N640SW

Part: LENS — UNSECURE (CABIN) · airframe 65,212 hrs · 50,934 cycles

FORWARD ENTRY EXIT LIGHT LENS FELL OFF. R&R LIGHT PER MM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 65,146 hrs · 50,880 cycles

L1 DOOR LOWER EMERGENCY EXIT SIGN LENS CRACKED. R&R SIGN PER AMM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 64,927 hrs · 50,681 cycles

L1 DOOR EXIT LIGHT LENS LOOSE. REPLACED THE LENS IAW MM.

Part: SKIN — DELAMINATED (LT WING SPOILER) · airframe 64,064 hrs · 50,086 cycles

LEFT WING NR 4 GROUND SPOILER DELAMINATED. R & R THE GROUND SPOILER PER AMM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 63,326 hrs · 49,593 cycles

RIGHT OVERWING EXIT SIGN LENS LOOSE. SECURED THE LENS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,281 hrs · 49,564 cycles

RIGHT OVERWING INTERIOR EMERGENCY EXIT FLOOD LIGHT BULB INOPERATIVE. R & R THE LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,281 hrs · 49,564 cycles

FORWARD RT OVERWING EMERGENCY EXIT LIGHT BULB INOP. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,281 hrs · 49,564 cycles

R2 DOOR EMERGENCY EXIT LIGHT BULB INOP. RELAMPED LIGHT PER AMM.

Part: COVER — LOOSE (CABIN) · airframe 63,188 hrs · 49,509 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER SIP.

Part: LENS — BROKEN (EXIT SIGN) · airframe 63,099 hrs · 49,452 cycles

FORWARD EMERGENCY EXIT SIGN LENS MOUNT TAB BROKEN. R&R LENS PER SIP.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,077 hrs · 49,435 cycles

LT WING AFT FLAP OUTBOARD UPPER SURFACE DELAMINATED AT NR 1 AFT CANOE FAIRING LOCATION. R&R AFT FLAP PER AMM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 63,022 hrs · 49,388 cycles

L1 DOOR EXIT LIGHT LENS LOOSE. SECURED THE LENS IAW MM.

Part: LENS — UNSECURE (CABIN) · airframe 62,776 hrs · 49,216 cycles

FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT COVER AT FELL OFF IN FLIGHT. REINSTALLED LENS IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 62,518 hrs · 49,039 cycles

FORWARD ENTRY DOOR EXIT LIGHT COVER LENS LOOSE. SECURED LENS IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 62,470 hrs · 49,006 cycles

L1 DOOR EXIT SIGN LOOSE. SECURED THE SIGN IAW MM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 62,438 hrs · 48,986 cycles

LT FORWARD CABIN EXIT SIGN EMERGENCY LIGHT COVER BROKEN. R&R THE SIGN IAW MM.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 62,425 hrs · 48,976 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHT LENS FELL OFF. SECURED LENS IAW MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 62,403 hrs · 48,964 cycles

FORWARD EXIT SIGN COVER LOOSE. SECURED THE COVER IAW AMM.

Part: COVER — UNSECURE (CABIN) · airframe 62,125 hrs · 48,788 cycles

RIGHT EMERGENCY EXIT COVER CAME OFF. REINSTALLED COVER IAW MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,485 hrs · 48,344 cycles

LEFT WING OTBD FLAP DELAMINATED ON LOWER SURFACE OF T/E SECTION. REPAIRED FLAP IAW SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 61,485 hrs · 48,344 cycles

LEFT WING FIXED T/E SPAR BULKHEAD ANGLE CRACKED AT WBL 209. R & R ANGLE IAW SRM.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 61,485 hrs · 48,344 cycles

LEFT VERTICAL STABILIZER FIN CLOSURE ANGLE CRACKED BETWEEN BS 1100 TO BS 1129. R & R ANGLE IAW SRM & DWG.

Part: BRACKET — CRACKED (RT WING) · airframe 61,485 hrs · 48,344 cycles

RIGHT WING UPPER INBD FIXED PANEL 8506 ATTACH ANGLE BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.

Part: BEAM — CRACKED (VERTICAL STAB) · airframe 61,485 hrs · 48,344 cycles

LEFT T/E BEAM ON VERTICAL STABILIZER CRACKED BETWEEN STA 13 TO STA 32. R & R STABILIZER IAW SRM AND DWG.

Part: RETAINING CLIP — CRACKED (VERTICAL STAB) · airframe 61,485 hrs · 48,344 cycles

VERTICAL STABILIZER PANEL 9504 RETAINER CLIP CRACKED AT EDGE. R & R CLIP IAW SRM & DWG.

Part: SKIN — CRACKED (RT WING) · airframe 61,485 hrs · 48,344 cycles

RIGHT WING UPPER SKIN CRACKED BETWEEN RSS 220.84 TO RSS 223.84 UPPER SPAR CHORD. REPAIRED SKIN IAW ER AND EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,485 hrs · 48,344 cycles

RIGHT UPPER WING SKIN CRACKED IN THE AFT ROW RSS 170 TE. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,485 hrs · 48,344 cycles

RIGHT WING SKIN CRACKED IN THE AFT ROW BETWEEN RSS 220.84 TO RSS 256.25. REPAIRED SKIN IAW ER AND EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,485 hrs · 48,344 cycles

RIGHT WING UPPER SKIN CRACKED BETWEEN RSS 264.3 TO RSS 268.55, AFT ROW T/E. REPAIRED SKIN IAW ER AND EA.

Part: SKIN — CRACKED (LT WING) · airframe 61,485 hrs · 48,344 cycles

LT WING UPPER WING SKIN CRACKED BETWEEN RSS 232 TO RSS 272. REPAIRED SKIN IAW ER AND EA.

Part: FITTING — CRACKED (LT WING) · airframe 61,485 hrs · 48,344 cycles

LEFT WING AFT MLG FITTING CRACKED AT NR 5 HOLE APPROX RSS 223.14. REPAIRED FITTING IAW ER & EA.

Part: SPAR — CRACKED (LT WING) · airframe 61,485 hrs · 48,344 cycles

LEFT WING REAR SPAR WEB CRACKED AT LSS 222.64, UPPER FASTENER HOLE 5. REPAIRED WEB IAW ER & EA.

Part: LINK ASSY — CORRODED (LT MLG) · airframe 61,485 hrs · 48,344 cycles

LT MAIN LANDING GEAR SUPPORT BEAM SWING LINK CORRODED ON AFT FACE AT BUSHINGS. R&R LINK ASSEMBLY IAW EA.

Part: WEB — CRACKED (RT WING) · airframe 61,485 hrs · 48,344 cycles

RIGHT WING WEB CRACKED BETWEEN RSS 219.54 TO RSS 222.64. REPAIRED WEB IAW ER & EA.

Part: STRUCTURE — CRACKED (RT WING) · airframe 61,485 hrs · 48,344 cycles

RT WING UPPER CHORD CRACKED BETWEEN RSS 221.54 TO RSS 222.64. REPAIRED CHORD IAW ER & EA.

Part: STRUCTURE — CRACKED (LT WING) · airframe 61,485 hrs · 48,344 cycles

LEFT WING UPPER CHORD CRACKED IN NR 5 HOLE. REPAIRED CHORD IAW ER & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,485 hrs · 48,344 cycles

FLOORBEAM CRACKED BETWEEN BS 727B-2 - 727B-3, LBL 47. REPAIRED FLOORBEAM IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,485 hrs · 48,344 cycles

FLOORBEAM CRACKED BETWEEN BS 727B-2 - 727B-3, LBL 44. REPAIRED FLOORBEAM IAW ER & EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,485 hrs · 48,344 cycles

AFT CARGO FLOOR CHANNEL CORRODED AT BS 773, RBL 8. REPAIRED CHANNEL IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,485 hrs · 48,344 cycles

AFT CARGO FLOOR CHANNEL CORRODED AT BS 773, LBL 3, UPPER & LOWER SURFACE. REPAIR CHANNEL IAW EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 61,485 hrs · 48,344 cycles

STRINGER CLIP CORRODED AT BS 727E, STRINGER 26R. R & R CLIP IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,485 hrs · 48,344 cycles

RIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 887 - 907. R & R WEB IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,485 hrs · 48,344 cycles

SKIN CORRODED BETWEEN BS 799 - 805, RBL 19. REPAIRED SKIN IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,485 hrs · 48,344 cycles

FRAME CORRODED AT BS 767, BETWEEN BL 0 - LBL 6. REPAIRED FRAME IAW SRM.

Part: HANDLE — CRACKED (OVERWING EXIT) · airframe 61,485 hrs · 48,344 cycles

LEFT OVERWING EXIT HATCH LIFT HANDLE CRACKED AT FASTENER LOCATION. R & R HANDLE IAW AMM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,485 hrs · 48,344 cycles

AFT PIT LOWER FRAME CORRODED AT BS 727C, BETWEEN RBL 5 - LBL 14. REPAIRED FRAME IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,485 hrs · 48,344 cycles

FRAME CORRODED AT BS 727E, BETWEEN LBL 16 - 24. R & R FRAME IAW SRM & DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,485 hrs · 48,344 cycles

SKIN CORRODED BETWEEN BS 799 - 805, RBL 19. REPAIRED SKIN IAW SRM & EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 61,485 hrs · 48,344 cycles

FLOORBEAM STABILIZING STRAP CRACKED AT BS 312, BL 0. R & R STRAP IAW DWG & SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 61,485 hrs · 48,344 cycles

FLOORBEAM STABILIZING STRAP CRACKED AT BS 328, LBL 10. R & R STRAP IAW SRM & DWG.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 61,303 hrs · 48,227 cycles

R2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 59,858 hrs · 47,261 cycles

L2 DOOR EMER EVAC SLIDE PRESS GAUGE OUT OF POSITION. REPOSITIONED SLIDE IAW SIP.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,381 hrs · 46,938 cycles

AFT RT EMER LIGHTS INOPERATIVE IN CABIN AISLE AT LOCATION M1672. R & R BATTERY PACK IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,985 hrs · 46,650 cycles

EMERGENCY BULLNOSE LIGHT INOPERATIVE AT ROW 7 DEF. R & R LIGHT IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 58,771 hrs · 46,493 cycles

FORWARD GALLEY EXIT LIGHT LENS LOOSE. R & R LIGHT ASSEMBLY IAW MM.

Part: ANGLE — CRACKED (TE FLAP) · airframe 57,931 hrs · 45,917 cycles

LEFT WING UPPER TE TO FLAP FAIRING ANGLE CRACKED OTBD OF NR 3 FLAP JACKSCREW. R & R ANGLE IAW SRM.

Part: PANEL — DELAMINATED (RT SPOILER) · airframe 57,931 hrs · 45,917 cycles

RIGHT WING NR 8 GND SPOILER PANEL DELAMINATED. R & R NR 8 GND SPOILER IAW AMM.

Part: SLAT — DELAMINATED (RT WING) · airframe 57,931 hrs · 45,917 cycles

RIGHT WING NR 5 SLAT INBD END DELAMINATED. R & R NR 5 SLAT IAW AMM.

Part: FLAP — DELAMINATED (RT WING) · airframe 57,931 hrs · 45,917 cycles

RIGHT WING OTBD AFT FLAP DELAMINATED BETWEEN MIDDLE TRACKS. R & R AFT FLAP IAW AMM.

Part: FAIRING — CRACKED (TE FLAP) · airframe 57,931 hrs · 45,917 cycles

RIGHT WING UPPER FIXED TE PANEL SUPPORT ANGLE OTBD OF INBD FLAP, OTBD TRACK FAIRING CRACKED AFT END. R & R FAIRING IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,043 hrs · 45,358 cycles

E & E COMPARTMENT ON THE LOWER SIDE OF MAIN CABIN FLOORBEAM CRACKED BETWEEN BS 312 TO 350, RBL 30. R & R STRAP IAW SRM & DWG.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,042 hrs · 45,358 cycles

L1 DOOR EXTERIOR SLIDE LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: FUSE — BLOWN (CABIN) · airframe 57,042 hrs · 45,358 cycles

R2 DOOR OVERHEAD EMER LIGHT INOPERATIVE. R & R FUSE IAW AMM & WDM.

Part: SPLICE — MISSING (CABIN) · airframe 57,043 hrs · 45,358 cycles

FORWARD GALLEY EMER LIGHT WIRING MISSING CONNECTOR SPLICE. R & R LIGHT IAW WDM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 57,043 hrs · 45,358 cycles

FUSELAGE STRINGER CLIP DAMAGED AT STATION 727E STRINGER 5L. R & R CLIP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,043 hrs · 45,358 cycles

SKIN CRACKED AT BS 380, STRINGER 14L LOWER ROW BOTH HOLES AT 3 & 9 O'CLOCK POSITIONS. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,043 hrs · 45,358 cycles

SKIN CRACKED AT BS 420 STRINGER 14L AT LOWER ROW AT THE 5 O'CLOCK POSITION. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,043 hrs · 45,358 cycles

SKIN CRACKED AT BS 400 STRINGER 14L AT LOWER ROW AT 3 O'CLOCK POSITION. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,043 hrs · 45,358 cycles

SKIN CRACKED AT BS 500 STRINGER 14R AT 3 & 9 O' CLOCK POSITIONS. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,043 hrs · 45,358 cycles

SKIN CRACKED AT BS 380 STRINGER 14R AT THE 5 O' CLOCK POSITION. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,043 hrs · 45,358 cycles

FUSELAGE STRINGER CLIP CRACKED AT STATION 727D STRINGER 6L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,043 hrs · 45,358 cycles

STRINGER CLIP CRACKED AT BS 500B STRINGER 11R. R & R CLIP IAW DWG & SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 57,043 hrs · 45,358 cycles

FORWARD LAVATORY EMER EXIT LIGHT ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,043 hrs · 45,358 cycles

SKIN CRACKED AT BS 380 STRINGER 14R AT THE 5 O' CLOCK POSITION. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,043 hrs · 45,358 cycles

SKIN CRACKED AT BS 500 STRINGER 14R AT 3 & 9 O' CLOCK POSITIONS. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,043 hrs · 45,358 cycles

SKIN CRACKED AT BS 806 STRINGER 10R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,043 hrs · 45,358 cycles

SKIN CRACKED AT BS 826 STRINGER 14R. REPAIRED SKIN IAW EA.

Part: LENS — UNSECURE (L1 DOOR) · airframe 57,036 hrs · 45,351 cycles

L1 DOOR EMER EXIT LIGHT COVER LENS FELL OFF. REINSTALLED LENS IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 56,727 hrs · 45,122 cycles

FORWARD ENTRY DOOR EMER EXIT LENS LOOSE. SECURED LENS IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,424 hrs · 44,895 cycles

FUSELAGE SKIN CRACKED AT BS 500C+11 STRINGER 10L. REPAIRED SKIN IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 56,415 hrs · 44,890 cycles

L1 DOOR EMER EXIT LIGHT COVER LOOSE. INSTALLED LENS IAW SIP.

Part: LENS — LOOSE (EXIT SIGN) · airframe 56,361 hrs · 44,845 cycles

L1 DOOR EMER EXIT SIGN COVER LENS LOOSE. REPAIRED LENS IAW AMM.

Part: MOUNT BRACKET — CRACKED (R2 DOOR) · airframe 56,181 hrs · 44,715 cycles

R2 DOOR SLIDE FWD MOUNT BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: COVER — MISALIGNED (EXIT SIGN) · airframe 55,978 hrs · 44,567 cycles

AFT CABIN EMER EXIT SIGN COVER MISALIGNED. ALIGNED COVER IAW MM.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 55,978 hrs · 44,566 cycles

PRESSURE WEB BULKHEAD CHANNEL STIFFENERS CORRODED AT BS 1016, BETWEEN STRINGER 27R TO STRINGER 27L. REPAIRED STIFFENER IAW EO & EA.

Part: ANGLE — CRACKED (RT WING) · airframe 55,978 hrs · 44,566 cycles

RIGHT WING UPPER INBD FIXED TE ANGLE CRACKED AT BS 727, WBL 72.25. R & R ANGLE IAW SRM & DWG.

Part: STRUCTURE — CORRODED (TE FLAP) · airframe 55,978 hrs · 44,566 cycles

LEFT WING NR 4 FLAP TRACK OTBD ATTACH POINT BORE CORRODED. REPAIRED BORE IAW EA.

Part: PLATE — CORRODED (TE FLAP) · airframe 55,978 hrs · 44,566 cycles

LEFT WING NR 4 FLAP TRACK SURFACE MOUNT PLATE CORRODED. REPAIRED PLATE IAW EA.

Part: COVER — CRACKED (CARGO DOOR) · airframe 55,978 hrs · 44,566 cycles

AFT CARGO DOOR AFT CUT OUT COVER CRACKED. R & R COVER IAW SRM & DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 55,978 hrs · 44,566 cycles

LEFT SIDE CHORD CRACKED AT BS 178, WL 207. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 55,978 hrs · 44,566 cycles

RIGHT SIDE CHORD CRACKED AT BS 178, WL 20. REPAIRED CHORD IAW EA.

Part: RIB — CRACKED (RT WING) · airframe 55,978 hrs · 44,566 cycles

RIGHT WING LOWER RIB CHORD CRACKED AT WBL 135.5, BETWEEN STRINGER 2 TO STRINGER 3. REPAIRED CHORD IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 55,978 hrs · 44,566 cycles

RIGHT WING INBD FORE FLAP UPPER SKIN DELAMINATED. REPAIRED SKIN IAW SRM.

Part: PLATE — CRACKED (LE SLAT) · airframe 55,978 hrs · 44,566 cycles

LEFT WING NR 1 SLAT PLATE CRACKED AT INBD MAIN TRACK. R & R PLATE IAW SRM & DWG.

Part: SKIN — CRACKED (LT WING) · airframe 55,978 hrs · 44,566 cycles

LEFT WING LE SKIN CRACKED AT WBL 213. REPAIRED SKIN IAW EA.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 55,978 hrs · 44,566 cycles

PRESS WEB BULKHEAD CHANNEL STIFFENERS CORRODED AT BS 1016, STRINGER 23L TO STRINGER 23R. REPAIRED STIFFENER IAW EO & EA.

Part: FLAP — CORRODED (RT WING) · airframe 55,978 hrs · 44,566 cycles

RIGHT WING NR 5 AFT FLAP CORRODED ON INBD AFT HOLE. REPAIRED AFT FLAP IAW CMM.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 55,978 hrs · 44,566 cycles

AFT PRESS BULKHEAD WEB ANGLE STIFFENER CORRODED AT BS 1016, BETWEEN STRINGER 23L TO STRINGER 23R. REPAIRED STIFFENERS IAW EO & EA.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 55,978 hrs · 44,566 cycles

BULKHEAD PRESS WEB STIFFENER CORRODED AT BS 1016, BETWEEN STRINGER 23L TO STRINGER 23R. REPAIRED STIFFENER IAW EO & EA.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 55,978 hrs · 44,566 cycles

ATTACHMENT CLIP CRACKED AT BS 348.2, STRINGER 16L. R & R CLIP IAW SRM & DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 55,978 hrs · 44,566 cycles

ATTACHMENT CLIP CRACKED AT BS 348.2, STRINGER 16L. R & R CLIP IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 55,978 hrs · 44,566 cycles

STRAP CRACKED AT BS 348.2, STRINGER 16L. R & R STRAP IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 55,978 hrs · 44,566 cycles

CLIP CRACKED AT BS 348.2, STRINGER 15L. R & R CLIP IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 55,978 hrs · 44,566 cycles

WEB CRACKED AT BS 348.2, STRINGER 16L. R & R WEB IAW SRM & DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 55,978 hrs · 44,566 cycles

L1 DOOR FRAME OUTER CHORD CRACKED AT BS 348.2, STRINGER 16L. REPAIRED CHORD IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 55,978 hrs · 44,566 cycles

STRAP CRACKED AT BS 312, RBL 50. R & R STRAP IAW SRM & DWG.

Part: BEAM — CRACKED (FUSELAGE) · airframe 55,978 hrs · 44,566 cycles

STUB BEAM CRACKED AT BS 685, LBL 45.5. REPAIRED STUB BEAM IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 55,978 hrs · 44,566 cycles

MAIN WW PRESS DECK CRACKED AT BS 664+9.5, LBL 30.5. REPAIRED DECK IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 55,978 hrs · 44,566 cycles

MAIN WW PRESS DECK CRACKED AT BS 664+1.5, LBL 30. REPAIRED DECK IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 55,978 hrs · 44,566 cycles

MAIN WW PRESS DECK CRACKED AT BS 664+1.5, LBL 32. REPAIRED DECK IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,978 hrs · 44,566 cycles

FUSELAGE SKIN CRACKED AT BS 520+8.5, LBL 5.5. REPAIRED SKIN IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,978 hrs · 44,566 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 708, LBL 24.8. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,978 hrs · 44,566 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 707, LBL 24.8. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,978 hrs · 44,566 cycles

FUSELAGE SKIN CRACKED AT BS 520+2.5, LBL 4.5. REPAIRED SKIN IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 55,978 hrs · 44,566 cycles

CHORD CRACKED AT BS 727, STRINGER 18A LT AT FWD LOWER FASTENER HOLE AT 3 & 9 O'CLOCK. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,978 hrs · 44,566 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 710, LBL 24.8. REPAIRED WEB IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 55,978 hrs · 44,566 cycles

CHORD CRACKED AT BS 727, STRINGER 18A RT AT FWD LOWER FASTENER HOLE AT 4 O'CLOCK DIRECTION. REPAIRED CHORD IAW EA.

Part: COVER — LOOSE (CABIN) · airframe 55,415 hrs · 44,185 cycles

FWD EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER IAW SIP.

Part: SIGN — BROKEN (CABIN) · airframe 55,198 hrs · 44,042 cycles

L1 DOOR EMERGENCY EXIT SIGN BROKEN. R & R SIGN ASSEMBLY IAW MM.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 55,144 hrs · 44,003 cycles

RT MLG WW CTR WING SECTION, REAR SPAR VERTICAL STIFFENER CRACKED AT BS 663.75 RBL 6.15. REPAIRED STIFFENER IAW SWA EA.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 54,160 hrs · 43,299 cycles

FRAME DAMAGED AT STATION 243.7 STRINGER 24L. REPAIRED FRAME IAW AAR EA & SWA EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 54,160 hrs · 43,299 cycles

STRINGER CRACKED AT STATION 240 STRINGER 24L. R & R STRINGER IAW SRM & DRAWING.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 54,160 hrs · 43,299 cycles

FRAME DAMAGED AT STATION 235.8 STRINGER 24L.. R & R CHORD IAW AAR EA & SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,014 hrs · 43,190 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R&R EMERGENCY EXIT LIGHT ASSEMBLY IAW MM.

Part: DOOR — CRACKED (L1) · airframe 53,945 hrs · 43,131 cycles

L1 DOOR CRACKED. R&R DOOR IAW MMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 53,622 hrs · 42,886 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE IAW MT.

Part: SIGN — BROKEN (EXIT SIGN) · airframe 52,967 hrs · 42,419 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS AND BASE BROKEN. REMOVED AND REPLACED SIGN PER M/M.

Part: SIGN — DAMAGED (CABIN) · airframe 52,985 hrs · 42,435 cycles

L1 DOOR THRESHOLD EMERGENCY EXIT SIGN DAMAGED. REMOVED AND REPLACED SIGN PER M/M.

Part: SLIDE — HUNG UP (L1 DOOR) · airframe 52,482 hrs · 42,052 cycles

FWD ENTRY DOOR ESCAPE SLIDE HUNG UP ON ATTEMPTED OPENING AT GATE IN LAX. RE-INSTALLED SLIDE AT FWD ENTRY DOOR PER MT 325-61-06

Part: STRIP — LOOSE (CABIN) · airframe 52,080 hrs · 41,761 cycles

EGRESS LIGHTING STRIP COMING LOOSE AT SEAT ROW 8ABC. REMOVED AND REPLACED EGRESS LIGHTING STRIP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,909 hrs · 41,653 cycles

AFT CARGO BIN INTERIOR FRAME LEGS BETWEEN STR 27R & 27L AT STA 787 ARE CRACKED. REPAIR PER SRM 53-00-07-2R-7.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,787 hrs · 41,561 cycles

RIGHT EMERGENCY EXIT LAMP INOP. REMOVED AND REPLACED LAMP ASSY PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 51,523 hrs · 41,368 cycles

AFT EMERGENCY LIGHTS INOP BETWEEN ROWS 21 TO ROW 23. REMOVED AND REPLACED BATTERY PACK CHARGER ASSY IAW MM.

Part: COVER — DETACHED (CABIN) · airframe 51,496 hrs · 41,347 cycles

FORWARD EMERGENCY EXIT LIGHT COVER FELL OFF DURING LANDING. REMOVED AND REPLACED BASE ASSY PER AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 51,200 hrs · 41,120 cycles

LEFT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP IAW AMM.

Part: SPINDLE — CORRODED (TE FLAP) · airframe 51,200 hrs · 41,120 cycles

NR 7 FLAP SPINDLE CORRODED. REMOVED AND REPLACED SPINDLE IAW MT.

Part: WINDOW — CRACKED (COCKPIT) · airframe 50,770 hrs · 40,792 cycles

L1 COCKPIT WINDOW ARCED AND CRACKED. REMOVED AND REPLACED L1 WINDOW ASSY PER MM.

Part: PANEL — DELAMINATED (RT SPOILER) · airframe 50,350 hrs · 40,472 cycles

RIGHT WING NR 6 SPOILER PANEL DELAMINATED. REMOVED AND REPLACED NR 6 SPOILER IAW AMM & SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

ANGLE CRACKED BETWEEN BS 520 TO BS 540, BL 0. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FLAP — CRACKED (LT WING) · airframe 50,350 hrs · 40,472 cycles

LEFT WING INBOARD RIB FORE FLAP CRACKED AT WBL 355. REMOVED AND REPLACED FORE FLAP IAW AMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

ANGLE CRACKED BETWEEN BS 380 TO BS 400, BL 0. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

SHEAR TIE CRACKED AT BS 360, BETWEEN STR 28L TO STR 27L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17. REPAIRED WEB IAW EA AND EO.

Part: WEB — CORRODED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

WEB CORRODED BETWEEN BS 767 TO BS 787, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

SUPPORT ANGLE CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

WEB ANGLE CRACKED AT BS 685, STR 9R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

SUPPORT ANGLE CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

SUPPORT ANGLE CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

TIE CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

TIE CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

TIE CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

ANGLE CRACKED AT BS 597, STR 11R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

SUPPORT ANGLE CRACKED AT BS 559, STR 10L. REMOVED AND REPLACED ANGLE PER SRM.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

TIE CLIP CORRODED AT BS 907, STR 26R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

STRINGER WEB CORRODED BETWEEN BS 616 AND BS 639, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

TIE CLIP CORRODED AT BS 787, STR 26R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

SUPPORT ANGLE CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

ANGLE CORRODED AT BS 986.5, BETWEEN STR 27L AND STR 26R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB IAW EA AND EO.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

STRINGER CORRODED BETWEEN BS 1088 TO BS 1138, WL 230. REMOVED AND REPLACED STRINGER PER SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 986.5, LBL 43. REPAIRED CHORD IAW EO AND EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

STRINGER CRACKED BETWEEN BS 492.4 TO BS 500, STR 22R. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

FRAME CRACKED AT BS 947.5, BETWEEN STR 24R TO STR 25R. REPAIRED FRAME IAW EA AND EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

STUB FRAME CRACKED BETWEEN BS 957+09 TO BS 957+10, BETWEEN STR 16R TO STR 17R. REPAIRED FRAME IAW EA AND EO.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

TIE CLIP CORRODED AT BS 500C, STR 28L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (BS 500C S27-28R) · airframe 50,350 hrs · 40,472 cycles

FRAME CORRODED AT BS 500C BETWEEN, STRINGERS 27 TO 28R. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

TIE CLIP CORRODED ON TIE CLIP AT BS 947.5, STR 20L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

VERTICAL BEAM WEB CRACKED AT BS 178, LBL 5.7. REPAIRED WEB IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

STRINGER SPLICE CORRODED AT BS 907, STR 22R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: FRAME — CORRODED (BS 500B S27-28L) · airframe 50,350 hrs · 40,472 cycles

FRAME CORRODED AT BS 500B, BETWEEN STRINGERS 27 TO 28L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

FRAME CRACKED AT BS 294.5, STR 7R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

TIE CLIP CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: ANGLE — CORRODED (BS 312-344) · airframe 50,350 hrs · 40,472 cycles

ZEE ANGLE CORRODED AT L1 DOOR LOWER SILL STRUCTURE, BETWEEN BS 312 AND BS 344, LBL 60.5. REMOVED AND REPLACED ZEE ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (BS 312-344) · airframe 50,350 hrs · 40,472 cycles

ZEE ANGLE CORRODED AT L1 DOOR LOWER SILL STRUCTURE BETWEEN BS 312 AND BS 344, LBL 63. REMOVED AND REPLACED ZEE ANGLE IAW SRM AND DWG.

Part: PAN — CRACKED (BS 927-942.5) · airframe 55,710 hrs · 44,376 cycles

RIGHT VACUUM RELIEF VALVE DOOR PAN CRACKED BETWEEN BS 942.5 - 927, BETWEEN STRINGER 18-20R. REPAIRED PAN IAW EA.

Part: SKIN — CRACKED (BS 344-348.2) · airframe 50,350 hrs · 40,472 cycles

L1 DOOR FUSELAGE SKIN CUTOUT CRACKED BETWEEN BS 344 TO BS 348.2, BETWEEN STR 16L TO STR 17L. REMOVED AND REPLACED SKIN IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

Z-ANGLE CORRODED BETWEEN BS 294.5 AND 328, RBL 57. REMOVED AND REPLACED Z-ANGLE IAW SRM AND DWG.

Part: FRAME — CRACKED (BS 520 S21-22L) · airframe 50,350 hrs · 40,472 cycles

FRAME CRACKED AT BS 520, BETWEEN STR 21 TO 22L. REPAIRED FRAME IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

WEB CRACKED BETWEEN BS 294.5 AND BS 303.9, STR 16L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

TIE CLIP CORRODED AT BS 747, STR 26R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

WEB CRACKED AT BS 294+3, RBL 56.5. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FLAP — CRACKED (LT WING) · airframe 50,350 hrs · 40,472 cycles

LEFT WING FORE FLAP O/B OF INBOARD LEADING EDGE CRACKED. REMOVED AND REPLACED FORE FLAP IAW AMM.

Part: ANGLE — CRACKED (RT WING) · airframe 50,350 hrs · 40,472 cycles

RIGHT WING TRAILING EDGE ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FITTING — WORN (GIRT BAR) · airframe 50,350 hrs · 40,472 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTINGS WORN. REMOVED AND REPLACED FITTINGS IAW AMM AND SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

FLOORBEAM CRACKED AT BS 328, LBL 29. REPAIRED BEAM IAW SRM.

Part: LENS — BROKEN (CABIN) · airframe 50,350 hrs · 40,472 cycles

FWD LAV EMERGENCY LIGHT LENS BROKEN. REMOVED AND REPLACED LENS IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

SKIN CRACKED AT BETWEEN BS 927 TO BS 992 AND BETWEEN STR 15R TO STR 22R. REPAIRED SKIN IAW EA.

Part: FITTING — CORRODED (GIRT BAR) · airframe 50,350 hrs · 40,472 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR BASE PLATE FITTING CORRODED. REMOVED AND REPLACED FITTING IAW AMM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

FLOORBEAM CRACKED AT BS 669, LBL 24.5. REPAIRED CHORD IAW EO AND EA.

Part: ACTUATOR — LEAKING (RT SPOILER) · airframe 50,350 hrs · 40,472 cycles

RIGHT WING NR 6 FLIGHT SPOILER ACTUATOR LEAKED. REMOVED AND REPLACED ACTUATOR IAW AMM.

Part: ACTUATOR — LEAKING (RT SPOILER) · airframe 50,350 hrs · 40,472 cycles

RIGHT WING NR 7 FLIGHT SPOILER ACTUATOR LEAKED. REMOVED AND REPLACED ACTUATOR IAW AMM.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 50,350 hrs · 40,472 cycles

L1 DOOR INTERNAL FRAME CRACKED AT BS 312 FWD LOWER CORNER. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: LENS — BROKEN (CABIN) · airframe 50,350 hrs · 40,472 cycles

RIGHT EMERGENCY EXIT BULLNOSE LIGHT LENS BROKEN BETWEEN ROW 2 TO ROW 14. REMOVED AND REPLACED LENS IAW CMM.

Part: LENS — BROKEN (CABIN) · airframe 50,350 hrs · 40,472 cycles

LEFT EMERGENCY EXIT BULLNOSE LIGHT LENS BROKEN BETWEEN ROW 4 TO ROW 12. REMOVED AND REPLACED LENS IAWCMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,350 hrs · 40,472 cycles

FUSELAGE WINDOW SKIN CUTOUT CRACKED ON LEFT SIDE UPPER CORNER AT BS 219.8. REPAIRED SKIN IAW EA AND EO.

Part: SKIN — CRACKED (TE FLAP) · airframe 50,350 hrs · 40,472 cycles

LEFT WING MIDFLAP SKIN CRACKED ON INBOARD, UPPER EDGE. REPAIRED SKIN IAW EO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,378 hrs · 39,764 cycles

DURING SCHEDULED RON FOUND, FUSELAGE SKIN CRACKED AT BS 727B+10, STR 4R. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 49,403 hrs · 39,788 cycles

L1 SLIDE FELL OUT (STILL OPERABLE). RE-INSTALLED SLIDE PER MT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,376 hrs · 39,763 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT FRAME INNER CHORD CRACKED AT BS 616. REPAIRED CHORD PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,376 hrs · 39,763 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME INNER CHORD CRACKED AT BS 616. REPAIRED CHORD IAW EA.

Part: COVER — BROKEN (CABIN) · airframe 48,895 hrs · 39,420 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 47,709 hrs · 38,509 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 3 SLAT I/B TRAILING EDGE CORNER DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 47,709 hrs · 38,509 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 5 SLAT T/E WEDGE O/B END DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 47,709 hrs · 38,509 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING I/B AFT FLAP O/B END TRAILING EDGE WEDGE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 47,709 hrs · 38,509 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 6 SLAT T/E WEDGE I/B END DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,991 hrs · 37,968 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 511D, STR 10R. REPAIRED SKIN PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,559 hrs · 37,655 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN BL 0 TO RBL 6. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,559 hrs · 37,655 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,559 hrs · 37,655 cycles

DURING SCHEDULED 14Y CHECK, FOUND CREASE BEAM O/B UPPER FLANGE CORRODED BETWEEN BS 918 TO BS 948. REPAIRED BEAM PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,559 hrs · 37,655 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,559 hrs · 37,655 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, STR 28L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,559 hrs · 37,655 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN RBL 18 TO RBL 24. REPAIRED SHEAR TIE PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 46,559 hrs · 37,655 cycles

DURING SCHEDULED 14Y CHECK, FOUND RIGHT O/B FLOOR WEB CRACKED AT CUTOUT I/B OF STA 178 SIDE CHORD. REMOVED AND REPLACED WEB PER BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,559 hrs · 37,655 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN LBL 8 TO LBL 12. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,559 hrs · 37,655 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 28R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,559 hrs · 37,655 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, RBL 17. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,559 hrs · 37,655 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 27L TO STR 28L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,559 hrs · 37,655 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, LBL 17. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,559 hrs · 37,655 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727B, RBL 9. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 46,559 hrs · 37,655 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REPAIRED SPLICE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,559 hrs · 37,655 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 867, BETWEEN STR 26R TO STR 867. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,977 hrs · 44,566 cycles

SHEAR TIE CORRODED AT BS 747, BETWEEN RBL 17 TO RBL 24. R & R SHEAR TIE IAW SRM.

Part: LENS — BROKEN (CABIN) · airframe 46,226 hrs · 37,410 cycles

LT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 45,731 hrs · 37,020 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 45,731 hrs · 37,020 cycles

L2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 44,222 hrs · 35,905 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT UPPER WEDGE SKIN DELAMINATED. REMOVED AND REPLACED NR 4 SLAT PER MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 44,222 hrs · 35,905 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 4 SLAT UPPER WEDGE SKIN DELAMINATED. REMOVED AND REPLACED NR 4 SLAT PER MM.

Part: INVERTER — INOPERATIVE (E&E BAY) · airframe 43,173 hrs · 35,139 cycles

ON FINAL FLIGHT ATTENDANT REPORTED ELECTRICAL TYPE SMELL AT RT SIDE BETWEEN ROW 3 TO ROW 7. FOUND INVERTER INOP. REMOVED AND REPLACED INVERTER PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 42,585 hrs · 34,709 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 42,024 hrs · 34,308 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD FITTING LOOSE. SECURED FITTING PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 42,024 hrs · 34,308 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD FITTING LOOSE. SECURED FITTING PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 40,923 hrs · 33,488 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME WEB CRACKED AT R1 DOOR, BS 291, STR 16R. REPAIRED FRAME PER ACO.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 40,957 hrs · 33,516 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,923 hrs · 33,488 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 772, LBL 3. REPAIRED BEAM PER SWA EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,923 hrs · 33,488 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 26R TO STR 26L. REPAIRED FRAME SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,923 hrs · 33,488 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 25R TO STR 26R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,923 hrs · 33,488 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 26R TO STR 26L. REPAIRED FRAME SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 40,923 hrs · 33,488 cycles

DURING SCHEDULED 12Y CHECK, FOUND SKIN CRACKED AT BS 304, BETWEEN STR 10L TO STR 13L. REPAIRED SKIN PER ER.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 40,957 hrs · 33,516 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,923 hrs · 33,488 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CORRODED AT BS 727C, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 40,923 hrs · 33,488 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING NR 2 SLAT T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 40,923 hrs · 33,488 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT WING NR 6 SLAT LOWER L/E SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,923 hrs · 33,488 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CORRODED AT BS 727D, BETWEEN STR 26R TO STR 27L. REPAIRED FRAME PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 40,923 hrs · 33,488 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT WING NR 4 SLAT T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,923 hrs · 33,488 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CORRODED AT BS 807, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,923 hrs · 33,488 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CORRODED AT BS 727E, BETWEEN STR 26R TO STR 26L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,923 hrs · 33,488 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 40,923 hrs · 33,488 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT WING NR 5 SLAT T/E WEDGE IS DELAMINATED AT I/B END. REPAIRED WEDGE PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 40,923 hrs · 33,488 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT WING NR 4 SLAT T/E WEDGE IS DELAMINATED AT I/B END. REPAIRED WEDGE PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 40,923 hrs · 33,488 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT WING NR 5 SLAT T/E WEDGE DELAMINATED AT I/B END. REPAIRED WEDGE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,254 hrs · 33,012 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED CLIP PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 39,500 hrs · 32,469 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT LOWER CORNER. REPAIRED FRAME PER ACO.

Part: FRAME — CORRODED (BS 500A S28L) · airframe 39,500 hrs · 32,469 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500A, STR 28L, WL 148. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (BS 430-450) · airframe 41,734 hrs · 34,494 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 430 AND BS 450, RBL 3. REPAIRED SKIN PER EA.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 39,424 hrs · 32,411 cycles

DURING SCHEDULED HC1 CHECK, FOUND FWD ENTRY DOOR CRACKED AT LOWER STOP MOUNT. R&R DOOR PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 39,424 hrs · 32,411 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. R&R FLAP PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 39,424 hrs · 32,411 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. R&R FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,188 hrs · 32,218 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 38,681 hrs · 31,840 cycles

L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. REMOVED AND REPLACED FITTING PER SRM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 38,542 hrs · 31,740 cycles

DURING SCHEDULED MV4 CHECK, FOUND LEFT WING NR 3 SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,518 hrs · 31,721 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510D, STR 10L. REPAIRED SKIN PER SWA EA.

Part: COVER — BROKEN (CABIN) · airframe 38,496 hrs · 31,705 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 38,352 hrs · 31,602 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 37,709 hrs · 31,130 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — BROKEN (L2 DOOR) · airframe 36,135 hrs · 29,923 cycles

L2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 35,450 hrs · 29,376 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SIGN — LOOSE (EMERGENCY EXIT) · airframe 34,931 hrs · 28,978 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 34,840 hrs · 28,914 cycles

L1 DOOR EVACUATION SLIDE LOOSE. REPOSITIONED SLIDE ASSY PER MM.

Part: FITTING — BROKEN (R2 GIRT BAR) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING BROKEN. REMOVED AND REPLACED GIRT BAR FITTING PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L AND 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L AND 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L AND 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R AND 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L AND 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 6R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 13R. REPAIRED FRAME SECTION PER BOEING DRAWING AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L AND 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R AND 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L AND 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 663 S10L) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663 S10R) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT AND LT HORIZONTAL STAB FITTING CLEVIS LUG FITTING CORRODED. REPAIRED HORIZONTAL STAB FITTING PER MM.

Part: RIB — CRACKED (HORIZ STAB) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT HORIZONTAL STAB L/E NR 1 AND NR 2 RIBS CRACKED. REMOVED AND REPLACED LT HORIZONTAL STAB L/E ASSY PER MM.

Part: STRINGER — CRACKED (BS 496 S23R) · airframe 34,298 hrs · 28,501 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER 23R CRACKED AT BS 496. REPAIRED STRINGER PER SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,066 hrs · 28,310 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR INTERIOR AND EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: TIRE — FAILED (RT MLG) · airframe 33,515 hrs · 27,894 cycles

DECLARED EMERGENCY, ON TAKEOFF FROM DEN, NR 4 TIRE TREAD SEPARATED. THE SEPARATED TREAD DAMAGED RT GEAR DOOR, NR 2 PYLON LOWER AFT AREA, RT FORE, MID AND AFT FLAPS, AND NR 5 GROUND SPOILER. REMOVED AND REPLACED NR 4 TIRE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 32,833 hrs · 27,238 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LENS — BROKEN (CABIN) · airframe 32,746 hrs · 27,258 cycles

DURING SCHEDULED MV1 CHECK, FOUND LOWER EMERGENCY EXIT LIGHT LENS COVER BROKEN AT FWD ENTRY DOOR. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 32,097 hrs · 26,739 cycles

L1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: SKIN — CRACKED (NR 5 SLAT) · airframe 30,932 hrs · 25,870 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND NR 5 L/E SLAT LOWER T/E SKIN CRACKED. REPAIRED SLAT PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,589 hrs · 25,618 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT AFT CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 29,215 hrs · 24,519 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SIGN — DISLODGED (R2 DOOR) · airframe 28,425 hrs · 23,905 cycles

R2 DOOR EMERGENCY EXIT SIGN FELL OFF IN FLIGHT. REINSTALLED SIGN PER MM.

Part: LIGHT — WORN (CABIN) · airframe 28,338 hrs · 23,827 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS STRIPS WORN ON RT SIDE AT ROW 1 AND ROW 16. REMOVED AND REPLACED EEPLS STRIPS PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,780 hrs · 23,390 cycles

DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHTS AT ROWS 12 DEF AND 14 DEF, INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 27,213 hrs · 22,935 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 26,871 hrs · 22,630 cycles

R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 26,860 hrs · 22,620 cycles

R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,440 hrs · 22,281 cycles

DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROWS 19 DEF, 23 DEF AND AFT RT GALLEY INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM.

Part: ACTUATOR — FAULTY (LT WING LE FLAP) · airframe 25,933 hrs · 21,877 cycles

AIR TURNBACK, LT WING NR 3 L/E FLAP ANNUNCIATOR ILLUMINATED AMBER AFTER FLAP RETRACTION ON TAKEOFF. CYCLED FLAPS, NO HELP. NORMAL INDICATIONS ON DESCENT. REMOVED AND REPLACED NR 3 L/E KRUEGER FLAP ACTUATOR PER MM.

Part: FITTING — CORRODED (LT W/W) · airframe 25,893 hrs · 21,850 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LEFT W/W AFT STABILIZER FITTING, CORRODED. REPAIRED PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 25,763 hrs · 21,738 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE IN AFT CARGO COMPARTMENT BS 807, LBL 7, CORRODED. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 25,763 hrs · 21,738 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE AT BS 807, LBL 7, CORRODED. REPAIRED SHEAR TIE PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 25,711 hrs · 21,687 cycles

RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: WEDGE — DELAMINATED (NR 5 SLAT) · airframe 24,643 hrs · 20,855 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT OUTBOARD T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 24,643 hrs · 20,855 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: LENS — CRACKED (L1 DOOR) · airframe 24,643 hrs · 20,855 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SKIN — DELAMINATED (RT WING FOREFLAP) · airframe 24,643 hrs · 20,885 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD FOREFLAP PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 23,692 hrs · 20,086 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: STRIP — LOOSE (AFT CABIN) · airframe 23,399 hrs · 19,842 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE LAST 4 ROWS IN CABIN LT SIDE. SECURED STRIP PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 22,818 hrs · 19,370 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: TIRE — FAILED (NLG) · airframe 22,083 hrs · 18,769 cycles

AIR TURNBACK, DECLARED EMERGENCY. AFTER TAKEOFF DURING GEAR RETRACTION, SUSPECT BLOWN TIRE. FOUND, LT NLG TIRE TREAD SECTION MISSING. REMOVED AND REPLACED BOTH NR 1 & 2 NLG WHEEL AND TIRE ASSY PER MM.

Part: MODULE — FAULTY (INSTRUMENT PANEL) · airframe 22,054 hrs · 18,748 cycles

DECLARED EMERGENCY. NUMEROUS CAUTION WARNING LIGHTS INOP IN COCKPIT. REMOVED AND REPLACED M564 MASTER DIM MODULE PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 21,919 hrs · 18,639 cycles

FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 20,313 hrs · 17,301 cycles

DURING SCHEDULED SERVICE CHECK, FOUND UPPER AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: COOLING FAN — OVERHEATED (E/E BAY) · airframe 19,316 hrs · 16,531 cycles

DIVERSION, DETECTED ODOR IN AFT CABIN AND FLT DECK. REMOVED AND REPLACED EQUIPMENT COOLING FAN PER MM.

Part: SENSOR — OUT OF ADJUST (LT MLG) · airframe 18,889 hrs · 16,197 cycles

AIR TURN BACK, THE LEFT MLG WOULD NOT RETRACT. ADJUSTED LEFT MLG UPLOCK SENSOR PER MM.

Part: LINK — CRACKED (NLG W/W) · airframe 18,090 hrs · 15,570 cycles

DURING SCHEDULED C1 CHECK, FOUND NLG LT AFT PUSH ROD ATTACH LINK CRACKED AT TRUNNION SIDE. REMOVED AND REPLACED ATTACH LINK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,601 hrs · 15,197 cycles

DURING SCHEDULED RON, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT PER MM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 17,188 hrs · 14,872 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT INBD T/E FOREFLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 17,188 hrs · 14,872 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT CREASE BEAM WEB CORRODED AT BS 827 TO BS 847. REPAIRED CREASE BEAM WEB SECTION PER SRM.

Part: COVER — MISSING (CABIN) · airframe 16,626 hrs · 14,394 cycles

EEPLS MISSING COVER AT ROW # 6. INSTALLED COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 16,526 hrs · 14,307 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS LOOSE AT FWD ENTRY. SECURED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,526 hrs · 14,307 cycles

DURING SCHEDULED C3 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM.

Part: COVER — BROKEN (CABIN) · airframe 16,022 hrs · 13,880 cycles

EEPLS COVERS BROKEN AT ROWS 5 & 7. R&R EEPLS COVERS PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 15,820 hrs · 13,706 cycles

EEPLS LOOSE AND WIRES EXPOSED AT ROW 7. SECURED EEPLS PER MM.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 13,623 hrs · 11,897 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS LOOSE AT ROW 15. SECURED EEPLS COVER PER MM.

Part: RETAINER — LOOSE (SERVICE DOOR) · airframe 13,623 hrs · 11,897 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE AFT RETAINER HOOK LOOSE. SECURED RETAINER HOOK PER MM.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 13,607 hrs · 11,879 cycles

EEPLS PULLED LOOSE AT ROW 15. SECURED EEPLS COVER PER MM.

Part: VALVE — VIBRATION (E/E COMPT) · airframe 12,776 hrs · 11,184 cycles

DIVERSION, AIRFRAME VIBRATION DURING CLIMB NEAR E & E AREA. REMOVED AND REPLACED AEROMATIC VALVE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,521 hrs · 10,054 cycles

FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R&R LIGHT ASSY PER MM.

Part: COVER — LOOSE (ROW 1)

DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK COVERS LOOSE AT ROW 1. RESECURED TRACK COVERS PER MM.

Part: SLIDE — LOW PRESSURE (PASSENGER DOOR)

FWD ENTRY DOOR EVACUATION SLIDE PRESSURE BELOW LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: CONTROLLER — MALFUNCTIONED (COCKPIT)

AIR DIVERSION, LEVEL AT 35000 FEET, ENGINE AND WING ANTI-ICE ON, THE ALT HORN SOUNDED. CABIN ALT PASSING 10,000 FEET CLIMBING 1000 FPM. OUTFLOW VALVE FULLY CLOSED WITH NO WARNING LIGHTS ILLUMINATED. BEGAN EMERGENCY DESCENT, CYCLED WING AND ENG ANTI-ICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND LAST THREE EMERGENCY EXIT FLOOR LIGHTS IN CABIN INOP. RESECURED WIRE AND LIGHTS OPS CK OK.