The following packages are an illustration of the work that NASA will
ask the Contractor to complete. Each Job number would be expected to be
complete in a three month period.

# JOB NUMBER 20-00XX

**1.0** THE FOLLOWING SERVICE BULLETIN INSPECTION WAS ACCOMPLISHED:

02-0008 53-2253-3 INSPECT BS340 TO 400 STRINGER 6 SKIN

**2.0** THE FOLLOWING A.D. WAS ACCOMPLISHED:

02-0009 90-23-14 INSPECT BS340 TO 400 STRINGER 6 SKIN

**3.0** THE FOLLOWING CPCP WORKCARDS WERE ACCOMPLISHED:

02-0010 D6-36022-034 C53-210-01 118 FSLG-UPPER LOBE- INTERIOR UPPER DECK
INCLUDING DOORS/FLOOR

02-0011 D6-36022-038 C53-210-01 5/8 FSLG-UPR LOBE-INTERIOR-CROWN AREA

02-0012 D6-36022-039 C53-210-01 6/8 FSLG-UPR LOBE-INTERIOR-CROWN AREA

02-0013 D6-36022-041 C53-210-01 8/8 FSLG-UPR LOBE- NTERIOR-CROWN

02-0014 D6-36022-043 C53-210-03 1/4 FSLG-UPR LOBE-AREAS UNDER UPPER DECK
LAV

02-0015 D6-36022-044 C53-210-03 2/4 FSLG-UPR LOBE-AREAS UNDER UPPER DECK
LAV

02-0016 D6-36022-045 C53-210-03 3/4 FSLG-UPR LOBE-AREAS UNDER MAIN DECK
LAV

**4.0** THE FOLLOWING MAJOR REPAIRS WERE ACCOMPLISHED:

03-0001 ECRA NO. N905NA-53-008-EAC REPAIR- CRACKED STRINGER #2 LH STA
1607-1620

03-0002 ECRA NO. N905NA-53-009-EAC REPAIR-CRACKED STRINGER #9 LH STA
1620

**5.0** THE FOLLOWING MINOR REPAIRS WERE ACCOMPLISHED.

03-0003 SRM REPAIR-CRACKED STRINGER #8 RH STA 1624

03-0004 SRM REPAIR-CRACKED STRINGER #14 RH STA 1620

03-0005 SRM REPAIR-CRACKED STRINGER #19 RH STA 1920

# JOB NUMBER 20-00XX 

**1.0** THE FOLLOWING CPCP WORKCARDS WERE ACCOMPLISHED:

02-0005 D6-36022-001 C32-715-01 1/1 NOSE LANDING GEAR

02-0006 D6-36022-002 C32-735-01 1/4 LH WING LANDING GEAR

02-0007 D6-36022-002 C32-735-01 214 RH WING LANDING GEAR

02-0008 D6-36022-002 C32-735-01 3/4 LH BODY LANDING GEAR

02-0009 D6-36022-002 C32-735-01 X14 RH BODY LANDING GEAR

02-0010 D6-36022-007 C32-735-03 3/4 LH WING TRUNNION BEARING HOUSING
FITTING

02-0011 D6-36022-008 C32-735-03 4/4 RH WING TRUNNION BEARING HOUSING
FITTING

**2.0** THE FOLLOWING MAJOR OVERHAULS WERE ACCOMPLISHED BY HAWKER
PACIFIC AEROSPACE (HPA)

02-0005 NOSE LANDING GEAR

02-0006 LH WING LANDING GEAR

02-0007 RH WING LANDING GEAR

02-0008 LH BODY LANDING GEAR

02-0009 RH BODY LANDING GEAR

02-0010 LH WING GEAR TRUNNION BEARING HOUSING FITTING

02-0011 RH WING GEAR TRUNNION BEARING HOUSING FITTING

# JOB NUMBER 20-00XX

**1.0** THE FOLLOWING SERVICE BULLETIN INSPECTIONS WERE ACCOMPLISHED

0008 21-2399 INSP RAM AIR HEADER DUCTS 8 WING CTR SECTION SION ABV THE
HEADER DUCTS

0009 24-2118a-3 INSP AND INSTALL MAIN 115 VAC POWER DISTRIBUTION WIRE
PROTECTIVE SLEEVE

0010 27-2358 STRIPING OF TRAILING EDGE FLAP TORQUE TUBE IN WHEEL WELL

0011 27-2366 PK #3 FLT CONTROL T E FLAP IS 4FLAP MID SEQUENCE CARRIAGE
DETENT ROLLER

0012 27-2366 PK #2 FLT CONTROL T E FLAP IB 4FLAP AND SEQUENCE CARRIAGE
OETENT ROLLER-

0013 52-2168-1 MOD MAIN ENTRY DOOR 02 AND 4 EDGE FRAME WSP AND
REINFORCEMENT

0014 52-2166-4 INSP LOWER LOBE CARGO DOORS PORTAL LATCH PIN SUPPORT
FITTING

0015 52-2218 REPLACE FWD AND AFT CARGO DOOR LINER ATTACH NUTPLATES

0016 53-2112-7 DVI INSP NOSE GEAR WHEEL WELL FWD CORNER FOR CRACKS

0017 53-2156-6 INTERNAL INSP BS 1740 TO 2180 STR 4OLT04GR LWR BODY SKW
PANEL

0018 53-2156-6 EXTERNAL INSP BS 1740 TO 2180 STR 48L TO 48R LWR BODY
SKIN PANEL

0019 53-2280A-3 INSP STR 23 BS 2598 LONGERON SKIN SPLICE FITTING AND
TENSION BOLTS

0020 53-2280A-3 INSP STR 11 BS 258 LONGERON SKIN SPLICE FITTING AND
TENSION BOLTS

0021 53-2293-7 INSP AREA 4 OF NOSE WHEEL WELL BODY STRUCTURE

0022 53-2297-1 INSP BS 940 TO 1000, STR OLT08RCROWN CREASE BEAM

0023 53-2302-1 INSP STA 2200 AND 2220 LOWER FRAME AT OUTFLOW VALVE
CUTOUT

0024 53-2304 INSP NOSE WHEEL WELL FWD CORNER AFT BODY SKIN PANEL

0025 53-2305-1 INSP NOSE WHEEL WELL AFT CORNER SKIN PANEL

0026 53-2321A-5 INSP UPR BDY SKIN AT LONGL ROW OF FASTENERS SEC 41 FLAT
SIDED SKIN

0027 53-2326A-1 INSP MAIN ENTRY DOOR #5 FWD EDGE STOP SUPPORT FITTING

0028 53-2406-1 HFEC AND INSP LONGITUDINAL ROW OF FASTENERS IN SECTION 41
AND 42

0029 53-2414A INSP #1 MAIN ENTRY DOOR FRAME CUTOUT AFT EDGE AT STA 448

0030 53-2417A-1 INSP #1 MAIN ENTRY DOOR FRAME CUTOUT FWD EDGE AT STA 434

0031 57-2184 INSP WING T E SUPPORT BEAM LOWER CHORD

0032 57-2240 INSP WING REAR SPAR WEB FUEL SYSTEM CUTOUTS

0033 57-2280 INSP FLOOR BEAMS AT BBL 11.33 AND 33.99

0034 57-2297-2 INSP FRONT SPAR CENTER SECTION WEB -

0035 57-2310A INSP T E FLAPS ACTUATOR ATTACH FITTING

0036 76-2099-5 MOD TURBINE EXHAUST PLUG RETENSION BOLT REPLACEMENT

**2.0** THE FOLLOWING AD\'S WERE ACCOMPLISHED

0037 98-26-023 INSP FOR CORR OF REAR SPAR WEB OF WING CTR SECT &
ADJACENT BLKHD FTG

0038 99-09-011 INSP STEEL ATTACH FITTINGS OF DIAGONAL BRACE TO 18 AND OB
NAC STRUTS

**3.0** THE FOLLOWING CPCP WORKCARDS WERE ACCOMPLISHED

0039 D6-36022-005 C32-735-03 1/4 LH WG TRUNION BEARING HOUSING SPT FTG

0040 D6-36022-006 C32-735-03 2/4 RH WG TRUNION BEARING HOUSING

0041 D6-36022-009 C53-100-01 1/10 LWR FSLG- EXT SURF-1\'LG AREA

0042 D6-36022-010 C53-100-91 2/10 LWR FSLG- EXT SURF- BS 134.75 TO 520

0043 D6-36022-014 C53-100-01 6/10 LWR FSLG\--EXT SURF-BS *1961 TO
2360\$3*

0044 D6-36022-015 C53-100-01 7110 LWR FSLG\--EXT SURF- LWLG

0045 D6-36022-016 C53-100-01 8n0 LWR FSLG-EXT SURF-RWLG BAY

0046 D6-36022-017 C53-100.01 X10 LWR FSLG\-- EXT SURF= LBLG

0047 D6-36022-018 C53-100-01 10110 LWR FSLG- EXT SURF;. RBLG WELL

0048 D6-36022-101 C57-500-01 1/2 LEFT WING- 00. EXTERIOR SURFACES

0049 D6-36022-102 C57-500-01 2/2 RIGHT WING. 041- EXTERIOR SURFACES

0050 D6-36022-103 C57-500-02 1/2 LEFT WING- 01111- EXTERIOR.. UPR SKIN
AT RABBET AREA

0051 D6-36022-104 C57-500-02 2/2 RIGHT WING OB- EXTERIOR- UPR SKW AT
RABBET AREA

0052 D6-36022-107 C57-510-01 1/4 LEFT WING-LEADING EDGE CAVITY- INTERIOR

0053 D6-36022-108 C57-610-01 2/4 RIGHT WING- LEADING EDGE CAVITY-
INTERIOR

0054 D6-36022-119 C57-560-01 1/2 LEFT WING-TE CAVITY-INTERIOR INCLUDING
FLAPS & FLAP TRACKS

0055 D6-36022-120 C57-560-03 2/2RIGHT WING-TE CAVITY-INTERIOR INLUDING
FLAPS 8 FLAP TRACKS

0056 D6-36022-121 C57-560-03 1/4 LEFT WINQ-TE CAVITY-NTERIOR-FLAP TRACKS
AND ATTACH FTG

0057 D6-36022-122 C57-560-03 2/4 RIGHT WING-TE CAVITY-INTERIOR4FLAP
TRACKS AID ATTACH FTG

0058 D6-36022-135 C57-560-09 1/4 LEFT WING-TE CAVITY-INTERIOR-FLAP
TRARKS (CARRIAGE STOP).

0059 D6-36022-136 C57-560-09 1/4 RIGHT WING-T\'E CAVITY-INTERIOR-FLAP
TRACKS (CARRIAGE STOP)

0060 D6-36022-096 C55-334-01 1/2 LEFT HORIZONTAL STA81LI2RrTRNIWG EDGE
CAVITY WTERIOR

0061 D6-36022-097 C55-334-01 2/2 RIGHT HORIZONTAL. STABILUERTRAILING
EDGE CAVITY PRIOR

# JOB NUMBER 20-00XX

**1.0** THE FOLLOWING SERVICE BUL LETIN INSPECTION WAS ACCOMPLISHED:

02-0008 53-2253 INSPECT BS340 TO 400 STRINGER 6 SKIN

**2.0** THE FOLLOWING A.D. WAS ACCOMPLISHED:

02-0009 90-23-14 INSPECT BS340 TO 400 STRINGER 6 SKIN

**3.0** THE FOLLOWING CPCP WORKCARDS WERE ACCOMPLISHED:

02-0010 D6-36022-028 C53-190-01-2/2 FSLG-UNDER RT WG TO BDY FAIRING., AC
BAY & KEEL BEAM

02-0011 D6-36022-038 C53-210-01 5/8 FSLG-UPR LOBE-INTERIOR-CROWN AREA ;.
. . , , .

02-0012 D6-36022-041 C53-210-01 8/8 FSLG-UPR LOBE-INTERIOR-CROWW AREA

02-0013 D6-36022-042 C53-210-02 8/8 FSLG-UPR LOBE- NTERIOR-CANTED
PRESSURE DECK -

02-0014 D6-36022-043 G53-210-03 \_ 1/4 FSLG-UPR LOBE-AREAS UNDER UPPER
DECK LAV -

02-0015 D6-36022-044 C53-210-03 214 FSLG-UPR LOBE-AREAS UNDER UPPER DECK
LAV

02-0016 D6-36022-045 C53-210-03 3/4 FSLG-UPR LOBE-AREAS UNDER MAIN DECK
LAV

**4.0** THE FOLLOWING MAJOR REPAIR WAS ACCOMPLISHED:

03-0037 ECRA NO. N911 NA-53-053-EAC REPAIR- CORROSION ON 65815009-2
CHORD SPLICE AT FS 1446