N684WN

Part: LENS — BROKEN (EXIT SIGN) · airframe 80,712 hrs · 68,275 cycles

R1 DOOR EMER EXIT SIGN LENS COVER BROKEN. R & R SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 80,220 hrs · 67,903 cycles

L2 DOOR EXTERIOR EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,173 hrs · 67,866 cycles

SKIN CRACKED AT BS 948-4, STRINGER 24R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,173 hrs · 67,866 cycles

SKIN CRACKED AT BS 806-2, STRINGER 19L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,812 hrs · 67,610 cycles

SKIN CRACKED BETWEEN BS 500B+5.5 - 500B+6.5, STRINGER 15R. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,812 hrs · 67,610 cycles

SKIN CRACKED AT BS 500A+15, STRINGER 19L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,812 hrs · 67,610 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 434 - 436, STRINGER 16R. REPAIRED SKIN IAW SWA.

Part: WIRE HARNESS — FAULTY (COCKPIT) · airframe 79,478 hrs · 67,370 cycles

AIR TURN BACK & DECLARED EMER. R2 COCKPIT WINDOW HEAT WIRE ARCED. R & R R2 WINDOW HEAT ELEC HARNESS IAW MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 79,362 hrs · 67,286 cycles

TAIL COMPARTMENT STRINGER HAT SECTION CRACKED AT BS 1054, STRINGER 19R. REPAIRED STRINGER IAW SRM & EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 79,060 hrs · 67,075 cycles

RIGHT WING INBD FORE FLAP UPPER SURFACE DELAMINATED. R & R FORE FLAP IAW MM.

Part: SPINDLE — CORRODED (TE FLAP) · airframe 78,975 hrs · 67,013 cycles

LEFT WING NR 2 FLAP SPINDLE CORRODED. R & R SPINDLE IAW MT.

Part: LIGHT — LOOSE (CABIN) · airframe 78,870 hrs · 66,929 cycles

RIGHT OVERWING EMER EXIT LIGHT LOOSE. SECURED LIGHT IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 78,445 hrs · 66,588 cycles

RIGHT EMER LIGHT INOPERATIVE AT ROW 20. R & R BATTERY ASSEMBLY IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 78,445 hrs · 66,588 cycles

R2 EXTERIOR EMER LIGHT INOPERATIVE. R & R BATTERY ASSEMBLY IAW AMM.

Part: CIRCUIT BREAKER — BROKEN (COCKPIT) · airframe 77,900 hrs · 66,200 cycles

DECLARED EMER, GEAR UNSAFE INDICATION NOTED GEAR AIR GND RELAY BREAKER BROKEN. ALL THREE GEARS UNSAFE. R & R AIR GND RELAY LIGHTS CB IAW SWP.

Part: LENS — LOOSE (CABIN) · airframe 77,748 hrs · 66,102 cycles

LEFT OVERWING EXIT AFT LIGHT LENS COVER LOOSE. R & R LENS IAW MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 77,748 hrs · 66,102 cycles

LEFT WING OTBD AFT FLAP DELAMINATED ON INBD EDGE. R & R FLAP IAW MM.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 79,153 hrs · 67,140 cycles

AFT CARGO DOOR FRAME FWD SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 77,748 hrs · 66,102 cycles

LEFT OVERWING EXIT FWD LIGHT LENS COVER LOOSE. R & R LENS IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,607 hrs · 65,989 cycles

FORWARD CABIN AREA EMER LIGHT INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 77,607 hrs · 65,989 cycles

VERTICAL STABILIZER PANEL 9508 SKATE SEAL ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

FORWARD OF NLG FAIL SAFE ON FWD LOWER CORNER OF THE FRAME CORRODED AT BS 219, LBL 16. REPAIRED CHORD IAW SRM & DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

INTERCOSTAL BRACKET CRACKED AT BS 947 BETWEEN STRINGER 24R TO 25R. R & R IAW SRM & DWG.

Part: STRUCTURE — CRACKED (LT MLG WW) · airframe 77,607 hrs · 65,989 cycles

LEFT MLG WW LOWER WHEEL CUT OUT RIB LOWER CURVED CHORD CRACKED AT BS 680 LBL 67. R & R CHORD IAW DWG & SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

STRINGER SPLICE UPPER L ANGLE CRACKED AT BS 360 STRINGER 7R. R & R ANGLE IAW EA.

Part: ATTACH FITTING — LOOSE (TE FLAP) · airframe 77,607 hrs · 65,989 cycles

RIGHT WING INBD FORE FLAP INBD TRACK TOGGLE ATTACH ARMS LOOSE. R & R FORE FLAP ASSEMBLY IAW MM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 77,607 hrs · 65,989 cycles

LEFT VERTICAL STABILIZER OTBD AFT SPAR LUG FWD & AFT BUSHING FITTING CORRODED. R & R FITTING IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

LOWER CHORD CRACKED AT BS 727 BETWEEN STRINGER 22R TO 25R. R & R CHORD IAW DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

FLOOR SUPPORT CRACKED AT BS 520 BETWEEN LBL 24 TO LBL 45. R & R SUPPORT IAW DWG.

Part: FLAP — DELAMINATED (LT WING) · airframe 77,607 hrs · 65,989 cycles

LEFT WING OTBD FORE FLAP INBD TE CORNER DELAMINATED. REPAIRED FORE FLAP IAW WO.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

FORWARD SERVICE DOOR UPPER STUB FRAME CRACKED AT BS 294 UPPER INBD FASTENER HOLE. R & R STUB FRAME IAW DWG & EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

AFT CARGO INTERCOSTAL CRACKED BETWEEN BS 947 TO 967 BETWEEN STRINGER 24R TO 25R. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

AFT CARGO COMPARTMENT INTERCOSTAL CORRODED BETWEEN BS 927 TO 947 STRINGER 25R. R & R INTERCOSTAL IAW SRM & DWG.

Part: SKIN — CORRODED (RUDDER) · airframe 77,607 hrs · 65,989 cycles

UPPER LT RUDDER SKIN CORRODED. REPAIRED SKIN IAW SRM.

Part: HINGE FITTING — CRACKED (TE FLAP) · airframe 77,607 hrs · 65,989 cycles

LEFT WING OTBD FORE FLAP OTBD TRACK HINGE FITTING FWD FASTENER HOLE CRACKED. R & R FORE FLAP IAW EA.

Part: LUG — CORRODED (VERTICAL STAB) · airframe 77,606 hrs · 65,989 cycles

VERTICAL STABILIZER LT FAILSAFE LUGS FWD & AFT ON ACFT CORRODED. REPAIRED LUG IAW EA.

Part: LUG — CORRODED (VERTICAL STAB) · airframe 77,606 hrs · 65,989 cycles

VERTICAL STABILIZER RT FAILSAFE LUGS FWD & AFT ON ACFT CORRODED. REPAIRED LUG IAW EA.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

HANGER BRACKET CRACKED AT BS 847 STRINGER 1R. R & R BRACKET IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

STRINGER CLIP CRACKED AT BS 947 STRINGER 19R. R & R CLIP IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

VERTICAL FLANGE ANGLE CORRODED AT BS 219, LBL 16. R & R FLANGE IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 669 LBL 24.5. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

FRAME WEB OUTER CHORD CRACKED AT BS 227 STRINGER 16R. REPAIRED WEB IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

AFT CARGO PIT CARGO DOOR UPPER SILL WEB CORRODED BETWEEN BS 820 TO 827 STRINGER 18R. REPAIRED WEB IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 658 LBL 24.5. REPAIRED CHORD IAW SRM & EA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

AFT CARGO PIT CARGO DOOR UPPER SILL WEB ANGLE CORRODED AT BS 807 STRINGER 18R. R & R WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

FRAME WEB CRACKED AT BS 380 STRINGER 16R. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 663 TO 670. REPAIRED CHORD IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

ANGLE CLIP CRACKED AT BS 639 STRINGER 14L. REPAIRED CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

FRAME CRACKED AT BS 727B, STRINGER 14R. REPAIRED FRAME IAW EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

INTERCOSTAL CORRODED BETWEEN BS 220 TO 227, BL 0. R & R INTERCOSTAL IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

FRAME CRACKED AT BS 947+4 STRINGER 19R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

FRAME CRACKED AT BS 947 BETWEEN STRINGER 24R TO 25R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

FRAME CRACKED AT BS 947 STRINGER 19R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

FRAME CRACKED AT BS 887 STRINGER 19L. REPAIRED FRAME IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

SHEAR TIE CORRODED AT BS 967 BETWEEN STRINGER 26R TO 27R. REPAIRED SHEAR TIE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

CREASE BEAM INNER CHORD CORRODED BETWEEN BS 305 TO 344, BETWEEN LBL 54 TO LBL 60. R & R CHORD IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

FRAME CRACKED AT BS 500 STRINGER 26L. REPAIRED FRAME IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

STRINGER CLIP CRACKED AT BS 360 STRINGER 21R. R & R CLIP IAW DWG & SRM.

Part: LUG — CORRODED (VERTICAL STAB) · airframe 77,606 hrs · 65,989 cycles

VERTICAL STABILIZER LT SIDE FWD LUG CORRODED. REPAIRED LUG IAW EA.

Part: LUG — CORRODED (VERTICAL STAB) · airframe 77,606 hrs · 65,989 cycles

VERTICAL STABILIZER RT SIDE FWD LUG BORE CORRODED. REPAIRED LUG IAW EA.

Part: RIB — CRACKED (LT WING) · airframe 77,607 hrs · 65,989 cycles

LEFT WING FUEL TANK WBL 254.00 INBD SIDE, 2 INCHES AFT OF FRONT SPAR, RIB ATTACH STRUCTURE CRACKED AT FASTENER HOLE. REPAIRED RIB IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,606 hrs · 65,989 cycles

FORWARD EEPLS INOPERATIVE. R & R EEPLS IAW MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

STRINGER CRACKED AT BS 1011 STRINGER 4L. R & R STRINGER IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

SEAT TRACK CORRODED BETWEEN BS 727D TO 727E LBL 24.5. REPAIRED SEAT TRACK IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 971 TO 986. R & R WEB IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

SEAT TRACK CORRODED BETWEEN BS 500C TO 500C+16 RBL 45.5. R & R SEAT TRACK IAW DWG & SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

SEAT TRACK CORRODED BETWEEN BS 381 TO 398, RBL 45.5. R & R SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

SEAT TRACK CORRODED BETWEEN BS 500C+12 TO 500D+11 LBL 45.5. REPAIRED SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

SEAT TRACK CORRODED BETWEEN BS 426 TO 447, LBL 45.5. R & R SEAT TRACK IAW DWG & SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

SEAT TRACK CORRODED BETWEEN BS 500+8 TO 500A+7 LBL 45.5. R & R SEAT TRACK IAW SRM.

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · airframe 77,606 hrs · 65,989 cycles

VERTICAL STABILIZER LT INBD AFT SPAR LUG FWD & AFT BUSHINGS ATTACH FITTING CORRODED. REPAIRED FITTING IAW AAR & EA.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

VERTICAL STABILIZER ATTACH FITTING ON ACFT FUSELAGE AFT SPAR LT OTBD FITTING AFT LUG CORRODED. REPAIRED FITTING IAW EA.

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · airframe 77,606 hrs · 65,989 cycles

VERTICAL STABILIZER RT INBD AFT SPAR LUG FWD & AFT BUSHINGS ATTACH FITTING CORRODED. REPAIRED FITTING IAW AAR & EA.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

VERTICAL STABILIZER ATTACH FITTING ON ACFT FUSELAGE FWD SPAR RT FITTING AFT LUG CORRODED. REPAIRED FITTING IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

L1 DOOR SURROUND STRUCTURE FWD LOWER WEB SUPPORT ANGLE CRACKED AT BS 348.2 STRINGER 15L. R & R ANGLE IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

LEFT CUSP WEB OVERWING CORRODED. R & R CUSP WEB IAW SRM & DWG.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

VERTICAL STABILIZER ATTACH FITTING ON ACFT FUSELAGE AFT SPAR LT OTBD FITTING FWD LUG CORRODED. REPAIRED FITTING IAW EA.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

VERTICAL STABILIZER ATTACH FITTING ON ACFT FUSELAGE AFT SPAR RT OTBD FITTING FWD LUG CORRODED. REPAIRED FITTING IAW EA.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 77,606 hrs · 65,989 cycles

VERTICAL STABILIZER RT FAILSAFE LUGS FWD & AFT ON ACFT CORRODED. REPAIRED FITTING IAW AAR EA & SWA EA.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 77,606 hrs · 65,989 cycles

RIGHT VERTICAL STABILIZER OTBD AFT SPAR LUG, FWD & AFT BUSHING FITTING CORRODED. REPAIRED FITTING IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

STRINGER CRACKED AT BS 328 STRINGER 20R. REPAIRED STRINGER IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 77,606 hrs · 65,989 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 664 BETWEEN LBL 3.0 TO 3.5. REPAIRED WEB IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

FLOORBEAM UPPER SURFACE T CAP CORRODED AT BS 986.5 RBL 35. R & R T CAP IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

FLOORBEAM UPPER SURFACE T CAP CORRODED AT BS 986.5 RBL 9. REPAIRED T CAP IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

FLOORBEAM UPPER SURFACE T CAP CORRODED AT BS 986.5 RBL 18. R & R T CAP IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

FLOORBEAM UPPER SURFACE T CAP CORRODED AT BS 986.5 RBL 27. R & R T CAP IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

FLOORBEAM UPPER SURFACE T CAP CORRODED AT BS 986.5 RBL 47. R & R T CAP IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

FLOORBEAM UPPER SURFACE T CAP CORRODED AT BS 986.5 RBL 40. R & R T CAP IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

FLOORBEAM UPPER SURFACE T CAP CORRODED AT BS 986.5 RBL 44. R & R T CAP IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

AFT OF L1 DOOR CUT OUT FRAME INNER CHORD CRACKED AT BS 348.2. R & R CHORD IAW EA.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

AFT OF L1 DOOR CUT OUT FRAME ATTACH CLIP CRACKED AT INBD LOWER FASTENER HOLE. R & R CLIP IAW EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

L1 DOOR SURROUND STRUCTURE INTERCOSTAL WEB FWD ATTACH ANGLE CRACKED AT BS 348.20 STRINGER 16L. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

FUSELAGE SKIN CRACKED AT BS 500A+5 STRINGER 16L. REPAIRED SKIN IAW SRM.

Part: STRAP — BROKEN (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

L1 DOOR SURROUND STRUCTURE FRAME STRAP BROKEN AT BS 348.20 STRINGER 16L. R & R STRAP IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

CREASE BEAM INNER CHORD UPPER SURFACE CORRODED BETWEEN BS 964 TO 980 LBL 52. R & R CHORD IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 500A TO 500B STRINGER 18R. REPAIRED SKIN IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

R1 DOOR CREASE BEAM INNER CHORD CORRODED BETWEEN BS 292 TO 358 BETWEEN LBL 54 TO LBL 60. R & R CREASE BEAM IAW SRM & DWG.

Part: FITTING — BROKEN (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

L1 DOOR SURROUND STRUCTURE FRAME CLIP BROKEN AT BS 348.20 STRINGER 16L. R & R CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (ENTRY DOOR) · airframe 77,607 hrs · 65,989 cycles

FORWARD ENTRY DOOR SURROUND STRUCTURE ANGLE CRACKED AT BS 360, STRINGER 11L. R & R ANGLE IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

L1 DOOR FRAME CRACKED AT BS 340 STRINGER 6L. REPAIRED FRAME IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

R2 DOOR CUT OUT CREASE BEAM INNER CHORD CORRODED ON UPPER SURFACE BETWEEN BS 957 TO 995 BETWEEN RBL 46 TO 56. R & R CHORD IAW SRM & DWG.

Part: MOUNT FITTING — CORRODED (GIRT BAR) · airframe 77,607 hrs · 65,989 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR FITTING MOUNT PLATE CORRODED BETWEEN BS 342 TO 344 BETWEEN LBL 58 TO 60. REPAIRED FITTING IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

FLOORBEAM T CAP CORRODED AT BS 344, BETWEEN LBL 15 TO RBL 10. R & R T CAP IAW SRM.

Part: PLATE — CORRODED (GIRT BAR) · airframe 77,607 hrs · 65,989 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR FITTING MOUNT PLATE CORRODED BETWEEN BS 313 TO 315 BETWEEN LBL 53 TO 56. REPAIRED PLATE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

CREASE BEAM INNER CHORD CORRODED BETWEEN BS 305 TO 344 BETWEEN LBL 54 TO LBL 60. R & R CHORD IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

STRINGER CLIP CRACKED AT BS 277 STRINGER 11R. R & R CLIP IAW SRM & DWG.

Part: LENS — CRACKED (CABIN) · airframe 77,607 hrs · 65,989 cycles

AFT GALLEY CTR EMER EXIT LIGHT CEILING PANEL LIGHT COVER LENS CRACKED. R & R LENS IAW AMM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

R2 DOOR CUT OUT FRAME CORRODED AT BS 993 STRINGER 17R. R & R FRAME IAW EA.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 77,607 hrs · 65,989 cycles

L1 DOOR CLIP ANGLE CRACKED AT BS 292 STRINGER 9L. R & R ANGLE IAW SRM & DWG.

Part: BEARING — CRACKED (TE FLAP) · airframe 77,607 hrs · 65,989 cycles

RIGHT WING TE MID FLAP CARRIAGE, OTBD TRACK FAIRING INBD PROGRAMMING BEARING CRACKED AT EDGE. R & R BEARING IAW CMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

SKIN CRACKED AT BS 845 STRINGER 18L. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 18A RT. R & R CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

FRAME CHORD CRACKED AT BS 727 STRINGER 18A LT. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

SKIN CRACKED AT BS 941 STRINGER 23R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

SKIN CRACKED AT BS 528 BETWEEN STRINGER 28L TO 28R. REPAIRED SKIN IAW EA.

Part: BRACE — CRACKED (FUSELAGE) · airframe 77,607 hrs · 65,989 cycles

AFT CARGO COMPARTMENT UPPER SUPPORT BRACE FOR THE FLIGHT RECORDER SHROUD CRACKED BETWEEN BS 887 TO 1008 STRINGER 20L. R & R BRACE IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 77,606 hrs · 65,989 cycles

FORWARD GALLEY DOOR CUT OUT STRUCTURE FRAME CRACKED AT BS 294.5 STRINGER 7R. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,313 hrs · 65,785 cycles

FUSELAGE SKIN CRACKED AT BS 00A+6, STRINGER 16R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,313 hrs · 65,785 cycles

FUSELAGE SKIN CRACKED AT BS 460+4, STRINGER 16R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,313 hrs · 65,785 cycles

FUSELAGE SKIN CRACKED AT BS 440+12, STRINGER 16R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,313 hrs · 65,785 cycles

FUSELAGE SKIN CRACKED AT BS 500B+15, STRINGER 19L. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 77,313 hrs · 65,785 cycles

FORWARD ENTRY DOOR EMERGENCY EXTERIOR LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,313 hrs · 65,785 cycles

FUSELAGE SKIN CRACKED AT BS 500+4, STRINGER 16R. REPAIRED SKIN IAW EA.

Part: HOUSING — BROKEN (CABIN) · airframe 76,870 hrs · 65,485 cycles

EMERGENCY LIGHT BATTERY PACK HOUSING ASSEMBLY BROKEN AT CABIN STATION 910. R & R BATTERY PACK ASSEMBLY IAW MM.

Part: LUG — BROKEN (LT SPOILER) · airframe 76,524 hrs · 65,245 cycles

LT WING INBD NR 4 GROUND SPOILER OTBD LUG BROKEN. R & R SPOILER IAW MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 76,487 hrs · 65,216 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. READJUSTED SLIDE IAW MT.

Part: ANGLE — CRACKED (RT MLG) · airframe 76,130 hrs · 64,964 cycles

RT MLG STAB BAR PANEL ANGLE BRACKET CRACKED. R & R ANGLE IAW SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 75,183 hrs · 64,225 cycles

FWD ENTRY EMERGENCY EXIT SIDE FLOOR LEVEL BROKEN. R & R LIGHT ASSY IAW AMM.

Part: SLAT — DELAMINATED (LT WING) · airframe 74,979 hrs · 64,085 cycles

LEFT WING UPPER T/E OF NR 2 SLAT DELAMINATED. REPAIRED NR 2 SLAT IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 74,979 hrs · 64,085 cycles

RT WING FIXED L/E CRACKED AT NR 6 SLAT AUX TRACK CUTOUT OTBD OF ACTUATOR. REPAIRED CUTOUT IAW EA.

Part: LENS — BROKEN (CABIN) · airframe 74,525 hrs · 63,744 cycles

FORWARD ENTRY EMERGENCY LIGHT LENS BROKEN. REMOVED AND REPLACED LENS IAW M/M.

Part: STRUCTURE — CRACKED (LE SLAT) · airframe 74,369 hrs · 63,641 cycles

NR 6 LEADING EDGE SLAT, INBOARD SLAT CAN IS CRACKED. REMOVED AND REPLACED NR 6 LEADING EDGE SLAT INBOARD SLAT CAN PER EA.

Part: RETAINER — OUT OF ADJUST (L2 DOOR) · airframe 74,293 hrs · 63,583 cycles

AFT ENTRY DOOR GIRT BAR RETAINER DIFFICULT TO DISENGAGE. ADJUSTED RETAINER PER M/M.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 74,100 hrs · 63,437 cycles

L1 DOOR SLIDE LOWER FLAP REQUIRES REPOSITION. REPOSITIONED L1 SLIDE MT325-61-06 AND MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 74,100 hrs · 63,437 cycles

R1 DOOR SLIDE LOWER FLAP REQUIRES REPOSITION. REPOSITIONED R1 SLIDE PER MT325-61-06 AND MM

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,100 hrs · 63,437 cycles

RIGHT EMERGENCY EXIT HATCH LIGHT INOP. REMOVED AND REPLACED RIGHT EMERGENCY EXIT HATCH LIGHT BULB PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,017 hrs · 63,371 cycles

FOUND 1.5" SURFACE CRACK BS 500D + 15" BELOW S15L. REPAIRED PER E/A 1-353-21463.

Part: SPINDLE — CORRODED (TE FLAP) · airframe 73,279 hrs · 62,815 cycles

RIGHT WING NR 8 SPINDLE CORRODED. REMOVED AND REPLACED NR 8 SPINDLE IAW MT.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 72,665 hrs · 62,334 cycles

R2 DOOR EMERGENCY EVAC SIGN BULBS INOP. REMOVED AND REPLACED BULBS PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,665 hrs · 62,334 cycles

L2 DOOR EMERGENCY EVAC SIGN BULBS INOP. REMOVED AND REPLACED BULBS PER AMM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 72,665 hrs · 62,334 cycles

COCKPIT FLOOR CRACKED AT BS 246, RBL 23. REPAIRED COCKPIT FLOOR PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,665 hrs · 62,334 cycles

L2 DOOR FUSELAGE SKIN CUTOUT CRACKED AT BS 987, STR 6L. REPAIRED SKIN IAW SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 72,665 hrs · 62,334 cycles

RIGHT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 72,665 hrs · 62,334 cycles

RIGHT WING O/B AFT FLAP I/B UPPER AND LOWER SURFACES DELAMINATED. REPAIRED AFT FLAP IAW SRM AND SB.

Part: WEB — CRACKED (NLG WW) · airframe 72,665 hrs · 62,334 cycles

LEFT NOSE WHEEL WELL WEB CRACKED AT BS 251.7, WL 177. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 72,665 hrs · 62,334 cycles

RIGHT NOSE WHEEL WELL WEB CRACKED BETWEEN BS 246 TO BS 248, WL 169. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 72,665 hrs · 62,334 cycles

LEFT NOSE WHEEL WELL WEB CRACKED BETWEEN BS 246 TO BS 249, WL 169. REMOVED AND REPLACED WEB SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,801 hrs · 61,657 cycles

FUSELAGE SKIN CRACKED AT BS 487, STR 16R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,801 hrs · 61,657 cycles

FUSELAGE SKIN CRACKED AT BS 424, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,801 hrs · 61,657 cycles

SKIN CRACKED AT BS 487, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,801 hrs · 61,657 cycles

SKIN CRACKED BS 424, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,801 hrs · 61,657 cycles

SKIN CRACKED BS 520, STR 15R. REPAIRED SKIN IAW SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 71,798 hrs · 61,655 cycles

LT WING NR 3 SLAT TRAILING EDGE INNER SURFACE DELAMINATED. REMOVED AND REPLACED NR 3 SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,798 hrs · 61,655 cycles

SKIN CRACKED AT BS 517, STR 15R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,798 hrs · 61,655 cycles

SKIN CRACKED AT BS 487, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,798 hrs · 61,655 cycles

SKIN CRACKED AT BS 424, STR 16R. REPAIRED SKIN PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 71,798 hrs · 61,655 cycles

LT WING NR 3 SLAT UPPER OUTBD CORNER IS DELAMINATED. REMOVED AND REPLACED NR 3 SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,798 hrs · 61,655 cycles

SKIN CRACKED AT BS 727D+2, STR 19R. REPAIRED SKIN PER SRM.

Part: LIGHT — DAMAGED (CABIN) · airframe 71,798 hrs · 61,655 cycles

RT EEPLS DAMAGED AT ROW 8. REMOVED AND REPLACED EEPLS PER AMM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,812 hrs · 60,897 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED BETWEEN BS 908 TO BS 947, STR 18L. REMOVED AND REPLACED STRINGER IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,812 hrs · 60,897 cycles

DURING SCHEDULED SPV CHECK FOUND, FRAME CRACKED AT BS 639, RBL 65.5. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,812 hrs · 60,897 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 866 TO BS 872, STR 1. REPAIRED SKIN IAW ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,812 hrs · 60,897 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 18L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,812 hrs · 60,897 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 927, BETWEEN STR 18L TO STR 19L. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,812 hrs · 60,897 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 21L. REMOVED AND REPLACED CLIP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,812 hrs · 60,897 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 908 TO BS 1016, BETWEEN STR 20L TO STR 25L. REPAIRD SKIN IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 70,812 hrs · 60,897 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 22L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,812 hrs · 60,897 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 946, STR 25L. REMOVED AND REPLACED STRINGER PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 70,812 hrs · 60,897 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 1 SLAT LOWER T/E SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,812 hrs · 60,897 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 827+6 TO BS 827+7, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,812 hrs · 60,897 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 927+4 TO BS 924+5, STR 22R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,812 hrs · 60,897 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 787+17 TO BS 787+19, STR 18L. REPAIRED SKIN PER SRM.

Part: TIRE — FAILED (NR 1) · airframe 69,877 hrs · 60,168 cycles

NR 1 MAIN TIRE BLEW ON TAKEOFF.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,439 hrs · 61,575 cycles

DURING SCHEDULED 24Y CHECK FOUND, FLOORBEAM CRACKED BETWEEN BS 663.75 TO BS 670, RBL 24.5. REPAIRED BEAM IAW EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,540 hrs · 59,928 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 68,796 hrs · 59,388 cycles

DURING SCHEDULED MV3 CHECK, FOUND FWD I/B FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,603 hrs · 59,247 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR FWD HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,603 hrs · 59,247 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR FWD HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT MAIN WHEEL WELL BULKHEAD SUPPORT ANGLE CRACKED. REPAIRED BRACKET PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 670.5, BL 0. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 660, BL 0. REPAIRED WEB PER EA.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND KEEL BEAM WEB CRACKED AT BS 500D, STR 28R. REMOVED AND REPLACED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 675, BL 0. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM T-CAP CRACKED AT BS 660, BL 0. REPAIRED T-CAP PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, FROM RBL 1 TO RBL 4. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED SPLICE PER SRM.

Part: FLAP — CRACKED (RT WING) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING O/B MID FLAP L/E CRACKED. REPAIRED MID FLAP PER SRM.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR INNER FRAME CRACKED AT 6TH STOP FITTING FROM UPPER END. REMOVED AND REPLACED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, RBL 8. REMOVED AND REPLACED SHEAR TIE PER BAC DWG AND SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO FRAME ANGLE CORRODED AT BS 847, RBL 8. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 12L. REMOVED AND REPLACED CLIP PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 29L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STUB FRAME CRACKED AT BS 294.5. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED STRINGER PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 28L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: DOOR FRAME — CRACKED (CARGO BAY) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO DOOR INTERIOR AFT EDGE FRAME CORNER CRACKED. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND FAIL SAFE CHORD CORRODED AT BS 500D, STR 28L. REMOVED AND REPLACED CHORD PER SRM AND BAC DWG.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND FAIL SAFE CHORD CORRODED AT BS 500D, STR 28R. REMOVED AND REPLACED CHORD PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 23R. REMOVED AND REPLACED CLIP PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 420, STR 1. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 20R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CRACKED AT BS 540, STR 26L. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 760, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,688 hrs · 58,522 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: SPINDLE — CRACKED (TE FLAP) · airframe 67,228 hrs · 58,177 cycles

DURING SCHEDULED OTS CHECK, FOUND T/E FLAP NR 8 SPINDLE CRACKED. REMOVED AND REPLACED NR 8 SPINDLE PER SI.

Part: FRAME — CORRODED (FUSELAGE) · airframe 67,192 hrs · 58,152 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME CORRODED AT BS 967, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER ER.

Part: SKIN — CRACKED (R2 DOOR) · airframe 67,192 hrs · 58,152 cycles

DURING SCHEDULED OTS CHECK, FOUND R2 DOOR SKIN LOWER FWD CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 67,189 hrs · 58,151 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FRAME CORRODED AT BS 967, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,982 hrs · 57,986 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 440, STR 16R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 65,788 hrs · 57,082 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 65,620 hrs · 56,966 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 65,620 hrs · 56,966 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 65,620 hrs · 56,966 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROWS 1 AND 13. REMOVED AND REPLACED EEPLS PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 65,591 hrs · 56,943 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,591 hrs · 56,943 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO BAY FRAME CRACKED AT BS 500B, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,591 hrs · 56,943 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO BAY FRAME CRACKED AT BS 500B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,591 hrs · 56,943 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO BAY FRAME CRACKED AT BS 520, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,591 hrs · 56,943 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO BAY FRAME CRACKED AT BS 500C, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,591 hrs · 56,943 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO BAY FRAME CRACKED AT BS 500D, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,171 hrs · 56,655 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 504D, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 65,018 hrs · 56,548 cycles

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

Part: FLUID — LEAKING (RT WING) · airframe 64,380 hrs · 56,066 cycles

DIVERSION / INFLT SHUTDOWN / DECLARED EMERGENCY. SUSPECTED POSSIBLE FUEL LEAK FROM NR 2 ENGINE. FLUID ON TOP OF WING. NR 2 ENGINE WAS SHUT DOWN PER QRH. FLIGHT WAS DIVERTED TO ORF. REMOVED AND REPLACED FASTENERS ON RT WING UPPER AFT PYLON PER SRM.

Part: WINDOW — ARCED (COCKPIT) · airframe 63,558 hrs · 55,442 cycles

R2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 62,437 hrs · 54,658 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CENTER OVERHEAD EMERGENCY EXIT LIGHT INOP. SECURED BATTERY PER MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 62,437 hrs · 54,658 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 L/E SLAT AFT WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 62,437 hrs · 54,658 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING NR 5 SLAT T/E WEDGE O/B END DELAMINATED. REPAIRED WEDGE PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 62,437 hrs · 54,658 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM PRESSURE DECK WEB CRACKED AT BS 664, LBL 24. REPAIRED WEB PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 62,163 hrs · 54,454 cycles

R1 EMERGENCY EXIT SLIDE COVER LOOSE. REPOSITIONED COVER PER MM.

Part: SKIN — DELAMINATED (NR 2 SLAT) · airframe 62,077 hrs · 54,385 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING NR 2 L/E SLAT INBOARD END DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: LIGHT — CRACKED (R2 DOOR) · airframe 62,077 hrs · 54,385 cycles

DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FRAME — CRACKED (BS 500C S8R) · airframe 62,077 hrs · 54,385 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,077 hrs · 54,385 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME CORRODED AT LOWER END. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 827 S8L) · airframe 62,077 hrs · 54,385 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 360 S20R) · airframe 62,077 hrs · 54,385 cycles

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

Part: SHEAR TIE — CRACKED (BS 967 S27R) · airframe 62,077 hrs · 54,385 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 706 S8L) · airframe 62,077 hrs · 54,385 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 727A S8R) · airframe 62,077 hrs · 54,385 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 706 S8R) · airframe 62,077 hrs · 54,385 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 62,077 hrs · 54,385 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 360 S13L) · airframe 62,077 hrs · 54,385 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 440 S8L) · airframe 62,077 hrs · 54,385 cycles

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

Part: STRINGER CLIP — CRACKED (BS 277 S10R/L) · airframe 62,077 hrs · 54,385 cycles

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

Part: FRAME — CRACKED (BS 727E S8L) · airframe 62,077 hrs · 54,385 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 887 S8L) · airframe 62,077 hrs · 54,385 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 480 S8L) · airframe 62,077 hrs · 54,385 cycles

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

Part: FRAME — CRACKED (BS 907 S8R) · airframe 62,077 hrs · 54,385 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 727B S8L) · airframe 62,077 hrs · 54,385 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500C S8L) · airframe 62,077 hrs · 54,385 cycles

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

Part: FRAME — CRACKED (BS 887 S7L) · airframe 62,077 hrs · 54,385 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 7L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 344 S10R) · airframe 62,077 hrs · 54,385 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 597 S8R) · airframe 62,077 hrs · 54,385 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 380 S23L) · airframe 62,077 hrs · 54,385 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 867 S8L) · airframe 62,077 hrs · 54,385 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 597 S8L) · airframe 62,077 hrs · 54,385 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 559 S8R) · airframe 62,077 hrs · 54,385 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 767 S8L) · airframe 62,077 hrs · 54,385 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,920 hrs · 53,553 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 979, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,920 hrs · 53,553 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AFT ENTRY DOOR FWD LOWER CORNER. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,920 hrs · 53,553 cycles

DURING SCHEDULED HC1 CHECK, FOUND STRINGER CLIP CRACKED AT BS 986, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (BS 520 S28L) · airframe 59,145 hrs · 52,213 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 28L. REPAIRED SKIN PER SWA EA.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 59,145 hrs · 52,213 cycles

DURING SCHEDULED HC2 CHECK, FOUND NLG W/W CEILING PANEL CRACKED AT BS 259, RBL 7.75. REPAIRED CEILING PANEL PER ACO.

Part: PANEL — CRACKED (NLG W/W) · airframe 59,145 hrs · 52,213 cycles

DURING SCHEDULED HC2 CHECK, FOUND NLG W/W CEILING PANEL CRACKED AT BS 259, LBL 7.75. REPAIRED CEILING PANEL PER ACO.

Part: ACTUATOR — DAMAGED (NR 4 SPOILER) · airframe 57,770 hrs · 51,149 cycles

LEFT WING NR 4 SPOILER OUTBOARD ACTUATOR MOUNT LOBE SHEARED. REMOVED AND REPLACED SPOILER ACTUATOR PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 57,358 hrs · 50,828 cycles

DURING SCHEDULED HC1 CHECK, FOUND LEFT WING INBOARD FORE FLAP DELAMINATED INBOARD UPPER SURFACE. REMOVED AND REPLACED FORE FLAP PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 57,358 hrs · 50,828 cycles

DURING SCHEDULED HC1 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 56,725 hrs · 50,343 cycles

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

Part: STRINGER — CORRODED (BS 327 S28R) · airframe 55,248 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 28R CORRODED AT BS 327. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT AND RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED HORIZONTAL STAB FITTING PER SRM.

Part: SKIN — CORRODED (BS 907-1016 S20R) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 907 TO BS 1016, STR 20R. REPAIRED SKIN PER ER.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME WEB CRACKED AT LOWER OUTBOARD STOP FITTING. REMOVED AND REPLACED FRAME PER SRM.

Part: RIB — CRACKED (LT WING) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING RIB CRACKED AT STA 135.5 AFT LOWER CHORD. REPAIRED WING RIB PER ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 2L. REPAIRED FRAME SECTION PER ER.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT AND RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER ER.

Part: STRINGER — CORRODED (BS 467) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 28L, CORRODED AT BS 467. REPAIRED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CORRODED (BS 380) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 380, LBL 4, WL 148. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (BS 287 S24R) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 287, STR 24R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: HINGE FITTING — CORRODED (RT SPOILER) · airframe 55,248 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 9 SPOILER OUTBOARD HINGE INBOARD MOUNT CORRODED. REMOVED AND REPLACED SPOILER PER MM.

Part: TORQUE TUBE — CORRODED (MID FLAP) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 14R. REPAIRED FRAME SECTION PER SRM.

Part: TORQUE TUBE — CORRODED (MID FLAP) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO DOOR CUTOUT, AFT FRAME CRACKED AT LOWER DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 14L CRACKED AT BS 900. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 277, STR 24R. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM WEB CORRODED AT BS 1016, LBL 19. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND SRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 65 AND LBL 65. REPAIRED FRAME PER BOEING SB.

Part: SKIN — DELAMINATED (LT AILERON) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING AILERON OUTBOARD T/E UPPER SURFACE DELAMINATED. REMOVED AND REPLACED LT WING AILERON PER MM.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT AND RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED STAB FITTING PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 361 S15L) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 361, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 767 S4L) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616 S4L) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 22R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 312, RBL 5 TO LBL 60. REMOVED AND REPLACED FLOORBEAM CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 20R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD ENTRY DOOR CUTOUT, FWD FRAME CORRODED AT BS 303, LBL 60, WL 210. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO DOOR CUTOUT, FWD FRAME WEB CRACKED AT BS 440, STR 24R. REMOVED AND REPLACED FRAME WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L AND STR 8R. REMOVED AND REPLACED FRAME SECTION IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED FRAME SECTION IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REMOVED AND REPLACED FRAME SECTION IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8L. REMOVED AND REPLACED FRAME SECTION IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REMOVED AND REPLACED FRAME SECTION IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER SPLICE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 55,428 hrs · 49,310 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED STRINGER SPLICE IAW SRM.

Part: SKIN — CRACKED (BS 942 S24L) · airframe 54,522 hrs · 48,631 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942.750, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 727E S18R) · airframe 54,522 hrs · 48,631 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 18R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 54,019 hrs · 48,243 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: GLOWSTRIP — WORN (RO 1 AND 6) · airframe 53,030 hrs · 47,461 cycles

DURING SCHEDULED C1 CHECK, FOUND PHOTOLUMINESCENT STRIP WORN BETWEEN ROW 1 AND ROW 6. REMOVED AND REPLACED STRIP PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,957 hrs · 47,408 cycles

DURING SCHEDULED A2 CHECK, FOUND LT AFT GALLEY EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: GATE — CRACKED (R2 DOOR) · airframe 52,109 hrs · 46,704 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR UPPER & LOWER GATES CRACKED AT FASTENER HOLES. REMOVED AND REPLACED R2 DOOR PER MM.

Part: ENGINE — MAKING METAL (LEFT) · airframe 52,109 hrs · 46,704 cycles

DURING SCHEDULED C4 CHECK, FOUND SEVERAL METAL PARTICLES AT THE NR 1 ENGINE FWD SCAVENGE SCREEN. REMOVED AND REPLACED NR 1 ENGINE PER MM.

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 52,109 hrs · 46,704 cycles

DURING SCHEDULED C4 CHECK, FOUND 2 EA AFT CARGO DOOR SKIN CRACKS AT SECOND ROW LIGHTENING HOLES. REPAIRED SKIN PER SRM.

Part: ENGINE — MAKING METAL (NR 1) · airframe 51,620 hrs · 46,304 cycles

DURING SCHEDULED RON CHECK, NR 1 ENGINE FWD SUMP CHIP DETECTOR HAD EXCESSIVE METAL & PHENOLIC DEBRIS. REMOVED AND REPLACED NR 1 ENGINE PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 51,395 hrs · 46,132 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER UPON DOOR OPENING. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,905 hrs · 45,742 cycles

DURING SCHEDULED A1 CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS FROM BS 967 TO BS 986, STRINGER 23L. REPAIRED SKIN SECTIONS PER EA.

Part: BEAM — CRACKED (R1 DOOR) · airframe 50,176 hrs · 45,184 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR NR 1 WEB BEAM, CRACKED. REMOVED AND REPLACED FWD SERVICE DOOR PER MM.

Part: SLIDE — OUT OF ADJUST (R1&R2 DOORS) · airframe 50,176 hrs · 45,184 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R1 AND R2 DOOR EVAC SLIDES PER MM.

Part: FAN — FAULTY (E&E BAY) · airframe 50,160 hrs · 45,172 cycles

PAX AND F/A REPORT STRANGE SMELL IN CABIN. SMELL OF SULFUR, TURNED OFF RECIRC FAN, SMELL DISSIPATED. GASPER FAN C/B TRIPPED. REMOVED AND REPLACED GASPER FAN PER MM.

Part: FITTING — CORRODED (LT WING) · airframe 49,664 hrs · 44,789 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT WING MLG AFT STABILIZER FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,627 hrs · 44,757 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 847, STRINGER 25R, CORRODED. REPAIRED SHEAR TIE PER EA.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 49,627 hrs · 44,757 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR LOWER STOP FITTING GUSSET CRACKED. REMOVED AND REPLACED DOOR GUSSET PER SRM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 49,627 hrs · 44,757 cycles

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM AT BS 727, RBL 6.30, CRACKED. REPAIRED KEEL BEAM PER EA.

Part: ATTACH FITTING — BROKEN (LT ELEVATOR) · airframe 49,627 hrs · 44,757 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT ELEVATOR TAB ATTACH LUG FOR INBOARD CONTROL ROD BROKEN. REMOVED AND REPLACED LEFT ELEVATOR TAB PER MM.

Part: CONTROL ROD — WORN (LT ELEVATOR) · airframe 49,627 hrs · 44,757 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT ELEVATOR TAB OUTBOARD CONTROL ROD END WORN. REMOVED AND REPLACED LEFT OUTBOARD CONTROL ROD PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 49,627 hrs · 44,757 cycles

DURING SCHEDULED 1/4D CHECK, FOUND ALL PHOTOLUMINESCENT STRIPS WORN. REMOVED AND REPLACED ALL PHOTOLUMINESCENT STRIPS PER EA.

Part: WEDGE — SEPARATED (RT WING FLAP) · airframe 49,627 hrs · 44,757 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD T/E MID FLAP WEDGE SEPARATED. REPAIRED WEDGE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,627 hrs · 44,757 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 581, STRINGER 2L, CRACKED. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,627 hrs · 44,757 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER TIE CLIP AT BS 706, STRINGER 1L, CRACKED. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 48,737 hrs · 44,026 cycles

DURING SPV, FOUND BULKHEAD WEB AT BS 178, RBL 6 TO RBL 10, CRACKED. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 48,066 hrs · 43,498 cycles

RT FWD CABIN EEPLS COVER BROKEN. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,471 hrs · 42,199 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER FWD CORNER CUT OUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 45,582 hrs · 41,485 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT CARGO DOOR OUTER SKIN CRACKED AT UPPER AFT CORNER OF HANDLE CUTOUT. REPAIRED SKIN PER SRM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 44,645 hrs · 40,752 cycles

DURING SCHEDULED C4 CHECK, SWA SI 11139-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 1 AND NR 2 HINGE HARDWARE AND BUSHINGS PER MM.

Part: SLIDE — OUT OF ADJUST (FWD CABIN DOORS) · airframe 44,645 hrs · 40,752 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: RECEPTACLE — FAULTY (E/E COMP) · airframe 44,062 hrs · 40,293 cycles

DIVERSION, AFTER DEPARTURE NLG FAILED TO RETRACT, GEAR HANDLE WAS CYCLED, NLG GREEN AND RED LIGHTS REMAINED ILLUMINATED. REMOVED AND REPLACED RECEPTACLE FOR NOSE GEAR LATCHING RELAY PER MM.

Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 41,824 hrs · 38,479 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 41,376 hrs · 38,111 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 199 AT RBL 7. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,376 hrs · 38,111 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CAPT'S WINDOW POST SKIN CRACKED AT LOWER RADIUS. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,376 hrs · 38,111 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 296, STR 10L. REPAIRED SKIN PER SWA RA.

Part: FLAP — DELAMINATED (RT WING) · airframe 41,376 hrs · 38,111 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT OTBD AFT T/E FLAP DELAMINATED JUST OTBD OF NR 7 CANOE FAIRING. REMOVED AND REPLACED AFT T/E FLAP PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 41,376 hrs · 38,111 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT BS 520 AT STR 16L AND BS 663 AT STR 10L. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: BRACKET — CORRODED (FWD SVC DOOR) · airframe 41,376 hrs · 38,111 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK BRACKET CORRODED. REMOVED AND REPLACED HOOK BRACKET PER SRM

Part: WEB — CRACKED (FUSELAGE) · airframe 41,376 hrs · 38,111 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD WEB CRACKED (3 EA) AT BS 178, RBL 7.0, WL 201, WL 213 AND WL 211. REPAIRED WEB PER SRM.

Part: DOOR — CRACKED (AFT CARGO DOOR) · airframe 40,822 hrs · 17,651 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR CRACKED .375 INCH ON FWD FRAME. REMOVED AND REPLACED DOOR PER MM.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 40,822 hrs · 37,651 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.

Part: SLIDE — LOOSE (AFT SVC DOOR) · airframe 40,822 hrs · 37,651 cycles

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

Part: BRACKET — MISSING (FWD SVC DOOR) · airframe 40,822 hrs · 37,651 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY AFT BRACKET MISSING FASTENER. INSTALLED FASTENER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,621 hrs · 37,484 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, ABOVE STR 16R. REPAIRED SKIN PER SRM.

Part: COVER — MISSING (CABIN) · airframe 40,570 hrs · 37,445 cycles

EEPLS WIRES EXPOSED AT AFT LOUNGE AREA.. INSTALLED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 39,003 hrs · 36,158 cycles

EEPLS COVER MISSING AT ROW 5. INSTALLED COVER PER MM.

Part: RETAINER — LOOSE (CABIN) · airframe 38,135 hrs · 35,398 cycles

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY FLASHLIGHT HOLDER LOOSE, FWD INBD LIGHT. SECURED HOLDER PER MM.

Part: TRACK — LOOSE (CABIN) · airframe 38,135 hrs · 35,398 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK LOOSE AT ROW 15. RESECURED TRACK PER MM.

Part: COVER — BROKEN (CABIN) · airframe 38,058 hrs · 35,336 cycles

EEPLS FLOOR TRACK COVER BROKEN AT ROW 8. R&R TRACK COVER PER MM.

Part: COVER — BROKEN (CABIN) · airframe 38,048 hrs · 35,326 cycles

EEPLS TRACK COVER BROKEN AT ROW 8. R&R EEPLS TRACK COVER AND 1 EA. LENS PER MM.

Part: IRU — FAILED (E&E BAY) · airframe 37,819 hrs · 35,134 cycles

DIVERSION, NR 2 IRU FAULT LIGHT ILLUMINATED DURING CRUISE. REMOVED AND REPLACED NR 2 IRU PER MM, OPS CHECK GOOD.

Part: LENS — MISSING (CABIN) · airframe 37,694 hrs · 35,029 cycles

DURING SCHEDULED A2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 37,358 hrs · 34,761 cycles

DURING SCHEDULED SERVICE CHECK, FOUND NR 2 L/E SLAT INBD EDGE OF T/E WEDGE DELAMINATED. REPAIRED SLAT PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 37,180 hrs · 34,629 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT RBL 1.0, WL 206. REPAIRED BULKHEAD WEB PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 37,180 hrs · 34,629 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND RT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED AFT FLAP PER MM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 37,180 hrs · 34,629 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 663 BULKHEAD STIFFENER CRACKED AT LBL 6.5. REMOVED AND REPLACED STIFFENER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,180 hrs · 34,629 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND T-CHORDS CRACKED AT BS 178, WL 207, LBL 28.0 & RBL 28.0. REPAIRED T-CHORDS PER RA''S.

Part: BEAM — CRACKED (FUSELAGE) · airframe 37,180 hrs · 34,629 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT RBL 17.1, WL 228. REPAIRED VERTICAL BEAM WEB PER RA 1-353-2435.

Part: PANEL — LEAKING (LT WING) · airframe 36,471 hrs · 34,072 cycles

DIVERSION, PAX REPORTED FUEL LEAKING OUT OF PANEL ON UPPER SURFACE OF LT WING. RESEALED DOME NUTS AND REMOVED AND REPLACED PANEL PER MM.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 35,486 hrs · 33,253 cycles

FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER INADVERTENTLY. REINSTALLED SLIDE ASSY PER MM.

Part: COVER — LOOSE (CABIN) · airframe 35,318 hrs · 33,114 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER LOOSE AT MID CABIN. R&R TRACK COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,676 hrs · 32,559 cycles

EEPLS INOP AT OVERWING EXIT. RELAMPED EEPLS PER MM.

Part: LIGHT — MISSING (CABIN)

EEPLS LIGHT ASSY MISSING AT OVERWING EXIT. REPLACED LIGHT ASSY DURING RON CHECK PER MM.

Part: LINE — LOOSE (AIR DATA COMP)

AIR TURNBACK, AFTER TAKEOFF, LOST AIRSPEED, ALTITUDE INDICATIONS. WARNING HORN WENT OFF. FOUND LINE TO AIR DATA COMPUTER LOOSE. REINSTALLED LINE PER MM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 12. REPAIRED BULKHEAD PER SRM.

Part: LIGHT — INOP (CABIN)

DURING SCHEDULED 1/2D CHECK, FOUND EEPLS INOP AT ROW 20. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — CRACKED (CABIN)

DURING SCHEDULED 1/2D CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROWS 4 THROUGH 8. REMOVED AND REPLACED TRACK COVER PER MM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 9. REPAIRED CRACKED PER SRM.

Part: LIGHT — MISSING (CABIN)

DURING SCHEDULED 1/4D CHECK, FOUND EEPLS FWD AND AFT END CAPS MISSING. REPLACED END CAPS PER MM.

Part: LIGHT — INOP (CABIN)

DURING SCHEDULED C3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LAMP — INOP (CABIN)

DURING SCHEDULED SC CHECK, FOUND SEVERAL FLOOR EMERGENCY EGRESS LIGHTS INOP. REPAIRED LIGHTING SYSTEM PER BOEING MM.

Part: HPT BLADE — DAMAGED (NR 1 ENGINE)

REPLACING NUMBER 1 ENGINE DUE TO BORESCOPE FINDINGS, HPT BLADE DAMAGE. REPLACED ENGINE ASSEMBLY PER BOEING M/M.

Part: FRAMES — DENTED (BS 747/767/787)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES DENTED AT BS 747 WL 156 AND BS 767, RBL 22, AND AT BS 787, RBL 24 TO 31, AT BS 907, RBL 24, AND AT BS 727, RBL 5.7. REPAIRED PER BOEING SRM.

Part: FRAME — GOUGED (BS 211)

DURING SCHEDULED D-CHECK, FOUND AFT FACE OF FRAME WEB GOUGED AT BS 211, RBL 38. REPAIRED PER BOEING SRM.

Part: STRINGER — CORRODED (BS 907)

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, S23R. REPAIRED PER BOEING SRM.

Part: KEEL BEAM — CHAFED (BS 680-725)

DURING SCHEDULED D- CHECK, FOUND CHAFING DAMAGE TO KEEL BEAM FLANGE TOP SIDE AT BOLT HOLE LOCATIONS, BS 680 TO 725.5. REPAIRED PER TRAMCO EWO 97-0346.

Part: STRINGER — GOUGED (BS 977)

DURING SCHEDULED D-CHECK, FOUND STRINGER 24L GOUGED AT BS 977. REPAIRED PER BOEING SRM.

Part: KEEL BEAM — CHAFING (BS 716/720/725)

DURING SCHEDULED D-CHECK, FOUND CHAFING DAMAGE TO KEEL BEAM FLANGE TOP SIDE, AT BS 716, 720, 725.5. REPAIRED PER TRAMCO EWO 97-0346.

Part: WEB — DAMAGED (BS 1019)

DURING SCHEDULED D-CHECK, FOUND WEB DAMAGED AT BS 1019, RBL 0-3. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (BS 871-886)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED UNDER DORSAL FIN, AT BS 871 TO 886. REPAIRED PER BOEING SRM.

Part: CLIP — CRACKED (BS 947.5)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACK AT BS 947.5, S26R. REPLACED PER BOEING SRM.

Part: BULKHEAD — DENTED (BS 178)

DURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD BS 178 DENTED AT RBL 33, WL 166. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5, AT RBL 43, 35, 23, LBL 43, 35, 25, 21. REPAIRED PER TRAMCO EWO 97-0306.

Part: FLOORBEAM — CORRODED (BS 967)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 967, AT RBL 42, WL 208. REPAIRED PER BOEING SRM.

Part: STRAP — CRACKED (BS 312)

DURING SCHEDULED D-CHECK, FOUND STABILIZER STRAP CRACKED AT BS 312, AT RBL 32, WL 200. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 375)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 375, BELOW S24R, AT BS 402, BELOW S15L AND AT BS 460, AT S27R. REPAIRED PER BOEING SRM.

Part: CONTROLLER — FAILED (CABIN)

RT WING BODY OVERHEAT LIGHT ILLUMINATED DURING CRUISE. LIGHT EXTINGUISHED AFTER EXECUTING QRH PROCEDURES, THEN COULD NOT CONTROL CABIN PRESSURE AT 4,000 FT. AIRCRAFT LANDED WITHOUT INCIDENT AT STL. REPLACED PRESSURE CONTROLLER AND OUTFLOW VALVE. UNABLE TO DUPLICATE WING BODY OVERHEAT. INSPECTED, NO LEAKS.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED C1 CHECK, FOUND A CRACK IN THE TOP CORNER OF FWD SERVICE DOOR LOWER HINGE CUTOUT AT PREVIOUS STOPPED DRILLED CRACK. REPAIRED PER SWA RA 1-352-0247.

Part: WIRE — BROKEN (CABIN)

DURING PRE-FLIGHT CHECK, FOUND EMERGENCY EXIT FLOOR TRACK LIGHTS AT EXIT INOP. REPAIRED BROKEN WIRES AND OP CHECKED PER BOEING M/M.

Part: WIRE — BROKEN (CABIN)

FOUND CABIN FLOOR TRACK LIGHTING INOP AT EMERGENCY EXITS. REPAIRED BROKEN WIRES AND MISSING LIGHT SOCKETS PER BOEING M/M.

Part: EEL BATT HOUSING — FAILED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND CABIN FORWARD SECTION OF FLOOR TRACK LIGHTING INOP. REPLACED BATTERY CHARGER HOUSING PER BOEING M/M.