
AW
EI
NOx
T/
O
Oxides
of
nitrogen
emission
index
(
g/
kg)
at
take
off
condition
AX
EI
CO
C/
O
Oxides
of
nitrogen
emission
index
(
g/
kg)
at
climb
out
condition
AY
EI
NOx
App
Oxides
of
nitrogen
emission
index
(
g/
kg)
at
approach
condition
AZ
EI
NOx
Idle
Oxides
of
nitrogen
emission
index
(
g/
kg)
at
idle
condition
BA
Number
test
Number
of
tests
done
for
oxides
of
nitrogen
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
Column
Description,
Page
148
of
151.
www.
QinetiQ.
com/
aviation_
emissions_
databank
Column
Description
Column
Heading
Full
Description
if
different
from
heading
BB
Number
eng
Number
of
engines
tested
for
oxides
of
nitrogen
BC
Dp/
Foo
(
NOx)
Average
Oxides
of
nitrogen
Dp/
Foo
(
g/
kN)
average
BD
Dp/
Foo
(
NOx)
Sigma
Oxides
of
nitrogen
Dp/
Foo
(
g/
kN)
standard
deviation
BE
Dp/
Foo
(
NOx)
range
Oxides
of
nitrogen
Dp/
Foo
(
g/
kN)
range
BF
Dp/
Foo
(
NOx)
characteristic
Oxides
of
nitrogen
characteristic
Dp/
Foo
value
BG
Characteristic
as
%
of
standard
­
original
The
characteristic
Dp/
Foo
value
expressed
as
a
percentage
of
the
original
NOx
regulatory
limit
(
see
part
a
of
the
NOx
regulatory
standards
in
section
7
of
Background).

BH
Characteristic
as
%
of
standard
­
CAEP
2
The
characteristic
Dp/
Foo
value
expressed
as
a
percentage
of
the
CAEP/
2
NOx
regulatory
limit
(
see
part
b
of
the
NOx
regulatory
standards
in
section
7
of
Background).

BI
Characteristic
as
%
of
standard
­
CAEP
4
The
characteristic
Dp/
Foo
value
expressed
as
a
percentage
of
the
CAEP/
4
NOx
regulatory
limit
(
see
part
c
of
the
NOx
regulatory
standards
in
section
7
of
Background).

BJ
LTO
total
mass
(
g)
The
total
mass
of
oxides
of
nitrogen
emitted
during
the
LTO
cycle
(
sum
of
time
in
mode
x
fuel
flow
x
average
EI
at
each
of
the
four
power
settings).

BK
UID
No
Unique
Identification
Number
BL
Smoke
Number
T/
O
Smoke
number
at
take
off
condition
BM
Smoke
Number
C/
O
Smoke
number
at
climb
out
condition
BN
Smoke
Number
App
Smoke
number
at
approach
condition
BO
Smoke
Number
idle
Smoke
number
at
idle
condition
BP
Number
test
Number
of
tests
done
for
smoke
BQ
Number
eng
Number
of
engines
tested
for
smoke
BR
Smoke
Number
Max
Maximum
smoke
number
measured
BS
Smoke
Number
sigma
Smoke
number
standard
deviation
BT
Smoke
Number
range
BU
Smoke
Number
characteristic
BV
Characteristic
%
of
Reg
limit
The
characteristic
smoke
number
value
expressed
as
a
percentage
of
the
regulatory
limit.

BW
UID
No
Unique
Identification
Number
BX
Fuel
Spec
Fuel
specification
BY
Fuel
H/
C
ratio
Ratio
of
hydrogen
atoms
to
carbon
atoms
in
the
fuel
BZ
Fuel
Arom
%
Percentage
of
aromatic
hydrocarbons
in
the
fuel
CA
Fuel
flow
T/
O
Fuel
flow
(
kg/
sec)
at
take
off
condition
CB
Fuel
flow
C/
O
Fuel
flow
(
kg/
sec)
at
climb
out
condition
CC
Fuel
flow
App
Fuel
flow
(
kg/
sec)
at
approach
condition
CD
Fuel
Flow
Idle
Fuel
flow
(
kg/
sec)
at
idle
condition
CE
Fuel
per
LTO
cycle
(
kg)
kg
of
fuel
used
during
the
LTO
cycle.

CF
UID
No
Unique
Identification
Number
CG
Loads
Power
extraction
kW
Load
extracted
during
tests
CH
Loads
Power
extraction
@
Power
Power
setting
at
which
load
extracted
CI
Loads
Stage
bleeds
­
%
CF
%
core
flow
taken
as
stage
bleeds
CJ
Loads
Stage
bleeds
@
power
Power
setting
at
which
stage
bleeds
taken
CK
Ambient
Baro
CL
Ambient
temp
CM
Ambient
Humidity
Ambient
humidity
in
kg
water
per
kg
dry
air
CN
UID
No
Unique
Identification
Number
CO
Manufacturer
Engine
manufacturer
CP
Test
organization
CQ
Test
location
CR
Test
dates
from
CS
Test
dates
to
CT
UID
No
Unique
Identification
Number
CU
Remarks
Filename
DCTM_
ARP.
xls
Printed
on
5/
20/
05
Check
website
for
latest
version
Column
Description,
Page
149
of
151.
www.
QinetiQ.
com/
aviation_
emissions_
databank