N357SW

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

E & E ACCESS DOOR CUT OUT INTERCOSTAL CRACKED BACKSIDE OF AFT FRAME, UPPER CHORD AREA, LBL 2. R & R INTERCOSTAL IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 75,023 hrs · 62,644 cycles

RIGHT HORIZONTAL STAB LOWER SKIN CRACKED NEAR AFT SPAR & RIB NR 5. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

FRAME CRACKED AT BS 360, BETWEEN STRINGER 13R - 14R. REPAIRED FRAME IAW EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

FRAME SHEAR TIE CRACKED AT BS 727, STRINGER 14R. REPAIRED SHEAR TIE IAW ER & EA.

Part: SPAR — CRACKED (RT WING) · airframe 75,023 hrs · 62,644 cycles

RIGHT WING UPPER REAR SPAR CHORD VERTICAL FLANGE CRACKED IN FASTENER HOLE AT RSS 221. REPAIRED FLANGE IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

STRINGER SPLICE CRACKED AT BS 907, STRINGER 5L. R & R SPLICE IAW ER & EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

STRINGER SPLICE CRACKED AT BS 908, STRINGER 5L. R & R SPLICE IAW ER & EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

INTERCOSTAL CRACKED BETWEEN BS 500D - 520, LBL 0. R & R INTERCOSTAL IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

FRAME SUPPORT ANGLE CRACKED AT BS 639, RBL 70. REPAIRED ANGLE IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

INTERCOSTAL INNER CHORD CRACKED, BETWEEN BS 277 - 291.5, BETWEEN STRINGER 10R - 11R. R & R INTERCOSTAL IAW ER & EA.

Part: HINGE — CRACKED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

L1 DOOR UPPER HINGE CRACKED AT BS 304.5, STRINGER 10L. REPAIRED L1 DOOR IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

STRINGER CLIP CRACKED AT BS 907, STRINGER 9L. R & R CLIP IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

E & E BAY FWD AIRSTAIR DOOR, CUT OUT ATTACH ANGLE CRACKED AT BS 336, BETWEEN STRINGER 21L - 22L. R & R ANGLE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

STRINGER CLIP CRACKED AT BS 907, STRINGER 8R. R & R CLIP IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

FRAME SUPPORT ANGLE CRACKED AT BS 847, STRINGER 1R. R & R ANGLE IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

E & E BAY FWD AIRSTAIR DOOR, CUT OUT FRAME ATTACH ANGLE CRACKED AT BS 320, BETWEEN STRINGER 21L - 22L. R & R ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

FRAME WEB CRACKED AT BS 847, BETWEEN STRINGER 1L - 1R. REPAIRED FRAME IAW ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

FRAME SHEAR TIE CORRODED AT BS 344, STRINGER 27R. REPAIRED SHEAR TIE IAW ER & EA.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

NOSE E BAY LOWER CHORD CORRODED AT BS 227, BETWEEN LBL 8 - RBL 8. REPAIRED CHORD IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

STRINGER CLIP CRACKED AT BS 927, STRINGER 11L. R & R CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

FRAME WEB CRACKED AT BS 907, STRINGER 1L. REPAIRED FRAME IAW ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

FRAME WEB SHEAR TIE CORRODED AT BS 360, BETWEEN STRINGER 28L - 28R. REPAIRED SHEAR TIE IAW ER & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

STRINGER CLIP CRACKED AT STATION 727E, STRINGER 10R. R & R CLIP IAW SRM.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 75,023 hrs · 62,644 cycles

FORWARD CARGO DOOR HANDLE FLAPPER DOOR CUT OUT CRACKED AT AFT UPPER CORNER. REPAIRED CUT OUT IAW ER & EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

AFT BULKHEAD LOWER SUPPORT, CORRODED AT BS 947, BETWEEN STRINGER 25R - 25L. R & R SUPPORT IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

AFT BULKHEAD SUPPORT ANGLE CORRODED, BETWEEN STRINGER 21R - 25R. R & R ANGLE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

STRINGER CLIP CRACKED AT BS 663, STRINGER 10L. R & R CLIP IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

RIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 847 - 867, WL 208. R & R WEB IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED, BETWEEN BS 867 - 847, BETWEEN STRINGER 25L - 25R. R & R SUPPORT IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

STRINGER CLIP CRACKED AT BS 500, STRINGER 8R. R & R CLIP IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

LEFT CREASE BEAM CORRODED AT STATION 420 - 440. REPAIRED BEAM IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

SHEAR TIE CORRODED AT BS 500, BETWEEN STRINGER 28L - 28R. REPAIRED SHEAR TIE IAW ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

SHEAR TIE CORRODED AT BS 500, BETWEEN STRINGER 28L - 28R. REPAIRED SHEAR TIE IAW ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

SHEAR TIE CORRODED AT STATION 420, BETWEEN STRINGER 23R & 24R. REPAIRED SHEAR TIE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

FRAME CRACKED AT BS 360, STRINGER 20R. REPAIRED FRAME IAW ER & EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

FORWARD CARGO COMPARTMENT ON FWD END OF KEEL BEAM CORRODED AT BS 540, STRINGER 28L. REPAIRED BEAM IAW ER & EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

CREASE BEAM WEB CORRODED, BETWEEN BS 480 - 500, STRINGER 17R. R & R WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

SKIN CRACKED AT BS 360, BETWEEN STRINGER 2L - 3L. REPAIRED SKIN IAW ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

SHEAR TIE CORRODED AT BS 420, BETWEEN STRINGER 24R - 25R. R & R SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

SHEAR TIE CORRODED AT BS 420, BETWEEN STRINGER 24R - 25R. R & R SHEAR TIE IAW ER & SRM.

Part: SPAR — CRACKED (RT WING) · airframe 75,023 hrs · 62,644 cycles

RIGHT WING UPPER REAR SPAR, CHORD CRACKED AT RSS 224.14. REPAIRED SPAR IAW EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

EXTERIOR SKIN CORRODED, BETWEEN BS 727D - 727E, BL 0. R & R SKIN IAW ER & EA.

Part: PANEL — CRACKED (FUSELAGE) · airframe 75,023 hrs · 62,644 cycles

FUSELAGE KEEL BEAM STRESS PANEL CRACKED AT STATION 699, RBL 6. REPAIRED PANEL IAW SRM.

Part: SPRING — BROKEN (GIRT BAR) · airframe 74,666 hrs · 62,370 cycles

R2 DOOR AFT FLOOR EMER SLIDE GIRT BAR LOCK, SPRING BROKEN. R & R GIRT BAR ASSEMBLY IAW MM.

Part: SPRING — BROKEN (L2 DOOR) · airframe 74,666 hrs · 62,370 cycles

L2 DOOR AFT FLOOR EMER SLIDE GIRT BAR LOCK SPRING BROKEN. R & R GIRT BAR ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 73,421 hrs · 61,396 cycles

LEFT FWD EXTERIOR EMER EXIT LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 73,421 hrs · 61,396 cycles

RIGHT WING NR 8 SLAT LOWER SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,421 hrs · 61,396 cycles

SKIN CRACKED AT BS 415, STRINGER 2R. REPAIRED SKIN IAW ER & EA.

Part: SPOILER — CRACKED (LT WING) · airframe 72,346 hrs · 60,616 cycles

LEFT WING INBD NR 4 GND SPOILER CRACKED. R & R SPOILER IAW AMM.

Part: PUMP — LEAKING (NR 1 ENGINE) · airframe 72,138 hrs · 60,481 cycles

DIVERSION, MASTER CAUTION LIGHT ASSOCIATED NR 1 ENG HYD LOW PRESS LIGHT. R & R ELEC MOTOR DRIVEN PUMP IAW AMM.

Part: FLASHLIGHT — FAULTY (CABIN) · airframe 71,771 hrs · 60,209 cycles

AFT FLASHLIGHT FAULTY. R & R FLASHLIGHT ASSEMBLY IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,089 hrs · 59,689 cycles

FUSELAGE SKIN CRACKED AT STATION 258.5, ABOVE STRINGER 23L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,089 hrs · 59,689 cycles

FUSELAGE SKIN CRACKED AT STATION 258.3, STRINGER 23L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,089 hrs · 59,689 cycles

FUSELAGE SKIN CRACKED AT STATION 258.5, ABOVE STRINGER 23R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,089 hrs · 59,689 cycles

FUSELAGE SKIN CRACKED AT STATION 258.3, STRINGER 23R. REPAIRED SKIN IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 70,975 hrs · 59,607 cycles

BUTT SPLICE STRAP CRACKED AT BS 359.5, STRINGER 4R. R & R STRAP IAW SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,975 hrs · 59,607 cycles

STRINGER CRACKED AT BS 376, STRINGER 4R. R & R STRINGER IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,975 hrs · 59,607 cycles

SKIN CRACKED AT BS 360, BETWEEN STRINGER 5R TO 6R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,975 hrs · 59,607 cycles

SKIN CRACKED AT BS 440+2, STRINGER 1L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,975 hrs · 59,607 cycles

SKIN CRACKED AT BS 360, BETWEEN STRINGER 5R TO 6R. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 70,664 hrs · 59,400 cycles

L2 DOOR OUTSIDE EMERGENCY EXIT LIGHT INOPERATIVE. R & R LIGHT IAW MM.

Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 70,463 hrs · 59,263 cycles

RIGHT WING HYD & FIRE EXIT LINES STAND ATTACH BRACKET CRACKED AT GND SPOILER INBD ACTUATOR LOWER ATTACH POINT. R & R BRACKET IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 70,463 hrs · 59,263 cycles

RIGHT EMERGENCY EXIT LENS LOOSE. SECURED LENS IAW MM.

Part: LIGHT — LOOSE (EXIT SIGN) · airframe 69,681 hrs · 58,714 cycles

LT OVERWING EMERGENCY EXIT SIGN LIGHT ASSEMBLY LOOSE. R & R LIGHT ASSEMBLY IAW AMM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

FUSELAGE CHORD CRACKED AT STATION 727, BETWEEN STRINGER 18L & STRINGER 27L. REPAIRED CHORD IAW SWA EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

FUSELAGE CHORD CRACKED AT STATION 727 RT SIDE 5 O'CLOCK TO 9 O'CLOCK POSITION. REPAIRED CHORD IAW SWA EA.

Part: ANGLE — CRACKED (RT PYLON) · airframe 69,605 hrs · 58,654 cycles

FRAME ANGLE CRACKED AT STATION 363.65 OTBD SIDE RT PYLON. R & R ANGLE IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

AFT CARGO COMPARTMENT UPPER CHANNEL CRACKED BETWEEN BS 787 TO BS 807. R & R CHANNEL IAW SRM & DRAWING.

Part: LENS — DAMAGED (CABIN) · airframe 69,605 hrs · 58,654 cycles

EMERGENCY EXIT LENS FOGGED. R & R LENS IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

SKIN CRACKED AT BS 706+10, RBL 5. REPAIRED SKIN IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

FWD ENTRY DOOR STRAP CRACKED BETWEEN BS 348.20 TO BS 355, STRINGER 16L. R & R STRAP IAW SRM & DRAWING.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

SHEAR WEB CRACKED AT BS 348.2 BETWEEN STRINGER 16L TO STRINGER 17L. R & R SHEAR WEB IAW SRM & DRAWING.

Part: ANGLE — CRACKED (RT WING) · airframe 69,605 hrs · 58,654 cycles

RT WING REAR SPAR AREA ANGLE CRACKED AT RSS 545. R & R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (LT WING) · airframe 69,605 hrs · 58,654 cycles

LT WING TE STRUCTURE ANGLE CRACKED AT WING RSS 175. R & R ANGLE IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 670, BBL 0.07. REPAIRED CHORD IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 360, STRINGER 14L. R & R CHANNEL IAW SRM & DRAWING.

Part: LENS — BROKEN (CABIN) · airframe 69,605 hrs · 58,654 cycles

FWD LAVATORY EMERGENCY EXIT LIGHT LENS BROKEN. R & R LENS IAW AMM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

RT KEEL BEAM CORRODED BETWEEN BS 707 TO BS 727. REPAIRED KEEL BEAM IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 360, STRINGER 16L. R & R CHANNEL IAW SRM & DRAWING.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

BULKHEAD ZEE STIFFENERS CRACKED AT BS 1016, STRINGER 13R. REPAIRED ZEE STIFFENER IAW EA.

Part: ANGLE — CRACKED (RT WING) · airframe 69,605 hrs · 58,654 cycles

RT WING REAR SPAR AREA ANGLE CRACKED AT WBL 198.60. R & R ANGLE IAW SRM & DRAWING.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

AFT PRESSURE BULKHEAD STIFFENER CORRODED AT STATION 1016, BL 0. REPAIRED STIFFENER IAW SWA EA.

Part: ANGLE — CRACKED (LT AILERON TAB) · airframe 69,605 hrs · 58,654 cycles

LT WING AILERON TAB INFERNAL ANGLE CRACKED AT RSS 533+12. R & R ANGLE IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

TIE CLIP CRACKED AT BS 277, STRINGER 10R. R & R TIE CLIP IAW SRM & DRAWING.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

LT KEEL BEAM CORRODED BETWEEN BS 707 TO BS 727. REPAIRED KEEL BEAM IAW EA.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

AFT PRESS BULKHEAD WEB CORRODED AT STATION 1016, RBL 1. REPAIRED IAW SWA EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 661, BBL 0.07. REPAIRED CHORD IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

ANGLE CRACKED AT BS 277+13, BETWEEN STRINGER 13R TO STRINGER 14R. R & R ANGLE IAW SRM & DRAWING.

Part: RETAINER — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

FWD ENTRY DOOR CUTOUT CRACKED ON UPPER FWD CORNER RETAINER AT BS 312. R & R RETAINER IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

WEB CRACKED BETWEEN BS 277 & BS 291.3, STRINGER 14R. R & R WEB IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

WEB CRACKED AT BS 294.5, STRINGER 11L. R & R WEB IAW SRM & DRAWING.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

FWD GALLEY DOOR STUB FRAME CUT OUT CRACKED AT BS 296.4, BETWEEN STRINGER 7R & STRINGER 10R. REPAIRED STUB FRAME IAW EO & EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

DOME WEB CRACKED AT BS 1016, STRINGER 23L. REPAIRED WEB IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 294.5 TO BS 303.9, STRINGER 10L. R & R ANGLE IAW SRM & DRAWING.

Part: RETAINER — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

FWD ENTRY DOOR CUTOUT IN FWD CABIN LOWER FWD CORNER RETAINER CRACKED AT BS 312. R & R RETAINER IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

FWD ENTRY DOOR LOWER HINGE CUTOUT CRACKED "H" STRAP BETWEEN BS 294.5 TO BS 303.9, STRINGER 13L. R & R "H" STRAP IAW SRM & DRAWING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

FLOOR STRUCTURE BEAM CORRODED AT BS 344, BETWEEN LBL 7 & LBL 9. REPAIRED BEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

FLOOR BEAM CORRODED AT STATION 989.5, LBL 15 TO RBL 46. REPAIRED BEAM IAW SWA EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

WEB CRACKED BETWEEN BS 294.5 TO BS 312, STRINGER 4L. R & R WEB IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

ANGLE CRACKED AT BS 328, RBL 31.5. R & R ANGLE IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

FITTING CRACKED BETWEEN BS 291.3 & BS 294.3, STRINGER 8R. R & R FITTING IAW EA.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

R1 DOOR CUTOUT T FITTING CRACKED AT BS 334, STRINGER 8R. R & R T FITTING IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

ANGLE CRACKED AT BS 328, LBL 45. R & R ANGLE IAW SRM & DRAWING.

Part: COVER — BROKEN (EXTERIOR) · airframe 69,605 hrs · 58,654 cycles

RT OVERWING EXTERNAL EMERGENCY EXIT LIGHT COVER BROKEN. R & R COVER IAW AMM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 69,605 hrs · 58,654 cycles

MAIN WW PRESSURE DECK CRACKED AT BS 664+2, LBL 24.5+8. REPAIRED DECK IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 661, BBL 0.07. REPAIRED CHORD IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

WEB CRACKED AT BS 706, LBL 46. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 69,605 hrs · 58,654 cycles

RT WING LE CRACKED AT STATION 208. REPAIRED SKIN IAW EA.

Part: SUPPORT ANGLE — CRACKED (NR 1 NACELLE) · airframe 69,605 hrs · 58,654 cycles

SUPPORT ANGLE CRACKED AT INTERNAL AREA OF STRUT TORQUE BOX ACCESS 5757L NR 1 ENG. R & R ANGLE IAW SRM & DRAWING.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 69,605 hrs · 58,654 cycles

MAIN WW PRESSURE DECK CRACKED AT BS 664, LBL 24.5+ 8. REPAIRED DECK IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

NLG WW CRACKED AT BS 243.7 +2.5, LBL 16.0. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (CARGO DOOR) · airframe 69,605 hrs · 58,654 cycles

WEB CRACKED ON INTERNAL STRUCTURE, 8" UP FROM AFT EDGE & 4" FROM AFT EDGE & 4" FROM AFT EDGE, AFT CARGO DOOR. R & R DOOR IAW AMM.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

NLG WW CRACKED AT BS 243.7 +3.5, LBL 16.0. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 69,605 hrs · 58,654 cycles

RT WING NR 6 SLAT INBD SIDE LOWER SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 69,605 hrs · 58,654 cycles

AFT LOWER CORNER OF FRAME EDGE OF AFT CARGO DOOR CRACKED. R & R DOOR IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

FUSELAGE BS 727 LT FRAME CHORD CRACKED AT STRINGER 18L TO STRINGER 27L. REPAIRED CHORD IAW SWA EA & EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

FUSELAGE BS 727 RT FRAME CHORD CRACKED AT STRINGER 18R. REPAIRED FRAME IAW SWA EA & EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

SKIN CRACKED AT BS 706 + 10, LBL 5. REPAIRED SKIN IAW SRM.

Part: LIGHT — DIRTY (CABIN) · airframe 69,605 hrs · 58,654 cycles

EEPLS DIRTY. R & R EEPLS IAW MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 69,605 hrs · 58,654 cycles

LT STRINGER 18A CRACKED AT BS 727. REPAIRED STRINGER IAW SWA EA & EO.

Part: GLOWSTRIP — DIRTY (CABIN) · airframe 68,808 hrs · 58,038 cycles

RT PHOTOLUMINESCENCE STRIP DIRTY AT ROW 8. CLEANED EEPLS IAW STANDARD INDUSTRY PRACTICES.

Part: WEB — CRACKED (NLG WW) · airframe 68,808 hrs · 58,038 cycles

RT NOSE WW CRACKED AT STATION 259.5 - 1", WL 179. REPAIRED WEB IAW SRM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 68,790 hrs · 58,026 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW AMM.

Part: HINGE FITTING — BROKEN (RT SPOILER) · airframe 68,384 hrs · 57,719 cycles

RT WING I/B GROUND SPOILER O/B HINGE FITTING BROKEN. R&R GROUND SPOILER IAW MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 68,221 hrs · 57,607 cycles

AFT INBD EMERGENCY FLASHLIGHT INOP. R & R BATTERY ASSY IAW MM.

Part: ATTACH FITTING — BROKEN (LT SPOILER) · airframe 67,442 hrs · 57,058 cycles

LEFT WING GROUND SPOILER (NR 4) ATTACH FITTING BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,213 hrs · 56,189 cycles

FUSELAGE SKIN CRACKED AT BS 400+14, STR 1L. REPAIRED SKIN PER EA.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 65,805 hrs · 55,865 cycles

RIGHT EMERGENCY EXIT LIGHTS INOP BETWEEN ROW 21 TO ROW 23. REMOVED AND REPLACED CHARGER PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,784 hrs · 55,848 cycles

LEFT EMERGENCY EXIT LIGHT INOP BETWEEN ROW 21 TO ROW 23. REMOVED AND REPLACED BATTERY PACK PER M/M.

Part: SIGN — LOOSE (CABIN) · airframe 65,526 hrs · 55,651 cycles

LEFT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER M/M.

Part: SIGN — LOOSE (CABIN) · airframe 65,525 hrs · 55,651 cycles

LEFT OVERWING EMERGENCY EXIT SIGN LOOSE. REINSTALLED OVERWING EXIT SIGN PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 65,162 hrs · 55,371 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER MP.

Part: LENS — LOOSE (CABIN) · airframe 65,093 hrs · 55,311 cycles

OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 2. SECURED LENS PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 64,638 hrs · 54,970 cycles

LT OVERHEAD BULLNOSE EMERGENCY EGRESS LIGHTS INOP AT ROW 2. REMOVED & REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 64,638 hrs · 54,970 cycles

RT OVERHEAD BULLNOSE EMERGENCY EGRESS LIGHTS INOP AT ROW 5. REMOVED & REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO BAY I/B VERTICAL STIFFENER CRACKED AT BS 727, STR 27L. REPAIRED STIFFENER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 25L. REMOVED AND REPLACED FRAME IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24.8. REPAIRED BEAM IAW EA.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO BAY INTERNAL DOUBLER CORRODED AT BS 967, BETWEEN STR 26L TO STR 27R. REPAIRED DOUBLER PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 18R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CORRODED AT BS 727E, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME IAW ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 25R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 867, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CORRODED BETWEEN BS 443 TO BS 489, STR 26R. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CORRODED AT BS 967, STR 27L. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 27L. REMOVED AND REPLACED CLIP IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CORRODED AT BS 727, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 280, STR 19R. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 794, STR 26R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO FRAME CORRODED AT BS 747, BETWEEN STR 26R TO STR 17R. REPAIRED FRAME IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO FRAME CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM AND DWG.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO BAY FRAME FAIL SAFE ANGLE CORRODED AT BS 727E, BETWEEN STR 27L TO STR 27R. REPAIRED ANGLE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 967, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 927, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 807, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO BAY SHEAR TIE CORRODED AT BS 927, BETWEEN STR 25R TOS TR 26R. REPAIRED SHEAR TIE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 328, BL 0. REMOVED AND REPLACED CHORD IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 867, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 18L. REMOVED AND REPLACED CLIP IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 727C+7, LBL 7.5. REPAIRED BEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK FOUND, FLOORBEAM INNER CHORD CORRODED AT BS 727D+6, LBL 12. REPAIRED CHORD IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 460, STR 21L. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULE 20Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 727A, STR 26L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK FOUND, RT FRAME INNER CHORD CRACKED AT BS 616, WL 203. REPAIRED CHORD IAW EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULE 20Y CHECK FOUND, FWD CARGO DOOR WEB CORRODED BETWEEN BS 440 TO BS 492, BETWEEN RBL 23 TO RBL 30. REPAIRED WEB IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK FOUND, SHEAR TIE CORRODED AT BS 440, BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK FOUND, STRINGER CLIP RACKED AT BS 727A, STR 25R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK FOUND, FRAME CORRODED AT BS 767, BETWEEN STR 26L TO STR 25L. REPAIRED FRAME IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 727B, STR 25L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,648 hrs · 54,223 cycles

DURING SCHEDULED 20Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 727D, STR 25L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: WEDGE — PUNCTURED (RT WING TE FLAP) · airframe 63,593 hrs · 54,180 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING I/B AFT FLAP WEDGE PUNCTURED. REMOVED AND REPLACED WEDGE IAW MM.

Part: ATTACH FITTING — BROKEN (LT WING SPOILER) · airframe 63,593 hrs · 54,180 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 4 GROUND SPOILER ATTACH LUG AT O/B ACTUATOR BROKEN. REMOVED AND REPLACED SPOILER IAW MM.

Part: CONTROLLER — FAULTY (COCKPIT) · airframe 63,533 hrs · 54,133 cycles

DIVERSION - ON CLIMBOUT, SMALL CABIN ALTITUDE NEEDLE POINTING AT "50." AT 10K, CARGO DIFF NEEDLE SHOWING 612. SWITCHES VERIFIED "FLT/AUTO" CABIN CLIMB MOVED BUT NOT IN NORMAL PATTERN. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 63,203 hrs · 53,889 cycles

DURING SCHEDULE MV1 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 62,928 hrs · 53,694 cycles

DURING SCHEDULED OTS CHECK, FOUND L1 DOOR EMERGENCY INADVERTANTLY FELL OUT, DID NOT DEPLOY. REINSTALLED SLIDE IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,538 hrs · 52,656 cycles

LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,344 hrs · 52,508 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME CRACKED AT BS 420, BETWEEN STR 18R TO STR 19R. REPAIRED FRAME PER EA.

Part: SKIN — PUNCTURED (FOREFLAP) · airframe 61,344 hrs · 52,508 cycles

DURING SCHEDULED OTS CHECK, FOUND RT WING I/B FORE FLAP LOWER SURFACE PUNCTURED. REPAIRED FORE FLAP PER SRM.

Part: ROD END — CORRODED (ELEVATOR TAB) · airframe 60,930 hrs · 52,193 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT ELEVATOR TAB ROD END CORRODED. REMOVED AND REPLACED ROD PER EA.

Part: LENS — LOOSE (CABIN) · airframe 60,007 hrs · 51,455 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 59,948 hrs · 51,401 cycles

AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 58,980 hrs · 50,654 cycles

LT WING EMERGENCY EXIT LIGHT SIGN LOOSE. SECURED SIGN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,781 hrs · 50,506 cycles

DURING SCHEDULED SPV CHECK, FOUND LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,926 hrs · 49,877 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 19L TO STR 20L. REPAIRED FRAME PER SI.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,926 hrs · 49,877 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CRACKED AT BS 364, STR 4L. REPAIRED STRINGER SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,926 hrs · 49,877 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,926 hrs · 49,877 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 4L. REPAIRED FRAME PER SRM.

Part: SIGN — CRACKED (CABIN) · airframe 57,926 hrs · 49,877 cycles

DURING SCHEDULED 18Y CHECK, FOUND FWD RT GALLEY EMERGENCY EXIT SIGN LIGHT CRACKED. REMOVED AND REPLACED SIGN PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,926 hrs · 49,877 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 19R TO STR 20R. REPAIRED FRAME PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 57,508 hrs · 49,562 cycles

DURING SCHEDULED MV1 CHECK, L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. REMOVED AND REPLACED SLIDE PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 57,115 hrs · 49,248 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 57,115 hrs · 49,248 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LEFT A/C BAY DOOR FRAME CRACKED AT BS 540. REMOVED AND REPLACED FRAME PER SRM.

Part: DETECTOR — FAULTY (APU) · airframe 56,989 hrs · 49,148 cycles

DECLARED EMERGENCY, APU FIRE INDICATION IN FLIGHT. DISCHARGED THE APU FIRE BOTTLE BUT THE FIRE INDICATION STAYED "ON" ALL THE WAY TO LANDING. REMOVED AND REPLACED M717, M515, M334 APU FIRE DETECTORS.

Part: GASPER FAN — FAULTY (CABIN) · airframe 55,947 hrs · 48,397 cycles

SULFUR SMELL NOTED ON CLIMBOUT. NO ABNORMAL INDICATIONS OR SMOKE NOTED. ODOR STRONGEST AT ROW 4. FLIGHT ATTENDANT NOTICED SIMILAR ODOR ON DESCENT. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 55,408 hrs · 48,018 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 54,696 hrs · 47,554 cycles

FOUND L2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 54,696 hrs · 47,554 cycles

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

Part: FIRE DETECTOR — FAULTY (APU) · airframe 54,244 hrs · 47,246 cycles

AT FL 8000 APU FIRE WARNING LIGHT ILLUMINATED AND WARNING SOUNDED, DISCHARGED FIRE BOTTLE AND LIGHT EXTINGUISHED. REMOVED AND REPLACED OVERHEAT DETECTOR PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,158 hrs · 47,176 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SHEAR TIE — CRACKED (BS 360 S28L) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 28L. REPAIRED SHEAR TIE PER SRM.

Part: TERMINAL — LOOSE (EMERGENCY LIGHT) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 6 DEF. FOUND LOOSE TERMINAL. SECURED TERMINAL PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500C, STR 26R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 11R CRACKED AT BS 355. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 20R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 23R CRACKED AT BS 540. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 22R CRACKED AT BS 540. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 540, STR 23R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 20R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 400, STR 13R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 23L. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER TEE CHORD CRACKED AT BS 724, LBL 25. REMOVED AND REPLACED TEE CHORD PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 13R. R&R STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 767, STR 17R. R&R SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER TEE CHORD CRACKED BETWEEN BS 655 AND BS 675, LBL 25. R&R CHORD PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 440, STR 13R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER TEE CHORD CRACKED BETWEEN BS 655 AND BS 675, RBL 25. REMOVED AND REPLACED TEE CHORD PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 420, STR 13L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 480, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, STR 13L. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CORRODED AT BS 312, LBL 11 TO LBL 19. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 13R. REPAIRED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 420, STR 13R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 460, STR 13R. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 16 TO RBL 37. REPAIRED FLOORBEAM PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 420, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 540, STR 18L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 480 TO BS 500, LBL 68. REMOVED AND REPLACED WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 967, RBL 28 TO RBL 42. REMOVED AND REPLACED CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 400 TO BS 420, LBL 68. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 53,826 hrs · 49,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 14R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,826 hrs · 49,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 14R CRACKED AT BS 887. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,826 hrs · 49,936 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 907 S6R) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 6R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (BS 188 S17L) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 188, STR 17L. REMOVED AND REPLACED CHORD PER SRM.

Part: FRAME — CRACKED (BS 188 S17R) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 188, STR 17R. REMOVED AND REPLACED CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S8L) · airframe 53,826 hrs · 49,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 188 S17R) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 188, STR 17R. REPAIRED FRAME CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616 S5L) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (BS 867-887) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 867 TO BS 887, LBL 65. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (BS 907 S4L) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616 S5R) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND NLG W/W RIGHT CEILING PANEL WEB CUTOUT CRACKED AT RBL 2.7. REPAIRED WEB PER ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT CRACKED AT BS 413, LBL 3. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R AND STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 53,826 hrs · 46,936 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CABIN EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: SLAT — CRACKED (LT WING) · airframe 53,583 hrs · 46,753 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR1 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,232 hrs · 45,738 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 945, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,109 hrs · 44,827 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 22L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CHAFED (FUSELAGE) · airframe 50,109 hrs · 44,076 cycles

DURING SCHEDULED BRDG CHECK, FOUND UPPER FUSELAGE SKIN CHAFED AT DORSAL FIN SECTION BS 857 TO BS 870. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,109 hrs · 44,076 cycles

DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR CUTOUT FWD FRAME CRACKED AT BS 303, STR 16L. REPAIRED FRAME SECTION PER SRM.

Part: FITTING — CORRODED (L1 DOOR) · airframe 50,109 hrs · 44,076 cycles

DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM.

Part: SHEAR TIE — CRACKED (BS 294 S10L) · airframe 50,109 hrs · 44,076 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CRACKED AT BS AT BS 294, STR 10L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,109 hrs · 44,076 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 743D, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,109 hrs · 44,076 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 742D, STR 24L. REPAIRED SKIN PER SWA EA.

Part: HANDLE — OUT OF ADJUST (COCKPIT) · airframe 50,109 hrs · 44,076 cycles

DURING SCHEDULED 14Y CHECK, FOUND FLIGHT COMPT R2 WINDOW EMERGENCY RELEASE HANDLE INOP. ADJUSTED R2 WINDOW RELEASE HANDLE PER MM.

Part: TORQUE TUBE — WORN (T/E FLAP) · airframe 50,109 hrs · 44,076 cycles

DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING AFT FLAP OUTBOARD TORQUE TUBE FAILED CHECK. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: SKIN — CRACKED (BS 743D S23L) · airframe 50,087 hrs · 44,061 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 743D, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 742 S24L) · airframe 50,087 hrs · 44,061 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 742D, STR 24L. REPAIRED SKIN PER SWA EA.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 49,122 hrs · 43,326 cycles

DURING SCHEDULED C4 CHECK, FOUND RT FWD CABIN EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: FITTING — CORRODED (LT MLG) · airframe 49,054 hrs · 43,268 cycles

DURING SCHEDULED A2 CHECK, FOUND LT MLG FWD OUTBOARD HANGER FITTING CORRODED. REMOVED AND REPLACED HANGER FITTING PER SWA EA.

Part: FAN — FAULTY (GASPERS) · airframe 48,083 hrs · 42,488 cycles

ON FINAL DESCENT, ODOR COMING FROM GASPER VENTS IN THE CABIN. REMOVED AND REPLACED GASPER FAN PER MM.

Part: ACTUATOR — FAILED (RT MLG WW) · airframe 47,535 hrs · 42,065 cycles

AIR TURNBACK, RT MLG UNSAFE GEAR INDICATION, GEAR HANDLE IN THE UP POSITION, RED UNSAFE LIGHT ILLUMINATED. REMOVED AND REPLACED RT MLG ACTUATOR PER MM.

Part: SKIN — CRACKED (BS 379) · airframe 47,269 hrs · 41,856 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 379, LBL 2, AFT SIDE OF E & E COOLING DUCT EXHAUST PORT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,269 hrs · 41,856 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT, LOWER AFT CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 47,269 hrs · 41,856 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 46,247 hrs · 41,069 cycles

DURING SCHEDULED RON CHECK, FOUND EEPLS STRIP DAMAGED. REMOVED AND REPLACED EEPLS SECTION PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 45,483 hrs · 40,471 cycles

EEPLS STRIP LOOSE AT FWD END. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (FWD GALLEY) · airframe 44,880 hrs · 39,970 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD GALLEY LOWER EMERGENCY EXIT LIGHT INOP. SECURED LIGHT PER MM.

Part: SLIDE — DEPLOYED (R2 DOOR) · airframe 44,521 hrs · 39,683 cycles

R2 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MM.

Part: SKIN — CRACKED (R1 DOOR) · airframe 44,409 hrs · 39,590 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,409 hrs · 39,590 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 769, STR 24L. REPAIRED SKIN PER SRM.

Part: LIGHT — FAULTY (COCKPIT) · airframe 44,336 hrs · 39,529 cycles

RIGHT MLG GREEN LIGHT INDICATOR INOP DURING GEAR EXTENSION. RECYCLED MLG HANDLE-LIGHT ILLUMINATED. REMOVED AND REPLACED KORRY LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,585 hrs · 38,125 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 24L. REPAIRED SKIN PER SWA EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,202 hrs · 37,824 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT AT ROW 8 DEF, INOP. RELAMPED LIGHT PER MM.

Part: SEAL — TORN (AFT CARGO DOOR) · airframe 41,782 hrs · 37,469 cycles

DECLARED EMERGENCY/DIVERSION. AT FL370 ALTITUDE WARNING HORN CAME ON. CABIN ALTITUDE WAS 9500 FT. WENT TO STANDBY ON PRESSURE CONTROLLER, NO HELP. WENT TO MANUAL AND STARTED AN EMERGENCY DESCENT, CABIN GOT TO 11500 FT. NO WARNING LIGHTS. REMOVED AND REPLACED AFT CARGO DOOR SEAL, PER MM.

Part: PUSHROD — WORN (ELEVLATOR) · airframe 41,775 hrs · 37,461 cycles

DURING SCHEDULED C4 CHECK, RT ELEVATOR FAILED THE FREEPLAY CHECK. REMOVED AND REPLACED RIGHT ELEVATOR CONTROL PUSH ROD ATTACH BOLTS PER MM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 41,488 hrs · 37,242 cycles

DURING RON, FOUND NLG ACTUATOR UPPER ATTACH FITTING GUSSET CRACKED. REMOVED AND REPLACED NLG FITTING PER SRM.

Part: DOUBLER — CRACKED (AFT CARGO DOOR) · airframe 41,368 hrs · 37,143 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR DOUBLER AT BS 793, RBL 9, CRACKED. REPAIRED DOUBLER PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 41,368 hrs · 37,143 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 794, RBL 7 TO RBL 11, CORRODED. REPAIRED SHEAR TIE PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 41,368 hrs · 37,143 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 927, STRINGER 27L, CORRODED. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 41,193 hrs · 37,000 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT WING AFT OUTBOARD T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING AFT OUTBOARD T/E FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,211 hrs · 35,411 cycles

DURING SCHEDULED PM CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT STRINGER 23L, BS 747, AND BS 727E. REPAIRED SKIN PER SRM.

Part: PCU — LEAKING (MLG WW) · airframe 38,891 hrs · 35,143 cycles

DIVERSION, DECLARED EMERGENCY HYD 'A' SYS QTY IND DECREASED AND 'A' SYS ENG DRIVEN PUMP LOW PRESS LIGHT ILLUMINATED. FOUND HYD FLUID LEAK AT 'A' SYS AILERON PCU. REMOVED AND REPLACED SAME PER MM.

Part: ENGINE — FAILED (NR 2) · airframe 38,694 hrs · 34,964 cycles

ABORTED TAKEOFF, NR 2 ENGINE WOULD NOT ACCELERATE ON TAKEOFF. REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,268 hrs · 33,794 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR, LOWER FWD CORNER CUTOUT. REPAIRED SKIN PER SRM.

Part: COVER — OUT OF POSITION (SERVICE DOOR) · airframe 36,486 hrs · 33,170 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE COVER FELL OFF. REINSTALLED COVER PER MM.

Part: TAB — WORN (LT ELEVATOR) · airframe 36,075 hrs · 32,833 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11139-55, LEFT ELEVATOR NR 3 AND NR 4 HINGE ATTACH POINTS WORN. REMOVED AND REPLACED LEFT ELEVATOR TAB PER MM.

Part: BEARING — FAILED (NR 2 ENGINE) · airframe 35,358 hrs · 32,228 cycles

DIVERSION, ON CLIMB-OUT FROM HOU, AIRFRAME LATERAL VIBRATION FELT, NR 2 ENGINE N2 IND FLUCTUATES 2.0 PERCENT. REMOVED AND REPLACED NR 2 ENGINE DUE TO AGB SHAFT BEARING FAILURE PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 34,591 hrs · 31,584 cycles

DURING SCHEDULED PM CHECK, FOUND LT OTBD T/E FLAP DELAMINATED ON BOTTOM SURFACE. REMOVED AND REPLACED LT OTBD T/E FLAP PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 34,495 hrs · 31,500 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB BUSHINGS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,081 hrs · 30,329 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (5 EA) AT STR 8L, BS'S 380, 400, 440, 867 AND 907. REPAIRED FRAMES PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,081 hrs · 30,329 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (4 EA) AT STR 8R, BS'S 360, 400, 440 AND 867. REPAIRED FRAMES PER BFG ER.

Part: ACTUATOR — CRACKED (SPOILER) · airframe 33,081 hrs · 30,329 cycles

DURING SCHEDULED D CHECK, FOUND NR 4 GROUND SPOILER OTBD ACTUATOR CRACKED. REMOVED AND REPLACED ACTUATOR PER MM.

Part: STIFFENER — CRACKED (LT HORIZ) · airframe 33,081 hrs · 30,329 cycles

DURING SCHEDULED D CHECK, FOUND LT HORIZ STAB MAIN BOX INTERIOR L/E STIFFENER ON INTERSPAR WEB CRACKED AT STA 95. REPAIRED STIFFENER PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 33,081 hrs · 30,329 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE WEB CRACKED AT BS 294, STR 12L. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,081 hrs · 30,329 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 827, WL 148 AND LBL 1. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,081 hrs · 30,329 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 33,081 hrs · 30,329 cycles

DURING SCHEDULED D CHECK, FOUND 2 EA STRINGER SPLICES CRACKED, BS 907, STR 4L AND STR 4R. REMOVED AND REPLACED STRINGER SPLICE SECTIONS PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,081 hrs · 30,329 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED, BS 616 TO BS 639 RT SIDE. REPAIRED BEAM WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 32,009 hrs · 29,442 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND WEB CRACKED .125 LONG ST BS 178, LBL 90 & WL 234. REPAIRED WEB PER SRM.

Part: COVER — DAMAGED (CABIN FLOOR) · airframe 31,419 hrs · 28,944 cycles

EEPLS COVERS DAMAGED. R&R EEPLS COVERS PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 30,752 hrs · 28,392 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY AND SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY''S PER MM.

Part: SLIDE — OUT OF ADJ (FWD SVC DOOR) · airframe 30,280 hrs · 28,105 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 29,141 hrs · 27,055 cycles

EEPLS WIRES EXPOSED. SECURED EEPLS TRACK PER MM.

Part: CONTROLLER — INOP (COCKPIT)

AIR TURNBACK, AIRCRFT WOULD NOT PRESSURIZE AFTER TAKEOFF. REMOVED AND REPLACED PRESSURE CONTROLLER PANEL PER MM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND THROUGH EDDY CURRENT INSP, BS 178 BULKHEAD SIDE CHORD CRACKED, LBL 26, AND RBL 26. REMOVED AND REPLACED SIDE CHORD SECTIONS PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 5 AND LBL 5. REPAIRED BULKHEAD PER SRM.

Part: LIGHT — INOP (ROW 17)

DURING SCHEDULED 1/4D CHECK, FOUND EEPLS INOP AT ROW 17. RELAMPED PER MM.

Part: FRAME — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT FRAME CRACKED AT LOWER END. REPAIRED FRAME PER BOEING DRAWING.

Part: LIGHT — LOOSE (ROW 9 & 14)

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHTS LOOSE AT OVERHEAD BIN BULLNOSE, ROWS 9 RT AND 14 LT. RESECURED LIGHTS PER MM.

Part: TO WARNING — ACTIVATED (COCKPIT.)

ABORTED TAKEOFF WHEN MASTER CAUTION, AND ENG ANNUNCIATOR LIGHTS STAYED OUT ON RECALL FOR TAKEOFF, TAKE OFF WARNING HORN SOUNDED. PERFORMED TAKEOFF WARNING CHECK PER MM OPS CHECKED GOOD.

Part: WIRE — EXPOSED (CABIN)

DURING INSPECTION, FOUND TRACK LIGHTING IN FLOOR BY ROW 14 HAS EXPOSED WIRES. SECURED WIRES PER MM.

Part: LIGHTS — INOPERATIVE (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY LIGHTS BETWEEN ROW 12-16 INOP. REPAIRED WIRING ON EGRESS LIGHTS PER BOEING MM.

Part: FLOOR LIGHTS — INOPERATIVE (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT FLOOR LIGHTS ROW 14-16 INOP. RESECURED PER BOEING MM.

Part: FAN BLADES — DAMAGED (NR 1 ENGINE)

RETURNED TO MSY AND MADE AN UNEVENTFUL LANDING DUE TO BIRD STRIKE TO RADOME AND NR 1 ENGINE. PERFORMED BIRD STRIKE INSPECTION, FOUND 8 ENGINE FAN BLADES BENT. REMOVED AND REPLACED 8 FAN BLADES PER BOEING MM, WITH A BORESCOPE SCHEDULED WITHIN 10 CYCLES.

Part: STRUCTURE — BIRD STRIKE (AIR FRAME)

AFTER TAKEOFF, SUSTAINED BIRD STRIKE TO AIRCRAFT. AIRCRAFT DIVERTED TO SMF AND MADE AN UNEVENTFUL LANDING. PERFOMED BIRD STIRKE INSPECTION PER BOEING M/M WITH NO DEFECTS NOTED.

Part: MODULE — FAILED (A-HYD SYSTEM)

AFTER TAKEOFF, EXPERIENCED A' SYSTEM HYD PRESSURE LOSS. ALSO, HAD NOSE LANDING GEAR RED LIGHT ILLUMINATED WITH GEAR HANDLE IN OFF. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. REPLACED A-SYSTEM MODULE CHECK VALVE AND RETRACTTION TESTED GEAR PER BOEING M/M.

Part: SKIN — DENTED (LT HORZ STAB)

DURING WALKAROUND INSPECTION, FOUND HORZ STAB L/E DENTED 4 FEET FROM ROOT AREA, LEFT SIDE. REPAIRED PER SWA RA 1-A55-0209R1.

Part: DOOR — OPEN (E/E COMPT)

AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE, NO WARNING INDICATION. RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND E AND E DOOR OPEN. SECURED DOOR, DEFERRED WARNING LIGHT AND CONTINUED PER MEL 52-2.

Part: FRAME — CRACKED (CARGO DOOR)

DURING SCHEDULED C4 CHECK, FOUND FWD CARGO DOOR FRAME CRACKED ON INNER RADIUS OF FWD SIDE, JUST UNDER LOCK HOOK ASSY. REPAIRED PER SWA RA 1-A52-198.