N670SW

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,692 hrs · 67,003 cycles

FORWARD GALLEY EMER LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,622 hrs · 66,948 cycles

FUSELAGE SKIN CRACKED AT BS 727D+2, STRINGER 19R. REPAIRED SKIN IAW SRM.

Part: SIGN — LOOSE (CABIN) · airframe 82,338 hrs · 66,734 cycles

RIGHT EMER EXIT SIGN LOOSE. R & R SIGN IAW WDM SIP.

Part: SKIN PANEL — CRACKED (RT WING) · airframe 81,700 hrs · 66,246 cycles

RIGHT WING FIXED LE LOWER SKIN PANEL JUST OTBD OF NR 2 ENG PYLON OTBD MID FITTING CRACKED. REPAIRED PANEL IAW EA.

Part: BRACKET — CRACKED (RT WING) · airframe 80,166 hrs · 65,164 cycles

RT WING TE BRACKET CRACKED BETWEEN WBL 157 & WBL 183.4. R & R BRACKET IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

TIE CLIP CRACKED AT BS 947.5 STRINGER 24R. R & R TIE CLIP IAW SRM & DRAWING.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

FAIL SAFE CHORD CRACKED AT BS 947.5 BETWEEN STRINGER 17R TO STRINGER 23R. R & R CHORD IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

FWD CARGO COMPARTMENT WEB CRACKED AT BS 520 BL 0. R & R WEB IAW SRM & DRAWING.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

STRINGER CRACKED AT BS 787, STRINGER 19L. REPAIRED STRINGER IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 706+7.5 BBL 0.07. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 80,166 hrs · 65,164 cycles

LT WING LE SKIN CRACKED AT WL 185. REPAIRED SKIN IAW EA.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

SUPPORT FITTING CRACKED AT BS 294.5 STRINGER 8R. R & R FITTING IAW DRAWING & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

FUSELAGE SKIN CRACKED AT BS 380+17 STRINGER 25L. REPAIRED SKIN IAW EO & EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

CHANNEL CRACKED AT BS 500 STRINGER 26R. R & R CHANNEL IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

WEB CRACKED BETWEEN BS 380 TO BS 400 BL 0. R & R WEB IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

ANGLE CRACKED BETWEEN BS 380 TO BS 400 BL 0. R & R ANGLE IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

TIE CLIP CRACKED AT BS 500D STRINGER 19R. R & R TIE CLIP IAW SRM & DRAWING.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

CHORD CRACKED AT BS 348.2 STRINGER 17L. R & R CHORD IAW SRM.

Part: DOUBLER — CRACKED (FLAP TRACK) · airframe 80,166 hrs · 65,164 cycles

LT WING NR 3 FAIRING FLAP TRACK INBD DOUBLER CRACKED. R & R DOUBLER IAW DRAWING & SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

BULKHEAD GORE WEB CRACKED AT BS 1016 STRINGER 7L. REPAIRED WEB IAW SWA EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

STUB BEAM CRACKED AT BS 294.5, STRINGER 17R. R & R STUB BEAM IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

FRAME CRACKED AT BS 328, BETWEEN STRINGER 20R TO STRINGER 21R. R & R FRAME IAW SRM & DRAWING.

Part: REVEAL — CRACKED (L1 DOOR) · airframe 80,166 hrs · 65,164 cycles

L1 DOOR REVEAL CRACKED AT BS 328 BETWEEN STRINGER 15L TO STRINGER 17L. R & R REVEAL IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

STUD FRAME CRACKED AT BS 294.5 BETWEEN STRINGER 7R TO STRINGER 8R. R & R STUD FRAME IAW SRM & DRAWING.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17.0. REPAIRED WEB IAW EO & EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

BULKHEAD VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17.0. REPAIRED WEB IAW EO & EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17.0. REPAIRED WEB IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

FRAME WEB CRACKED AT BS 947.5, BETWEEN STRINGER 18R TO STRINGER 19R. R & R FRAME IAW EO & EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

STRINGER CRACKED AT BS 380+17 STRINGER 5L. REPAIRED STRINGER IAW EO & EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

STRINGER CRACKED AT BS 400+3.5 STRINGER 5L. REPAIRED STRINGER IAW EO & EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

STRINGER CRACKED AT BS 400+2.7 STRINGER 5L. REPAIRED STRINGER IAW EO & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

ANGLE CRACKED AT BS 827 BETWEEN STRINGER 1L & STRINGER 2L. R & R ANGLE IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

DOME CAP WEB CRACKED AT BS 1016 STRINGER 15L. REPAIRED WEB IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

DOME CAP WEB CRACKED AT BS 1016 STRINGER 7L. REPAIRED WEB IAW EA.

Part: SKIN — DELAMINATED (NR 3 SPOILER) · airframe 80,166 hrs · 65,164 cycles

LT WING NR 3 SPOILER UPPER SURFACE DELAMINATED. R & R SPOILER IAW AMM.

Part: WEB — CRACKED (NLG WW) · airframe 80,166 hrs · 65,164 cycles

RT SIDE NLG WHEEL WEB CRACKED AT BS 259.5, WL 185. REPAIRED WEB IAW SRM.

Part: FRAME — MISSING (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

FRAME INNER CHORD MISSING FASTENER HOLE AT BS 348.2 STRINGER 15L. R & R CHORD IAW SRM EO & EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 907 STRINGER 4R. R & R CHANNEL IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

FWD CARGO DOOR CUTOUT CRACKED AT BS 492.4, STRINGER 25R. REPAIRED CUTOUT IAW SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 80,166 hrs · 65,164 cycles

FWD CARGO DOOR SKIN CUTOUT CRACKED. REPAIRED SKIN IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

WEB CRACKED BETWEEN BS 344 TO BS 360 BL 0. R & R WEB IAW SRM & DRAWING.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 665.5 LBL 24.5. REPAIR CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

SKIN CRACKED AT BS 294.5+15, STRINGER 7R. REPAIRED SKIN IAW EO & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

LONGITUDINAL FLOOR BEAM CRACKED AT BS 667 RBL 24.8. REPAIRED CHORD IAW EO & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 665.5 RBL 24.5. REPAIRED CHORD IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

SKIN CRACKED AT BS 867 STRINGER 20L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

SKIN CRACKED AT BS 328-2.5, STRINGER 8R. REPAIRED SKIN IAW EO & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED BETWEEN BS 707 TO BS 711 BL 0. REPAIRED WEB IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

WEB CRACKED BETWEEN BS 294.5 TO BS 312 LBL 27. R & R WEB IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

ANGLE CRACKED BETWEEN BS 887 TO BS 907, RBL 46. R & R ANGLE IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

FUSELAGE SKIN CRACKED AT BS 294.5+11 STRINGER 18R. REPAIRED SKIN IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 671 LBL 24.5. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

LONGITUDINAL FLOOR BEAM CHORD CRACKED AT BS 670 RBL 24.8. REPAIRED CHORD IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

FUSELAGE SKIN CRACKED AT BS 328 STRINGER 8R. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

FUSELAGE SKIN CRACKED AT BS 500C+2.5 STRINGER 26L. REPAIRED SKIN IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 667, LBL 24.5. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

FUSELAGE SKIN CRACKED AT BS 500D+14.5, STRINGER 16L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

FUSELAGE SKIN CRACKED AT BS 500D+5 STR 16L. REPAIRED SKIN IAW EO & EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 80,166 hrs · 65,164 cycles

LT WW PRESS FLOOR DECK WEB CRACKED AT BS 663.75 LBL 24.5+14. REPAIRED WEB IAW EO & EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 80,166 hrs · 65,164 cycles

MAIN WW FLOOR DECK WEB CRACKED AT BS 663.75 RBL 24.5+18. REPAIRED WEB IAW EO & EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

RT OTBD CHORD CRACKED AT BS 727 AFT LOWER FASTENER HOLE AT 6 O'CLOCK. R & R CHORD IAW EO & EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

STRINGER CRACKED AT BS 727 18A RT AFT LOWER FASTENER HOLE BETWEEN 6 & 12 O'CLOCK. REPAIRED STRINGER IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

STRINGER CRACKED AT BS 727 18A LT AT LOWER AFT FASTENER HOLE BETWEEN 12 & 8 O'CLOCK. REPAIRED STRINGER IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

FRAME OTBD CHORD CRACKED AT BS 727 LT AT FASTENER HOLES BETWEEN 3 & 9 O'CLOCK. REPAIRED CHORD IAW EO & EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 80,166 hrs · 65,164 cycles

STRINGER CRACKED AT BS 727 18A LT AT UPPER AFT FASTENER HOLE AT 12 O'CLOCK. REPAIRED STRINGER IAW EO & EA.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 79,827 hrs · 64,916 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,900 hrs · 64,200 cycles

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

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 78,900 hrs · 64,200 cycles

BEAR STRAP SKIN CORRODED AT BS 986, BL 0. R&R BEAR STRAP IAW SRM & DRAWING.

Part: SKIN — CORRODED (FUSELAGE) · airframe 78,900 hrs · 64,200 cycles

BELLY SKIN CORRODED BETWEEN BS 908 - BS 1016, BETWEEN STRINGER 25L - 25R. R&R SKIN IAW DRAWING & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,900 hrs · 64,200 cycles

FUSELAGE SKIN CRACKED AT BS 416.5, STRINGER 26R. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,900 hrs · 64,200 cycles

SKIN CRACKED BETWEEN BS 500A+6 - 500A+6.7, STRINGER 26L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,900 hrs · 64,200 cycles

FUSELAGE SKIN CRACKED AT BS 908, STRINGER 1R. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,900 hrs · 64,200 cycles

SKIN CRACKED AT BS 500D + 13, STRINGER 21L. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,900 hrs · 64,200 cycles

CHEM MILL SKIN CRACKED BETWEEN BS 473.2 - 473.9, STRINGER 26L. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,900 hrs · 64,200 cycles

FUSELAGE SKIN CRACKED AT BS 977.5, STRINGER 4R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,900 hrs · 64,200 cycles

CHEM MILL SKIN CRACKED AT BS 813.5, STRINGER 18L. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,900 hrs · 64,200 cycles

CHEM MILL SKIN CRACKED AT BS 942, STRINGER 20L. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,900 hrs · 64,200 cycles

AFT ENTRY DOOR CUTOUT SKIN CRACKED AT LOWER FWD CORNER AT BS 968, STRINGER 17L. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,900 hrs · 64,200 cycles

CHEM MILL SKIN CRACKED AT BS 494, STRINGER 16L. REPAIRED SKIN IAW ER & EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 78,763 hrs · 64,097 cycles

RIGHT WING OUTBOARD AFT FLAP DELAMINATED ON INBOARD END. REMOVED AND REPLACED AFT FLAP PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,763 hrs · 64,097 cycles

FUSELAGE SKIN CRACKED AT STA 312, STR 20R. REPAIRED SKIN PER EA.

Part: LIGHT — MISSING (CABIN) · airframe 78,763 hrs · 64,097 cycles

RIGHT EEPLS MISSING AT ROW 11. INSTALLED EEPLS PER M/M.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 78,140 hrs · 63,638 cycles

FUSELAGE SKIN PANEL CRACKED AT BS 727E +13, STR 18R. REPAIRED SKIN PER SRM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 77,889 hrs · 63,461 cycles

AFT SERVICE DOOR - ESCAPE SLIDE PRESSURE GAUGE BELOW GREEN RANGE. REMOVED AND REPLACED AFT SERVICE DOOR SLIDE PER MM ICT 769328 PN OFF/ON: 61621-469 S/N OFF:0605A S/N ON: 0089A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,095 hrs · 62,898 cycles

SKIN CRACKED AT BS 360+4, STR 26L. REPAIRED SKIN PER ER AND EA.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 76,287 hrs · 62,259 cycles

L1 DOOR EMERGENCY EVAC SLIDE COVER LOOSE. SECURED SLIDE ASSY IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 75,715 hrs · 61,806 cycles

RT OVERHEAD EMERGENCY EXIT BULL NOSE LIGHT LENS MISSING AT ROW 19. INSTALLED LENS PER M/M.

Part: LATCH — LOOSE (COCKPIT) · airframe 75,358 hrs · 61,515 cycles

FIRST OFFIER'S ESCAPE ROPE STOWAGE DOOR EXCESS STRAP DOOR LATCH ASSY LOOSE. REMOVED AND REPLACED LATCH ASSY PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

STRINGER TIE CLIP CRACKED AT BS 727A, STR 26R. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

STRINGER CLIP CRACKED AT BS 787, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (BS 905 S27R) · airframe 75,319 hrs · 61,486 cycles

STRINGER CRACKED AT BS 905, S27R. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

STRINGER CRACKED BS 530 STR 26R. REPAIRED STRINIGER IAW SRM.

Part: STRINGER — CORRODED (BS 532 S26L) · airframe 75,319 hrs · 61,486 cycles

STRINGER CORRODED AT BS 532, . REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

BS 747, STR 26R STRINGER CLIP CRACKED. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,319 hrs · 61,483 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,319 hrs · 61,483 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 24L. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

BS 727E, STR 26R STRINGER CLIP CRACKED. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

BS 747, STR 25R STRINGER CLIP CRACKED. REMOVED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

BS 767, STR 25R STRINGER CLIP CRACKED. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

BS 807, STR 26L STRINGER CLIP CRACKED. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

BS 747, STR 26L STRINGER CLIP CRACKED. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

BS 727E, STR 25R STRINGER CLIP CRACKED. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (BS 727E S26L) · airframe 75,319 hrs · 61,486 cycles

STRINGER CLIP CRACKED AT BS 727E, STR 26L. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

BS 727D, STR 26L STRINGER CLIP CRACKED. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,319 hrs · 61,483 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 767, RBL 8. REPAIRED SUPPORT IAW EA.

Part: STRINGER CLIP — CRACKED (BS 787 S26R) · airframe 75,319 hrs · 61,486 cycles

STRINGER CLIP CRACKED AT BS 787, STR 26R. REMOVED AND REPLACED STRINGER CLIP IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO COMPARTMENT FRAME SUPPORT ANGLE CRACKED AT BS 500D, STR 21R. REMOVED AND REPLACED ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKD AT BS 500B, STR 21L. REPAIRED CLIP IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

AFT CARGO BAY, VERTICAL STIFFENER CRACKED I/B SIDE OF RT KEEL BEAM AFT SIDE OF BS 727 BULKHEAD. REMOVED STIFFENERS IAW DWG AND SRM.

Part: SHEAR TIE — CORRODED (BS 767 S26-27L) · airframe 75,319 hrs · 61,486 cycles

SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26L TO 27L. REMOVED AND REPLACED SHEAR TIE IAW SRM, DWG AND MPM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

AFT CARGO BAY, VERTICAL STIFFENER CRACKED I/B SIDE OF LT KEEL BEAM AFT SIDE OF BS 727 BULKHEAD. REMOVED AND REPLACED STIFFENERS IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM SHEAR WEB CORRODED BETWEEN BS 727C TO BS 727D, LBL 70. REPAIRED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM SHEAR WEB CORRODED BETWEEN BS 727D TO BS 727E, LBL 70. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

SKIN CRACKED AT BS 473, STR 16R. REPAIRED SKIN PER ER AND EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM SHEAR WEB CORRODED BETWEEN BS 727E TO BS 747, LBL 70. REPAIRED WEB PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

BS 304 STR 16L INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL PER SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

SHEAR TIE BS 520 BETWEEN STR 28L-27L IS CORRODED. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

CREASE BEAM CHORD CORRODED AT BS 390, WL 208 RT. REPAIRED CHORD PER ER AND EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

FRAME SHEAR TIE CRACKED AT STR 16L BS 400. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

CORROSION ON CREASE BEAM SHEAR WEB BS 727B-727C, LBL 70. REMOVED WEB PER SRM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

CORROSION ON CREASE BEAM SHEAR WEB, BS 380-400, RBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

CORROSION ON CREASE BEAM SHEAR WEB, BS 480-500, LBL 70, WL 208. REMOVED AND REPLACED WEB PER SRM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

CORROSION ON CREASE BEAM SHEAR WEB, BLS 500A-500B, LBL 70. REMOVED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

R1 DOOR CUTOUT FWD LOWER CORNER SKIN IS CRACKED. REPAIRED SKIN PER ER AND EA.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

CORROSION ON CREASE BEAM SHEAR WEB, BLS 420-440, RBL 70. REMOVED WEB PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

CORROSION ON STRINGER STR 25L BS 967-987. REPAIRED STRINGER PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

FLOOR SUPPORT CORRODED AT BS 767, LBL 2.5. REMOVED AND REPLACED SUPPORT PER SRM.

Part: FRAME — CRACKED (BS 438 S24R) · airframe 75,319 hrs · 61,486 cycles

FWD CARGO COMPARTMENT FRAME WEB CRACKED AT BS 438, STR 24R. REMOVED AND REPLACED WEB INTERCOSTAL PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

CORROSION ON STRINGER TO BULKHEAD TIE CHANNEL AT BS 532 STR 26R. REMOVED & REPLACED CHANNEL IAW SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 75,319 hrs · 61,486 cycles

CORROSION ON LEFT KEEL BEAM, BS 500D+15" TO BS 520, STR 28L. REMOVED AND REPLACED BEAM PER SRM.

Part: SKIN — CRACKED (BS 500D S16R) · airframe 75,319 hrs · 61,486 cycles

SKIN CRACKED AT BS 500D+13, STR 16R. REPAIRED SKIN PER ER AND EA.

Part: LENS — LOOSE (EXIT SIGN) · airframe 74,157 hrs · 60,567 cycles

L1 DOOR EMERGENCY EXIT SIGN LOOSE. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,622 hrs · 60,145 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 747+3 TO BS 747+14, STR 18L. REPAIRED SKIN PER EA.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 73,622 hrs · 60,145 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE MISROUTED. REROUTED CABLE IAW MM.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 73,622 hrs · 60,145 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE MISROUTED. RE-ROUTED CABLE IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,122 hrs · 59,745 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 909, STR 4L. REPAIRED SKIN PER ER AND EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 73,122 hrs · 59,745 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,118 hrs · 59,744 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 907+2, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,998 hrs · 59,648 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 822 TO BS 825, STR 17L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,998 hrs · 59,648 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME WEB CRACKED AT BS 500D, RBL 7. REPAIRED FRAME PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,998 hrs · 59,648 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 767-787, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,998 hrs · 59,648 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 803, STR 18L. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,998 hrs · 59,648 cycles

DURING SCHEDULED OTS CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 28L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,998 hrs · 59,648 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 504D, STR 16R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,998 hrs · 59,648 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 500, RBL 6.50. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,998 hrs · 59,648 cycles

DURING SCHEDULED OTS CHECK, FOUND RT EEPLS INOP BETWEEN ROW 1 TO ROW 8. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,998 hrs · 59,648 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED BETWEEN BS 822 TO BS 825, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,320 hrs · 59,155 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 928+12, STR 24R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 72,320 hrs · 59,155 cycles

L1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 72,293 hrs · 59,138 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178.5, RBL 5.7. REPAIRED WEB PER ER AND EA.

Part: ANGLE — CRACKED (RT MLG WW) · airframe 72,293 hrs · 59,138 cycles

DURING SCHEDULED SPV CHECK, FOUND RT MAIN WHEEL WELL VERTICAL "L" ANGLE CRACKED AT BS 663, RBL 6.1. REMOVED AND REPLACED ANGLE PER SRM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 71,819 hrs · 58,767 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,279 hrs · 58,344 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 404 TO BS 406.5, STR 26L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,279 hrs · 58,344 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 412.5 TO BS 417, STR 26L. REPAIRED SKIN PER EA.

Part: WEB — CRACKED (NLG WW) · airframe 70,739 hrs · 57,925 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND NLG WHEEL WELL LT SIDE PANEL WEB CRACKED AT BS 243.7. REPAIRED WEB PER EA AND BAC DWG.

Part: GASPER FAN — FAULTY (A/C BAY) · airframe 70,714 hrs · 57,904 cycles

FUMES REPORTED AT ROWS 15 TO 17. TURNED OFF RIGHT A/C PACK AND RECIRC FANS. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 907 AT STR 14R. REPAIRED SKIN PER EO AEM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CRACKED AT BS 666, RBL 24.5. REPAIRED BEAM PER AEM.

Part: BRACKET — CORRODED (EVAC SLIDE) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FLOOR BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS PER MMK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR FWD FRAME CRACKED AT BS 329. REMOVED AND REPLACED R1 DOOR FRAME PER SRM & BAC DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 277 RT SIDE. REPAIRED FRAME PER EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, BETWEEN STR 19R & 20R. REPAIRED FRAME PER SRM & EO.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED AT UPPER SURFACE. REPAIRED SLAT PER SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND UPPER CHORD CORRODED AT BS 227.8, LBL 7 TO RBL 23. REPAIRED UPPER CHORD PER EO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD GALLEY EMERGENCY EXIT BULB INOP. REMOVED AND REPLACED BULB PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING I/B FORE FLAP LOWER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD EMERGENCY EXIT LIGHT BULB INOP. REMOVED AND REPLACED BULB PER MM.

Part: LENS — MISSING (CABIN) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING I/B FORE FLAP LOWER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 6 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING FORE FLAP UPPER SURFACE DELAMINATED BETWEEN WBL 153 TO WBL 156. REPAIRED FORE FLAP PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT EMERGENCY EXIT LIGHT BULB INOP. REMOVED AND REPLACED BULB PER MM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND SUPPORT Z CORRODED ON LOWER SILL AT LBL 66.5 L1 DOOR. REMOVED AND REPLACED SUPPORT Z PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING I/B NR 6 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 296, STR 17R. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CORRODED AT BS 312, BBL 0. REMOVED AND REPLACED STRINGER PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING I/B FORE FLAP SKIN DELAMINATED BETWEEN WBL 132 TO WBL 136. REPAIRED FORE FLAP PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING T/E INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME LOCATED AT BS 1016 FWD FACE AFT PRESSURE BULKHEAD CRACKED. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 14L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,327 hrs · 57,624 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,291 hrs · 57,601 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 70,240 hrs · 57,562 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SKIN PANEL — CRACKED (NLG WW) · airframe 69,470 hrs · 56,985 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND NLG W/W RT SIDE PANEL 3103R CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,064 hrs · 56,682 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 924, BETWEEN STR 23R TO STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,064 hrs · 56,682 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,064 hrs · 56,682 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,064 hrs · 56,682 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 464, STR 26L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,064 hrs · 56,682 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,064 hrs · 56,682 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 410, STR 26L. REPAIRED SKIN PER ER.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,064 hrs · 56,682 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR UPPER HINGE CUTOUT INNER WEB ANGLE CRACKED AT BS 293, STR 11R. REMOVED AND REPLACED ANGLE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,064 hrs · 56,682 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 908, STR 23R. REPAIRED SKIN PER SRM.

Part: AXLE — BROKEN (RT MLG) · airframe 69,060 hrs · 56,680 cycles

DURING LANDING, NR 3 MLG WHEEL AXLE BROKE. REMOVED AND REPLACED RT MLG INNER CYLINDER ASSY PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 680,665 hrs · 55,912 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING I/B FOREFLAP UPPER SURFACE DELAMINATED. R&R FOREFLAP PER MM.

Part: LENS — LOOSE (CABIN) · airframe 67,986 hrs · 55,851 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 67,986 hrs · 55,851 cycles

LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED PER SWA EA.

Part: LENS — MISSING (CABIN) · airframe 67,863 hrs · 55,769 cycles

LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. REPLACED LENS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 67,422 hrs · 55,451 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. ADJUSTED SLIDE PER MT.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 66,630 hrs · 54,889 cycles

FOUND FWD I/B EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 66,639 hrs · 54,894 cycles

FOUND FWD I/B EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,301 hrs · 54,648 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,236 hrs · 54,601 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, STR 26L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,236 hrs · 54,601 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 793, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,236 hrs · 54,601 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,236 hrs · 54,601 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 784, STR 18L. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 65,695 hrs · 54,186 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: PUSHROD — CORRODED (LT ELEVATOR TAB) · airframe 64,529 hrs · 53,302 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT ELEVATOR TAB PUSH RODS CORRODED AT FWD END. REMOVED AND REPLACED PUSH RODS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 64,529 hrs · 53,302 cycles

DURING SCHEDULED BRDG CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 16 DEF. SECURED LENS PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR CUTOUT FWD FRAME CRACKED AT BS 951, BETWEEN STR 10R AND STR 11R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 9R. REPAIRED FRAME PER SWA EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 27L CRACKED AT BS 390. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 2R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

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

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 663, STR 3L. REPAIRED BELTFRAME PER SRM.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 663, STR 1. REPAIRED BELTFRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 663, STR 2L. REPAIRED BELTFRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 344, STR 9R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 9R. REPAIRED FRAME PER SWA EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CRACKED AT BS 663, STR 3L. REPAIRED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 9R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 9L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BETWEEN BS 433 AND BS 448, LBL 3 AND RBL 2. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 335, STR 17L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 512A, RBL 14. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 312, LBL 1. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 344, LBL 1 TO LBL 9. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 29 TO RBL 42. REPAIRED FLOORBEAM PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STA 66 AND STA 94. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME INNER CHORD CRACKED AT RT BS 616. REPAIRED FRAME CHORD PER SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND VERTICAL BEAM CRACKED AT BS 178, RBL 17, WL 182. REPAIRED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 500, RBL 4. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 360, RBL 1. REPAIRED FLOORBEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 400 AND BS 440, RBL 70. REMOVED AND REPLACED WEB PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,516 hrs · 53,292 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 64,503 hrs · 53,277 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 1 DEF. SECURED STRIP PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 64,161 hrs · 53,018 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 827, STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,156 hrs · 53,015 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 986, STR 18L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 64,156 hrs · 53,015 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 887, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 64,156 hrs · 53,015 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 747, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 64,020 hrs · 52,914 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP CRACKED AT ROW 1 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,995 hrs · 52,897 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 63,039 hrs · 52,127 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: HINGE FITTING — WORN (LT ELEVATOR TAB) · airframe 63,039 hrs · 52,127 cycles

DURING SCHEDULED C1 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE FITTING PER SWA EA.

Part: CHANNEL — CRACKED (AFT CARGO DOOR) · airframe 62,978 hrs · 52,071 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR FRAME UPPER U-CHANNEL CRACKED. REMOVED AND REPLACED U-CHANNEL PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,978 hrs · 52,071 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,235 hrs · 51,487 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 374, STR 26L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,235 hrs · 51,487 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504D, STR 14L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,791 hrs · 51,156 cycles

DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 793, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,423 hrs · 50,873 cycles

DURING SCHEDULED MV1 CHECK, FOUND LEFT WING INBOARD MID FLAP OUTBOARD T/E DELAMINATED. REMOVED AND REPLACED MID FLAP PER MM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 60,239 hrs · 49,970 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,239 hrs · 49,970 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 59,480 hrs · 49,375 cycles

EMERGENCY EXIT LIGHT ASSY BROKEN AT FWD ENTRY DOOR. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 58,679 hrs · 48,724 cycles

EMERGENCY EXIT LIGHT ASSY LOOSE AT LT ROW 6. SECURED LIGHT ASSY PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 58,649 hrs · 48,698 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT INBOARD CORNER. R&R FWD FRAME SECTION PER SRM.

Part: WEB — CRACKED (BS 348 S16L) · airframe 58,649 hrs · 48,698 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE WEB CRACKED AT BS 348, STR 16L. REPAIRED WEB ASSY PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,649 hrs · 48,698 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 348, STR 15L. REPAIRED FRAME PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 58,649 hrs · 48,698 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, AFT FRAME NR 5 STOP FITTING. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (BS 360) · airframe 58,649 hrs · 48,698 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,649 hrs · 48,698 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 474, STR 7R. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 58,649 hrs · 48,698 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, BETWEEN STR 13L & STR 15L. R&R SHEAR TIE PER SRM.

Part: SKIN — CRACKED (BS 947) · airframe 58,435 hrs · 48,528 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 58,435 hrs · 48,528 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 5 L/E SLAT DELAMINATED. REPAIRED SLAT PER SRM.

Part: FLOOR SUPPORT — CRACKED (CABIN FLOOR) · airframe 56,853 hrs · 47,300 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CRACKED BETWEEN BS 660.5 TO BS 664, RBL 0.5, BL 0. REPAIRED FLOORBEAM PER SWA EA.

Part: SKIN — CRACKED (R2 DOOR AREA) · airframe 56,853 hrs · 47,300 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (BS 664) · airframe 56,853 hrs · 47,300 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 664, LBL 24.75. REPAIRED FLOORBEAM PER SWA EA.

Part: BULKHEAD — CRACKED (BS 1016) · airframe 56,853 hrs · 47,300 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT DOME CAP, 5 O'CLOCK POSITION. REPAIRED WEB PER SWA EA.

Part: FLOOR SUPPORT — CRACKED (BS 664-668) · airframe 56,853 hrs · 47,300 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CRACKED BETWEEN BS 664 TO BS 668, RBL 24.75. REPAIRED FLOORBEAM PER SWA EA.

Part: FRAME — CRACKED (BS 303) · airframe 56,853 hrs · 47,300 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, L1 DOOR FWD LOWER STOP FITTING. REMOVED AND REPLACED STOP FITTING PER SRM.

Part: GUSSET — CRACKED (R1 DOOR) · airframe 56,853 hrs · 47,300 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT LOWER GUSSET CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: ANGLE — CRACKED (BS 1016) · airframe 56,853 hrs · 47,300 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 AFT PRESSURE BLKHD Z-ANGLE CRACKED AT 6:30 O'CLOCK POSITION. REMOVED AND REPLACED Z-ANGLE PER SRM.

Part: WINDOW — LOOSE (COCKPIT) · airframe 56,560 hrs · 47,062 cycles

DIVERSION, LOUD SQUEAL IN COCKPIT COMING FROM R1 WINDOW. RETORQUED COCKPIT R1 WINDOW PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 56,473 hrs · 46,976 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,473 hrs · 46,976 cycles

DURING SCHEDULED C2 CHECK, AFT CABIN EMERGENCY EXIT LIGHTS BATTERY FAILED TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 56,473 hrs · 46,976 cycles

DURING SCHEDULED C2 CHECK, FOUND BULLNOSE LIGHT LENS LOOSE AT ROW 21 ABC. SECURED LENS PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 55,955 hrs · 46,565 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 55,696 hrs · 46,374 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,559 hrs · 46,264 cycles

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

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 55,456 hrs · 46,183 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING OUTBOARD T/E FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,456 hrs · 46,183 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 55,456 hrs · 46,183 cycles

DURING SCHEDULED C1 CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED AT INBOARD BALANCE BAY. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 54,454 hrs · 45,387 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 54,454 hrs · 45,387 cycles

DURING SCHEDULED C4 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 11 ABC, BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 53,472 hrs · 44,614 cycles

DURING SCHEDULED C3 CHECK, FOUND ZEE ANGLE AT BS 664, RBL 31.83, CRACKED. REPAIRED ZEE ANGLE PER EA.

Part: LAMP — INOPERATIVE (ROW 21ABC) · airframe 53,464 hrs · 44,609 cycles

DURING SCHEDULED C3 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT AT ROW 21 ABC, INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 53,444 hrs · 44,591 cycles

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

Part: SLIDE — OUT OF LIMITS (R2 DOOR) · airframe 53,097 hrs · 44,320 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EVAC SLIDE PRESSURE IND OUT OF LIMITS. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — DEPLOYED (L1 DOOR) · airframe 52,850 hrs · 44,122 cycles

L1 DOOR EVAC SLIDE DEPLOYED. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM.

Part: FITTING — CORRODED (LT/RT MLG) · airframe 50,867 hrs · 42,505 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH LT AND RT MLG FWD WALKING BEAM HANGER FITTINGS CORRODED. REPAIRED FITTINGS PER SWA EA.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 50,715 hrs · 42,388 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM.

Part: SKIN — DELAMINATED (RT WING SPOILER) · airframe 49,858 hrs · 41,724 cycles

DURING SCHEDULED C3 CHECK, FOUND NR 3 FLIGHT SPOILER DELAMINATED. REMOVED AND REPLACED NR 3 FLIGHT SPOILER PER MM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 49,123 hrs · 41,122 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT AFT END OF HANDLE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,123 hrs · 41,122 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIPS CRACKED AT STR 10R, BS 597 & BS 578. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,123 hrs · 41,122 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B BELOW STR 20L. REPAIRED FUSELAGE FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,123 hrs · 41,122 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, BELOW STR 17L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (AFT FUSELAGE) · airframe 48,964 hrs · 40,996 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STRINGER 24L. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (AFT FUSELAGE) · airframe 48,964 hrs · 40,996 cycles

DURING SCHEDULED C2 CHECK, FOUND BS 1016 BULKHEAD CRACKED BETWEEN 12 & 2 O'CLOCK POSITIONS. REPAIRED BULKHEAD PER SWA EA.

Part: SLIDE — DISLODGED (FWD ENTRY DOOR) · airframe 48,944 hrs · 40,978 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER WHEN OPENING DOOR. REINSTALLED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,065 hrs · 40,314 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 20L, BS 970 AND BS 980. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (AFT SVC DOOR) · airframe 48,038 hrs · 40,291 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR OUTER SKIN CRACKED (2 EA) AT LOWER FWD CORNER ABOVE LOWER GATE. REMOVED AND REPLACED AFT SVC DOOR PER MM.

Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 48,038 hrs · 40,291 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 46,810 hrs · 39,287 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — DEPLOYED (FWD ENTRY DOOR) · airframe 46,800 hrs · 39,279 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — UNSERVICEABLE (AFT ENTRY DOOR) · airframe 46,407 hrs · 38,945 cycles

DURING SCHEDULED A2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: TAB — WORN (RT ELEVATOR) · airframe 45,667 hrs · 38,304 cycles

DURING SCHEDULED A2 CHECK, SWA SI 11111-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 43,605 hrs · 36,626 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 42,605 hrs · 35,822 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM.

Part: BEARING — GROOVED (RT MLG) · airframe 42,507 hrs · 35,735 cycles

DURING SCHEDULED SERVICE CHECK, FOUND GROOVED RT MLG TRUNNION BEARING. REMOVED AND REPLACED RT MLG TRUNNION BEARING PER MM.

Part: BEAM — WORN (RT MLG) · airframe 42,507 hrs · 35,735 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT MLG ACTUATOR CLEVIS BEAM ARM BUSHING WORN AND CORRODED. REMOVED AND REPLACED CLEVIS BEAM ARM PER MM.

Part: TRANSMITTER — MALFUNCTIONED (LT/RT FLAPS) · airframe 42,024 hrs · 35,313 cycles

DECLARED EMERGENCY, L/E & T/E FLAPS WOULD NOT EXTEND USING NORMAL METHOD. EXTENDED NORMALLY USING ALT FLAP SYSTEM. REMOVED AND REPLACED LT AND RT FLAP POS TRANSMITTERS PER MM. OPS CHECK NORMAL.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 41,995 hrs · 35,288 cycles

DECLARED EMERGENCY, L/E AND T/E DEVICES WOULD NOT EXTEND. A AND B HYD SYSTEM NORMAL. EXTENDED FLAPS USING ALT FLAP SYSTEM. CLEANED FLAP POS IND AND OPERATED FLAPS PER MM AT HOU. REMOVED AND REPLACED FLAP POS INDICATOR FOR MX CONVENIENCE PER MM.

Part: SLIDE — UNSERVICEABLE (R2 DOOR) · airframe 40,906 hrs · 34,382 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT SERVICE DOOR EVAC SLIDE PRESSURE INDICATOR LOW. R&R SLIDE ASY PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 40,906 hrs · 34,382 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CENTER SECTION BS 665 BEADED WEB CRACKED, LBL 32.5. REPAIRED WEB PER TI-353-046.

Part: LIGHT — LOOSE (CABIN) · airframe 40,906 hrs · 34,382 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EEPLS LOOSE AT ROW 16. SECURED EEPLS PER MM.

Part: LIGHT — LOOSE (ROW 8) · airframe 39,837 hrs · 33,456 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK LOOSE AT ROW 8. SECURED TRACK PER MM.

Part: TURBINE — FAILED (NR 2 ENGINE) · airframe 39,261 hrs · 32,980 cycles

AIR TURNBACK, AFTER TAKEOFF NR 2 ENG BEGAN A LOUD NOISE AND SURGE. REDUCED THRUST AT 60 PERCENT N1 AND ENG STABILIZED. SUSPECTED TURBINE FAILURE. REMOVED AND REPLACED NR 2 ENG PER MM.

Part: ENGINE — SURGES (NR 2) · airframe 39,261 hrs · 32,980 cycles

AIR TURNBACK, AFTER TAKEOFF NR 2 ENG BEGAN A LOUD NOISE AND SURGE. REDUCED THRUST AT 60 PERCENT N1 AND ENG STABILIZED. SUSPECTED TURBINE FAILURE. REMOVED AND REPLACED NR 2 ENG PER MM.

Part: SKIN — DELAMINATED (TE FLAP)

DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: COVER — LOOSE (CABIN)

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER LOOSE AT ROW 8. RESECURED TRACK COVER PER MM.

Part: INNER CYLINDER — GOUGED (NR 1 MLG)

DURING RON, FOUND NR 1 MLG AXLE SLEEVE ROTATED 90 DEGREES AND HAS SMALL GOUGES WITH PAINT DISCOLORATION ON AXLE. REMOVED AND REPLACED NR 1 MLG INNER CYLINDER ASSY PER MM. (THIS IS A CONTINUATION OF SDR FORM NR SWAA99-1459, SUBMITTED SEPT 3, 1999).

Part: BEARING — FAILED (LT MLG)

ON DEPARTURE OUT OF BUR, TOWER NOTIFIED ACFT LOST OF NR 1 WHEEL ASSY AND ACFT DIVERTED TO ONT. FOUND NR 1 AXLE NUT STILL ATTACHED AND TIGHT, THE INNER BEARING STILL ON THE AXLE AND UNDAMAGED. THE OUTER BEARING INNER RACE ON AXLE SEVERELY SCARRED, MUTILATED AND FROZEN IN PLACE. AFTER CLEAN UP OF AREA, FOUND AXLE SLEEVE ROTATED 90 DEGREES BUT STILL FIRMLY IN PLACE. INSPECTION OF INNER AXLE PER MM PROCEDURE FOR WHEEL BEARING FAILURE REVEALED PAINT DISCOLORATION. REMOVED AND REPLACED BOTH NR 1 AND NR 2 TIRE/WHEEL ASSY'S, NR 1 BRAKE ASSY AND MX FERRY ACFT TO PHX FOR AXLE REPAIR.

Part: TAB — CRACKED (LT ELEVATOR)

DURING SCHEDULED BC4 CHECK, FOUND LT ELEVATOR TAB CRACKED. REMOVED AND REPLACED LT ELEVATOR TAB ASSY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FWD SECTION OF EMERGENCY ESCAPE FLOOR TRACK LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: RETRACT MECH — OUT OF ADJUST (NR 4 LE FLAP)

NR 4 LEADING EDGE SLAT SHOWED UNSAFE INFLIGHT. COULD SEE NR 4 SLAT DROOPING ABOUT ONE INCH. AIRCRAFT MADE AN UNEVENTFUL LANDING. INSPECTED AND PERFORMED OPERATIONAL CHECK ON FLAP AND LEADING EDGE DEVICES SYSTEM PER BOEING MM. OPS CH OK.

Part: FLAP INDICATION — SPLIT (TE FLAPS)

AFTER TAKEOFF, RETRACTING THE FLAPS FROM POSITION 5 TO 1, FLAPS SPLIT. THE RIGHT FLAP STOPPED AT 2 AND THE LEFT FLAP STOPPED AT 1. A/C TURNBACK, MADE AN UNEVENTFUL LANDING. PERFORMED ASSEMITY CHECK. UNLOCKED FLAP INDICATE. OPS CHECKS NORMAL, FLAP CYCLED STANDBY AND NORMAL. SYSTEM OPERATED NORMAL PER BOEING MM.

Part: FRAME — CORRODED (BS 847)

DURING SCHEDULED D-CHECK, FOUND CORRODED FRAME AT BS 847, RBL 19, WL 165. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (TAIL)

DURING SCHEDULED D-CHECK, FOUND CRACKED WEB ON I/B SIDE OF HOLES STAB APPROX 12 AFT OF REAR SPAR ATTACH FITTINGS. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (E/E DOORWAY)

DURING SCHEDULED D-CHECK, FOUND CRACKED SKIN .2 LONG AT E AND E BAY DOOR FWD RIGHT CORNER. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727-947)

DURING SCHEDULED D-CHECK, FOUND CORRODED CARGO FLOORBEAM AT BS 727 TO 947, RBL 3, WL 159. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727-947)

DURING SCHEDULED D-CHECK, FOUND CORRODED CARGO FLOORBEAM AT BS 727 TO 947, LBL 12.5, WL 159 LBL 8, WL 159 AND LBL 3 WL 159. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 794-847)

DURING SCHEDULED D-CHECK, FOUND CORRODED VERTICAL SUPPORT WEB AT BS 794 TO 847, RBL 19, WL 164. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 400-420)

DURING SCHEDULED D-CHECK, FOUND CRACKED INTERCOSTAL AT BS 400 TO 420, LBL 25 WL 156. REPAIRED PER BOEING SRM.

Part: BULKHEAD — DENTED (BS 727)

DURING SCHEDULED D-CHECK, FOUND DENTED BULKHEAD PANEL SUPPORT ANGLE AT BS 727+3 RBL 53 WL 191. REPAIRED PER BOEING SRM.

Part: FRAME — DENTED (BS 767)

DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 767, RBL 29, WL 158. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 270)

DURING SCHEDULED D-CHECK, FOUND CRACKED L-ANGLE STIFFENER AT BS 270 LBL 47, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — GOUGED (BS 1010)

DURING SCHEDULED D-CHECK, FOUND GOUGED SKIN AT BS 1010 2 BELOW STRINGER 5 LT. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727-947)

DURING SCHEDULED D-CHECK, FOUND CORRODED CARGO FLOORBEAM AT BS 727 TO 947, RBL 8, WL 159. REMOVED AND REPLACED PER BOEING SRM.

Part: BEAM — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACKED CREASE BEAM AT BS 178, RBL 29, WL 207. REPAIRED PER BOEING SRM.

Part: WEB — CORRODED (BS 787-847)

DURING SCHEDULED D-CHECK, FOUND CORRODED VERTICAL SUPPORT WEB TIE STRAP AT BS 787 TO 847, RBL 19, WL 157 TO 162. REMOVED AND REPLACED PER BOEING SRM.

Part: STRAP — CORRODED (BS 840-852)

DURING SCHEDULED D-CHECK, FOUND CORRODED LOWER VERTICAL TIE STRAP AT BS 840 TO 852, RBL 19, WL 161. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 328)

DURING SCHEDULED D-CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 328, RBL 66, WL 210. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 339)

DURING SCHEDULED D-CHECK, FOUND CORRODED THRESHOLD Z-ANGLE SUPPORT AT BS 339 TO 317, LBL 63.5 TO LBL 60, WL 209. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 295)

DURING SCHEDULED D-CHECK, FOUND CRACKED LOWER STUB FRAME AT BS 295, WL 209, RBL 55. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 887)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET BETWEEN STRINGER 9RT AND 8RT AT BS 887. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 270)

DURING SCHEDULED D-CHECK, FOUND CORRODED Z-ANGLE CHORD AT BS 270, LBL 9, 6, 3, 5, BL 0, RBL 10, 6, 3, 5, WL 207. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 277)

DURING SCHEDULED D-CHECK, FOUND CRACKED INTERCOSTAL AT BS 277, WL 231, RBL 54. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 787-794)

DURING SCHEDULED D-CHECK, FOUND CORRODED INTERCOSTAL AT BS 787 TO 794, RBL 23, WL 158. REMOVED AND REPLACED PER BOEING SRM.

Part: COVER — DENTED (BS 492-496)

DURING SCHEDULED D-CHECK, FOUND DOOR FRAME COVER PLATE DENTED AND GOUGED AT BS 492 TO 496, RBL 25 TO 30, WL 156 TO 158. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 767-787)

DURING SCHEDULED D-CHECK, FOUND CORRODED VERTICAL SUPPORT WEB AT 767 TO 787, RBL 19, WL 156. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 268)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 268, LBL 10, WL 207. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 274)

DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 274, RBL 53, WL 247. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 380)

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 380 STR 1, AND STR 2 RT. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 1007)

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER AT BS 1007, STR 16 LT. REPAIRED PER BOEING SRM.

Part: DOUBLER — DAMAGED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND DAMAGED SKIN DOUBLER OF FUSELAGE. REPAIRED PER BOEING SRM.

Part: WEB — GOUGED (BS 1028)

DURING SCHEDULED D-CHECK, FOUND GOUGED WEB AT BS 1028, RBL 2, WL 208. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 348)

DURING SCHEDULED D-CHECK, FOUND CRACKED L-ANGLE AT DOOR STOP FITTING NR 9 AT BS 348, LBL 65, WL 223. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 301.9)

DURING SCHEDULED D-CHECK, FOUND CRACKED L-ANGLE AT BS 301.9 WL 257.5, LT 54. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CORRODED (BS 987-1016)

DURING SCHEDULED D-CHECK, FOUND CORRODED WEB AT BS 987 TO 1016, RBL 39 TO 46, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 295)

DURING SCHEDULED D-CHECK, FOUND CRACKED WEB INTERCOSTAL AT BS 295, WL 215, LBL 58 AND BS 295, WL 244, LBL 55. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 294)

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 294, WL 252, LBL 54. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 1146)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 1146, RBL 18. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 178, WL 207, RBL 25 TO 29 AND LBL 25 TO 29. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CORRODED (BS 947)

DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR TO BULKHEAD SUPPORT ANGLE AT BS 947, LBL 21, RBL 21 AND WL 180. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — WORN (BS 727)

DURING SCHEDULED D CHECK, FOUND WORN T-ANGLE AT BS 727 TO 727B, STR 20 LT AND BS 727, STR 20 RT. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DAMAGED (BS 500)

DURING SCHEDULED D CHECK, FOUND DAMAGED SKIN AT BS 500 + 19, RBL 1, WL 148. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 947)

DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT BS 947, STR 24 RT WL 160. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 500)

DURING SCHEDULED D CHECK, FOUND CRACKED INTERCOSTAL AT BS 500A-500B, RBL 25 WL 156. REPAIRED PER BOEING SRM.

Part: DORSAL FIN — DAMAGED (FUSELAGE)

DURING SCHEDULED D CHECK, FOUND DAMAGED DORSAL FIN OK TO CORE SPLICE. REPAIRED PER BOEING SRM.

Part: CHORD — CRACKED (BS 178)

DURING SCHEDULED CHECK, FOUND CRACKED SIDE CHORD AT BS 178, RBL 29 WL 207. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CHAFED (BS 890 -945)

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CHAFFED AT BS 890 TO BS 945, RBL 4.5-9.5, WL 306.5. REPAIRED PER TRAMCO EO NR 98-0409.

Part: COVER — CORRODED (BS 792-794)

DURING SCHEDULED D CHECK, FOUND CORRODED DOOR FRAME COVER PLATE AT BS 792-794, RBL 41-48, WL 164-170. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 907)

DURING SCHEDULED D CHECK, FOUND CRACKED STRINGER SPLICE AT BS 907, STR 4LT. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 294)

DURING SCHEDULED D CHECK, FOUND CORRODED FLOORBEAM AT BS 294, RBL 39, 45 TO 52, WL 208 AND WL 207. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — DRILLED (BS 1006)

DURING SCHEDULED D CHECK, FOUND HOLE DRILLED IN RADIUS OF FLOORBEAM AT BS 1006, WL 208, RBL 30. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 767)

DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 9LT AND 8LT, AT BS 847; BS 827, STRINGERS 9LT AND 8LT; AND BS 767, STRINGERS 9LT AND 8LT. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 867/787)

DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 9LT AND 8LT, AT BS 867; BS 787, STRINGERS 9RT AND 8RT. REPAIRED PER BOEING SRM.

Part: SEAL — COLLAPSED (EMER EXIT DOOR)

DURING SCHEDULED D CHECK, FOUND EMERGENCY EXIT DOOR HANDLE PRESSURE SEAL COLLAPSED LT. REMOVED AND INSTALLED NEW EMERGENCY EXIT DOOR HANDLE PRESSURE SEAL PER BOEING MM.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED D CHECK, FOUND CRACKED FLOORBEAM STIFFENER AT BS 328, RBL 32, WL 200. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 827/907/887)

DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 9RT AND 8RT, AT BS 827; BS 907, STRINGERS 9LT AND 8LT; AND BS 887, STRINGERS 9LT AND 8LT. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 500)

DURING SCHEDULED D CHECK, FOUND CRACKED SHEAR WEB UPPER ATTACH L ANGLE AT BS 500D-11, WL 208, BL 0. REPAIRED PER BOEING SRM.

Part: CHANNEL — CORRODED (BS 500)

DURING SCHEDULED D CHECK, FOUND CORRODED CHANNEL AT BS 500-500A, LBL 25, WL 156; BS 500B-500C, RBL 25, WL 156; AND BS 500C-500D, RBL 25, WL156. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 947)

DURING SCHEDULED D CHECK, FOUND CORRODED FLOORBEAM AROUND NUTPLATE HOLES AT BS 947, WL 208, RBL 5 TO LBL 43. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND CRACKED WEB AT BS 178, BL 0, WL 188-189. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (HORIZ STAB)

DURING SCHEDULED D CHECK, FOUND GOUGE AT RT HORIZ STAB LEADING EDGE PANEL LE BS 149.75. REMOVED AND REPLACED PER BOEING SRM.

Part: PANEL — GOUGED (HORIZ STAB)

DURING SCHEDULED D CHECK, FOUND GOUGE AT RT HORIZ STAB LEADING EDGE PANEL LE BS 100.56. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — DENTED (BS 460)

DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 460, LBL 35, WL 161. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 500)

DURING SCHEDULED D-CHECK, FOUND CRACKED INTERCOSTAL TO FRAME SUPPORT ANGLE AT BS 380, LBL 25, WL 254. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 663)

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 663, STR 10RT. REPAIRED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SERVICE CHECK, FOUND CRACKED BULKHEAD WEB AT BS 178, WL 198.25 TO 199.25, WL 200.25 - 201.25, RBL 4.7; BS 178, WL 208.5- 209, LBL 6.7 AND WL 211.375 -211.75, LBL 6.7; AND BS 178, WL 201.5-202, LBL 6.7. REPAIRED PER BOEING SRM.

Part: FRAME — DENTED (BS 727)

DURING SCHEDULED D CHECK, FOUND DENTED FRAME AT BS 727 E LBL 44, WL 166; AND\NBS 807, LBL 49, WL 173. REPAIRED PER BOEING SRM.

Part: BULKHEAD ANGLE — CORRODED (BS 500)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR TO BULKHEAD SUPPORT ANGLE AT BS 500D, RBL 23, LBL 23, WL 156. REMOVED AND REPLACED PER BOEING SRM.

Part: TIE STRAP — CORRODED (BS 859)

DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR PANEL TIE STRAP AT BS 859, RBL 18.5, LBL 21, WL 168. REMOVED AND REPLACED PER BOEING MM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND CRACKED BULKHEAD WEB AT BS 178, WL 199-200 AND WL 201.5-202.25, LBL 47; WL 198.50-199.25, RBL 6.7 AND WL 212-213, RBL 47. REPAIRED PER BOEING SRM.

Part: BULKHEAD ANGLE — CORRODED (BS 500)

DURING SCHEDULED D-CHECK, FOUND CORRODED SIDEWALL TO BULKHEAD SUPPORT ANGLE AT BS 500D, RBL 25, WL 158. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 500)

DURING SCHEDULED D CHECK, FOUND CORRODED INTERCOSTAL AROUND NUTPLATE LOC AT BS 500C-500D, LBL 25, WL 156; BS 500B PLUS 18, LBL 25, WL 156; AND BS 500A PLUS 2 LBL 25 WL 156. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CORRODED (BS 469)

DURING SCHEDULED D-CHECK, FOUND CORRODED SKIN AROUND NR 1 DME ANTENNA AT BS 469, BL0, WL 148. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 500)

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 500D, STR 19 RT. REMOVED AND REPLACED PER BOEING SRM.

Part: CLIP — CRACKED (BS 663)

DURING SCHEDULED D CHECK, FOUND CRACKED STRINGER CLIP AT BS 663, STR 10 LT. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 639)

DURING SCHEDULED D CHECK, FOUND CRACKED INTERCOSTAL AT BS 639, RBL 68.5 WL 221. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 569)

DURING CHEDULED D CHECK, FOUND CRACKED LT SKATE ANGLE AT BS 569, LBL 48 WL 173. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 569)

DURING SCHEDULED D-CHECK, FOUND CRACKED RT SKATE ANGLE AT BS 569, RBL 48 WL 173. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 387)

DURING SCHEDULED D CHECK, FOUND CRACKED SHEAR WEB UPPER ATTACH L-ANGLE AT BS 387 BL 0 WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 947)

DURING SCHEDULED D CHECK, FOUND CRACKED ANGLE STIFFENER AT BS 947 BELOW STR 14 RT. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CORRODED (BS 794)

DURING SCHEDULED D-CHECK, FOUND CORRODED FRAME AT BS 794, RBL 26, WL 158. REPAIRED PER BOEING SRM.

Part: FRAME — DENTED (BS 500)

DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 500, RBL 41, WL 164. REPAIRED PER BOEING SRM.

Part: LAMPS — FAILED (CABIN)

DURING SCHEDULED C1 CHECK, FOUND SEVERAL LAMPS INOP NEAR FWD ENTRY DOOR. RELAMPED PER BOEING M/M.

Part: LIGHT — BROKEN (CABIN)

DURING SCHEDULED 3C1 CHECK, FOUND EMERGENCY LIGHTING AT FWD F/A STATION BROKEN. REPLACED LIGHT ASSEMBLY PER BOEING M/M.

Part: INDICATOR — INACCURATE (NR 2 FUEL TANK)

DIVERTED TO ABQ DUE TO TOTAL FUEL QUANTITY FLUCTUATING, +/- 2,000 LBS. INSPECTED FOR LEAKS AND CHECKED FUEL QUANITITY, DEFERRED NR 2 FUEL TANK INDICATION AND CONTINUED PER MEL 28-6.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED RON CHECK, FOUND LEFT AFT DOOR EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: FLOOR BEAM — CRACKED (BS 315)

DURING SCHEDULED 1/4 D-CHECK, FOUND FLOOR BEAM STRAP CRACKED AT BS 315 LBL 12. REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 787-794)

DURING SCHEDULED 1/4 D-CHECK, FOUND WEB CRACKED AT AFT CARGO DOOR BS 787 TO 794, S 24 TO 25. REPLACED PER BOEING SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR AND GALLEY EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND RIGHT AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: TRANSIT LIGHT — MALFUNCTIONED (FLAP INDICATION)

AFTER FLAP RETRACTION, TRANSIT INDICATION LIGHT REMAINED ILLUMINATED ON FWD AND OVERHEAD PANELS. CYCLED FLAPS TWICE, NO HELP. AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING. CYCLED SLATS/FLAPS PER BOEING M/M, VERIFIED PROBLEM TO BE INDICATION, DEFERRED AND CONTINUED PER MEL 27-3.