# V2500

- ENG

- 72

- A 0615

Page 1 of 2

IAE PROPRIETARY INFORMATION

© IAE International Aero Engines AG (date as above). All right reserved.

Not Subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3). 

# ALERT SERVICE BULLETIN REVISI O N N O TICE

N O N

- M O D I F I C A

TI ON SE R V I C E BULL E TI N

— E N G I N E

— H I GH P R ESS UR E ( H P)

C O M P R ESSOR

— S T A GE 3 T O 8 C O M P R ESSOR DRU M

— UL T R A SO N I C I N SPE C TI ON

( U S I ) F OR S T R ESS C O RR OS I ON CR A CK I N G



# Tu r bo j et E ng i ne A l

e r t S e r v i ce B u ll

e ti n N o. V 250 0

- EN G

- 72

- A 0615

R e v i s i on N o. 6 da t ed September 4

, 2014.

Rev i s i on H i s t ory

Or i g i nal I ssue Ju l y 19, 2010

Rev i s i on 1 da t ed A ugust 2, 2010

Rev i s i on 2 da t ed Nove m ber 24, 2010

Rev i s i on 3 da t ed S ep t e m ber 20, 2011

Rev i s i on 4 da t ed M ay 2, 2013

Rev i s i on 5 da t ed A ugu st 5, 2014

Rev i s i on 6 da t ed September 4

, 2014

Reason for t he Rev i s i on

For Revision 5:

To rev i se t he E ng i ne E ffec ti v it y and Co m p li ance i n t he Pl ann i ng I nfor m a ti on section

. To add A dd iti onal I ns t ruc ti on.

To add A cco m p li sh m ent P rofor m a Tab l e i n t he A cco m p li sh m ent I ns t ruc ti ons.

To add M a t er i al Da t a Tab l e for A 1 /A 5 / D5 E ng i ne m ode l s.

To de l e t e F A A Ai r w or t h i ness D i rec ti ve Nu m ber i n References.

For Revision 6:

To correct the A319 Engine Effectivity Data

To correct the group A Time Compliance Table.

To update Group C Engine Serial Numbers.

To correct the initial issue date of th is Service Bulletin.

E ffect of Rev i s i on on P r i or Co m p li ance

None.

# V2500

- ENG

- 72

- A 0615

Page 2 of 2

IAE PROPRIETARY INFORMAT ION

© IAE International Aero Engines AG (date as above). All right reserved.

Not Subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3). 

## Th i s i s a Co m p l e t e Rev i s i on (Not A pp li cab l e t o t he S G M L vers i on)

The for m at of t h i s S erv i ce B u ll e ti n has been changed from prev i ous vers i ons. Th i s rev i s i on sho w s

f l ow bars and t he rev i s i on da t e on t he bo tt om of every page. Techn i cal changes i ncorpora t ed i n t h i s

rev i s i on are m arked w it h rev i s i on bars. The c on t en t s are i n accordance w it h t he li st of effec ti ve

pages.

MODEL APPLICATION

V2500

- A1, V2522

- A5, V2524

- A5, V2527

- A5, V2527E

- A5, V2527M

- A5, V2530

- A5, V2533

- A5, V2525

- D5, V2528

- D5

BULLETIN ISSUE SEQUENCE

V2500 Series 72

- A0615



### A copy of this Revision Notice and any future revision notices must be filed as a permanent

record with your copy of the subject bulletin.

### January 

### 19/10

REVISION NO. 6

– September 04 /14 

# V2500

- ENG

- 72

- A 0615

IAE PROPRIETARY INFORMATION Page 1 of 23

© IAE International Aero Engines AG (date as above). All r ights reserved. 

# ALERT SERVICE BULL ETIN

NON

- MODIFICATION SERVICE BULLETIN

— ENGINE

— HIGH PRESSURE (HP)

COMPRESSOR

— STAGE 3 TO 8 COMPRESSOR DRUM

— ULTRASONIC INSPECTION

(USI) FOR STRESS CORROSION CRACKING

M ODEL APPLICATION

V 2500

- A 1, V 2522

- A 5, V 2524

- A 5, V 2527

- A 5, V 2527 E

- A 5, V 2527 M

- A 5, V 2530

- A 5,

V 2533

- A 5, V 2525

- D5, V 2528

- D5

B ULL E T I N ISS UE SE QU E NCE

V 2500 S er i es 72

- A 0615

A TA NU M BE R

72

- 41

- 11

IA E P RO P R IE T A RY I NFOR M A T I ON

Th i s docu m ent i s t he proper t y of I n t erna ti onal A ero E ng i nes ( IAE ). Y ou m ay not possess, use, copy

or d i sc l ose t h i s docu m ent or any i nfor m a ti on i n it

, for any purpose, i nc l ud i ng w it hout li m it a ti on t o

des i gn, m anufac t ure, or repa i r par t s, or ob t a i n F A A or o t her govern m ent approval t o do so, w it hout

IAE 's e x press w r itt en per m i ss i on. Ne it her rece i pt nor possess i on of t h i s docu m ent a l one, from any

source, cons tit u t es such per m i ss i on. P ossess i on, use, cop y i ng or d i sc l osure by an y one w it hout IAE 's

e x press w r itt en per m i ss i on i s not au t hor i z ed and m ay resu l t i n cr i m i nal and / or c i v i l li ab ilit y

.

Not Subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3).



## Compliance Ca t egory

3

### January 

### 19/10

REVISION NO. 6

– September 04 /14 

# V2500

- ENG

- 72

- A 0615

IAE PROPRIETARY INFORMATION Page 2 of 23

© IAE International Aero Engines AG (date as above). All rights reserved.

Not Subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3). S u mm ary

The purpose of t h i s S erv i ce B u ll e ti n i s t o pr ov i de U lt rason i c I nspec ti on (U SI ) t hresho l ds of t he HP co m pressor St age 8

d i sk t o be carr i ed out "I n

- S erv i ce" and "A t Overhau l"

. Cracks w ere h i gh li gh t ed dur i ng an E ng i ne M anual crack i nspec ti on

of t he St age 7

- 8 d i sk i n t ernal cav it y

.

1. Pl ann i ng I nfor m a ti on

A. E ffec ti v it y Da t a

(1) Airbus A319

(a) V 2522

- A 5, V 2524

- A 5, V 2527 M

- A 5 Engines from Serial No. V10001 to Serial No.

V13190.

(b) V 2522

- A 5, V 2524

- A 5, V 2527 M

- A 5 Engines from Serial No. V1 5 001 to Serial No.

V16728 except Serial No. V16707

(2) Airbus A320

(a) V2500

- A1 Engine Serial No. V0001 to Serial No. V0361

(b) V2527

- A5, V2527E

- A5 Engines from Serial No. V10001 to Serial No. V13190.

(c) V2527

- A5, V2527E

- A5 Engines from Serial No. V15001 to Serial No. V16728 except Serial No. V16707.

(3) Airbus A321

(a) V2530

- A5, V2533

- A5 Engines from Serial No. V10001 to Serial No. V13190.

(b) V2530

- A5, V2533

- A5 Engines from Serial No. V15001 to Serial No. V16728 except Serial No. V16707.

(4) Boeing MD

- 90

( a) V2525

- D5, V2528

- D5 Engines from Serial No. V20001 to Serial No.V20285

Note : For an eng i ne not t o requ i re an U lt rason i c I nspec ti on (U SI ) i n accordance w it h t h i s Non

-

M od i f i ca ti on S erv i ce B u ll e ti n, t he cond iti on t hat fo ll o w s m ust be ach i eved:

The eng i ne m ust have i ns t a ll ed a HP Co m pressor St age 3

- 8 Drum A sse m b l y (72

- 41

- 11

- 01

- 200)

t hat has never opera t ed w it h P re S erv i ce B u ll e ti n V 2500

- E NG

- 72

- 0632

(72

- 41

- 12, 01

- 602) s t andard nu t s.

B. Concurrent Requ i re m en t s

The Non

- Modification Service Bulletin that follows must be done at the same time as this one:

V 2500

- E NG

- 72

- 0638.

NON

- MODIFICATION SERVICE BULLETIN

- ENGINE

- HIGH PRESSURE (HP) COMPRESSOR

- STAGE 3 TO 8 COMPRESSOR DRUM

- ULTRASONIC INSPECTION PROCEDURE (USI)

C Reason

(1) Cond iti on:

Cracks have been found on t he H i gh P ressure (H P ) co m pressor St age 3

- 8 drum asse m b l y dur i ng

overhau l

.

### January 

### 19/10

REVISION NO. 6

– September 04 /14 

# V2500

- ENG

- 72

- A 0615

IAE PROPRIETARY INFORMATION Page 3 of 23

© IAE International Aero Engines AG (date as above). All rights reserved.

Not Subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3). (2) B ackground:

Cracks w ere h i gh li gh t ed dur i ng an E ng i ne M anual crack i nspec ti on of t he St age 7

- 8 d i sk i n t ernal cav it y

.

(3) Ob j ec ti ve:

To def i ne U lt rason i c I nspec ti on (U SI ) t hresho l ds of t he HP co m pressor St age 8 d i sk t o be carr i ed out "I n

-

S erv i ce" and "A t Overhau l"

.

(4) S ubs t an ti a ti on:

Cracks have been found on t he HP co m presso r St age 3

- 8 drum asse m b l y dur i ng overhau l

. I nspec ti ons ( E ddy

Curren t

, F l uorescent P ene t rant and U lt rason i c) have been deve l oped and have sho w n t he capab ilit y of

de t ec ti ng cracks "I n

- S erv i ce" and "A t Overhau l"

.

(5) E ffec t s of B u ll e ti n on:

(a) Re m ov a l/I ns t a ll a ti on:

Not affec t ed.

(b) D i sasse m b l y

/A sse m b l y :

Not affec t ed.

(c) C l ean i ng:

Not affec t ed.

(d) I nspec ti on / Check:

Not affec t ed.

(e) Repa i r:

Not affec t ed.

(f) Tes ti ng:

Not affec t ed.

(6) S upp l e m en t al I nfor m a ti on

None.

D. Descr i p ti on

Th i s Non

- M od i f i ca ti on S erv i ce B u ll e ti n i den ti f i es t he t hresho l ds and i n t erva l s for t he U S I i nspec ti on of t he HP

co m pressor St age 8 d i sk i nner cav it y for t he eng i nes li s t ed under E ffec ti v it y t o be acco m p li shed i n accordance w it h

Reference 6

, Non

- M od i f i ca ti o n S erv i ce B u ll e ti n V 2500

- E NG

- 72

- 0638 i n iti al i ssue or l a t er approved rev i s i on.

E. Co m p li ance

Ca t egory 3

### January 

### 19/10

REVISION NO. 6

– September 04 /14 

# V2500

- ENG

- 72

- A 0615

IAE PROPRIETARY INFORMATION Page 4 of 23

© IAE International Aero Engines AG (date as above). All rights reserved.

Not Subject to the EAR per 15 C.F.R. Cha pter 1, Part 734.3(b)(3). Note : The co m p li ance paragraph i s d i v i ded i n t o s i x groups (A t o F). For i nd i v i dual app li cab ilit y and t he

resu lti ng u lt rason i c i nspec ti on s t ar t

, t hresho l d and i nspec ti on i n t erva l

, refer t o t he group descr i p ti on.

Note : A dd iti ona ll y

, IA E offers Grace P er i ods t hat can i n t errup t/ de l ay t he U lt rason i c I nspec ti on (U SI ) for an

app li cab l e dru m

, i f t he drum i s c l eaned, F l uorescent P ene t rant I nspec t ed (F PI ) and / or E ddy Current

I nspec t ed ( E C I ) at overhau l

. Refer t o t he grace per i od t ab l e be l ow t he co m p li ance ti m e t ab l e for

app li cab ilit y

.

The I nspec ti on i n t erval re m a i ns as i ns t ruc t ed i n t he app li cab l e Co m p li ance T i m e t ab l e, once t he Grace

P er i od i s e x haus t ed.

### January 

### 19/10

REVISION NO. 6

– September 04 /14 

# V2500

- ENG

- 72

- A 0615

IAE PROPRIETARY INFORMATION Page 5 of 23

© IAE International Aero Engines AG (date as above). All rights reserved.

Not Subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3). Group A:

V 2500

- A 1 E ng i nes V 0008, V 0013, V 0026, V 0050, V 0052, V 0064, V 0068, V 0070, V 0073, V 0077, V 0080,

V 0087, V 0094, V 0105, V 0109, V 0114, V 0116, V 0125, V 0145, V 0149, V 0150, V 0151, V 0158, V 0160,

V 0180, V 0197, V 0200, V 0220, V 0221, V 0222, V 0228, V 0233, V 0236, V 0243, V 0244, V 0252, V 0281,

V 0296, V 0297, V 0298, V 0299, V 0303, V 0306, V 0309, V 0312, V 0329, V 0338, V 0342, V 0350, V 0352,

V 0354, V 0355, V 0356 and V 0358.

HP Co m pressor St age 3

- 8 Drum A sse m b l y P Ns: P N 6 A 8236, P N 6 A 8318, P N 6 B 1401, P N 6 B 1403 and

P N 6 B 1406 (T i 6246 Drum M a t er i a l ).

Co m p li ance T i m e Tab l e:

I nspec ti on

l oca ti on HP co m pressor

3

- 8 Drum c y c l es

s i nce new Thresho l d From Regu l ar Repeat

I nspec ti on

I n t erval

Outer and Inner

Diameters >8000 A cco m p li sh w it h i n

200 c y c l es. Da t e of Rev i s i on 6 of

Non

- M od i f i ca ti on S erv i ce

B u ll e ti n V 2500

- E NG

- 72

-

A 0615. Not m ore t han

750 c y c l es.

<=8000 A cco m p li sh w it h i n 200

c y c l es of t he drum

reach i ng 8000 c y c l es.

### January 

### 19/10

REVISION NO. 6

– September 04 /14 

# V2500

- ENG

- 72

- A 0615

IAE PROPRIETARY INFORMATION Page 6 of 23

© IAE International Aero Engines AG (date as above). All rights reserved.

Not Subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3). Grace P er i ods Tab l e:

Co m p li ance

Group Nu t/ Drum St andard Requ i red Drum Cond iti on P er m itt ed

Grace P er i od

(C y c l es)

A For dru m s t hat w ere f itt ed

w it h any s t andard of nut Reference 1, E ng i ne M anua l

, T AS K 72

- 41

- 11

- 110

- 001

(C l ean)

Reference 1, E ng i ne M anua l

, T AS K 72

- 41

- 11

- 200

- 001 (F PI ) 4000

Reference 1, E ng i ne M anua l

, T AS K 72

- 41

- 11

- 110

- 001

(C l ean)

Reference 1, E ng i ne M anua l

, T AS K 72

- 41

- 11

- 200

- 001 (F PI )

Reference 3, Non

- M od i f i ca ti on S erv i ce B u ll e ti n V 2500

- E NG

72

- 0625 ( E C I ) 5000

For dru m s t hat w ere

f itt ed w it h Reference 4,

V 2500

- E NG

- 72

- 0632

initial issue, dated

Dece m ber 20 t h 2012 or

l a t er approved rev i s i on Refe rence 1, E ng i ne M anua l

, T AS K 72

- 41

- 11

- 110

- 001

(C l ean)

Reference 5, Non

- M od i f i ca ti on S erv i ce B u ll e ti n

V 2500

- E NG

- 72

- 0637 ( E nhanced F PI ) 6000

Reference 1, E ng i ne M anua l

, T AS K 72

- 41

- 11

- 110

- 001

(C l ean)

Reference 5, Non

- M od i f i ca ti on S erv i ce B u ll e ti n

V 2500

- E NG

- 72

- 0637 ( E nhanced F PI )

Reference 3, Non

- M od i f i ca ti on S erv i ce B u ll e ti n

V 2500

- E NG

- 72

- 0625 ( E C I ) 8000

### January 

### 19/10

REVISION NO. 6

– September 04 /14 

# V2500

- ENG

- 72

- A 0615

IAE PROPRIETARY INFORMATION Page 7 of 23

© IAE International Aero Engines AG (date as above). All rights reserved.

Not Subject to the EAR per 15 C. F.R. Chapter 1, Part 734.3(b)(3). I nspec ti on

l oca ti on HP co m pressor

3

- 8 Drum c y c l es

s i nce new Thresho l d From Regu l ar Repeat

I nspec ti on

I n t erval

Ou t er and I nner

D i a m e t ers >8000 A cco m p li sh w it h i n 200

c y c l es. Da t e of Rev i s i on 6 of

Non

- M od i f i ca ti on S erv i ce

B u ll e ti n V 2500

- E NG

- 72

-

A 0615. Not m ore t han

750 c y c l es. <=8000 A cco m p li sh w it h i n 200

c y c l es of t he drum

reach i ng 8000 c y c l es. Group B :

V 2500

- A 1 E ng i nes V 0023, V 0024, V 0027, V 0028, V 0030, V 0036, V 0038, V 0043, V 0044, V 0045, V 0056,

V 0057, V 0059, V 0062, V 0063, V 0071, V 0072, V 0074, V 0079, V 0082, V 0092, V 0095, V 0097, V 0098, V 0100,

V 0102, V 0107, V 0108, V 0117, V 0118, V 0133, V 0134, V 0140, V 0198, V 0224, V 0234, V 0238, V 0257, V 0270,

V 0271, V 0272, V 0273, V 0278, V 0279, V 0280, V 0282, V 0290, V 0304, V 0307, V 0308, V 0330, V 0341

, V 0345,

V 0346, V 0353, V 0357, V 0359 and V 0360.

HP compressor stage 3

- 8 drum assembly P/Ns: 6A2030, 6A2355, 6A2455, 6A2645, 6A3508, 6A3648, 6A3934, 6A3936,

6A4189, 6A5467, 6A5592, 6A5594, 6A5659, 6A6473, 6A7379, 6A7380, 6A7382, 6A7384, 6A7385, 6A7401

, 6A8 350,

6B1379, 6B1380, 6B1381, 6B138 2, 6B1383, 6B1384 and 6B1402 ( Ti5331 Drum Material).

Co m p li ance T i m e Tab l e:

### January 

### 19/10

REVISION NO. 6

– September 04 /14 

# V2500

- ENG

- 72

- A 0615

IAE PROPRIETARY INFORMATION Page 8 of 23

© IAE International Aero Engines AG (date as above). All rights reserved.

Not Subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3). Grace P er i ods Tab l e:

Co m p li ance

Group Nu t/ Drum St andard Requ i red Drum Cond iti on P er m itt ed

Grace P er i od

(C y c l es)

For dru m s t hat w ere

f itt ed w it h any

s t andard of nu t

. Reference 1, E ng i ne M anua l

, T AS K 72

- 41

- 11

- 110

- 001

(C l ean)

Reference 1, E ng i ne M anua l

, T AS K 72

- 41

- 11

- 200

- 001 (F PI ) 2000

B Reference 1, E ng i ne M anua l

, T AS K 72

- 41

- 11

- 110

- 001

(C l ean)

Reference 1, E ng i ne M anua l

, T AS K 72

- 41

- 11

- 200

- 001 (F PI )

Reference 3, Non

- M od i f i ca ti on S erv i ce B u ll e ti n V 2500

- E NG

72

- 0625 ( E C I ) 5000

For dru m s t hat w ere

f itt ed w it h Reference

4

,

V 2500

- E NG

- 72

- 0632

i n iti al i ssue, da t ed

Dece m ber 20 t h 2012

or l a t er app roved

rev i s i on Reference 1, E ng i ne M anua l

, T AS K 72

- 41

- 11

- 110

- 001

(C l ean)

Reference 5, Non

- M od i f i ca ti on S erv i ce B u ll e ti n

V 2500

- E NG

- 72

- 0637 ( E nhanced F PI ) 5000

Reference 1, E ng i ne M anua l

, T AS K 72

- 41

- 11

- 110

- 001

(C l ean)

Reference 5, Non

- M od i f i ca ti on S erv i ce B u ll e ti n

V 2500

- E NG

- 72

- 0637 ( E nhanced F PI )

Reference 3, Non

- M od i f i ca ti on S erv i ce B u ll e ti n

V 2500

- E NG

- 72

- 0625 ( E C I ) 8000

### January 

### 19/10

REVISION NO. 6

– Sep tember 04 /14 

# V2500

- ENG

- 72

- A 0615

IAE PROPRIETARY INFORMATION P age 9 of 23

© IAE International Aero Engines AG (date as above). All rights reserved.

Not Subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3). Group C:

V 2500

- A 5 E ng i nes V 10001, V 10005, V 10096, V 10101, V 10102, V 10103, V 10195, V 10196, V 10204,

V 10341, V 104 75, V 10478, V 10481, V 10490, V 10518, V 10519, V 10937, V 11009, V 11475, V 11482,

V 11516, V 11521, V 11788, V 11848, V 11849, V 11871, V 11879, V 11884, V 11899, V 11904, V 11917,

V 11937, V 11978, V 11980, V 11982, V 11999, V 12000, V 12002, V 12037, V 12038, V 12044, V 12116,

V 121 20, V 12122, V 12129, V 12131, V 12140, V 12142, V 12148, V 12150, V 12166, V 12168, V 12171,

V 12174, V 12178, V 12223, V 12227, V 12242, V 12252, V 12270, V 12289, V 12294, V 12314, V 12327,

V 12330, V 12331, V 12333, V 12340, V 12342, V 12345, V 12346, V 12354, V 12377, V 12379, V 123 89,

V 12391, V 12394, V 12396, V 12400, V 12404, V 12408, V 12412, V 12414, V 12416, V 12420, V 12425,

V 12427, V 12432, V 12443, V 12445, V 12447, V 12449, V 12451, V 12477, V 12479, V 12480, V 12488,

V 12489, V 12495, V 12524, V 12539, V 12541, V 12543, V 12554, V 12569, V 12573, V 125 75, V 12576,

V 12586, V 12601, V 12603, V 12622, V 12646, V12654, V 12668, V 12703, V 12705, V 12721, V 12723,

V 12725, V 12758, V 12774, V 12793, V 12795, V 12809, V 12813, V12849, V12851, V 12879, V 12881,

V 12884, V 12888, V 12921, V 12930, V 12968, V 13071, V 13124, V 13137, V 131 70, V 13184, V 13186,

V 13187, V 15003, V15006, V 15007, V 15009, V 15033, V 15050, V 15104, V 15111, V 15161, V 15162,

V 15168, V 15191, V 15207, V 15216, V 15226, V15253, V15300, V 15304, V 15347, V 15349, V 15453,

V 15465, V15469, V 15508, V 15518, V 15530, V 15531, V 15537, V 156 02, V 15610, V 15620, V 15622,

V 15633, V 15635, V 15652, V 15653, V 15676, V 15678, V 15680, V 15702, V 15726, V 15728, V 15731,

V 15732, V 15738, V 15765, V 15768, V 15770, V 15805, V 15865, V 15866, V 15867, V 15872, V 15873,

V 15918, V 15920, V 15924, V 15926, V 15949, V 15951, V 159 76, V 15985, V 15986, V 15996, V 15998,

V 16000, V 16002, V 16034, V 16035, V 16057, V 16061, V 16085, V 16090, V 16091, V 16113, V 16117,

V 16129, V 16130, V 16171, V 16173, V 16177, V 16179, V 16185, V 16187, V 16190, V 16191, V 16193,

V 16237, V 16238, V 16290, V 16292, V 16321, V 163 22, V 16340, V 16341, V 16363, V 16366, V 16378,

V 16379, V 16400, V 16401, V 16418, V 16419, V 16430, V 16431, V 16478, V 16493, V 16515, V 16516,

V 16535, V 16553, V 16554, V 16556, V 16599, V 16602, V 16603, V 16615, V 16617, V 16618, V 16666,

V 16667, V 16684 and V 16685.

HP Co m p ressor St age 3

- 8 Drum A sse m b l y P Ns: P N 6 A 7705, P N 6 A 8236, P N 6 A 8316, P N 6 B 1385, P N

6 B 1386, P N 6 B 1392, P N 6 B 1393, P N 6 B 1404 and P N 6 B 1405 (T i 6246 Drum M a t er i a l ).

Co m p li ance T i m e Tab l e:

I nspec ti on

l oca ti on HP co m pressor

3

- 8 Drum c y c l es

s i nce new Thresho l d From Regu l ar Repeat

I nspec ti on

I n t erval

Ou t er and I nner

D i a m e t ers >6250 A cco m p li sh

w it h i n 200 c y c l es. Da t e of Rev i s i on 6 of

Non

- M od i f i ca ti on S erv i ce

B u ll e ti n V 2500

- E NG

- 72

-

A 0615. Not m ore t han

750 c y c l es.

<=6250 A cco m p li s h w it h i n 200

c y c l es of t he drum

reach i ng 6250 c y c l es.

### January 

### 19/10

REVISION NO. 6

– September 04 /14 

# V2500

- ENG

- 72

- A 0615

IAE PROPRIETARY INFORMATION Page 10 of 23

© IAE International Aero Engines AG (date as above). All ri ghts reserved.

Not Subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3). Grace P er i ods Tab l e :

Co m p li ance

Group Nu t/ Drum St andard Requ i red Drum Cond iti on P er m itt ed

Grace P er i od

(C y c l es)

C For dru m s t hat w ere

f itt ed w it h any

s t andard of nu t

. Refe rence 1, or Reference 2

, E ng i ne M anua l

, T AS K 72

- 41

-

11

- 110

- 001 (C l ean)

Reference 1, or Reference 2

, E ng i ne M anua l

, T AS K 72

- 41

-

11

- 200

- 001 (F PI ) 4000

Reference 1, or Reference 2

, E ng i ne M anua l

, T AS K 72

- 41

-

11

- 110

- 001 (C l ean)

Reference 1, or Reference 2

, E ng i ne M anua l

, T AS K 72

- 41

-

11

- 200

- 001 (F PI )

Reference 3, Non

- M od i f i ca ti on S erv i ce B u ll e ti n V 2500

- E NG

72

- 0625 ( E C I ) 5000

For dru m s t hat w ere

f itt ed w it h Reference 4

,

V 2500

- E NG

- 72

- 0632

i n iti al i ssue, da t ed

Dece m ber 20 t h 2012 or

l a t er approved rev i s i on Reference 1, or Reference 2

, E ng i ne M anua l

, T AS K 72

- 41

-

11

- 110

- 001 (C l ean)

Reference 5, Non

- M od i f i ca ti on S erv i ce B u ll e ti n

V 2500

- E NG

- 72

- 0637 ( E nhanced F PI ) 6000

Reference 1, or Reference 2

, E ng i ne M anua l

, T AS K 72

- 41

-

11

- 110

- 001 (C l ean)

Referenc e 5, Non

- M od i f i ca ti on S erv i ce B u ll e ti n

V 2500

- E NG

- 72

- 0637 ( E nhanced F PI )

Reference 3, Non

- M od i f i ca ti on S erv i ce B u ll e ti n

V 2500

- E NG

- 72

- 0625 ( E C I ) 8000

### January 

### 19/10

REVISION NO. 6

– September 04 /14 

# V2500

- ENG

- 72

- A 0615

IAE PROPRIETARY INFORMATION Page 11 of 23

© IAE International Aero Engines AG (date as above). All rights reserved.

Not Subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3). I nspec ti on

l oca ti on HP co m pressor

3

- 8 Drum c y c l es

s i nce new Thresho l d From Regu l ar Repeat

I nspec ti on I n t erval

Ou t er and I nner

D i a m e t ers >3750 A cco m p li sh w it h i n 200

c y c l es. Da t e of Rev i s i on 6 of

Non

- M od i f i ca ti on S erv i ce

B u ll e ti n V 2500

- E NG

- 72

-

A 0615. Not m ore t han 500

c y c l es.

<=3750 A cc o m p li sh w it h i n 200

c y c l es of t he drum

reach i ng 3750 c y c l es. Group D:

V 2500

- A 5 E ng i nes V 10310, V 10408, V 10503, V 10531 and V 10860.

HP Co m pressor St age 3

- 8 Drum A sse m b l y P Ns: P N 6 A 4900, P N 6 A 5467, P N 6 A 6473, P N 6 A 7383, P N 6 A 7384,

P N 6 A 7385, P N 6 A 7401, P N 6 B 1379, P N 6 B 1380, P N 6 B 1381, P N 6 B 1384, P N 6 B 1387 and P N 6 B 1391 (T i 5331

Drum M a t er i a l ).

### January 

### 19/10

REVISION NO. 6

– September 04 /14 

# V2500

- ENG

- 72

- A 0615

IAE PROPRIETARY INFORMATION Page 12 of 23

© IAE International Aero Engines AG (date as above). All rights reserved.

Not Subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3). G race P er i ods Tab l e:

Co m p li ance

Group Nu t/ Drum St andard Requ i red Drum Cond iti on P er m itt ed

Grace P er i od

(C y c l es)

D For dru m s t hat

w ere f itt ed w it h any

s t andard of nu t

. Reference 1, or Reference 2, E ng i ne M anua l

, T AS K 72

- 41

- 11

-

110

- 001 (C l ean)

Reference 1, or Reference 2

, E ng i ne M anua l

, T AS K 72

- 41

- 11

-

200

- 001 (F PI ) 2000

Reference 1, or Reference 2

, E ng i ne M anua l

, T AS K 72

- 41

- 11

-

110

- 001 (C l ean)

Reference 1, or Reference 2

, E ng i ne M anua l

, T AS K 72

- 41

- 11

-

200

- 001 (F PI )

Reference 3, Non

- M od i f i ca ti on S erv i ce B u ll e ti n V 2500

- E NG

- 72

-

0625 ( E C I ) 3000

For dru m s t hat

w ere f itt ed w it h

Reference 4

,

V 2500

- E NG

- 72

-

0632

i n iti al i ssue, da t ed

Dece m ber 20 t h

2012 or l a t er

approved rev i s i on Reference 1, or Reference 2

, E ng i ne M anua l

, T AS K 72

- 41

- 11

-

110

- 001 (C l ean)

Reference 5, Non

- M od i f i ca ti on S erv i ce B u ll e ti n V 2500

-

E NG

- 72

- 0637 ( E nhanced F PI ) 5000

Reference 1, or Reference 2

, E ng i ne M anua l

, T AS K 72

- 41

- 11

-

110

- 001 (C l ean)

Reference 5, Non

- M od i f i ca ti on S erv i ce B u ll e ti n V 2500

-

E NG

- 72

- 0637 ( E nhanced F PI )

Reference 3

, Non

- M od i f i ca ti on S erv i ce B u ll e ti n V 2500

-

E NG

- 72

- 0625 ( E C I ) 5000

### January 

### 19/10

REVISION NO. 6

– September 04 /14 

# V2500

- ENG

- 72

- A 0615

IAE PROPRIETARY INFORMATION Page 13 of 23

© IAE International Aero Eng ines AG (date as above). All rights reserved.

Not Subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3). I nspec ti on

l oca ti on HP co m pressor

3

- 8 Drum c y c l es

s i nce new Thresho l d From Regu l ar Repeat

I nspec ti on

I n t erval

Ou t er and I nner

D i a m e t ers >12500 A cco m p li sh w it h i n 200

c y c l es. Da t e of

Rev i s i on 6 of

Non

- M od i f i ca ti on

S erv i ce B u ll e ti n

V 2500

- E NG

- 72

-

A 0615. Not m ore t han

750 c y c l es.

<=12500 A cco m p li sh w it h i n 200

c y c l es of t he drum

reach i ng 12500

c y c l es. Group E :

V 2500

- A 1 /A 5 / D5 E ng i nes t hat are not li s t ed spec i f i ca ll y i n Gro ups A

, B

, C or D.

HP Co m pressor St age 3

- 8 Drum A sse m b l y P Ns: P N 6 A 7705, P N 6 A 8236, P N 6 A 8316, P N 6 A 8318, P N

6 B 1385, P N 6 B 1386, P N 6 B 1392, P N 6 B 1393, P N 6 B 1401, P N 6 B 1403, P N 6 B 1404, P N 6 B 1405 and P N

6 B 1406 (T i 6246 Drum M a t er i a l ).

Co m p li ance T i m e Tab l e :

### January 

### 19/10

REVISION NO. 6

– September 04 /14 

# V2500

- ENG

- 72

- A 0615

IAE PROPRIETARY INFORMATION Page 14 of 23

© IAE International Aero Engines AG (date as above). All rights reserved.

Not Subject to the EAR per 15 C.F. R. Chapter 1, Part 734.3(b)(3). Grace P er i ods Tab l e:

Co m p li ance

Group Nu t/ Drum St andard Requ i red Drum Cond iti on P er m itt ed

Grace P er i od

(C y c l es)

E For dru m s t hat

w ere f itt ed w it h

any s t andard of

nu t

. Reference 1, or Reference 2

, E ng i ne M anua l

, T AS K 72

- 41

- 11

-

110

- 001 (C l ean)

Reference 1, or Reference 2

, E ng i ne M anua l

, T AS K 72

- 41

- 11

-

200

- 001 (F PI ) 4000

Reference 1, or Reference 2

, E ng i ne M anua l

, T AS K 72

- 41

- 11

-

110

- 001 (C l ean)

Reference 1, or Reference 2

, E ng i ne M anua l

, T AS K 72

- 41

- 11

-

200

- 001 (F PI )

Reference 3, Non

- M od i f i ca ti on S erv i ce B u ll e ti n V 2500

- E NG

- 72

-

0625 ( E C I ) 10000

For dru m s t hat w ere

f itt ed w it h Reference 4

,

V 2500

- E NG

- 72

- 0632

i n iti al i ssue, da t ed

Dece m ber 20 t h 2012

or l a t er approved

rev i s i on Reference 1,or Reference 2

, E n g i ne M anua l

, T AS K 72

- 41

- 11

-

110

- 001 (C l ean)

Reference 5, Non

- M od i f i ca ti on S erv i ce B u ll e ti n V 2500

-

E NG

- 72

- 0637 ( E nhanced F PI ) 6000

Reference 1, or Reference 2

, E ng i ne M anua l

, T AS K 72

- 41

- 11

-

110

- 001 (C l ean)

Reference 5, Non

- M od i f i ca ti on S erv i ce B u ll e ti n V 2 500

-

E NG

- 72

- 0637 ( E nhanced F PI )

Reference 3, Non

- M od i f i ca ti on S erv i ce B u ll e ti n V 2500

-

E NG

- 72

- 0625 ( E C I ) 13000

### January 

### 19/10

REVISION NO. 6

– September 04 /14 

# V2500

- ENG

- 72

- A 0615

IAE PROPRIETARY INFORMATION Page 15 of 23

© IAE International Aero Engines AG (date as above). All rights reserved.

Not Subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3). I nspec ti on

l oca ti on HP co m pressor

3

- 8 Drum c y c l es

s i nce new Thresho l d From Regu l ar Repeat

I nspec ti on I n t erval

Ou t er and I nner

D i a m e t ers >9000 A cco m p li sh w it h i n 200

c y c l es. Da t e of Rev i s i on 6 of

Non

- M od i f i ca ti on S erv i ce

B u ll e ti n V 2500

- E NG

- 72

-

A 0615. Not m ore t han 750

c y c l es.

<=9000 A cco m p li sh w it h i n 200

c y c l es of t he drum

reach i ng 9000 c y c l es. Group F:

V2500

- A1/A5/D5 Engines that are not listed spe cifically in Groups A, B, C or D.

HP Co m pres sor St age 3

- 8 Drum A sse m b l y P Ns: P N 6 A 2030, P N 6 A 2355, P N 6 A 2455, P N 6 A 6473, P N 6 A 8350,

P N 6 A 2645, P N 6 A 3508, P N 6 A 3648, P N 6 A 3934, P N 6 A 3936, P N 6 A 4900, P N 6 A 5467, P N 6 A 5592, P N 6 A 6973,

P N 6 A 7379, P N 6 A 7380, P N 6 A 7382, P N 6 A 7383, P N 6 A 7384, P N 6 A 7385, P N 6 A 7401, P N 6 A 8250,

PN 6A5594, PN 6A5659, PN 6A4189, P N 6 B 1379, P N 6 B 1380, P N 6 B 1381, P N 6 B 1382, P N 6 B 1383,

P N 6 B 1384, P N 6 B 1387, P N 6 B 1391 and P N 6 B 1402 (T i 5331 Drum M a t er i a l ).

Co m p li ance T i m e Tab l e:

### January 

### 19/10

REVISION NO. 6

– September 04 /14 

# V2500

- ENG

- 72

- A 0615

IAE PROPRIETARY INFORMATION Page 16 of 23

© IAE Internat ional Aero Engines AG (date as above). All rights reserved.

Not Subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3). Grace P er i ods Tab l e:

Co m p li ance

Group Nu t/ Drum St andard Requ i red Drum Cond iti on P er m itt ed

Grace P er i od

(C y c l es)

F For dru m s t hat w ere

f itt ed w it h any

s t andard of nu t

. Reference 1, or Reference 2

, E ng i ne M anua l

, T AS K 72

- 4 1

-

11

- 110

- 001 (C l ean)

Reference 1, or Reference 2, E ng i ne M anua l

, T AS K 72

- 41

-

11

- 200

- 001 (F PI ) 2000

Reference 1, or Reference 2

, E ng i ne M anua l

, T AS K 72

- 41

-

11

- 110

- 001 (C l ean)

Reference 1, or Reference 2

, E ng i ne M anua l

, T AS K 72

- 41

-

11

- 200

- 001 (F PI )

Refere nce 3, Non

- M od i f i ca ti on S erv i ce B u ll e ti n V 2500

- E NG

72

- 0625 ( E C I ) 5000

For dru m s t hat w ere

f itt ed w it h Reference 4

,

V 2500

- E NG

- 72

- 0632

i n iti al i ssue, da t ed

Dece m ber 20 t h 2012

or l a t er approved

rev i s i on Reference 1, or Reference 2

, E ng i ne M a nua l

, T AS K 72

- 41

-

11

- 110

- 001 (C l ean)

Reference 5, Non

- M od i f i ca ti on S erv i ce B u ll e ti n

V 2500

- E NG

- 72

- 0637 ( E nhanced F PI ) 5000

Reference 1, or Reference 2

, E ng i ne M anua l

, T AS K 72

- 41

-

11

- 110

- 001 (C l ean)

Reference 5, Non

- M od i f i ca ti on S erv i ce B u ll e ti n

V 2500

- E NG

- 72

- 0637 ( E nhanced F PI )

Reference 3, Non

- M od i f i ca ti on S erv i ce B u ll e ti n

V 2500

- E NG

- 72

- 0625 ( E C I ) 8000

### January 

### 19/10

REVISION NO. 6

– September 04 /14 

# V2500

- ENG

- 72

- A 0615

IAE PROPRIETARY INFORMATION Page 17 of 23

© IAE International Aero Engines AG (date as above). All rights reserved.

Not Subject to t he EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3). F. A dd iti onal I ns t ruc ti on

Note: To co m p l y w it h t he IA E des i gn po li c y

, IA E reco mm ends t hat eng i ne s i n t h i s effec ti v it y m ust have

i ns t a ll ed a HP Co m pressor St age 3

- 8 Drum A sse m b l y (72

- 41

- 11

- 01

- 200) t hat has never opera t ed w it h P re

S erv i ce B u ll e ti n V 2500

- E NG

- 72

- 0632 (72

- 41

- 12, 01

- 602) s t andard nu t s by t he 31st of Dece m ber 2021.

I f an eng i ne t ha t i s not li s t ed i n t he effec ti v it y

, has a HP co m pressor St age 3

- 8 drum t hat has opera t ed w it h

P re S erv i ce B u ll e ti n V 2500

- E NG

- 72

- 0632 (72

- 41

- 12

, 01

- 602) s t andard nu t s, i t m ust be i nspec t ed accord i ng t o

t he app li cab l e requ i re m en t s of Group A

, B

, C, D, E or F. The eng i ne shou l d be i nspec t ed accord i ng t o t he

app li cab l e requ i re m en t s of Group A

, B

, C or D, i f t hat drum has s t a y ed shu t do w n m ore t han s i x hours i n I nd i a

af t er eng i ne shu t do w n, m ore t han four ti m es.

E ng i nes w h i ch are not spec i f i ca ll y li s t ed i n Groups A

, B

, C or D, shou l d be i nspec t ed accord i ng t o t he

app li cab l e requ i re m en t s of Group A

, B

, C or D, i f t he eng i ne has a HP Co m pressor St age 3

- 8 Drum A sse m b l y

(72

- 41

- 11

- 01

- 200) t hat has s t a y ed shu t do w n m ore t han s i x hours i n I nd i a af t er eng i ne shu t do w n, m ore t han

four ti m es.

I f an eng i ne t hat i s not li s t ed spec i f i ca ll y i n Group A

, B

, C or D s t a y s shu t do w n m ore t han s i x hours i n I nd i a

af t er eng i ne shut do w n, for t he four t h ti m e, do t he procedure t hat fo ll o w s:

1. De t er m i ne t he new co m p li ance t hresho l d and g race per i od for t he appropr i a t e Group A

, B

, C, or D.

1. I f t he eng i ne i s be y ond t he new co m p li ance t hresho l d and grace per i od, perform t he i n iti al

U lt rason i c I nspec ti on w it h i n 200 c y c l es.

2. No ti fy IA E w h i ch Group A

, B

, C, or D, t hat t he eng i ne and drum be l ong s t o.

G. A pproval

The co m p li ance s t a t e m ent and t he procedures descr i bed i n t h i s S erv i ce B u ll e ti n have been sho w n t o co m p l y

w it h t he app li cab l e Federal A v i a ti on Regu l a ti ons and are F AA

- APP RO VE D for t he eng i ne m odel li s t ed.

H. M anpo w er

E s ti m a t ed m an

- ho urs t o carry out t h i s Non

- M od i f i ca ti on S erv i ce B u ll e ti n i n fu ll :

(1) Refer t o Reference 6

, Non

- M od i f i ca ti on S erv i ce B u ll e ti n V 2500

- E NG

- 72

- 0638.

Note : The u lt rason i c i nspec ti on def i ned i n Reference 6

, Non

- M od i f i ca ti on S erv i ce B u ll e ti n V 2500

- E NG

- 72

-

0638 m ust on l y be perfor m ed by personnel qua li f i ed t o u lt rason i c i nspec ti on l evel 2 or h i gher i n

accordance w it h E N4179 and / or N AS 410 or a lt erna ti ve s t andards/ gu i de li nes accep t ed by t he

app li cab l e Na ti onal A v i a ti on A u t hor it y

.

I. W e i ght and B a l ance

(1) W e i ght Change

None.

### January 

### 19/10

REVISION NO. 6

– September 04 /14 

# V2500

- ENG

- 72

- A 0615

IAE PROPRIETARY INFORMATION Page 18 of 23

© IAE International Aero Engines AG (date as above). All rights reserved.

Not Subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3). (2) M o m ent A rm

No E ffec t

.

(3) Da t um

E ng i ne Front M ount Cen t er li ne ( P o w er Pl ant St a ti on ( PPS ) 100)

J. El ec t r i cal Load Da t a

Th i s S erv i ce B u ll e ti n has no effect on t he a i rcraft e l ec t r i cal l oad.

K. S of t w are A cco m p li sh m en t S u mm ary

Not A pp li cab l e.

L. References

Note : I n 2014 IAE converted the V2500 Technical Publications to a new system. As a result of the conversion, some

manuals were consolidated. All manuals received new P&W part numbers. To facilitate the us e of this Service

Bulletin, a Technical Publications conversion table is provided in the Appendix

(1) V2500 A1/A5 Series Engine Manual, P&W Ref. PN 2A4407

, Chapter 72

- 41

- 11.

(2) V2500

- D5 Series Engine Manual, P&W Ref. PN 2A4416 Chapter 72

- 41

- 11.

(3) Non

- Modification Service Bulletin V2500

- ENG

- 72

- 0625

NON

- MODIFICATION SERVICE BULLETIN

- ENGINE

- HIGH PRESSURE (HP) COMPRESSOR STAGE 3 TO 8

COMPRESSOR DRUM

- EDDY CURRENT INSPECTION (ECI)

(4) Service Bulletin V2500

- ENG

- 72

- 0632

ENGINE

- HIGH PRESSURE (HP) COMPRESSOR DISCS

- INTRODUCTION OF SILVER FREE NUTS

(5) Non

- Modification Service Bulletin V2500

- ENG

- 72

- 0637.

NON

- MODIFICATION SERVICE BULLETIN

- ENGINE

- HIGH PRESSURE (HP) COMPR ESSOR

- ENHANCED

FLUORE SCENT PENETRANT INSPECTION (FPI)

(6) Non

- Modification Service Bulletin V2500

- ENG

- 72

- 0638

NON

- MODIFICATION SERVICE BULLETIN

- ENGINE

- HIGH PRESSURE (HP) COMPRESSOR

- STAGE 3 TO 8

COMPRESSOR DRUM

- ULTRASONIC INSPECTION PROCEDURE (USI)

(7) SEN5088 Issue 1. "Significant shop findings on HPC 3

- 8 drum".

(8) SEN5088 Issue 2. "Significant shop findings on HPC 3

- 8 drum".

(9) SE N5088 I ssue 2. "Si gn i f i cant shop f i nd i ngs on H P C 3

- 8 dru m "

.

(10) SI L 277 I ssue 1. " H P C 3

- 8 Drum U S I c l ar i f i ca ti on "

.

(11) Internal Reference No. E A 1 4VC146 A

(12) ATA Locator

- 72

- 41

- 12.

### January 

### 19/10

REVISION NO. 6

– September 04 /14 

# V2500

- ENG

- 72

- A 0615

IAE PROPRIETARY INFORMATION Page 19 of 23

© IAE International Aero Engines AG (date as above). All rights reserved.

Not Subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3). M. O t her P ub li ca ti ons A ffec t ed

None.

N. I n t erchangeab ilit y of P ar t s

Not A pp li cab l e.

2. M a t er i al I nfor m a ti on

None

3. A cco m p li sh m ent I ns t ruc ti ons

A. I nspec ti on I ns t ruc ti ons

(1) A cco m p li sh t he U lt ra S on i c I nspec ti on (U SI ) i ns t ruc t ed w it h Reference 6

, Non

- M od i f i ca ti on S erv i ce B u ll e ti n

V 2500

- E N G

- 72

- 0638 i n iti al i ssue or l a t er approved rev i s i on, i n accordance w it h t he app li cab l e co m p li ance

t hresho l d and i n t erval g i ven i n Co m p li ance of t h i s Non

- M od i f i ca ti on S erv i ce B u ll e ti n.

(a) For V 2500

- A 1 /A 5 / D5 eng i nes:

(i) A ccept and re j ect cr it er i a (Ou t er D i a m e t er):

(1) A ny u lt rason i c response i n t he ga t ed area above or at t he a m p lit ude of 40 percent F S H

—

re j ect t he eng i ne.

(2) A ny u lt rason i c response i n t he ga t ed area be l ow t he a m p lit ude of 40 percent F S H

—

accep t

.

(ii) A ccept and re j ect cr it er i a ( I nner D i a m e t e r):

(1) For HP co m pressor dru m s of T i 6 m a t er i a l : T i 6246

A A ny u lt rason i c response i n t he ga t ed area above or at t he a m p lit ude of 30 percent

F S H

— re j ect t he eng i ne.

B A ny u lt rason i c response i n t he ga t ed area be l ow t he a m p lit ude of 30 percent F S H

— accep t

.

(2) For HP co m pressor dru m s of T i 5 m a t er i a l : T i 5331

A A ny u lt rason i c response i n t he ga t ed area above or at t he a m p lit ude of 55 percent

F S H

— re j ect t he eng i ne.

B A ny u lt rason i c response i n t he ga t ed area be l ow t he a m p lit ude of 55 percent F S H

—

accep t

.

B Record i ng I ns t ruc ti ons

(1) Co m p l e t e a separa t e A cco m p li sh m ent P rofor m a for ou t er and i n ner d i a m e t er. S ee Tab l e 1.

Re t a i n t he profor m a for record keep i ng.

(2) Record t he i ncorpora ti on of Non

- M od i f i ca ti on S erv i ce B u ll e ti n V 2500

- E NG

- 72

- A0 615 i n t he app li cab l e

eng i ne record.

### January 

### 19/10

REVISION NO. 6

– September 04 /14 

# V2500

- ENG

- 72

- A 0615

IAE PROPRIETARY INFORMATION Page 20 of 23

© IAE International Aero Engines AG (date as above). All ri ghts reserved.

Not Subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3). Tab l e 1 A cco m p li sh m ent P rofor m a A 1 /A 5 / D5

Gene ral I nfor m a ti on

A cco m p li sh m ent Da t e

Ai rcraft Reg i s t ra ti on (Ta il ) Nu m ber

E ng i ne P os iti on

E ng i ne S er i al Nu m ber

I nspec ti on I nfor m a ti on

Position Inspected

(C i rc l e One

— Co m p l e t e 1

— Form for I nner and 1

— Form for o u t er) Ou t er I nner

B o rescope I nspec ti on Of St age 7 L i ner

— D i d y ou f i nd L i ner Loss Under P a t h of

P robe? (C i rc l e One) ( A 1 on l y ) Y es No

P robe S er i al Nu m ber

W ork i ng St andard S er i al Nu m ber

I nspec ti on Resu lt s (C i rc l e One) PAS S F AI L Not

A cco m p li shed 1

1 No t es and / or B r i ef Desc r i p ti on A s To W hy I nspec ti on Not A cco m p li shed). I s t here an y t h i ng e l se y ou w ou l d li ke E ng i neer i ng t o

be a w are of concern i ng t h i s E ng i ne? 1

2

I nspec t or St a m p or P r i n t ed Na m e

U lt rason i c I nd i ca ti on S u mm ary Tab l e D i rec ti on of drum ro t a ti on c l ock w i se / an ti c l o ck w i se. ( l ook i ng for w ard)

#

%

F

S

H T i m e

B ase

P os it ion Drum

P os it ion

A ng l e (D E G)

( I f poss i b l e) #

%

F

S

H T i m e

B ase

P os it ion Drum

P os iti on

A ng l e (D E G)

( I f poss i ble) #

%

F

S

H T i m e

B ase

P os it ion Drum

P os it ion

A ng l e (D E G)

( I f poss i b l e)

1 1

1 21

2 1

2 22

3 1

3 23

4 1

4 24

5 1

5 25

6 1

6 26

7 1

7 27

8 1

8 28

9 1

9 29

10 2

0 30

Note : The borescope i nspec ti on for li ner m a t er i al l oss i s requ i r ed t o ensure c l earance of t he ro t or pa t h for t he

u lt rason i c probe. Th i s i s recorded for i nfor m a ti on on l y

, and does not need t o be s t a m ped off as part of

t he for m al acco m p li sh m ent records ( A 1 on l y ).

Note : A separa t e A cco m p li sh m ent P rofor m a i s t o be co m p l e t ed for each i nner and ou t er d i a m e t er i nspec ti on.

### January 

### 19/10

REVISION NO. 6

– September 04 /14 

# V2500

- ENG

- 72

- A 0615

IAE PROPRIETARY INFORMATION Page 21 of 23

© IAE International Aero Engines AG (date as above). All rights reserved.

Not Subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3). A ppend i x

A dded Da t a

I n t ernal Reference I nfor m a ti on

Rev i s i on No. Reference Docu m ent Or i g i na ti on

Original E C10 V R775 RN /IE L

1 E C10 V R775A RN /IE L

2 E C10 V R775B RN /IE L

3 E C10 V R775C RN /IE L

4 E C10 V R775D RN /IE L

5 EA 14 V C146 RN /IE L

6 EA 14 V C146 A ARO /AT

### January 

### 19/10

REVISION NO. 6

– September 04 /14 

# V2500

- ENG

- 72

- A 0615

IAE PROPRIETARY INFORMATION Page 22 of 23

© IAE International Aero Engines AG (date as above). All rights reserved.

Not Subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3). NOTE: In 2014 IAE converted the V2500 Technical Publications to a new system. As a result of the

conversion, some manuals were consolidated. All manuals received new P&W part numbers.

To facilitate the use of this Service Bulletin, the following Technical Publications cross reference

table is provided



### .

Technical Publications Cross Reference Table

Publication Engine

Model(s) IAE IETM Pub Ref P&W Part

Number

ENGINE MANUAL

— A1, A5 All E

- V25 00

- 1IA 2A4407

CMM

- EHC

— A1, A5 All EHC

- V2500

- 1IA 2A4409

CMM

- FN

— A1, A5 All FN

- V2500

- 1IA 2A4410

CMM

- MMC

— A1, A5 All MECH

- V2500

- 1IA 2A4411

CMM

- THD

— A1, A5 All THD

- V2500

- 1IA 2A4412

TLM

— A1, A5 All T

- V2500

- 1IA 2A4408

ENGINE MANUAL

— D5 All E

- V2500

- 3I A 2A4416

CMM

- EHC

— D5 All EHC

- V2500

- 31A 2A4418

CMM

- FN

— D5 All FN

- V2500

- 3IA 2A4419

CMM

- MMC

— D5 All MECH

- V2500

- 3IA 2A4420

CMM

- THD

— D5 All THD

- V2500

- 3IA 2A4423

TLM

— D5 All T

- V2500

- 3IA 2A4417

### January 

### 19/10

REVISION NO. 6

– September 04 /14 

# V2 500

- ENG

- 72

- A 0615

IAE PROPRIETARY INFORMATION Page 23 of 23

© IAE International Aero Engines AG (date a s above). All rights reserved.

Not Subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3). 

### Publication Engine Model(s) IAE IETM Pub

Ref P&W Part

Number

SPPM (SPM)

— A1, A5, D5 All SPP

- V2500

- 1IA 2A4414

EIPC

— A1 V2500

- A1102Q00 S

- V2500

- 1IA 2A4427

EIPC

— A5 V2522/V2524/V2527M

- AQ02 S

- V2500

- 6IA

2A4428 V2522/V2524/V2527M

- AQ03 S

- V2500

- 6IB

V2522/V2524/V2527M

- SQ02 S

- V2500

- 6SA

V2522/V2524/V2527M

- SQ03 S

- V2500

- 6SB

V2522/V2524/V2527M

- SQ04 S

- V2500

- 6NA

V2522/V2524/V2527M

- SQ05 S

- V2500

- 6NB

V2527/V2527E

- AQ02 S

- V2500

- 7IA

V2527/V2527E

- AQ03 S

- V2500

- 7IB

V2527/V2527E

- SQ02 S

- V2500

- 7SA

V2527/V2527E

- SQ03 S

- V2500

- 7SB

V252 7/V2527E

- SQ04 S

- V2500

- 7NA

V2527/V2527E

- SQ05 S

- V2500

- 7NB

V2530

- AQ02 S

- V2500

- 2IA

V2530

- AQ03 S

- V2500

- 2IB

V2530

- SQ02 S

- V2500

- 2SA

V2530

- SQ03 S

- V2500

- 2SB

V2530

- SQ04 S

- V2500

- 2NA

V2530

- SQ05 S

- V2500

- 2NB

V2533

- AQ02 S

- V2500

- 5IA

V2533

- AQ03 S

- V2500

- 5IB

V2533

- SQ02 S

- V2500

- 5SA

V2533

- SQ03 S

- V2500

- 5SB

V2533

- SQ04 S

- V2500

- 5NA

V2533

- SQ05All S

- V2500

- 5NB

EIPC

— D5 V2525/V2528

- AQ02 S

- V2500

- 3IA

2A4426 V2525/V2528

- AQ03 S

- V2500

- 3IB

V2525/V2528

- AQ04 S

- V2500

- 3IC