N512SW
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
301 reports on file, 1996-04-25 – 2013-07-23.
Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 68,230 hrs · 63,946 cycles
R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM & MT.
Part: FAN — FAULTY (AC BAY) · airframe 68,021 hrs · 63,700 cycles
DIVERSION/DECLARED EMERGENCY AT CRUISE FL 370, F/A REPORTED STRONG ELECTRICAL BURNING SMELL IN FWD GALLEY AREA. R & R AIR RECIRCULATION FAN IAW MM.
Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 67,489 hrs · 63,135 cycles
LEFT ELEVATOR MISSING OUTER LAYER OF FIBERGLASS ON UPPER SURFACE. REMOVED AND REPLACED LEFT ELEVATOR IAW M/M.
Part: LENS — MISSING (CABIN) · airframe 67,381 hrs · 63,015 cycles
RIGHT OVERWING EMERGENCY EXIT LENS MISSING. INSTALLED REPLACEMENT LENS IAW M/M.
Earlier reports · 1996–2012 · 297 reports
2012
Part: CONTROLLER — FAULTY (E&E BAY) · airframe 66,853 hrs · 62,474 cycles
DIVERSION / DECLARED EMERGENCY -- CABIN ALTITUDE WARN HORN ACTIVATED. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER PER MM.
Part: FUSE — BLOWN (CABIN) · airframe 66,747 hrs · 62,373 cycles
EMERGENCY LIGHTS INOP AT GALLEY AREA. REPLACED FUSE IAW AMM.
Part: WEB — CRACKED (NLG WW) · airframe 66,747 hrs · 62,373 cycles
CRACK ON WEB LOCATED AT BSTA 227.8 TO BSTA 231 OF NOSE LANDING GEAR NOSE WHEEL WELL. REPLACED WEB LOCATED AT BS 227.8 TO BS 259.5 OF NOSE LANDING GEAR WHEEL WELL IAW SRM B737-500 51-10-02 ITEM 8, SRM B737-500 51-40-02 AND DWG 002180.
Part: FAIRING — CRACKED (TE FLAP) · airframe 66,747 hrs · 62,373 cycles
CRACK ON NR 2 FLAP TRACK FAIRING (AFT, ATTACHED TO CENTER FAIRING). REPAIRED NR 2 FLAP TRACK FAIRING (AFT, ATTACHED TO CENTER FAIRING) IAW SRM 51-70-17-0G-0 PARA 4I REP 9.
Part: LENS — BROKEN (CABIN) · airframe 66,747 hrs · 62,373 cycles
BROKEN LENS OF EMERGENCY EXIT LIGHT LOCATED BETWEEN FWD LAV AND GALLEY NR 1. REPLACED LENS OF EMERGENCY EXIT LIGHT LOCATED BETWEEN FWD LAV AND GALLEY NR 1 IAW AMM 33-51-81.
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON SUPPORT ANGLE LOCATED BS 291 TO BS 294.5 RBL 60 UNDER FLOOR STRUCTURE AREA OF PAX CABIN. REPLACED SUPPORT ANGLE LOCATED BS 291 TO BS 294.5 RBL 60 UNDER FLOOR STRUCTURE IAW SRM 737-500 51-10-02 ITEM 8 AND 51-40-02 AND DRAWING 65-45875.
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON SUPPORT ANGLE AT BS 294.5 STR 23L INTERNAL AREA OF NOSE LANDING GEAR. REPLACED ANGLE IAW SRM AND DWG.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON FRAME (SHEAR TIE) LOCATED AT BS 520 AND BETWEEN STR 21R TO STR 22R FWD CARGO COMPARTMENT. REPAIRED FRAME (SHEAR TIE) LOCATED AT BS 520 AND BETWEEN STR 21R TO STR 22R FWD CARGO COMPARTMENT IAW SRM B737-500 53-00-07-2R-7 REPAIR 7 FOR INS
Part: WEB — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON WEB LOCATED AT BS 303 BETWEEN STR 28L TO STR 27R INTERNAL AREA E/E COMPARTMENT. REPLACED WEB LOCATED AT BS 303 BETWEEN STR 28L TO STR 27R INTERNAL AREA E/E COMPARTMENT IAW SRM B737-500 51-10-02 AND DRAWING 65-63879.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK FRAME SHEAR TIE AT BS 520 AND BETWEEN STR 21R TO 22R. REPAIRED SHEAR TIE IAW SRM.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK FRAME SHEAR TIE AT BS 520 AND BETWEEN STR 21R TO 22R. REPAIRED SHEAR TIE IAW SRM.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON FRAME (SHEAR TIE) LOCATED AT BS 520 AND BETWEEN STR 21R TO STR 22R FWD CARGO COMPARTMENT. REPAIRED FRAME (SHEAR TIE) LOCATED AT BS 520 AND BETWEEN STR 21R TO STR 22R FWD CARGO COMPARTMENT IAW SRM B737-500 53-00-07-2R-7 REPAIR 7 FOR INS
Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON STRINGER SPLICE LOCATED AT BS 360 STRINGER 15L IN FWD PAX CABIN. REPLACED STRINGER SPLICE LOCATED AT BS 348 TO BS 368 STRINGER 15L IN FWD PAX CABIN IAW SRM B737-500 51-10-02 ITEM 8 AND DRAWING 65-17685 AND 65-45800.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON TIE CLIP LOCATED ON BS 294.5 STR 12L FWD CABIN. REPLACED TIE CLIP LOCATED ON BS 294.5 STR 12L FWD CABIN IAW SRM B737-500 51-10-02 ITEM 8 SRM B737-500 51-40-02 AND DWG #65-45808.
Part: FITTING — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON CLIP LOCATED ON BS 294.5 AND STR 13L FWD CABIN. REPLACED CLIP LOCATED ON BS 294.5 AND STR 13L FWD CABIN IAW SRM B737-500 51-10-02 AND DRAWING 65-1633.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ANGLE AT GALLEY DOOR BETWEEN BS 277 TO 291.5 STR 11R TO 12R CABIN. REPLACED ANGLE IAW SRM AND DRAWING.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON ANGLE BETWEEN BS 294.5 TO BS 312 AND RBL 32 FWD CABIN.REPLACED ANGLE LOC BETWEEN BS 294.5 TO BS 312 AND RBL 32 FWD CABIN IAW B737-500 SRM 51-10-02 ITEM 8, SRM 51-40-02 AND DRAWING 65C33970.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON TIE CLIP LOCATED AT BSTA 360 LEVEL STR 5L FWD CABIN. REPLACED TIE CLIP LOCATED AT BS 360 LEVEL STR 5L FWD CABIN IAW SRM B737-500 51-10-02 ITEM 8, 51-40-02 SRM B737-500 AND DRAWING 65-58280.
Part: STRAP — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON STRAP LOCATED AT BSTA 344 AND LBL 45.5 UNDER FLOOR STRUCTURE. REPLACED STRAP LOCATED AT BS 344 AND LBL 45.5 UNDER FLOOR STRUCTURE IAW SRM B737-500 51-10-02 ITEM 8 SRM B737-500 51-40-02 AND DRAWING 65C33970.
Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON STRINGER SPLICE LOCATED AT BSTA 360 STR 2L FWD CABIN. REPLACED RIVETS 2EA ON STRINGER SPLICE LOCATED AT BS 360 STR 2L FWD CABIN IAW SRM B737-500 51-40-02 AND DWG 65-45765.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ANGLE AT GALLEY DOOR BETWEEN BS 277 TO 291.5 TO STR 11R CABIN. REPLACED ANGLE IAW SRM AND DRAWING.
Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON THRESHOLD WEB LOWER SURFACE ON BS 294.5 AND TBL 56 UNDER FLOOR STRUCTURE. REPLACED THRESHOLD WEB LOC ON BS 291.5 TO BS 360 STR 17R IAW SRM B737-500 51-10-02 ITEM 8 AND SRM B737-500 51-40-02 DRAWING 65-45875.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ANGLE AT GALLEY DOOR BETWEEN BS 277 TO 291.5 STR 9R TO 10R CABIN. REPLACED ANGLE IAW SRM AND DRAWING.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ANGLE AT GALLEY DOOR BETWEEN BSTA 277 TO 291.5 AT LEVEL STR 9R. REPLACED ANGLE IAW SRM AND DWG.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON ANGLE LOCATED AT BSTA 1006 AND LEVEL STR 2 AFT CABIN. REPLACED ANGLE LOCATED AT BS 1006 AND LEVEL STR 2R AFT CABIN IAW SRM B737-500 51-10-02 ITEM 8 AND DRAWING 65-58293 AND B737-500 51-40-02.
Part: WEB — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON WEB AT BS 947.5 TO BS 967 AND LBL 21 UNDER FLOOR STRUCTURE CABIN. REPLACED WEB IAW SRM AND DRAWING.
Part: PLATE — CRACKED (COWLING) · airframe 66,747 hrs · 62,373 cycles
CRACK ON PLATE LOCATED ON CUT OUT LOWER SIDE OF CSD OIL ACCESS OF THE OUTBOARD FAN COWL. REPLACED PLATE LOCATED ON CUT OUT LOWER SIDE OF CSD OIL ACCESS OF THE OUTBOARD FAN COWL IAW B737-500 SRM 51-40-02 AND DRAWING #314A1127.
Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON STOP PAD LOCATED AT BSTA 616 OF LT ESCAPE HATCH (2 EA). REPLACED STOP PAD LOCATED ON BS 616 AT EMERGENCY EXIT HATCH LT (2EA) IAW SRM 51-40-02.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON TIE CLIP AT BS 927 AND STR 22R IN AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOC AT BS 927 AND STR 22R IN AFT CARGO COMPARTMENT IAW SRM B737-500 51-10-02 ITEM 8 AND DRAWING 65-46559.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON TIE CLIP AT BS 927 AND STR 24R IN AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOC AT BS 927 AND STR 24R IN AFT CARGO COMPARTMENT IAW SRM B737-500 51-10-02 ITEM 8 AND DRAWING 65-46559.
Part: FRAME — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON FRAME HOLE AT BS 482B BETWEEN STR 20L TO STR 21L. REPAIRED FRAME IAW SRM.
Part: CHANNEL — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON CHANNEL AT BS 540 BETWEEN BL 0 TO LBL 24.5 CEILING AREA CARGO COMPARTMENT. REPLACED CHANNEL IAW SRM AND DRAWING.
Part: RETAINER — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON RETAINER LOCATED BETWEEN STA 312 TO STA 328 CUTOUT FWD ENTRY DOOR. REPLACED RETAINER (REVEAL) LOCATED BETWEEN STA 312 TO STA 328 OF CUT OUT FWD ENTRY DOOR, IAW SRM B737-500 51-10-02 ITEM 8 AND DRAWING 65-2983.
Part: FRAME — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON FRAME AT BS 482 BETWEEN STR 20R TO 21R. REPAIRED FRAME IAW SRM.
Part: PLATE — CRACKED (TE FLAP) · airframe 66,747 hrs · 62,373 cycles
CRACK ON PLATE LOCATED MID FLAP AT LEVEL WBL 118 INTERNAL CAVITY LEFT WING. REMOVED AND REPLACED PLATE LOCATED MID FLAP AT LEVEL WBL 118 INTERNAL CAVITY LEFT WING IAW CMM 57-53-24.
Part: WEB — CRACKED (NLG WW) · airframe 66,747 hrs · 62,373 cycles
CRACK ON THE RIGHT SIDE OF THE NLG W/W AT WBL 169.1 AND BS 251.6 - 4.5. REPAIRED WEB IAW SRM.
Part: WEB — CRACKED (NLG WW) · airframe 66,747 hrs · 62,373 cycles
CRACK RIGHT SIDE OF NLG W/W AT BS 251.6 AND WL 185-4.5. REPAIRED WEB IAW SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON EXTERNAL SKIN AT BS 291.5 AND STR 14R IN UPPER FUSELAGE. REPAIRED SKIN IAW EO.
Part: PLATE — CRACKED (LT HORIZ STAB) · airframe 66,747 hrs · 62,373 cycles
CRACK ON PLATE OF THE ACCESS PANEL 9124 L LEFT HORIZONTAL STABILIZER. REPLACED PLATE OF THE ACCESS PANEL 9124L LEFT HORIZONTAL STABILIZER IAW SRM B737-500 51-10-02 ITEM 8 AND SRM 51-40-02.
Part: WEB — CRACKED (NLG WW) · airframe 66,747 hrs · 62,373 cycles
CRACK ON NLG W/W AT BS 259.5 ABOVE REPAIR DOUBLER LEFT SIDE. REPAIRED WEB IAW SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK RIGHT SIDE OF NLG W/W AT WL 169.1 AND BS 251.6-5.5. REPAIRED WEB IAW SRM.
Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 66,747 hrs · 62,373 cycles
CRACK ON SUPPORT ANGLE LOC AT LEVEL OF WBL 71.24 OF THE TREALING EDGE AREA R/T WING. REPLACED SUPPORT ANGLE LOC AT LEVEL OF WBL 71.24 OF THE TRAILING EDGE AREA RT WING IAW SRM B737-500 51-10-02, 51-40-02 AND DRAWING 65-50820.
Part: PAN — CRACKED (L1 DOOR) · airframe 66,747 hrs · 62,373 cycles
CRACK ON LOWER PAM LOCATED AFT EDGE OF FWD ENTRY DOOR. REPLACED SUPPORT PLATE (LOWER PAN) LOC ON EDGE OF FWD ENTRY DOOR IAW SRM B737-500 51-40-02 AND DRAWING 65-49649.
Part: SKIN — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON EXTERNAL SKIN AT BS 306 AND 0.500 UPPER EDGE GALLEY DOOR. REPAIRED SKIN IAW EO AND EA.
Part: SPLICE PLATE — CRACKED (RT WING) · airframe 66,747 hrs · 62,373 cycles
CRACK ON PLATE LOC BETWEEN RSS 196 TO RSS 210 TRAILING EDGE AREA R/T WING. REPLACED SPLICE PLATE LOC BETWEEN RSS 196 TO RSS 210 TRAILING EDGE AREA R/T WING IAW B737-500 SRM 51-10-02 ITEM 8, SRM 51-40-02 AND DRAWING 65-50821.
Part: SPLICE PLATE — CRACKED (LT WING) · airframe 66,747 hrs · 62,373 cycles
CRACK ON PLATE LOCATED AT LEVEL RSS 200 REAR SPAR LT WING INTERNAL CAVITY. REPLACED SPLICE PLATE LOC AT LEVEL RSS 200 T/E LEFT WING IAW B737-500 SRM 51-10-02-0G-0 ITEM 8, SRM 51-40-02-0G-0 AND DRAWING 65-50821.
Part: ANGLE — CRACKED (RT WING) · airframe 66,747 hrs · 62,373 cycles
CRACK ON ANGLE LOC WBL 204.40 TRAILING EDGE AREA AT RIGHT WING. REPLACED ANGLE LOCATED WBL 204.40 TRAILING EDGE AREA AT RIGHT WING IAW B737-500 SRM 51-40-02 AND DRAWING 65C26300.
Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 66,747 hrs · 62,373 cycles
CRACK ON UPPER SUPPORT ANGLE AT LEVEL WBL 188 TRAILING EDGE AREA R/T WING INTERNAL AREA. REPLACED SUPPORT ANGLE (CLIP) AT LEVEL WBL 188 TRAILING EDGE AREA R/T WING INTERNAL AREA IAW B737-500 SRM 51-10-02, SRM 51-40-02 AND DRAWING #65C26300.
Part: PLATE — CRACKED (RT HORIZ STAB) · airframe 66,747 hrs · 62,373 cycles
CRACK ON PLATE OF THE ACCESS PANEL 9224 R RIGHT HORIZONTAL STABILIZER. REPLACED PLATE OF THE ACCESS PANEL 9224R RIGHT HORIZONTAL STABILIZER IAW SRM B737-500 51-10-02 ITEM 8.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON OVAL HOLE LOCATED ON LBL 24.5 BS 667 CENTER WING BOX. REPAIRED FLOORBEAM UPPER CHORD AT LBL 24.82 BETWEEN STA 656 AND STA 685 WING CENTER SECTION IAW EO AEM-HC57-291/12 R0 AND EA 1-557-7751 REV-
Part: PAN — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON EXTERNAL FUSELAGE AT BS 268.25, STR 22R. REPLACED PAN RING IAW SRM AND DWG.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,747 hrs · 62,373 cycles
CRACK ON LONGITUDINAL FLOORBEAM WEB LOCATED AT BS 708 APPROX AT LBL 24.8 CENTER WING BOX. REPAIRED FLOORBEAM WEB AT LBL 24.82 BETWEEN STA 698 AND STA 717 IAW EAN 1-557-7739 AND EO AEM-HC57-290/12 R0
Part: RIVET — CRACKED (LT WING) · airframe 66,743 hrs · 62,370 cycles
LEFT WING IFOT FAIRING INBOARD FLAP TRACK CUTOUT LOWER BRACKET HAS TWO CRACKED RIVETS (MARKED). REMOVED AND REPLACED FASTENERS PER SRM 51-40-02.
Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 66,729 hrs · 62,356 cycles
R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER M/M.
Part: SKIN — CRACKED (FUSELAGE) · airframe 65,262 hrs · 61,324 cycles
R2 DOOR FWD SKIN CRACKED AT UPPER HINGE CUTOUT LWR CORNER. REPAIRED SKIN PER SRM.
Part: PANEL — CRACKED (RT WING) · airframe 66,746 hrs · 62,373 cycles
CRACK ON BOTH SIDES OF FASTENER HOLE ON PYLON/WING PANEL AFT OF 58710R. REPLACED PANEL 5871 OR ON PYLON/WING RIGHT IAW SRM B737-500 51-40-05 AND DWG 65C27356.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 65,091 hrs · 61,205 cycles
R2 DOOR LOWER EMERGENCY EXIT SIGN BULBS INOP. REMOVED AND REPLACED SIGN PER M/M.
Part: WINDOW — ARCED (COCKPIT) · airframe 65,015 hrs · 61,160 cycles
DIVERSION -- L2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED L2 COCKPIT WINDOW ASSY PER MM.
2011
Part: SKIN — CRACKED (FUSELAGE) · airframe 63,242 hrs · 60,052 cycles
DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 947.5+12, STR 21L. REPAIRED SKIN IAW SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,242 hrs · 60,052 cycles
DURING SCHEDULED OTS CHECK, FOUND STRINGER CLIP CRACKED AT BS 986, STR 22L. REMOVED AND REPLACED CLIP IAW SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 63,242 hrs · 60,052 cycles
DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 482B+15, STR 15R. REPAIRED SKIN IAW SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 63,242 hrs · 60,052 cycles
DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 437.5, STR 17R. REPAIRED SKIN IAW SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 63,160 hrs · 60,009 cycles
DURING SCHEDULED SPV CHECK, FOUND RT FRAME INNER CHORD CRACKED AT BS 616, STR 17R. REPAIRED CHORD IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 63,160 hrs · 60,009 cycles
DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 929 TO BS 932, STR 21L. REPAIRED SKIN PER SRM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,160 hrs · 60,009 cycles
DURING SCHEDULED SPV CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB IAW MM.
Part: SUPPORT — DAMAGED (AILERON) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED HEAVY CHECK, FOUND AILERON LATER CONTROL POWER CONTROL SUPPORT BEARING BORE DAMAGED. REPAIRED PER EA.
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 63,066 hrs · 59,946 cycles
DURING SCHEDULED MV1 CHECK, FOUND LT AFT GALLEY EMERGENCY EXIT LIGHT BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: ACTUATOR — CRACKED (SPOILER) · airframe 62,856 hrs · 59,804 cycles
DURING SCHEDULED MV1 CHECK, FOUND LT WING I/B GROUND SPOILER I/B ACTUATOR CRACKED. REMOVED AND REPLACED GROUND SPOILER ACTUATOR PER MM.
Part: FAN — FAULTY (CARGO BAY) · airframe 62,323 hrs · 59,437 cycles
DIVERSION/DECLARED EMERGENCY. FLIGHT ATTENDANTS REPORTED STRONG ELECTRICAL ODOR IN AFT GALLEY AND MID CABIN. STRONG ODOR ALSO NOTICED IN COCK.
Part: SKIN — CRACKED (FUSELAGE) · airframe 62,258 hrs · 59,392 cycles
DURING SCHEDULED MV1 CHECK FOUND, SKIN CRACKED AT BS 807, STR 21L. REPAIRED SKIN PER SRM.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,103 hrs · 41,919 cycles
DURING SCHEDULED 16Y CHECK, FOUND CRACK ON AFT CARGO COMPARTMENT TIE CLIP STA 727A, STR 21L. REPLACED TIE CLIP PER SRM.
Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND LT MLG TRUNNION FITTING LUG FACES CORRODED. REMOVED AND REPLACED FITTING PER EA.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,470 hrs · 58,856 cycles
DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND LT FAIL SAFE CHORD ATTACH FITTING CORRODED AT BS 1088. REPAIRED FITTING PER EA.
Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND RT FAIL-SAFE CHORD ATTACH FITTING CORRODED AT BS 1088. REPAIRED FITTING PER EA.
Part: FITTING — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND RT VERTICAL FIN TERMINAL FITTING CORRODED AT BS 1016. REPAIRED FITTING PER EA.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 669, RBL 24.5. REPAIRED BEAM PER EA.
Part: STRAP — CRACKED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND SKIN STRAP CRACKED BETWEEN BS 370 TO BS 395, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED STRAP PER SRM AND BAC DWG.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 790, RBL 3. REPAIRED CHANNEL PER EA.
Part: SPAR — CRACKED (LT WING) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND LT WING CRACKED ON UPPER CHORD REAR SPAR RSS 223.14. REPAIRED SPAR PER EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 367 STR 28R+8. REPAIRED SKIN EA.
Part: LENS — BROKEN (CABIN) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND LT AFT EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.
Part: FLAP — DELAMINATED (RT WING) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.
Part: SLAT — DELAMINATED (LT WING) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND LT WING NR 2 SLAT O/B EDGE DELAMINATED. REPAIRED SLAT PER SRM.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND STIFFENER CRACKED AT BS 727, STR 27L. REMOVED AND REPLACED STIFFENER PER SRM AND BAC DWG.
Part: FRAME — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND FRAME CORRODED AT BS 460, STR 26R. REPAIRED FRAME PER EA.
Part: FLAP — DELAMINATED (LT WING) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 482, BETWEEN STR 28R TO STR 28L. REPAIRED SHEAR TIE PER SRM.
Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO COMPARTMENT SUPPORT CHANNEL CRACKED AT BS 460, STR 26R. REMOVED AND REPLACED CHANNEL PER SRM AND BAC DWG.
Part: FRAME — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND FRAME CORRODED AT BS 927, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 482, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 3. REPAIRED CHANNEL PER EA.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 751, RBL 3. REPAIRED CHANNEL PER EA.
Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND KEEL BEAM CORRODED AT BS 482B, STR 28L. REPAIRED BEAM PER SRM AND BAC DWG.
Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND KEEL BEAM CORRODED AT BS 706, BETWEEN LBL 45.50 TO LBL 59.0. REPAIRED BEAM PER SRM AND BAC DWG.
Part: FRAME — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND FRAME CORRODED AT BS 482A, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 787+18, STR 23L. REPAIRED SKIN PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 482, BETWEEN STR 24R TO STR 28R. REPAIRED SHEAR TIE PER SRM.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 12.50. REPAIRED CHANNEL PER EA.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 360, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM.
Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 363, STR 16L. REMOVED AND REPLACED SPLICE PER SRM.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, RBL 8.10. REPAIRED CHANNEL PER EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 282, BETWEEN STR 24R TO STR 25R. REPAIRED SKIN PER SRM.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 8.10. REPAIRED CHANNEL PER EA.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED BETWEEN BS 732B TO BS 727C+25, LBL 3. REPAIRED CHANNEL PER EA.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 860, RBL 8.10. REPAIRED CHANNEL PER EA.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 860, LBL 8.10. REPAIRED CHANNEL PER EA.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 860, RBL 3. REPAIRED CHANNEL PER EA.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 860, LBL 3. REPAIRED CHANNEL PER EA.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727B+5, LBL 3. REPAIRED CHANNEL PER EA.
Part: LENS — BROKEN (CABIN) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT ASSY BROKEN AT ROW 9. REMOVED AND REPLACED LENS PER MM.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727B+5, RBL 3. REPAIRED CHANNEL PER EA.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727B+5, RBL 8.10. REPAIRED CHANNEL PER EA.
Part: FRAME — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND FRAME CORRODED AT BS 460, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME PER SRM.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,330 hrs · 58,756 cycles
DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, RBL 3. REPAIRED CHANNEL PER EA.
2010
Part: SKIN — CRACKED (FUSELAGE) · airframe 61,327 hrs · 58,755 cycles
DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 884, STR 25R. REPAIRED SKIN PER SRM.
Part: SKIN — DELAMINATED (SPOILER) · airframe 59,868 hrs · 57,715 cycles
DURING SCHEDULED 2HC2 CHECK, FOUND RT WING O/B NR 7 FLIGHT SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED NR 7 SPOILER PER MM.
Part: SLIDE — LOOSE (L2 DOOR) · airframe 59,732 hrs · 57,617 cycles
L2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MT.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,614 hrs · 57,537 cycles
DURING SCHEDULED MV1 CHECK, FOUND FWD LT OVERHEAD EMERGENCY LIGHT BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,614 hrs · 57,537 cycles
DURING SCHEDULED MV1 CHECK, FOUND FWD RT OVERHEAD EMERGENCY LIGHT BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 59,614 hrs · 57,537 cycles
DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 933, STR 23R. REPAIRED SKIN PER SRM AND EA.
Part: LIGHT — LOOSE (CABIN) · airframe 59,585 hrs · 57,518 cycles
EEPLS LOOSE AT ROW 7. SECURED EEPLS PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,656 hrs · 56,902 cycles
EMERGENCY EXIT LIGHT INOP AT FWD LAV. SECURED LIGHT PER MM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,493 hrs · 56,794 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 482B, STR 20R. REPAIRED FRAME PER SRM.
Part: TAB — CRACKED (AILERON) · airframe 58,493 hrs · 56,794 cycles
DURING SCHEDULED SPV CHECK, FOUND LT WING AILERON TAB END CRACKED. REMOVED AND REPLACED TAB PER MM.
Part: FITTING — LOOSE (GIRT BAR) · airframe 58,493 hrs · 56,794 cycles
DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.
2009
Part: SKIN — CRACKED (FUSELAGE) · airframe 58,105 hrs · 56,567 cycles
DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER EA.
Part: FLAP — DELAMINATED (RT WING) · airframe 57,418 hrs · 56,138 cycles
DURING SCHEDULED MV4 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.
Part: GIRT BAR — CORRODED (L1 DOOR) · airframe 56,676 hrs · 55,667 cycles
DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR CORRODED. REMOVED AND REPLACED GIRT BAR PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 56,676 hrs · 55,667 cycles
DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 784, STR 23L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (BS 303) · airframe 56,180 hrs · 55,358 cycles
DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 303, WL 238. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (BS 304) · airframe 56,180 hrs · 55,358 cycles
DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 304, WL 238. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (BS 304) · airframe 56,180 hrs · 55,358 cycles
DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 304, WL 257. REPAIRED SKIN PER SWA EA.
Part: SPINDLE — WORN (TE FLAP) · airframe 55,816 hrs · 55,079 cycles
DURING T/E FLAP EXTENSION FELT RIGHT ROLL REQUIRING RUDDER TRIM OF 2-3 UNITS. FOUND NR 7 T/E FLAP SPINDLE BEARING WORN. REMOVED AND REPLACED FLAP CARRIAGE & SPINDLE BEARING ASSY PER MM.
2008
Part: COVER — OUT OF POSITION (CABIN) · airframe 55,232 hrs · 54,570 cycles
FWD LT EMERGENCY EXIT LIGHT COVER FELL OFF. INSTALLED COVER PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 55,199 hrs · 54,542 cycles
DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 764, BETWEEN STR 21L TO STR 22L. REPAIRED SKIN PER SRM.
Part: WINDOW — ARCED (COCKPIT) · airframe 55,176 hrs · 54,523 cycles
DURING SCHEDULED MV2 CHECK, FOUND R1 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM.
Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 55,041 hrs · 54,418 cycles
L1 DOOR SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. INSTALLED SLIDE PER MM.
Part: DOOR FRAME — CRACKED (SERVICE DOOR) · airframe 53,460 hrs · 53,193 cycles
DURING SCHEDULED BRDG CHECK, FOUND FWD SERVICE DOOR LOWER FRAME CRACKED AT LOWER FWD CORNER. REPAIRED FRAME PER SRM.
Part: GLOWSTRIP — DELAMINATED (CABIN) · airframe 53,460 hrs · 53,193 cycles
DURING SCHEDULED BRDG CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DELAMINATED AT ROW 10 ABC. REMOVED AND REPLACED STRIP PER MM.
Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 53,460 hrs · 53,193 cycles
DURING SCHEDULED BRDG CHECK, FOUND NLG W/W CEILING PANEL WEB CRACKED AT RBL 7.5. REPAIRED WEB PER ACO.
Part: FRAME — CRACKED (BS 986 S3L) · airframe 53,460 hrs · 53,193 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 986.5, STR 3L. REPAIRED FRAME PER SRM.
Part: FRAME — CRACKED (BS 986 S2L) · airframe 53,460 hrs · 53,193 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 986.5, STR 2L. REPAIRED FRAME PER SRM.
Part: SKIN — WORN (BS 980-1002) · airframe 53,460 hrs · 53,193 cycles
DURING SCHEDULED BRDG CHECK, FOUND UPPER FUSELAGE SKIN WORN BETWEEN BS 980 AND BS 1002, BELOW DORSAL FIN. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (BS 386 S25L) · airframe 53,460 hrs · 53,193 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 386, STR 25L. REPAIRED SKIN PER SRM.
Part: SKIN — WORN (BS 895-930) · airframe 53,460 hrs · 53,193 cycles
DURING SCHEDULED BRDG CHECK, FOUND UPPER FUSELAGE SKIN WORN BETWEEN BS 895 AND BS 930 BELOW DORSAL FIN. REPAIRED SKIN PER EA.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,460 hrs · 43,193 cycles
DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6L. REPAIRED WEB PER SRM.
Part: FITTING — LOOSE (GIRT BAR) · airframe 53,460 hrs · 53,193 cycles
DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM.
Part: FITTING — LOOSE (GIRT BAR) · airframe 53,460 hrs · 53,193 cycles
DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM.
Part: FLAP TRACK — LOOSE (T/E FLAP) · airframe 53,460 hrs · 53,193 cycles
DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING NR 8 FLAP TRACK "A" FRAME LOOSE AT CARRIAGE. REMOVED AND REPLACED FLAP TRACK PER MM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,460 hrs · 53,193 cycles
DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,460 hrs · 53,193 cycles
DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: HOOK — LOOSE (GIRT BAR) · airframe 53,460 hrs · 53,193 cycles
DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,460 hrs · 53,193 cycles
DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,460 hrs · 53,193 cycles
DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 52,971 hrs · 52,819 cycles
DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, STR 16L. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 52,971 hrs · 52,819 cycles
DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 400, STR 15L. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 52,971 hrs · 52,819 cycles
DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 482, STR 16R. REPAIRED SKIN PER SWA EA.
Part: GUIDE — LOOSE (T/E FLAP) · airframe 52,961 hrs · 52,811 cycles
DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD FORE FLAP GUIDE LOOSE. REMOVED AND REPLACED FLAP PER MM.
Part: LUG — CRACKED (NR 5 SPOILER) · airframe 52,961 hrs · 52,811 cycles
DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 GROUND SPOILER ACTUATOR LUG CRACKED. REPAIRED ACTUATOR PER SWA EA.
Part: FLAP — DELAMINATED (RT WING) · airframe 52,961 hrs · 52,811 cycles
DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.
Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 52,961 hrs · 52,811 cycles
DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT DOOR HANDLE CUTOUT. REPAIRED SKIN PER SWA EA.
Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 52,335 hrs · 52,288 cycles
L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
2007
Part: LENS — CRACKED (EMERGENCY LIGHTS) · airframe 52,152 hrs · 52,120 cycles
RT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.
Part: HOOK — LOOSE (GIRT BAR) · airframe 52,027 hrs · 51,999 cycles
DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.
Part: SIGN — MISSING (EMERGENCY EXIT) · airframe 51,771 hrs · 51,756 cycles
FWD CABIN EMERGENCY EXIT SIGN MISSING. INSTALLED EXIT SIGN PER MM.
Part: GLOWSTRIP — WORN (CABIN) · airframe 51,156 hrs · 51,168 cycles
DURING SCHEDULED C2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT RT OVERWING EMERGENCY EXIT ROW. REMOVED AND REPLACED STRIP PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,156 hrs · 51,168 cycles
DURING SCHEDULED C2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 50,262 hrs · 50,265 cycles
DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,829 hrs · 49,846 cycles
DURING SCHEDULED SERVICE CHECK, FOUND RIGHT CEILING MID CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: FAN — FAULTY (A/C BAY) · airframe 49,819 hrs · 49,836 cycles
DIVERSION, ELECTRICAL ODOR IND PAX CABIN. GASPER FAN C/B TRIPPED. REMOVED AND REPLACED GASPER FAN PER MM.
Part: LENS — MISSING (CABIN) · airframe 49,698 hrs · 49,725 cycles
EMERGENCY EXIT LIGHT LENS MISSING AT ROW 16 DEF. INSTALLED LIGHT LENS PER MM.
Part: GLOWSTRIP — LOOSE (CABIN) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND RIGHT FWD CABIN EEPLS PHOTOLUMINESCENT STRIP LOOSE. SECURED STRIP PER MM.
Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.
Part: FRAME — CRACKED (BS 440) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R AND 8L. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (BS 747 S8R) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (BS 727B S8R) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (BS 867) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (BS 827) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (BS 480) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (BS 787) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (BS 907) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (BS 380) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (BS 727B) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME SECTION PER SWA EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME SECTION PER SWA EA.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME SECTION PER SWA EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME SECTION PER SWA EA.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,572 hrs · 49,602 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
2006
Part: SKIN — CRACKED (FUSELAGE) · airframe 49,399 hrs · 49,426 cycles
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (BS 970 S20L) · airframe 49,399 hrs · 49,426 cycles
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 20L. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (BS 730D S18L) · airframe 48,663 hrs · 48,658 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730D, STR 18L. REPAIRED SKIN IAW SRM.
Part: SKIN — CRACKED (BS 944 S25R) · airframe 48,603 hrs · 48,588 cycles
DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 25R. REPAIRED SKIN PER SRM.
Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 48,134 hrs · 48,069 cycles
L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 47,805 hrs · 47,714 cycles
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 765, STR 23L. REPAIRED SKIN PER SWA EA AND SRM.
Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 46,938 hrs · 46,775 cycles
DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY PER MM.
2005
Part: FLOORBEAM — CORRODED (BS 947) · airframe 46,398 hrs · 46,185 cycles
DURING SCHEDULED 1/2D CHECK, FOUND CABIN FLOORBEAM CORRODED AT BS 947.5, LBL 16 TO RBL 6. REPAIRED FLOORBEAM PER SRM.
Part: FLOORBEAM — CORRODED (BS 1016) · airframe 46,398 hrs · 46,185 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 1016, RBL 12 TO RBL 36. REPAIRED FLOORBEAM PER SRM.
Part: SHEAR TIE — CRACKED (BS 360) · airframe 46,398 hrs · 46,185 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, STR 14R TO STR 15R. REPAIRED SHEAR TIE PER SRM.
Part: FLOOR SUPPORT — CRACKED (BS 727B) · airframe 46,398 hrs · 46,185 cycles
DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24.75. REPAIRED FLOORBEAM PER SWA EA.
Part: STRINGER CLIP — CRACKED (BS 663) · airframe 46,398 hrs · 46,185 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER — CRACKED (BS 520) · airframe 46,398 hrs · 46,185 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 520, STR 10R. REPAIRED STRINGER PER SWA EA.
Part: FLOORBEAM — CRACKED (BS 294.5) · airframe 46,398 hrs · 46,185 cycles
DURING SCHEDULED 1/2D CHECK, FOUND CABIN FLOORBEAM UPPER CHORD CRACKED AT BS 294.5, LBL 22 TO LBL 27. REPAIRED FLOORBEAM PER SRM.
Part: BELTFRAME — CRACKED (BS 482) · airframe 46,398 hrs · 46,185 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 482, STR 21L. REPAIRED BELTFRAME PER SWA EA.
Part: SKIN — CRACKED (BS 465-471) · airframe 46,398 hrs · 46,185 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE LOWER SKIN CORRODED BETWEEN BS 465 TO BS 471, AT NR 1 DME ANTENNA. REPAIRED SKIN PER SWA EA AND SRM.
Part: FRAME — CRACKED (FWD CARGO) · airframe 46,398 hrs · 46,185 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, AFT FRAME LOWER STOP FITTING. REPAIRED FRAME PER SWA EA.
Part: BELTFRAME — CRACKED (BS 482A) · airframe 46,398 hrs · 46,185 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 482A, STR 21L. REPAIRED BELTFRAME PER SWA EA.
Part: STRINGER CLIP — CRACKED (BS 294) · airframe 46,398 hrs · 46,185 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294.5, STR 11R. REMOVED AND REPLACED CLIP PER SRM.
Part: FLOORBEAM — CORRODED (BS 967) · airframe 46,398 hrs · 46,185 cycles
DURING SCHEDULED 1/2D CHECK, FOUND CABIN FLOORBEAM CORRODED AT BS 967, RBL 18 TO RBL 42. REPAIRED FLOORBEAM PER SRM.
Part: FRAME — CRACKED (FWD CARGO) · airframe 46,398 hrs · 46,185 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, AFT FRAME NR 2 STOP FITTING. REPAIRED FRAME PER SRM.
Part: FLOORBEAM — CORRODED (BS 344) · airframe 46,398 hrs · 46,185 cycles
DURING SCHEDULED 1/2D CHECK, FOUND CABIN FLOORBEAM CORRODED AT BS 344, BETWEEN BL 0 TO LBL 7.REPAIRED FLOORBEAM PER SWA EA.
Part: FLOORBEAM — CORRODED (BS 328) · airframe 46,398 hrs · 46,185 cycles
DURING SCHEDULED 1/2D CHECK, FOUND CABIN FLOORBEAM CORRODED AT BS 328, BL 0. REPAIRED FLOORBEAM PER SWA EA.
Part: STIFFENER — CORRODED (BS 1016) · airframe 46,398 hrs · 46,185 cycles
DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 AFT PRESSURE BLKHD STIFFENER CHANNEL CORRODED AT 6 O'CLOCK POSITION. REPAIRED STIFFENER CHANNEL PER SWA ACO AND BAC DRAWING.
Part: FLOORBEAM — CORRODED (BS 312) · airframe 46,398 hrs · 46,185 cycles
DURING SCHEDULED 1/2D CHECK, FOUND CABIN FLOORBEAM CORRODED AT BS 312, RBL 35. REPAIRED FLOORBEAM PER SWA EA.
Part: POST — CRACKED (COCKPIT) · airframe 46,398 hrs · 46,185 cycles
DURING SCHEDULED 1/2D CHECK, FOUND L1 COCKPIT WINDOW POST CRACKED AT UPPER OUTBOARD CORNER. REPAIRED WINDOW POST PER SRM.
Part: PRESSURE PANEL — CRACKED (MLG W/W) · airframe 46,398 hrs · 46,185 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 663, LBL 32. REPAIRED WEB PER SRM.
Part: SWITCH — INTERMITTENT (EMERGENCY LIGHT) · airframe 45,778 hrs · 45,549 cycles
DURING SCHEDULED SERVICE CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHTS INTERMITTANT. REMOVED AND REPLACED COCKPIT LIGHT SWITCH PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 45,685 hrs · 45,451 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 10R. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 45,598 hrs · 45,349 cycles
DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 945, STR 24R. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 45,317 hrs · 45,048 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 25R. REPAIRED SKIN PER SRM.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,994 hrs · 44,710 cycles
DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 44,491 hrs · 44,190 cycles
LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.
Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 44,465 hrs · 44,154 cycles
DURING SCHEDULED C2 CHECK, FOUND RT FWD CARGO LWR DOOR STOP FITTING CRACKED. REMOVED AND REPLACED CARGO DOOR PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 44,456 hrs · 44,143 cycles
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER AFT CORNER OF CUTOUT. REPAIRED SKIN PER SWA EA & SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 44,285 hrs · 43,996 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACK AT BS 750, STR 23L. REPAIRED FUSELAGE SKIN PER SRM.
Part: VALVE — FAULTY (MLG) · airframe 44,222 hrs · 43,918 cycles
LANDING GEAR HANDLE WOULD NOT RETRACT. REMOVED AND REPLACED RT MLG SNUBBING VALVE PER MM.
2004
Part: FAN — FAULTY (E/E BAY) · airframe 43,226 hrs · 42,886 cycles
AIR TURNBACK, F/A AND PAX COMPLAINED OF BURNING SMELL. REMOVED AND REPLACED GASPER FAN PER MM.
Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 42,644 hrs · 42,278 cycles
DURING SPV, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS AT ROW 2 DEF, BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.
Part: LENS — BROKEN (ROW 11ABC) · airframe 42,101 hrs · 41,750 cycles
DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT LENS AT ROW 11 ABC, BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.
Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 41,879 hrs · 41,534 cycles
DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED SLIDE CABLE PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 41,879 hrs · 41,534 cycles
DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 944, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM.
2003
Part: CABLE — MISROUTED (ESCAPE SLIDE) · airframe 40,088 hrs · 39,816 cycles
DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.
Part: CABLE — MISROUTED (ESCAPE SLIDE) · airframe 40,088 hrs · 39,816 cycles
DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.
Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 39,717 hrs · 39,481 cycles
AIR TURNBACK, NR 1 ENGINE COMPRESSOR STALLED. REMOVED AND REPLACED NR 1 ENGINE PER MM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 39,471 hrs · 39,247 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 660, BL 0. REPAIRED FLOORBEAM PER SWA EA.
Part: CAP — MISSING (CABIN) · airframe 39,471 hrs · 39,247 cycles
DURING SCHEDULED 1/4D CHECK, FOUND EEPLS END CAP MISSING IN AFT CABIN. INSTALLED END CAP PER MM.
Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 39,471 hrs · 39,247 cycles
DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 663, RBL 43. REPAIRED BEADED WEB PER SRM.
Part: STRIP — CRACKED (CABIN) · airframe 39,471 hrs · 39,247 cycles
DURING SCHEDULED 1/4D CHECK, FOUND EEPLS STRIP CRACKED AT ROW NR 2. REMOVED AND REPLACED EEPLS STRIP PER MM.
Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 39,394 hrs · 39,183 cycles
(AIR TURNBACK, AIRCRAFT WOULD NOT PRESSURIZE. FOUND WEB CRACKED IN NLG W/W AT BS 259, WL 174. REPAIRED NLG W/W WEB PER SWA EA.
Part: TRUNNION PIN — CORRODED (RT MLG) · airframe 38,245 hrs · 38,087 cycles
DURING SCHEDULED RON, SWA SI 11251-32, FOUND RT MLG TRUNNION PIN CORRODED. REMOVED AND REPLACED RT MLG TRUNNION PIN PER MM.
2002
Part: WINDOW — CRACKED (COCKPIT) · airframe 37,668 hrs · 37,554 cycles
DURING CRUISE FO'S R1 COCKPIT WINDOW ARCED AND CRACKED. REMOVED AND REPLACED R1 WINDOW PER MM.
Part: CABLE — MISROUTED (AFT SVC DOOR) · airframe 37,293 hrs · 37,202 cycles
DURING SCHEDULED C2 CHECK, FOUND AFT SVD DOOR EMERGENCY EVAC SLIDE GIRT ASSY CABLE MISROUTED. REROUTED CABLE PER MM.
Part: LIGHT — LOOSE (CABIN) · airframe 36,356 hrs · 36,317 cycles
DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BIN EMERGENCY EXIT BULL NOSE LIGHT LOOSE AT ROW NR 16 DEF. SECURED LIGHT PER MM.
Part: SKIN — CRACKED (HORIZ STAB) · airframe 35,496 hrs · 35,497 cycles
DURING SCHEDULED C4 CHECK, FOUND HORIZ STAB SKIN CRACKED AT STA 108 OF THE STAB REAR SPAR. REPAIRED SKIN PER SRM.
Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 34,666 hrs · 34,693 cycles
DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.
2001
Part: ACTUATOR — FAILED (SPOILER) · airframe 34,098 hrs · 34,162 cycles
NR 7 SPOILER WOULD NOT DEPLOY. FOUND NR 7 SPOILER CABLE LOOSE OUTSIDE THE SPOILER HOUSING AND NR 7 SPOILER ACTUATOR INOP. REMOVED AND REPLACED SPOILER CONTROL CABLES AND SPOILER ACTUATOR PER MM.
Part: SLIDE — DIRTY (FWD SVC DOOR) · airframe 33,815 hrs · 33,895 cycles
DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND WINDOW DIFFICULT TO SEE THROUGH. CLEANED WINDOW PER MM.
Part: FASTENER — LOOSE (ENTRY DOOR) · airframe 33,815 hrs · 33,895 cycles
DURING SCHEDULED C2 CHECK, FOUND LOOSE FASTENER AT FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINING HOOK. SECURED GIRT BAR HOOK PER MM.
Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 33,815 hrs · 33,895 cycles
DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.
Part: FASTENER — LOOSE (SERVICE DOOR) · airframe 33,815 hrs · 33,895 cycles
DURING SCHEDULED C2 CHECK, FOUND LOOSE FASTENER AT FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINING HOOK. SECURED GIRT BAR HOOK PER MM.
Part: PLATE — BROKEN (ENTRY DOOR) · airframe 32,501 hrs · 32,599 cycles
DURING SCHEDULED RON CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT BASE PLATE BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BASE PLATE ASSY PER MM.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 32,294 hrs · 32,391 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER 18R CRACKED AT BS 1076, REPAIRED STR PER SRM.
Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 31,997 hrs · 32,090 cycles
DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM.
Part: SLIDE — OUT OF TOLERANCE (ENTRY DOOR) · airframe 31,956 hrs · 32,043 cycles
DURING SCHEDULED RON CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM.
Part: SPLICE — CRACKED (CABIN) · airframe 31,579 hrs · 31,668 cycles
DURING SCHEDULED D-CHECK AT DALFORT, FOUND STR 4R SPLICE CRACKED AT BS 907. REMOVED AND REPLACED STR SPLICE PER SRM.
Part: FITTING — CRACKED (LT WING) · airframe 31,579 hrs · 31,668 cycles
DURING SCHEDULED D-CHECK AT DALFORT, FOUND LT MLG SUPPORT BEAM FITTING CRACKED. REMOVED AND REPLACED BEAM FITTING PER ACO.
Part: SPLICE — CRACKED (CABIN) · airframe 31,579 hrs · 31,668 cycles
DURING SCHEDULED D-CHECK AT DALFORT, FOUND STR SPLICE CRACKED AT BS 907 & BS 908, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM.
Part: SHEAR TIE — CRACKED (CABIN) · airframe 31,579 hrs · 31,668 cycles
DURING SCHEDULED D-CHECK AT DALFORT, FOUND SHEAR TIE CRACKED AT BS 967, BETWEEN STR 6L & STR 7L. REPAIRED SHEAR TIE PER SRM.
2000
Part: WIRE — EXPOSED (CABIN) · airframe 31,349 hrs · 31,424 cycles
EEPLS LOOSE & WIRING EXPOSED AT ROW 7. INSTALLED TRACK COVER LENS PER MM.
Part: BRACKET — BROKEN (FWD ENTRY) · airframe 30,864 hrs · 30,937 cycles
FWD ENTRY DOOR EMERGENCY EVAC SLIDE BRACKET BROKEN. REMOVED AND REPLACED BRACKET ASSY PER MM.
Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 30,711 hrs · 30,782 cycles
AIR TURNBACK, CLIMBING THRU 13,000 FT, CABIN ALT WARN SOUNDED. UNABLE TO STOP CABIN ALT FROM CLIMBING BEFORE O2 MASKS DROPPED. PERFORMED PRESSURIZATION CHECK AND PACK CONFIDENCE CHECK PER SAM 728 AND MM. AT HOU, REMOVED AND REPLACED CABIN ALT IND PER MM.
Part: BATTERY — INOPERATIVE (CABIN) · airframe 30,318 hrs · 30,383 cycles
DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT MID CABIN. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,299 hrs · 30,364 cycles
DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP AT MID CABIN AND END CAP MISSING AT FWD END. REMOVED AND REPLACED LIGHT ASSY''S AT MID CABIN, AND INSTALLED FWD END CAP PER MM.
Part: ENGINE — OUT OF ADJ (NR 1) · airframe 30,299 hrs · 30,364 cycles
ABORTED TAKEOFF, NR 1 ENG SLOW TO SPOOL, 15 TO 20 SECS BEHIND NR 2 ENG. ADJUSTED VSV''S, VBV''S AND SPECIFIC GRAVITY PER MM.
Part: SENSOR — INOPERATIVE (SERVICE DOOR) · airframe 29,312 hrs · 29,345 cycles
AIR TURNBACK, FWD SERVICE DOOR FAILED TO SEAL AROUND UPPER SECTION. DOOR WARNING LIGHT WOULD NOT TURN ON WITH DOOR OPENED. OPERATED AND INSPECTED DOOR. NO DEFECT NOTED, OPS CK GOOD. DEFERRED DOOR WARNING LIGHT, LATER AT SLC REMOVED AND REPLACED DOOR PROX SENSOR SPRING PER MM.
Part: SENSOR — INOPERATIVE (ELEVATOR SHIFT)
WHEN AUTOPILOT ENGAGED, ACFT WOULD NOT HOLD ALTITUDE (RAPID NOSE DOWN TRIM). REMOVED AND REPLACED ELEVATOR NEUTRAL SHIFT SENSOR PER MM.
1999
Part: LENS — MISSING (ROW 7)
DURING SCHEDULED C1 CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT LENS MISSING AT ROW 7. INSTALLED LENS PER MM.
Part: SLIDE — FAILED (PAX DOOR)
DURING SCHEDULED RON, FOUND AFT ENTRY DOOR EVACUATION SLIDE SHOWS LOW PSI. REMOVED AND REPLACEDR SLIDE ASSY PER MM.
1998
Part: LINE — CHAFED (EMERG BRAKE)
DURING SERVICE CHECK, FOUND FWD EMERGENCY BRAKE HYD LINE CHAFED. REMOVED AND REPLACED FWD EMERGENCY BRAKE HYD LINE PER BOEING MM.
Part: LIGHT — FAILED (CABIN)
DURING ROUTINE SLIDE DISASSEMBLY AND CHECK, FOUND ONE EMERGENCY SLIDE LIGHT INOP ON LIGHT STRIP. REMOVED AND REPLACED LIGHT PER BOEING M/M.
1997
Part: SKIN — CRACKED (SERVICE DOORWAY)
DURING SCHEDULED B-CHECK, FOUND AFT SERVICE DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED PER BOEING SRM.
1996
Part: LIGHTS — INOPERATIVE (CABIN)
DURING WALKAROUND, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT ROW 7. RELAMPED AND OP CHECKED PER BOEING M/M.
Part: UPLOCK ACTUATOR — FAILED (LT GEAR)
AFTER TAKEOFF, LEFT MAIN GEAR UPLOCK FAILURE, RED UNSAFE LIGHT REMAINS ILLUMINATED AND GEAR FREE FALLS TO DOWN AND LOCKED POSITION WITH GEAR HANDLE IN OFF. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. REPLACED LEFT GEAR UPLOCK ACTUATOR, MODULE CHECK VALVE AND PERFORMED GEAR RETRACTION TEST PER BOEING M/M.
Part: STRINGER — CRACKED (BS 727)
DURING SCHEDULED 1/2 D-CHECK, FOUND LT AFT STRINGER 18A CRACKED TO 1ST FASTENER AT BS 727. REPAIRED PER ACO 6580-53.
Part: ANGLE — CRACKED (BS 540)
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM SUPPORT ANGLE CRACKED AT BS 540, O/B OF SWING LINK AT BL 0 LEFT SIDE. REPLACED PER BOEING SRM.
Part: ANGLE — CRACKED (BS 291.5)
DURING SCHEDULED 1/2 D-CHECK, FOUND ANGLE CRACKED BETWEEN S10 AND 9R AT BS 291.5. REPLACED ANGLE PER BOEING SRM.
Part: ANGLE — CRACKED (BS 294.5)
DURING SCHEDULED 1/2 D-CHECK, FOUND RT SKATE ANGLE CRACKED AT BS 294.5 RBL 55. REPAIRED PER TI-A53-0233.
Part: ANGLE — CRACKED (BS 380-400)
DURING SCHEDULED 1/2 D-CHECK, FOUND UPPER ANGLE WEBS CRACKED EXTENDING FROM CLIP NUT, BS 380 TO 400, BL 0 AND AT BS 482 TO 520. REPLACED ANGLES PER BOEING SRM.
Part: BLKHD STRAP — CRACKED (BS 727)
DURING SCHEDULED 1/2 D-CHECK, FOUND RT HORIZ STRAP CRACKED AT FWD END AT BS 727 BULKHEAD, AT S22R. REPLACED PER BOEING SRM.
Part: CLIP — CRACKED (BS 663)
DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER TO LT FRAME TIE CLIP CRACKED AT I/B END, BS 663. REPLACED PER BOEING SRM.
Part: BULKHEAD — CRACKED (BS 948)
DURING SCHEDULED 1/2 D-CHECK, FOUND SEVERAL CRACKS AT BLOW OUT PANEL CUTOUT IN CENTER OF BULKHEAD AT BS 948. REPAIRED PER BOEING SRM.
Part: ANGLE — CORRODED (BS 947/986.5)
DURING SCHEDULED 1/2 D-CHECK, FOUND AFT SERVICE DOOR THRESHOLD Z-ANGLE CORRODED AT BS 947 AND 986.5. REPLACED PER BOEING SRM.
Part: BLKHD CHANNEL — CRACKED (BS 727)
DURING SCHEDULED 1/2 D-CHECK, FOUND U-CHANNEL CRACKED AT BS 727 BULKHEAD AT RBL 3. REPLACED PER BOEING SRM.
Part: ANGLE SUPPORT — CORRODED (BS 303.9)
DURING SCHEDULED 1/2 D-CHECK, FOUND Z-ANGLE SUPPORT STRIP AT BS 303.9 CORRODED. REPLACED PER BOEING SRM.
Part: BEAM — CRACKED (RT WW)
DURING SCHEDULED 1/2 D-CHECK, FOUND CRACK IN AFT EDGE OF RT W/W STRINGER 18A SHEAR BEAM O/B HOLE. REPAIRED PER SWA ACO 6580-53.