N754AS

Part: BULLNOSE — CRACKED (NR 2 SPOILER) · airframe 67,185 hrs · 38,632 cycles

NR 2 SPOILER INBD HINGE BULLNOSE IS CRACKED, INBD OF HINGE ON TOP OF WING. ACFT GROUNDED. R & R NR 2 SPOILER INBD OF HINGE BULLNOSE PANEL IAW SRM 51-40-02 AND 51-40-05.

Part: STIFFENER — CRACKED (RAM AIR INLET) · airframe 67,185 hrs · 38,632 cycles

DURING DISASSEMBLING OF RT RAM AIR INLET LOWER DUCT WALL ASSY, FOUND LOWER WEB UPPER STIFFENER ANGLE RADIUS CRACKED. FABRICATED NEW STIFFENER IAW SRM 51-40-05-06-0.

Part: ANGLE — CORRODED (BS 867-947) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

AFT CARGO BAY RT TRANSITION ANGLE CORRODED FROM BS 867 - 947. REPAIRED IAW SRM 53-60-53-2R-S.

Part: BULKHEAD WEB — CORRODED (MLG WW) · airframe 67,185 hrs · 38,632 cycles

RIGHT MLG WW WEB HAS CORROSION ON AFT SIDE. REMOVED CORRODED WEB, FABRICATED, TREATED RESTORED FINISH AND INSTALLED. REPAIR WEB AND REPAIR PARTS IAW EA NR 400-53EA-10802.

Part: STRINGER CLIP — CORRODED (BS 727G) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

STRINGER CLIP 25L CORRODED AT BS 727G. ACFT GROUNDED. REMOVED STRINGER CLIP, BLEND CORRODED, FOUND OUT OF LIMITS, FABRICATED NEW STRINGER CLIPD AND INSTALLED IAW SRM 53-00-07-1A-1, FIG 101, 51-40-02-0G-0, 51-40-05-0G-0, 51-10-02-0G-0, AMM 51-21-21 307-014 AND 51-21-99-307-022 AND DWG 69-35352-7.

Part: CARGO TRACK — CORRODED (BS 773) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO TRACK RBL 13.8, CORRODED AT BS 773. REPAIRED AFT CARGO TRACK IAW EA 400-53EA-11683.

Part: CARGO TRACK — CORRODED (BS 926-945) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

AFT CARGO BAY, CARGO TRACK LBL 3 IS CORRODED BS 926-945. REPAIRED CARGO TRACK IAW SRM 53-00-53-2R-1, FIG 201.

Part: SUPPORT — CORRODED (BS 992) · airframe 67,185 hrs · 38,632 cycles

LEFT GALLEY SUPPORT ANGLE IS CORRODED AT STA 992, LBL 32. ACFT GROUNDED. LOCATED AND DRILLED NEW GALLEY SUPPORT ZEE IAW SRM 51-40-05, FABRICATED MIG 5 5418352.

Part: ANGLE — CORRODED (BS 727G-807) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO FLOOR STRUCTURE LT TRANSITION ANGLE CORRODED IN MULTIPLE AREAS ON UPPER AND LWR SURFACES FROM BS 727G TO 807. ACFT GROUNDED. R & R LT TRANSITION ANGEL IAW SRM 51-40-02-0G-0.

Part: FRAME — CORRODED (BS 460) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

FRAME BS 460 HAS CORROSION BETWEEN S26-27R. REPAIRED FRAME IAW SRM 53-00-07-2R-3.

Part: CHANNEL — CORRODED (BS 767-794) · airframe 67,185 hrs · 38,632 cycles

RT TRANSITION CHANNEL BS 767 - 794 IS CORRODED ON BOTTOM SIDE AT NUTPLATES. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS, LOCATED AND DRILLED NEW RT TRANSITION CHANNEL IAW SRMS 53-60-53-1A-1, AND 51-30-01-0G-0.

Part: ANGLE — CORRODED (BS 947 BULKHEAD) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO BAY BS 947, LOWER BULKHEAD SUPPORT ANGLE IS CORRODED LBL 20 TO RBL 20. REMOVED ANGLE IAW SRM 51-40-02. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-0I-1. INSTALLED NEW ANGLE IAW SRM 51-40-02.

Part: BULKHEAD WEB — CORRODED (LT MLG WW) · airframe 67,185 hrs · 38,632 cycles

LEFT MLG WW BULKHEAD WEB HAS MULTIPLE AREAS OF CORROSION AROUND LOWER ROW OF RIVETS ON AFT SIDE. R & R BULKHEAD WEB SECTION IAW EA 400-53EA-10802.

Part: CARGO TRACK — CORRODED (BS 825) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

AFT CARGO TRACK LBL 8.1 CORRODED ON LOWER SURFACE AT BS 825. REMOVED CORROSION FROM CARGO TRACK. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-1A, DETAIL V. REPAIRED.

Part: ANGLE — BENT (BS 727) · airframe 67,185 hrs · 36,832 cycles

BS 727, BULKHEAD AFT SIDE, RT UPPER OTBD SIDE WALL SUPPORT ANGLE BENT. ACFT GROUNDED. R & R ANGLE IAW SRM 51-40-02-0G-0.

Part: MOUNT — CORRODED (GALLEY) · airframe 67,185 hrs · 38,632 cycles

LEFT FWD G4 GALLEY MOUNT IS CORRODED. BLENDED GALLEY MOUNTS AND FOUND TO BE OUT OF LIMITS, RECEIVED NEW MOUNT IAW SRM 53-60-51-1A-1.

Part: MOUNT — CORRODED (FWD GALLEY) · airframe 67,185 hrs · 38,632 cycles

RIGHT FWD G4 GALLEY MOUNT IS CORRODED. BLENDED RT FWD G4 GALLEY MOUNT AND FOUND TO BE OUT OF LIMITS, INSTALLED NEW MOUNT IAW SRM 53-60-51-1A-1.

Part: CARGO TRACK — CORRODED (BS 727D) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO TRACK AT RBL 8.1 CORRODED ON LOWER SURFACE AT BS 727D. REPAIRED IAW EA 400-53EA-11673, REV NEW.

Part: ANGLE — CORRODED (LT MLG WW) · airframe 67,185 hrs · 38,632 cycles

LEFT MLG WW UPPER ANGLE HAS CORROSION. R & R UPPER ANGLE IAW SRM 51-40-02-0G-0.

Part: STRUCTURE — CHAFED (LT WING) · airframe 67,185 hrs · 38,632 cycles

LEFT WING T/E IS CHAFED JUST INBD INBD FLAP, OTBD TRACK TORQUE TUBE ACCESS PANEL, PN 65-69646-150. BLENDED PANEL, FOUND TO BE OUT OF LIMITS, FABRICATED, LOCATED AND DRILLED NEW PANEL FOR LT WING TORQUE TABS ACCESS PANEL IAW SRM 57-02-1A-1 AND SRM 51-40-02-0G-0.

Part: SUPPORT — CORRODED (BS 887) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO BAY SIDEWALL SUPPORT ATTACHED TO FRAME BS 887 CORRODED AROUND LOWER FASTENER HOLES. BLENDED AREAS FOUND TO BE OUT OF LIMITS, FABRICATED NEW SUPPORT AND INSTALLED IAW SRM 53-00-07-1A-1, 51-30-01-0G-0, 51-40-02-0G-0.

Part: STRINGER — CORRODED (BS 1129-1156) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

APU BAY RT SIDE AFT SIDE OF INTAKE OPENING LWR STRINGER CORRODED ON FWD END CORRODED FOUND TO BE 100 MATERIAL LOSS RECEIVED NEW STRINGER, LOCATED, DRILLED, RESTORED FINISH AND INSTALLED IAW SRM 53-80-13-1A-2.

Part: CARGO TRACK — CORRODED (BS 897-945) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO BAY, CARGO TRACK RBL 13.8 CORRODED BS 897 - 945. REPAIRED CARGO TRACK IAW SRM 53-00-53-2R-2.

Part: CARGO TRACK — CORRODED (BS 727D) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

AFT CARGO TRACK AT RBL 3 CORRODED ON LOWER SURFACE AT BS 727D. REMOVED CORROSION , FOUND TO BE OUT OF LIMITS IAW SRM 53-60 53-1A-1. REPAIRED.

Part: INTERCOSTAL — CORRODED (BS 270) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

DURING REMOVAL OF NLG VIEWING WINDOW SUPPORT FOUND INTERCOSTAL REPAIR AT BS 270, LBL 12 TO RBL 12 WITH CORROSION ON REPAIR AND INTERCOSTAL. REMOVED CORROSION ON INTERCOSTAL, MATERIAL LOSS FOUND TO BE OUT OF LIMITS, REPLACED INTERCOSTAL IAW SRMS 51-40-02-0G-0, W 2.0, O .051, R .040, L 4., D .011.

Part: MOUNT — CORRODED (LAVATORY FLOOR) · airframe 67,185 hrs · 38,632 cycles

AFT LAV MOUNT, RBL 51.55, BS 947 IS CORRODED. MEASURED DAMAGE AREA FOUND TO BE OUT OF DWG TOLERANCE, INSTALLED NEW AFT LAV MOUNT IAW DWG 69-77308.

Part: SUPPORT — CORRODED (BS 986-1016) · airframe 67,185 hrs · 38,632 cycles

LEFT GALLEY GUTTER LBL 32, BS 986 -1016 HAS CORROSION. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT LIMIT IAW SRM 53-60-51-1A-1. FABRICATED NEW LT GALLEY GUTTER.

Part: DOOR FRAME — CORRODED (BS 847) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

AFT CARGO DOOR CUTOUT AFT SIDE HAS AREAS OF CORRODED. R & R AFT CARGO DOOR FRAME BS 847 IAW SRM 51-40-02-0G-0 AND DWG 65-47960.

Part: SUPPORT — CORRODED (LT MLG WW) · airframe 67,185 hrs · 38,632 cycles

LEFT MLG WW LOWER FWD INBD FAIRING SUPPORT HAS CORROSION. R & R SUPPORT IAW SRM 51-40-02-0G-0.

Part: FRAME — CORRODED (BS 794) · airframe 67,185 hrs · 38,632 cycles

CORROSION ON AFT SIDE OF FRAME IN AFT CARGO BAY UNDER LOWER SILL WEB FWD END BS 794, STR 25R. REMOVED CORROSION IAW SRM 57-10-02 AND 51-40-02-0G-0.

Part: STRAP — DAMAGED (TAILCONE) · airframe 67,185 hrs · 38,632 cycles

TAILCONE REINFORCEMENT STRAP DAMAGED AT LT SIDE APU AUGMENTOR TUBE ATTACH. ACFT GROUNDED. R & R REINFORCEMENT STRAP IAW SRM 51-40-02-0G-0.

Part: SPLICE — CORRODED (CARGO TRACK) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO TRACK AT LBL 17.2 SPLICE ANGLE CORRODED AT BS 761. R & R SPLICE ANGLE IAW SRM 53-00-53-2R-2.

Part: FRAME — CORRODED (BS 480) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

FRAME BS 480 HAS CORROSION BETWEEN S26-27R. REPAIRED FRAME IAW SRM 53-00-07-2R-3.

Part: CHANNEL — CORRODED (L1 DOORWAY) · airframe 67,185 hrs · 38,632 cycles

L1 DOOR MOPSILL HAS CORROSION FROM BS 300-347. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-1A-1. R & R MOPSILL IAW SRM 51-40-02-0G-0.

Part: CARGO TRACK — CORRODED (BS 926-945) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO BAY, CARGO TRACK RBL 8.1 CORRODED, BS 926 - 945. REPAIRED CARGO TRACK IAW SRM 53-00-53-2R-1, FIG 201.

Part: CARGO TRACK — CORRODED (BS 767E) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO TRACK LBL 12.50. CORRODED AT BS 767E. REPAIRED CARGO TRACK IAW SRM 53-00-53-2R-1.

Part: CARGO TRACK — CORRODED (BS 767) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO TRACK LBL 3, CORRODED AT BS 767. REPAIRED CARGO TRACK IAW SRM 53-00-53-2R-1.

Part: ANGLE — CORRODED (BS 727-727F) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

AFT CARGO FLOOR STRUCTURE RT TRANSITION ZEE CORRODED IN MULTIPLE AREAS ON UPPER AND LWR SURFACES FROM BS 727 TO STA 727F. R & R TRANSITION ANGLE IAW SRM 51-40-02-0G-0.

Part: CARGO TRACK — CORRODED (BS 897-947) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO BAY, CARGO TRACK LBL 17.2 CORRODED BS 897 - 947. R & R CARGO TRACK IAW SRM 53-00-53-2R-2, FIG 201 AND 51-40-02-0G-0, PARA 7.

Part: CHANNEL — CORRODED (L2 DOOR) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

MOP SILL CORRODED AT L2 DOOR LOWER SEAL AREA, BS 948 - 990. R & R MOP SILL IAW SRM 51-40-02-0G-0.

Part: BAFFLE — CORRODED (BS 867-887) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO BAY BAFFLE IS CORRODED, BS 867-887. LOCATED & DRILLED NEW BAFFLE IAW SRM 51-10-02-0G-0.

Part: SUPPORT BRACKET — CORRODED (BS 947) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO BAY, BULKHEAD SUPPORT BRACKET CORRODED BS 947 FROM S22-26L. BLENDED AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 53-60-53-01-1, FIG 101 & 51-40-02-0G-0.

Part: SKIN — CORRODED (VERTICAL STAB) · airframe 67,185 hrs · 38,632 cycles

VERTICAL STABILIZER PANEL 9562 CORRODED. FABRICTED NEW PANEL AND RESTORED FINISH IAW DWG 65C25922 & AMM 51-21-21-307-014 AND AMM 51-21-99-307-022.

Part: INTERCOSTAL — CORRODED (BS 792) · airframe 67,185 hrs · 38,632 cycles

DURING REMOVAL OF FRAME FOUND CORROSION ON INTERCOSTAL BS 792, S25R. R & R INTERCOSTAL IAW SRM 51-40-2-0G-0 AND DWG 65-47959.

Part: DOOR FRAME — CORRODED (BS 794-847) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO DOOR CUTOUT HAS AREAS OF CORRODED ON FWD AND BOTTOM SIDES. R & R WEB IAW SRM 51-40-02-0G-0.

Part: CARGO TRACK — CORRODED (AFT CARGO BAY) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO, CARGO TRACK RBL 3 IS CORRODED BS 817 TO 947. REMOVED DAMAGED CARGO TRACK AND REPLACED IAW SRM 53-00-53-2R-1 AND SRM 51-40-02.

Part: SILL — CORRODED (R2 DOOR) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

AFT R2 DOOR LOWER SILL CORRODED AT BS 947.5 - 990. R & R R2 DOOR SILL IAW SRM 51-40-02-0G-0.

Part: SUPPORT — CORRODED (BS 947-967) · airframe 67,185 hrs · 38,632 cycles

RIGHT LAVATORY SUPPORT BS 947-967, RBL 24 HAS CORROSION AROUND FASTENER HOLES. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51-1A-1. LOCATED AND DRILLED NEW SUPPORT IAW SRM 51-40-05-0G-0 AND SRM 51-40-02-0G-0.

Part: ANGLE — CORRODED (BS 727E-727G) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO FLOOR STRUCTURE LT TRANSITION ANGLE CORRODED IN MULTIPLE AREAS ON UPPER AND LWR SURFACES FROM BS 727E TO 727G4. ACFT GROUNDED. R & R ANGLE IAW SRM 51-40-02-0G-0.

Part: SUPPORT ANGLE — CORRODED (BS 727D) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO BAY RT SIDEWALL PANEL SUPPORT ANGLE ATTACHED TO FRAME AT BS 727D IS BENT & CORRODED ON UPPER AND LOWER SURFACES, AND GOUGED AROUND FASTENER HOLES ENTIRE LENGTH. BLENDED AREA FOUND TO BE OF LIMITS IAW SRM 53-00-07-1A-1. R & R SUPPORT IAW SRM 51-40-02-0G-0.

Part: STRAP — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

DURING REMOVAL OF AFT CARGO AFT DOOR FRAME BS 847, FOUND FRAME REINFORCEMENT STRAP TO BE CORRODED MORE THAN 15 OF PARENT MATERIAL. R & R FRAME REINFORCEMENT STRAP IAW SRM 51-40-02-0G-0.

Part: BRACKET — CORRODED (BS 328-344) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

E & E BAY RBL 15.47 SHEAR PLATE BETWEEN BS 328-344 CORRODED, REPAIRED SHEAR PLATE IAW SRM 53-00-07-2R-8.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 67,185 hrs · 38,632 cycles

LEFT OTBD FOREFLAP L/E IS CHAFED IN TWO AREAS JUST INBD FLAP OTBD TRACK. REPAIRED IAW SRM 57-53-01-2R-1, FIG 201.

Part: ANGLE — CORRODED (RT MLG WW) · airframe 67,185 hrs · 38,632 cycles

RT MLG WW LOWER FWD ANGLE IS CHAFED ON BOTTOM SIDE. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED CORRODED ANGLE AND INSTALLED NEW IAW SRM 53-60-71-1A-1.

Part: SUPPORT — CORRODED (RT MLG WW) · airframe 67,185 hrs · 38,632 cycles

RIGHT MLG WW FWD INBD FAIRING SUPPORT IS CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS, REMOVED FAIRING SUPPORT, FABRICATED, LOCATED, DRILLED AND INSTALLED IAW SRM 53-60-71-1A-1, AMM 51-21-21-307-014, AMM 51-21-99-307-022.

Part: ATTACH BRACKET — CORRODED (GIRT BAR) · airframe 67,185 hrs · 38,632 cycles

L1 DOOR FWD GIRT BAR BRACKET IS CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51-1A-1, DETAIL 1X. R & R L1 FWD GIRT BAR BRACKET IAW SRM 51-40-02-06-0 AND AMM 20-50-11-912-002, TABLE 203.

Part: FLOORBEAM — CORRODED (BS 312) · airframe 67,185 hrs · 38,632 cycles

TEE FITTING ON FLOORBEAM AT STA 312 HAS SEVERAL AREAS OF CORROSION. REPAIRED FLOORBEAM FROM LBL 20 TO RBL 20 IAW SRM 53-10-51-2R-5, REPAIR 5.

Part: FLOOR SUPPORT — CORRODED (BS 336) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

FLOOR SUPPORT BS 336, RBL 48 HAS AREA OF LIGHT CORROSION, BLENDED FLOOR SUPPORT FOUND TO BE OUT OF LIMITS, FABRICATED, LOCATED, AND DRILLED NEW SUPPORT AND INSTALLED IAW SRM 51-40-02-0G-1, SRM 51-40-05-0G-0 AND SRM 53-30-51-1A-1.

Part: PRESSURE BLKHD — CORRODED (BS 1030) · airframe 67,185 hrs · 38,632 cycles

AFT PRESSURE WEB BS 1030, LBL 5-19 CORRODED. R & R PRESSURE WEB IAW SRM 51-40-02-0G-0.

Part: PANEL — CRACKED (NACELLE) · airframe 67,185 hrs · 38,632 cycles

ACCESS PANEL 5815 CRACKED. INSTALLED NEW ACCESS PANEL.

Part: ATTACH ANGLE — CRACKED (NR 1 NACELLE) · airframe 67,185 hrs · 38,632 cycles

DURING REMOVAL OF NR 1 PYLON OTBD STRUT PANEL SUPPORT FOUND ATTACHING ANGLE TO BE CRACKED. REMOVED DAMAGED ANGLE. FABRICATED, TREATED , PRIMED AND INSTALLED NEW ATTACHING ANGLE IAW SRM 51-40-02-0G-0, 51-30-01-0G-0, AND AMM 51-21-307-014.

Part: DOOR — DAMAGED (APU INLET) · airframe 67,185 hrs · 38,632 cycles

THE APU INLET DOOR VORTEX GENERATOR ROD ELONGATED THE HOLE THROUGH THE DOOR IT IS MOUNTED ON. REMOVED DAMAGE AND FOUND TO BE ACCEPTABLE FOR CONTINUED SERVICE IAW EA 400-49EA-11626, REV NEW.

Part: FLOOR SUPPORT — CORRODED (BS 947-967) · airframe 67,185 hrs · 38,632 cycles

AFT WET AREA FLOOR SUPPORT, RBL 51.55, BS 947 - 967 CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51-1A-1. LOCATED AND DRILLED IAW SRM 51-40-05-0G-0.

Part: FAIRING — CHAFED (LEFT) · airframe 67,185 hrs · 38,632 cycles

LEFT NR 5 SKI JUMP FAIRING IS CHAFED ON INNER LIP. INSTALLED ON 400-53FCD-10237.

Part: FLOOR SUPPORT — CORRODED (BS 859) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO FLOOR SUPPORT LBL 8.1CORRODED BS 859. REPAIRED IAW EA 400-53EA-11620.

Part: DOUBLER — CORRODED (B 500A) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

ANTENNA DOUBLER CORRODED BETWEEN BS 500A S27L-27R. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01-1A-1. R & R ANTENNA DOUBLER IAW SRM 51-40-02-0G-0.

Part: CARGO TRACK — CORRODED (BS 727-727A) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO TRACK AT LBL 8.1 CORRODED ON LWR SURFACE FROM BS 727 - 727A. REPAIRED TRACK IAW SRM 53-00-53-2R-3.

Part: STRINGER — CORRODED (BS 1088-1115) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

APU BAY CENTER FWD STRINGER RT, AT INTAKE OPENING, CORRODED AT AFT END REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-80-13-1A-2. REMOVED STRINGER, LOCATED, DRILLED AND RESTORED FINISH AND INSTALLED IAW SRM 53-80-13-1A2.

Part: STIFFENER — CORRODED (BS 1128) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

APU BAY RT SIDE AFT VERTICAL STIFFENER ON TORQUE BOX SIDE, AT INTAKE OPENING. CORRODED BY CABLE GUARD TUBE. FOUND TO BE OUT OF LIMITS, STIFFENER LOCATED, DRILLED, RESTORED FINISH AND INSTALLED IAW SRM 53-80-13-1A-2 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 294-312) · airframe 67,185 hrs · 38,632 cycles

FLOOR SUPPORT, BS 294-312, RBL 16 HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51-1A-1. R & R FLOOR SUPPORT IAW SRM 51-40-02-0G-0.

Part: SUPPORT ANGLE — CORRODED (BS 950) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

AFT WET AREA SUPPORT ANGLE AT RBL 51, BS 950 IS CORRODED. FABRICATED NEW SUPPORT ANGLE IAW SRM 51-40-05.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

G4 GALLEY MOUNT AT BS 1016, RBL 32 IS CORRODED. BLENDED DAMAGED AREA FOUND TO BE OUT OF LIMITS, MOUNT INSTALLED IAW DWG 69-77476 AND SRM 53-60-51-1A-1.

Part: CARGO TRACK — CORRODED (BS 727A) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO TRACK AT LBL 17.2 CORRODED ON LWR SURFACE BS 727A. REPAIRED CARGO TRACK IAW SRM 53-00-53-2R 2, FIG 201.

Part: FLOOR SUPPORT — CORRODED (BS 947.5-967) · airframe 67,185 hrs · 38,632 cycles

AFT LAVATORY OTBD AFT FLOOR SUPPORT CORRODED LBL 45, BS 947.5 - 967. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51-01-1. LOCATION AND DRILLED IAW SRM 51-40-05.

Part: SUPPORT ANGLE — CORRODED (BS 727D) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO BAY LT SIDEWALL SUPPORT ANGLE ATTACHED TO FRAME AT BS 727D CORRODED AND GOUGED AROUND FASTENER HOLES ENTIRE LENGTH. BLENDED AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-02-1A-1, R & R SUPPORT IAW SRM 51-40-02-0G-0.

Part: INTERCOSTAL — BROKEN (BS 300) · airframe 67,185 hrs · 38,632 cycles

DURING REMOVAL OF E1 RACKS, FOUND INTERCOSTAL BS 300, LBL 8 TO RBL 16, PART OF UPPER FLANGE BROKEN OFF. ACFT GROUNDED. REMOVED DAMAGED INTERCOSTAL & FABRICATED IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, & DWG 69-48283, INSTALLED INTERCOSTAL IAW SRM 51-40-02-0G-0.

Part: FLOORBEAM — CORRODED (BS 946) · airframe 67,185 hrs · 38,632 cycles

FLOORBEAM UPPER TEE AT BS 947.5 IS CORRODED, LBL 24 TO 51. ACFT GROUNDED. BLENDED CORROSION IAW SRM 51-10-02, FOUND OUT OF LIMITS IAW SRM 53-60-51-1A-1. REPAIRED FLOORBEAMS IAW EA 400-53EA-11682.

Part: PLATE — CORRODED (FLOOR PANEL) · airframe 67,185 hrs · 38,632 cycles

FLOOR PANEL 2476 HAS CORRODED PLATE ON BOTTOM SURFACE, LOCATED, DRILLED,& FABRICATED NEW PLATE IAW SRM 51-40-02-0G-0, TREATED AND PRIMED IAW AMM 51-21-21-307-014. INSTALLED NEW PLATE IAW SRM 51-40-02-0G-0.

Part: MOUNT — CORRODED (GALLEY) · airframe 67,185 hrs · 38,632 cycles

LEFT AFT G4 GALLEY MOUNT IS CORRODED. BLENDED GALLEY MOUNT AND FOUND TO BE OUT OF LIMITS, INSTALLED NEW MOUNT IAW SRM 53-60-51-1A-1.

Part: STRINGER CLIP — CORRODED (BS 727G) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

STRINGER CLIP 25L BS 727G CORRODED. REMOVED STRINGER CLIP, BLEND CORROSION, FOUND OUT OF LIMITS, FABRICATED NEW STRINGER CLIP, ALODINED, PRIMED, TOPCOATED AND REINSTALLED IAW SRM 53-00-07-1A-1, FIG 101, 51-40-02-0G-0, 51-40-05-0G-0, 51-10-02-0G-0, AMM 51-21-21-307-014 AND 51-21-99-307-022 AND DWG 69-35352-7.

Part: PANEL — CHAFED (THRUST REVERSER) · airframe 67,185 hrs · 38,632 cycles

NR 2 ENG INBD THRUST REVERSER CHAFED BEHIND FWD COMPRESSION PAD REPAIRED NR 2 ENG INBD THRUST REVERSER UPPER PANEL IAW EA 400-78EA-11679, REV NEW.

Part: STRINGER CLIP — CORRODED (BS 727D) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

STRINGER CLIP AT 25R BS 727D CORRODED . R & R STRINGER CLIP IAW SRM 51-40-02-0G-0.

Part: ANGLE — DAMAGED (TAILCONE) · airframe 67,185 hrs · 38,632 cycles

TAILCONE LT SIDE ANGLE FOR PANEL ATTACH, DAMAGED. R & R ANGLE IAW SRM 51-40-02-0G-0.

Part: FLOOR SUPPORT — CORRODED (BS 727F-767) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED BS 727F - 767. REPAIRED IAW SRM 53-60 53-2R-5.

Part: ANGLE — CORRODED (LT MLG WW) · airframe 67,185 hrs · 38,632 cycles

LEFT MLG WW LOWER AFT ANGLE IS CORRODED. R & R ANGLE IAW SRM 51-40-02-0G-0.

Part: SUPPORT — CORRODED (BS 847) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO RT TRANSITION SUPPORT AT BS 847 IS CORRODED. FABRICATED NEW SUPPORT IAW SRM 51-30-01-0G-0.

Part: FLOORBEAM — CORRODED (BS 328) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

FLOORBEAM TEE BS 328 HAS CORROSION IN SEVERAL PLACES OVER ENTIRE LENGTH. REPAIRED FLOORBEAM IAW EA 400-53EA-11614, REV NEW.

Part: CARGO TRACK — CORRODED (BS 727A-727B) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

AFT CARGO TRACK AT RBL 3 CRACKED AND CORRODED FROM BS 727A - 727B. CUT OUT DAMAGED AREA AND REPAIRED CARGO TRACK IAW SRM 53-00-53-2R1.

Part: ANGLE — CORRODED (BS 663-727) · airframe 67,185 hrs · 38,632 cycles

RT MLG W/W UPPER ANGLE HAS CORROSION. BLENDED AND FOUND TO BE OUT OF LIMITS, REMOVED ANGLE AND INSTALLED NEW IAW SRM 53-60-71-1A-1.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO BAY , CARGO TRACK LBL 12.5 CORRODED. REPAIRED CARGO TRACK IAW SRM 53-00-53-2R-1.

Part: CARGO TRACK — CORRODED (BS 727F) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO TRACK AT LBL 17.2 CORRODED ON LOWER SURFACE AT BS 727F. REPAIRED CARGO TRACK IAW SRM 53-00-53-2R-2.

Part: FRAME — DENTED (BS 727E) · airframe 67,185 hrs · 38,632 cycles

FRAME BS 727E, FLANGE DENTED, S22-23R. CUT OUT DAMAGE, FABRICATED NEW REPAIR DOUBLER AND INSTALLED IAW EA 15428, SRM 51-10-02-0G-0, 51-40-02-0G-0 AND AMM 51-21-99-307-022 AND EA 400 53, EA 11669.

Part: SUPPORT BRACKET — CORRODED (BS 947) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO BAY, BULKHEAD SUPPORT BRACKET CORRODED BS 947 FROM S22-26R. BLENDED AND FOUND TO BE OUT OF LIMITS. REMOVED SUPPORT BRACKET AND INSTALLED NEW IAW SRM 53-60-53.

Part: SUPPORT — CORRODED (BS 992) · airframe 67,185 hrs · 38,632 cycles

RIGHT GALLEY SUPPORT ZEE ANGLE CORRODED, BS 992, RBL 32.10. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT LIMIT IAW SRM 53-60-51-1A-1. FABRICATED NEW RT GALLEY SUPPORT ANGLE.

Part: STRUCTURE — CHAFED (NR 1 NACELLE) · airframe 67,185 hrs · 38,632 cycles

NR 1 PYLON, OTBD MID-FAIRING SIDE LINK MISSING ONE NUTPLATE. STRUCTURE UNDER NUTPLATE FOUND TO HAVE CHAFING AND IS OUT OF LIMITS. LOCATED AND DRILLED NEW NUTPLATE IAW SRM 54-50-71-1A-1, FIG 101, 51-40-05-0G-0 AND AMM 51-21-21-307-014.

Part: WEB — CORRODED (BS 727A-727B) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

AFT CARGO FLOOR WEB AT LBL 17.20, BS 727A TO 727B CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04-1A-1. R & R WEB IAW SRM 51-40-02-0G-0.

Part: FLOORBEAM — CORRODED (BS 967) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

FLOORBEAM, BS 967 UPPER CAP IS CORRODED BL 0 TO RBL 24. BLENDED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-60-51-1A-1. REPAIRED FLOORBEAM IAW SRM 53-00-51, FIG 201 AND 53-00-51-2R-3.

Part: WEB — CORRODED (BS 986-992) · airframe 67,185 hrs · 38,632 cycles

DURING REMOVAL OF R2 DOOR MOPSILL, FOUND DOOR SILL WEB FROM BS 986.5 - 992 CORRODED. REMOVED CORRODED SILL WEB AND FOUND TO BE OUT LIMITS IAW SRM 400-53-60-15-1A-1. FABRICATED NEW WEB IAW SRM 51-40-05.

Part: SUPPORT — DAMAGED (BS 727G) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO COMPARTMENT LT SIDE WALL SUPPORT ATTACHED TO FRAME BS 727G DAMAGED AT FASTENER HOLES ENTIRE LENGTH. ACFT GROUNDED. R & R LT SIDE WALL SUPPORT IAW SRM 51-40-02-0G-0.

Part: CARGO TRACK — CORRODED (BS 767) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO TRACK RBL 3 CORRODED AT BS 767. REPAIRED CARGO TRACK IAW SRM 53-00-53-2.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 67,185 hrs · 38,632 cycles

FLOORBEAM BS 986.5 TEE IS CORRODED ACROSS ENTIRE LENGTH. ACFT GROUNDED. REPAIRED FLOORBEAM TEE IAW EA 400-53EA-11666.

Part: ANGLE — CORRODED (BS 707-727) · airframe 67,185 hrs · 38,632 cycles

RIGHT MLG WW LOWER AFT ANGLE IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-71-1A-1. REMOVED DAMAGED ANGLE, INSTALLED NEW ANGLE AND RESTORED AND RESTORED FINISH IAW SRM 53-60-71-1A-1.

Part: CARGO TRACK — CORRODED (BS 727-727A) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO BAY, CARGO TRACK AT LBL 3.0, CORRODED ON LOWER SURFACE FROM BS 727 - 727A. R & R SECTION OF CARGO TRACK IAW SRM 51-40-02-0G-0.

Part: ANGLE — BENT (BS 727) · airframe 67,185 hrs · 38,632 cycles

BS 727, BULKHEAD AFT SIDE, RT LOWER OTBD SIDE WALL SUPPORT ANGLE BENT. ACFT GROUNDED. R & R ANGLE IAW SRM 51-40-02-0G-0.

Part: FAIRING — CHAFED (NR 6 FLAP) · airframe 67,185 hrs · 38,632 cycles

NR 6 FLAP FAIRING DOOR LANDING CHAFED. R & R LANDING IAW SRM 5140-02.

Part: FLOOR PANEL — CORRODED (FWD CARGO BAY) · airframe 67,185 hrs · 38,632 cycles

FWD CARGO NR 4 FLOOR PANEL HAS NUMEROUS AREAS OF CORROSION ON END UPPER SURFACE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS AND FABRICATED NEW FWD CARGO FLOOR PANEL IAW SRM 53-30-53-1A-1, FIG 101, DETAIL IV, 51-40-05-06-0, 51-20-01-0G-0, PARA 66 AND SWOPM 20-41-02, PARA 6F.

Part: ATTACH BRACKET — CORRODED (GIRT BAR) · airframe 67,185 hrs · 38,632 cycles

L1 DOOR AFT GIRT BAR BRACKET CORRODED, BS 344. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51-1A-1, DETAIL IX. R & R L1 AFT GIRT BAR BRACKET IAW SRM 51-40-02-0G-0 AND AMM 20-50-11-912-002-TABLE 203.

Part: SKATE ANGLE — CHAFED (BS 1022-1034) · airframe 67,185 hrs · 38,632 cycles

VERTICAL STAB TO FUSELAGE LT SKATE ANGLE CHAFED IN SEVERAL AREAS. ACFT GROUNDED. REPAIRED SKATE ANGLE IAW EA 400-53, EA-11653.

Part: DOUBLER — CORRODED (BS 500A) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

ANTENNA DOUBLER CORRODED BETWEEN FS 500A AND STR 27L AND 27R. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01-1A1. R & R VHF ANTENNA DOUBLER IAW SRM 51-40-02-0G-0, W 2", O .050", R .043", L 3", D .007.

Part: FLOORBEAM — CORRODED (BS 344) · airframe 67,185 hrs · 38,632 cycles

BS 344 FLOORBEAM TEE FITTING HAS CORROSION. REPAIRED FLOORBEAM IAW IAW EA 400-53EA-11602, REV NEW.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

G4 GALLEY FWD MOUNT FITTING CORRODED. R & R MOUNT FITTING IAW SOPM 20-50-01.

Part: CARGO TRACK — CORRODED (BS 813) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

AFT CARGO TRACK LBL 8.1 CORRODED ON LWR SURFACE AT BS 813. REMOVED CORRODED FROM CARGO TRACK, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-1A, FIG 101, DETAIL V, FABRICATED AND INSTALLED REPAIR.

Part: BAFFLE — CRACKED (BS 727A-727B) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO BAY LT BAFFLE BETWEEN BS 727A - 727B UNDER TRANSITION PANEL IS CRACKED. LOCATED, FABRICATED AND DRILLED NEW BAFFLE IAW SRM 51-40-05-0G-0, TREATED AND PRIMED IAW MM 51-21-21 307-014 AND TOPCOATED IAW SOPM 20-41-02.

Part: BAFFLE — CORRODED (BS 747-767) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

AFT CARGO BAY BAFFLE BS 747-767 IS CORRODED. LOCATED & DRILLED NEW BAFFLE IAW SRM 51-01-02-0G-0.

Part: STRINGER CLIP — CORRODED (BS 794) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

STRINGER CLIP 26R CORRODED AT BS 794. ACFT GROUNDED. R & R IAW SRM 51-40-02-0G-0.

Part: MOUNT — CORRODED (LAVATORY) · airframe 67,185 hrs · 38,632 cycles

RIGHT LAVATORY AFT INBD MOUNT CORRODED, FOUND TO BE OUT OF DWG TOLERANCE, INSTALLED NEW RT LAVATORY INBD MOUNT IAW DWG 69-77308.

Part: CARGO TRACK — CORRODED (BS 767) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

AFT CARGO TRACK AT LBL 8.10 CORRODED BS 767. REMOVED DAMAGED ANGLE FABRICATED AND LOCATED AND DRILLED NEW AND INSTALLED IAW SRM 53-00-53-2R-1.

Part: CARGO TRACK — CORRODED (BS 727) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO TRACK AT LBL 3 CORRODED ON LOWER SURFACE AT BS 727. REPAIRED CARGO TRACK IAW EA 400-53EA-11674, REV NEW.

Part: STRAP — DAMAGED (TAILCONE) · airframe 67,185 hrs · 3,862 cycles

TAILCONE REINFORCEMENT STRAP DAMAGED AT LT SIDE APU AUGMENTOR TUBE ATTACH. ACFT GROUNDED. R & R REINFORCEMENT STRAP IAW SRM 51-40-02-0G-0.

Part: BRACKET — CRACKED (BS 300) · airframe 67,185 hrs · 38,632 cycles

E/E BAY RACK E1 RT FWD VERTICAL SUPPORT CRACKED. AIRCRAFT GROUNDED. REMOVED DAMAGED STANCHION, VERTICAL SUPPORT, AND FABBED NEW STANCHION IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, AND BD WING 65-63813. INSTALLED NEW STANCHION IAW SRM 51-40-02-0G-0 AND SRM 51-40-04-0G-0.

Part: ANGLE — CRACKED (HORIZONTAL STAB) · airframe 67,185 hrs · 38,632 cycles

RIGHT HORIZONTAL STABILIZER INBD ANGLE FWD OF AFT MOUNT LUGS HAS EDGE DAMAGE AND CRACKED. AIRCRAFT GROUNDED. R & R ANGLE IAW SRM 51-40-02-0G-0.

Part: STRAP — CRACKED (DOOR FRAME) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO DOOR SILL VERTICAL WEB UPPER STRAP CRACKED. FABRICATED NEW STRAP IAW SRM 51-40-05-0G-0.

Part: BRACKET — CRACKED (BS 300) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO BAY LT BAFFLE BETWEEN STA 727A AND 727B UNDER TRANSITION PANEL IS CRACKED. AIRCRAFT GROUNDED. LOCATED, FABBED AND DRILLER NEW BAFFLE IAW SRM 51-40-05-0G-0, TREATED AND PRIMED IAW MM 51-21-21-307-014 AND TOPCOATED IAW SOPM 20-41-02.

Part: ATTACH BRACKET — CRACKED (INTERCOSTAL) · airframe 67,185 hrs · 38,632 cycles

INTERCOSTAL ATTACH BRACKET IS CRACKED IN RADIUS AT BS 360 S11L. ACFT GROUNDED. R & R INTERCOSTAL ATTACH BRACKET IAW SRM 51-40-02-0G-0.

Part: BRACKET — CRACKED (BS 328) · airframe 67,185 hrs · 38,632 cycles

E & E BAY BRACKET CRACKED FOR SHELF E1-3, FOUND DURING CLEANING OF E & E BAY, GROUNDED. R & R DAMAGED BRACKET IAW SRM 51-40-02-0G-0, 51-40-05-0G-0, AND DWG 69-48277.

Part: LINER — CRACKED (APU BAY) · airframe 67,185 hrs · 38,632 cycles

APU COMPARTMENT TORQUE BOX INBD LINER IS CRACKED. FABRICATED NEW APU TORQUE BOX LINER ON MIG5, SN 5418430.

Part: TEE FITTING — DAMAGED (BS 792) · airframe 67,185 hrs · 38,632 cycles

DURING REMOVAL OF FRAME, FOUND TEE ANGLE AT BS 792, S24R TO HAVE ELONGATED HOLE. ACFT GROUNDED. REMOVED, FABRICATED AND INSTALLED NEW TEE ANGL IAW SRM 51-40-02 0G-0 AND 51-40-05-0G-0.

Part: BAFFLE — CRACKED (BS 727A-727B) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO BAY LT BAFFLE BETWEEN BS 727A AND 727B UNDER TRANSITION PANEL IS CRACKED. AIRCRAFT GROUNDED. LOCATED, FABRICATED AND DRILLER NEW BAFFLE IAW SRM 51-40-05-0G-0, TREATED AND PRIMED IAW MM 51-21-21-307-014 AND TOPCOATED IAW SOPM 20-41-02.

Part: INTERCOSTAL — CRACKED (BS 727A-727B) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO BAY LEFT BAFFLE BETWEEN BS 727A - 727B UNDER TRANSITION PANEL CRACKED. ACFT GROUNDED. REMOVED AND REPLACED IAW SRM-51-40-05-0G-0 AND MM 51-21-21-307-014.

Part: FRAME — CRACKED (BS 867) · airframe 67,185 hrs · 38,632 cycles

FRAME BS 867, IS CRACKED BETWEEN STR 8-9L. REPAIRED FRAME IAW AD20062609-400-53-1.

Part: DOUBLER — DAMAGED (DOOR FRAME) · airframe 67,185 hrs · 38,632 cycles

UPON REMOVAL OF AFT CARGO DOOR CUTOUT FWD FRAME FOUND INNER PRODUCTION DOUBLER TO HAVE ELONGATED HOLES. ACFT GROUNDED. R & R 794 FRAME INNER PRODUCTION DOUBLER IAW SRM 51-40-02-0G-0.

Part: SHROUD — CRACKED (BS 1129) · airframe 67,185 hrs · 38,632 cycles

DURING ACCOMPLISHMENT OF T/C 48749002, STEP 3D FOUND APU AIR INLET DUCT OUTER FLANGE, ON UPPER SHROUD, BENT AND CRACKED ON LWR FWD CORNER, WHERE IT MATES TO TORQUE BOX LINER, ACFT GROUNDED. R & R APU AIR INLET DUCT OUTER FLANGE IAW SRM 51-40-02-0G-0.

Part: DOUBLER — CRACKED (BS 492) · airframe 67,185 hrs · 38,632 cycles

ON REMOVAL OF BS 492 FRAME FOUND INNER DOUBLER CRACKED LOCATED AND DRILLED NEW INNER DOUBLER IAW SRM 51-40-05-0G-0.

Part: BRACKET — CRACKED (RADOME SUPPORT) · airframe 67,185 hrs · 38,632 cycles

LT RADOME HOLD OPEN ROD STORAGE BRACKET IS CRACKED AND BENT. R & R BRACKET IAW SRM 51-40-02-0G-0.

Part: STRINGER CLIP — CRACKED (BS 787) · airframe 67,185 hrs · 38,632 cycles

STRINGER CLIP AT S20R, CRACKED BS 787, ACFT GROUNDED. REMOVED AND INSTALLED NEW STRINGER CLIP IAW SRM 51-40-02-0G-0.

Part: STRINGER CLIP — CRACKED (BS 787) · airframe 67,185 hrs · 38,632 cycles

STRINGER CLIP 21R CRACKED AT BS 787. ACFT GROUNDED. REMOVED CRACKED STRINGER CLIP. LOCATED AND DRILLED NEW STRINGER CLIP AND INSTALLED IAW SRM 51-40-02-0G-0, 51-40-05-0G-0.

Part: STRINGER CLIP — CORRODED (BS 794) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

STRINGER CLIP AT 26R CORRODED BS 794. ACFT GROUNDED. R & R STRINGER CLIP IAW SRM 51-40-02-0G-0.

Part: DUCT — CORRODED (COOLING EXHAUST) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

AVIONICS COOLING EXHAUST DUCT FLANGE IS CORRODED AROUND FASTENERS AT FS 380. ACFT GROUNDED. REPAIRED SKIN AROUND AVIONICS COOLING EXHAUST DUCT IAW EA 400-53EA-11698, REV.

Part: FRAME — DENTED (BS 767) · airframe 67,185 hrs · 38,632 cycles

FRAME AT BS 767, FREE FLANGE DENTED S24-25L. ACFT GROUNDED. REPAIRED FRAME IAW EA 400 53, EA 11609, REV NEW.

Part: ANGLE — CORRODED (BS 328-344) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

ANGLE AND FASTENERS ARE CORRODED ON LT SIDE E & E BAY DOOR SURROUND BETWEEN BS 328 AND 344. ACFT GROUNDED. REMOVED DAMAGE AND FOUND TO BE ACCEPTABLE FOR CONTINUE SERVICE IAW EA 400-53EA-11656, REV NEW.

Part: STRINGER CLIP — CRACKED (BS 787) · airframe 67,185 hrs · 38,632 cycles

STRINGER CLIP 21R CRACKED AT BS 787. ACFT GROUNDED. REMOVED CRACKED STRINGER CLIP. LOCATED AND DRILLED NEW STRINGER CLIP AND INSTALLED IAW SRM 51-40-02-0G-0, 51-40-05-0G-0.

Part: FRAME — DENTED (BS 727F) · airframe 67,185 hrs · 38,632 cycles

FRAME AT BS 727F, FREE FLANGE DENTED BETWEEN S24-25L. ACFT GROUNDED. REPAIRED FRAME IAW, EA 400-53 EA11637 AND SRM 53-00-07, REPAIR 14.

Part: SUPPORT — CHAFED (BS 727G) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO BAY RT GILL LINER SUPPORT ATTACHED TO FRAME AT STA 727G DAMAGED AT FASTENER HOLES ENTIRE LENGTH. ACFT GROUNDED. R & R RT GILL LINER SUPPORT AT FRAME STA 727-G IAW SRM 51-40-02-0G-0.

Part: STRINGER CLIP — CRACKED (S 727E) · airframe 67,185 hrs · 38,632 cycles

STRINGER CLIP 25L CRACKED AT BS 727E. ACFT GROUNDED. REMOVED AND REPLACED IAW SRM-51-40-02-0G-0, 51-40-05-0G-0, AMM 51-2-21-307-014, 51-21-99-307-022 AND DWG 69-35352-1.

Part: INTERCOSTAL — CRACKED (BS 277) · airframe 67,185 hrs · 38,632 cycles

INTERCOSTAL CRACKED AT BS 277, STRINGER 14R. ACFT GROUNDED. R & R INTERCOSTAL IAW SRM 51-40-02-0G-0.

Part: FLOOR SUPPORT — CRACKED (BS 380-400) · airframe 67,185 hrs · 38,632 cycles

FLOOR SUPPORT BS 380 - 400 BL 0 CRACKED. R & R FLOORBOARD SUPPORT IAW SRM 51-40-02-0G-0.

Part: ANGLE — CORRODED (BS 727-727F) · corrosion level 2 · airframe 67,185 hrs · 38,632 cycles

AFT CARGO FLOOR STRUCTURE RT TRANSITION ZEE CORRODED IN MULTIPLE AREAS ON UPPER AND LWR SURFACES FROM STA. 727 TO STA 727F. ACFT GROUNDED. R & R TRANSITION ZEE STA 727 TO 727F 4/H IAW SRM 51-40-02-0G-0, W 2.0, O .040, R .019, L 3.0, D .021.

Part: ANGLE — CORRODED (BS 727-727D) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO FLOOR STRUCTURE LT TRANSITION ZEE CORRODED IN MULTIPLE AREAS ON UPPER AND LOWER SURFACES FROM STA 727 TO STA 727, D10. ACFT GROUNDED. R & R LT TRANSITION ZEE STA 727 TO 727D10 IAW SRM 51-40-02-0G-0, W 1, O .040, R .020, L 2, D .020.

Part: ANGLE — BENT (BS 727) · airframe 67,185 hrs · 38,632 cycles

BS 727 BULKHEAD AFT SIDE LT LOWER OTBD GILL LINER SUPPORT ANGLE BENT. ACFT GROUNDED. R & R ANGLE IAW, SRM 51-40-02-0G-0.

Part: SHEAR WEB — CRACKED (BS 986-1016) · airframe 67,185 hrs · 38,632 cycles

DURING REMOVAL OF L2 MOPSILL FOUND CORROSION ON UPPER SURFACE OF LT SHEAR WEB. ACFT GROUNDED. FURTHER INVESTIGATION FOUND LT SHEAR WEB CRACKED. FABRICATED NEW SHEAR WEB IAW SRM 51-40-05.

Part: ANGLE — CRACKED (BS 277-291) · airframe 67,185 hrs · 38,632 cycles

ANGLE BS 277 - 291, WL 254 IN FRONT OF R1 DOOR IS CRACKED. ACFT GROUNDED. R & R ANGLE IAW SRM 51-40-02-0G-0.

Part: FLOOR SUPPORT — CORRODED (BS 727G-807) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO FLOOR SUPPORT CORRODED BS 727G TO 807. ACFT GROUNDED. R & R IAW SRM 51-40-02-0G-0.

Part: STRINGER CLIP — CRACKED (BS 727A) · airframe 67,185 hrs · 38,632 cycles

STRINGER CLIP CRACKED BS 727A AND S26L. ACFT GROUNDED. REMOVED AND INSTALLED NEW STRINGER CLIP IAW SRM 51-40-02-0G-0.

Part: WEB — DAMAGED (BS 787-847) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO DOOR SILL BEAM WEB ST 256R BETWEEN BS 787 AND BS 847, FWD FACE OF WEB CONTAINS DRILL DAMAGE ON ALL SECTIONS OF WEB. ACFT GROUNDED. BLENDED DAMAGED AREAS, FOUND TO BE OUT OF LIMITS, LOCATED AND DRILLED NEW SILL BEAM WEB IAW SRM 53-670-15-1A-1, 51-40-05-0G-0.

Part: CHANNEL — CORRODED (BS 727E-727G) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO TRANSITION CHANNEL CORRODED BS 727E TO 727G. ACFT GROUNDED. R & R TRANSITION CHANNEL IAW SRM 51-40-02-0G-0.

Part: CARGO TRACK — CORRODED (BS 817-947) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO BAY, CARGO TRACK, RBL 3 IS CORRODED BS 817 TO 947. ACFT GROUNDED. REMOVED DAMAGED CARGO TRACK AND REPLACED IAW SRM 53-00-53-2R-1 AND SRM 51-40-02.

Part: SUPPORT — CRACKED (BS 260) · airframe 67,185 hrs · 38,632 cycles

NOSE LANDING GEAR VIEWING WINDOW SUPPORT IS CRACKED AT BS 260, LBL 3. ACFT GROUNDED. R & R NLG VIEWING WINDOW SUPPORT IAW SRM 51-40-02-0G-0.

Part: SEAT TRACK — GOUGED (BS 344-480) · airframe 67,185 hrs · 38,632 cycles

SEAT TRACK AT RBL 24.75, BS 344 TO 480 HAS NUMEROUS NICKS AND GOUGES. ACFT GROUNDED. R & R SEAT TRACK IAW SRM 53-00-52-2R-2 AND EA 400-53EA-04953, REV NEW.

Part: COVER — CHAFED (BS 211-243) · airframe 67,185 hrs · 38,632 cycles

PILOTS OTBD FLOOR PANEL, RACEWAY COVER, DAMAGED ON FWD END. ACFT GROUNDED. R & R PILOTS OTBD FLOOR PANEL RACEWAY COVER IAW SOPM 20-50-01 AND AMM 20-50-11-912-002, TABLE 208, PAGE 11.

Part: COVER — CHAFED (COCKPIT) · airframe 67,185 hrs · 38,632 cycles

CO-PILOTS OTBD FLOOR PANEL, RACEWAY COVER, DAMAGED ON FWD END. ACFT GROUNDED. R & R CO-PILOTS OTBD FLOOR PANEL RACEWAY COVER IAW SOPM 20-50-01 AND AMM 20-50-11-912-002, TABLE 208, PAGE 11.

Part: FRAME — CRACKED (BS 500A) · airframe 67,185 hrs · 38,632 cycles

FRAME AT BS 500A IS CRACKED BETWEEN STR 8-9R. REPAIRED FRAME IAW AD20062609-400-53-1.

Part: FRAME — CRACKED (BS 480) · airframe 67,185 hrs · 38,632 cycles

FRAME AT BS 480 IS CRACKED BETWEEN STR 8-9L. REPAIRED FRAME IAW AD20062609-400-53-1.

Part: FRAME — CRACKED (BS 400) · airframe 67,185 hrs · 38,632 cycles

FRAME BS 400 IS CRACKED BETWEEN STR 8-9L. ACFT GROUNDED. REPAIRED FRAME IAW AD20062609-400-53-1.

Part: FRAME — CRACKED (BS 380) · airframe 67,185 hrs · 38,632 cycles

FRAME AT BS 380 IS CRACKED BETWEEN STR 8-9R. REPAIRED FRAME IAW AD20062609-400-53-1.

Part: FRAME — CRACKED (BS 360) · airframe 67,185 hrs · 38,632 cycles

FRAME BS 360 IS CRACKED BETWEEN STRINGERS 8-9L. ACFT GROUNDED. REPAIRED FRAME IAW AD20062609 400-53-1.

Part: WEB — CORRODED (LT MLG WW) · airframe 67,185 hrs · 38,632 cycles

LT MLG WW WEB HAS MULTIPLE AREAS OF CORROSION AROUND LOWER ROW OF RIVETS ON AFT SIDE. ACFT GROUNDED. R & R WEB SECTION IAW EA 400-53EA-10802.

Part: FRAME — CRACKED (BS 727F) · airframe 67,185 hrs · 38,632 cycles

FRAME BS 727F IS CRACKED BETWEEN STR 8-9L. ACFT GROUNDED. REPAIRED FRAME IAW AD20062609-400-53-1.

Part: FRAME — CRACKED (BS 827) · airframe 67,185 hrs · 38,632 cycles

FRAME BS 827 IS CRACKED BETWEEN STR 8-9L. ACFT GROUNDED. REPAIRED FRAME IAW AD20062609-400-53-1.

Part: FRAME — CRACKED (BS 440) · airframe 67,185 hrs · 38,632 cycles

FRAME BS 440, IS CRACKED BETWEEN STR 8-9L. ACFT GROUNDED. REPAIRED FRAME IAW AD20062609-400-53-1.

Part: FRAME — CRACKED (BS 500C) · airframe 67,185 hrs · 38,632 cycles

FRAME AT BS 500C, IS CRACKED BETWEEN STR 8-9L. REPAIRED LT FRAME STA 500C IAW AD20062609 400-53-1.

Part: FRAME — CRACKED (BS 400) · airframe 67,185 hrs · 38,632 cycles

FRAME AT BS 400 IS CRACKED BETWEEN STR 8-9R. REPAIRED FRAME IAW AD 20062609-400-53-1.

Part: FRAME — CRACKED (BS 500F) · airframe 67,185 hrs · 38,632 cycles

FRAME AT BS 500F, IS CRACKED BETWEEN STR 8-9L. REPAIRED LT FRAME, STA 500F IAW AD20062609-400-53-1.

Part: FRAME — CRACKED (BS 480) · airframe 67,185 hrs · 38,632 cycles

FRAME BS 480 IS CRACKED BETWEEN STRINGERS 8-9R. ACFT GROUNDED. REPAIRED FRAME IAW AD20062609 400-53-1.

Part: FRAME — CRACKED (BS 500A) · airframe 67,185 hrs · 38,632 cycles

FRAME AT BS 500A IS CRACKED BETWEEN STR 8-9L. REPAIRED FRAME IAW AD 20062609-400-53-1.

Part: FRAME — CRACKED (BS 727D) · airframe 67,185 hrs · 38,632 cycles

FRAME BS 727D, IS CRACKED BETWEEN STRINGERS 8-9L. ACFT GROUNDED. REPAIRED FRAME IAW AD20062609 400-53-1.

Part: FRAME — CRACKED (BS 500D) · airframe 67,185 hrs · 38,632 cycles

FRAME BS 500D, IS CRACKED BETWEEN STR 8-9L. ACFT GROUNDED. REPAIRED FRAME IAW AD20062609-400-53-1.

Part: FRAME — CRACKED (BS 440) · airframe 67,185 hrs · 38,632 cycles

FRAME BS 787, IS CRACKED BETWEEN STRINGERS 8-9L. ACFT GROUNDED. REPAIRED FRAME IAW AD20062609 400-53-1.

Part: FRAME — CRACKED (BS 907) · airframe 67,185 hrs · 38,632 cycles

FRAME AT BS 907, IS CRACKED BETWEEN STR 8-9R. REPAIRED FRAME FS 907 RT IAW AD20062609-400-53-1.

Part: FRAME — CRACKED (BS 727F) · airframe 67,185 hrs · 38,632 cycles

FRAME BS 727F, IS CRACKED BETWEEN STRINGERS 8-9R. ACFT GROUNDED. REPAIRED FRAME IAW AD20062609 400-53-1.

Part: FRAME — CRACKED (BS 727D) · airframe 67,185 hrs · 38,632 cycles

FRAME AT BS 727D, IS CRACKED BETWEEN STR 8-9R. REPAIRED FRAME IAW AD20062609-400-53-1.

Part: FRAME — CRACKED (BS 867) · airframe 67,185 hrs · 38,632 cycles

FRAME BS 867, IS CRACKED BETWEEN STRINGERS 8-9R. ACFT GROUNDED. REPAIRED FRAME IAW AD20062609 400-53-1.

Part: FRAME — CRACKED (BS 787) · airframe 67,185 hrs · 38,632 cycles

FRAME AT BS 787, IS CRACKED BETWEEN STR 8-9R. REPAIRED FRAME IAW AD 20062609-400-53-1.

Part: FRAME — CRACKED (BS 747) · airframe 67,185 hrs · 38,632 cycles

FRAME BS 747, IS CRACKED BETWEEN STR 8-9R. ACFT GROUNDED. REPAIRED FRAME RT IAW AD20062609 400-53-1.

Part: FRAME — CRACKED (BS 907) · airframe 67,185 hrs · 38,632 cycles

FRAME AT BS 907, IS CRACKED BETWEEN STR 8-9L. REPAIRED FRAME IAW AD 20062609-400-53-1.

Part: FINGER DOUBLER — DAMAGED (DOOR FRAME) · airframe 67,185 hrs · 38,632 cycles

AFT CARGO DOOR CUTOUT AFT LOWER WRAP AROUND FINGER DOUBLER DAMAGED. ACFT GROUNDED. R & R COVER ON AFT CARGO DOOR CUTOUT AFT SIDE IAW SRM 51-10-02-0G, ITEM 4B, PAGE 2.

Part: FRAME — CRACKED (BS 827) · airframe 67,185 hrs · 38,632 cycles

FRAME BS 827, IS CRACKED BETWEEN STRINGERS 8-9R. ACFT GROUNDED. REPAIRED FRAME IAW AD20062609 400-53-1.

Part: FRAME — CRACKED (BS 787) · airframe 67,185 hrs · 38,632 cycles

FRAME AT BS 787, IS CRACKED BETWEEN STR 8-9L. REPAIRED LT FRAME IAW AD20062609-400-53-1.

Part: FRAME — CRACKED (BS 747) · airframe 67,185 hrs · 38,632 cycles

FRAME BS 747, IS CRACKED BETWEEN STR 8-9L, ACFT GROUNDED. REPAIRED FRAME IAW AD 20062609-400-53-1.

Part: DOOR FRAME — CRACKED (BS 492) · airframe 67,185 hrs · 38,632 cycles

FWD CARGO DOOR AFT FRAME HAS CRACK AT THE INBD UPPER EDGE OF THE VERTICAL FOOTPRINT OF THE TOP STOP PAD FITTING BETWEEN STR 19R AND 20R APPROX .1875 INCHES LONG. ACFT GROUNDED. REPAIRED FRAME IAW SRM 51-40-02-0G-0.

Part: RADOME — DAMAGED · airframe 24,399 hrs · 7,300 cycles

THE NOSE RADOME HAS 2 ELONGATED HOLES ALONG THE TOP RT, 11 O"CLOCK, ACFT GROUNDED. REPAIRED ELONGATED HOLES ON NOSE RADOME AT 11 O`CLOCK IAW SRM 53-10-72-22-0, PAR 18.

Part: RADOME — DAMAGED · airframe 24,399 hrs · 7,300 cycles

THE NOSE RADOME HAS 2 ELONGATED HOLES AT THE TOP LT POSITION, 1 O`CLOCK. ACFT GROUNDED. REPAIRED ELONGATED HOLES, NOSE RADOME AT 10 O`CLOCK IAW SRM 63-10-72-22-0, PAR 18 .

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 65,955 hrs · 37,865 cycles

POSSIBLE CRACK ON RT HORIZONTAL STAB T/E OF IN SPAR SKIN STAB 97. ACFT GROUNDED. CONFIRMED SKIN CRACK REF BNDT 51-00-00, FIG 23, PART 6 HFEC. PERFORMED HFEC OF ADJACENT BAYS IAW SRM 55-10-01-2R-13, STEP Q, NO INDICATIONS NOTED. INSP NR 3. ACCOMPLISHED CAT B REPAIR IAW EA 400-55EA-10350 AND SRM 55-10-01-2R-113.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 64,554 hrs · 36,987 cycles

POSSIBLE CRACK LT HORIZONTAL STAB LOWER SKIN - FWD OF REAR SPAR. CRACK INDICATION VERIFIED BY INSP WITH HFEC ON T/E OF STAB, STA 129 ON INSPAR SKIN, IAW SRM 55-10-01, AD-1, PG 104 AND NOTE E CRACKS ARE NOT PERMITTED. ACCOMPLISHED REPAIR OF CRACK DAMAGE IAW EA 400-55EA-09218.

Part: FRAME — CRACKED (BS 440) · airframe 63,844 hrs · 36,581 cycles

FORWARD CARGO FORWARD FRAME AT STR 24 CRACKED. ACFT GROUNDED. REMOVED AND REPLACED FRAME.

Part: FRAME — CRACKED (BS 440) · airframe 63,844 hrs · 36,581 cycles

FWD CARGO FWD FRAME AT STR 24 CRACKED. ACFT GROUNDED. R & R FRAME.

Part: ANGLE — CRACKED (BS 727D-727E) · airframe 63,844 hrs · 36,581 cycles

AFT CARGO BAY BS 727D TO 727E, BL 0 CHANNEL AND ZEE ANGLE CRACKED. REPLACED ANGLE.

Part: DOOR — NOISY (L1) · airframe 62,666 hrs · 35,931 cycles

L1 DOOR VERY HARD TO CLOSE AND MAKES LOUD SQUEAL AFTER TAKEOFF. INSPECTED DOOR SEAL NO DEFECTS NOTED. PERFORMED FORWARD ENTRY DOOR OPERATIONAL TEST PER 52 11 00 L1 DOOR OPS CHECK NORMAL.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 61,833 hrs · 35,460 cycles

AFTER REMOVAL OF STR TIE CLIP ON FRAME STA 500B STR 20R HAS A CRACK. REPAIRED STRINGER IAW B737 400 SRM 53-00-03 REPAIR 1 FIG 201.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,833 hrs · 35,460 cycles

FRAME 500F RT SIDE CRACKED AT STAND OFF PEG BELOW STR 21. REPAIRED CRACKED FRAME IAW EA 400 53EA 06775.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,833 hrs · 35,460 cycles

FRAME 500B LT HAS CRACK AT WIRE PENETRATION HOLE. REPAIRED FRAME IAW B737 400 SRM 53 00 07 REPAIR 13.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,833 hrs · 35,460 cycles

FRAME 500B RT SIDE CRACKED AT WIRE PENETRATION HOLE. REPAIRED FRAME AT 500B RT IAW B737 400 SRM 53 00 07 FIG 202 REPAIR 13.

Part: HOUSING — CORRODED (R2 DOOR) · airframe 60,275 hrs · 34,564 cycles

R2 DOOR HANDLE MECHANISM HOUSING ASSEMBLY CAM SHAFT BEARING HOUSING CORRODED. REMOVED CORRODED HOUSING AND INSTALLED REPLACEMENT PART IAW BOEING CMM 52 46 05.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 60,275 hrs · 34,564 cycles

MAIN CABIN BS 368 STR 14L HAS EXISTING PILOT HOLE THRU STRINGER ONLY. REMOVED DAMAGED STRINGER AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 53 30 03 FIG 201.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,275 hrs · 34,564 cycles

STRINGER CLIP CRACKED AT STR 4R BS 727A. INSTALL REPLACEMENT CLIP IAW DWG A53100265816.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,275 hrs · 34,564 cycles

STRINGER CLIP CRACKED AT STR 4R BS 727B. REMOVED AND REPLACED STRINGER CLIP IAW DWG A53100265816.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,275 hrs · 34,564 cycles

STRINGER CLIP CRACKED AT STR 4L BS 727B. INSTALL REPLACEMENT CLIP IAW DWG A53100265816.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,275 hrs · 34,564 cycles

STRINGER CLIP CRACKED AT STR 4R BS 727F. INSTALL REPLACEMENT CLIP IAW DWG A53100265816.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,275 hrs · 34,564 cycles

STRINGER TIE CRACKED AT STR 4L BS 727C. INSTALL REPLACEMENT CLIP IAW DWG A53100265816.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,275 hrs · 34,564 cycles

STRINGER CLIP AT STR 4R BS 727A CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW B737 400 SRM 51 40 02.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 60,275 hrs · 34,564 cycles

MAIN CABIN LEFT SIDE BS 360 STR 14 STRINGER SPLICE CHANNEL CRACKED. REMOVED AND REPLACED CHANNEL AND CLIP IAW TIMCO REO G13605 REV 1R AND ALASKA EA AD20091614 400 53 100.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,275 hrs · 34,564 cycles

STRINGER CLIP CRACKED AT STR 4L BS 727D. INSTALL REPLACEMENT CLIP IAW DWG A53100265816.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 60,275 hrs · 24,564 cycles

AFT PIT STRINGER CLIP CORRODED AT BS 947.5 RBL 12 RBL 20. REMOVED AND REPLACED STRINGER CLIP IAW B737 400 SRM 51 40 02.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 60,275 hrs · 34,564 cycles

STRINGER 16L AT BS 294 IS GOUGED. REPAIRED STRINGER IAW B737 400 SRM 51 70 11.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,275 hrs · 34,564 cycles

INTERCOSTAL WEB CRACKED AT BS 294.5 STR 12L. REMOVED AND REPLACED WEB IAW TIMCO REO G 13609 REV 1R AND ASA EA 400 53EA 05237.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,275 hrs · 34,564 cycles

CRACKED STRINGER CLIP AT BS 294.5 STR 11L. REMOVED AND REPLACED STRINGER CLIP IAW TIMCO REO G 13607 REV 1R AND ASA EA 400 53EA 05236.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,275 hrs · 34,564 cycles

MAIN CABIN INTERCOSTAL WEB CRACKED AT BS 294 STR 11L. REMOVED AND REPLACED WEB IAW TIMCO REO G 13608 REV 1R AND ASA EA 400 53EA 05235.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,276 hrs · 34,564 cycles

MAIN CABIN INTERCOSTAL WEB CRACKED AT BS 294 STR 7L. REMOVED AND REPLACED INTERCOSTAL WEB P/N 65 17684 642 IAW TIMCO REO G13610 REV IR.

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 57,900 hrs · 33,242 cycles

L1 DOOR IS HARD TO CLOSE. ADJUSTED L1 ENTRY DOOR GUIDE ARM PER AMM 52 11 00 705 007 STEP G (1) (2) (A)(B)(C). PERFORMED L1 ENTRY DOOR TEST PER AMM 52 11 00 755 051. DOOR TEST GOOD.

Part: CLAMP — OUT OF POSITION (GASPER VENT) · airframe 57,139 hrs · 32,759 cycles

DURING PREFLIGHT/BOARDING ALT COOLING FAN LIGHT ON. NORMAL SUPPLY FAN C/B OUT NO HISTORY ATTEMPTED RESET PER GPM 05 00 91. SMOKE / WIRING FIRE IN COCKPIT OVERHEAD BEHIND OVERSER'S GASPER AIR VENT. SHUT OFF ELECTRIC POWER AND EXTINGUISHED WITH HALON. FOUND GASPER VENT HOSE CLAMP THUMB SCREW CHAFING WIRING HARNESS W018 DUE TO IMPROPER ORIENTATION. REPAIRED P18 WIRING GOING & DISCONT STATION AP1800 AND AP0500 REF WIRING PRACTICE MANUAL 20 10 13.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,932 hrs · 32,624 cycles

THE 727 FRAME IS CRACKED 2 EA PLACES AT STR 14L & 15L. REPAIRED CRACKED FRAME.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 56,932 hrs · 32,624 cycles

LEFT I/B FLAP TRAILING EDGE WEDGE DELAMINATED ON UPPER SURFACE AT I/B AND OB ENDS. REMOVED DAMAGED SKIN AND INSTALLED FILLERS AND DOUBLERS.

Part: SKIN — CHAFED (FUSELAGE) · airframe 56,932 hrs · 32,624 cycles

FUSELAGE SKIN UNDER DORSAL FIN CHAFED LT SIDE STA 860 887. INSTALLED 2 EA DOUBLERS 1 TRIPLER AND 4 SPLICE STRAPS.

Part: SKIN — DELAMINATED (MIDFLAP) · airframe 56,932 hrs · 32,624 cycles

RT WING I/B MID FLAP WEDGE LOWER SURFACE HAS DELAMINATION AT PREVIOUS REPAIR 18 INCHES FROM I/B EDGE. BONDED DOUBLER AND FILLER.

Part: SKIN — DELAMINATED (MIDFLAP) · airframe 56,932 hrs · 32,624 cycles

RT WING O/B MID FLAP HAS DELAMINATED DENT ON LOWER SURFACE OF THE TRAILING EDGE 34 INCHES O/B OF I/B TRACK. BONDED DOUBLER AND FILLER.

Part: SKIN — GOUGED (MIDFLAP) · airframe 56,932 hrs · 32,624 cycles

RIGHT WING I/B MID FLAP WEDGE LOWER SURFACE GOUGED JUST ABOVE THE O/B PUSH/PULL ROD. INSTALLED DOUBLER AND FILLER AND BONDED.

Part: SKIN — DENTED (MIDFLAP) · airframe 56,932 hrs · 32,624 cycles

LT WING I/B TRAILING EDGE MID FLAP, TRAILING EDGE WEDGE NUMEROUS SHARP DENTS 38 TO 39 INCHES FROM I/B EDGE. BONDED REPAIR DOUBLER.

Part: SKIN — DENTED (MIDFLAP) · airframe 56,932 hrs · 32,624 cycles

LT WING I/B TRAILING EDGE MID FLAP TRAILING EDGE WEDGE LOWER SURFACE SHARP DENT AT I/B EDGE. BONDED 2EA REPAIR DOUBLER.

Part: WINDOW — CRACKED (COCKPIT) · airframe 55,974 hrs · 32,059 cycles

F/O R2 WINDOW ARCING WITH LITE SMOKE. TURNED OFF WINDOW HT AND R2 WINDOW OUTER PANE CRACKED. REMOVED R2 WINDOW REF MM 56 12 11. TASK CARD 48156001 COMPLETED. INSTALLED R2 WINDOW REF MM 56 12 11 404 007, OPS NORMAL.

Part: SKIN — DENTED (HORIZ STAB) · airframe 53,618 hrs · 31,394 cycles

LT HORIZONTAL STABILIZER L/E HAS DENT WITH POSSIBLE BENT STRUCTURE AT APPROX 110 INCHES FROM O/B EDGE OF O/B LEADING EDGE. REMOVED RIB & REWORKED DENT. HFEC INSPECTION IS OK. REPAIRED L/E DENT BY INSTALLING EXTERNAL DOUBLER IAW SRM 55 10 01 REPAIR 3 EA 400 55EA 00805.

Part: SKIN — DENTED (FUSELAGE) · airframe 53,594 hrs · 30,709 cycles

DENT FWD LAV RT SIDE BS 310 316 BETWEEN STR 23 AND 26R. DIMENSION OF DENT ARE DEPTH .148 WIDTH 6.1" HEIGHT 5.4" AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-01. REPAIRED STRINGER IAW SRM 53-00-03.

Part: SKIN — DENTED (FUSELAGE) · airframe 53,594 hrs · 30,709 cycles

DENT FWD LAV RT SIDE BS 310-316 BETWEEN STR 23 AND 26R. DIMENSIONS OF DENT AER DEPTH .148 WIDTH 6.1" HEIGHT 5.4" AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-01. REPAIRED UPPER SKIN PANEL IAW SRM 53-00-31 REPAIR 31.

Part: FRAME — CRACKED (BS 727 S12-16L) · airframe 53,498 hrs · 30,651 cycles

BODY STA 727 FRAME IS CRACKED 2 EA PLACES AT STR 14L AND 15L. REPAIRED FRAME IAW EA 5330 02380 BY INSTALLING TWO REPAIR ANGLES AND TWO CLIPS.

Part: FLOOR SUPPORT — CORRODED (BS 312-328) · corrosion level 1 · airframe 53,498 hrs · 30,651 cycles

CABIN FLOOR SUPPORT CORRODED STA 312 TO STA 328 LBL 11. REMOVED DAMAGED FLOOR SUPPORT, LOCATED DRILLED AND INSTALLED A REPLACEMENT FLOOR SUPPORT IAW B737 400 SRM 51 40 02.

Part: STRAP — CORRODED (BS 275-298) · airframe 53,498 hrs · 30,651 cycles

R1 DOOR INNER CHORD STRAP CORRODED STA 275 TO STA 298.5 RBL 54 WL 208. REMOVED DAMAGED STRAP, FABRICATED, LOCATED, DRILLED AND INSTALLED IAW B737 400 SRM 51 40 02 PGS 3 & 4.

Part: WEB — CORRODED (BS 1025-1029) · corrosion level 2 · airframe 53,498 hrs · 30,651 cycles

AFT CABIN FLOOR WEB UNDER G4 GALLEY CORRODED STA 1025 TO STA 1029 LBL 10 TO LBL 17 AREA. CUT OUT DAMAGED AREA, FABRICATED FILLER AND DOUBLER, LOCATED, DRILLED AND INSTALLED IAW B737 400 SRM 51 70 13 FIG 1.

Part: DOUBLER — CORRODED (R1 DOOR) · corrosion level 1 · airframe 53,498 hrs · 30,651 cycles

R1 INNER CHORD DOUBLER CORRODED AT FORWARD SIDE OF DOOR CUTOUT STA 293 TO STA 298. REMOVED, FABBED AND INSTALLED NEW R1 DOOR INNER CHORD DOUBLER IAW SRM 51-40-02 AND 51-30-01.

Part: HINGE FITTING — CRACKED (RT AILERON) · airframe 53,498 hrs · 30,651 cycles

UPON REMOVAL OF RT AILERON TAB FOUND 2ND FROM O/B HINGE FITTING ON AILERON CRACKED AT FWD UPPER CENTER. AREA APPROX .200 LENGTH. RECEIVED A REPLACEMENT FITTING, INSTALLED NEW FITTING IAW B737 400 SOPM 20 50 01 PG 2 STEP 3 AND CMM 57 50 25 PG 701 STEP 2E FIG 56 INITIATED.

Part: FLOORBEAM — CORRODED (BS 993) · corrosion level 2 · airframe 53,498 hrs · 30,651 cycles

AFT CABIN FLOOR SUPPORT CORRODED STA 993 FROM LBL 32 TO LBL 44.5. REMOVED CORRODED SUPPORT, FABRICATED, LOCATED, DRILLED TRUSTED PRIMED AND TOP COATED AND INSTALLED NEW SUPPORT IAW B737 400 SRM 51 40 02 PG 2.

Part: FRAME — DENTED (BS 500G) · airframe 53,498 hrs · 30,651 cycles

FWD CARGO COMPT FRAME 500 G DENTED JUST ABOVE STR 24L. CUT OUT DAMAGED AREA OF FRAME, FABRICATED REPAIR DOUBLER, LOCATED, DRILLED AND INSTALLED IAW B737 400 SRM 51 70 11 PAGES 1 THRU 5.

Part: FLOOR SUPPORT — DAMAGED (BS 820-874) · airframe 53,498 hrs · 30,651 cycles

AFT CARGO PIT FLOOR SUPPORT HAS DOUBLE DRILLED HOLES AT STA 860 LBL 19. CUT OUT DAMAGED AREA, LOCATED DRILLED AND INSTALLED A REPLACEMENT FLOOR SUPPORT (SPLICE REPAIR) IAW B737 400.

Part: FLOORBEAM — CORRODED (BS 857) · airframe 53,498 hrs · 30,651 cycles

AFT CARGO PIT FLOOR SUPPORT CORRODED STA 857 LBL 6. CUT OUT DAMAGE AREA OF FLOOR SUPPORT, FABRICATED REPAIR ANGLES, REPAIR PARTS LOCATED DRILLED AND INSTALLED IAW AAR EA 12811 AWE ASA EA 5310 02810.

Part: STRINGER — CRACKED (BS 887 S4L) · airframe 53,498 hrs · 30,651 cycles

STRINGER 4L IS CRACKED AT STA 887. REMOVED AND REPLACED DAMAGED STRINGER IAW SRM.

Part: FLOOR SUPPORT — DAMAGED (BS 727G-767) · corrosion level 2 · airframe 53,498 hrs · 30,651 cycles

AFT CARGO PIT FLOOR SUPPORT CORRODED STA 727G TO STA 767. REMOVED DAMAGED ZEE ANGLE, LOCATED DRILLED AND INSTALLED A REPLACEMENT ANGLE IAW B737 400 SRM 51 40 02 PG 2 AND 51 40 05 PG 3.

Part: SHEAR TIE — CORRODED (500C S28L/R) · corrosion level 2 · airframe 53,498 hrs · 30,651 cycles

AFT CARGO PIT SHEAR TIE CORRODED STA 500C BETWEEN STR 28L AND STR 28R. CUT OUT DAMAGED SHEAR TIE, FABRICATED SHEAR TIE AND REPAIR PARTS LOCATED, DRILLED AND INSTALLED IAW B737 400 SRM 53 00 07 REPAIR 3 PAGE 201.

Part: SHEAR TIE — CORRODED (BS 500E) · corrosion level 1 · airframe 53,498 hrs · 30,651 cycles

SHEAR TIE AT STA 500E IS CORRODED BETWEEN STRINGERS 28L TO 26R. CORROSION FOUND TO BE ON PREVIOUS REPAIR, REMOVED AND REPLACED SHEAR TIE IAW B737 400 SRM 53 00 07.

Part: SHEAR TIE — CORRODED (BS 727G S25-26L) · corrosion level 2 · airframe 53,498 hrs · 30,651 cycles

SHEAR TIE CORRODED AT STA 727G FROM STRINGER 25L TO 26L. REMOVED CORRODED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE IAW B737 400 SRM 53 00 07.

Part: SHEAR TIE — CORRODED (BS 460 S28L/R) · corrosion level 2 · airframe 53,498 hrs · 30,651 cycles

SHEAR TIE AT STA 460 BETWEEN STRINGER 28 L TO 28R IS CORRODED. REMOVED AND REPLACED SHEAR TIE IAW B737 SRM 53 00 07.

Part: STRINGER — CRACKED (BS 907 S4L) · airframe 53,498 hrs · 30,651 cycles

STRINGER 4L IS CRACKED FROM FASTENER HOLES AT STA 907. REMOVED AND REPLACED DAMAGE STRINGER IAW SRM 53-00-03.

Part: STRINGER CLIP — CRACKED (BS 887 S4L) · airframe 53,498 hrs · 30,651 cycles

STRINGER CLIP STA 887 STRINGER 4L CRACKED. REMOVED DAMAGED STRINGER CLIP, LOCATED, DRILLED AND INSTALLED A REPLACEMENT STRINGER CLIP IAW SRM 51-40-02 PAR 4.

Part: FLOOR SUPPORT — CORRODED (BS 270) · corrosion level 1 · airframe 53,498 hrs · 30,651 cycles

FLIGHT DECK FLOOR SUPPORT CORRODED AT STA 270 LBL 11 INCHES TO RBL 11 INCHES. REMOVED CORRODED FLOOR SUPPORT, FABRICATED, LOCATED, DRILLED AND INSTALLED A NEW FLOOR SUPPORT IAW B737 400 SRM 51 40 05 FIG 6.

Part: BRACKET — CRACKED (BS 291 S10-11R) · airframe 53,498 hrs · 30,651 cycles

INTERIOR FUSELAGE STIFFENER BRACKET CRACKED 1.5 INCHES IN LENGTH FWD OF STA 291 BETWEEN STRINGERS 10R AND 11R. REMOVED DAMAGED ANGLE, LOCATED, DRILLED AND INSTALLED A REPLACEMENT STIFFENER IAW SRM 51-40-02 PG 30 DETAIL 1.

Part: SHEAR TIE — CORRODED (BS 520) · corrosion level 2 · airframe 53,498 hrs · 30,651 cycles

FWD CARGO PIT SHEAR TIE CORRODED STA 520 RBL 110. REMOVED DAMAGED SHEAR TIE, LOCATED DRILLED AND INSTALLED A REPLACEMENT SHEAR TIE IAW SRM 51-40-02 PAGE 4.

Part: BRACKET — CRACKED (BS 291 S11-12R) · airframe 53,498 hrs · 30,651 cycles

INTERIOR FUSELAGE STIFFENER BRACKET CRACKED 1 INCH LENGTH FWD OF STA 291 BETWEEN STRINGERS 11R AND 12R. REMOVED DAMAGED ANGLE, LOCATED DRILLED AND INSTALLED A REPLACEMENT STIFFENER IAW SRM 51-40-02 PG 3 DETAIL 1.

Part: BRACKET — CRACKED (BS 291 S12-13R) · airframe 53,498 hrs · 30,651 cycles

INTERIOR FUSELAGE STIFFENER BRACKET CRACKED 4.5 INCH LENGTH FWD OF STA 291 BETWEEN STRINGERS 12R AND 13R. REMOVED DAMAGED ANGLE, LOCATED DRILLED AND INSTALLED A REPLACEMENT STIFFENER IAW SRM 51-40-02 PG 30 DETAIL 1.

Part: THRESHOLD — CORRODED (BS 447-485) · corrosion level 2 · airframe 53,498 hrs · 30,651 cycles

FWD CARGO DOOR CUTOUT THRESHOLD WEB CORRODED ON LWR SIDE AROUND NUT PLATES STA 447 TO STA 485 RBL 30 TO RBL 32 WL 156. REMOVED DAMAGED THRESHOLD WEB LOCATED DRILLED AND INSTALLED A REPLACEMENT WEB IAW SRM 51-40-02 FIG 9.

Part: FRAME — CRACKED (BS 616) · airframe 53,498 hrs · 30,651 cycles

CRACK FOUND ON LT BS 616 FRAME INNER CHORD WL 201 TO WL 200 AREA DURING ACCOMPLISHMENT OF EO 5310 02528. REMOVED DAMAGED FRAME INNER CHORD, CUT OUT AREA, FABRICATED FILLER SHIM AND STIFFENING ANGLE AND INSTALLED IAW EO 5310 02528 SECTION 5.

Part: SILL — CORRODED (BS 259-360) · corrosion level 1 · airframe 53,498 hrs · 30,651 cycles

R1 DOOR THRESHOLD INNER CHORD (MOP SILL) CORRODED. REMOVED DAMAGED INNER CHORD. LOCATED, DRILLED AND INSTALLED A REPLACEMENT INNER CHORD IAW B737 400 SRM 51 40 02 PAGE 2 AND 4.

Part: FLOORBEAM — CORRODED (BS 294) · corrosion level 2 · airframe 53,498 hrs · 30,651 cycles

CABIN FLOORBEAM UPPER CHORD CORRODED LBL 20 TO RBL 60 STA 294.5. REMOVED DAMAGED UPPER CHORD, FABRICATED REPAIR PARTS, LOCATED DRILLED AND INSTALLED SPLICE ANGLE AND UPPER BEAM CHORD IAW B737 400 SRM 53 10 51 FIG 201.

Part: THRESHOLD — CORRODED (BS 298-328) · corrosion level 1 · airframe 53,498 hrs · 30,651 cycles

R1 DOOR THRESHOLD WEB CORRODED BETWEEN STA 298 TO 328 AREA. REMOVED DAMAGED WEB, FABRICATED LOCATED DRILLED AND INSTALLED NEW WEB IAW B737 400 SRM 51 30 01 PG 7 AND 51 40 02 PAGES 2 AND 4.

Part: SILL — CORRODED (BS 948-1006) · corrosion level 1 · airframe 53,498 hrs · 30,651 cycles

CABIN R2 DOOR INNER CHORD (MOP SILL) CORRODED. REMOVED DAMAGED INNER CHORD, LOCATE, DRILLED AND INSTALLED A REPLACEMENT INNER CHORD IAW SRM 51 40 02 PAGES 2 AND 6.

Part: FLOORBEAM — CORRODED (BS 328) · corrosion level 2 · airframe 53,498 hrs · 30,651 cycles

CABIN FLOORBEAM STA 328 CORRODED IN SEVERAL AREAS ON UPPER SURFACE. REMOVED DAMAGED UPPER CHORD, FABRICATED, LOCATED, DRILLED INSTALLED REPAIR PARTS AND UPPER CHORD IAW AAR EA 12802 AND ASA EA 5310 02813

Part: FLOORBEAM — CORRODED (BS 947) · corrosion level 1 · airframe 53,498 hrs · 30,651 cycles

FUSELAGE STA 947.5 CENTER OF FRAME HAS CORROSION ON UPPER CAP. REPAIRED FLOORBEAM IAW ASA EA 5310-02812, REMOVED AND REPLACED T-CAP WITH SPLICE ANGLES AND STRAPS.

Part: FLOORBEAM — CORRODED (BS 344) · corrosion level 1 · airframe 53,498 hrs · 30,651 cycles

FLOORBEAM UPPER CHORD CORRODED STA 344 CENTER AREA TO LBL 35. REMOVED DAMAGED CHORD, FABRICATED UPPER CHORD AND REPAIR PARTS, LOCATED DRILLED AND INSTALLED IAW ASA EA 5310 02811 AND AAR EA 12804.

Part: FLOORBEAM — CORRODED (BS 312) · corrosion level 2 · airframe 53,498 hrs · 30,651 cycles

CABIN FLOORBEAM STA 312 SEVERAL AREAS OF CORROSION ON CAP RBL 32 TO LBL 27. REMOVED DAMAGED UPPER CHORD, FABRICATED UPPER CHORD AND REPAIR SPLICES, LOCATED DRILLED AND INSTALLED IAW B737 400 SRM 53 10 51 REPAIR 5 PAGE 203 FIG 201.

Part: SILL — CORRODED (BS 948-1006) · corrosion level 1 · airframe 53,498 hrs · 30,651 cycles

L2 DOOR MOP SILL IS CORRODED FROM STA 948 TO 1006. REMOVED AND REPLACED MOP SILL IAW B7373 400 SRM 51 40 02 AND 51 40 05.

Part: BEAR STRAP — CORRODED (BS 483-496) · airframe 53,498 hrs · 30,651 cycles

FWD CARGO PIT BILGE AREA BEAR STRAP EXFOILATED STA 490 RBL 10.5 TO RBL 13. REMOVED DAMAGED AREA, HFEC INSPECTED IAW NDTM PT6 FIG 23 AND FIG 16, NO DEFECTS NOTED. FABRICATED, LOCATED, DRILLED AND INSTALLED REPAIR PARTS AND EXT DOUBLER AND TRIPLER IAW ASA EA 5330 02377.

Part: SKIN — CHAFED (NR 4 SLAT) · airframe 53,498 hrs · 30,651 cycles

RT WING NR 4 2 E SLAT LOWER TRAILING EDGE WEDGE CHAFED. PREPARED DAMAGED AREA, FABRICATED FILLERS AND DOUBLERS AND BONDED IAW SRM 51-70-10 REPAIR 4.

Part: WEDGE — DENTED (RT WING TE FLAP) · airframe 53,498 hrs · 30,651 cycles

RIGHT I/B MID FLAP LOWER SURFACE OF TRAILING EDGE WEDGE DENTED JUST O/B OF NR 3 TRACK. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51 70 10.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 53,498 hrs · 30,651 cycles

LT WING TRAILING EDGE I/B FORE FLAP SEVERAL DENTS ON LOWER SURFACE CENTER I/B AREAS. REMOVED DAMAGED DOUBLERS AND SKINS, FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10.

Part: SKIN — DENTED (NR 8 SPOILER) · airframe 53,498 hrs · 30,651 cycles

RT WING NR 8 SPOILER DENTED ON LOWER SURFACE CENTER AREA. PREPARED DAMAGED AREA, FABRICATE REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 PAGES 201 203 REPAIR 2.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 53,498 hrs · 30,651 cycles

LT WING O/B TRAILING EDGE AFT FLAP 3 EACH DENTS ON LOWER SURFACE. PREPARED DAMAGED AREAS, FABRICATED DOUBLERS AND BONDED IN ACCORDANCE WITH B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (NR 5 SPOILER) · airframe 53,498 hrs · 30,651 cycles

RT WING NR 5 SPOILER UPPER SURFACE DENTED AT 8 INCHES FROM TRAILING EDGE AND 2.5 FROM O/B EDGE. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND BONDED IAW B747 400 SRM 51 70 10 PAGES 201 203 REPAIR 2.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 53,498 hrs · 30,651 cycles

RT WING I/B TRAILING EDGE FOREFLAP HAS MULTIPLE DENTS ON LOWER SURFACE I/B AREA. PREPARED DAMAGED AREA, APPLIED ADHESIVE FILLER, FABRICATED REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (NR 3 SPOILER) · airframe 53,498 hrs · 30,651 cycles

LEFT WING NR 3 SPOILER UPPER SURFACE HAS AREA OF SEVERAL DENTS. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-70-10.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 53,498 hrs · 30,651 cycles

LT WING NR 3 L/E SLAT I/B LWR SURFACE OF T/E WEDGE CHAFED. REMOVED DAMAGED AREA OF SKIN, FABRICATED REPAIR PARTS AND DOUBLER BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (BS 400) · airframe 53,498 hrs · 30,651 cycles

FUSELAGE SKIN DENTED WITH CREASE STA 400 JUST BELOW STR 15R. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLED, LOCATED, DRILLED AND INSTALLED IAW SRM 53-00-01 REPAIR 31.

Part: SKIN — DENTED (BS 363-375) · airframe 53,498 hrs · 30,651 cycles

EXTERNAL FUSELAGE STA 368 DENTED WITHIN 3 INCHES OF LAP SPLICE BETWEEN STR 18R AND 19R. CUT OUT DAMAGED AREA OF SKIN, HFEC AND MFEC INSPECTED AREA, NO DEFECTS NOTED, FABRICATED FILLERS AND DOUBLER, LOCATED, DRILLED & INSTALLED IAW B737 400 SRM 53 00 01 DETAIL XXIX .

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,562 hrs · 29,022 cycles

FUSELAGE SKIN BULGING. FRAME TO SKIN ATTACH SHEAR TIE REMOVED AND REPLACED IAW SRM 53-00-07 FIG 201 REPAIR 5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,562 hrs · 29,022 cycles

AFT CARGO PIT FLOOR SUPPORT CHANNEL CORRODED. FLOOR SUPPORT CHANNEL REPAIRED IAW SRM 53-00-53 FIG 201 REPAIR 1.

Part: SKIN — DENTED (FUSELAGE) · airframe 49,676 hrs · 28,524 cycles

LEFT FWD EXTERIOR FUSELAGE SKIN DENTED OUT OF LIMITS AT FS 330 BETWEEN STR 27L 28L. CUT OUT DAMAGED AREA OF SKIN, FABRICATED AND INSTALLED AN EXTERNAL REPAIR DOUBLER IAW EA 5330 02198.

Part: SKIN — PUNCTURED (FORE FLAP) · airframe 49,676 hrs · 28,523 cycles

THE LEFT WING INBOARD FORE FLAP IS PUNCTURED ON THE LWR SURFACE 4 INCHES FROM THE TRAILING EDGE AND 20 INCHES FROM THE INBOARD SIDE. REMOVED THE DAMAGED AREA OF LWR SKIN, FABRICATED AND INSTALLED A SKIN FILLER AND A REPAIR DOUBLER IAW SRM 51-70-10 PARA 7, 8, 15, 18 AND 20.

Part: SKIN — DENTED (SPOILER) · airframe 49,676 hrs · 28,523 cycles

THE LT WING NR 0 SPOILER UPPER SURFACE IS DENTED. REMOVED THE DAMAGED AREA OF UPPER SKIN, FABRICATED AND INSTALLED A SKIN FILLER AND A REPAIR DOUBLER IAW SRM 57-50-10 REPAIR 4.

Part: SKIN — DELAMINATED (NR 6 SPOILER) · airframe 49,676 hrs · 28,523 cycles

THE RIGHT WING NR 6 SPOILER UPPER SURFACE IS DELAMINATED. REMOVED TWO DAMAGED AREAS OF UPPER SKIN, FABRICATED AND INSTALLED TWO REPLACEMENT FILLERS AND TWO REPLACEMENT DOUBLERS IAW SRM 51-70-10 REPAIR 2.

Part: INTERCOSTAL — CRACKED (BS 294-303) · airframe 49,676 hrs · 28,523 cycles

INTERCOSTAL HAS A 2.3 INCH CRACK IN THE WEB. REMOVED THE DAMAGED INTERCOSTAL LOCATED DRILLED AND INSTALLED A REPLACEMENT INTERCOSTAL IAW EA 5310 02712 REV NEW.

Part: SKIN — DENTED (FORE FLAP) · airframe 49,676 hrs · 28,523 cycles

THE RIGHT INBOARD FORE FLAP IS DENTED ON THE LWR INBOARD SIDE. PREPARED THE DAMAGED SURFACE OF THE LWR SKIN FOR BONDING, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 51-70-10 PARA 7, 8, 12, 15, 18 AND 20.

Part: SKIN — CHAFED (FORE FLAP) · airframe 49,676 hrs · 28,523 cycles

THE LEFT WING OUTBOARD FORE FLAP IS CHAFED ON AN EXISTING LEADING EDGE REPAIR AT THE INBOARD END. REMOVED THE EXISTING SKIN REPAIR DOUBLER IAW SRM 57-53-01 FIG 201.

Part: GUIDE ARM — OUT OF ADJUST (R1 DOOR) · airframe 47,339 hrs · 27,244 cycles

ON TAKEOFF FLT CREW FOUND THE R 1 DOOR HANDLE (STRIGHT UP) AND WOULD NOT STAY IN THE DOWN POSITION. PRESSURIZATION NOT AFFECTED. SLIDE AND LINING WAS REMOVED. DOOR INSPECTED IAW AMM. NO DISCREPANCIES NOTED. HOWEVER THE GUIDE ARM WAS MISADJUSTED. AFTER RE ADJUSTING THE GUIDE ARM THE DOOR OPS CHECKED GOOD.

Part: SKIN — PUNCTURED (TE FLAPS) · airframe 47,332 hrs · 27,238 cycles

LEFT OUTBOARD FORE FLAP REPAIR DOUBLER I/B END DAMAGED FROM TORQUE BOX SCREW. REMOVED PREVIOUS REPAIR DOUBLER, FABRICATED NEW REPAIR DOUBLER AND INSTALLED PER SRM 57-53-01 REPAIR 1 PG 201, 202.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 45,958 hrs · 26,527 cycles

FOUND FWD CARGO DOOR SKIN GOUGED. REPAIRED FWD CARGO DOOR SKIN PER SRM 52 30 01.

Part: SKIN — DENTED (CARGO DOOR) · airframe 45,958 hrs · 26,527 cycles

FOUND AFT CARGO DOOR SKIN DENTED. RE SKINNED AFT CARGO DOOR.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,958 hrs · 26,527 cycles

AFT CARGO BAY FLOOR STRIP IS CORRODED. CORRODED OUT OF LIMITS REMOVED AND INSTALLED NEW STRAP PER SRM 51 40 02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 45,958 hrs · 26,527 cycles

CORROSION ON FLOOR BEAM AT PREVIOUS REPAIR. REPAIRED PER SRM 53 00 51 REPAIR 3.

Part: SKIN — DENTED (TE FLAPS)

OKC - FOUND LEFT OUTBOARD FLAP HAS A DENT ON THE LOWER SURFACE SKIN, A=.5, Y=.55, AY=9. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM. (M)

Part: STRUCTURE — DAMAGED (NR 4 SPOILER)

OKC - FOUND NR 4 SPOILER LOWER SEAL INSERTS IS CORRODED AND BROKEN SCREW STUDS. REMOVED DAMAGED SPOILER, ORDERED AND INSTALLED NEW SPOILER PER AMM. (M)

Part: SKIN PANEL — DENTED (FUSELAGE)

OKC - FOUND PANEL 7420 HAS DENT AFT SIDE. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER PER SRM. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - FOUND FUSELAGE SKIN HAS 2 EACH DENTS WITHIN 10 INCHES OF E/E BAY DOOR CUTOUT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE PER AS EA AND AAR EA. P/N'S 6545800-1, 6545815-65. (M)

Part: SKIN — SCRATCHED (TE FLAP)

OKC - FOUND RIGHT OUTBOARD FLAP UPPER SURFACE IS SCRATCHED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CORE PLUG AND DOUBLER IAW SRM. (M)

Part: SKIN — DELAMINATED (TE FLAP)

OKC - FOUND RIGHT OUTBOARD FLAP INBOARD CORNER IS DELAMINATED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM. (M)

Part: WIRE — INOPERATIVE (EMERGENCY EXIT)

GYR - FOUND FLOOR TRACK LIGHTING SYSTEM AT THE OVERWING EMERGENCY EXIT HAS 6 WHITE LIGHTS THAT ARE NOT ILLUMINATED AND HAS EXPOSED WIRES. RECONNECTED WIRES. REINSTALLED COVER RAIL, FLOOR TRACK LIGHTING OPS CHECK NORMAL. (M)

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

ONT - DURING MAINTENANCE, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIV AT ROW 16. RESECURED AND CONNECTED FLOOR TRACK WIRING. OPS CHECKED GOOD. (M)

Part: CONNECTOR — LOOSE (EMERGNECY LIGHT)

YVR - DURING LINE CHECK FOUND NEAR ROW 14-16 FLOOR TRACK LIGHTING INOPERATIVE. REATTACHED LOOSE CONNECTION, SYSTEM OPERATIONAL CHECKED GOOD. (M)

Part: WIRE — LOOSE (EMERGENCY LIGHT)

SEA - DURING RON CHECK, FOUND ROW 14 TO ROW 17 EMERGENCY LIGHTS INOPERATIVE. RECONNECTED LOOSE WIRES, OPS CHECKED GOOD. (M)

Part: SNUBBER — BROKEN (FWD ENTRY DOOR)

SIT - DURING PREFLIGHT CHECK, THE L1 DOOR SNUBBER WAS FOUND BROKEN. SNUBBER WAS REPLACED. DOOR THEN OPERATED NORMALLY. (M)

Part: LIGHT — MALFUNCTIONED (CABIN)

PDX - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROWS 13-17, DISCONNECTED WIRES. RECONNECTED WIRES, OPS CHECKED NORMAL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY FLOOR LIGHTS ARE INOPERATIVE NEAR AFT LAVATORY AREA. RECONNECTED TRACK LIGHTS. TRACK LIGHTS THEN OPERATED NORMALLY.

Part: STRAP — CORRODED (FUSELAGE)

SEA - DURING C-CHECK, FOUND STRAP AT BS 793.4 AND STRINGER 24R-26R CORRODED. REPAIRED IAW EA. (M)

Part: FRAME — CORRODED (FUSELAGE)

SEA - DURING C-CHECK, FOUND Z-ANGLE FRAME AT BS 793R AND STRINGER 12R-20R CORRODED. REPAIRED IAW EA. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SEA - DURING C-CHECK, FOUND SEAT TRACK CORROSION AT STATION 900 TO 915 AND WL 218. REPAIRED PER EA AND SRM. (M)

Part: CREASE BEAM — CORRODED (FUSELAGE)

SEA - DURING C-CHECK, FOUND CREASE BEAM HAS SURFACE CORROSION AT STATION 540 TO 1016 L2 DOOR. REPAIRED PER EA. (M)

Part: FLANGE — CRACKED (FUSELAGE)

SEA - DURING C-CHECK, FOUND RIGHT EXHAUST LOUVERS, SUPPORT FLANGE CRACKED. BONDED SUPPORT FLANGE PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SEA - DURING C-CHECK, FOUND FLOORBEAM CORRODED AT STATION 986.5 AND LBL 29-41 CORRODED AROUND NUT PLATE HOLES. REPAIRED PER EA. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTS NEAR ROW 1 INOPERATIVE. REATTACHED WIRES ON INOPERATIVE SECTIONS. OPERATIONAL CHECKED GOOD. (M)

Part: LIGHT — INOPERATIVE (L2 DOOR)

SEA - DURING LIGHT CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT, OPS NORMAL. (M)

Part: LIGHT — MISSING (CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT MISSING. REPLACED TRACK LIGHT, OPS CHECKED NORMAL. (M)

Part: ROLLER — LACK OF LUBE (L1 DOOR)

ANC - FOUND CREW REPORTED L1 DOOR DIFFICULT TO OPEN. LUBED DOOR LATCH ROLLERS AND CAMS THEN DOOR CHECKS NORMAL. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOP AT ROW 14-18. RECONNECTED WIRES, OPS CHECK NORMAL. (M)

Part: LIGHT — DISCONNECTED (CABIN)

ANC - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE OVERWING EXITS. RECONNECTED EMERGENCY FLOOR TRACK LIGHTING. OPERATIONS CHECK GOOD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ANC - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROW 10. REPLACED EMERGENCY FLOOR TRACK LIGHTING. OPERATIONS CHECK GOOD. (M)

Part: WIRE — DISCONNECTED (ROW 14 - 16)

ANC - PRIOR TO FLIGHT 62, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 14-16 WERE FOUND TO BE INOPERATIVE. SECURED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN) · airframe 26,132 hrs · 15,845 cycles

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTS AT ROWS 14-17 WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X)

Part: ROLLER — DAMAGED (PAX DOOR)

SEA - PRIOR TO FLT 723 - THE L1 DOOR WAS REPORTED TO BE DIFFICULT TO OPEN OR CLOSE. REPLACED FORWARD CAM FOLLOWER ROLLER AND DOOR OPERATED NORMALLY. (M)

Part: DOOR — LACK OF LUBE (FUSELAGE)

SEA - PRIOR TO FLIGHT 389, THE L1 DOOR WAS REPORTED TO BE HARD TO OPEN OR CLOSE. LUBRICATED DOOR AND DOOR OPERATED NORMALLY. (M)

Part: FUSE — FAILED (BATTERY PACK)

LAX - DURING MAINTENANCE CHECK, THE FORWARD EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN THE FORWARD FIRST CLASS CABIN AREA. REPLACED FUSE IN THE LEFT FORWARD BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X)

Part: MECHANISM — LACK OF LUBE (L1 DOOR)

PDX - PRIOR TO FLIGHT 409, CREW REPORTED THAT THE L1 DOOR WAS DIFFICULT TO CLOSE. INSPECTED, CLEANED, AND LUBRICATED DOOR. DOOR OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROW 16)

ONT - FLT 354 - THE EMERGENCY EXIT FLOOR TRACK LIGHTS IN ROW 16 AREA WERE FOUND INOPERATIVE. RECONNECTED LOOSE WIRING AT ROW 16 AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROW 19)

OAK - FLT 389 - THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 19 WERE FOUND INOPERATIVE. RECONNECTED BROKEN WIRING AT ROW 19 AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROW 16/17)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 14 THROUGH 17. RECONNECTED WIRING AND LIGHTS AT ROWS 16 AND 17, AND RELAMPED. LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROW 15)

PDX - PRIOR TO FLIGHT 343 - THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERTIVE AT ROW 15. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROW 14-18)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 14-18. RECONNECTED LIGHTS AND WIRING AT ROW 18 AND LIGHTS OPERATED NORMALLY. (M)

Part: SUPPORT — CORRODED (BS 945)

SEA - DURING SCHEDULED SI, THE FLOOR SUPPORT IN THE LOWER AFT CARGO COMPARTMENT AT BS 945 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5320-01358. (M)

Part: SHROUD — CHAFED (APU)

SEA - DURING SCHEDULED SI, THE APU LOWER SHROUD WAS FOUND TO BE CHAFED ON THE FORWARD LEFT SIDE. REPAIRED PER EA 4910-01028. (M)

Part: BRACKET — FRETTED (BS 727)

SEA - DURING SCHEDULED SI, FRETTING WAS FOUND ON THE ANGLE BRACKET LOWER FUSELAGE STATION 727 RBL 10. REPAIRED PER EA 5320-01333. (M)

Part: WEB — GOUGED (BS 294-312)

SEA - DURING SCHEDULED SI, GOUGES WERE FOUND IN THE SHEAR WEB ASSEMBLY UPPER SURFACE AT STATION 294-312 LBL 11. REPAIRED PER EA 5310-01644 AND BOEING TELEX ASA-SEA-99-0053RR. (M)

Part: FLOORBEAM — CORRODED (BS 772)

SEA - DURING SCHEDULED SI, THE UPPER FLANGE OF THE CARGO FLOORBEAM AT STATION 772 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01646. (M)

Part: FLOORBEAMS — CORRODED (BS 727)

SEA - DURING SCHEDULED SI, FOUND CORROSION IN THE UPPER FLANGE OF THE CARGO FLOORBEAMS BETWEEN BS 727F AND 727G. REPAIRED PER EA 5310-01645. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, ONE EMERGENCY EXIT FLOOR TRACK LIGHT WAS FOUND INOPERATIVE AT THE FORWARD EXIT. RECONNECTED WIRING AND OPERATED NORMALLY. (M)

Part: IRU — MALFUNCTIONED (NR 1)

LAX - FLT 582 - DURING DESCENT, CREW REPORTED THAT THE FMC AND BOTH EHSI'S FAILED, NO COMPASS INFORMATION AVAILABLE (EXCEPT THE STANDBY COMPASS), NO TCAS AIRCRAFT SYMBOLS, WARNING FLAGS ON ADI (COMPASS) AND ALL WARNING FLAGS ON EHSI. UNABLE TO RESTORE IN FLIGHT. DIVERTED TO PSP AND LANDED WITHOUT INCIDENT. REPLACED NR 1 IRU AND FERRIED AIRCRAFT TO SEA FOR FURTHER TROUBLESHOOTING. AIRCRAFT OPERATED NORMALLY DURING FERRY FLIGHT. SUBSEQUENTLY REPLACED THE FMC AS PRECAUTIONARY MEASURE AND SYSTEM OPERATED NORMALLY. (M)

Part: FMC — MALFUNCTIONED (E/E BAY)

LAX - FLT 582 - DURING DESCENT, CREW REPORTED THAT THE FMC AND BOTH EHSI'S FAILED, NO COMPASS INFORMATION AVAILABLE (EXCEPT THE STANDBY COMPASS), NO TCAS AIRCRAFT SYMBOLS, WARNING FLAGS ON ADI (COMPASS) AND ALL WARNING FLAGS ON EHSI. UNABLE TO RESTORE IN FLIGHT. DIVERTED TO PSP AND LANDED WITHOUT INCIDENT. REPLACED NR 1 IRU AND FERRIED AIRCRAFT TO SEA FOR FURTHER TROUBLESHOOTING. AIRCRAFT OPERATED NORMALLY DURING FERRY FLIGHT. SUBSEQUENTLY REPLACED THE FMC AS PRECAUTIONARY MEASURE AND SYSTEM OPERATED NORMALLY. REFERENCE ASAA9640091.

Part: BATTERY PACK — DISCHARGED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE R2 DOOR EVACUATION SLIDE BATTERY PACK ACTIVATION PIN WAS FOUND TO BE DISCONNECTED FROM THE PACK. REMOVED AND REPLACED EVACUATION SLIDE. (M)

Part: SKIN — SCRAPED (BS 884-937)

SEA - ON ARRIVAL OF FLT 105, CREW REPORTED POSSIBLE TAIL SKID CONTACT WITH RUNWAY DURING LANDING. PERFORMED HARD LANDING AND TAIL DRAG INSPECTIONS. FOUND DAMAGE TO LOWER FUSELAGE SKIN PANELS BS 884-937, STR 28L-28R. INSTALLED PERMANENT REPAIR PER EA 5330-01259 AND BOEING TELEX ASA-SEA-96-0312RR DATED 7/15/96. (M)

Part: DOOR — LACK OF LUBE (L-1)

LAX - FLT 538 - L-1 DOOR WAS DIFFICULT TO CLOSE. LUBED L-1 DOOR ROLLERS AND ACTUATOR, DOOR OPERATED NORMALLY. (M)

Part: CIRCUIT BREAKER — TRIPPED (LANDING GEAR)

SFO - FLT 88 - ON ARRIVAL, CREW REPORTED UNABLE TO MOVE GEAR HANDLE TO THE 'UP' POSITION AFTER TAKEOFF SEA. USED OVERRIDE TO RAISE THE HANDLE. NOTED LANDING GEAR 'LATCH AND PRESS WARN' CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BREAKER, CYCLED GEAR AND ALL SYSTEMS OPERATED NORMALLY. LANDED WITHOUT INCIDENT. REPLACED CIRCUIT BREAKER AS PRECAUTIONARY. PERFORMED LANDING GEAR EXTENSION AND RETRACTION SEVERAL TIMES AND OPERATED NORMALLY. (X)

Part: SENSOR — OUT OF ADJUST (NLG)

SFO - FLT 110 - GEAR HANDLE WOULD NOT GO BEYOND THE 'OFF' POSITION AFTER TAKEOFF SEA. RETRACTED THE FLAPS AND NO HORN SOUNDED. USED OVERRIDE AND GEAR RETRACTED NORMALLY. RECYCLED GEAR AGAIN WITH NORMAL RETRACTION AND INDICATIONS. CONTINUED TO SFO AND LANDED WITHOUT INCIDENT. FOUND AIR SAFETY SENSOR AIR GAP EXCESSIVE. ADJUSTED SENSOR, PERFORMED GEAR RETRACTION, AND SYSTEM OPERATED NORMALLY. (X)

Part: EEL SOCKET — LOOSE (CABIN)

SEA - LEFT TRAILING EDGE FLAP EMERGENCY EXIT LIGHT INOP. MAINTENANCE REPAIRED LIGHT SOCKET. (W)

Part: DOOR — LACK OF LUBE (FWD CABIN)

ANC - CHECK, L1 DOOR HARD TO SHUT. MAINTENANCE INSPECTED AND LUBRICATED DOOR. OPS CHECKED NORMAL. (W)