N103SW
Registered owner: TVPX AIRCRAFT SOLUTIONS INC TRUSTEE, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Sunset Aviation LLC (7SSA) | Certificate holder | — | Matched by certificate designator |
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.
134 reports on file, 1995-01-24 – 2004-11-15.
Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 64,855 hrs · 70,606 cycles
RIGHT WING NR 5 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 5 L/E SLAT PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 64,468 hrs · 70,104 cycles
DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN AT BS 847, STRINGER 24L, CRACKED. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 64,460 hrs · 70,092 cycles
DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 18L, CRACKED. REPAIRED SKIN PER EA.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,822 hrs · 69,247 cycles
DURING SCHEDULED PM CHECK, FOUND AFT CABIN OVERHEAD CENTER AISLE EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK PER MM.
Part: CASTING — CRACKED (LT SPOILER) · airframe 63,633 hrs · 69,010 cycles
DURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD NR 5 GROUND SPOILER ACTUATOR CASTING, CRACKED. REMOVED AND REPLACED NR 5 ACTUATOR CASTING PER MM AND SRM.
Part: CABLE — OUT OF ADJUST (NR 2 ENGINE) · airframe 62,786 hrs · 67,926 cycles
ABORTED TAKEOFF, NR 2 THRUST LEVER MOVEMENT RESTRICTED. ADJUSTED NR 2 ENGINE THRUST REVERSER FOLLOW-UP CABLE PER MM.
Part: SWITCH — FAULTY (NR 1 ENGINE) · airframe 62,721 hrs · 67,845 cycles
INFLIGHT SHUTDOWN, AIRTURN BACK, DECLARED EMERGENCY, NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. LIGHT WOULD NOT EXTINGUISH. REMOVED AND REPLACED OIL FILTER, NO DEFECTS NOTED. DEFERRED OIL BYPASS SYSTEM PER MEL. ON 02/06/04 AT DAL, REMOVED AND REPLACED NR 1 ENGINE OIL FILTER BYPASS SWITCH PER MM.
Earlier reports · 1995–2003 · 127 reports
2003
Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,022 hrs · 66,956 cycles
DURING SCHEDULED PM CHECK, FOUND EEPLS INOP AT ROW 3 AND ROW 8. RELAMPED EEPLS PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 61,591 hrs · 66,389 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 575, STR 10R. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 61,591 hrs · 66,389 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B + 16, STR 17R. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 61,132 hrs · 65,792 cycles
DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 945, STR 21R. REPAIRED SKIN PER SRM.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 61,123 hrs · 65,782 cycles
DURING SCHEDULED PM CHECK, FOUND STRINGER CRACKED AT BS 945, STR 21R. REPAIRED STRINGER PER SRM.
Part: CABLE — MISROUTED (ESCAPE SLIDE) · airframe 61,015 hrs · 65,639 cycles
DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 60,943 hrs · 65,546 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 17L. REPAIRED SKIN PER SRM.
Part: SLIDE — DEPLOYED (AFT ENTRY DOOR) · airframe 60,450 hrs · 64,920 cycles
AFT ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED WHEN OPENING THE DOOR. MX FERRY TO MCO, REMOVED AND REPLACED SLIDE PER MM.
Part: VALVE — LEAKING (LT ENGINE) · airframe 59,915 hrs · 64,260 cycles
AIR TURNBACK, F/A REPORTED FLUID SMELL IN FWD CABIN. FOUND NR 1 ENGINE TR ISOLATION VALVE LEAKING. REMOVED AND REPLACED NR 1 ENGINE TR ISOLATION VALVE PER MM.
2002
Part: SKIN — CRACKED (FUSELAGE) · airframe 59,727 hrs · 64,041 cycles
DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 761, BELOW STR 18R. REPAIRED SKIN PER SRM.
Part: CAP — MISSING (CABIN) · airframe 59,675 hrs · 63,975 cycles
DURING SCHEDULED C2 CHECK, FOUND EEPLS END CAP MISSING AT AFT CABIN. INSTALLED EEPLS END CAP PER MM.
Part: ADC — FAULTY (E/E COMP) · airframe 59,607 hrs · 63,890 cycles
AIR TURNBACK, CAPTAINS ALTIMETER FAILED, ALTITUDE ALERT FAILED AND MACH TRIM FAIL LIGHT ILLUMINATED. REMOVED AND REPLACED AIR DATA COMPUTER PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 59,425 hrs · 63,652 cycles
DURING WALKAROUND INSP, FOUND FUSELAGE SKIN CRACKED APPROX 2.25 LONG, BS 787+6, STRINGER 18L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 59,425 hrs · 63,625 cycles
FUSELAGE SKIN CRACKED AT BS 787, STR 18L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 58,825 hrs · 62,905 cycles
DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 344, STR 22L. REPAIRED SKIN PER SWA EA.
Part: BATTERY — DISCHARGED (CABIN) · airframe 58,688 hrs · 62,733 cycles
DURING SCHEDULED PM CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT OVERWING EXIT. REMOVED AND REPLACED BATTERY PER MM.
Part: CAP — MISSING (CABIN) · airframe 58,192 hrs · 62,104 cycles
DURING SCHEDULED C4 CHECK, FOUND EEPLS END CAP MISSING IN AFT CABIN. INSTALLED END CAP PER MM.
Part: RETAINER — LOOSE (FWD SVC DOOR) · airframe 58,192 hrs · 62,104 cycles
DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE CASE RETAINER LOOSE. REMOVED AND REPLACED CASE RETAINER PER MM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 57,530 hrs · 61,291 cycles
DURING SCHEDULED C3 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT MID LOUNGE. REMOVED AND REPLACED BATTERY PER MM.
2001
Part: BATTERY — DISCHARGED (CABIN) · airframe 56,999 hrs · 60,644 cycles
DURING SCHEDULED A2 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT MID CABIN. REMOVED AND REPLACED EXIT LIGHT BATTERY PER MM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 56,536 hrs · 60,070 cycles
DURING SCHEDULED A1 CHECK, FOUND EEPLS BATTERY INOP. REMOVED AND REPLACED BATTERY PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,527 hrs · 60,061 cycles
DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: SLIDE — UNSERVICEABLE (AFT ENTRY DOOR) · airframe 56,117 hrs · 59,604 cycles
AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.
Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 56,117 hrs · 59,604 cycles
DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM.
Part: BEARING — WORN (ELEVATOR) · airframe 55,343 hrs · 58,701 cycles
AT LOWER SPEED, LESS THAN 250 KNOTS, A PRONOUNCED DEAD SPOT IN PITCH CONTROL FELT. Removed and replaced ELEV CONTROL LOWER TORQUE TUBE BEARINGS PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,183 hrs · 58,509 cycles
DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT MID CABIN. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: WIRE — LOOSE (CABIN) · airframe 55,158 hrs · 58,476 cycles
EEPLS TRACK WIRES LOOSE. SECURED EEPLS WIRES PER MM.
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP, LT AND RT. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D CHECK, FOUND BEAR STRAP CRACKED AT BS 304, LBL 70 AND WL 258. REPAIRED STRAP PER BFG ER.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D CHECK, FOUND STRINGER 6R CRACKED AT BS 1010. REPAIRED STR PER SRM.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D CHECK, FOUND 2 EA STRINGERS CORRODED AT BS 1008, 26R & 27L. REPAIRED STR PER SRM.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 480, STR 14R. REPAIRED SHEAR TIE PER SRM.
Part: FITTING — CORRODED (HORIZ STAB) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D CHECK, FOUND LT HORIZ STAB CENTER SECTION AFT SPAR UPPER CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED FITTING PER BFG ER.
Part: FITTING — CORRODED (HORIZ STAB) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D CHECK, FOUND RT HORIZ STAB CENTER SECTION FRONT SPAR UPPER CLEVIS AFT LUG CORRODED. REPAIRED FITTING PER BFG ER.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D CHECK, FOUND 2 EA CRACKS AT STR 11R, BS 484 & BS 500+4. REPAIRED STR PER SRM & BAC DWG.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D CHECK, FOUND STR CLIP CRACKED AT BS 301, STR 9L. R&R STR CLIP PER SRM.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D CHECK, FOUND ANGLE CRACKED BS 301, STR14L. R&R ANGLE PER SRM.
Part: SKIN — CORRODED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN BULGED AT BS 727+15, STR 27L. REPAIRED SKIN PER BFG ER.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D CHECK, FOUND FWD BULKHEAD STIFFENER CRACKED AT BS 188, WL 208, LBL 25. REPAIRED STIFFENER PER BFG ER.
Part: FITTING — CORRODED (HORIZ STAB) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D CHECK, FOUND RT HORIZ STAB CENTER SECTION REAR SPAR LOWER CLEVIS AFT LUG, AFT FACE, CORRODED. REPAIRED FITTING PER BFG ER.
Part: FITTING — CORRODED (HORIZ STAB) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND HORIZ STAB CENTER SECTION AFT SPAR UPPER HINGE HOUSING ATTACH LUGS CORRODED AT RT SIDE, INBOARD AND OUTBOARD FACES. REPAIRED FITTING PER BFG ER.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND STR 4L CRACKED AT BS 907. REPAIRED STR PER SRM.
Part: FITTING — CORRODED (HORIZ STAB) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D CHECK, FOUND HORIZ STAB CENTER SECTION AFT SPAR LOWER HINGE HOUSING ATTACH FITTING CORRODED AT OUTBD LUG, INBD FACE, LT SIDE. REPAIRED FITTING PER BFG ER.
Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE BEAR STRAP CRACKED AT FWD ENTRY DOOR CUTOUT, UPPER FORWARD CORNER, APPROX 1 IN LENGTH. REPAIRED BEAR STRAP PER SWA ACO.
Part: FRAME — CORRODED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 492, WL 156, RT SIDE. REPAIRED FRAME PER SRM.
Part: FITTING — CORRODED (HORIZ STAB) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D CHECK, FOUND LT HORIZ STAB CENTER SECTION REAR SPAR HINGE HOUSING LOWER INBD ATTACH CLEVIS CORRODED AT OUTBD FACE. REPAIRED FITTING PER BRG ER.
Part: FITTING — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D CHECK, FOUND STRINGER END FITTING CRACKED AT BS 360, STR 5L. R&R STR END FITTING PER SRM.
Part: DOUBLER — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME DOUBLER CRACKED AT AFT CARGO DOOR FWD CUTOUT, BS 794, WL 159. R&R FRAME DOUBLER PER SRM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEBS CRACKED AT RBL 17.1, WL 181 & LBL 17.1, WL 234. REPAIRED VERTICAL BEAM WEB PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND BS 1156 BULKHEAD FRAME CHORD CRACKED AT LBL 1, 6 O''CLOCK POSITION. REPAIRED FRAME CHORD PER SRM.
Part: SLAT — DELAMINATED (LT WING) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND NR 2 L/E SLAT DELAMINATED AT AFT INBD CORNER. REPAIRED SLAT PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED 1/2D CHECK, FOUND 4 FUSELAGE SKIN CRACKS, UNDER PREVIOUS REPAIR, AT BS 663.75, BETWEEN STR 4R & STR 3L. REPAIRED SKIN PER SRM & T1-A51-002.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 908, BELOW STR 14R. REPAIRED SHEAR TIE PER SRM.
Part: SLAT — DELAMINATED (LT WING) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND NR 3 L/E SLAT DELAMINATED AT T/E INBOARD CORNER. REPAIRED SLAT PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME LOWER CHORD CRACKED AT BS 188, RBL 31. REPAIRED FRAME CHORD PER SRM.
Part: SPLICE — CORRODED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND 2 STR SPLICES CORRODED AT BS 907, STR 21L & STR 23L. REMOVED AND REPLACED STR SPLICES PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 727B+12, STR 18L. REPAIRED SKIN PER SRM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND BS 1016 BULKHEAD WEB SPLICE CRACKED AT AFT SIDE, STR 7R, FIRST TWO FASTENER HOLES FROM CENTER RING. REPAIRED BULKHEAD WEB PER SRM.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR FWD FUSELAGE FRAME CRACKED AT BS 794, RBL 29. REPAIRED FRAME PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND 6 STR CLIPS CRACKED AT BS 727A, STR 7L, BS 747, STR 6L &7L, BS 807, STR 7L, BS 767, STR 7L & BS 787, STR 10R. REMOVED AND REPLACED STR CLIPS PER SRM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CRACKED AT BS 947, LBL 55. REPAIRED FLOORBEAM PER T1-253-024 & T1 -453-037.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND 2 STR CLIPS CRACKED AT BS 727B, STR 6L & BS 747, STR 7R. REMOVED AND REPLACED STR CLIPS PER SRM.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND STR 23L CORRODED AT BS 910. REPAIRED STR SECTION PER SRM.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND STR 21L CORRODED AT BS 911. REPAIRED STR PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACK AT RADIO ALTIMETER ANTENNA AFT CUTOUT, FWD FASTENER HOLES. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSLEAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACKS AT WINDOWS 5L, 7L & 9L, FWD UPPER CORNERS. REPAIRED SKIN PER SRM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT STR 15L SPLICE. REPAIRED BULKHEAD WEB PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACKS AT WINDOWS 8R & 12R, FWD UPPER CORNERS. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACKED AT WINDOW 8L, AFT LOWER CORNER. REPAIRED SKIN PER SRM.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD SKIN ATTACH ANGLE CRACKED AT WL 218, RT SIDE. REMOVED AND REPLACED ATTACH ANGLE PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACKS AT WINDOWS 24L, 25L, 26L, 27L, 28L & 29L, FWD LOWER CORNERS. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACKS AT WINDOWS 3L, 8L & 11L, FWD UPPER CORNERS. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACKED AT WINDOW 10L, AFT LOWER CORNER. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACKED AT WINDOW 9R, UPPER FWD CORNER. REPAIRED SKIN PER SRM.
Part: SPLICE — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND STR 4L SPLICE CRACKED AT BS 908. REMOVED AND REPLACED STR SPLICE PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACKS AT WINDOWS 6R AND 11R, AFT LOWER CORNERS. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACKED AT WINDOW 10L, FWD UPPER CORNER. REPAIRED SKIN PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND 4 STR CLIPS CRACKED AT BS 807, STR 5L & 13R, BS 727B, STR 7R & BS 847, STR 4R. REMOVED AND REPLACED STR CLIPS PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACKS AT WINDOWS 24L, 25L, 28L & 29L, AFT UPPER CORNERS. REPAIRED SKIN PER SRM.
Part: STRINGER CLIP — CRACKED (CABIN) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND 6 STR CLIPS CRACKED AT BS 727A, STR 7L, BS 747, STR 6L & 7L, BS 767, STR 7L, BS 787, STR 10R, & BS 807, STR 7L. REMOVED AND REPLACED STR CLIPS PER SRM.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND BS 1016 BULKHEAD RADIAL STIFFENER ZEE ANGLE CRACKED AT STR 9L, LBL 5. REPAIRED STIFFENER ZEE ANGLE PER SRM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED T BS 986, LBL 45. REPAIRED FLOORBEAM PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND 3 STR CLIPS CRACKED AT BS 727B, STR 8L & 9L, & BS 807, STR 5L. REMOVED AND REPLACED STR CLIPS PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,150 hrs · 58,468 cycles
DURING SCHEDULED D-CHECK, FOUND STR CLIPS CRACKED AT BS 727B, STR 6L & BS 747 STR 7R. REMOVED AND REPLACED STR CLIPS PER SRM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,639 hrs · 57,923 cycles
DURING SCHEDULED C3 CHECK, FOUND AFT SVC AND ENTRY DOOR EMERGENCY EXIT OVERHEAD LIGHT ASSY INOP. RELAMPED LIGHT ASSY''''S PER MM.
2000
Part: BATTERY PACK — LOOSE (CABIN) · airframe 54,239 hrs · 57,487 cycles
AFT LEFT EMERGENCY EXIT LIGHT LOOSE AT MOUNT. R&R BATTERY PACK & LIGHT ASSY PER MM.
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 53,960 hrs · 57,170 cycles
DURING SCHEDULED A2 CHECK, FOUND EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED POWER PACK PER MM.
Part: SKIN — BIRD STRIKE (FUSELAGE) · airframe 53,861 hrs · 57,067 cycles
AIR TURNBACK, DECLARED EMERGENCY. AFTER TAKEOFF HAD MULTIPLE BIRD STRIKES. NO ENG, FLT CONTROL OR AIRFRAME PROBLEMS DURING RETURN TO AUS. INSPECTED AIRCRAFT PER MM, ZERO DAMAGE.
Part: BULB — FAILED (CABIN) · airframe 53,815 hrs · 57,014 cycles
DURING SCHEDULED C2 CHECK, FOUND MID CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT ASSY PER MM.
Part: ACTUATOR — INOPERATIVE (LT WING SLAT) · airframe 53,819 hrs · 57,019 cycles
AIR TURNBACK, NR 1 L/E SLAT WOULD NOT RETRACT AFTER TAKEOFF, EXTENDED NORMALLY. REMOVED AND REPLACED NR 1 L/E SLAT ACTUATOR PER MM.
Part: CSD — INOPERATIVE (NR 1 ENGINE) · airframe 53,708 hrs · 56,977 cycles
AIR TURNBACK, LOST NR 1 GENERATOR DURING TAKEOFF. REMOVED AND REPLACED NR 1 CSD PER MM.
Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 52,523 hrs · 55,601 cycles
AIR TURNBACK, DURING CLIMB AT APPROX 17,000 FT, RUMBLE HEARD ON NR 2 ENG AFTER ENG ANTI-ICE WAS TURNED OFF, ENG LOST POWER FROM 1.95 TO 1.7 EPR, N1 FROM 95 PERCENT TO 83 PERCENT, FUEL FLOW DROPPED TO 100 LBS. ALL OTHER INDS NORMAL. REMOVED AND REPLACED NR 2 ENG PER MM.
Part: FRAME — CRACKED (FUSELAGE)
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STUB FRAME CRACKED NEXT TO AFT SERVICE DOOR AFT OF DOOR ASSIST HANDLE. REMOVED AND REPLACED FRAME ASSY PER SRM.
Part: SKIN — CRACKED (BS 940)
DURING SCHEDULED 1/4D CHECK, FOUND THRU HFEC INSPECTION FUSELAGE EXTERNAL SKIN CRACKED, BS 940, STRINGER 11L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE)
DURING SCHEDULED 1/4D CHECK, FOUND THRU HFEC INSP, AFT ENTRY DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM.
1999
Part: SKIN — DAMAGED (LT LE SLAT)
UPPER AFT SECTION OF NR 1 L/E SLAT TORN AND DELAMINATED. REMOVED AND REPLACED NR 1 L/E SLAT PER MM.
Part: SKIN — CRACKED (BS 312)
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED, BS 312, STRINGER 18R. REPAIRED SKIN PER SRM.
Part: ACTUATOR — LEAKING (RT SPOILER)
AIR TURNBACK, MASTER CAUTION HYDRAULIC, AND BOTH ENGINE DRIVEN PUMPS LOW PRESSURE LIGHTS CAME ON AT ROTATION. BRAKE ENERGY APPROX 18 FOOT POUNDS AFTER LANDING. FOUND NR 6 FLIGHT SPOILER ACTUATOR LEAKING (BLOWN SEAL). REMOVED AND REPLACED ACTUATOR PER MM.
Part: SWITCH — MALFUNCTIONED (NR 2 ENGINE)
DURING CRUISE, NR 2 ENGINE OIL BYPASS FILTER LIGHT CAME ON. DIVERTED TO LAS WITH THRUST LEVER BACK TO IDLE, LIGHT REMAINED ON AND WENT OUT DURING DESCENT. INSPECTED NR 2 OIL FILTER AND FOUND NO CONTAMINANTS. DRAINED ALL OIL FROM TANK AND RESERVICED. OIL FILTER BYPASS STILL REMAINED LIT. REMOVED AND REPLACED OIL DIFFERENTIAL SWITCH AND ALL CHECKED GOOD PER MM.
Part: OIL SCREEN — DIRTY (NR 2 ENGINE)
AIR TURBACK, IN FLIGHT ENGINE SHUT DOWN. OIL FILTER BYPASS LIGHT ILLUMINATED ON NR 2 ENG DID NOT GO OUT AT IDLE. OIL TEMP WAS STEADILY CLIMBING ABOVE 120 DEGREES C. FOUND CARBON DEPOSIT ON MAIN OIL SCREEN. REMOVED AND REPLACED OIL SCREEN PER MM.
Part: FIRE WARNING — MALFUNCTIONED (APU)
APU FIRE WARNING BELL AND LIGHT ILLUMINATED DURING FLIGHT. PULLED FIRE HANDLE AND DISCHARGED APU FIRE BOTTLE. INSPECTED APU AND TAILPIPE, NO EVIDENCE OF FIRE FOUND. OK TO CONTINUE PER MEL. REMOVED AND REPLACED FIRE BOTTLE DURING OVERNIGHT CHECK PER MM.
Part: SKIN — CRACKED (BS 885)
DURING SCHEDULED C4 CHECK, FOUND A 2.5 INCH LONG CRACK AT FUSELAGE SKIN, BS 885, STR 24R, (CONFIRMED WITH EDDY CURRENT INSPECTION). REPAIRED PER SRM.
Part: LINE — CHAFED (NR 1 ENGINE)
AIR TURNBACK DUE TO 'A' SYSTEM HYDRAULIC SYSTEM LOSS. FOUND ON NR 1 ENG TWO HYD LINES CHAFED CAUSING HOLE. REPLACED BOTH LINES PER MM.
1998
Part: BATTERY PACK — DISCHARGED (COCKPIT)
DURING CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER BOEING MM.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND RIGHT OVERWING EMERGENCY LIGHTS WON'T ILLUMINATE. REMOVED AND REPLACED BOTH BATTERY PACK AND SUPPLY FOR RIGHT OVERWING EMERGENCY LIGHTS PER BOEING MM.
Part: LIGHT — INOPERATIVE (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND FLOOR TRACK LIGHTS (4 EA) AT ROW 12-13 INOP. REPAIRED PER BOEING MM.
Part: LIGHT — INOPERATIVE (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT OUT. REPAIRED EMERGENCY EXIT LIGHT PER BOEING MM.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY LIGHT BATTERY PACK IS BAD. REMOVED AND REPLACED BATTERY PACK PER BOEING MM, OPS CHECK GOOD.
Part: OVERHEAT LIGHT — ILLUMINATED (NR 1 ENG)
ON FINAL APPROACH NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED FOR ABOUT 5 SECONDS THEN WENT OUT. ALL ENGINE INDICATIONS WERE NORMAL. AIRCRAFT MADE AN UNEVENTFUL LANDING. INSPECTED ENGINE FOR LEAKS, INSPECTED LOOPS, WIRING AND CONNECTORS, NO ABNORMALITIES NOTED. REPLACED ENGINE OVERHEAT DETECTOR UNIT AND OPERATED NR 1 ENG PER AMM.
Part: INTERCOSTAL — CRACKED (CARGO COMPT)
DURING SCHEDULED C4 CHECK, FOUND CRACKED AFT CARGO DOOR UPLOCK BRACKET INTERCOSTAL. REPAIRED PER BOEING SRM.
Part: ANGLE — CRACKED (FWD DOORWAY)
DURING SCHEDULED C3 CHECK, FOUND 1 CRACK IN ANGLE AT FWD LOWER CORNER OF DOOR FRAME. REPAIRED PER BOEING SRM.
Part: SLIDE — LOW PRESSURE (CABIN)
DURING SCHEDULED A2, FOUND AFT ENTRY DOOR EMERGENCY EXIT SLIDE LOW PRESSURE. REMOVED AND REPLACED PER BOEING MM.
1997
Part: ENGINE — FAILED (NR 1)
DURING DESCENT, NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. CREW PERFORMED ENGINE SHUTDOWN CHECKLIST. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED AND FOUND METAL SHAVINGS IN OIL AND IN TAILPIPE. REPLACED ENGINE PER BOEING M/M.
Part: SKIN — DAMAGED (FUSELAGE)
SPECIAL VISIT FOR REPAIR OF LIGHTNING STRIKE DAMAGE VARIOUS AREAS OF FUSELAGE SKIN \N\NREPAIRED, PRIMED AND PAINTED AFFECTED AREAS PER BOEING SRM
Part: SKIN — CRACKED (BS 927)
DURING SCHEDULED SERVICE CHECK, FOUND A 2.5 INCH FUSELAGE SKIN CRACK, 4 INCHES AFT OF BS 927 AT S22R. REPAIRED PER BOEING SRM.
Part: STRINGER — CRACKED (BS 967-1016)
DURING SCHEDULED C-CHECK, FOUND S25L CORRODED BETWEEN BS 967 AND 1016, AFT CARGO DOORWAY FWD FRAME CRACK UNDER DOUBLER, AFT GALLEY DOOR LOWER HINGE CUTOUT CRACKED, AND A .375 INCH CRACK AT FWD ENTRY DOOR OUTER SKIN, PASSING THROUGH RIVET. REPAIRED ALL PER BOEING SRM.
Part: BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED C3 CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT FLICKERING. REPLACED BATTERY PACK PER BOEING M/M.
1996
Part: SKIN — GOUGED (BS 920)
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 920, AT S23R. REPAIRED PER BOEING SRM.
Part: BULKHEAD SKIN — OIL CANNING (BS 1016)
DURING SCHEDULED C1 CHECK, FOUND BULKHEAD SKIN OIL CANNING AT BS 1016 FWD OF APU GENERATOR CABLES. REPAIRED PER BOEING SRM.
Part: FRAME — CRACKED (CARGO DOORWAY)
DURING SCHEDULED B-CHECK, FORWARD CARGO DOORWAY FRAME CRACKED AT LOWER STOP, UPPER INBOARD CORNER. REPAIRED PER SWA RA 1-353-1494.
Part: SKIN — CRACKED (CARGO DOOR)
DURING SCHEDULED B-CHECK, FOUND AFT CARGO DOOR HANDLE CUTOUT UPPER AFT CORNER CRACKED .25 INCH ON OUTER SKIN. REPAIRED PER SWA RA 1-A52-020.
Part: BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN OVERHEAD EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M.
Part: SKIN — CRACKED (FUSELAGE)
DURING SCHEDULED B-CHECK, FOUND AFT CARGO DOOR HANDLE CUTOUT UPPER CORNER CRACKED ON OUTER SKIN. REPAIRED PER SWA RA 1-A50-020.
Part: SKIN — CRACKED (BS 727)
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B AT S18R. REPAIRED PER BOEING SRM.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SCHEDULED A1 CHECK, FOUND AFT CABIN FLOOR LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.
1995
Part: COMPRESSOR — STALLED (NR 1 ENGINE)
EN ROUTE PHX TO AUS, CREW EXPERIENCED NR 1 ENGINE COMPRESSOR STALL. CREW PERFORMED ENGINE SHUTDOWN CHECKLIST. AIRCRAFT DIVERTED TO ELP AND MADE AN UNEVENTFUL LANDING. BORESCOPED INSPECTED AND DETERMINED ENGINE CHANGE REQUIRED. REPLACED ENGINE ASSEMBLY AND PERFORMED POWER ASSURANCE RUN PER BOEING M/M.
Part: SKIN — CRACKED (RT FUS)
DURING WALKAROUND INSPECTION , FOUND A 4 INCH SKIN CRACK ON RIGHT SIDE FUSELAGE, JUST AFT OF T/E FLAPS. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.