N703AS

Part: DOUBLER — CRACKED (BS 948-972) · airframe 53,971 hrs · 30,578 cycles

L2 DOOR CUTOUT BEARSTRAP IS CRACKED AT THE FWD LOWER RADIUS. ACFT GROUNDED. REPAIRED L2 DOORWAY CUTOUT FWD, LOWER BEAR STRAP IAW SRM 53-00-01-2R-32, DETAIL IV. THIS IS A CAT B REPAIR WITH AN INSPECTION THRESHOLD OF 66,000 FLT. CYCLES AFTER AIRPLANE DELIVERY AND A REPEAT INTERVAL AT 24,000 FLT CYCLES.

Part: DOOR SILL — CORRODED (BS 328-335) · corrosion level 2 · airframe 53,972 hrs · 30,578 cycles

L1 MOPSILL HAS AREAS OF CORROSION ON UPPER SURFACE. ACFT GROUNDED. BLENDED CORRODED AREAS ON L1 MOPSILL, INNER CHORD OUT OF LIMITS, REMOVED AND INSTALLED NEW MOPSILL, INNER CHORD IAW SRM 53-10-15-1A-1, FIG 101, DETAIL IX, 51-40-02-0G-0, W 1.0, O .090, R .076, L 7.0, D .014.

Part: STIFFENER — CORRODED (BS 1088) · corrosion level 2 · airframe 53,972 hrs · 30,578 cycles

APU TORQUE BOX CUTOUT AT 10888 BULKHEAD INBD STIFFENER FLANGE CORRODED. ACFT GROUNDED. REMOVED CORROSION AND CHECKED LIMITS, FOUND TO BE OUT OF LIMITS IAW SRM 53-80-08-1A-1, FIG 11. NOTED G DETAIL VI R & R STIFFENER IAW SRM 51-40-02-0G-0, PARA 4, W .75", O .070", R .056", L 2.0", D .014".

Part: INTERCOSTAL — CORRODED (BS 360-380) · corrosion level 2 · airframe 53,972 hrs · 30,578 cycles

FLOOR SUPPORT STRUCTURE AT APPROXIMATELY BS 360 JUST AFT OF G2 INBD GALLEY MOUNT IS CORRODED. ACFT GROUNDED. REAMED HOLE FOR NUTPLATE ON FLOOR SUPPORT STRUCTURE AT APPROXIMATELY BS 360 JUST AFT OF G-2 INBD GALLEY MOUNT TO .261, CORROSION STIL EXISTS, OUT OF LIMITS REMOVED AND INSTALLED NEW FLOOR STRUCTURE, INTERCOSTAL, IAW SRM 53-30 51-1A-1 DET III, 51-4-02-0G-0, 51-40-04-0G-0-FIG 1, TABLE 1B DWG 65-51268, W .500, O .325, R .000, L .500, D .325.

Part: FRAME — CORRODED (BS 992) · corrosion level 2 · airframe 53,972 hrs · 30,578 cycles

FRAME AT BS 992 HAS AREAS OF CORRODED JUST ABOVE L2 MOPSILL. ACFT GROUNDED. REPAIRED FRAME IAW EA 400 53EA, 15969. THIS IS A CAT B REPAIR WITH TRACKING IAW 400, 53DTI, 15970. INSPECTION THRESHOLD OF 66,000 FLT CYCLES, CURRENT FLT CYCLES AT TIME OF REPAIR IS 30,578, W 1", O .071", R .051", L 5", D .020".

Part: STRINGER — CORRODED (BS 907-1016) · corrosion level 2 · airframe 53,972 hrs · 30,578 cycles

STRINGER 21R AT BS 986 HAS LARGE AREA OF CORROSION. ACFT GROUNDED. REMOVED CORROSION AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-A-1. REMOVED, FABRICATED NEW AND INSTALLED NEW STIFFENER IAW SRM 51-40-02-0G-0, PARA 4 AND 7D SRM 51-40-05-0G-0, FIG 2, W .80", O .040", R 0", L 12.0", D .040".

Part: ANGLE — CRACKED (BS 727A) · airframe 53,972 hrs · 30,578 cycles

INTERCOSTAL AT BS 727A AT 25R HAS A CRACKED ATTACH ANGLE. ACFT GROUNDED. REMOVED ANGLE IAW SRM 51-40-02-0G-0, FIG 8 INSTALLED NEW ANGLE IAW SRM 51-40-02-0G-0, PARA 4.

Part: STRINGER CLIP — CRACKED (BS 947) · airframe 53,972 hrs · 30,578 cycles

STRINGER CLIP AT BS 947 AT 25R IS CRACKED. ACFT GROUNDED. REMOVED, LOCATED AND DRILLED NEW CLIP AND INSTALLED IAW SRM 51-40-02-0G-0, 51-40-05-0G-0.

Part: FRAME — CRACKED (BS 400) · airframe 53,972 hrs · 30,578 cycles

FRAME AT BS 400 BETWEEN STRINGERS 8-9L IS CRACKED. ACFT GROUNDED. REPAIRED THE FRAME IAW TC QAD20062609 400-53-107, FIG 2.

Part: DOOR SILL — CORRODED (BS 908-1016) · corrosion level 2 · airframe 53,972 hrs · 30,578 cycles

L2 MOPSILL HAS AREAS OF CORROSION ON UPPER SURFACE. ACFT GROUNDED. R & R MOPSILL IAW SRM 51-40-02-0G-0 AND DWG NR 65-52878, W 5", O .071", R .060, L 1", D .011".

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 53,972 hrs · 30,578 cycles

BS 986 FLOORBEAM UPPER HORIZONTAL FLANGE HAS AREAS OF CORROSION. ACFT GROUNDED. REPAIRED FLOORBEAM IAW EA 400, 53EA 15973.

Part: ANGLE — CRACKED (BS 500F) · airframe 53,972 hrs · 30,578 cycles

INTERCOSTAL AT BS 500F 26L HAS A CRACKED ANGLE. ACFT GROUNDED. R & R ANGLE IAW SRM 51-40-02-0G-0, PARA 4 AND 7D.

Part: ANGLE — CRACKED (BS 500E) · airframe 53,972 hrs · 30,578 cycles

INTERCOSTAL AT BS 500E AT 26L HAS A CRACKED ANGLE. ACFT GROUNDED. R & R ANGLE IAW SRM 51-40-02-0G-0, PARA 4 AND 7D.

Part: STRINGER — CORRODED (BS 500G) · corrosion level 2 · airframe 53,972 hrs · 30,578 cycles

STRINGER AT BS 500G AT 27R IS CORRODED AROUND DOMENUT. ACFT GROUNDED. REMOVED CORRODED FROM STR 27R AT BS 500G FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03-1A-1, FIG 101, DETAIL II, REPAIRED STR 27R AT BS 500G IAW SRM 53-30-03-2R-1, REPAIR 1, W 1.00, O .063, R .00, L 1.00, D .063.

Part: ANGLE — CRACKED (BS 500F) · airframe 53,972 hrs · 30,578 cycles

INTERCOSTAL AT BS 500F AT 26R HAS A CRACKED ANGLE. ACFT GROUNDED. R & R ANGLE IAW SRM 51-40-02-0G-0, PAR 4 AND 7D.

Part: SPAR — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 53,972 hrs · 30,578 cycles

RIGHT HORIZONTAL STABILIZER AFT UPPER ATTACH LUG, STABILIZER SIDE, HAS CORROSION ON AFT FACE. ACFT GROUNDED. REPAIRED RT HORIZONTAL STABILIZER AFT UPPER ATTACH LOG CORROSION IAW EA COMPARTMENT 55 EA 15987.

Part: ATTACH ANGLE — CRACKED (BS 500E) · airframe 53,972 hrs · 30,578 cycles

INTERCOSTAL AT BS 500E AT 26R HAS A CRACKED ATTACHED ANGLE. ACFT GROUNDED. R & R ATTACH ANGLE IAW SRM 51-40-02-0G-0, PARA 4 AND 7D.

Part: FLOOR SUPPORT — CRACKED (BS 660-666) · airframe 51,041 hrs · 28,795 cycles

FLOOR SUPPORT, LBL 24.82 BETWEEN BS 660 - 666 IS CRACKED. ACFT GROUNDED. REPAIRED IAW EA NR AD20080506-400-57-119.

Part: SKIN — CHAFED (EXHAUST GATE) · airframe 51,041 hrs · 28,795 cycles

RT WING INDB EXHAUST GATE UPPER SKIN IS CHAFED. ACFT GROUNDED. REMOVED EXISTING REPAIR AND INSTALLED NEW REPAIR DOUBLER ON RT WING INBD EXHAUST GATE UPPER SKIN IAW SRM 57-53-01-2R-10, REPAIR 10.

Part: SKIN — CHAFED (LT WING TE LFAP) · airframe 51,041 hrs · 28,795 cycles

LEFT INBD MID FLAP IS CHAFED AT INBD UPPER EDGE. ACFT GROUNDED. REPAIRED LT INBD MID FLAP INBD UPPER SKIN IAW SRM 57-53-01-2R-3.

Part: FRAME — CRACKED (BS 360) · airframe 51,041 hrs · 28,795 cycles

FRAME BS 360 CRACKED BY A SCREW THAT WAS TOO LONG IN NUT PLATE BETWEEN STRINGERS 12 AND 13L. ACFT GROUNDED. REPAIRED FRAME IAW EA 400, 53EA, 13259.

Part: SKIN — CHAFED (EXHAUST GATE) · airframe 51,041 hrs · 28,795 cycles

LEFT WING INBD EXHAUST GATE UPPER OTBD CORNER IS CHAFED. ACFT GROUNDED. REPAIRED EXHAUST GATE IAW SRM 57-53-01-2R-10 ADJUSTMENT CK GOOD IAW MM 27-51-05-404-016 STEP 3.E5.B-F.

Part: LIGHT — BROKEN (LT OVERWING) · airframe 50,271 hrs · 28,327 cycles

AFT OVERWING EXIT DOOR LT SIDE EMERGENCY LIGHT ASSY BROKEN. ACFT GROUNDED. REPLACED AFT LT OVERWING EMERGENCY LIGHT ASSY OPS CHECK GOOD IAW AMM 33-31-01.

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 49,786 hrs · 28,033 cycles

EXIT LAMP COVER FELL OFF AT RT FORWARD OVERWING EXIT. ACFT GROUNDED. RE-INSTALLED EXIT LENSE COVER RT FWD OVERWING EXIT.

Part: SUPPORT — CRACKED (WING) · airframe 47,650 hrs · 26,708 cycles

NR 6 SLAT ACTUATOR DOOR LANDING ON WING BENT. R & R 36 SLAT ACT DOOR LANDING (SUPPORT) IAW SRM 51-40-02-0G-0.

Part: HINGE — CHAFED (RT MLG DOOR) · airframe 47,650 hrs · 26,708 cycles

RT MLG OUTER DOOR AFT HINGE ARM CHAFED. ACFTGROUNDED. R & R RT MLG OUTER DOOR AFT HINGE ARM IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (NR 2 NACELLE) · airframe 47,650 hrs · 26,708 cycles

NR 2 ENG PYLON AFT RT PANEL SUPPORT BRACKET CRACKED ON UPPER END (AFT OF RT MID SPAR ATTACH PIN LUG) ACFT GROUNDED. REMOVED NR 2 OTBD SUPPORT ASSY, FABRICATED NEW ANGLE INSTALLED SUPPORT ASSY IAW SRM 51-40-02 AND 51-40-05-0G 0.

Part: RETAINER — CORRODED (LT MLG) · airframe 47,650 hrs · 26,708 cycles

LT MLG NR 4 LWR BLADE SEAL RETAINER HAS MULTIPLE SPOTS OF CORROSION. ACFT GROUNDED. R & R RETAINER IAW SRM 51-40-05-0G-0, FIG 2, PAGE 5, W .50, O .063, R .056, L 8.0, D 0.007.

Part: WEB — GOUGED (BS 794) · airframe 47,650 hrs · 26,708 cycles

AFT CARGO DOOR CUTOUT LWR FWD REVEAL WEB IS DAMAGED ALONG AFT EDGE. ACFT GROUNDED. FABRICATED NEW REVEAL IAW SRM 51-70-13, OG 0 AND DWG NO 65-56655-2.

Part: FAIRING — CHAFED (MLG) · airframe 47,650 hrs · 26,708 cycles

RIGHT AFT NR 5 MLG SKI JUMP FAIRING IS CHAFED. ACFT GROUNDED.

Part: RETAINER — CRACKED · airframe 47,650 hrs · 26,708 cycles

SEAL RETAINER CRACKED FOR SEAL ON LWR SHELF PANEL AFT OF RT MLG FOUND DURING SEAL REPLACEMENT. ACFT GROUNDED. FABRICATED, LOCATED AND DRILLED NEW RETAINER IAW BDWG 65C35229.

Part: RETAINER — CORRODED · airframe 47,650 hrs · 26,708 cycles

LEFT NR 3 UPPER BLADE SEAL RETAINER IS CORRODED ON BOTTOM SIDE. ACFT GROUNDED. REMOVED CORROSION ON LT NR 3 UPPER BLADE SEAL RETAINER. MATERIAL LOSS FOUND TO BE OUT OF LIMITS. LOCATED AND DRILLED NEW RETAINER IAW SRM 53-60-71-1A-1, FIG 101 AND 51-40-5. NEW RETAINER TO BE INSTALLED ON ASA T/C 400 53FCD 10237 1, W 1.5, O .063, R .056, L 2.0, D .007.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 57,650 hrs · 26,708 cycles

RT INBD FOREFLAP FOUND DENT CLUSTER ON LWR SURFACE STARTING AT 43" FROM INBD END TO 53" AND 2 TO 12" FROM T/E. ACFT GROUNDED. REPAIRED IAW SRM 51-70-10-2R-4, REPAIR 4.

Part: TAB — DAMAGED (LT ELEVATOR) · airframe 47,650 hrs · 26,708 cycles

LEFT ELEVATOR TAB INBD EDGE IS DAMAGED. BONDED REPAIR ON LT ELEVATOR TAB, INBD CORNER EDGE IAW SRM 51-70-17, REPAIR 11.

Part: SEAT — CRACKED (DOOR SEAL) · airframe 47,650 hrs · 26,708 cycles

L1 DOOR FWD UPPER DOOR SEAL LOCATOR IS CRACKED. R & R L1 DOOR FWD SEAL LOCATOR IAW BAC5065, PG 24-27.

Part: SKIN — DENTED (SPOILER) · airframe 47,650 hrs · 26,708 cycles

NR 3 SPOILER UPPER SURFACE DENTED WITH A CREASE LOCATION 4.5 FROM T/E AND 12 FROM INBD END. REPAIRED NR 3 SPOILER UPPER AFT INBD SKIN IAW SRM 51-70-10-2R-4, REPAIR 4.

Part: STRUCTURE — CORRODED (BS 698) · airframe 47,650 hrs · 26,708 cycles

RIGHT WHEEL WELL MANIFOLD ASSY LOWER FWD STRUCTURE HAS BARE METAL AND SURFACE CORRODED, FWD AND AFT SIDES. ACFT GROUNDED. BLENDED CORROSION, FOUND TO BE 100 MATERIAL LOSS IAW SRM 53-60-71. FABRICATED NEW LOWER FWD STRUCTURE IAW SRM 51-40-02. INSTALLED NEW LOWER FWD STRUCTURE IAW SRM 51-40-02.

Part: SKIN — DENTED (BS 1010) · airframe 47,650 hrs · 26,708 cycles

FUSELAGE DAMAGE AFT OF L2 DOOR BOTTOM CORNER. ACFT GROUNDED. REPAIRED FUSELAGE SKIN AFT OF L2 DOOR BOTTOM CORNER STA 1010, STR 15L IAW SRM 53-00-01-2R-35.

Part: FLOORBEAM — CORRODED (BS 727D) · corrosion level 2 · airframe 47,650 hrs · 26,708 cycles

ON REMOVAL OF NR 2 AFT CARGO FLOORBOARD, FOUND FLOOR SPLICE AT BS 727D CORRODED. ACFT GROUNDED. BLENDED AND FOUND TO BE OUT OF LIMITS. FABRICATED, ALODINED, PRIMED AND TOPCOATED NEW FLOORBOARD SPLICE IAW SRM 53-60-53, FIG 101-51-10-02-0G-0, 51-40 05-00-0 AND SOPM 20-41-02.

Part: STRAP — CRACKED (BS 847-867) · airframe 47,650 hrs · 26,708 cycles

AFT CARGO COMPARTMENT UNDER STRAP, FS 847-867 IS CRACKED. ACFT GROUNDED. FABRICATED NEW STRAP STA 847-867, STR 25R IAW SRM 51-40-05-0G-0 STRAP TO BE INSTALLED ON MIG5 5408009.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 47,650 hrs · 26,708 cycles

AFT CARGO DOOR CUTOUT FWD FRAME REPAIR DOUBLER IS CORRODED. FOUND ON REMOVAL OF TRANSITION PANEL. ACFT GROUNDED. R & R AFT CARGO DOOR CUTOUT FWD FRAME AND FACTORY DOUBLER IAW SRM 51-40-02.

Part: STIFFENER — CORRODED (BS 1088-1156) · corrosion level 2 · airframe 47,650 hrs · 26,708 cycles

APU BAY RT TORQUE BOX INLET CUTOUT LOWER STIFFENER IS CORRODED, BS 1118-1127. R & R RT TORQUE BOX INLET CUTOUT LOWER STIFFENER IAW SRM 51-40-05-0G-0 AND 51-40-02-0G-0.

Part: RETAINER — CORRODED · airframe 47,650 hrs · 26,708 cycles

LEFT MLG NR 3 LOWER BLADE SEAL RETAINER HAS BARE METAL. ACFT GROUNDED. R & R LEFT MLG NR 3 LWR BLADE SEAL RETAINER IAW SRM 51-40-05-0G-0, FIG 2, PAGE 5, W 0.50, O 0.063, R 0.054, L 4.0, D 0.009.

Part: STIFFENER — CORRODED (APU BAY) · corrosion level 2 · airframe 47,650 hrs · 26,708 cycles

APU COMPARTMENT RT TORQUE BOX INLET CUTOUT UPPER STIFFENER IS CORRODED STA 1112 TO 1127. ACFT GROUNDED. R & R TORQUE BOX CUT OUT UPPER STIFFENER IAW SRM 51-40-02-0G-0.

Part: WEB — CORRODED (MLG WW) · airframe 47,650 hrs · 26,708 cycles

UPON REMOVAL OF AFT RT LWR MANIFOLD STRUCTURE FOUND WEB TO BE CORRODED. ACFT GROUNDED. REPAIRED RT MLG MANIFOLD WEB IAW EA 400 53, EA 10436, REV NEW DATED 30MAY13.

Part: SUPPORT ANGLE — CRACKED (NR 1 NACELLE) · airframe 47,650 hrs · 26,708 cycles

NR 1 PYLON INBD AFT SUPPORT ANGLE AFT OF FUSE PIN IS CRACKED. ACFT GROUNDED. REMOVED AND INSTALLED NR 1 PYLON INBD SUPPORT ANGLE IAW SRM 51-40-02.

Part: WEB — CRACKED (BS 348.2-351.2) · airframe 47,650 hrs · 26,708 cycles

L1 AFT REVEAL WEB IS CRACKED. FABRICATED NEW WEB L1 AFT REVEAL IAW BAC DWG 65-17685.

Part: CHANNEL — CORRODED (BS 767-6787) · corrosion level 2 · airframe 47,650 hrs · 26,708 cycles

ON REMOVAL OF CARGO SIDEWALL PANEL, FOUND RT TRANSITION PANEL CHANNEL, BS 767-787, CORRODED AROUND FASTENER HOLES. ACFT GROUNDED. R & R TRANSITION PANEL CHANNEL STA 767-787, RBL 22 IAW SRMS 51-40-05-0G-0 AND 51-40-02.

Part: WEB — DAMAGED (BS 700) · airframe 47,650 hrs · 26,708 cycles

RIGHT WHEEL WELL MANIFOLD ASSY UPPER WEB AT 4 O`CLOCK POSITION AFT INBD CORNER DAMAGED. ACFT GROUNDED. R & R RT WW MANIFOLD ASSY UPPER WEB IAW EA 15138 AND EA 400 53EA 10434.

Part: TRANSITION PANEL — CORRODED (BS 727-767) · corrosion level 2 · airframe 47,650 hrs · 26,708 cycles

RT TRANSITION PANEL BS 727 TO 767 CORRODED AROUND FASTENER HOLES. REMOVED, FABRICATED NEW TRANSITION PANEL AND INSTALLED NEW IAW SRM 53-60-53-2R-5, FIG 201 AND SRM 51-40-02.

Part: STRUCTURE — CORRODED (BS 700-710) · airframe 47,650 hrs · 26,708 cycles

RIGHT MLG WHEEL WELL MANIFOLD ASSY LOWER AFT STRUCTURE CORRODED AT 4 O`CLOCK POSITION CORRODED DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-60-71, FIG 101. R & R DAMAGED SECTION OF STRUCTURE IAW SRM 51-40-02.

Part: FLOOR PANEL — CORRODED (BS 727-727D) · corrosion level 2 · airframe 47,650 hrs · 26,708 cycles

ON REMOVAL OF PIT SIDEWALL PANEL FOUND NR 1 FLOOR PANEL RT EDGE TO HAVE LIGHT SURFACE CORROSION. REMOVED CORROSION ON NR 1 FLOOR PANEL MATERIAL LOSS FOUND TO BE OUT OF LIMITS AND FABRICATED NEW FLOOR PANEL IAW SRMS 53-60-53-1A-1 AND 51-40-05-0G-0 W 2.0, O .071, L 8, R 0.0, D .071.

Part: PANEL — CORRODED (BS 727D-727F) · corrosion level 2 · airframe 47,650 hrs · 26,708 cycles

UPON REMOVAL OF PIT SIDEWALL PANEL FOUND NR 2 FLOOR PANEL LT AND RT EDGES TO HAVE LIGHT SURFACE CORROSION. ACFT GROUNDED. REMOVED CORROSION ON AFT PIT NR2 FLOOR PANEL MATERIAL LOSS FOUND TO BE OUT OF LIMITS AND FABRICATED NEW FLOOR PANEL IAW SRM 53-60-53-1A-1 AND 51-40-05-0G-0.

Part: FLOORBEAM — CORRODED (BS 772) · airframe 47,650 hrs · 26,708 cycles

ON DISPLACING AFT CARGO FLOOR PANEL TO REPLACE NUTPLATE ON INCOMING DISCREPANCIES, FOUND FLOOR PANEL SPLICE TEE AT BS 772 TO BE CORRODED. REMOVED CORROSION ON FLOOR PANEL SPLICE TEE AT BS 772, FOUND TO BE OUT OF LIMITS AND FABRICATED NEW TEE IAW SRM 53-60-53-1A-1 AND 51-40-05-0G-0.

Part: SUPPORT — CORRODED (BS 727-787) · airframe 47,650 hrs · 26,708 cycles

ON REMOVAL OF CARGO SIDEWALL PANEL, FOUND LT TRANSITION PANEL, BS 727D-727G CORRODED AROUND FASTENER HOLES. REPAIRED LT TRANSITION PANEL IAW SRM 53-60-53-2R4.

Part: ANGLE — CHAFED (LT WING) · airframe 47,650 hrs · 26,708 cycles

LT WING INBD UPPER T/E SHELF PANEL ATTACH ANGLE CHAFED ON LWR SIDE. ACFT GROUNDED. DAMAGE AREA FOUND TO BE OUT OF LIMITS IAW SRM 57-51-02-1A-1. R & R ANGLE IAW SRM 51-40-02-0G-0.

Part: FLOORBEAM — CORRODED (BS 727F) · corrosion level 2 · airframe 47,650 hrs · 26,708 cycles

ON REMOVAL OF NR 2 FLOORBOARD, FOUND AFT CARGO FLOOR SPLICE AT BS 727F 7.6 CORRODED BLENDED CORROSION, FOUND TO BE OUT OF LIMITS, FABRICATED, ALODINED , PRIMED AND TOPCOATED NEW FLOORBOARD SPLICE IAW SRM 53-60-53-1A-1, FIG 101, 51-10-02-0G-0, 51-40-05-0G-0 AND SOPM 20-41-02, W 4.00, O .070, R .044, L 1.00, D .026.

Part: FLOOR PANEL — CORRODED (BS 727-727D) · corrosion level 2 · airframe 47,650 hrs · 26,708 cycles

UPON REMOVAL OF PIT SIDEWALL PANEL FOUND NR 1 FLOOR PANEL RT EDGE TO HAVE LIGHT SURFACE CORROSION. ACFT GROUNDED. REMOVED CORROSION ON NR 1 FLOOR PANEL MATERIAL LOSS FOUND TO BE OUT OF LIMITS AND FABRICATED NEW FLOOR PANEL IAW SRMS 53-60-53-1A-1 AND 51-40-05-0G-0, W 2.0, O .071, L 8, R 0.0, D .071.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 47,650 hrs · 26,708 cycles

RT INBD FOREFLAP UPPER INBD SURFACE CHAFED. ACFT GROUNDED. REPAIRED RT INBD FOREFLAP UPPER INBD SURFACE IAW SRM 51-70-10-2R-0, REPAIR 4, PARA 20.

Part: SHEAR TIE — CHAFED (RT WING) · airframe 47,650 hrs · 26,708 cycles

RT UPPER FIXED T/E PANEL SHEAR TIE CHAFED INBD NR 6 FLAP TRACK FAIRING. ACFT GROUNDED. REMOVED, FABRICATED NEW ANGLE AND INSTALLED NEW SHEAR TIE IAW SRM 41-50-02-0G 0, STEP 4B.

Part: LIGHT — INOPERATIVE (R1 DOOR SLIDE) · airframe 47,650 hrs · 26,708 cycles

DURING R1 DOOR ESCAPE SLIDE TEST THE LOWER FORWARD EMERGENCY LIGHT DID NOT COME ON AFTER SLIDE DEPLOYMENT. ACFT GROUNDED. SLIDE REPLACED AFTER TEST.

Part: SKIN — DENTED (NR 3 SPOILER) · airframe 47,650 hrs · 26,708 cycles

NR 3 SPOILER OUTER UPPER SURFACE HAS DENT FOUND DURING INSERT REPLACEMENT. REPAIRED NR3 SPOILER UPPER OTBD SKIN IAW SRM 51-70-10-2R-4, REPAIR 4.

Part: WEB — CORRODED (LT MLG WW) · corrosion level 2 · airframe 47,334 hrs · 26,525 cycles

AFTER REMOVING LT WHEEL WELL AFT SKI JUMP ANGLE CORROSION DAMAGED NOTED ON ADJACENT WEB OF MANIFOLD ASSY. ACFT GROUNDED. REMOVED AND REINSTALLED LT WHEEL WELL BLADE TYPE SEALS.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 44,290 hrs · 24,808 cycles

RT WING NR 5 SLAT OUTBD T/E CORNER UPPER AND LOWER SURFACES DELAMINATED. REPAIRED DELAMINATION DAMAGE IAW B737 400 SRM 51 70 10 REPAIR 4 PG 201.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 44,290 hrs · 24,808 cycles

RT WING 4 SLAT I/B TRAILING EDGE WEDGE UPPER SURFACE DELAMINATED. REPAIRED DAMAGED AREA IAW B737 400 SRM 51 70 10 PARA 20.

Part: GUIDE ARM — MALFUNCTIONED (R1 DOOR) · airframe 42,503 hrs · 23,658 cycles

R1 DOOR WILL NOT CLOSE WITH THE HANDLE ALONE. NEEDED TO PUSH TO CLOSE. REPLACED R1 DOOR GUIDE ARM ASSEMBLY IAW 52 41 21.

Part: BOLT — MISSING (R2 DOOR) · airframe 41,956 hrs · 23,316 cycles

FOUND L2 (AFT ENTRY DOOR) OPEN AFTER FLEET SERVICE CLEANING DOOR WILL NOT CLOSE. REMOVED DOOR LINER FOR ACCESS TO DOOR MECHANISIM FOUND BOLT TO PUSHROD AND TORQUE TUBE CRANK NOT INSTALLED. CONNECTED PUSH ROD TO TORQUE TUBE CRANK WITH NEW HARDWARE IAW AMM 52-13-00-705-023 AND ADJUSTED DOOR SNUBBER ASSY IAW AMM 52-13-00-705-001. DOOR CLOSES NORMAL.

Part: ROLLER — LACK OF LUBE (ENTRY DOOR) · airframe 41,167 hrs · 22,854 cycles

F/A REPORTS L2 (AFT ENTRY) DOOR STIFF TO OPEN LUBRICATED L2 DOOR 4EA LATCH ROLLERS AND LATCH CRANK BEARINGS 4EA AND UPPER & LOWER HINGE LINKS AND GUIDE PLATE IAW B737 400 AMM 12 25 11 603 005. L2 DOOR OPERATIONAL TEST GOOD PER B737 400 AMM 52 13 00 700 805.

Part: FILLER — BROKEN (ENTRY DOOR) · airframe 41,113 hrs · 22,830 cycles

F/A REPORTS L2 (AFT ENTRY) DOOR DIFFICULT TO OPEN REMOVED L2 DOOR HANDLE AND TRIM PIECE. REMOVED SMALL PIECE OF BROKEN FOAM HANDLE INSERT. RE-INSTALLED HANDLE & TRIM WITH INSERT. DOOR OPERATES NORMALLY REF B737 400 AMM 52 41 00 705.

Part: EXHAUST GATE — CHAFED (RT WING) · airframe 40,892 hrs · 22,701 cycles

RIGHT I/B EXHAUST GATE UPPER SURFACE CHAFED. TRIMEED DAMAGED SKIN FABRICATED TREATED PRIMED TOP COATED AND INSTALLED REPAIR DOUBLER + FILLERS IAW ASA EA 400 57EA 04516.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,892 hrs · 22,701 cycles

BS 986 FLOORBEAM HAS CORROSION SEVERAL AREAS ON FORWARD FLANGE. REMOVED CORRODED T CAP FABRICATED T CAP TREATED PRIMED TOP COATED AND INSTALLED REPAIR IAW ASA EA 400 53EA 04506.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,892 hrs · 22,701 cycles

AFT PRESSURE BULKHEAD DOME WEB HAS CORROSION JUST AFT OF BS 1016 JUST ABOVE LOWER Y CHORD. CUT OUT DAMAGE AND REPAIRED WEB IAW ASA EA 400 53EA 04475.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,892 hrs · 22,701 cycles

BS 907 FRAME CRACKED BETWEEN STR 8R AND STR 9R. REPAIRED FRAME IAW ASA EA AD20062609 400 53 108 REV NEW DATED 21DEC10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,892 hrs · 22,701 cycles

BS 380 FRAME CRACKED BETWEEM STR 8R AND STR 9R. REPAIRED FRAME IAW ASA EA AD20062609 400 53 108 REV NEW DATED 21DEC10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,892 hrs · 22,701 cycles

BS 747 FRAME CRACKED BETWEEN STR 8L AND 9L. REPAIRED FRAME IAW ASA EA AD20062609 400 53 108 REV NEW DATED 21DEC10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,892 hrs · 22,701 cycles

BS 480 FRAME CRACKED BETWEEN STR 9R AND STR 8R. REPAIRED FRAME IAW ASA EA AD20062609 400 53 108 REV NEW DATED 21DEC10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,892 hrs · 22,701 cycles

BS 827 FRAME CRACKED BETWEEN STR 8R AND STR 9R. REPAIRED FRAME IAW ASA EA AD20062609 400 53 108 REV NEW DATED 21DEC10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,892 hrs · 22,701 cycles

BS 787 FRAME CRACKED BETWEEN STR 8L AND STR 9L. REPAIRED FRAME IAW ASA EA AD20062609 400 53 108 REV NEW DATED 21DEC10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,892 hrs · 22,701 cycles

BS 727F FRAME CRACKED BETWEEN STR 8R AND STR 9R. REPAIRED FRAME IAW ASA EA AD20062609 400 53 108 REV NEW DATED 21DEC10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,892 hrs · 22,701 cycles

BS 827 FRAME CRACKED BETWEEN STR 8L AND STR 9L. REPAIRED FRAME IAW ASA EA AD20062609 400 53 108 REV NEW DATED 21DEC10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,892 hrs · 22,701 cycles

BS 400 FRAME CRACKED BETWEEN STR 8R AND STR 9R. REPAIRED FRAME IAW ASA EA AD20062609 400 53 108 REV NEW DATED 21DEC10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,892 hrs · 22,701 cycles

BS 787 FRAME CRACKED BETWEEN STR 8R AND STR 9R. REPAIRED FRAME IAW ASA EA AD20062609 400 53 108 REV NEW DATED 21DEC10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,892 hrs · 22,701 cycles

BS 907 FRAME CRACKED BETWEEN STR 8L AND STR 9L. REPAIRED FRAME IAW ASA EA AD20062609 400 53 108 REV NEW DATED 21DEC10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,892 hrs · 22,701 cycles

BS 747 FRAME CRACKED BETWEEN STR 8R AND STR 9R. REPAIRED FRAME IAW ASA EA AD20062609 400 53 108 REV NEW DATED 21DEC10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,892 hrs · 22,701 cycles

BS 867 FRAME CRACKED BETWEEN STR 8R AND STR 9R. REPAIRED FRAME IAW ASA EA AD20062609 400 53 108 REV NEW DATED 21DEC10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,892 hrs · 22,701 cycles

B6 867 FRAME CRACKED BETWEEN STR 8L AND STR 9L. REPAIRED FRAME IAW ASA EA AD20062609 400 53 108 REV NEW DATED 21DEC10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,892 hrs · 22,701 cycles

BS 727F FRAME CRACKED BETWEEN STR 8L AND STR 9L. REPAIRED FRAME IAW ASA EA AD20062609 400 53 108 REV NEW DATED 21DEC10.

Part: SKIN — CHAFED (TE FLAP) · airframe 40,892 hrs · 22,701 cycles

LEFT OUTBOARD FLAP LOWER SKIN CHAFED AT T/E JUST INBOARD OF THE INBOARD FLAP TRACK. BONDED REPAIR FILLER AND DOUBLER IAW B737 400 SRM 51 70 10.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,892 hrs · 22,701 cycles

SKIN DENTED ACROSS STRINGER 13L STA 1030. INSTALLED REPAIR DOUBLER IAW AAR EA14233 AND ASA EA 400 53EA 04430.

Part: FAILSAFE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,892 hrs · 22,701 cycles

FAIL SAFE CHORD IS CORRODED AT BS 847 BETWEEN STR 27R AND 26R. REMOVED AND REPLACED FAIL SAFE CHORD IAW B737 400 SRM 51 40 02.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,892 hrs · 22,701 cycles

RADIAL STIFFENER AT BS 1016 LBL 12 AT LOWER "Y" CHORD IS CORRODED. REPAIRED AFT PRESSURE BULKHEAD RADIAL STIFFENER IAW BOEING DRAWING 65C28106.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,892 hrs · 22,701 cycles

AFT PRESSURE BULKHEAD LOWER RADIAL STIFFENER AT RBL 0 HAS CORROSION. REPAIRED AFT PRESSURE BULKHEAD RADIAL STIFFENER IAW BOEING DRAWING 65C28106.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,892 hrs · 22,701 cycles

VERTICAL SILL WEB CORRODED FROM BS 794 TO BS 847. LOCATED DRILLED AND INSTALLED NEW SILL WEB IAW B737 400 SRM 51 40 05.

Part: SKIN — DENTED (TE FLAP) · airframe 40,892 hrs · 22,701 cycles

LT OUTBOARD AFT FLAP LOWER SURFACE DENTED 17 INCHES OUTBOARD OF INBOARD END AND 6.5 INCHES FORWARD OF T/E. REPAIRED DAMAGED AREA IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,892 hrs · 22,701 cycles

INTERCOSTAL FROM BS 827 TO 847 AT STR 27R CRACKED. LOCATED DRILLED AND INSTALLED NEW INTERCOSTAL IAW B737 400 SRM 51 40 05.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 40,892 hrs · 22,701 cycles

AFT DRAIN MAST DOUBLER HAS CORROSION. INSTALLED NEW DRAIN MAST DOUBLER IAW B737 400 SRM 51 40 02.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,892 hrs · 22,701 cycles

FRAME IN FORWARD PIT CORRODED BS 500D STR 28L STR 28R. REMOVED CORROSION FABRICATED REPLACEMENT SHEAR TIE TREATED PRIMED TOP COATED AND INSTALLED IAW B737 400 SRM 53 00 07 FIG 201.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,892 hrs · 22,701 cycles

R1 SILL INNER CHORD HAS CORROSION. REMOVED AND REPLACED R1 INNER SILL CHORD.

Part: SKIN — DENTED (SPOILER) · airframe 40,892 hrs · 22,701 cycles

RT WING NR 7 SPOILER UPPER SURFACE DENTED ON THE REPAIR DOUBLER. REPAIRED NR 7 SPOILER.

Part: RIB — CRACKED (RT WING) · airframe 40,892 hrs · 22,701 cycles

RT WING RIB CHORD AT STA 135 CRACKED BETWEEN STR 2-3 (IN TANK). TRIMMED ROTO PEENED TREATED AND PRIMED LOWER CHORD. FABRICATED TWO FILLERS AND REPAIR T PRIMED TREATED AND INSTALLED REPAIR IAW ASA EA 400 57EA 0443.

Part: RIB — CRACKED (LT WING) · airframe 40,892 hrs · 22,701 cycles

LT WING RIB CHORD STA 135 CRACKED BETWEEN STR 2-3 TRIMMED ROTO PEENED AND TREATED LOWER CHORD. FABRICATED TWO FILLERS TREATED AND INSTALLED REPAIR IAW ASA EA 400 57EA 04433.

Part: SKIN — CHAFED (TE FLAP) · airframe 40,892 hrs · 22,701 cycles

RT WING INBOARD UPPER SURFACE INBOARD EDGE CHAFED. REMOVED DAMAGED SKIN, FABRICATED TREATED PRIMED BONDED REPAIR PARTS AND INSTALLED REPAIR IAW B737 400 SRM 57 53 01 FIG 201.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,892 hrs · 22,701 cycles

CABIN FLOORBEAM STA 344 LBL 44 HAS SURFACE CORROSION. REMOVED DAMAGED CHORD (FLOORBEAM). FABRICATED REPAIR CHORD FILLER AND REPAIR ANGLES. HEAT TREATED PRIMED TOP COATED AND INSTALLED REPAIR IAW ASA EA 400 53EA 04470.

Part: SILL — CORRODED (FUSELAGE) · airframe 40,892 hrs · 22,701 cycles

AFT GALLEY DOOR (R2) MOP SILL CORRODED. REMOVED CORRODED MOP SILL AND INSTALLED NEW SILL IAW B737 400 SRM 51 40 02.

Part: SILL — CORRODED (FUSELAGE) · airframe 40,892 hrs · 22,701 cycles

AFT ENTRY DOOR (L 2) MOP SILLL CORRODED. REMOVED CORRODED MOP SILL AND INSTALLED NEW SILL IAW B737 400 SRM 51 40 02.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,892 hrs · 22,701 cycles

STA 847 FRAME UPPER FLANGE CORRODED. REMOVED CORRODED SECTION AND INSTALLED NEW FRAME SECTION IAW B737 400 SRM 51 40 02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,892 hrs · 22,701 cycles

SHEAR TIE CORRODED ON BOTH SIDES OF FS 747 BETWEEN S26R AND S27R. REPAIRED SHEAR TIE/FRAME IAW ASA EA 400 53EA 04519.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,892 hrs · 22,701 cycles

CABIN FLOORBEAM STA 947 AFT FLANGE AT RBL 30 HAS CORROSION AT FASTENER HOLE. REPAIRED FLOORBEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,892 hrs · 22,701 cycles

CABIN FLOORBEAM STA 967 LBL 16 FWD FLANGE HAS CORROSION. REPAIRED FLOORBEAM UPPER CHORD.

Part: PIN — MISSING (L1 DOOR) · airframe 38,196 hrs · 21,004 cycles

L1 DOOR HARD TO OPEN GUIDE ARM PIN ASSY MISSING SCREW + WASHER. REMOVED & REPLACED PIN SCREW AND WASHER PER 52 11 21 404 0078 002, OPS NORMAL. OK FOR SERVICE.

Part: BULKHEAD — GOUGED (BS 178) · airframe 38,157 hrs · 20,972 cycles

BULKHEAD STATION 178 FOUND 2 GOUGES ON FWD SIDE AND A DENT AND PUNCTURE. TRIMMED OUT DAMAGE REMOVED STRAP FABRICATED FILLER AND DOUBLER AND INSTALLED. REMOVED AND REPLACED STIFFENER.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 37,948 hrs · 20,823 cycles

LEFT I/B FORE FLAP UPPER SURFACE HAS A DELAM 34 INCHES FROM O/B EDGE AND 8.5 FROM T/E. INSTALLED REPAIR FILLER AND DOUBLER.

Part: SKIN — DENTED (SPOILER) · airframe 37,948 hrs · 20,823 cycles

NR 4 SPOILER LOWER SURFACE IS MIDDLE SECTION IS DENTED. INSTALLED REPAIR DOUBLER.

Part: SKIN — DENTED (SPOILER) · airframe 37,948 hrs · 20,823 cycles

NR 4 SPOILER UPPER I/B SURFACE IS DENTED 37 INCHES FROM O/B EDGE 7 INCHES FROM L/E. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER INSTALLED REPAIR.

Part: SKIN — CHAFED (TE FLAP) · airframe 37,948 hrs · 20,823 cycles

RIGHT WING O/B FORE FLAP O/B END L/E CHAFED. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER INSTALLED REPAIR.

Part: SKIN — DENTED (SPOILER) · airframe 37,948 hrs · 20,823 cycles

NR 4 SPOILER LOWER I/B SURFACE HAS DENTS. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER INSTALLED REPAIR.

Part: DOUBLER — DELAMINATED (TE FLAP) · airframe 37,948 hrs · 20,823 cycles

LEFT I/B MID FLAP UPPER SURFACE REPAIR IS DELAMINATING NEXT TO EXHAUST GATE. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER INSTALLED REPAIR.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 37,948 hrs · 20,823 cycles

LEFT O/B AFT FLAP LOWER SKIN DELAMINATED AT I/B EDGE. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER, INSTALLED REPAIR.

Part: SKIN — DAMAGED (TE FLAP) · airframe 37,948 hrs · 20,823 cycles

LEFT O/B FORE FLAP TRAILING EDGE HAS EXPOSED CORE FOR 11 INCHES AT I/B END. REMOVED DAMAGED AREA, FABRICATED FILLER, INSTALLED REPAIR.

Part: SKIN — DENTED (SPOILER) · airframe 37,948 hrs · 20,823 cycles

NR 3 SPOILER LOWER I/B SURFACE HAS DENTS. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER INSTALLED REPAIR.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,948 hrs · 20,823 cycles

AFT PIT THRESHOLD WEB HAS CORROSION. REMOVED CORRODED WEB AND REPLACED WITH NEW WEB.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 37,948 hrs · 20,823 cycles

LEFT INBOARD AFT FLAP UPPER SURFACE OUTBOARD END IS DELAMINATED. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER BONDED REPAIR.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 37,948 hrs · 20,823 cycles

NR 2 SLAT TRAILING EDGE WEDGE IS DELAMINATED AT THE O/B EDGE. REMOVED DELAMINATED AREA SKIN AND CORE FABBED REPAIR PARTS AND BONDED REPAIR.

Part: WEB — GOUGED (CARGO BAY) · airframe 37,948 hrs · 20,823 cycles

AFT CARGO COMPARTMENT THRESHOLD SUPPORT BEAM VERTICAL WEB HAS GOUGES ON OUTBOARD FACE OF WEB. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPLACEMENT WEB.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 37,948 hrs · 20,823 cycles

L1 DOOR FRAME BEAR STRAP IS CRACKED AT LOWER HINGE LOWER INSPECTION FASTENER. FABRICATED FILLER AND DOUBLER AND INSTALLED REPAIR.

Part: WEB — CORRODED (CARGO BAY) · corrosion level 2 · airframe 37,948 hrs · 20,823 cycles

AFT CARGO DOOR CUTOUT CLOSEOUT WEB HAS CORROSION AROUND NUT PLATE HOLE TOP AND BOTTOM SIDE. REMOVED DAMAGED WEB, FABBED REPLACEMENT WEB AND INSTALLED WEB.

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 37,948 hrs · 20,823 cycles

L1 DOOR UPPER HINGE LOWER FITTING IS CRACKED. REMOVED AND REPLACED UPPER HINGE FITTING MODIFIED AND INSTALLED PARTS.

Part: FLAP TRACK — CORRODED (NR 1 FLAP) · airframe 35,845 hrs · 19,541 cycles

ALL BEARING SURFACES OF NR 1 FLAP TRACK CORRODED. REMOVED CORROSION FLAP PEENED AND APPLIED TEMPORARY COATING PER OHM 57-53-15 EA 400-57EA-00291 AND EA 5750-01485

Part: FLAP TRACK — CORRODED (NR 2 FLAP) · airframe 35,845 hrs · 19,541 cycles

ALL BEARING SURFACES OF NR 2 FLAP TRACK CORRODED. REMOVED CORROSION FLAP PEENED AND APPLIED TEMPORARY COATING PER OHM 57-53-15-EA-400-57EA-00291 AND EA 5750-01485.

Part: FLAP TRACK — CORRODED (NR 7 FLAP) · airframe 35,845 hrs · 19,541 cycles

ALL BEARING SURFACES OF NR 7 FLAP TRACK CORRODED. REMOVED CORROSION FLAP PEENED AND APPLIED TEMPORARY COATING PER OHM 57-53-15 EA 400-57EA-00291 AND EA 5750-01485.

Part: DOOR — LACK OF LUBE (R1) · airframe 35,072 hrs · 19,102 cycles

F/A'S REPORT, DOOR R1 HAS LARGE GAP WHEN CLOSED. CHECKED R1 DOOR, FOUND THE DOOR LINER UPPER TRIM COVERING NOT FLUSH WITH DOOR CUTOUT. OPS CK DOOR, FOUND DOOR HARD TO CLOSE AND UPPER DOOR PNL DIDN'T CLOSE PROPERLY. LUBED DOOR PER T C 43152005, POST LUBE CK GOOD. DOOR CLOSES SMOOTH AND UPPER DOOR PNL CLOSES.

Part: CUSP WEB — DAMAGED (BS 380) · airframe 34,196 hrs · 18,639 cycles

CUSP WEB IS CREASED AT STA 380 LT SIDE. REMOVED DAMAGED AREA FABBED AND INSTALLED REPAIR IAW SRM 51 70 13 FIG 1.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 34,196 hrs · 18,639 cycles

RT OTBD AFT FLAP HAS A DENT 23 INCHES FROM INBD END ON UPPER SURFACE. REMOVED DAMAGED SKIN FABBED FILLER SKIN AND EXTERNAL DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 PARA'S 20 22 PGS 254 257.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 34,196 hrs · 18,639 cycles

FWD CARGO DOOR EXTERNAL SKIN HAS CREASE. REMOVED DAMAGED AREA OF SKIN FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 52 00 01 REPAIR 2.

Part: SKIN — DENTED (CARGO DOOR) · airframe 34,196 hrs · 18,639 cycles

AFT CARGO DOOR HAS 10 EA DENTS. REMOVED CARGO DOOR SKIN FABRICATED AND INSTALLED REPLACEMENT SKIN IAW B737 400 SRM 52 30 01 PG 201.

Part: SILL — CORRODED (BS 800-827) · corrosion level 2 · airframe 34,196 hrs · 18,639 cycles

AFT CARGO DOOR CUTOUT SILL WEB IS CORRODED. REMOVED CORRODED WEB AND INSTALLED NEW WEB IAW SRM 51 40 02 PG 3.

Part: SKIN — DENTED (NR 5 SPOILER) · airframe 34,196 hrs · 18,639 cycles

NR 5 SPOILER DENTED ON UPPER SURFACE CENTER TRAILING EDGE. PREPPED AREA FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: WEDGE — DENTED (TE FLAP) · airframe 34,196 hrs · 18,639 cycles

LT INBD MID FLAP TRAILING EDGE HAS NUMEROUS DENTS. PREPPED DAMAGED AREA FABRICATED AND INSTALLED REPAIR DOUBLERS IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — PUNCTURED (RT WING FLAP) · airframe 34,196 hrs · 18,639 cycles

SEVERAL DENTS ON RT INBD FORE FLAP SKIN PUNCTURED. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR GENERAL.

Part: SKIN — DENTED (NR 6 SPOILER) · airframe 34,196 hrs · 18,639 cycles

NR 6 SPOILER UPPER SURFACE DENTED ABOVE INBD HINGE. PREPPED AREA FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (SPOILER) · airframe 34,196 hrs · 18,639 cycles

NR 5 SPOILER DENTED AT UPPER OTBD SURFACE. PREPPED AREA FABRICATED AND INSTALLED REPAIR DOUBLERS IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (LT WING FLAP) · airframe 34,196 hrs · 18,639 cycles

DENT ON LT INBD FORE FLAP LOWER SKIN. SKIN IS PUNCTURED. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR GENERAL.

Part: SKIN — DENTED (SPOILERS) · airframe 34,196 hrs · 18,639 cycles

NR 6 SPOILER UPPER SURFACE HAS PROTRUDING DENTS ABOVE BLADE SEAL. PREPPED AREA FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (SPOILER) · airframe 34,196 hrs · 18,639 cycles

NR 7 SPOILER UPPER SURFACE HAS PROTRUDING DENTS. PREPPED AREA FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM REPAIR 4.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 34,196 hrs · 18,639 cycles

RT HORIZONTAL STABILIZER LEADING EDGE IS DENTED. REMOVED DAMAGED AREA OF SKIN FABRICATED AND INSTALLED REPAIR SKIN AND SPLICE PLATES IAW B737 400 SRM 55 10 01 REPAIR 12.

Part: SKIN — DAMAGED (FORE FLAP) · airframe 34,196 hrs · 18,639 cycles

LT INBD FORE FLAP HAS NUMEROUS DENTS ON LOWER SURFACE. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR GENERAL.

Part: SKIN — DENTED (SPOILER) · airframe 34,196 hrs · 18,639 cycles

NR 7 SPOILER UPPER SURFACE DENTED OTBD OF INBD HINGE. PREPPED AREA FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (BS 322-334) · airframe 34,196 hrs · 18,639 cycles

DENT FOUND ON FUSELAGE BELOW R1 DOOR. REMOVED DAMAGED AREA OF SKIN FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLER IAW ASA EA5330 02347.

Part: SKIN — DENTED (BS 380 S16-17L) · airframe 34,196 hrs · 18,639 cycles

DENT ON FUSELAGE SKIN AT STA 380 STR 16L 17L. REMOVED DAMAGED SECTION OF SKIN FABRICATED AND INSTALLED REPAIR FILLER DOUBLER AND TRIPLER IAW ASA EA5330 02346.

Part: SKIN — DENTED (BS 322-334) · airframe 34,196 hrs · 18,639 cycles

CORRECTION TO MFR'S PART NUMBER. DENT FOUND IN FUSELAGE BELOW R1 DOOR. REMOVED DAMAGED AREA OF SKIN FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLER IAW ASA EA5330 02347.

Part: PIN — MISSING (L1 DOOR) · airframe 33,428 hrs · 18,243 cycles

COULD NOT OPEN FORWARD PAX ENTRY (L1) DOOR (PRESUMABLY FROM THE INSIDE). REPLACED MISSING DOOR GUIDE ARM RETAINING RING PIN. DOOR THEN FUNCTIONED OK.

Part: LINER — LOOSE (L1 DOOR) · airframe 31,371 hrs · 17,129 cycles

L1 FWD ENTRY DOOR JAMMED ON ARRIVAL AT YVR. UNJAMMED DOOR LINING AND REMOVED FOR INSPECTION OF CONTROL RODS DOOR CAM AND DOOR JAMB LATCHING ROLLERS PER AMM 52-11-00. DOOR OPERATION CHECKED NUMEROUS TIMES AND UNABLE TO DUPLICATE. AIRCRAFT PRESSURIZATION CARRIED OUR PER AMM 21 00 05 AND NO AIR LEAKS FOUND. AIRCRAFT CONSIDERED SERVICABLE FOR FLIGHT.

Part: SKIN — PUNCTURED (SPOILERS)

OKC - FOUND NR 5 SPOILER PUNCTURED ON LOWER SURFACE 4 INCHES FROM T/E 33 INCHES FROM INBOARD END. REPAIRED DAMAGED AREA IAW ASA EA 5770-01067

Part: WEDGE — DENTED (TE FLAP)

OKC - RIGHT INBOARD MID FLAP T/E WEDGE DENTED IN SEVERAL AREAS. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW B737-400 SRM 51-70-10. (M)

Part: SKIN — DENTED (FS 500E)

OKC - FOUND FUSELAGE SKIN DENTED AT BS 500E PLUS 14 INCHES. REMOVED DAMAGED SECTION OF SKIN, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW ASA EA 5330-02039. (M)

Part: SKIN — DENTED (FORE FLAP)

OKC - RIGHT INBOARD FORE FLAP DENTED ON LOWER SIDE 14 INCHES FROM INBOARD SIDE 7 INCHES FROM TRAILING EDGE. PREPPED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737-400 SRM 51-70-10 REPAIR 2. (M)

Part: SKIN — DENTED (TE FLAP)

OKC - FOUND RIGHT INBOARD AFT FLAP DENTED ON LOWER SIDE 1 INCH FROM TRAILING EDGE. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW B737-400 SRM 51-70-10. (M)

Part: SKIN — GOUGED (FS 804-830)

OKC - FOUND FUSELAGE SKIN AND SKIN DOUBLER AT BS 807, STRINGER 26-27R GOUGED. REMOVED DAMGAED AREA OF SKIN. REMOVED PREVIOUSLY INSTALLED REPAIR PARTS. FABRICATED AND INSTALLED REPAIR PIECES IAW ASAEA 5360-01051. (M)

Part: FLOORBEAM — MAINT ERROR (BS 787)

OKC - FOUND FLOORBEAM AT BS 787 HAS HOLE DRILLED THROUGH LOWER CHORD RADIUS AT RBL 15. TRIMMED LOWER FLANGE TO REMOVE DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES, STRAP AND FILLER IAW ASA EA 5360-01050. (M)

Part: SKIN — DELAMINATED (TE FLAP)

OKC - RIGHT OUTBOARD AFT FLAP TRAILING EDGE DELAMINATED AT INBOARD SIDE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW B737-400 SRM 51-70-10 REPAIR 4. (M)

Part: SKIN — DELAMINATED (TE FLAP)

OKC - FOUND LEFT INBOARD AFT FLAP OUTBOARD T/E WEDGE IS DELAMINATED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW B737-400 SRM 51-70-10 REPAIR 4. (M)

Part: SKIN — DENTED (TE FLAP)

OKC - FOUND RIGHT INBOARD AFT FLAP HAS SHARP DENT ON THE LOWER SIDE OF FLAP 6 INCHES L/E, 10 INCHES FROM INBOARD END. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER MATERIAL IAW B737-400 SRM 51-70-10 REPAIR 2. (M)

Part: SKIN — DENTED (TE FLAP)

OKC - FOUND LEFT INBOARD AFT FLAP L/E DENTED AT INBOARD END. REMOVED AND REPLACED SKIN SECTION IAW B737-400 SRM 51-40-02. (M)

Part: FRAME — CRACKED (FS 294)

OKC - FOUND CABIN FUSELAGE FRAME AT BS 294.5 CRACKED BETWEEN STRINGER 2 AND 3 LEFT. REMOVED AND REPLACED FRAME SECTION IAW B737-400 SRM 51-10-02 AND 51-40-02 FIGURE 8. (M)

Part: SILL — CORRODED (FS 914-1006)

OKC - FOUND CORROSION ON R2 DOOR THRESHOLD MOPSILL, INNER CHORD. REMOVED AND REPLACED R2 DOOR THRESHOLD MOPSILL IAW B737-400 SRM 53-60-15 FIG 101 DETAIL 5, AND SRM 51-40-02, 51-40-05 AND 51-40-08. (M)

Part: FLAP — CHAFED (LT TE FLAP) · airframe 26,578 hrs · 14,501 cycles

LT OB MID FLAP CHAFED ON L/E IB SIDE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM. (K)

Part: FLAP — CHAFED (LT TE FLAP) · airframe 26,578 hrs · 14,501 cycles

LT OB FORE FLAP CHAFED ON L/E 1 INCH FROM IB SIDE. REMOVED AND REPLACED CHAFED SECTION OF L/E IAW SRM. (K)

Part: WEB — CRACKED (FUSELAGE) · airframe 26,578 hrs · 14,501 cycles

FLOOR WEB CRACKED AT BSTA 990, RBL 39, WL 208. REMOVED CRACKED WEB, FRABRICATED AND INSTALLED REPLACEMENT WEB IAW SRM. (K)

Part: SKIN — DENTED (FUSELAGE) · airframe 26,578 hrs · 14,501 cycles

FUSELAGE SKIN DENTED AT BSTA 995 BETWEEN STRINGER 13-14 LT. REMOVED SKIN AT BSTA 986.5-1016, STRINGER 10-14 LT, FABRICATED AND INSTALLED REPLACEMENT SKIN IAW DWG AND SRM. (K)

Part: CONTROL PANEL — UNKNOWN (APU FIRE DETECT)

LAX - ENGINE FIRE DETECT `FAULT LIGHT` FLICKERED ON AND OFF IN FLIGHT, DID NOT TURN ON MASTER CAUTION LIGHT. REMOVED AND REPLACED ENGINE AND APU FIRE CONTROL PANEL PER AMM 26-10-02. SYSTEM CHECKED GOOD PER AMM 26-11-00. TESTED NORMAL. (M)

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 24,821 hrs · 13,481 cycles

OPEN HOLES IN FLOOR SUPPORT. REMOVED DAMAGED AREA AND REPAIRED. (K)

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 24,821 hrs · 13,481 cycles

CORROSION ON FRAME SHEAR TIE B-STA 500C BETWEEN BETWEEN 28L-29R. REPAIRED IAW SRM. (K)

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 24,821 hrs · 13,481 cycles

CORROSION ON CARGO TRACK TIE DOWN AT STA 947, RBL 13, WL 179. REMOVED AND REPLACED. (K)

Part: SKIN — DENTED (BS1003-1016) · airframe 26,578 hrs · 14,501 cycles

SKIN HAS 5 EACH DENTES AT BSTA 1003-1016. REMOVED SKIN AT BSTA 986.51016, STRINGER 10-14 RT, FABRICATED AND NSTALLED REPALCEMENT SKIN IAW DWG AND IAW SRM. (K)

Part: FRAME — CRACKED (FUSELAGE)

OAK - AFT CARGO FRAME AT BS 794.3 HAS DAMAGE FROM STOP DRILLING, PER EA 5310-02274, PERMANENT REPAIR TO BE ACCOMPLISHED AT C-CHECK. REMOVED STOP DRILL DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND FILLER REPAIR REF SRM 51-70-11 PAGES 1-5. (M)

Part: ANGLE — CRACKED (NR 2 PYLON)

DURING C-CHECK, FOUND CRACKED ANGLE ON NR 2 PYLON OUTBOARD SIDE COMMON TO UPPER T/E PANEL. REPAIRED IAW SRM. (M)

Part: STRAP — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON STRAP AT NUT-PLATE LOCATION AT BS 842-852, RBL 19.5 AND WL 155. REPAIRED IAW SRM. (M)

Part: STRAP — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON STRAP AT NUT-PLATE AT BS 787-794, RBL 19.5 AND WL 155. REPAIRED IAW SRM. (M)

Part: SKIN — DENTED (PAX DOOR)

DURING C-CHECK, FOUND DENT ON AFT DOOR SKIN. REPAIRED IAW SRM. (M)

Part: ARM — DAMAGED (LT MLG)

SEA - DURING LINE CHECK, FOUND LEFT MAIN LANDING GEAR ACTUATOR BEAM ARM ASSEMBLY TO HAVE A DISCONTINUITY. REMOVED AND REPLACED LEFT MLG ACTUATOR BEAM ARM ASSEMBLY. (M)

Part: STRINGER — DAMAGED (FUSELAGE)

PAE - DURING C-CHECK, FOUND DAMAGED STRINGER AT BS 486. REPAIRED STRINGER 1 AT BS 486 PER SRM. (M)

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE)

PAE - DURING INSPECTION, FOUND AFT CARGO FLOOR SUPPORT AT BS 767 AND RIB LINE 10 HAS HOLES FROM TEMPORARY REPAIR. REPAIRED AFT CARGO FLOOR SUPPORT AT BS 740-780 AND RIB LINE 10 IAW SRM 53-00-03 AND ASA EA 5320-01378. (M)