N665WN

Part: SKIN — CRACKED (FUSELAGE) · airframe 91,028 hrs · 67,460 cycles

FUSELAGE SKIN CRACKED AT STATION 1010, STRINGER 23L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 91,028 hrs · 67,460 cycles

FUSELAGE SKIN CRACKED AT STATION 930, STRINGER 22R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 91,028 hrs · 67,460 cycles

FUSELAGE SKIN CRACKED AT STATION 466, STRINGER 16R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 91,028 hrs · 67,460 cycles

FUSELAGE SKIN CRACKED AT STATION 804, STRINGER 19L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 91,028 hrs · 67,460 cycles

FUSELAGE SKIN CRACKED AT STATION 813, STRINGER 19L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 91,028 hrs · 67,460 cycles

FUSELAGE SKIN CRACKED AT STATION 506, STRINGER 15L. REPAIRED SKIN IAW EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 91,028 hrs · 67,460 cycles

FUSELAGE STRINGER CORRODED AT STATION 727A+8 TO 727A+16, STRINGER 26L. REPAIRED STRINGER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 91,028 hrs · 67,460 cycles

FUSELAGE SKIN CRACKED AT STATION 582, STRINGER 10L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 91,028 hrs · 67,460 cycles

FUSELAGE SKIN CRACKED AT STATION 503B, STRINGER 15L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 91,028 hrs · 67,460 cycles

FUSELAGE SKIN CRACKED AT STATION 908 - 916, STRINGER 21L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 91,028 hrs · 67,460 cycles

FUSELAGE SKIN CRACKED AT STATION 961, STRINGER 5R. REPAIRED SKIN IAW EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 90,394 hrs · 67,002 cycles

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

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 90,394 hrs · 67,002 cycles

L1 DOOR EMER EVAC SLIDE GIRT NEEDS LOOSE. SECURED GIRT IAW MT.

Part: CABLE — MISROUTED (R2 DOOR GIRT BAR) · airframe 89,880 hrs · 66,620 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR WIRE CABLE MISROUTED. REROUTED CABLE IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,387 hrs · 66,244 cycles

LEFT OVERWING EMER EXIT LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: COVER — BROKEN (CABIN) · airframe 89,129 hrs · 66,043 cycles

R2 DOOR EMER EXIT LIGHT COVER BROKEN. REPAIRED COVER IAW SIP.

Part: LIGHT — LOOSE (CABIN) · airframe 88,838 hrs · 65,829 cycles

RIGHT CABIN OVERHEAD BIN EMER LIGHT LOOSE AT ROW 5. SECURED LIGHT HOUSING IAW MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 88,805 hrs · 65,804 cycles

L2 DOOR LOWER EMER LIGHT INOPERATIVE. R & R BATTERY IAW CMM.

Part: FUSE — INOPERATIVE (CABIN) · airframe 88,805 hrs · 65,804 cycles

RIGHT EMER EXIT DOOR LIGHT INOPERATIVE AT M1135. R & R FUSE IAW CMM & WDM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 88,805 hrs · 65,804 cycles

R2 DOOR LOWER EMER LIGHT INOPERATIVE. R & R BATTERY IAW CMM.

Part: ANGLE — CRACKED (FLAP TRACK) · airframe 88,805 hrs · 65,804 cycles

RIGHT WING NR 6 FLAP TRACK FAIRING ANGLE CRACKED AT WBL 201. R & R ANGLE IAW SRM & DWG.

Part: STIFFENER — CRACKED (RT WING) · airframe 88,805 hrs · 65,804 cycles

RIGHT WING STIFFENER CRACKED AT WS 505.00. REPAIRED STIFFENER IAW EA & EO.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FORWARD CARGO COMPARTMENT SUPPORT CHANNEL CRACKED BETWEEN BS 495 TO 500A, STRINGER 26R. R & R CHANNEL IAW SRM & DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FRAME SHEAR TIE CRACKED AT BS 500B, BETWEEN STRINGER 15R TO 16R. REPAIRED SHEAR TIE IAW EO & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FLOORBEAM CRACKED AT BS 294.5, RBL 53. REPAIRED FLOORBEAM IAW SRM.

Part: STIFFENER — CRACKED (LT WING) · airframe 88,805 hrs · 65,804 cycles

LEFT WING UPPER PANEL STIFFENER 2 CRACKED BETWEEN WBL 114 TO WBL 135.50. REPAIRED STIFFENER IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FRAME WEB CRACKED AT BS 887, STRINGER 17R. REPAIRED FRAME WEB IAW EO & EA.

Part: SKIN — CRACKED (TE FLAP) · airframe 88,805 hrs · 65,804 cycles

LEFT WING LE SKIN CRACKED ON INBD MID FLAP. REPAIRED SKIN IAW EO & EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

CLIP CRACKED AT BS 639, RBL 45.5. R & R CLIP IAW SRM & DWG.

Part: BEAM — CRACKED (RT WING) · airframe 88,805 hrs · 65,804 cycles

RIGHT WING AILERON AREA BEAM ASSEMBLY CRACKED BETWEEN 415 WBL TO 523.50 WBL. R & R BEAM ASSEMBLY IAW SRM & DWG.

Part: DOUBLER — CRACKED (FLAP TRACK) · airframe 88,805 hrs · 65,804 cycles

LEFT WING NR 3 FLAP TRACK INBD INTERNAL CAVITY DOUBLER CRACKED. R & R DOUBLER IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FUSELAGE FRAME CORRODED AT STATION 787, BETWEEN STRINGERS 24L & 25L. REPAIRED FRAME IAW EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

SHEAR TIE CRACKED AT BS 460, BETWEEN STRINGER 15L TO 16L. REPAIRED SHEAR TIE IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FUSELAGE FRAME CORRODED AT STATION 787, BETWEEN STRINGERS 26L & 25L. REPAIRED FRAME IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 1016, LBL 5. REPAIRED CHORD IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

CLIP CRACKED AT BS 947.5, STRINGER 22L. R & R CLIP IAW SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

STRINGER CRACKED AT BS 440, STRINGER 18R. R & R STRINGER IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

SUPPORT ANGLE CRACKED AT BS 986.5, STRINGER 23R. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

TIE CLIP CRACKED AT BS 887, STRINGER 23L. R & R TIE CLIP IAW SRM & DWG.

Part: SHIM — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

SPLICE ANGLE SHIM CRACKED AT BS 540, BETWEEN STRINGER 22L - 23L. R & R SHIM IAW DWG & SRM.

Part: BRACKET — CRACKED (RT SPOILER) · airframe 88,805 hrs · 65,804 cycles

RIGHT WING NR 5 SPOILER FITTING SUPPORT ANGLE BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 88,805 hrs · 65,804 cycles

LEFT WING INBD FLAP CARRIAGE TORQUE TUBE CORRODED INBD SIDE. R & R FLAP CARRIAGE IAW CMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FUSELAGE FRAME CRACKED AT STATION 727A, BETWEEN STRINGERS 13R & 14R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FUSELAGE FRAME CRACKED AT STATION 500A, BETWEEN STRINGERS 13L & 14L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FUSELAGE FRAME CRACKED AT STATION 500A, BETWEEN STRINGERS 15L & 16L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FRAME OUTER CHORD CRACKED AT BS 420, BETWEEN STRINGER 13L TO 14L. REPAIRED CHORD IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FUSELAGE FRAME CRACKED AT STATION 420, BETWEEN STRINGERS 13R & 14R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FRAME OUTER CHORD CRACKED AT BS 400, BETWEEN STRINGER 13R TO 14R. REPAIRED FRAME IAW EA & EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FRAME OUTER CHORD CRACKED AT BS 400, BETWEEN STRINGER 13L - 14L. REPAIRED FRAME IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FUSELAGE FRAME CRACKED AT STATION 480, BETWEEN STRINGERS 13L & 14L. REPAIRED FRAME IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 88,805 hrs · 65,804 cycles

LEFT WING OTBD FORE FLAP DELAMINATED INBD SIDE. REPAIRED FORE FLAP IAW SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

CREASE BEAM INNER CHORD CRACKED AT BS 639, STRINGER 17L. REPAIRED CHORD IAW EO & EA.

Part: STIFFENER — CRACKED (RT WING) · airframe 88,805 hrs · 65,804 cycles

RIGHT WING FUEL TANK CRACKED ON STIFFENER AT WBL 279.25 & RSS 352. REPAIRED STIFFENER IAW MT.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

RIGHT SIDE WING TO BODY FAIRING STRUCTURE T CHORD CRACKED AT BS 540. R & R T CHORD IAW EO & EA.

Part: STIFFENER — CRACKED (RT WING) · airframe 88,805 hrs · 65,804 cycles

RIGHT WING FUEL TANK UPPER SURFACE PANEL STIFFENER CRACKED AT WS 329.75, STRINGER 8. REPAIRED STIFFENER IAW EA.

Part: STIFFENER — CRACKED (LT WING) · airframe 88,805 hrs · 65,804 cycles

LEFT WING UPPER PANEL STIFFENER CRACKED AT WBL 329.75, STRINGER 7. REPAIRED STIFFENER IAW EO & EA.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 88,805 hrs · 65,804 cycles

LEFT VERTICAL STABILIZER ANGLE CRACKED AT LEVEL BS 1026. R & R ANGLE IAW SRM & DWG.

Part: STIFFENER — CRACKED (LT WING) · airframe 88,805 hrs · 65,804 cycles

LEFT WING FUEL TANK UPPER PANEL STIFFENER CRACKED AT WS 479, STRINGER 8. REPAIRED STIFFENER IAW EA.

Part: RIB — CRACKED (LT WING) · airframe 88,805 hrs · 65,804 cycles

LEFT WING RIB UPPER CHORD CRACKED AT WBL 114, STRINGER 2. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FUSELAGE FRAME CRACKED AT STATION 986.5, STRINGERS 20R. REPAIRED FRAME IAW EA.

Part: SKIN — DELAMINATED (AILERON TAB) · airframe 88,805 hrs · 65,804 cycles

LEFT WING AILERON TAB DELAMINATED ON LOWER SURFACE. REPAIRED TAB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FUSELAGE FRAME CRACKED AT STATION 500D, BETWEEN STRINGERS 23R & 24R. REPAIRED FRAME IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

STRINGER CRACKED BETWEEN BS 597 TO 616, STRINGER 15R. R & R STRINGER IAW SRM & DWG.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

TIE CLIP CORRODED AT BS 867, STRINGER 27R. R & R TIE CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FRAME CRACKED AT BS 947.5, STRINGER 26R. REPAIRED FRAME IAW EO & EA.

Part: SLAT — CRACKED (RT WING) · airframe 88,805 hrs · 65,804 cycles

RIGHT WING NR 5 SLAT CRACKED. REPAIRED SLAT IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FUSELAGE FRAME CRACKED AT STATION 947.5, STRINGERS 19R. REPAIRED FRAME IAW EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

AFT CARGO COMPARTMENT STRINGER CHANNEL CRACKED AT BS 727, STRINGER 21L. R & R CHANNEL IAW SRM & DWG.

Part: ANGLE — CRACKED (RT HORIZ STAB) · airframe 88,805 hrs · 65,804 cycles

RIGHT HORIZONTAL STABILIZER LOWER ANGLE INTERNAL CAVITY CRACKED ON STAB STATION 133.15. R & R ANGLE IAW SRM & DWG.

Part: STIFFENER — CRACKED (TE FLAP) · airframe 88,805 hrs · 65,804 cycles

RIGHT WING NR 6 FLAP TRACK CANOE FAIRING STIFFENER CRACKED. R & R STIFFENER IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FRAME WEB CRACKED AT BS 440, STRINGER 24R. REPAIRED FRAME IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

WEB CRACKED BETWEEN BS 294.5 TO 303.9, STRINGER 12L. R & R WEB IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 360, STRINGER 4R. R & R CHANNEL IAW EO.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FORWARD ENTRY DOOR CUT OUT STRUCTURE AFT UPPER REVEAL ANGLE CRACKED. R & R ANGLE IAW EO & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

ANGLE CRACKED AT BS 348, BETWEEN STRINGER 10L - 15L. R & R ANGLE IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

L1 DOOR UPPER HINGE CUT OUT H STRAP CRACKED. R & R CUT OUT IAW SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

STRINGER CRACKED BETWEEN BS 597 TO 616, STRINGER 15L. R & R STRINGER IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FRAME SECTION CRACKED AT BS 947.5, STRINGER 19L. R & R FRAME IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

TIE CLIP CRACKED AT BS 727B, STRINGER 19L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

TIE CLIP CRACKED AT BS 887, STRINGER 24L. R & R TIE CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

STUB FRAME CRACKED AT BS 294.5, STRINGER 7R. REPAIRED STUB FRAME IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

STRAP CRACKED AT BS 344, RBL 33. R & R STRAP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

STUB FRAME CRACKED AT BS 294.5, STRINGER 11R. R & R STUB FRAME IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

ANGLE CRACKED AT BS 294.5, STRINGER 7R. R & R ANGLE IAW SRM & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

STRINGER 27R CORRODED BETWEEN STATION 847 & 867. REPAIRED STRINGER IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

AFT CARGO COMPARTMENT FRAME CORRODED BETWEEN BS 827, BETWEEN STRINGER 27R - 27L. REPAIRED FRAME IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

STRINGER 27L CORRODED BETWEEN STATION 827 & 847. REPAIRED STRINGER IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 312, RBL 34. REPAIRED CHORD IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

AFT CARGO COMPARTMENT FRAME CORRODED AT BS 807, BETWEEN STRINGER 26L TO 25L. REPAIRED FRAME IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

STRINGER 27L CORRODED BETWEEN STATION 867 & 887. REPAIRED STRINGER IAW SRM.

Part: PLATE — CRACKED (VERTICAL STAB) · airframe 88,805 hrs · 65,804 cycles

VERTICAL STABILIZER ACCESS PANEL 9507 PLATE CRACKED. R & R PLATE IAW SRM & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

STRINGER 27R CORRODED BETWEEN STATION 867 & 887. REPAIRED STRINGER IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

AFT CARGO COMPARTMENT FRAME CORRODED AT BS 747, BETWEEN STRINGER 27R TO 27L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FUSELAGE FRAME CORRODED AT STATION 787, BETWEEN STRINGERS 27R & 27L. REPAIRED FRAME IAW EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

Z SUPPORT ANGLE CORRODED ON AFT ENTRY DOOR LOWER SILL. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FUSELAGE FRAME CORRODED AT STATION 787, BETWEEN STRINGERS 27L & 26L. REPAIRED FRAME IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FLOOR STRUCTURE WEB CRACKED AT BS 616, RBL 45.5. REPAIRED WEB IAW EA & EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

AFT CARGO COMPARTMENT FRAME CORRODED AT BS 747, BETWEEN STRINGER 27R TO 26R. REPAIRED FRAME IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

SUPPORT ANGLE CRACKED AT BS 639, STRINGER 17L. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FUSELAGE FRAME CORRODED AT STATION 787, BETWEEN STRINGERS 27R & 26L. REPAIRED FRAME IAW EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

CREASE BEAM INNER CHORD CRACKED AT BS 639, STRINGER 17R. REPAIRED CHORD IAW EO & EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

CHANNEL CRACKED AT BS 540, BETWEEN BL 0 TO RBL 24.7. R & R CHANNEL IAW SRM & DWG.

Part: SUPPORT — CRACKED (RT WING) · airframe 88,805 hrs · 65,804 cycles

RIGHT WING ANGLE SUPPORT CRACKED ON INBD & OTBD STABILIZING LINK WBL 114.0, BETWEEN THE MLG & THE REAR SPAR BRACKET. R & R SUPPORT IAW SRM & AMM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

CHANNEL CRACKED AT BS 540, BETWEEN BL 0 & LBL 24.75. R & R CHANNEL IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

AFT CARGO COMPARTMENT FRAME CORRODED AT BS 727B, BETWEEN STRINGER 26L TO 25L. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

L2 DOOR LOWER FWD SKIN CRACKED AT BS 947.5+14, STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

SKIN CORRODED BETWEEN BS 520 TO 540, BETWEEN STRINGER 28L TO 28R. R & R SKIN IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

SKIN CRACKED BETWEEN BS 900 TO BS 908, BETWEEN STRINGER 1 TO 4R. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

SKIN CRACKED AT BS 807+4, STRINGER 14R. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

SKIN CRACKED AT BS 500+5, STRINGER 15R. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

SKIN CRACKED AT BS 727B+4.5, STRINGER 14R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

SKIN CRACKED AT BS 500B+4, STRINGER 15R. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

SKIN CRACKED AT BS 440+14.5, STRINGER 16L. REPAIRED SKIN IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FRAME OUTER CHORD CRACKED AT BS 616, BETWEEN STRINGER 5R TO 18R. REPAIRED FRAME IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FRAME WEB CRACKED AT BS 639, STRINGER 17R. REPAIRED FRAME IAW EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

STUB BEAM CRACKED AT BS 616, BETWEEN STRINGER 5R - 18R. REPAIRED STUB BEAM IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FRAME WEB CRACKED AT BS 639, STRINGER 17L. REPAIRED FRAME IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

SKIN CRACKED AT BS 460+14.750, STRINGER 16L. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FRAME CRACKED AT BS 500D, BETWEEN STRINGER 20R TO 21R. REPAIRED FRAME IAW SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 88,805 hrs · 65,804 cycles

RIGHT MAIN WW PRESS DECK CRACKED AT BS 663.75, RBL 38.5. REPAIRED DECK IAW EO & EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 88,805 hrs · 65,804 cycles

MAIN WW PRESS DECK CRACKED AT BS 663.75, LBL 40.5. REPAIRED DECK IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

LEFT FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727, STRINGER 18A, ON AFT LOWER HOLE. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

LEFT FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727, STRINGER 18A, ON UPPER AFT HOLE. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

LEFT FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727, STRINGER 18A, ON FWD LOWER HOLE. REPAIRED CHORD IAW EA.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 88,678 hrs · 65,724 cycles

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

Part: SKIN — DELAMINATED (RUDDER) · airframe 88,489 hrs · 65,589 cycles

RUDDER UPPER HORN ADJACENT SKIN DELAMINATED. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 87,884 hrs · 65,138 cycles

R1 DOOR EXTERIOR EMER LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW AMM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 87,854 hrs · 65,115 cycles

SHEAR WEB BELOW AFT LAVATORY CUT OUT IN SHEAR WEB FOR DUMP TUBE CORRODED AROUND CUT OUT. R & R SHEAR WEB IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 87,854 hrs · 65,115 cycles

FLOORBEAM UPPER TEE CORRODED AT BS 1006 LBL 20. REPAIRED FLOORBEAM IAW SRM & EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 87,854 hrs · 65,115 cycles

CABIN FLOORBEAM TO WEB SUPPORT STIFFENER CRACKED AT BS 328 LBL 45. R & R STIFFENER IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 87,854 hrs · 65,115 cycles

FRAME ANGLE CRACKED AT BS 348 STRINGER 7R. R & R ANGLE IAW SRM & DWG.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 87,854 hrs · 65,115 cycles

PRESSURE BULKHEAD WEB CORRODED AT BS 1016 LBL 3. REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 87,854 hrs · 65,115 cycles

FUSELAGE FRAME CRACKED AT BS 340 STRINGER 6L. REPAIRED FRAME IAW SRM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 87,854 hrs · 65,115 cycles

AFT PRESS BULKHEAD WEB CORRODED AT BS 1016 BETWEEN BL 0 TO RBL 3. REPAIRED WEB IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 87,854 hrs · 65,115 cycles

AFT CARGO COMPARTMENT INTERCOSTAL CORRODED BETWEEN BS 927 TO 947 STRINGER 21L. R & R INTERCOSTAL IAW SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 87,854 hrs · 65,115 cycles

CABIN FLOORBEAM UPPER CHORD CRACKED AT BS 328 LBL 45. R & R CHORD IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,854 hrs · 65,115 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 927+6 TO 927+7 STRINGER 22L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,854 hrs · 65,115 cycles

SKIN CRACKED AT BS 500+6 STRINGER 19L. REPAIRED SKIN IAW SRM.

Part: TAB — DELAMINATED (RT AILERON) · airframe 87,659 hrs · 64,977 cycles

RIGHT WING AILERON TAB DELAMINATED. R & R AILERON TAB IAW MM.

Part: ROLL PIN — DEFECTIVE (COCKPIT) · airframe 87,422 hrs · 64,796 cycles

CAPTAIN`S ESCAPE ROPE LATCH INOPERATIVE. R & R ROLL PIN IAW SIP.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,352 hrs · 64,740 cycles

SKIN CRACKED AT BS 486, STRINGER 9R. REPAIRED SKIN IAW EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 87,314 hrs · 64,716 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 86,219 hrs · 63,956 cycles

FUSELAGE SKIN CRACKED AT BS 312+6 STRINGER 25R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 85,366 hrs · 63,322 cycles

FS CHEM MILL SKIN CRACKED AT BS 425, STRINGER 16R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 85,366 hrs · 63,322 cycles

FS CHEM MILL SKIN CRACKED AT BS 380+13, STRINGER 15L. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 85,366 hrs · 63,322 cycles

FS CHEM MILL SKIN CRACKED AT BS 380+13, STRINGER 15R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 85,366 hrs · 63,322 cycles

FS CHEM MILL SKIN CRACKED AT BS 927+13, STRINGER 4L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 85,366 hrs · 63,322 cycles

FS CHEM MILL SKIN CRACKED AT BS 492, STRINGER 16L. REPAIRED SKIN IAW ER & EA.

Part: LENS — MISSING (CABIN) · airframe 85,052 hrs · 63,080 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,786 hrs · 62,883 cycles

R2 DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED CUTOUT IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,801 hrs · 62,891 cycles

L2 DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED CUTOUT IAW SRM.

Part: HINGE — BROKEN (RT SPOILER) · airframe 84,474 hrs · 62,652 cycles

RIGHT WING NR 5 GROUND SPOILER HINGE BROKEN. R & R GROUND SPOILER IAW MM.

Part: PUMP — FAULTY (HYDRAULIC SYS) · airframe 84,337 hrs · 62,548 cycles

DECLARED EMERGENCY - "B" SYS HYD FAILURE. GOT A LOW PRESS LIGHT ON B SIDE ENGINE & PUMP 1ST, THEN LOW PRESS LIGHT B SIDE ELEC CAME ON B HYD QTY BETWEEN 1/4 & 1/2. REMOVED AND REPLACED HOSE, "B" ELEC PUMP AND NR 2 ENGINE DRIVEN PUMP, "B" SYSTEM RETURN FILTER, CASE DRAIN FILTER AND ENGINE CASE DRAIN FILTER.

Part: SUPPORT BRACKET — CRACKED (RT MLG WW) · airframe 84,248 hrs · 62,478 cycles

RIGHT MAIN WHEEL WELL SUPPORT BRACKET CRACKED AT BS 727-10 +21" FROM CENTER OF KEEL BEAM. REPAIRED BRACKET PER SRM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 84,155 hrs · 62,405 cycles

R1 WINDOW CRACKED AND ARCED. REMOVED AND REPLACED R1 WINDOW AND HEAT CONTROLLER IAW AMM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CRACK ON CHANNEL LOCATED AT BS 203.8 RBL 3.2 AND WL 174.8 LOWER NOSE COMPARTMENT. REPLACED CHANNEL LOCATED AT BS 203.8 RBL 3.2 AND WL 174.8 LOWER NOSE COMPARTMENT AND FASTENERS IAW B737-300 SRM 51-40-02 AND SRM 51-10-02 AND DRAWING 65C26143.

Part: WEB — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CRACK ON WEB LOCATED BS 277 TO BS 294.5 AND STRINGER 14R PAX CABIN. REPLACED WEB LOCATED BS 277 TO BS 294.5 AND STRINGER 14R PAX CABIN IAW SRM B737-300 51-10-02 ITEM 8 AND DWG 65-45807.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CRACK ON TIE CLIP LOCATED BS 277 AND STRINGER 15R PAX CABIN. REPLACED TIE CLIP LOCATED BS 727 AND STRINGER 15R PAX CABIN IAW SRM B737-300 51-10-02 ITEM 8 AND DWG 65-45805.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CRACK ON FRAME LOCATED BS 277 BETWEEN STR 14R TO STR 15R PAX CABIN. REPLACE FRAME (WEB MID SIDE) LOCATED BS 277 BETWEEN STR 13R TO STR 18R IAW SRM B737-300 51-10-02 ITEM 8 AND DWG 65-45805.

Part: WEB — CRACKED (NLG WW) · airframe 83,825 hrs · 62,173 cycles

WEB CRACKED AT BS 228.5 AND BL0 WL186 INTERNAL AREA OF NOSE W/W. R & R WEB IAW SRM AND DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CRACK ON STRINGER 16L AT BS 500C +16" INTERNAL AREA PAX CABIN FUSELAGE. REPLACED STRINGER 16L LOCATED BETWEEN BS 500C+15" TO BS 540 IAW SRM B737-300 51-10-02 AND 51-40-02.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CRACK ON SHEAR TIE LOCATED AT BS 520 AND BETWEEN STR 16L TO STR 17L PAX CABIN. REPLACED SHEAR TIE LOCATED AT BS 520 AND BETWEEN STR 16L TO STR 17L PAX CABIN IAW SRM B737-300 51-10-02 AND 51-40-02 DRAWING 65-46534.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 83,825 hrs · 62,173 cycles

CRACK ON ANGLE ON INTERNAL AREA OF RIGHT EMERGENCY EXIT DOOR. REPLACED ANGLE ON INTERNAL AREA OF RIGHT EMERGENCY EXIT DOOR IAW B737-300 51-10-02 ITEM 8 AND 51-40-02 AND DRAWING 50-7978.

Part: PLATE — CRACKED (FAIRING) · airframe 83,825 hrs · 62,173 cycles

CRACK ON PLATE LOCATED WING TO BODY FAIRING RIGHT AFT. REPLACED PLATE LOCATED WING TO BODY FAIRING RIGHT AFT IAW SRM B737-300 51-10-02 ITEM 8.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

SHEAR TIE CORRODED AT BS 312 BETWEEN STR 28L TO 27L E/E COMPARTMENT. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

SHEAR TIE CORRODED AT BS 312 BETWEEN STR 28L TO 27L E/E COMPARTMENT. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

SHEAR TIE CORRODED AT BS 312 BETWEEN STR 28L TO 28R E/E COMPARTMENT. REPAIRED SHEAR TIE IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

STRAP CRACKED BETWEEN BS 328 TO 344, LBL 45.5 E/E COMPARTMENT. R & R STRAP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

SHEAR TIE CORRODED AT BS 312 BETWEEN STR 28L TO 28R E/E COMPARTMENT. REPAIRED SHEAR TIE IAW SRM.

Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 83,825 hrs · 62,173 cycles

CRACK ON ANGLE LOCATED ON OUTBOARD SIDE PYLON NR 2 NAC STA 255.72. REPLACED ANGLE IAW SRM B737-300 51-10-02 ITEM 8 AND DRAWING 311A1680.

Part: SKIN — CORRODED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

SKIN CORRODED AT BS 360 BETWEEN STR 28R TO 28L E/E COMPARTMENT. REPAIRED SKIN IAW EO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CORROSION ON SHEAR TIE LOCATED BS 360 AFT AND FWD FACE BETWEEN STR 27L TO STR 28L E/E COMPARTMENT. REPLACED SHEAR TIE LOCATED BS 360 BETWEEN STR 27L TO 28L E/E COMPARTMENT IAW SRM B737-300 51-10-02 AND DRAWING 65-58280.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CRACK INDICATION FOUND IN THE FUSELAGE SKIN ALONG THE CHEM-MILL STEP LOCATED ABOVE STR 13R AND BS 500D+12" CRACK LENGTH 1.3" APPROX. REPAIRED FUSELAGE SKIN ALONG THE CHEM-MILL STEP LOCATED ABOVE STR 13R AND BS 500D+12" CRACK LENGTH 1.3" APPROX IAW EO AEM-HC53-026/13 R0 AND EA 1-353- 21786, FOR INSPECTION SEE TLD T037051.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CRACK INDICATION FOUND IN THE FUSELAGE SKIN ALONG THE CHEM-MILLED STEP LOCATED ABOVE STR 15L AND BS S00D+3" CRACK LENGTH:1.5" APPROX. REPAIRED FUSELAGE SKIN IAW EO AEM-HC53-022/13 R0 AND EA 1-353-21716 REV 0.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CRACK FOUND ON EXTERNAL SKIN AT THE CHEM-MILLED STEP LOCATED AT BS 500D + 4.5" BELOW STR 15 L, CRACK LENGHT APROX. = 1.8". REPAIRED FUSELAGE SKIN IAW EO AEM-HC53-022/13 R0 AND EA 1-353-21716 REV 0.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CRACK FOUND ON EXTERNAL SKIN AT THE CHEM-MILLED STEP LOCATED BS 500D+12" ABOVE STR 13L CRACK LENGHT APPROX=1.4". REPAIRED FUSELAGE SKIN IAW EO AEM-HC53-022/13 R0 AND EA 1-353-21716 REV 0.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CRACK FOUND ON EXTERNAL SKIN AT THE CHEM-MILLED STEP LOCATED AT BS 500D+2" ABOVE STR 12L CRACK LENGHT APPROX=1.8". REPAIRED FUSELAGE SKIN IAW EA 1-353-21716 REV 0.

Part: SKIN — CANNING (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

OIL CAN ON EXTERNAL FUSELAGE SKIN BETWEEN BS 727E TO 747 AND STR 25R TO 26R LOWER LOBE FUSELAGE. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

SKIN CRACKED AT THE CHEM-MILLED STEP BS 500C + 13" AND ABOVE STR 9L. REPAIRED SKIN IAW EO.

Part: NUT PLATE — CRACKED (R2 DOOR) · airframe 83,825 hrs · 62,173 cycles

R2 DOOR ESCAPE SLIDE SUPPORT BRACKET NUT PLATE CRACKED. R & R PLATE IAW SRM AND DWG.

Part: SEAL — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

DURING THE REMOVAL OF DOOR WAY LINNING, CRACK WAS FOUND ON RETAINER TRIM SEAL LOCATED ON AFT SIDE FWD ENTRY DOOR CUTOUT AT BS 351. REMOVED AND REPLACED RETAINER TRIM SEAL LOC ON AFT SIDE FWD ENTRY DOOR CUTOUT AT BS 351 IAW SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CORROSION ON STRINGER 27L AT BS 1006 IN AFT CARGO COMPARTMENT. REPAIRED STRINGER 27L BETWEEN BS 986.5 TO BS 1016 IN AFT CARGO COMPARTMENT IAW B737-300 SRM 53-00-03- 2R REPAIR 1 DETAIL VI.

Part: SUPPORT BRACKET — CRACKED (R2 DOOR) · airframe 83,825 hrs · 62,173 cycles

CRACK ON SUPPORT BRACKET ESCAPE SLIDE AFT SERVICE DOOR FWD POSITION. REPLACED SUPPORT BRACKET ESCAPE SLIDE AFT SERVICE DOOR FWD POSITION IAW B737-300 SRM 51-40-02.

Part: WEB — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

WEB CRACKED BETWEEN BS 787 TO 807 RBL 17 AT LEVEL MAIN DECK FLOOR STRUCTURE IN CARGO COMPARTMENT. R & R WEB IAW SRM AND DWG.

Part: BULKHEAD — PUNCTURED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

PUNCTURE ON BULKHEAD BS 227.8 BL 0 WL 186 LOWER NOSE COMPARTMENT. REPAIRED BULKHEAD LOWER WEB BS 227.8 BETWEEN WL 180/ WL 190 AND BL 0 IAW EO N. AEM-HC53-012/13 R0 AND EA N. 1-353-21731 R0 FOR INSPECTION REQUIRED SEE TLD #T027942.

Part: RETAINER — CRACKED (LT WING) · airframe 83,825 hrs · 62,173 cycles

CRACK ON RETAINER LOCATED ON INBOARD FIXED TRAILING EDGE AT WBL 92.50 LEFT WING. REPLACED RETAINER LOCATED ON INBOARD FIXED TRAILING EDGE AT WBL 92.50 LEFT IAW B737-300 SRM 51-10-02 AND DRAWING 65-50820.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

INTERCOSTAL CRACKED AT STR 7L BETWEEN BS 294.5 TO 303 ENTRY DOOR SURROUND STRUCTURE. R & R INTERCOSTAL IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

WEB CRACKED AT LEVEL OF STR 11L BETWEEN BS 294.5 TO 303 ENTRY DOOR SURROUND STRUCTURE. R & R WEB IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CRACK ON STRAP LOCATED ON BS 312 BBL 0 E/E COMPARTMENT UPPER SURFACE. REPLACED STRAP LOCATED ON BS 312 BBL 0 E/E COMPARTMENT UPPER SURFACE IAW B737-300 SRM 51-10-02 ITEM 8, SRM 51-40-02 AND DRAWING 6545834.

Part: ANGLE — CRACKED (LT WING) · airframe 83,825 hrs · 62,173 cycles

CRACK ON ANGLE LOCATED ON TRACK FAIRING IN BOARD SIDE AT WBL 183.40 OF LEFT WING. REPLACED ANGLE LOCATED ON TRACK FAIRING INBOARD SIDE AT WBL 183.40 OF LEFT WING IAW B737-300 SRM 51-10-02 ITEM 8 AND SRM 51-40-02 AND DRAWING 65-50820.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 83,825 hrs · 62,173 cycles

RT WING FIXED T/E EDGE UPPER ACCESS PANEL NR 5835R SUPPORT ANGLE CRACKED. R & R ANGLE SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 83,825 hrs · 62,173 cycles

CRACK ON SUPPORT ANGLE LOCATED ON TRACK FAIRING OUTBOARD SIDE AT WBL 198.60 LEFT WING. REPLACED SUPPORT LOCATED ON TRACK FAIRING OUTBOARD SIDE AT WBL 198.60 LEFT WING IAW SRM B737-300 51-10-02 ITEM 8, SRM B737-300 51-40-02 AND DRAWING 65C26300.

Part: SUPPORT ANGLE — CRACKED (TE FLAP) · airframe 83,825 hrs · 62,173 cycles

CRACK ON SUPPORT ANGLE LOCATED ON TRACK FAIRING INBOARD SIDE TRAILING EDGE OF LT WING. REPLACED SUPPORT ANGLE LOCATED ON TRACK FAIRING INBOARD SIDE TRAILING EDGE OF LEFT WING IAW B737-300 SRM 51-10-02 ITEM 8, SRM 51-40-02 AND DWG 65C26300

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 83,825 hrs · 62,173 cycles

RT WING FIXED T/E EDGE UPPER ACCESS PANEL NR 5714R SUPPORT ANGLE CRACKED. R & R SUPPORT IAW SRM AND DWG.

Part: REPAIR — CORRODED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CORRODED AT BS 887 AND BETWEEN STR 26R TO 27R CARGO COMPARTMENT. REMOVED AND REPLACED REPAIR IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CORROSION ON STR 28L BETWEEN BS 460 TO BS 480 FWD CARGO COMPARTMENT. REPAIRED STR 28L BETWEEN BS 460 TO BS 480 FWD CARGO COMPARTMENT IAW SRM B737-300 53-00-03-2R-1 REPAIR 1 DETAIL VII SRM B737-300 51-40-02.

Part: FRAME — CORRODED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CORRODED ON FRAME BS 500C BETWEEN STR 28L TO 28R CARGO COMPARTMENT. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CRACK ON SHEAR TIE LOCATED BS 520 BETWEEN STR 21L TO STR 22L. REPAIRED SHEAR TIE LOCATED AT BS 520 BETWEEN STR 21L TO STR 22L IAW B737-300 SRM 53-00-07 2R-7 FOR RE-INSPECTION REQUIREMENTS SEE TLD T027914.

Part: PANEL — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CRACK ON BULKHEAD PANEL 1542 IN CARGO COMPARTMENT. REPAIRED PANEL IAW AMM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CORROSION ON STR 26R BETWEEN BS 807 TO BS 827 AFT CARGO COMPARTMENT. REPAIRED STRINGER 26R BETWEEN BS 807 TO BS 827 AFT CARGO COMPARTMENT IAW SRM B737-300 53-00-03-2R-1 REPAIR 1 AND EO AE-HC53-024/13 R0 AND EA 1-353-21648.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27R TO STR 26R. REPAIRED SHEAR TIE IAW SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 83,825 hrs · 62,173 cycles

DELAMINATION AT 29" FROM INBOARD END OF INBOARD AFT FLAP R/T WING. REPAIRED AT 29" FROM INBOARD END OF INBOARD AFT FLAP R/T WING IAW B737-300 SRM 51-70-10-2R-0.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CRACK ON ANGLE LOCATED BS 727 INTERNAL AREA OF LEFT MAIN LANDING GEAR BAY BULKHEAD. REPLACED ANGLE LOCATED BS 727 INTERNAL AREA OF LEFT MAIN LANDING GEAR BAY BULKHEAD IAW B737-300 SRM 51-10-02 ITEM 8, SRM 51-40-02 AND DWG 65-44547.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CORROSION ON STRINGER 26L BS 787 AFT CARGO COMPARTMENT. REPAIRED STRINGER 26L BETWEEN BS 767 TO BS 807 AFT CARGO COMPARTMENT IAW SRM B737-300 53-00-03-2R-1 REPAIR 1 TABLE I FIG 201, SHEET 4 AND SRM B737-300 51-40-02

Part: FRAME — CORRODED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

FRAME CORRODED AT BS 747 AND BETWEEN STR 25L TO 26L CARGO COMPARTMENT. REPAIRED FRAME IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CRACK ON SHEAR TIE LOCATED BS 520 BETWEEN STR 21L TO STR 22L. REPAIRED SHEAR TIE LOCATED AT BS 520 BETWEEN STR 21L TO STR 22L IAW B737-300 SRM 53-00-07 2R-7.

Part: FRAME — CORRODED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CORRODED ON FRAME BS 500C BETWEEN STR 28L TO 28R CARGO COMPARTMENT. REPAIRED FRAME IAW SRM.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CORRODED ON BEAR STRAP AT LEVEL BS 492 AND BETWEEN STR 28R TO 27R CARGO COMPARTMENT. REPAIRED SKIN IAW EO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CORROSION ON SHEAR TIE LOCATED AT BS 827 AND BETWEEN STR 27R TO STR 26R AFT CARGO COMPARTMENT. REPLACED SHEAR TIE LOCATED AT BS 827 AND BETWEEN STR 26R TO STR 27R AFT CARGO COMPARTMENT IAW SRM B737-300 51-10-02 ITEM 8 AND DRAWING 65-46552.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CRACK ON CHANNEL BETWEEN BS 492 TO 500A AT LEVEL STR 26R CARGO COMPARTMENT. REPLACED CHANNEL IAW SRM AND DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CORROSION ON EXISTING REPAIR LOCATED AT BS 887 AND BETWEEN STR 26R TO STR 27R AFT CARGO COMPARTMENT. REPLACED EXISTING REPAIR LOCATED AT BS 887 AND BETWEEN STR 26R TO STR 27R AFT CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 AND 51-40-02 DWG 65-46557 FOR

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CRACK ON EXTERNAL SKIN, FWD GALLEY DOOR CUTOUT, FWD LOWER CORNER L APPROX 0.26" DOOR CUTOUT. REPAIRED EXTERNAL SKIN AT FWD GALLEY DOOR CUTOUT FWD LOWER CORNER BETWEEN BSTA 290 TO BSTA 315 AND FROM S-15R TO S-20R IAW EO AEM-HC53-011/13 AND EA N. 1-353-21730 REV 1 FOR INSPECTION SEE TLD #T027944.

Part: WEB — CRACKED (NLG WW) · airframe 83,825 hrs · 62,173 cycles

NLG W/W AROUND FASTENER HEAD CRACKED AT BS 251.6, WL 169.1+7. REPAIRED WEB IAW SRM.

Part: SEAL DEPRESSOR — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

DEPRESSOR SEAL CORNER CRACKED AT AIRSTAIRS DOOR. REPLACED SEAL IAW SRM AND DWG.

Part: STRIP — CRACKED (AC BAY) · airframe 83,825 hrs · 62,173 cycles

CRACK ON STRIP LOCATED AT FWD EDGE OF AIR CONDITIONING ACCESS DOOR LEFT SIDE. REPLACED STRIP LOCATED AT FWD EDGE OF AIR CONDITIONING ACCESS DOOR LEFT IAW B737-300 SRM 51-40-02, SRM 51-10-02 ITEM8 AND DWG 65-48685.

Part: SKIN — CRACKED (KRUEGER FLAP) · airframe 83,825 hrs · 62,173 cycles

CRACK ON FIXED LEADING EDGE SKIN AT KRUEGER FLAP SEAL DOOR CUTOUT AT LES 213. REPAIRED FIXED LEADING EDGE SKIN AT KRUEGER FLAP SEAL DOOR CUTOUT AT LES 213 IAW EA 1-A57-0503 REV 4.

Part: WEB — CRACKED (NLG WW) · airframe 83,825 hrs · 62,173 cycles

NLG W/W AROUND FASTENER HEAD CRACKED AT BS 251.6, WL 169.1+8. REPAIRED WEB IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 83,825 hrs · 62,173 cycles

DELAMINATION WAS FOUND ON OUTBOARD AND LOWER CORNER OF OUTBOARD AFT FLAP LEFT WING. REPAIRED OUTBOARD AND LOWER CORNER OF OUTBOARD AFT FLAP LEFT WING IAW B737-300 SRM 51-70-10-2R-0

Part: WEB — CRACKED (NLG WW) · airframe 83,825 hrs · 62,173 cycles

NLG W/W AROUND FASTENER HEAD CRACKED AT BS 251.6, WL 169.1+6. REPAIRED WEB IAW SRM.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 83,825 hrs · 62,173 cycles

CRACK ON ANGLE ON INTERNAL AREA OF RIGHT EMERGENCY EXIT DOOR. REPLACED ANGLE LOCATED ON INTERNAL AREA OF RIGHT EMERGENCY EXIT DOOR IAW SRM B737-300 51-10-02 ITME 8 AND INSTALLED FASTENERS IAW SRM B737-300 51-40-02 AND DRAWING 50-7978.

Part: SKIN — CRACKED (R1 DOOR) · airframe 83,825 hrs · 62,173 cycles

CRACK ON EXTERNAL SKIN LOCATED BS 312 BETWEEN STR 11R OF FWD GALLEY DOOR. REPAIRED EXTERNAL SKIN FWD GALLEY DOOR UPPER HINGE CUTOUT BS 312 STR 11R IAW EO AEM-HC52-001/13 REV 0 AND EA 1-352-1313 R0.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CRACK ON SUPPORT ANGLE LOCATED AT BS 540 AT LEVEL OF STR 24L AIR CONDITIONING BAY. REPLACED SUPPORT ANGLE LOCATE AT BS 540 AT LEVEL OF STR 24L AIR CONDITIONING BAY IAW SRM B737-300 51-40-02 ITEM 8 AND 51-40-02 AND DRAWING 65-48608.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 83,825 hrs · 62,173 cycles

CRACK ANGLE ON INTERNAL AREA OF LEFT EMERGENCY EXIT DOOR. REPLACED ANGLE LOCATED ON INTERNAL AREA OF LEFT EMERGENCY DOOR IAW B737-300 SRM 51-10-02 ITEM 8 AND INSTALLED FASTENER IAW SRM B737-300 51-40-02 AND DRAWING 50-7978

Part: STRIP — CRACKED (AC BAY) · airframe 83,825 hrs · 62,173 cycles

CRACK ON STRIP LOCATED AT BS 540 AT LEVEL OF STR 26L AIR CONDITIONING BAY. REPLACED STRIP LOC AT BS 540 AT LEVEL OF STR 26L AIR CONDITIONING BAY IAW B737-300 SRM 51-40-02 AND SRM B737-300 51-10-02 ITEM 8 AND DRAWING 65-48670.

Part: STRIP — CRACKED (AC BAY) · airframe 83,825 hrs · 62,173 cycles

CRACK ON STRIP LOCATED AT BS 540 AT LEVEL OF STR 23R AIR CONDITIONING BAY. REPLACED STRIP, LOC AT BS 540 AT LEVEL OF STR 23R AIR CONDITIONING BAY IAW B737-300 SRM 51-40-02 AND SRM B737-300 51-10-02 ITEM 8 AND DRAWING 65-48670.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

NLG W/W AROUND FASTENER HEAD CRACKED AT BS 243.7+3, WL 169.1. REPAIRED SKIN IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CRACK ON OVAL HOLE LOCATED IN THE LBL 24.5 LONGITUDINAL FLOORBEAM UPPER CHORD BS667 PAX CABIN. REPAIRED CHORD AND WEB IAW EO AEM-HC57-002/13 R0 AND EA 1-357-7903.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

CRACK ON TIE CLIP LOCATED BS 312 AND STR 18R INTERNAL AREA E/E COMPARTMENT. REPLACED TIE CLIP LOCATED BS 312 AND STR 18R INTERNAL AREA E/E COMPARTMENT IAW SRM B737-300 51-10-02 ITEM 8 AND DWG 65-45810.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,825 hrs · 62,173 cycles

FUSELAGE SKIN CRACKED AT BS 727D+5, STR 20L. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,676 hrs · 62,060 cycles

EMERGENCY LIGHT IN BULLNOSE AT SEAT 12 DEF INOP. RELAMPED PER M/M OPS CHECK GOOD PER M/M.

Part: LENS — BROKEN (CABIN) · airframe 82,829 hrs · 61,437 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,699 hrs · 61,341 cycles

SKIN CRACKED AT BS 500B+18, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,699 hrs · 61,341 cycles

SKIN CRACKED AT BS 939, STR 21R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,699 hrs · 61,341 cycles

SKIN CRACKED AT BS 913, STR 22L. REPAIRED SKIN PER SRM.

Part: ACTUATOR — BROKEN (RT SPOILER) · airframe 81,866 hrs · 60,700 cycles

RIGHT WING INBOARD GROUND SPOILER NR 5 BROKEN OUTBOARD ACTUATOR. REMOVED AND REPLACED ACTUATOR PER M/M.

Part: LUG — BROKEN (NR 4 SPOILER) · airframe 81,796 hrs · 60,646 cycles

LEFT WING NR 4 GROUND SPOILER BOARD O/B LUG BROKEN. REMOVED AND REPLACED SPOILER PER AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 81,796 hrs · 60,646 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER AMM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 81,796 hrs · 60,646 cycles

L2 DOOR EMERGENCY EVAC SLIDE COVER AFT GIRT BAR STOW HOOK LOOSE. SECURED HOOK PER AMM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 81,796 hrs · 60,646 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER AFT GIRT BAR STOW HOOK LOOSE. SECURED HOOK PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 81,796 hrs · 60,646 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITIONED. REPOSITIONED SLIDE PER AMM.

Part: SENSOR — LOOSE (MLG WW) · airframe 81,819 hrs · 60,662 cycles

NEITHER THRUST REVERSER WOULD DEPLOY DURING LANDING. FOUND DOWNLOCK SENSOR LOOSE & OUT OF RANGE. ADJUSTED SENSOR IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 81,620 hrs · 60,511 cycles

FUSELAGE SKIN CRACKED AT STA 747+5STR, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 81,620 hrs · 60,511 cycles

FUSELAGE SKIN CRACKED AT STA 787+5.5, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 81,620 hrs · 60,511 cycles

FUSELAGE SKIN CRACKED AT STA 767+13, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 81,620 hrs · 60,511 cycles

FUSELAGE SKIN CRACKED AT STA 727E +15.5, STR 19L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 81,620 hrs · 60,511 cycles

STRINGER CLIP DAMAGED AT STA 520, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 81,620 hrs · 60,511 cycles

FUSELAGE SKIN CRACKED AT STA 500C+5 ABOVE STR 15R. REPAIRED PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 81,617 hrs · 60,510 cycles

FUSELAGE SKIN CRACKED AT BS 500C + 5, STR 15R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 81,224 hrs · 60,221 cycles

FRAME CRACKED AT 500C, STR 21R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 81,220 hrs · 60,217 cycles

FRAME CRACKED AT BS 500C ON I/B RIGHT SIDE. REPAIRED FRAME PER SRM.

Part: SIGN — LOOSE (CABIN) · airframe 80,614 hrs · 59,773 cycles

DURING SCHEDULED CV CHECK, FOUND FWD GALLEY CENTER UPPER EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 80,380 hrs · 59,596 cycles

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

Part: BULKHEAD — CRACKED (NLG WW) · airframe 79,689 hrs · 59,055 cycles

DURING SCHEDULED OTS CHECK, FOUND NOSE WHEEL WELL RT VERTICAL BULKHEAD CRACKED BETWEEN BS 235.825 TO BS 251.625. REPAIRED BULKHEAD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,689 hrs · 59,055 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 294.5+9, BETWEEN STR 17L TO STR 18L. REPAIRIED SKIN IAW SRM.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 79,706 hrs · 59,067 cycles

DURING SCHEDULED OTS CHECK, FOUND NOSE WHEEL WELL SKIN PANEL CRACKED BETWEEN BS 235.825 TO BS 251.625. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,689 hrs · 59,055 cycles

DURINGS SCHEDULED OTS CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,687 hrs · 59,054 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 294.5, BETWEEN STR 17L TO STR 18L. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 79,687 hrs · 59,054 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING T/E FLAP DELAMINATED. REMOVED AND REPLACED FLAP IAW MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 79,687 hrs · 59,054 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 79,218 hrs · 58,670 cycles

OVERHEAD PANEL EMERGENCY EXIT LIGHT MISSING. INSTALLED LIGHT PER MM.

Part: SUPPORT FITTING — FAULTY (ELEVATOR TAB) · airframe 79,201 hrs · 58,653 cycles

DIVERSION - EXCESSIVE AIRCRAFT VIBRATION EN ROUTE - VIBRATION FELT BY AFT FLIGHT ATTENDANT. DID NOT EXCEED 1.0 ON ENG VIBRATION - VVI INDICATOR DID NOT REVERT TO TA/RA AFTER TAKEOFF INDICATING SQUAT SWITCH (GROUND SENSOR) PROBLEM. REMOVED AND REPLACED RT ELEVATOR CONTROL TAB NR 1 SUPPORT FITTING IAW MM.

Part: LATCH — LOOSE (L1 DOOR) · airframe 78,920 hrs · 58,433 cycles

L1 DOOR EMERGENCY ESCAPE SLIDE LATCH LOOSE. SECURED LATCH PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 662, BBL 0. REPAIRED BEAM PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, LBL 3. REPAIRED SHEAR TIE PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 930, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT LOWER AFT CORNER. REMOVED AND REPLACED SKIN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 960, STR 21L. REPAIRED SKIN PER EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 460, BETWEEN STR 13L TO STR 14L. REPAIRED SHEAR TIE PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER CORNER CUTOUT, BS 952, STR 17R. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM LOWER CHORD CRACKED AT BS 664.5, RBL 44.5. REPAIRED BEAM PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 986, STR 20L. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 871 TO BS 878, STR 26R. REPAIRED STRINGER PER ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 460, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 668, BBL 0.07. REPAIRED BEAM PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 14R. REMOVED AND REPLACED SKIN PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM ANGLE CRACKED AT BS 639, LBL 45.5. REPAIRED ANGLE PER ER AND EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT FWD CARGO COMPARTMENT SKIN CORRODED AT BS 500D+17. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 271, STR 16R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 937, STR 23R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT KEEL BEAM CORRODED AT BS 540. REMOVED AND REPLACED KEEL BEAM SECTION PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 520, BETWEEN STR 27R TO STR 28R. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24YCHECK, FOUND STRINGER CRACKED AT BS 986, STR 22L. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 794, STR 18L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED BETWEEN BS 749 TO BS 752, STR 18L. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 616, BETWEEN STR 7L TO STR 8L. REPAIRED SHEAR TIE PER ER AND EA.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT FLOOR SUPPORT SPLICE CORRODED AT BS 727D+6, RBL 3. REPAIRED SPLICE PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 947, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 14L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 23R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, BETWEEN LBL 5 TO RBL 5. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 847, LBL 1. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 770, STR 18L. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 907, BETWEEN LBL 1 TO LBL 5. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, BETWEEN STR 5L TO STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 480, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND CORROSION STA 771D, RBL 3 AFT PIT FLOOR SPLICE. REPAIRED PER EA.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 78,788 hrs · 58,332 cycles

DURING SCHEDULED 24Y CHECK, FOUND CORROSION STA 727D +6, LBL 3 AFT PIT FLOOR SPLICE. REPAIRED PER EA.

Part: BALLAST — FAULTY (CABIN) · airframe 78,776 hrs · 58,324 cycles

FLIGHT ATTENDANT NOTED ELECTRICAL ODOR MID CABIN, IT DISSIPATED WITH PACKS ON HIGH RECIRC AND GASPER FANS OFF. FOUND RT SIDEWALL LIGHT INOP AT ROW 12 CAUSE OF SMELL. REMOVED AND REPLACED BALLAST FOR SIDEWALL LIGHT PER MM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 78,741 hrs · 58,300 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 77,700 hrs · 57,552 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT RT EMERGENCY EXIT BULLNOSE LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: HINGE FITTING — BROKEN (SPOILER) · airframe 76,791 hrs · 56,859 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING NR 4 GROUND SPOILER HINGE FITTING BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,141 hrs · 56,360 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 745E, STR 23R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,141 hrs · 56,360 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 506D, STR 15R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,141 hrs · 56,360 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 517D, STR 16L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 88,805 hrs · 65,804 cycles

FUSELAGE SKIN CRACKED AT STATION 500D+ 17, STRINGER 16L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,727 hrs · 55,291 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 937, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 930 S23L) · airframe 74,727 hrs · 55,291 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 930, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 937 S23R) · airframe 74,727 hrs · 55,291 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 937, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,727 hrs · 55,291 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 930, STR 23L. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 74,670 hrs · 55,255 cycles

DURING SCHEDULED MV2 CHECK, FOUND FLOORBEAM T-CAP CRACKED AT BS 312. REMOVED AND REPLACED T-CAP PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,121 hrs · 54,843 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,052 hrs · 54,790 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 986, STR 27R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,052 hrs · 54,790 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 767, STR 22R. REPAIRED SKIN PER EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 74,052 hrs · 54,790 cycles

DURING SCHEDULED SPV CHECK, FOUND RT KEEL BEAM CORRODED FROM BS 520 TO BS 525. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,052 hrs · 54,790 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 740D, STR 21R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,115 hrs · 54,837 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 740D, STR 21R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,115 hrs · 54,837 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 767, STR 22R. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, BETWEEN RBL 42 TO RBL 46. REPAIRED BEAM PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED BETWEEN BS 277 TO BS 291, STR 10R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 13R. REPAIRED FRAME PER PAE EA.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BS 291, WL 233. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 887, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND PRESSURE DOME WEB CRACKED AT BS 1016, STR 6L. REPAIRED WEB PER SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT, BS 291, WL 259. REPAIRED SKIN PER ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 819 TO BS 827, STR 26L. REPAIRED STRINGER PER SRM.

Part: TAB — DELAMINATED (AILERON) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING AILERON TAB O/B END DELAMINATED. REPAIRED AILERON PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 670, RBL 24. REPAIRED BEAM PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767 BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 303, WL 238. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BS 290, WL 235. REPAIRED SKIN PER ER.

Part: FLAP — DELAMINATED (RT WING) · airframe 73,182 hrs · 54,180 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 45. REPAIRED BEAM PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 987, BETWEEN STR 19R TO STR 20R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CORRODED BETWEEN BS 360 TO BS 363, STR 28L. REMOVED AND REPLACED SPLICE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 13R. REPAIRED FRAME PER PAE EA.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING TRAILING EDGE O/B FORE FLAP TRAILING EDGE WEDGE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 13L. REPAIRED FRAME PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 819 TO BS 827, STR 26L. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CORRODED AT BS 360, STR 28R. REPAIRED STRINGER PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT NOSE WHEEL WELL CEILING ACCESS DOOR CUTOUT CRACKED. REPAIRED SKIN PER ACO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 887, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING I/B MIDFLAP T/E WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING NR 1 SLAT SKIN CRACKED AT O/B END. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 360 TO BS 363, STR 28R. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 767, STR 13L. REPAIRED FRAME PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 360, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED BETWEEN BS 727B TO BS 727C, STR 24L. REPAIRED SKIN PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 847, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 500D, STR 13R. REPAIRED FRAME PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 727C TO BS 747, STR 23L. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: CAP — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT BULKHEAD DOME CAP CRACKED AT BS 1016, STR 23R. REPAIRED DOME CAP PER SRM.

Part: CAP — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT BULKHEAD DOME CAP CRACKED AT BS 1016, STR 15R. REPAIRED DOME CAP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 24. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L TO STR 9L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L TO STR 9L. REPAIRED FRAME PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,182 hrs · 54,180 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 887, STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,912 hrs · 53,259 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR LOWER HINGE CUTOUT SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,912 hrs · 53,259 cycles

DURING SCHEDULED C4 CHECK, FOUND SKIN CRACKED AT STR 24L, STA 908 + 3. REPAIRED SKIN PER SRM.

Part: SEAL — TORN (FLASHLIGHT) · airframe 71,912 hrs · 53,259 cycles

EMERGENCY FLASHLIGHT SEAL TORN. REMOVED AND REPLACED SEAL PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 71,788 hrs · 53,178 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: SLIDE — DISCHARGED (L1 DOOR) · airframe 71,679 hrs · 53,099 cycles

L1 DOOR EMERGECNY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: VALVE — INOPERATIVE (NLG STEERING) · airframe 71,608 hrs · 53,052 cycles

RETURN TO GATE. NLG STEERING INOP, LOCKED HARD RIGHT. REMOVED AND REPLACED METERING VALVE PER MM.

Part: LENS — CRACKED (CABIN) · airframe 70,542 hrs · 52,285 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,416 hrs · 52,189 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737E, STR 22L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 70,266 hrs · 52,074 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 69,931 hrs · 51,826 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,889 hrs · 51,799 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 450, BL 0. REPAIRED SKIN PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,889 hrs · 51,799 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 27L CORRODED AT BS 503 TO BS 512B. REPAIRED STRINGER PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 69,876 hrs · 51,790 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER ACO.

Part: WINDOW — CRACKED (COCKPIT) · airframe 69,683 hrs · 51,657 cycles

FLIGHT DECK L1 WINDOW CRACKED AND ARCED INFLIGHT. REMOVED AND REPLACED WINDOW PER MM.

Part: BRACKET — LOOSE (R1 DOOR GIRT BAR) · airframe 69,244 hrs · 51,338 cycles

R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR BRACKET LOOSE. REMOVED AND REPLACED GIRT BAR BRACKET PER MM.

Part: SKIN — CRACKED (BS 980 S21L) · airframe 69,157 hrs · 51,273 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 980, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (780 S21L) · airframe 68,130 hrs · 50,486 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 21L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,711 hrs · 50,150 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 67,265 hrs · 49,789 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 66,828 hrs · 49,450 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,695 hrs · 49,355 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 763, STR 23R. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,695 hrs · 49,355 cycles

DURING SCHEDULED A2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 66,490 hrs · 49,191 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 66,483 hrs · 49,182 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 66,344 hrs · 49,071 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 66,344 hrs · 49,071 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR FWD FRAME CRACKED AT BETWEEN NR 2 AND NR 3 STOP FITTINGS. REMOVED AND REPLACED CARGO DOOR PER MM.

Part: SKIN — CRACKED (BS 847 S24L) · airframe 66,344 hrs · 49,071 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 847, STR 24L. REPAIRED SKIN PER SRM.

Part: ATTACH FITTING — BROKEN (SPOILER ACTUATOR) · airframe 65,342 hrs · 48,330 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING NR 5 SPOILER INBOARD ACTUATOR FWD ATTACH FITTING BROKEN. REMOVED AND REPLACED INBOARD ACTUATOR PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 65,342 hrs · 48,330 cycles

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

Part: GASPER FAN — OVERHEATED (E/E BAY) · airframe 65,114 hrs · 48,137 cycles

HOT ACRID SMELL IN COCKPIT, ALSO PRESENT IN CABIN. REMOVED AND REPLACED GASPER FAN PER MM.

Part: KEELBEAM — CORRODED (BS 740) · airframe 65,102 hrs · 48,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM CHORD CORRODED AT BS 740, RBL 6.5. REPAIRED CHORD PER SWA EA.

Part: STRINGER — CORRODED (BS 967 S25L) · airframe 65,102 hrs · 48,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 25L CORRODED AT BS 967. REPAIRED STRINGER PER SRM.

Part: KEELBEAM — CORRODED (BS 727-738) · airframe 65,102 hrs · 48,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM CHORD CORRODED AT BS 727 TO BS 738, RBL 6. REPAIRED CHORD PER SWA EA.

Part: KEELBEAM — CORRODED (BS 741) · airframe 65,102 hrs · 48,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM SPLICES CORRODED AT BS 741, RBL 6.5. REPAIRED CHORD PER SWA EA.

Part: FRAME — CORRODED (BS 847) · airframe 65,102 hrs · 48,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, RBL 18. REMOVED AND REPLACED FRAME SECTION PER SWA EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 65,102 hrs · 48,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 440, STR 28R. REPAIRED SKIN PER SWA EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,102 hrs · 48,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 28R CORRODED AT BS 490. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 65,102 hrs · 48,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR CUTOUT AFT FRAME CRACKED AT NR 2 DOOR STOP. REPAIRED FRAME SECTION PER SWA EA.

Part: BEAR STRAP — CRACKED (BS 338 S17L) · airframe 65,102 hrs · 48,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT BS 338, STR 17L. REPAIRED SKIN PER SWA EA.

Part: STRINGER — CORRODED (BS 475 S27L) · airframe 65,102 hrs · 48,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 27L CORRODED AT BS 475. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (BS 747 S24R) · airframe 65,102 hrs · 48,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 24R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (L/E SLAT) · airframe 65,102 hrs · 48,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT WING NR 3 L/E SLAT LOWER T/E SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 65,102 hrs · 48,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FIRST OFFICER NR 1 OUTBOARD WINDOW POST CRACKED. REPAIRED WINDOW POST PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,102 hrs · 48,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT STR 23L, BS 750 TO BS 770. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,102 hrs · 48,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 765, STR 19R. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,093 hrs · 48,119 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,634 hrs · 47,745 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 11L. REPAIRED SKIN PER SWA EA.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 64,643 hrs · 47,745 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE HARDWARE MISROUTED. REMOVED AND REPLACED EVAC SLIDE CABLE HARDWARE PER MM.

Part: STRUCTURE — CRACKED (LT FOREFLAP) · airframe 64,634 hrs · 47,745 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD FORE FLAP CRACKED ON INBOARD SIDE. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,634 hrs · 47,745 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 306, STR 18R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 765) · airframe 59,865 hrs · 43,999 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 765, BETWEEN STR 19R TO STR 20R. REPAIRED SKIN IAW EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,865 hrs · 43,999 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740E, STR 23L. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,865 hrs · 43,999 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504D, STR 16L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,865 hrs · 43,999 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT, FWD UPPER CORNER. REPAIRED SKIN IAW SWA EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,865 hrs · 43,999 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,768 hrs · 45,492 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 765, STR 24R. REPAIRED SKIN PER SRM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 61,768 hrs · 45,492 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR BRACKET LOOSE. SECURED BRACKET PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 61,768 hrs · 45,492 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,768 hrs · 45,492 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 735, STR 25R. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,768 hrs · 45,492 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 22R. REPAIRED SKIN PER SWA EA AND SRM.

Part: ENGINE — FAILED (NR 2) · airframe 61,402 hrs · 45,204 cycles

INFLIGHT SHUTDOWN/DECLARED EMERGENCY/DIVERSION. NR 2 ENGINE FAILED AT 34,000 FT, LOUD BANG TWICE & LOSS OF THRUST. REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,770 hrs · 44,722 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 22L. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (RT WING FOREFLAP) · airframe 60,770 hrs · 44,722 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,770 hrs · 44,722 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 847, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,770 hrs · 44,722 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 807, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,770 hrs · 44,722 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 867, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,770 hrs · 44,722 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,342 hrs · 43,603 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727E + 3, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 58,907 hrs · 43,275 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,861 hrs · 43,231 cycles

DURING SCHEDULED C2 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 787, STRINGER 24L, BS 727E, STRINGER 20R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 58,861 hrs · 43,231 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,861 hrs · 43,231 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 967, STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 58,226 hrs · 42,725 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,937 hrs · 42,497 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 727D + 4, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,085 hrs · 41,839 cycles

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

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D CHECK, FOUND CORROSION ON KEEL BEAM LT OUTBOARD FLANGE AT BS 727. REMOVED AND REPLACED OUTBOARD FLANGE PER ER.

Part: SPAR — CORRODED (VERTICAL STAB) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D CHECK, FOUND CORROSION ON VERTICAL STAB FRONT SPAR RT LUG FORWARD AND AFT FACES. REPAIRED STAB PER EO.

Part: RIB — CRACKED (RT WING) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D CHECK, FOUND RT WING WBL 135, RIB LOWER CHORD CRACKED. REPAIRED CHORD PER ER.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM CHORD CRACKED AT BS 638, LBL 64, WL 208. REMOVED AND REPLACED CHORD SECTION PER SRM.

Part: BEAM — CORRODED (RT MLG) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D CHECK, FOUND CORROSION ON RT MLG BEAM FASTENER HOLES LOWER BEAM. REPAIRED RT MLG BEAM PER ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CORRODED AT BS 847, RBL 30 TO RBL 45. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED AT BS 948 TO BS 990 RBL 55, WL 208 CORRODED. REPAIRED CREASE BEAM PER SRM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL STAB RT AND LT FITTING AFT SPAR LUGS CORRODED. REPAIRED VERTICAL STAB FITTING PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 787, STRINGER 9L. REPAIRED FRAME SECTION PER ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 707 TO BS 713, LBL 25, WL 203. REPAIRED FLOORBEAM SECTION PER ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CRACKED AT BS 986, RBL 55 TO LBL 14, WL 208. REPAIRED FLOORBEAM PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME CRACKED AT BS 492, STRINGER 24R. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 787, STRINGER 9R. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 767, STRINGER 9L. REPAIRED FRAME SECTION PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 907, STRINGER 9R AND AT BS 907, STRINGER 9L. REPAIRED FRAME SECTIONS PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 867, STRINGER 9R. REPAIRED FRAME SECTION PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D CHECK, FOUND FRAME INBOARD CHORD CRACKED AT BS 616, RBL 64, WL 202. REMOVED AND REPLACED FRAME SECTION PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 907, STRINGER 9L. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 400, STRINGER 9L. REPAIRED FRAME SECTION PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULE D CHECK, FOUND FRAME CRACKED AT BS 807, STRINGER 9L. REPAIRED FRAME SECTION PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 827, STRINGER 9L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D CHECK, FOUND R1 DOOR CUTOUT SUBFRAME CRACKED AT BS 303, RBL 56, WL 208. REMOVED AND REPLACED SUBFRAME SECTION PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 617, LBL 65, WL 208. REMOVED AND REPLACED CREASE BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 500, LBL 1 TO LBL 3, WL 148. REPAIRED SHEAR TIE PER SRM.

Part: BEAM — CORRODED (RT MLG) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON RT MLG BEAM ON AFT STABILIZER BEAM FITTING. REMOVED AND REPLACED BEAM FITTING PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 188, STRINGER 17R. REMOVED AND REPLACED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 767, LBL 2. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 637, RBL 65, WL 208. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 663, STRINGER 2R. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 188, STRINGER 17 L. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICES CRACKED AT BS 907, STRINGER 4R AND STRINGER 4L. REPAIRED STRINGER SPLICES PER SRM.

Part: STRAP — CRACKED (CARGO FLOOR) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D-CHECK, FOUND MID CABIN FLOOR SUPPORT STRAP CRACKED AT BS 540, RBL 1, WL 208. REPAIRED FLOOR STRAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 360, STRINGER 4L, AND BS 344, STRINGER 9R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 967, ABOVE L2 DOOR. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D-CHECK, FOUND SKIN CORRODED AT FAIRING ATTACHMENT POINT BS 727B + 10 TO BS 727D, BETWEEN STRINGER 21R AND STRINGER 25R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D CHECK, FOUND 2 EACH FORWARD CARGO COMPARTMENT STRINGER CLIPS CRACKED AT BS 500D, BETWEEN STRINGER 19R AND STRINGER 19L. REPAIRED STRINGER CLIPS PER SRM.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D CHECK, FOUND FLOOR WEB CRACKED FROM BS 178 TO BS 188, LBL 27. REPAIRED FLOOR WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 360, STRINGER 5L, BS 360, STRINGER 3L AND BS 344, STRINGER 11R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D CHECK, FOUND 2EA STRINGER CLIPS CRACKED AT BS 616, STRINGER 5R AND BS 597, STRINGER 8R.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 56,681 hrs · 41,527 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED FROM BS 948 TO BS 990, LBL 55, WL 208. REPAIRED CREASE BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,331 hrs · 41,250 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 727E, STR 24R AND STR 23L. REPAIRED SKIN SECTIONS PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 56,146 hrs · 41,115 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 56,021 hrs · 41,029 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,941 hrs · 40,959 cycles

DURING SCHEDULED SVC CHECK, FOUND FUSELAGE SKIN CRACKED 2 LONG BETWEEN BS 517-BS 519, JUST BELOW STR 12R. REPAIRED SKIN PER SRM.

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 55,864 hrs · 40,898 cycles

DURING SCHEDULED RON, FOUND VERTICAL STIFFENER CRACKED AT LT W/W FWD BULKHEAD, BS 663 AND LBL 6.15. REPAIRED VERTICAL STIFFENER PER SWA EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 53,375 hrs · 38,931 cycles

DURING SCHEDULED C4 CHECK, FOUND RT OTBD AFT T/E FLAP DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED RT OTBD AFT T/E FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,368 hrs · 38,926 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 751, STR 18R AND STR 19R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 52,322 hrs · 38,077 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST AND SLIDE CABLE MISROUTED. ADJUSTED SLIDE AND REROUTED CABLE PER MM.

Part: LENS — MISSING (CABIN) · airframe 51,421 hrs · 37,352 cycles

DURING SCHEDULED C2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,743 hrs · 36,803 cycles

DURING SCHEDULED A2 CHECK, FOUND INTERCOSTAL CRACKED AT STR 10R, ONE INCH AFT OF FWD SVC DOOR. REPAIRED INTERCOSTAL PER SWA ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,743 hrs · 36,803 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727, STR 24L. REPAIRED SKIN PER SRM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 50,541 hrs · 36,646 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,641 hrs · 35,934 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, BELOW STR 12L. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (ENTRY DOOR) · airframe 49,237 hrs · 35,623 cycles

FWD ENTRY DOOR EMERGENCY EXIT LIGHT BEZEL FELL OFF. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 48,793 hrs · 35,242 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT LOWER FWD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BRACKET — CORRODED (AFT SVC DOOR) · airframe 48,597 hrs · 35,086 cycles

DURING SCHEDULED 1/4D CHECK AT DALFORT, FOUND CORRODED NUTPLATE AT AFT SVC DOOR EMERGENCY EVAC SLIDE AFT MOUNT BRACKET. R&R BRACKET NUTPLATE PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 48,597 hrs · 35,086 cycles

DURING SCHEDULED 1/4D CHECK AT DALFORT, FOUND STIFFENER CRACKED AT BS 178, LH & WL 195. REPAIRED STIFFENER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,810 hrs · 34,425 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR CUT OUT FUSELAGE SKIN CRACKED AT LWR AFT CORNER. REPAIRED FUSELAGE SKIN PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 47,810 hrs · 34,425 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING OTBD AFT FLAP DELAMINATED AT INBD CORNER. R&R FLAP ASSY PER MM.

Part: RETAINER — LOOSE (ENTRY DOOR) · airframe 47,810 hrs · 34,425 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. RESECURED GIRT BAR HOOK PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 47,594 hrs · 34,234 cycles

EEPLS LOOSE NEAR FWD SECTION. SECURED EEPLS PER MM.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 46,920 hrs · 33,688 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 663 VERTICAL STIFFENER CRACKED AT RBL 6.25. REMOVED AND REPLACED VERTICAL STIFFENER PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 46,920 hrs · 33,688 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND RT LOWER KEEL BEAM CORRODED AT BS 525. REPAIRED KEEL BEAM PER RA.

Part: RELAY — ERRATIC (MLG HANDLE) · airframe 46,913 hrs · 33,679 cycles

AIR TURNBACK, ON T/O GEAR HANDLE WOULD NOT COME UP. PULLED OVERRIDE TRIGGER AND GEAR RETRACTED. RESEATED R276 RELAY, RESET C/B. HANDLE OPS CHECKED GOOD PER MM.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 45,981 hrs · 32,899 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR HANDLE FLAP CUTOUT CRACKED AT AFT CORNER. REPAIRED DOOR PER SRM.

Part: COVER — LOOSE (ESCAPE SLIDE) · airframe 45,981 hrs · 32,899 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE LATCH WOULD NOT ENGAGE COVER RETAINER CORRECTLY. REPOSITIONED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,964 hrs · 32,883 cycles

DURING SCHEDULED PM CHECK, FOUND 1.5 EXTERNAL FUSELAGE SKIN CRACK AT BS 732, STR 1R. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 45,292 hrs · 32,320 cycles

DURING SCHEDULED A1 CHECK, FOUND FIRST LT AND SECOND RT EMERGENCY AISLE LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOP (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT FWD END. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: NUT PLATE — DAMAGED (LT EXTERIOR EEL)

DURING OVERNIGHT CHECK, FOUND DAMAGED ATTACH NUT PLATE FOR EMERGENCY LIGHT ON LEFT FUSELAGE AFT OF WING. REMOVED AND REPLACED NUT PLATE PER MM AND SRM.

Part: SLIDE — DETACHED (L 1 DOOR)

FWD ENTRY DOOR EVACUATION SLIDE OUT OF CASE. REPOSITIONED SLIDE PER MM.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED SC CHECK, FOUND EMERGENCY LIGHT ON LEFT FUSELAGE AFT OF WING INOP. RELAMPED EMERGENCY LIGHT ON LEFT FUSELAGE PER M/M, OPS CHECK OK.

Part: BULKHEAD CHORD — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 T-CHORD CRACKED AT LBL 5.7, WL 184. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727, 941, 965)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORROSION AT BS 727, 772, 941 AND 965. REPAIRED PER BOEING SRM.

Part: STRAP — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 VERTICAL STRAP CRACKED AT LBL 6.6. INSTALLED REPAIR DOUBLER PER SWA BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5, LBL 4. REPAIRED DAMAGED SECTION PER SWA RA 1-353-1993.

Part: FLOORBEAM — CORRODED (BS 787-847)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORROSION AT BS 787 TO 847, LBL 3. REPLACED SECTION PER BOEING SRM.

Part: FLOORBEAM — CRACKED (BS 488)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED AT BS 488. SPLICED IN NEW SECTION PER SWA BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM SCREW HOLE CORROSION, VARIOUS PLACES AT BS 986.5, AFT GALLEY AREA.

Part: RELAY — BURNT (P6 PANEL)

ELECTRICAL ODOR NOTED FROM BEHIND P6 PANEL. INSPECTED AND FOUND R18 RELAY BURNED AND PLUG ARCED. REPLACED RELAY, PLUG AND C/B PER BOEING M/M.

Part: BASE — INOPERATIVE (CABIN)

DURING SCHEDULED TERMINAL CHECK, FOUND AFT SERVICE DOOR EMERGENCY LIGHT INOP. REPLACED LIGHT BASE PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

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