N663SW

Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,205 hrs · 70,890 cycles

R2 DOOR LOWER EMER EXIT LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,205 hrs · 70,890 cycles

FUSELAGE SKIN CRACKED AT BS 757+2, STRINGER 2R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,205 hrs · 70,890 cycles

SKIN CRACKED AT BS 480+3, STRINGER 7R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,205 hrs · 70,890 cycles

FUSELAGE SKIN CRACKED AT BS 430+6, STRINGER 1L. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,205 hrs · 70,890 cycles

SKIN CRACKED AT BS 460+7, STRINGER 8L. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,205 hrs · 70,890 cycles

SKIN CRACKED AT BS 530+5, STRINGER 7R. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,205 hrs · 70,890 cycles

SKIN CRACKED AT BS 500A+2, STRINGER 8L. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,205 hrs · 70,890 cycles

SKIN CRACKED AT BS 766+3, STRINGER 2R. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,201 hrs · 70,889 cycles

SKIN CRACKED AT BS 500C+16, STRINGER 1L. REPAIR SKIN IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 89,536 hrs · 70,368 cycles

LEFT WING OTBD AFT FLAP LOWER SKIN DELAMINATED AT INBD AFT CORNER. REPAIRED AFT FLAP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,536 hrs · 70,368 cycles

FUSELAGE SKIN CRACKED AT BS 312, BETWEEN STRINGER 19R TO 20R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,536 hrs · 70,368 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 400+2" TO 400+4, STRINGER 1L. REPAIRED SKIN IAW EA.

Part: FAIRING — CRACKED (RT MLG WW) · airframe 89,142 hrs · 70,062 cycles

RIGHT MLG WW FILLET FAIRING CRACKED SPAR TO STATION 729.5. R & R FAIRING IAW DWG & SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 88,512 hrs · 69,592 cycles

R1 DOOR EGRESS LOWER LIGHT LOOSE. REPAIRED LIGHT IAW EA.

Part: SENSOR — FAULTY · airframe 88,495 hrs · 69,578 cycles

AIR TURN BACK, AFTER TAKEOFF GEAR HANDLE VERY DIFFICULT, WITH GEAR HANDLE IN UP, POWER ADVANCEMENT PAST MID THROTTLE CAUSE THE TAKEOFF WARNING HORN TO ACTIVATE. AFTER GEAR HANDLE IN OFF, RESULTS THE SAME, GEAR CAME DOWN NORMALLY. R & R SENSOR S106 IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 88,201 hrs · 69,366 cycles

L2 DOOR EMER LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 88,201 hrs · 69,366 cycles

R2 DOOR EMER LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,787 hrs · 69,089 cycles

FORWARD GALLEY EMER EXIT LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: SPAR — CORRODED (LT HORIZ STAB) · airframe 87,787 hrs · 69,089 cycles

LEFT HORIZONTAL STABILIZER REAR SPAR CORRODED AT LEVEL STAB STATION 239.90. REPAIRED SPAR IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

TIE CLIP CRACKED AT BS 520 STRINGER 15L. R & R TIE CLIP IAW DWG & SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

WEB CRACKED BETWEEN BS 500 TO 500A STRINGER 26L. R & R WEB IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

WEB CRACKED BETWEEN BS 460 TO 480 STRINGER 26L. R & R WEB IAW SRM & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

STRINGER CORRODED AT BS 767 + 10 STRINGER 25R. REPAIRED STRINGER IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

STRINGER CHANNEL CRACKED AT BS 727 STRINGER 23L. R & R CHANNEL IAW SRM & DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

SKIN CORRODED BETWEEN BS 792 TO 807, BETWEEN STRINGER 25R TO 26R. REPAIRED SKIN IAW EA.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

STRINGER SPLICE ANGLE CORRODED BETWEEN BS 807 TO 827 STRINGER 26R. R & R ANGLE IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

STRINGER SPLICE CORRODED AT BS 908 STRINGER 25R. R & R SPLICE IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

SEAT TRACK CRACKED AT BS 727B RBL 24.5. REPAIRED SEAT TRACK IAW EO & EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

STRINGER CHANNEL CRACKED AT BS 727 STRINGER 23R. R & R CHANNEL IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

FRAME CRACKED AT BS 500B BETWEEN STRINGER 15L TO 16L. REPAIRED FRAME IAW SRM.

Part: SUPPORT ANGLE — CRACKED (TE FLAP) · airframe 87,787 hrs · 69,089 cycles

LEFT WING NR 2 FLAP TRANSMISSION SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (TE FLAP) · airframe 87,787 hrs · 69,089 cycles

LEFT WING NR 1 FLAP TRANSMISSION SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (TE FLAP) · airframe 87,787 hrs · 69,089 cycles

RIGHT WING NR 7 TRANSMISSION FLAP ANGLE SUPPORT CRACKED. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 658.75 RBL 24.8. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

SKIN CRACKED AT BS 685 + 15 STRINGER 10L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

SKIN CRACKED AT BS 500D + 14.5 STRINGER 7R. REPAIRED SKIN IAW SRM.

Part: DOOR — BROKEN (TE FLAP TRACK) · airframe 87,787 hrs · 69,089 cycles

RIGHT WING NR 6 FLAP TRACK INBD DOOR HINGE BROKEN. R & R DOOR ASSEMBLY IAW CMM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 663.75 RBL 24.8. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

SKIN CRACKED AT BS 685 + 6.5 STRINGER 10L. REPAIRED SKIN IAW EA.

Part: ANGLE — CRACKED (LT HORIZ STAB) · airframe 87,787 hrs · 69,089 cycles

LEFT HORIZONTAL STABILIZER ANGLE LOCATED ON ACCESS PANEL 9126 CRACKED. R & R ANGLE IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 87,787 hrs · 69,089 cycles

RIGHT WING FIXED LE SKIN CRACKED AT LEVEL OF LES 72. REPAIRED SKIN IAW SRM.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 87,787 hrs · 69,089 cycles

LEFT WING NR 1 SPINDLE CARRIAGE ASSEMBLY CORRODED. R & R CARRIAGE ASSEMBLY IAW MT.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 87,787 hrs · 69,089 cycles

RIGHT WING NR 8 SPINDLE CARRIAGE ASSEMBLY CORRODED. R & R CARRIAGE ASSEMBLY IAW MT.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 87,787 hrs · 69,089 cycles

LEFT WING SUPPORT ANGLE CRACKED ON STABILIZING LINKS BETWEEN MLG BEAM & REAR SPAR. R & R ANGLE IAW SRM & DWG.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 87,787 hrs · 69,089 cycles

RIGHT WING NR 7 SPINDLE CARRIAGE ASSEMBLY CORRODED. R & R CARRIAGE ASSEMBLY IAW MT.

Part: ANGLE — CRACKED (LT WING) · airframe 87,787 hrs · 69,089 cycles

LEFT WING ANGLE CRACKED ON TRACK FAIRING NR 3 INBD SIDE UPPER STRUCTURE. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

TIE CLIP CRACKED BS 927 STRINGER 24R. R & R TIE CLIP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

SKIN CRACKED BETWEEN BS 727B + 12 INCHES TO BS 727D + 8 INCHES BETWEEN STRINGER 1 TO 3R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

SKIN CRACKED AT BS 727C+1.5 STRINGER 2R. REPAIRED SKIN IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

STRINGER SPLICE CRACKED AT BS 908 STRINGER 24R. R & R SPLICE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

SKIN CRACKED AT BS 907 STRINGER 6R. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (TE FLAP) · airframe 87,787 hrs · 69,089 cycles

LEFT WING NR 3 FLAP TRACK ANGLE CRACKED ON INBD SIDE. R & R ANGLE IAW SRM & DWG.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 87,787 hrs · 69,089 cycles

LEFT WING NR 2 SPINDLE CARRIAGE ASSEMBLY CORRODED. R & R CARRIAGE ASSEMBLY IAW MT.

Part: STRAP — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

STRAP CRACKED BETWEEN BS 312 TO 344 BL 0. R & R STRAP IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

FRAME CORRODED AT BS 827 BETWEEN STRINGER 27L TO 27R. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

SKIN CRACKED AT BS 908 BETWEEN STRINGER 6L TO 7L. REPAIRED SKIN IAW EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

Z STIFFENER CRACKED ON FWD FLANGE AT BS 1016 STRINGER 15L. REPAIRED Z STIFFENER IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

ANGLE CRACKED BETWEEN BS 927 TO 947.5 BL 0. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

FRAME CORRODED AT BS 807 BETWEEN STRINGER 25L TO 26L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

FRAME CORRODED AT BS 807 BETWEEN STRINGER 26L TO 27L. REPAIRED FRAME IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

WEB CRACKED BETWEEN BS 312 TO 328 RBL 31.6. R & R WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

FRAME CRACKED AT BS 348.2 STRINGER 16L. REPAIRED FRAME IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

FUSELAGE SKIN CRACKED AT STATION 524 STRINGER 8L. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

SKIN CRACKED AT BS 500B + 14.5 STRINGER 26R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

FUSELAGE SKIN CRACKED AT STATION 502D STRINGER 8L. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

SKIN CRACKED AT BS 380 + 5.5 STRINGER 26R. REPAIRED SKIN IAW SRM.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 87,787 hrs · 69,089 cycles

CROSSBEAM E WEB CRACKED AROUND FASTENER HEAD LOCATION AT 4.0 INCHES FROM AFT EDGE. REPAIRED CROSSBEAM E IAW EA.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 87,787 hrs · 69,089 cycles

AFT CARGO DOOR CROSSBEAM E WEB CRACKED AROUND FASTENER HEAD LOCATION AT 4.0 INCHES FROM FWD EDGE. REPAIRED CROSSBEAM E IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

SKIN CRACKED AT BS 500A + 14 STRINGER 16R. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

FRAME CRACKED AT BS 349.2 STRINGER 16L. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

SKIN CRACKED AT BS 460 + 13 STRINGER 16L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

SKIN CRACKED AT BS 500B+15 STRINGER 15L. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

SKIN CRACKED AT BS 500 + 13.750 STRINGER 15L. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

SKIN CRACKED AT BS 947.25+14 STRINGER 5R. REPAIRED SKIN IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 662.75 RBL 24.8. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 663.75 RBL 24.8. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

SKIN CRACKED AT BS 500D+15.5 STRINGER 16L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

SKIN CRACKED AT BS 440 + 12 STRINGER 26L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

SKIN CRACKED AT BS 460 + 14 STRINGER 15L. REPAIRED SKIN IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 727B RBL 24.8. REPAIRED CHORD IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

SKIN CRACKED AT BS 360+13 STRINGER 26L. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

SKIN CRACKED AT BS 344+1.5 STRINGER 2L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

SKIN CRACKED AT BS 344 STRINGER 2L. REPAIRED SKIN IAW SRM.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

PRESSURE DECK WEB CRACKED AT BS 664 LBL 34. REPAIRED WEB IAW EA & EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

FRAME OTBD CHORD AFT UPPER FASTENER HOLE CRACKED AT BS 727 STRINGER 18A LT SIDE AT 1 O'CLOCK & 8 O'CLOCK. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727 STRINGER 18A LT SIDE AT 2 O'CLOCK. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 18A LT SIDE AT 2 O'CLOCK. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727, STRINGER 18A RT SIDE AFT LOWER FASTENER HOLE AT 11 O'CLOCK. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

FRAME OTBD CHORD AFT LOWER FASTENER HOLE CRACKED AT BS 727 STRINGER 18A LT SIDE AT 8 O'CLOCK. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 87,787 hrs · 69,089 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727, STRINGER 18A RT SIDE FOUND ON THE FWD LOWER FASTENER HOLE AT 8 O'CLOCK. REPAIRED CHORD IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 87,645 hrs · 68,983 cycles

RIGHT CABIN EMER EXIT LIGHT LENS LOOSE AT ROW 8. REPAIRED LENS IAW AMM.

Part: FLAP — DELAMINATED (RT WING) · airframe 87,645 hrs · 68,983 cycles

RIGHT WING OTBD AFT TE FLAP DELAMINATED. REPAIRED AFT FLAP IAW AMM.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 87,645 hrs · 68,983 cycles

L2 DOOR EMER EXIT LIGHT DIM. REPAIRED LIGHT IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 87,530 hrs · 68,894 cycles

RIGHT OVERHEAD EMER EXIT LIGHT COVER LENS MISSING AT ROW 8. INSTALLED LENS IAW MM.

Part: COVER — MISSING (CABIN) · airframe 86,832 hrs · 68,394 cycles

FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER IAW AMM.

Part: SLIDING WINDOW — FAULTY (COCKPIT) · airframe 86,619 hrs · 68,245 cycles

FIRST OFFICER'S WINDOW HEAT CORD AFT OF WINDOW SMOKED. R & R NR 2 SLIDING WINDOW IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 86,490 hrs · 68,158 cycles

RIGHT BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 8. SECURED LENS IAW MM.

Part: SENSOR — FAULTY (CABIN PRESSURE) · airframe 83,317 hrs · 68,036 cycles

DIVERTED AND DECLARED EMERGENCY, CABIN ALTITUDE WARNING INDICATION. R & R 105 LG AIR SAFETY SENSOR IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 85,842 hrs · 67,717 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. R & R LENS IAW AMM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 85,842 hrs · 67,717 cycles

RT HORIZONTAL STABILIZER IN SPAR SKIN CRACKED 62 INCHES OTBD AT AFT SPAR RIVET ROW. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 85,842 hrs · 67,717 cycles

LT HORIZONTAL STABILIZER IN SPAR SKIN CRACKED 116 INCHES OTBD AT AFT SPAR RIVET ROW. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (RT MLG WW) · airframe 85,842 hrs · 67,717 cycles

RT MLG WW FWD GEAR CUT OUT INNER ANGLE CRACKED. REPAIRED ANGLE IAW EA.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 85,307 hrs · 67,338 cycles

INTERCOSTAL LOWER ATTACH CLIP CRACKED AT BS 348.2, STRINGER 15L. R & R CLIP IAW SRM & DRAWING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,307 hrs · 67,338 cycles

R2 DOOR LOWER EMERGENCY LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: COVER — BROKEN (CABIN) · airframe 85,258 hrs · 67,303 cycles

AFT ENTRY EMERGENCY EXIT LIGHT COVER BROKEN. R &R LIGHT ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,046 hrs · 67,128 cycles

R2 DOOR EMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 84,285 hrs · 66,511 cycles

LT MAIN WHEEL WELL LT FWD BULKHEAD CRACKED AT BS 663, LBL 44. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (ENTRY DOOR) · airframe 84,177 hrs · 66,432 cycles

AFT ENTRY DOOR SKIN AT UPPER HINGE CUTOUT CRACKED. REPAIRED CUTOUT IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,734 hrs · 66,121 cycles

FORWARD ENTRY DOOR EMERGENCY LIGHT INOP. RELAMPED BULB PER AMM.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 83,734 hrs · 66,121 cycles

BAFFLE CRACKED BETWEEN BS 400 TO BS 420, STR 26R. REMOVED AND REPLACED BAFFLE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,734 hrs · 66,121 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 583.25 - BS 584, STR 10R. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,734 hrs · 66,121 cycles

CHEM MILL SKIN CRACKED BETWEEN BS 500B+13.5- 500B+14, STR 18R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,734 hrs · 66,121 cycles

SKIN CRACKED BETWEEN BS 750 - BS 750.25, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,734 hrs · 66,121 cycles

SKIN CRACKED BETWEEN BS 384.5 - BS 386, STR 15R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,734 hrs · 66,121 cycles

FUSELAGE SKIN BETWEEN BS 910.75 - BS 911.25, STR 23R. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,734 hrs · 66,121 cycles

SKIN CRACKED BETWEEN BS 405.5 TO BS 405.875, STR 26R. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,734 hrs · 66,121 cycles

SKIN CRACKED BETWEEN BS 763 - BS 764, STR 20L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,734 hrs · 66,121 cycles

SKIN CRACKED BETWEEN BS 831.5 - BS 832.25, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,734 hrs · 66,121 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 500C+13.5 - 500C+16.25, STR 8R. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,734 hrs · 66,121 cycles

FUSELAGE SKIN CRACKED AT BS 356, AT LOWER AFT CORNER OF NR 1 RIGHT CABIN WINDOW CUTOUT. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,734 hrs · 66,121 cycles

FUSELAGE SKIN CRACKED AT BS 406, STR 15L. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,383 hrs · 65,890 cycles

FUSELAGE SKIN CRACKED JUST ABOVE STR 8R, 2.75 IN LONG AT STA 500C +4 INCHES. REPAIRED PER EA 1-353-21660.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 83,383 hrs · 65,890 cycles

R-2 DOOR SLIDE GIRT NEEDS RE-INSTALLED, TOO LONG. REPOSITIONED SLIDE PER MM AND MT 325-61-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,706 hrs · 65,392 cycles

R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER AMM.

Part: SKIN — CUT (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FUSELAGE SKIN CUT AT BS 887+2, BETWEEN STR 18L TO STR 19L. REPAIRED SKIN IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

STRINGER SPLICE CRACKED AT BS 360, STR 6R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

STRINGER SPLICE CRACKED AT BS 360, STR 5R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

WEB CRACKED BETWEEN BS 500D TO BS 520, STR 28L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

STRINGER CRACKED AT BS 380, STR 23R. REPAIRED STRINGER IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

WEB CRACKED BETWEEN BS 727A TO BS 727B, STR 25R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

CRACKED ANGLE AT BELLY FAIRING AREA LEFT SIDE BETWEEN BS 530 TO BS 550 AND STR 21L TO STR 22L. REMOVED AND REPLACED ANGLES IAW SRM AND DRAWING.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

STRINGER SPLICE CORRODED AT BS 360, STR 23R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FRAME CRACKED AT BS 520, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME IAW EO AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FRAME CRACKED AT BS 520, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME IAW EO AND EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

TIE CLIP CRACKED AT BS 380, STR 15L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

TIE CLIP CRACKED AT BS 400, STR 15L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

TIE CLIP CRACKED AT BS 440, STR 16L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

TIE CLIP CRACKED AT BS 500A, STR 16L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FRAME SHEAR TIE CRACKED AT BS 460, BETWEEN STR 14R TO STR 15R. REPAIRED FRAME IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

WEB CRACKED AT BS 1016+9, RBL 34. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

WEB CRACKED AT BS 1016+3, RBL 37. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

SKIN CRACKED AT BS 360+1.5, STR 6R. REPAIRED SKIN IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

F-25A CRACK ON SPLICE ANGLE LOCATED AT BS 540 BULKHEAD BETWEEN S-21L AND S-22L IN ORDER TO ACCOMPLISH AD/SSID 11810-53 (L=2.310" APPROX). REMOVED AND REPLACED ANGLE IAW EO AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 662, LBL 24.5. REPAIRED CHORD IAW EA AND EO.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

BULKHEAD WEB SPLICE CRACKED AT BS 1016, BL 0. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FRAME CRACKED AT BS 947.5, STR 19R. REMOVED AND REPLACED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FRAME CRACKED AT BS 947.5, STR 19L. REPAIRED FRAME IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

WEB CRACKED BETWEEN BS 500A TO BS 500B, STR 26L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FLOORBEAM CRACKED AT BS 967, RBL 50. REPAIRED BEAM IAW SRM.

Part: LENS — BROKEN (CABIN) · airframe 82,704 hrs · 65,391 cycles

EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS IAW AMM.

Part: WEB — CRACKED (NLG WW) · airframe 82,704 hrs · 65,391 cycles

RIGHT NLG WHEEL WELL WEB CRACKED AT BS 243.7+2.5, WL 169. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 82,704 hrs · 65,391 cycles

NLG WHEEL WELL WEB CRACKED AT BS 243.7+3.5, WL 169.1 LEFT SIDE. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 82,704 hrs · 65,391 cycles

NLG WHEEL WELL WEB CRACKED AT BS 243.7+3.5, WL 169.1 RIGHT SIDE. REPAIRED WEB IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

WEB CORRODED BETWEEN BS 947+12 TO BS 986.5, RBL 50. REMOVED AND REPLACED WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

WEB CRACKED AT BS 520+6, BETWEEN STR 22L AND STR 24L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

WEB CRACKED AT BS 520+6, BETWEEN STR 22R TO STR 24R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

TIE CLIP CRACKED AT BS 787, STR 16L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FUSELAGE SKIN CRACKED AT R1 DOOR FWD UPPER CORNER CUTOUT. REPAIRED SKIN IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

TIE CLIP CRACKED AT BS 747, STR 16L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

TIE CLIP CRACKED AT BS 727D, STR 16L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 82,704 hrs · 65,391 cycles

RIGHT WING SUPPORT ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

SPLICE CHANNEL CRACKED AT BS 360, STR 7L. REMOVED AND REPLACED CHANNEL IAW SRM AND DWG.

Part: FAIRING — CRACKED (RT PYLON) · airframe 82,704 hrs · 65,391 cycles

CRACK ON AFT STRUT FAIRING LOWER POSITION OUTBOARD SIDE ENGINE 2. REPAIRED AFT STRUT FAIRING LOWER POSITION AT OUTBOARD SIDE ENGINE 2 IAW EA 1-354-150 0 REV 0 AND EO AEM-HC54-053/12 RO

Part: FLAP — CORRODED (RT WING) · airframe 82,704 hrs · 65,391 cycles

RIGHT WING INBOARD MID FLAP BORE OF OUTBOARD CARRIAGE CORRODED. REPAIRED MID FLAP IAW AMM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

STRINGER SPLICE CORRODED AT BS 540, STR 26L. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

CRACK ON SUPPORT ANGLE LOCATED BS 380 BETWEEN STR 20L TO STR 21L OF THE AFT FACE PARTITION IN E/E COMPARTMENT. REPAIRED SUPPORT ANGLE IAW SRM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

KEEL BEAM WEB CRACKED AT BS 711. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

STRINGER SPLICE CORRODED AT BS 360+5, STR 20R. REMOVED AND REPLACED STRINGER SPLICE SECTION PER SRM & BAC DRAWING.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

RIGHT STRINGER CORRODED BETWEEN BS 1118 TO BS 1138 IN TORQUE BOX AREA. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.

Part: ACTUATOR — BROKEN (NR 4 SPOILER) · airframe 82,704 hrs · 65,391 cycles

LEFT WING NR 4 GROUND SPOILER O/B ACTUATOR BROKEN. REMOVED AND REPLACED NR 4 GROUND SPOILER O/B ACTUATOR IAW AMM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6R. REPAIRED WEB IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

TIE CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FRAME CRACKED AT BS 344, BETWEEN STR 23L TO STR 24L. REMOVED AND REPLACED FRAME PER SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

STRINGER CORRODED BETWEEN BS 344 TO BS 360, STR 25L. REPAIRED STRINGER IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

AFT PRESSURE BULKHEAD DOME WEB CRACKED AT BS 1016, STR 6R. REPAIRED WEB IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

SKIN CORRODED AT BS 360, BL 0. REPAIRED SKIN IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

VERTICAL ANGLE CRACKED AT BS 328, RBL 32. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 82,704 hrs · 65,391 cycles

LEFT WING NR 2 SLAT SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: STRIP — CRACKED (FLAP TRACK) · airframe 82,704 hrs · 65,391 cycles

CRACK ON STRIP LOCATED AT UPPER STRUCTURE OUTBOARD SIDE OF FLAP TRACK FAIRING NR 6 RT WING. REMOVED AND REPLACED STRIP IAW SRM AND DRAWING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 344, BL 0. REPAIRED CHORD IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

STRAP CRACKED AT BS 344, LBL 45.6. REMOVED AND REPLACED STRAP PER AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

TIE CLIP CRACKED AT BS 986.5, STR 27L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

SUPPORT CHANNEL CRACKED BETWEEN BS 787 TO BS 807, RBL 14. REMOVED AND REPLACED CHANNEL IAW DWG AND SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FWD GALLEY DOOR STUB FRAME CRACKED AT BS 294.5, BETWEEN STR 6R TO STR 7R. REPAIRED STUB FRAME IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FRAME CORRODED AT BS 807, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

CHANNEL CORRODED AT BS 767+5, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

CHANNEL CORRODED AT BS 767+5, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

SUPPORT ANGLE CRACKED AT BS 1016, LBL 6. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

CHANNEL CORRODED AT BS 767+5, RBL 8.0. REPAIRED CHANNEL IAW EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

STRINGER CORRODED BETWEEN BS 727E TO BS 747, STR 26R. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

SHEAR TIE CORRODED AT BS 807, STRINGER 25R TO STRINGER 26R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DRAWING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 986.5, BETWEEN RBL 29 TO RBL 44. REPAIRED BEAM IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

SHEAR TIE CORRODED AT BS 947.5, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FITTING CRACKED AT BS 332.1, STR 8R. REMOVED AND REPLACED FITTING IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

STRINGER CORRODED BETWEEN BS 747 TO BS 767, STR 26R. REPAIRED STRINGER PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

CHANNEL CORRODED AT BS 767+5, LBL 3.0. REPAIRED CHANNEL IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

STRINGER SPLICE CRACKED BETWEEN BS 348.2 TO BS 360+8, STR 7L. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

STRINGER 26L CORRODED AT BAS 1006 TO BS 1016. REPAIRED STRINGER PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FRAME CORRODED AT BS 887, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

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

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

CHANNEL CORRODED AT BS 847+12, RBL 3.0. REPAIRED CHANNEL IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

TIE CLIP CRACKED AT BS 727D, STR 25R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

CHANNEL CORRODED AT BS 847+12, LBL 8.10. REPAIRED CHANNEL IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

TIE CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FRAME CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

TIE CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

TIE CLIP CRACKED AT BS 767, STR 23L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FRAME WEB CRACKED AT BS 332, BETWEEN STR 1R TO STR 8R. REPAIRED FRAME IAW EO AND EA.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

SUPPORT ZEE CRACKED BETWEEN BS 727A TO BS 727C+9, STR 25R. REMOVED AND REPLACED SUPPORT ZEE IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

CHANNEL CORRODED AT BS 847+12, LBL 12.50. REPAIRED CHANNEL IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

TIE CLIP CRACKED AT BS 727E, STR 18R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

STRINGER CORRODED BETWEEN BS 927 TO BS 947.5, STR 26R. REPAIRED STRINGER IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FRAME CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FRAME CORRODED AT BS 747, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

CHANNEL CORRODED AT BS 847+12, LBL 3.0. REPAIRED CHANNEL IAW EA.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

STRINGER SPLICE CORRODED AT BS 907, STR 20L. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FRAME CORRODED AT BS 500C, BETWEEN STR 28R AND STR 28L. REPAIRED FRAME IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

WEB CRACKED BETWEEN BS 500B AND BS 500C, STR 26L. REMOVED AND REPLACED WEB IAW SRM DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FRAME CORRODED AT BS 500B, BETWEEN STR 26R AND STR 27R. REPAIRED FRAME IAW SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 82,727 hrs · 65,408 cycles

CRACK ON ANGLE SUPPORT LOCATED AT EXHAUST OF APU AT LEVEL BS 1217 TAIL CONE. REMOVED AND REPLACED SUPPORT IAW SRM AND DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FRAME CORRODED AT BS 500B, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

WEB CRACKED BETWEEN BS 500A AND BS 500B, STR 26R. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FRAME CORRODED AT BS 500C, BETWEEN STR 27L AND STR 26L. REPAIRED FRAME PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

STIFFENER CRACKED AT BS 727, STR 27R. REMOVED AND REPLACED STIFFENER PER SRM AND DWG.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 82,727 hrs · 65,408 cycles

CRACKS ON EDGE FRAME AT BS 440 AT LEVEL STR 25R INTERNAL STRUCTURE FWD CARGO COMP DOOR. REMOVED AND REPLACED FWD CARGO COMPARTMENT DOOR IAW AMM 52-31-00-404-022.

Part: FRAME — CORRODED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FRAME CORRODED AT BS 500C, BETWEEN STR 26R AND STR 27R. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

SKIN CRACKED AT BS 259.5, STR 16L. REPAIRED SKIN IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

FORWARD ENTRY DOOR SUPPORT ANGLE CRACKED AT FWD UPPER CORNER. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (R1 DOOR) · airframe 82,704 hrs · 65,391 cycles

R1 DOOR FORWARD EDGE SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,704 hrs · 65,391 cycles

SKIN CRACKED AT BS 440+15, STR 16R. REPAIRED SKIN IAW EO AND EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,378 hrs · 65,133 cycles

AFT GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,378 hrs · 65,133 cycles

AFT EXTERIOR EMERGENCY EXIT SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,058 hrs · 64,884 cycles

SKIN CRACKED AT BS 727D +5.0, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,058 hrs · 64,884 cycles

SKIN CRACKED AT BS 480 + 16.5, STR 16L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,058 hrs · 64,884 cycles

SKIN CRACKED AT BS 520 + 20, STR 1. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,058 hrs · 64,884 cycles

FUSELAGE SKIN CRACKED AT BS 500B + 5.0, STR 15L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,058 hrs · 64,884 cycles

FUSELAGE SKIN CRACKED AT BS 360 + 1.50, STR 6R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,058 hrs · 64,884 cycles

SKIN CRACKED AT BS 360+1.5, BETWEEN STR 5R TO STR 6R. REPAIRED SKIN IAW EA.

Part: LAMP — INOPERATIVE (SIGN) · airframe 81,129 hrs · 64,177 cycles

R2 DOOR EMERGENCY EXIT SIGN BULB INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 81,129 hrs · 64,177 cycles

LT OVERWING EMERGENCY EXIT SIGN BULBS INOPERATIVE. RELAMPED IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 80,682 hrs · 63,839 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 80,349 hrs · 63,584 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY. REINSTALLED SLIDE PER MM AND MT.

Part: LIGHT — BROKEN (CABIN) · airframe 79,426 hrs · 62,873 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,253 hrs · 62,742 cycles

DURING SCHEDULED MV2 CHECK FOUND, R2 DOOR EMERGENCY EXIT LIGHT BULB INOP. RELAMPED PER MM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK FOUND, R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS PER MM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED SPV CHECK, FOUND RT CREASE BEAM CRACKED AT BS 616. REMOVED AND REPLACED BEAM PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK FOUND, RT FLOORBEAM CRACKED AT BS 616. REMOVED AND REPLACED BEAM PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND LONGITIDUNAL FLOORBEAM WEB CRACKED AT BS 707, LBL 24.5. REPAIRED BEAM PER EA.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND BULKHEAD LOWER CHORD CORRODED AT BS 227.5, RBL 9. REPAIRED CHORD PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK FOUND, LOWER FUSELAGE SKIN CRACKED AT STA 907+10.5 TO 907+12, ABOVE STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK FOUND, CRACKED LOWER FUSELAGE SKIN, STA 927+15.5 TO 927+18.5, ABOVE STR 24R. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CORRODED (NLG WW) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND NOSE LANDING GEAR WHEEL WELL PRESSURE BULKHEAD LOWER CHORD CORRODED BETWEEN BS 246 TO BS 251, RBL 20. REMOVED AND REPLACED CHORD PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CRACK, RT SIDE OF PASSENGER CABIN, BS 639. REPAIRED PER DOC.

Part: FRAME — CORRODED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND CORROSION AFT PIT FRAME, STA 794 BETWEEN STR 27R AND 25R. REPAIRED PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED BETWEEN BS 747+17 TO BS 747+18, STR 19L. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26L TO STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — DELAMINATED (SPOILER) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT WING 0 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED 0 SPOILER PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CORRODED AT BS 787, STR 27L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED BETWEEN BS 727E+12.5 TO BS 727E+14, STR 18L. REPAIRED SKIN PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND CREASE BEAM WEB CRACKED BETWEEN BS 635 TO BS 638.5, BETWEEN LBL 68.5 TO LBL 69.5. REPAIRED WEB PER SRM AND BAC DWG.

Part: STRUCTURE — CORRODED (NLG WW) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND NOSE LANDING GEAR WHEEL WELL RT GEAR DOOR CENTER HINGE BOX SURFACE CORRODED ON LOWER SIDE. REMOVED AND REPLACED BOX PER SRM AND BAC DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND FLOORBEAM CORRODED AT BS 727D+5, LBL 12. REPAIRED BEAM PER SRM AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CORRODED AT BS 380, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — DELAMINATED (AILERON TAB) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT WING AILERION TAB I/B LOWER SKIN DELAMINATED. REPAIRED TAB PER MM.

Part: LENS — CRACKED (CABIN) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN LENS CRACKED. REMOVED AND REPLACED LENS ASSY PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED ADN REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CORRODED AT BS 767, STR 27L. REMOVED AND REPLACED STRINGER PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 79,136 hrs · 62,656 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CORRODED AT BS 827, STR 26L. REPAIRED FRAME PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 79,004 hrs · 62,561 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 78,819 hrs · 62,421 cycles

L1 DOOR SLIDE OUT OF ADJUST. REMOVED AND REPLACED SLIDE PER MT.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 78,778 hrs · 62,390 cycles

AFT O/B EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 78,646 hrs · 62,302 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,646 hrs · 62,302 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 19R TO STR 22R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,646 hrs · 62,302 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 520, BETWEEN STR 19L TO STR 22L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,646 hrs · 62,302 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 19L TO STR 22L. REPAIRED FRAME PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 78,263 hrs · 62,020 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING O/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,263 hrs · 62,020 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 323, STR 23R. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 78,263 hrs · 62,020 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 78,263 hrs · 62,020 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,314 hrs · 60,725 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKN CRACKED AT BS 484, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,418 hrs · 61,357 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 729D, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,418 hrs · 61,357 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 770, STR 18R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,418 hrs · 61,357 cycles

DURING SCHEDULED CV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,418 hrs · 61,357 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 394, STR 15L. REPAIRED SKIN PER EA.

Part: LENS — MISSING (CABIN) · airframe 77,418 hrs · 61,357 cycles

DURING SCHEDULED CV CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,418 hrs · 61,357 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 770, STR 18L. REPAIRED SKIN PER SRM.

Part: SHUTOFF VALVE — LEAKING (HYDRAULIC SYS) · airframe 77,343 hrs · 61,297 cycles

DECLARED EMERGENCY, HYDRAULIC A SYSTEM FAILED ON CLIMBOUT. REMOVED AND REPLACED HYDRAULIC MODULAR PACKAGE SHUT OFF VALVES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,250 hrs · 61,223 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 520, STR 17R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,250 hrs · 61,223 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 505D, STR 15L. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 77,176 hrs · 61,172 cycles

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

Part: BALLAST — INOPERATIVE (CABIN) · airframe 76,797 hrs · 60,895 cycles

ELECTRICAL SMELL NEAR OVERHEAD CABIN, LIGHT BETWEEN ROW 15 TO ROW 17 INOP. REMOVED AND REPLACED BALLAST PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 76,694 hrs · 60,815 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 76,614 hrs · 60,758 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 76,600 hrs · 60,744 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MM.

Part: LENS — MISSING (CABIN) · airframe 75,960 hrs · 60,262 cycles

R2 DOOR EMERGENCY EXIT LIGHT SIGN LENS MISSING. REMOVED AND REPLACED LENS PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,791 hrs · 60,137 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED BETWEEN BS 910 TO BS 912, STR 22L. REMOVED AND REPLACED STRINGER PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 75,791 hrs · 60,137 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING NR 5 SLAT DELAMINATED. REMOVED AND REPLACED NR 5 SLAT PER MM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 75,791 hrs · 60,137 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED BETWEEN BS 904 TO BS 910, STR 22L. REMOVED AND REPLACED SPLICE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,791 hrs · 60,137 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 986, BETWEEN STR 23L TO STR 24L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 75,791 hrs · 60,137 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED BETWEEN BS 904 TO BS 910, STR 19L. REMOVED AND REPLACED SPLICE PER SRM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 75,125 hrs · 59,660 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 3 SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 75,125 hrs · 59,660 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 4 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 73,809 hrs · 58,690 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR FWD GALLEY EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: FRAME — CRACKED (BS 559 S13R) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 559, STR 13R. REPAIRED FRAME PER AAR EA.

Part: FRAME — CRACKED (BS 727C S13L) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 727C, STR 13L. REPAIRED FRAME PER AAR EA.

Part: SKIN — CRACKED (BS 291) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT, BS 291, WL 258. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 982 S21L) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 982, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 291) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT, BS 291, WL 258. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (BS 308) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT, BS 308, WL 139. REPAIRED SKIN PER AAR EA.

Part: STRINGER SPLICE — CORRODED (BS 537-540 S27L) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CORRODED BETWEEN BS 537 TO BS 540, STR 27L. REMOVED AND REPLACED SPLICE PER SRM.

Part: SKIN — CRACKED (BS 306-308) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT, BETWEEN BS 306 TO BS 308, BETWEEN WL 139 TO WL 140. REPAIRED SKIN PER SRM.

Part: ATTACH FITTING — CRACKED (CENTER FUEL TANK) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND CENTER FUEL TANK UPPER ATTACH FITTING CRACKED AT BS 540, RBL 39. REMOVED AND REPLACED FITTING PER SRM.

Part: ATTACH FITTING — CRACKED (CENTER FUEL TANK) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND CENTER FUEL TANK UPPER ATTACH FITTING CRACKED AT BS 540, LBL 33. REMOVED AND REPLACED FITTING PER SRM.

Part: ATTACH FITTING — CRACKED (CENTER FUEL TANK) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND CENTER FUEL TANK UPPER ATTACH FITTING CRACKED AT BS 540, LBL 41. REMOVED AND REPLACED FITTING PER SRM.

Part: ATTACH FITTING — CRACKED (CENTER FUEL TANK) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND CENTER FUEL TANK UPPER ATTACH FITTING CRACKED AT BS 540, LBL 58. REMOVED AND REPLACED FITTING PER SRM.

Part: ATTACH FITTING — CRACKED (CENTER FUEL TANK) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND CENTER FUEL TANK UPPER ATTACH FITTING CRACKED AT BS 540, RBL 57. REMOVED AND REPLACED FITTING PER SRM.

Part: ATTACH FITTING — CRACKED (CENTER FUEL TANK) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND CENTER FUEL TANK UPPER ATTACH FITTING CRACKED AT BS 540, RBL 32. REMOVED AND REPLACED FITTING PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 277, BELOW STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 440, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 13L. REPAIRED FRAME PER AAR EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 277, ABOVE STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 420, STR 13R. REPAIRED FRAME PER AAR EA.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND NLG W/W CEILING RT SNUBBER SPRING ATTACH POINT CRACKED. REPAIRED SKIN PER ACO.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND NLG W/W CEILING LT SNUBBER SPRING ATTACH POINT CRACKED. REPAIRED SKIN PER ACO.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM ANGLE CRACKED BETWEEN BS 291 TO BS 295, STR 17R. REMOVED AND REPLACED ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 360, BETWEEN STR 13R TO STR 14R, WL 235. REPAIRED FRAME PER AAR EA.

Part: WEB — CRACKED (NLG WW) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND CENTER WEB NOSE WHEEL WELL CRACKED BETWEEN BS 227 TO BS 259. REPAIRED WEB PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING O/B AFT FLAP I/B END DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED BETWEEN BS 537 TO BS 540, LBL 39, WL 154. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 13L. REPAIRED FRAME PER AAR EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED CLIP PER BOEING DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 1 SLAT I/B LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN LBL 2 TO RBL 2. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT CREASE BEAM CRACKED AT BS 639, RBL 64. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO DOOR SKIN CUTOUT UPPER AFT CORNER CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT CREASE BEAM WEB CRACKED BETWEEN BS 727B TO BS 727C, STR 17L. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, BETWEEN RBL 16 TO RBL 20. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 847, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING O/B AFT FLAP I/B END DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CRACKED BETWEEN BS 616 TO BS 639, STR 17R. REMOVED AND REPLACED WEB PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM T-CAP CRACKED AT BS 540, RBL 3. REMOVED AND REPLACED CHANNEL PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8R. REMOVED AND REPLACED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 270, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500D, STR 13L. REMOVED AND REPLACED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED FRAME PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 2 SLAT I/B WEDGE LOWER SURFACE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 2 SLAT O/B WEDGE LOWER SURFACE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING NR 6 SLAT O/B WEDGE LOWER SURFACE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING NR 5 SLAT I/B WEDGE LOWER SURFACE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 727C, STR 13L. REPAIRED FRAME PER AAR EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26 TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT BETWEEN BS 233 TO BS 304. REPAIRED SKIN PER AAR EA.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING NR 4 SLAT O/B WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 73,567 hrs · 58,517 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING NR 5 SLAT O/B WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,488 hrs · 58,462 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 446, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,703 hrs · 65,391 cycles

SKIN CRACKED AT BS 446, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,703 hrs · 65,391 cycles

SKIN CRACKED AT BS 446, STR 16R. REPAIRED SKIN IAW EO AND EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,274 hrs · 58,309 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR LOWER EMERGENCY EXIT LIGHT BULBS INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 728,080 hrs · 57,973 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 982 STR 21L. REPAIRED SKIN PER SWA EA.

Part: LENS — LOOSE (L1 DOOR) · airframe 72,416 hrs · 57,707 cycles

FOUND L1 DOOR EMERGENCY EXIT LENS UNSECURED. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,134 hrs · 57,517 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 798, ABOVE STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,134 hrs · 57,517 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 797, BELOW STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,134 hrs · 57,517 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,134 hrs · 57,517 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 791, ABOVE STR 18L. REPAIRED SKIN PER SRM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 71,084 hrs · 56,761 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 70,725 hrs · 56,508 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 70,674 hrs · 56,473 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,594 hrs · 56,415 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737, STR 18R. REPAIRED SKIN PER SWA EA.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 70,555 hrs · 56,374 cycles

AFTER CONFIGURATION FOR LANDING AND VERIFYING ALL GEARS DOWN AND LOCKED (THREE GREEN LIGHTS ILLUMINATED), RECEIVED "TOO LOW GEAR" AURAL WARNING AT 1000 AGL, ALL GEARS HAD RED AND GREEN LIGHTS ILLUMINATED. DID A GO AROUND. PERFORMED SI ON LANDING GEAR HANDLE, CHECKS GOOD PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,349 hrs · 56,228 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 20L. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 69,944 hrs · 55,931 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE BEADED PRESSURE WEB CRACKED AT BS 664, LBL 40. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,933 hrs · 55,923 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 986, STR 27R. REPAIRED SHEAR TIE PER SWA EA.

Part: LOGIC CARD — FAULTY (E&E BAY) · airframe 69,769 hrs · 55,810 cycles

NLG RED LIGHT ILLUMINATED, CYCLED GEAR, LIGHT EXTINGUISHED. REMOVED AND REPLACED LOGIC CARD AND RELAY PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 69,158 hrs · 55,356 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: MIXING VALVE — FAULTY (A/C BAY) · airframe 415,959 hrs · 54,976 cycles

AIRTURN BACK/DECLARED EMERGENCY. ON DESCENT TO DHN EXPERIENCED SMOKE IN FLIGHTDECK, NO SMOKE DETECTED IN LAV OR CABIN. SMOKE DISSIPATED, SOURCE OF SMOKE NOT DETERMINED. INSPECTED AIRCRAFT, REMOVED AND REPLACED RT MIX VALVE PER MM.

Part: SKIN — DELAMINATED (RT WING SPOILER) · airframe 68,670 hrs · 54,870 cycles

DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING NR 9 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,670 hrs · 54,970 cycles

DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — BROKEN (L1 DOOR) · airframe 68,670 hrs · 54,870 cycles

DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,670 hrs · 54,970 cycles

DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CORRODED (BS 910 S27L) · airframe 68,670 hrs · 54,870 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 910, STR 27L. REPAIRED SKIN PER SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,670 hrs · 54,970 cycles

DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 68,670 hrs · 54,970 cycles

DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. FOUND UN-TERMINATED WIRE, RE-TERMINATED WIRE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,670 hrs · 54,970 cycles

DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,670 hrs · 54,970 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 28R CORRODED AT BS 326. REPAIRED STRINGER PER SRM.

Part: FITTING — CORRODED (EVAC SLIDE) · airframe 68,670 hrs · 54,970 cycles

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

Part: TORQUE TUBE — WORN (T/E FLAP) · airframe 68,670 hrs · 54,970 cycles

DURING SCHEDULED BRDG CHECK, FOUND RIGHT OUTBOARD T/E FLAP TORQUE TUBE WORN. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,527 hrs · 54,858 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,270 hrs · 53,878 cycles

L1 DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,197 hrs · 53,820 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, STR 15L. REPAIRED SKIN PER SWA EA.

Part: HOOK — BROKEN (R2 DOOR) · airframe 67,188 hrs · 53,813 cycles

R2 DOOR EVACUATION SLIDE GIRT BAR FWD ATTACH HOOK BROKEN. REMOVED AND REPLACED R2 DOOR SLIDE COVER ASSY PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 66,761 hrs · 53,477 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 66,212 hrs · 53,035 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT L2 DOOR FWD LOWER CORNER. REPAIRED SKIN PER SWA EA.

Part: STRUCTURE — CRACKED (RT WING SLAT) · airframe 66,212 hrs · 53,035 cycles

DURING SCHEDULED C3 CHECK, FOUND RIGHT WING NR 6 L/E SLAT CRACKED AT AFT OUTBOARD END. REPAIRED SLAT PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 65,278 hrs · 52,397 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER BOEING DRAWING AND ACO.

Part: BEAM — CORRODED (RT MLG) · airframe 64,867 hrs · 51,987 cycles

DURING SCHEDULED A2 CHECK, FOUND RT MLG WALKING BEAM CORRODED. REMOVED AND REPLACED RT MLG WALKING BEAM PER MM AND SI.

Part: BEAM — CORRODED (LT MLG) · airframe 64,867 hrs · 51,987 cycles

DURING SCHEDULED A2 CHECK, FOUND LT MLG WALKING BEAM CORRODED. REMOVED AND REPLACED LT MLG WALKING BEAM PER MM AND SI.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 64,356 hrs · 51,612 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,337 hrs · 51,596 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER FWD RADIUS. REPAIRED SKIN PER SRM.

Part: PANEL — DELAMINATED (LT MIDFLAP) · airframe 64,337 hrs · 51,596 cycles

DURING SCHEDULED C1 CHECK, FOUND LT WING T/E INBOARD MID FLAP WEDGE PANEL DELAMINATED. REMOVED AND REPLACED LT MID FLAP WEDGE PANEL PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,337 hrs · 51,596 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER AFT RADIUS. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,337 hrs · 51,596 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737, STR 19R. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (BS 946) · airframe 63,915 hrs · 51,260 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 946, STR 21L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 312) · airframe 63,709 hrs · 51,094 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 18R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 63,398 hrs · 50,855 cycles

DURING SCHEDULED C4 CHECK, FOUND RH HORIZONTAL STAB LOWER SKIN CRACKED AT AFT SPAR ATTACH POINT. REPAIRED HORIZONTAL STAB PER SRM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,169 hrs · 50,661 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF LIMITS (L1 DOOR) · airframe 62,030 hrs · 49,730 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATED OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,488 hrs · 49,299 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 957, STR 21L. REPAIRED SKIN PER SWA EA & SRM.

Part: SUPPORT BEAM — CORRODED (LT MLG) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND LT MLG SUPPORT BEAM CORRODED AT FASTENER HOLES. REPAIRED BEAM PER PAE ER.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE KEEL BEAM CORRODED AT BS 723, BS 725, BS 529 & BS 500D + 6. REMOVED AND REPLACED KEEL BEAM PER SRM.

Part: LIGHT — BROKEN (L2 DOOR) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 529, STR 28L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE CHORD CRACKED AT BS 727, RBL 30. REPAIRED CHORD PER PAE ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 360, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND LT HORIZONTAL STAB, AFT SPAR, UPPER CHORD CORRODED AT STA 276.70. REPAIRED LT HORIZONTAL STAB PER SRM & SB.

Part: FRAME — CRACKED (FWD CARGO) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND FWD CARGO COMPARTMENT CUTOUT FRAME CRACKED AT BS 490, RBL 37, WL 158. REPAIRED FRAME PER PAE ER.

Part: FLOORBEAM — CORRODED (COCKPIT) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOORBEAM UPPER CHORD CORRODED AT BS 260, BETWEEN RBL 2 TO LBL 9, WL 200. REPAIRED FLOORBEAM PER PAE ER & SRM.

Part: FRAME — CORRODED (AFT CARGO) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FUSELAGE FRAME AT BS 847, BETWEEN STR 23R & STR 25R. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION AT BS 360, STR 27L. REPAIRED STRINGER PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND 4 EA CRACKS ON LONGITUDINAL BEAMS AT BS 727A + 17, RBL 25, RBL 45, LBL 25, LBL 45. REPAIRED BEAMS PER PAE ER.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON KEEL BEAM AT BS 727, LT OUTBOARD CHORD STRAP. REPAIRED KEEL BEAM PER SRM.

Part: LIGHT — WORN (FWD CABIN) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND FWD CABIN EEPLS STRIPS WORN. REMOVED AND REPLACED EEPLS STRIPS PER MM.

Part: STRINGER — CORRODED (AFT CARGO BAY) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON STRINGER BETWEEN BS 1006 TO BS 1014, STR 26R. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 360, BETWEEN STR 27L & STR 28L. REPAIRED SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND BS 1016 PRESS BULKHEAD CRACKED AT STR 9R. REPAIRED PRESS BULKHEAD PER PAE ER.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 747, LBL 9, WL 147. REPAIRED SHEAR TIE PER SRM.

Part: CLEVIS — CORRODED (VERTICAL STAB) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FUSELAGE FRAME STRAP AT BS 847, RBL 17, WL 154. REMOVED AND REPLACED STRAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, BETWEEN STR 13L & STR 14L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 344) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R AND STR 13R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727C, STR 9R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND 3 EA CRACKS ON LONGITUDINAL BEAM WEB AT BS 710, RBL 25, WL 201. REPAIRED BEAM PER PAE ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FRAME CRACKS AT BS 663, STR 3L & STR 3R. REPAIRED FRAME PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND 4 EA CRACKS AT BS 1016 PRESS BULKHEAD, STR 7L, STR 15L, STR 23R & DOME CAP. REPAIRED PRESS BULKHEAD PER PAE ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FUSELAGE FRAME AT BS 1006, LBL 39, WL 200. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 9L. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (RT WING SPOILER) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND RT WING T/E NR 6 SPOILER LWR SURFACE DELAMINATED. REMOVED AND REPLACED NR 6 SPOILER ASSY PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA FLOOR WEB CRACKS BETWEEN BS 188 TO BS 196, STR 17L & STR 17R. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 727D, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9L. REPAIRED FUSELAGE FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER AT BS 360, STR 14L. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 9R. REPAIRED FUSELAGE FRAME PER SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND LT HORIZONTAL STAB L/E NR 1 RIB CRACKED. REPAIRED LT HORIZONTAL STAB RIB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 847, RBL 17, WL 154. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACK AT BS 380, STR 9R. REPAIRED FUSELAGE FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 277, STR 14R. REPAIRED FRAME WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 9R. REPAIRED FUSELAGE FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L & 17R. REPAIRED FUSELAGE FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 303.9, STR 4L. REPAIRED FRAME WEB PER SRM.

Part: FRAME — CRACKED (BS 727E) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 9L. REPAIRED FUSELAGE FRAME PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 360, STR 15L. REPAIRED FUSELAGE STRINGER SPLICE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON LT CREASE BEAM WEB AT BS 727D, LBL 68. REPAIRED CREASE BEAM WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON RT CREASE BEAM WEB AT BS 727B, RBL 70. REPAIRED CREASE BEAM WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 9R. REPAIRED FUSELAGE FRAME PER SRM.

Part: FRAME — CRACKED (BS 827) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 9R. REPAIRED FUSELAGE FRAME PER SRM.

Part: FITTING — CORRODED (LT MLG STRUT) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON LT MLG LOWER STRUT FITTING. REMOVED AND REPLACED LT MLG LOWER STRUT FITTING PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 344, RBL 17. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 907, BL 0, WL 160. REPAIRED SHEAR TIE PER SRM.

Part: SPLICE — CRACKED (BS 907) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, BETWEEN STR 4L AND STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 807, STR 9L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON STRINGER CLIP AT BS 727E, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CRACK AT LT CREASE BEAM WEB AT BS 375. REPAIRED BEAM WEB PER SRM.

Part: LIGHT — INOPERATIVE (R2 DOOR) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND R2 DOOR ESCAPE SLIDE LIGHT INOP. REMOVED AND REPLACED LIGHT HOUSING PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 887, STR 9R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 807, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA CRACKED STRINGER CLIPS BETWEEN BS 767 AND BS 787 STR 11L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727C) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 727C, BETWEEN STR 2R AND 6R CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 60,529 hrs · 48,520 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 727B, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 827, STR 9R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 727C, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727C) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 727C,BETWEEN STR 5L AND 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 767, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

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

Part: STRINGER CLIP — CRACKED (BS 597) · airframe 60,529 hrs · 48,520 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 616, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 727A, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA CRACKED STRINGER CLIPS AT BS 727E, BETWEEN STR 5L AND 7L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND BS 440 FRAME CRACKED AT STR 9L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 727A, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 907, STR 9R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND 3 EA CRACKED STRINGER CLIPS AT BS 727D, BETWEEN STR 4L AND 6L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 727D, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND CRACK AT STRINGER SPLICE, BS 663, STR 7L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,529 hrs · 48,520 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, STR 9R CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 59,542 hrs · 47,762 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 59,542 hrs · 47,762 cycles

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

Part: LIGHT — LOOSE (ROW 2 ABC) · airframe 58,941 hrs · 47,243 cycles

BULL NOSE EMERGENCY EXIT LIGHT AT ROW 2 ABC, LOOSE. SECURED BULL NOSE EMERGENCY EXIT LIGHT PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 58,931 hrs · 47,233 cycles

EMERGENCY EXIT BULLNOSE LIGHT LOOSE AT ROW 2. SECURED LIGHT ASSY PER MM.

Part: LENS — MISSING (EMERGENCY EXIT) · airframe 58,771 hrs · 47,111 cycles

CENTER AISLE OVERWING EMERGENCY EXIT LIGHT MISSING 2 EACH LENSES. INSTALLED 2 EACH LIGHT LENSES PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,665 hrs · 47,020 cycles

DURING SPV, FOUND FWD OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — LOOSE (ROW 3) · airframe 58,115 hrs · 46,561 cycles

DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT AT ROW 3 ABC, LOOSE. SECURED EMERGENCY EXIT LIGHT PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,334 hrs · 45,963 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — GROUNDED (PAX DOOR) · airframe 56,734 hrs · 45,474 cycles

DURING SPECIAL VISIT FOUND LOWER R1 AND L1 EMERGENCY LIGHTS INOP. REPAIRED GROUNDED WIRE PER WDM AND MM.

Part: FIRE WARNING — FAULTY (APU BAY) · airframe 56,485 hrs · 45,277 cycles

APU FIRE WARN LIGHT ILLUMINATED DURING FLIGHT. INSPECTED APU AREA. NO EVIDENCE OF FIRE OR DAMAGE. DEFERRED APU AND APU FIRE WARN SYS'S PER MEL.

Part: RELAY — FAULTY (COCKPIT) · airframe 55,809 hrs · 44,736 cycles

INTERMITTENT NLG UNSAFE LIGHT WITH HANDLE IN OFF OR UP, WITH GEAR EXTENDED ALL LIGHTS NORMAL. REMOVED AND REPLACED R-374 RELAY, M1214 AND M1215 LOGIC CARDS PER MM.

Part: CONTROL UNIT — FAULTY (FIRE WARNING) · airframe 54,654 hrs · 43,789 cycles

AIR TURNBACK, DURING TAKEOFF BOTH FWD AND AFT CARGO FIRE INDICATION LIGHTS ILLUMINATED. REMOVED AND REPLACED FIRE WARNING CENTRAL CONTROL UNIT PER MM.

Part: LENS — LOOSE (CABIN) · airframe 54,244 hrs · 43,456 cycles

OVERHEAD BIN EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 7 ABC. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,167 hrs · 43,395 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED, BS 1013, BETWEEN STRINGERS 21L & 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,561 hrs · 42,131 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR LOWER AFT CUTOUT, BS 350 AND ABOVE STR 17L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,561 hrs · 42,131 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R-1 COCKPIT WINDOW FRAME SKIN CRACKED AT UPPER OTBD CORNER. REPAIRED SKIN PER SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 52,559 hrs · 42,129 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AIRSTAIR DOOR CUTOUT CRACKED AT BS 344, STR 21L. REPAIRED DOUBLER PER SWA EA.

Part: SPOILER — DELAMINATED (LT WING) · airframe 52,559 hrs · 42,129 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT T/E SPOILERS, NR 0, NR 1, NR 2 AND NR 3 DELAMINATED. REMOVED AND REPLACED LT T/E SPOILERS, NR 0, NR 1, NR 2 AND NR 3 PER MM. SERIAL NUMBERS, 2825Y AT NR 0, 2857Y AT NR 1, 2779Y AT NR 2 AND 2885Y AT NR 3.

Part: SKIN — DELAMINATED (RT WING) · airframe 52,559 hrs · 42,129 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT T/E INBD FORE FLAP DELAMINATED ON UPPER SKIN. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (MID CABIN) · airframe 52,559 hrs · 42,129 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 663, BL 0. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CRACKED (AFT CARGO) · airframe 52,559 hrs · 42,129 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 727D + 6, LBL 8. REPAIRED FLOORBEAM PER SWA RA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,559 hrs · 42,129 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 825, RBL 3. REPAIRED FLOORBEAM PER SRM AND SWA RA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 52,559 hrs · 42,129 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 663.75, LBL 6.15. REPAIRED STIFFENER PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,230 hrs · 41,864 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUT OUT. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,141 hrs · 41,798 cycles

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

Part: WINDOW — DEFECTIVE (COCKPIT) · airframe 51,728 hrs · 41,451 cycles

F/O'S WINDOW WILL NOT OPEN FROM THE OUTSIDE USING THE EMERGENCY RELEASE HANDLE. REMOVED AND REPLACED F/O'S WINDOW PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,412 hrs · 41,195 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,412 hrs · 41,195 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS (2 EA) AFT CABIN INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: HOSE — LEAKING (RT MLG W/W) · airframe 51,381 hrs · 41,171 cycles

AIR TURNBACK, B HYD SYSTEM, FLUID LEAK NOTICED INFLIGHT AND RETURNED TO PHX. REMOVED AND REPLACED B HYD SYSTEM FLEX HOSE FROM B HYD PUMP TO ACOUSTIC FILTER PER MM.

Part: SLIDE — OUT OF ADJUST (AFT ENTRY DOOR) · airframe 51,339 hrs · 41,144 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,319 hrs · 41,128 cycles

DURING SCHEDULED RON, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,271 hrs · 41,088 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BOTH LT AND RT OUTBOARD BULKHEAD CHORDS CRACKED AT BS 178, WL 207. REMOVED AND REPLACED CHORDS PER SWA ACO.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,269 hrs · 41,085 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEBS CRACKED (2 EA) AT BS 180, RBL 17.1, WL 214 AND WL 224. REMOVED AND REPLACED WEBS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,236 hrs · 41,056 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 19R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJ (L2 DOOR) · airframe 50,461 hrs · 40,442 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 49,937 hrs · 40,034 cycles

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

Part: CABLE — FRAYED (AFT SVC DOOR) · airframe 49,459 hrs · 39,624 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. R&R CABLE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 48,662 hrs · 38,961 cycles

DURING SCHEDULED BC4 CHECK, FOUND EMERGENCY EXIT SIGN LENS LOOSE AT RT OVERWING EXIT. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM.

Part: FLAP — CRACKED (LT WING) · airframe 48,662 hrs · 38,961 cycles

DURING SCHEDULED C4 CHECK, FOUND LT OTBD T/E MID FLAP LEADING EDGE CRACKED AT CONTROL ROD CUTOUT. REPAIRED FLAP PER SWA RA 1-357-1047 REV 1.

Part: FLAP — DEBONDED (LT WING) · airframe 48,662 hrs · 38,961 cycles

DURING SCHEDULED C4 CHECK, FOUND LT OTBD AFT FLAP DISBONDED AT INBD LWR END. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 47,730 hrs · 38,168 cycles

DURING SCHEDULED C3 CHECK, FOUND NR 1 L/E SLAT SKIN CRACKED AT AFT ROW OF FASTENERS, INBD OF OUTBD AUX TRACK. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 47,730 hrs · 38,168 cycles

DURING SCHEDULED C3 CHECK, FOUND NR 2 L/E SLAT SKIN CRACKED AT 3 FASTENER HOLES ON AFT ROW. REPAIRED SKIN PER SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 47,382 hrs · 37,861 cycles

FWD SVC DOOR EMERGENCY EXIT LIGHT ILLUMINATED AFTER PUSHBACK. REMOVED AND REPLACED HOUSING CHARGER ASSY PER MM.

Part: BATTERY PACK — DISCHARGED (SERVICE DOOR) · airframe 47,382 hrs · 37,861 cycles

DURING SCHEDULED PM CHECK, FOUND FWD SVC DOOR OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: EEC — ERRATIC (NR 1 ENGINE) · airframe 47,234 hrs · 37,724 cycles

DIVERSION, DECLARED EMERGENCY. NR 1 ENGINE ROLLED BACK. EGT DROPPED RAPIDLY AND OTHER INDICATIONS FLUCTUATED FOR APPROX 10 SECONDS. NOTED A STRONG ODOR IN THE COCKPIT. ENGINE RECOVERED ON ITS OWN AND ODOR DISSAPATED AFTER ABOUT 10 MINUTES. NR 1 ENG FUEL SHUT OFF VALVE C/B TRIPPED WHEN FUEL CUT OFF. REMOVED AND REPLACED FUEL PUMP (P/N 301-779-005) AND MEC OPS, LEAK CHECK AND TRIM GOOD PER MM. REPAIRED FUEL SHUT OFF VALVE WIRING AT DISCONNECT BRACKET, STA 720L, PER MM. OPS CHECK NORMAL PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 45,820 hrs · 36,557 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE RELEASE CABLE FRAYED AND GIRT ASSY OUT OF ADJUST. REMOVED AND REPLACED CABLE AND ADJUSTED SLIDE ASSY PER MM.

Part: CONNECTOR — DAMAGED (NR 1 AND 4 SLATS) · airframe 45,810 hrs · 36,546 cycles

DIVERSION, AFTER TAKEOFF NR 1 AND 4 L/E SLAT LIGHTS ILLUMINATED. RESEATED NR 1 L/E SLAT PIN CONNECTOR, AND CLEANED NR 4 L/E SLAT CONNECTOR AT ACTUATORS. OPS CK GOOD PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 45,596 hrs · 36,355 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FRAME — CRACKED (BS 619)

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAMES CRACKED, BS 619, LBL 65.7 AND RBL 65.7. REPAIRED FRAMES PER TI-153-018.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM UPPER SURFACE, BS 328, LBL 28. REPAIRED BEAM PER RA NR 1-353-2232.

Part: FRAME — CRACKED (BS 986)

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STUB FRAME CRACKED, BS 986, WL 208 LT SIDE. REPAIRED FRAME PER SRM.

Part: BRACKET — CORRODED (GIRT BAR)

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT BAR FLOOR MOUNT BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS PER SRM.

Part: SLIDE — DISLODGED (FWD ENTRY DOOR)

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (BS 312)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 312, BETWEEN STRINGERS 25L-26L. REPAIRED SKIN PER SRM.

Part: REGULATOR — INOP (NR 2 ENGINE)

AIR TURNBACK DUE TO NR 2 ENG BLEED AIR VALVE C/B POPPED IN FLIGHT AND WOULD NOT RESET. REMOVED AND REPLACED NR 2 ENG BLEED AIR REGULATOR.

Part: SKIN — DAMAGED (BS 540)

DURING SCHEDULED C2 CHECK, FOUND PULLED RIVET AT SKIN NEAR CONDITIONED AIR DOOR AT BS 540 KEEL BEAM. MADE PERMANENET REPAIR PER RA 1-353-1897.

Part: INTERCOSTAL — CRACKED (BS 520)

DURING SCHEDULED C2 CHECK, FOUND INTERCOSTAL CRACKED AT BS 520. REMOVED AND REPLACED PER BOEING SRM.

Part: WINDOW POST — CRACKED (LT COCKPIT)

DURING SCHEDULED C4 CHECK, FOUND CAPT NR 1 WINDOW O/B POST CRACKED AT UPPER CORNER. REPAIRED PER SWA RA 1-A53-003.

Part: SENSOR — INOP (RT PACK)

AFTER TAKEOFF, UNABLE TO CONTROL CABIN PRESSURIZATION USING AUTO, STANDBY OR MANUAL. AIRCRAFT RETURNED TO LAS AND MADE AN UNEVENTFUL LANDING. INSPECTED AND PERFORMED BITE TEST, ALL SYSTEMS NORMAL PER BOEING M/M. RIGHT PACK THEN TRIPPED ON GROUND AND WOULDN'T RESET. REPLACED TURBINE INLET SENSOR PER BOEING M/M.

Part: CHORD — CORRODED (BS 847)

DURING SCHEDULED TRANSITION CHECK, FOUND FAILSAFE CHORD CORRODED AT BS 847, BL 0, WL 148. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SHEAR TIE — GOUGED (BS 727D)

DURING SCHEDULED TRANSITION CHECK, FOUND SHEAR TIE GOUGED AT BS 727D, BETWEEN S19 TO 20R. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: WEB — CORRODED (BS 822/860)

DURING SCHEDULED TRANSITION CHECK, FOUND UPPER FLANGE OF VERTICAL SUPPORT WEB CORRODED AT BS 822 AND AT 860, RBL22, WL 154. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DENTED (BS 300-312)

DURING SCHEDULED TRANSITION CHECK, FOUND 12 FUSELAGE SKIN DENT AT BS 300 TO 312, S20R. INSTALLED REPAIR PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FRAME — CRACKED (BS 727)

DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727, WL 160, RBL 24. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SUPPORT — CORRODED (BS 947-967)

DURING SCHEDULED TRANSITION CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CORRODED FROM BS 947 TO 967, LBL 41, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DAMAGED (BS 500)

DURING SCHEDULED TRANSITION CHECK, FOUND 11 LIGHTNING STRIKE DAMAGE AREAS TO FUSELAGE SKIN AT BS 500 TO 500D, BETWEEN S2 AND 4R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: DOOR FRAME — CRACKED (BS 957)

DURING SCHEDULED TRANSITION CHECK, FOUND AFT GALLEY DOORWAY UPPER FORWARD FRAME SECTION CRACKED AT BS957, WL 260, RBL 60. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: STRAP — CORRODED (BS 787-847)

DURING SCHEDULED TRANSITION CHECK, FOUND THRESHOLD TIE STRAP CORRODED FROM BS 787 TO 847, RBL 21, WL 154. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: INTERCOSTAL — CORRODED (BS 328-344)

DURING SCHEDULED TRANSITION CHECK, FOUND INTERCOSTAL WEB CORROSION FROM BS 328 TO 344, RBL 27, WL 208.1. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DAMAGED (BS 747-847)

DURING SCHEDULED TRANSITION CHECK, FOUND 14 LIGHTNING STRIKE DAMAGE AREAS TO FUSELAGE SKIN FROM BS 747 TO 827, BETWEEN S2 AND 3R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: DOOR SILL — CORRODED (BS 440-490)

DURING SCHEDULED TRANSITION CHECK, FOUND FWD CARGO DOOR SILL WEB CORRODED AT NUTPLATE HOLES AT BS 440 TO 490, WL 156, RBL 29. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SUPPORTS — CORRODED (BS 992.5)

DURING SCHEDULED TRANSITION CHECK, FOUND LAVATORY WALL SUPPORTS CORRODED AT BS 992.5, LBL 15, 20, 27, AND 43, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DAMAGE (BS 440-500)

DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN LIGHTNING STRIKE DAMAGE FROM BS 440 TO 500, BETWEEN S2 AND 4R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FLOORBEAM — CORRODED (BS 344)

DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM NUTPLATE HOLES CORRODED AT BS 344, BL 0, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: ANGLE — CRACKED (BS 536)

DURING SCHEDULED TRANSITION CHECK, FOUND UPPER DRAG ANGLE CRACKED AT BS 536, WL 172, BETWEEN S21 AND 22R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SUPPORTS — CORRODED (BS 956)

DURING SCHEDULED TRANSITION CHECK, FOUND LAVATORY WALL SUPPORTS CORRODED AT BS 956, LBL 27 AND 38, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: CLIP — CRACKED (BS 663.7)

DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CLIPS CRACKED AT BS 663.7, S10L AND R. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FLOORBEAM — CORRODED (BS 1007-1016)

DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR SUPPORT CORRODED FROM BS 1007 TO 1016, LBL 0, WL 208. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FLOORBEAM — CORRODED (BS 1006)

DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM CHORD CORROSION AT BS 1006, LBL 12, WL 208. REPAIRED PER TRAMCO EWO 95-0327.

Part: FLOORBEAM — DAMAGED (BS 807)

DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM HAS A HOLE IN RADIUS AFT SIDE, BS 807, LBL 47.5, WL 208. REPAIRED PER TRAMCO EWO 95-0318.

Part: SKIN — DENTED (BS 806)

DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT BS 806, BETWEEN S25 AND 26R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DENTED (E/E DOOR)

DURING SCHEDULED MAINT CHECK, FOUND E AND E DOOR, LT FWD AND AFT O/B CORNERS DENTED AND GOUGED. INSTALLED NEW SKIN PER BOEING SRM.

Part: SKIN — GOUGED (BS 952)

DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 952, 6 INCHES BELOW S17L. REPAIRED PER TRAMCO EWO 95-0031.

Part: BLKHD WEB — CRACKED (BS 178)

DURING SCHEDULED MAINT CHECK, FOUND PRESSURE BULKHEAD WEB CRACKED AT BS 178, LBL 57 AND WL 201. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DAMAGE (FS 380-440)

DURING SCHEDULED MAINT CHECK, FOUND LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN FROM BS 380 TO 440, BETWEEN S2 AND 4R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SILL — CORRODED (FS 942-986.5)

DURING SCHEDULED MAINT CHECK, FOUND AFT ENTRY DOORWAY LOWER MOP SILL CORRODED FROM BS 942 TO 986.5, WL 208, LBL 60. REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING SCHEDULED MAINT CHECK, FOUND FLOOR BEAM CORROSION AT BS 986.5, RBL 45, WL 208, AT BS 294.5, LBL 19, WL 208, AND AT BS 328, RBL 34 AND 48, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DENTED (FUSELAGE)

DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN DENTED AT THE FOLLOWING LOCATIONS: BS 910, WL 185, ABOVE STRINGER 19R, AT BS 932, AT S24L, AND AT BS 324, BETWEEN S22 AND 23R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — NICKED (FS 305/320)

DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN NICKED AND SCRATCHED AT BS 305 AND 320, BETWEEN S3 AND 4L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: CLIP — CRACKED (BS 570)

DURING SCHEDULED MAINT CHECK, FOUND LEFT AND RIGHT SKATE ANGLES CRACKED AT BS 570, WL 167.5, RBL 59. REPLACED PER BOEING M/M.

Part: SKIN — DENTED (BS 990-1016)

DURING SCHEDULED MAINT CHECK, FOUND AFT ENTRY DOOR SKIN DENTED AT BS 990-1016, BETWEEN S8 AND 10L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — GOUGED (BS 306)

DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN GOUGED AND DENTED AT BS 306, WL 255, 3 INCHES BELOW FWD ENTRY DOOR AT HINGE UPPER HINGE CUTOUT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED MAINT CHECK, FOUND BULKHEAD CHORD CRACKED AT BS 178, WL 195, ACCESS PLATE CUTOUT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SHEAR TIE — CORRODED (BS 927)

DURING SCHEDULED MAINT CHECK, FOUND SHEAR TIE CORRODED AT BS 927, LBL 22, WL 164. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DAMAGE (FUSELAGE)

DURING SCHEDULED MAINT CHECK, FOUND LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN FROM BS 520 TO 578, BETWEEN S1 AND 3R, AND AT BS 500D TO 520, BETWEEN S2 AND 3R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FRAME — GOUGED (BS 1104)

DURING SCHEDULED MAINT CHECK, FOUND DEEP GOUGE AT FRAME AT BS 1104, AT S14R. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: DOOR FRAME — DENTED (BS 727B)

DURING SCHEDULED MAINT CHECK, FOUND AFT CARGO FRAME DENTED AT 727B, S24R, RBL 32. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FRAME — GOUGED (BS 439)

DURING SCHEDULED MAINT CHECK, FOUND FWD CARGO DOOR FWD FRAME TO SIDEWALL SUPPORT DENTED AND GOUGED AT BS 439, WL 158, RBL 27. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.