N330SW
Registered owner: SKYWAYS AIR TRANSPORTATION INC, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
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.
208 reports on file, 1996-01-30 – 2011-08-01.
Part: SIGN — BROKEN (CABIN) · airframe 75,857 hrs · 67,565 cycles
FWD EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,026 hrs · 67,846 cycles
DURING SCHEDULED MV2 CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED IAW MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 75,488 hrs · 67,296 cycles
DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 11L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 75,488 hrs · 67,296 cycles
DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 277, FWD WHEEL WELL UPPER AFT WEB. REPAIRED WEB PER SRM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,320 hrs · 67,160 cycles
DURING SCHEDULED SPV CHECK FOUND, AFT ENTRY EMERGENCY EXIT LIGHT BULBS INOP. RELAMPED PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,320 hrs · 67,160 cycles
DURING SCHEDULED SPV CHECK FOUND, RT OVERWING EMERGENCY EXIT LIGHT BULBS INOP. RELAMPED PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,320 hrs · 67,160 cycles
DURING SCHEDULED SPV CHECK FOUND, LT OVERWING EMERGENCY EXIT LIGHT BULBS INOP. RELAMPED PER MM.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,319 hrs · 67,158 cycles
DURING SCHEDULED SPV CHECK FOUND, STRINGER CORRODED AT BS 351, STR 28R. REMOVED AND REPLACED STRINGER PER SRM.
Part: SKIN — PUNCTURED (FOREFLAP) · airframe 75,319 hrs · 67,158 cycles
DURING SCHEDULED SPV CHECK FOUND, RT WING I/B FORE FLAP LOWER SURFACE PUNCTURED. REMOVED AND REPLACED FORE FLAP PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 75,319 hrs · 67,158 cycles
DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 264.5, STR 15R. REPAIRED SKIN PER SRM.
Part: SPAR — CORRODED (HORIZ STAB) · airframe 75,319 hrs · 67,158 cycles
DURING SCHEDULED SPV CHECK, FOUND LT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD CORRODED BETWEEN STA 182 TO BS 189. REMOVED AND REPLACED STABILIZER PER SRM.
Part: TRIM TAB — DELAMINATED (AILERON) · airframe 75,113 hrs · 67,004 cycles
DURING SCHEDULED MV2 CHECK, FOUND LT WING AILERON TRIM TAB DELAMINATED. REMOVED AND REPLACED TAB PER MM.
Part: LENS — MISSING (CABIN) · airframe 74,594 hrs · 66,618 cycles
DURING SCHEDULED CV CHECK, FOUND RT EEPLS LENS MISSING. INSTALLED LENS PER MM.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 74,554 hrs · 66,590 cycles
FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,294 hrs · 66,399 cycles
DURING SCHEDULED MV2 CHECK, FOUND RT EEPLS INOP AT ROW 2. RELAMPED PER MM.
Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 74,236 hrs · 66,355 cycles
R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.
Part: SKIN — CRACKED (FUSELAGE) · airframe 74,100 hrs · 66,256 cycles
DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 759, STR 18R. REPAIRED SKIN PER EA.
Part: LIGHT — LOOSE (CABIN) · airframe 74,100 hrs · 66,256 cycles
DURING SCHEDULED SPV CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT ASSY LOOSE AT ROW 8. SECURED LIGHT ASSY PER MM.
Part: LIGHT — LOOSE (CABIN) · airframe 74,100 hrs · 66,256 cycles
DURING SCHEDULED SPV CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT ASSY LOOSE AT ROW 14. SECURED LIGHT ASSY PER MM.
Earlier reports · 1996–2010 · 189 reports
2010
Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 74,080 hrs · 66,240 cycles
R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 73,979 hrs · 66,165 cycles
AFT CABIN EMERGENCY FLASHLIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 73,654 hrs · 65,908 cycles
DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 812, STR 20L. REPAIRED SKIN PER ER.
Part: SKIN — CRACKED (FUSELAGE) · airframe 73,654 hrs · 65,908 cycles
DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 844, STR 20L. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 73,654 hrs · 65,908 cycles
DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 513B, STR 20R. REPAIRED SKIN PER EA.
Part: LIGHT — DAMAGED (CABIN) · airframe 73,487 hrs · 65,780 cycles
L1 DOOR EMERGENCY EXIT LIGHT DAMAGED. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: SLIDE — LOOSE (R2 DOOR)
R2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MT.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,827 hrs · 65,249 cycles
DURING SCHEDULED OTS CHECK, FOUND LT EMERGENCY EXIT LIGHT INOP BETWEEN ROW 6 TO ROW 10. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 72,827 hrs · 65,249 cycles
DURING SCHEDULED OTS CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 22R. REMOVED AND REPLACED SPLICE PER SRM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,827 hrs · 65,249 cycles
DURING SCHEDULED OTS CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP AT ROW 8. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 72,827 hrs · 65,249 cycles
DURING SCHEDULED OTS CHECK, FOUND STRINGER CORRODED AT BS 914, STR 22R. REMOVED AND REPLACED STRINGER PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 72,827 hrs · 65,249 cycles
DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 932, STR 21L. REPAIRED SKIN PER SRM.
Part: SLIDE — FAILED (R1 DOOR) · airframe 72,803 hrs · 65,231 cycles
DURING SCHEDULED CV CHECK, R1 DOOR EMERGENCY EVAC SLIDE FAILED DEPLOYMENT TEST. REMOVED AND REPLACED SLIDE ASSY PER MT.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,594 hrs · 65,077 cycles
AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK ASSY PER MM.
Part: LIGHT — BROKEN (CABIN) · airframe 71,905 hrs · 64,561 cycles
L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.
Part: LENS — LOOSE (CABIN) · airframe 71,804 hrs · 64,483 cycles
RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.
Part: LENS — MISSING (CABIN) · airframe 71,446 hrs · 64,211 cycles
DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS LENS MISSING AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.
2009
Part: LIGHT — LOOSE (CABIN) · airframe 71,258 hrs · 64,077 cycles
DURING SCHEDULED CV CHECK, FOUND LT EMERGENCY EXIT BULLNOSE LIGHT LOOSE AT ROW 6. SECURED LIGHT PER MM.
Part: LENS — MISSING (CABIN) · airframe 70,455 hrs · 63,481 cycles
DURING SCHEDULED 2HC2 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 2. INSTALLED LENS PER MM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 70,364 hrs · 63,413 cycles
DURING SCHEDULED 22Y CHECK, FOUND RT FRAME CRACKED AT BS 290, WL 259. REMOVED AND REPLACED FRAME PER SRM.
Part: LIGHT — BROKEN (CABIN) · airframe 70,364 hrs · 63,413 cycles
DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 70,364 hrs · 63,413 cycles
DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 70,364 hrs · 63,413 cycles
DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 360, BETWEEN WL 208 TO WL 216. REPAIRED SKIN PER EA.
Part: CHARGER — DISCHARGED (CABIN) · airframe 70,364 hrs · 63,413 cycles
DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,364 hrs · 63,413 cycles
DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 747, STR 19L. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,364 hrs · 63,413 cycles
DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CHORD CRACKED AT BS 663, RBL 24.8. REPAIRED BEAM PER SWA EA.
Part: SKIN — CRACKED (LE SLAT) · airframe 70,364 hrs · 63,413 cycles
DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT I/B SIDE OF ACTUATOR. REPAIRED SLAT SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 70,364 hrs · 63,413 cycles
DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED BETWEEN BS 751 TO BS 754, STR 18L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 70,364 hrs · 63,413 cycles
DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 263, WL 221 LT SIDE. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 70,364 hrs · 63,413 cycles
DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 263, WL 223 LT SIDE. REPAIRED SKIN PER SWA EA.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,364 hrs · 63,413 cycles
DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 277, BETWEEN STR 15L TO STR 16L. REMOVED AND REPLACED SHEAR TIE PER BAC DWG.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,364 hrs · 63,413 cycles
DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 380, AT STR 14L. REMOVED AND REPLACED SHEAR TIE PER BAC DWG.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,364 hrs · 63,413 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 13L. REMOVED AND REPLACED CLIP PER SRM.
Part: LENS — CRACKED (CABIN) · airframe 70,364 hrs · 63,413 cycles
DURING SCHEDULED 22Y CHECK, FOUND AFT EMERGENCY EXIT LIGHT LENS CRACKED. REPAIRED LENS PER MM.
Part: LIGHT — BROKEN (CABIN) · airframe 70,364 hrs · 63,413 cycles
DURING SCHEDULED 22Y CHECK, FOUND AFT F/A'S STATION EMERGENCY EXIT LIGHT BROKEN. REPAIRED LIGHT ASSY PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 70,364 hrs · 63,413 cycles
DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 751 TO BS 754, STR 18L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 70,364 hrs · 63,413 cycles
DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 26L. REPAIRED SKIN PER SRM.
Part: FLAP — DELAMINATED (RT WING) · airframe 70,122 hrs · 63,228 cycles
DURING SCHEDULED CV CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 66,511 hrs · 59,071 cycles
DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 504B, STR 19L. REPAIRED SKIN PER SRM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,798 hrs · 63,009 cycles
DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 6. RELAMPED EMERGENCY LIGHT PER MM.
Part: SLAT — PEELING (LT WING) · airframe 69,061 hrs · 62,496 cycles
DURING SCHEDULED MV1 CHECK, FOUND LT WING NR 2 SLAT PEELING AT O/B CORNER. REPAIRED SLAT PER SRM.
Part: SKIN — CRACKED (LE SLAT) · airframe 68,825 hrs · 62,326 cycles
DURING SCHEDULED SPV CHECK, FOUND LT WING NR 1 SLAT SKIN CRACKED. REPAIRED SKIN PER MM.
Part: SLAT — PUNCTURED (RT WING) · airframe 68,825 hrs · 62,326 cycles
DURING SCHEDULED SPV CHECK, FOUND RT WING NR 5 SLAT PUNCTURED. REMOVED AND REPLACED SLAT PER MM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 68,825 hrs · 62,326 cycles
DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB PER ER.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 68,825 hrs · 62,326 cycles
DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17. REMOVED AND REPLACED WEB PER SRM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 68,825 hrs · 62,326 cycles
DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17. REMOVED AND REPLACED WEB PER SRM.
2008
Part: SKIN — CRACKED (FUSELAGE) · airframe 68,576 hrs · 62,154 cycles
DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16L. REPAIRED SKIN PER SWA EA.
Part: STRUCTURE — CRACKED (BS 178) · airframe 67,706 hrs · 61,523 cycles
DURING SCHEDULED SPV CHECK, FOUND VERTICAL CHORD CRACKED AT BS 178, LBL 5.5. REPAIRED CHORD PER SRM.
Part: SHEAR TIE — CRACKED (BS 500D S16R) · airframe 67,609 hrs · 61,443 cycles
DURING SCHEDULED HC2 CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, STR 16R. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 67,609 hrs · 61,443 cycles
DURING SCHEDULED HC2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 67,609 hrs · 61,443 cycles
DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SERVICE DOOR LOWER HINGE. REPAIRED SKIN PER SRM.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 66,797 hrs · 60,810 cycles
DURING SCHEDULED MV2 CHECK, FOUND RT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,924 hrs · 60,171 cycles
DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,924 hrs · 60,171 cycles
DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 65,857 hrs · 60,123 cycles
R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 65,745 hrs · 60,049 cycles
DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930 AND BS 920, STR 23R. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 65,745 hrs · 60,049 cycles
DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 791, STR 18L. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 65,745 hrs · 60,049 cycles
DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 21R. REPAIRED SKIN PER SRM.
2007
Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND NLG W/W PRESSURE WEB CRACKED AT RIGHT BS 245. REPAIRED WEB PER ACO.
Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND NLG W/W PRESSURE WEB CRACKED AT LEFT BS 245. REPAIRED WEB PER ACO.
Part: STRINGER CLIP — CRACKED (BS 747 S8R) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 867 S8L) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CORRODED (BS 540 S27R) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CORRODED AT BS 540, STR 27R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: FRAME — CRACKED (BS 303 S16L) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, STR 16L. REPAIRED FRAME PER SRM.
Part: SHEAR TIE — CORRODED (BS 500) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BL 0. REPAIRED SHEAR TIE PER SRM.
Part: FRAME — CRACKED (BS 727D S8R) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (BS 500D S14R) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 14R. REPAIRED FRAME PER SWA EA.
Part: STRINGER CLIP — CRACKED (BS 294 S13L) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND STR CLIP CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED STR CLIP PER SRM.
Part: FRAME — CRACKED (BS 706 S8L) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8L. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (BS 520 S8L) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.
Part: STRINGER SPLICE — CRACKED (BS 360 S15L) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.
Part: FRAME — CRACKED (BS 500A S8R) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (BS 342 S6L) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 342, STR 6L. REPAIRED FRAME PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.
Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 500C, STR 20R. REPAIRED BELTFRAME PER SWA EA.
Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 500B, STR 20R. REPAIRED BELTFRAME PER SWA EA.
Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND KEEL BEAM CORRODED AT BS 540, RBL 6.50. REPAIRED KEEL BEAM PER SRM.
Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 500B, STR 20L. REPAIRED BELTFRAME PER SWA EA.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 662, LBL 0.07. REPAIRED FLOORBEAM PER SWA EA.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 827, STR 27L. REPAIRED SHEAR TIE PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16R. REPAIRED FRAME PER SRM.
Part: SKIN — CORRODED (FUSELAGE) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 808, BL 0. REPAIRED SKIN PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20L. REPAIRED FRAME PER SWA EA.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,972 hrs · 58,678 cycles
DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,954 hrs · 58,660 cycles
DURING SCHEDULED A1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,929 hrs · 58,642 cycles
DURING SCHEDULED 14Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,929 hrs · 58,642 cycles
DURING SCHEDULED 14Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,929 hrs · 58,642 cycles
DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
Part: FLAP — DELAMINATED (LT WING) · airframe 63,378 hrs · 58,203 cycles
DURING SCHEDULED C3 CHECK, FOUND LEFT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD T/E. REMOVED AND REPLACED AFT FLAP PER MM.
Part: LIGHT — BROKEN (CABIN) · airframe 63,314 hrs · 58,153 cycles
DURING SCHEDULED SERVICE CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT BROKEN AT ROW 11 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: SKIN — CRACKED (BS 765 S20L) · airframe 63,308 hrs · 58,147 cycles
FUSELAGE SKIN CRACKED AT BS 765, STR 20L. REPAIRED SKIN PER SWA EA.
Part: SLIDE — DISLODGED (R2 DOOR) · airframe 63,109 hrs · 58,003 cycles
R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.
Part: FRAME — CRACKED (R1 DOOR) · airframe 62,433 hrs · 57,498 cycles
DURING SCHEDULED C2 CHECK, FOUND R1 DOOR LOWER FRAME CRACKED BELOW LOWER CAM. REMOVED AND REPLACED R1 DOOR PER MM.
Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 62,433 hrs · 57,498 cycles
DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
Part: GLOWSTRIP — WORN (CABIN) · airframe 62,433 hrs · 57,498 cycles
DURING SCHEDULED C2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 1 DEF. REMOVED AND REPLACED STRIP PER MM.
Part: SKIN — CRACKED (BS 514D S15L) · airframe 62,433 hrs · 57,498 cycles
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514D, STR 15L. REPAIRED SKIN SECTION PER SWA EA.
Part: FRAME — CRACKED (CARGO DOOR) · airframe 62,433 hrs · 57,498 cycles
DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR AFT FRAME CRACKED AT NR 5 STOP FITTING. REMOVED AND REPLACED AFT CARGO DOOR PER SWA EA.
2006
Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,343 hrs · 57,429 cycles
DURING SCHEDULED A1 CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
Part: BEARING — WORN (ELEVATOR TAB) · airframe 61,450 hrs · 56,743 cycles
DURING SCHEDULED C1 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR NR 1 TAB HINGE BEARING PER MM.
Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 61,450 hrs · 56,743 cycles
DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 61,450 hrs · 56,743 cycles
DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,046 hrs · 56,420 cycles
DURING SCHEDULED SERVICE CHECK, FOUND LOWER EMERGENCY EXIT LIGHT INOP AT R1 DOOR. REMOVED AND REPLACED LIGHT BULB PER MM.
Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 60,890 hrs · 56,281 cycles
DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMEREGENCY EXIT LIGHT INOP. SPLICED BROKEN WIRE PER MM.
Part: SKIN — CORRODED (HORIZ STAB) · airframe 60,504 hrs · 55,990 cycles
DURING SCHEDULED PM CHECK, FOUND RIGHT HORIZONTAL STAB UPPER SKIN CORRODED. REMOVED AND REPLACED RIGHT HORIZONTAL STAB PER MM.
Part: ATTACH FITTING — BROKEN (NR 4 SPOILER) · airframe 60,449 hrs · 55,985 cycles
DURING SCHEDULED C4 CHECK, FOUND LT WING NR 4 GROUND SPOILER OUTBOARD ATTACH LUG BROKEN. REMOVED AND REPLACED NR 4 SPOILER PER MM.
Part: FRAME — CRACKED (BS 492) · airframe 60,135 hrs · 55,715 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT FWD CARGO DOOR CUTOUT BS 492, NR 5 STOP PAD. REMOVED AND REPLACED FRAME SECTION PER ER AND SB.
Part: FRAME — CRACKED (BS 847) · airframe 60,135 hrs · 55,715 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME WEB CRACKED AT AFT CARGO DOOR CUTOUT BS 847, NR 1 LOWER DOOR STOP. REMOVED AND REPLACED WEB PER ER.
Part: SKIN — CRACKED (FUSELAGE) · airframe 60,049 hrs · 55,645 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 743E TO BS 744E, STR 19L TO STR 20L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 60,049 hrs · 55,645 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 741D TO BS 750, STR 18R TO STR 19R. REPAIRED SKIN PER SWA EA & SRM.
Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 55,732 hrs · 52,265 cycles
R1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM.
2005
Part: LIGHT — LOOSE (CABIN) · airframe 58,573 hrs · 54,520 cycles
DURING SCHEDULED C2 CHECK, FOUND EEPLS STRIP LOOSE BETWEEN ROW 8 TO ROW 10. REMOVED AND REPLACED STRIP PER MM.
Part: CIRCUIT CARD — FAULTY (MLG) · airframe 58,375 hrs · 54,363 cycles
RED UNSAFE LT MLG LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. RECYCLED GEAR HANDLE AND RED UNSAFE LIGHT EXTINGUISHED. REMOVED AND REPLACED MLG RED LIGHT SWITCH PC CARD M986 PER MM.
Part: LIGHT — LOOSE (ROW 10) · airframe 58,156 hrs · 54,192 cycles
EEPLS STRIP LOOSE AT ROW 10. SECURED STRIP PER MM.
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 58,058 hrs · 54,101 cycles
DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,907 hrs · 53,981 cycles
DURING SCHEDULED RON CHECK, FOUND FWD GALLEY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,675 hrs · 53,804 cycles
DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY INTERIOR & EXTERIOR LIGHTS INOP AT BOTH ENTRY DOORS. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: LIGHT — LOOSE (MID CABIN) · airframe 57,631 hrs · 53,768 cycles
RIGHT OVERWING EMERGENCY EXIT DOOR LIGHT LOOSE. SECURED LIGHT ASSY PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 57,631 hrs · 53,768 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKS BETWEEN BS 727E + 3 AND BS 747, STR 19R. REPAIRED SKIN PER SWA EA AND SRM.
Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 57,129 hrs · 53,350 cycles
DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 56,639 hrs · 52,954 cycles
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 25R. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 56,639 hrs · 52,954 cycles
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500 D, STR 15R. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 56,639 hrs · 52,954 cycles
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 19L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 56,639 hrs · 52,954 cycles
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 18R. REPAIRED SKIN PER SRM.
Part: LENS — LOOSE (R2 DOOR) · airframe 56,639 hrs · 52,954 cycles
DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.
Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 55,732 hrs · 52,265 cycles
DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 747, RBL 6 TO LBL 6, DAMAGED. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 55,732 hrs · 52,265 cycles
DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT LIGHT AT BS 673, LOW CHARGE. REMOVED AND REPLACED BATTERY PER MM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 55,732 hrs · 52,265 cycles
DURING SCHEDULED 1/4D CHECK, FOUND 3 EACH CRACKS AT PANEL NR 7 AND ONE EACH CRACK AT PANEL NR 2, ON BULKHEAD WEB AT BS 1016. REPAIRED BULKHEAD WEB PER EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 55,732 hrs · 52,265 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 500C + 6, ABOVE STRINGER 15R, CRACKED. REPAIRED SKIN PER EA.
2004
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,732 hrs · 52,265 cycles
DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPT FRAME SHEAR TIE CORRODED AT BS 807, LBL 5 TO RBL 5. REPAIRED SHEAR TIE PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,732 hrs · 52,265 cycles
DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPT FRAME SHEAR TIE CORRODED AT BS 747, RBL 7 TO RBL 13. REPAIRED SHEAR TIE PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,732 hrs · 52,265 cycles
DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPT SHEAR TIE CORRODED AT BS 787, RBL 8. REPAIRED SHEAR TIE PER SRM.
Part: SKIN — CRACKED (DOOR) · airframe 55,707 hrs · 52,237 cycles
DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR SKIN AT LOWER FWD RADIUS CRACKED. REPAIRED DOOR SKIN PER SRM.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,473 hrs · 52,051 cycles
DURING SCHEDULED RON, FOUND BOTH L1 & R1 DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: SKIN — DELAMINATED (LT WING AILERON) · airframe 55,190 hrs · 51,824 cycles
DURING SCHEDULED SERVICE CHECK, FOUND LT WING AILERON DELAMINATED. REMOVED AND REPLACED LT AILERON PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,741 hrs · 51,451 cycles
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 967, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,742 hrs · 51,451 cycles
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 540, STRINGER 12L, CRACKED. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,742 hrs · 51,451 cycles
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 350, STRINGER 26L, CRACKED. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,735 hrs · 51,444 cycles
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT L2 DOOR UPPER HINGE CUTOUT, CRACKED. REPAIRED SKIN PER EA.
Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 54,735 hrs · 51,444 cycles
DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.
Part: SLIDE — LOOSE (R2 DOOR) · airframe 54,435 hrs · 51,196 cycles
R2 DOOR EVAC SLIDE LOOSE. SECURED R2 DOOR EVAC SLIDE PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 53,589 hrs · 50,529 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 951, LOWER RT LAP SEAM, CRACKED. REPAIRED SKIN PER SRM.
Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 52,816 hrs · 49,904 cycles
DURING SCHEDULED RON, FOUND LEFT EXIT SIDE WALL PANEL LIGHT INOP AT EMERGENCY EXIT DOOR. RELAMPED PER MM.
2003
Part: FLAP — DELAMINATED (RT WING) · airframe 51,206 hrs · 48,638 cycles
RT OUTBD AFT T/E FLAP PREVIOUS REPAIR CAME APART. REMOVED AND REPLACED RT OUTBD AFT T/E FLAP PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 51,101 hrs · 48,546 cycles
DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) BS 915 AT STR 23L, BS 915 AT STR 24L AND BS 975 AT STR 21L. REPAIRED SKIN PER SRM.
Part: LATCH — INOPERATIVE (ESCAPE COVER) · airframe 50,758 hrs · 48,251 cycles
CAPT'S ESCAPE ROPE COVER LATCH INOP. REMOVED AND REPLACED ROPE COVER LATCH PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 50,120 hrs · 47,722 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 25L. REPAIRED SKIN PER SRM.
Part: TORQUE TUBE — BROKEN (LT WING) · airframe 49,461 hrs · 47,184 cycles
T/E FLAPS INDICATED 5 DEGREE SPLIT ON APPROACH AND WOULD NOT RETRACT AFTER LANDING. FOUND LEFT FLAPS INBD TORQUE TUBE BROKEN, REMOVED AND REPLACED LEFT INBD TORQUE TUBE PER MM.
Part: WEB — CRACKED (NLG W/W) · airframe 49,247 hrs · 47,022 cycles
DURING SCHEDULED BC CHECK, FOUND NLG WHEEL WELL RT SIDE WEB CRACKED AT BS 259, WL 174. REPAIRED WEB PER SWA EA.
Part: SLIDE — OUT OF ADJUST (AFT ENTRY DOOR) · airframe 49,247 hrs · 47,022 cycles
DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.
2002
Part: LENS — BROKEN (CABIN) · airframe 47,919 hrs · 45,977 cycles
DURING SCHEDULED 1/2D CHECK, FOUND BOTH AFT CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHT LENSES BROKEN. REMOVED AND REPLACED LENSES PER MM.
Part: SLAT — DELAMINATED (RT WING) · airframe 47,919 hrs · 45,977 cycles
DURING SCHEDULED 1/2D CHECK, FOUND NR 5 L/E SLAT DELAMINATED AT T/E OTBD END. REPAIRED NR 5 L/E SLAT PER SRM.
Part: STRUCTURE — CRACKED (ENTRY DOOR) · airframe 47,919 hrs · 45,977 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR CRACKED AT LOWER HINGE AREA, BS 316 AND WL 236. REPAIRED DOOR PER BOEING SB.
Part: SPLICE — CRACKED (FUSELAGE) · airframe 47,919 hrs · 45,977 cycles
DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICES CRACKED AT BS 360, STR 4R AND STR 4L. REMOVED AND REPLACED STR SPLICES PER SRM.
Part: SPLICE — CRACKED (FUSELAGE) · airframe 47,919 hrs · 45,977 cycles
DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE'S CRACKED (2 EA) AT BS 908, STR 4R AND STR 4L. REPAIRED SPLICE'S PER SRM.
Part: SLIDE — DEPLOYED (FWD SVC DOOR) · airframe 47,726 hrs · 45,813 cycles
DURING SCHEDULED RON, FWD SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MM.
2001
Part: FRAME — CRACKED (FUSELAGE) · airframe 46,094 hrs · 44,483 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD LT SIDE CHORD CRACKED, WL 207. REMOVED AND REPLACED CHORD PER SWA ACO.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,089 hrs · 44,480 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND BS 178, BOTH LT AND RT LOWER VERTICAL WEBS CRACKED. REMOVED AND REPLACED BOTH WEBS PER SRM.
Part: BATTERY — DISCHARGED (SERVICE DOOR) · airframe 45,959 hrs · 44,373 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.
Part: SPOILER — DELAMINATED (RH WING) · airframe 45,489 hrs · 43,980 cycles
DURING SCHEDULED C4 CHECK, FOUND # 9 SPOILER DELAMINATED AT UPPER SIDE. R&R SPOILER PER MM.
Part: LENS — BROKEN (CABIN) · airframe 44,594 hrs · 43,241 cycles
DURING SCHEDULED C3 CHECK, FOUND SIDE WALL EMERGENCY LIGHT LENS BROKEN AT FWD ENTRY. R&R LENS PER MM.
Part: STIFFENER — CRACKED (MLG WW) · airframe 43,968 hrs · 42,710 cycles
DURING SCHEDULED SERVICE CHECK, FOUND VERTICAL STIFFENER CRACKED AT MLG WHEEL WELL, BS 663, RBL 6.5. REPAIRED PER SWA RA.
2000
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,662 hrs · 41,648 cycles
DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR OVERHEAD EMERGENCY EXIT SIGN INOP. R&R BATTERY PACK PER MM.
Part: LENS — LOOSE (CABIN) · airframe 42,662 hrs · 41,648 cycles
DURING SCHEDULED C1 CHECK, FOUND BULL NOSE EGRESS LIGHT LENS LOOSE AT ROW 22 DEF. SECURED LENS PER MM.
Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 42,662 hrs · 41,648 cycles
DURING SCHEDULED C1 CHECK, FOUND AFT SVC & AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS INDS OUT OF VIEW. ADJUSTED SLIDE ASSY PER MM.
Part: BOTTLE — DISCHARGED (ESCAPE SLIDE) · airframe 42,351 hrs · 41,387 cycles
AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM.
Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 42,230 hrs · 41,278 cycles
DURING SCHEDULED SERVICE CHECK, FOUND LT WING INBOARD TRAILING EDGE AFT FLAP DELAMINATED AT LOWER INBOARD SECTION. REMOVED AND REPLACED FLAP PER MM.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 41,715 hrs · 40,826 cycles
DURING SCHEDULED C4 CHECK, FOUND RT HORIZ STAB LOWER SKIN CRACKED, STA 128 ABOVE REAR SPAR. REPAIRED SKIN PER SRM.
Part: LIGHT — LOOSE (CABIN) · airframe 40,819 hrs · 40,059 cycles
DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK LOOSE AT FWD END. RESECURED TRACK ASSY PER MM.
Part: SENSOR — INOPERATIVE (RT MLG) · airframe 40,784 hrs · 40,026 cycles
AIR TURNBACK, RT MLG WOULD NOT FULLY RETRACT. VISUAL INSPECTION CONFIRMED PARTIAL RETRACTED ONLY. REMOVED AND REPLACED RT MLG UPLOCK SENSOR PER MM.
Part: SLIDE — DISCHARGED (PAX DOOR) · airframe 40,749 hrs · 39,996 cycles
DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.
Part: STRAP — CRACKED (BS 1138)
DURING SCHEDULED 1/4D CHECK, FOUND BS 1138, FUSELAGE SKIN STRAP CRACKED, STRINGER 12L. REMOVED AND REPLACED STRAP PER SRM.
Part: BULKHEAD — CRACKED (BS 178)
DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, WL 234, RBL12. REPAIRED BULKHEAD PER SRM.
1999
Part: GIRT BAR — OUT OF POSITION (PAX DOORWAY)
AFT ENTRY DOOR EVACUATION SLIDE GIRT BAR OUT OF HANGERS. REPOSITIONED GIRT BAR PER MM.
Part: SLIDE — DETACHED (SERVICE DOOR)
AFT SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.
Part: SLIDE — DEPLOYED (SERVICE DOOR)
DURING SCHEDULED SC CHECK, FWD SERVICE DOOR EMERGENCY ESCAPE SLIDE WAS INADVERTANTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER BOEING M/M.
1998
Part: ROD — BROKEN (LANDING GEAR)
RETURNED TO PHX DUE TO AFTER TAKEOFF LANDING GEAR WOULD NOT RAISE. ALL COCKPIT INDICATIONS POINTED TO A AIR/GROUND SENSOR PROBLEM. FOUND GROUND SPOILER INTERLOCK CABLE LOWER ROD END BROKEN. REPLACED AND RIGGED CABLE AS REQUIRED PER M/M. CYCLED GEAR, OPS NORMAL.
Part: SKIN — CRACKED (WING LE)
DURING SCHEDULED C4 CHECK, FOUND LEADING EDGE SKIN CRACKED AT I/B END OF HINGE CUTOUT OF SPRING LOADED DOOR. REPAIRED PER ACO NR 6820-57.
Part: SLIDE — DEPLOYED (PAX DOOR)
DURING WALKAROUND CHECK, FOUND FORWARD ENTRY DOOR SLIDE DEPLOYED. REMOVED AND REPLACED FWD ENTRY DOOR SLIDE ASSY PER BOEING MM.
Part: INTERCOSTAL — CRACKED (BS 178)
DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED INSIDE INTERCOSTAL AT BS 178 LBL 26, WL 195 FWD END. REMOVED AND REPLACED PER BOEING SRM.
1997
Part: SKIN — GOUGED (BS 947.6)
DURING SCHEDULED BC4 CHECK, FOUND A DEEP GOUGE IN FUSELAGE SKIN BELOW L2 DOOR, AT BS 947.6. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (FUSELAGE)
DURING SCHEDULED BC4 CHECK, FOUND FUSELAGE SKIN CRACKED 2.5 INCH LONG AFT OF WING TO BODY FAIRING, BELOW EMERGENCY EXIT LIGHT, BETWEEN S24 AND 25. REPAIRED PER BOEING SRM.
Part: BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED TERMINALCHECK, FOUND FWD CABIN FLOOR TRACK LIGHTING INOP. REPLACED BATTERY PACK AND CHARGER PER BOEING M/M.
1996
Part: SKIN — CRACKED (DOOR CUTOUT)
DURING SCHEDULED C1 CHECK, FOUND FWD GALLEY DOOR UPPER HINGE CUTOUT CRACKED AT LOWER AFT CORNER. REPAIRED PER SWA RA 1-352-0257.
Part: SKIN — CRACKED (BS 755)
DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 755, S23L. REPAIRED PER BOEING SRM.
Part: BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED TERMINAL CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK AND CHARGER PER BOEING M/M.
Part: BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED TERMINAL CHECK, FOUND MIS CABIN EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SCHEDULED TERMINAL CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK AND HOUSING PER BOEING M/M.