N067SW
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.
47 reports on file, 1998-08-11 – 2001-12-08.
Part: SKIN — CRACKED (FUSELAGE) · airframe 67,100 hrs · 74,191 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 777, STR 25L. REPAIRED SKIN PER SRM.
Part: TRANSMITTER — ERRATIC (NR 2 EPR) · airframe 65,599 hrs · 72,437 cycles
(ABORTED TAKEOFF) NR 2 EPR INDICATION ERRATIC DURING POWER INCREASE. REMOVED AND REPLACED NR 2 EPR TRANSMITTER PER MM.
Part: PIN — BENT (CONNECTOR) · airframe 65,596 hrs · 72,435 cycles
(ABORTED TAKEOFF) NR 2 EPR DID NOT RESPOND INITIALLY, CAME UP BUT VARIED FROM IDLE TO APPROX 1.6. REMOVED AND REPLACED NR 2 ENG EPR TRANSMITTER AND REMOVED AND REPLACED BENT PIN AT TRANSMITTER CONNECTOR PER MM.
Part: BATTERY PACK — DISCHARGED (ENTRY DOOR) · airframe 65,445 hrs · 72,260 cycles
DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,376 hrs · 72,179 cycles
DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. R&R LT OVERWING LIGHT ASSY PER MM.
Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 65,298 hrs · 72,083 cycles
FWD SVC DOOR EMERGENCY EXIT LIGHT INOP. R&R EMERGENCY EXIT LIGHT ASSY PER MM.
Part: CAP — MISSING (CABIN) · airframe 65,025 hrs · 71,787 cycles
DURING SCHEDULED C1 CHECK, FOUND EEPLS END CAP MISSING AND WIRING EXPOSED AT FWD GALLEY. REPLACED END CAP AND SECURED WIRING PER MM.
Part: TRACK — LOOSE (CABIN) · airframe 64,715 hrs · 71,435 cycles
EEPLS TRACK SECTION LOOSE. SECURED TRACK SECTION PER MM.
Earlier reports · 1998–2000 · 39 reports
2000
Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 64,108 hrs · 70,775 cycles
FWD ENTRY DOOR EMERGENCY EVAC SLIDE PARTIALLY OUT OF CONTAINER. REPOSITIONED EVAC SLIDE ASSY PER MM.
Part: BATTERY — DISCONNECTED (CABIN) · airframe 64,099 hrs · 70,763 cycles
DURING SCHEDULED SERVICE CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT INOP. RECONNECTED BATTERY AND OPS CK GOOD.
Part: COVER — LOOSE (CABIN FLOOR) · airframe 63,765 hrs · 70,380 cycles
EEPLS TRACK LIGHT LOOSE. SECURED LIGHT COVER PER MM.
Part: COVER — LOOSE (CABIN FLOOR) · airframe 63,765 hrs · 70,380 cycles
EEPLS TRACK COVER LOOSE. SECURED TRACK COVER PER MM.
Part: BRACKET — LOOSE (GIRT BAR) · airframe 63,461 hrs · 70,037 cycles
DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR GIRT BAR BRACKET LOOSE IN FLOOR. SECURED BRACKET PER MM.
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 63,446 hrs · 70,020 cycles
DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT LIGHTING INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 62,945 hrs · 69,456 cycles
DURING SCHEDULED SERVICE CHECK, FOUND LT WING NR 1 L/E SLAT I/B TRAILING EDGE DELAMINATED. REMOVED AND REPLACED L/E SLAT PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 62,862 hrs · 69,353 cycles
DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR UPPER HINGE FUSELAGE SKIN CUT OUT CRACKED. REPAIRED SKIN PER SRM.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,862 hrs · 69,353 cycles
DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 28R CORRODED BETWEEN BS 344-350. REPAIRED STRINGER PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 62,862 hrs · 69,353 cycles
DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR FWD LOWER FUSELAGE SKIN CUT OUT CRACKED. REPAIRED SKIN PER XEA X2-53-280.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,862 hrs · 69,353 cycles
DURING SCHEDULED 1/4D CHECK, FOUND SEVERAL EEPLS INOPERATIVE. R&R SEVERAL LIGHT ASSY''S PER MM.
Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 62,862 hrs · 69,353 cycles
DURING SCHEDULED 1/4D CHECK, FOUND RT WING EXTERNAL EMERGENCY ESCAPE LIGHT INOPERATIVE. R&R LIGHT ASSY PER MM.
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 62,862 hrs · 69,353 cycles
DURING SCHEDULED 1/4D CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. R&R BATTERY PACK PER MM.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 62,862 hrs · 69,353 cycles
DURING SCHEDULED A2 CHECK, FOUND AFT EMERGENCY FLASHLIGHT INOPERATIVE. CONNECTED BATTERY CHARGER PER MM. OPS CK GOOD.
Part: STRINGER — CORRODED (E/E BAY) · airframe 62,862 hrs · 69,353 cycles
DURING SCHEDULED 1/4D CHECK, FOUND CORROSION DAMAGE AT STRINGER 28R, BETWEEN BS 312-328. REPAIRED STRINGER PER SRM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,862 hrs · 69,353 cycles
DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, WL 218, LBL 8 TO LBL 16, WL 207, LBL 11 TO LBL 12.5 AND RBL 9 TO RBL 12. REPAIRED BULKHEAD PER SRM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,862 hrs · 69,353 cycles
DURING SCHEDULED 1/4 D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 2.5, WL 223. REPAIRED PER ACO.
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 62,800 hrs · 69,287 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY — INOPERATIVE (ROW 4) · airframe 62,791 hrs · 69,276 cycles
DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD EMERGENCY LIGHT INOP AT ROW 4. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: SLIDE — DISLODGED (PAX DOOR) · airframe 62,089 hrs · 68,522 cycles
FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.
Part: BLEED VALVE — ERRATIC (APU)
AIR TURNBACK, DURING CLIMB, AIRCRAFT HAD A LOUD THUMPING NOISE AND VIBRATION MOSTLY HEARD IN AT THE AFT SECTION. PERFORMED AIRFRAME VIBRATION CONDITION INSPECTION. NO DEFECTS NOTED. POSSIBLY APU COMPRESSOR STALL. DURING RON, REMOVED AND REPLACED APU ANTI-SURGE BLEED CONTROL VALVE PER MM.
1999
Part: SKIN — DELAMINATED (NR 4 LE SLAT)
DURING SCHEDULED SERVICE CHECK, FOUND NR 4 L/E SLAT DELAMINATED ON OUTBOARD UPPER CORNER. REPAIRED SLAT PER SRM.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD GALLEY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BOTH FWD GALLEYS EMERGENCY EXIT LIGHT BATTERY PACKS PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FWD CABIN EMERGENCY EXIT LIGHT BATTERY PACK PER MM.
Part: BULB — FAILED (CABIN)
DURING SCHEDULED SPECIAL VISIT, FOUND EEPLS LIGHT INOP. REPLACED LIGHT BULBS PER MM.
Part: POWER SUPPLY — INOPERATIVE (CABIN)
DURING SCHEDULED SPECIAL VISIT, FOUND AFT CEILING EMERGENCY LIGHT POWER SUPPLY INOP. REMOVED AND REPLACED POWER SUPPLY ASSY PER MM.
Part: LENS — MISSING (SERVICE DOOR)
DURING SCHEDULED SPECIAL VISIT, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT LENS MISSING. REPLACED LENS ASSY PER MM.
Part: FRAME — CRACKED (BS 947)
DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FRAME CRACKED, BS 947, BETWEEN STRINGERS 17R-19R. REPAIRED FRAME PER SRM.
Part: STRINGER — CORRODED (BS 968)
DURING SCHEDULED SPECIAL VISIT CHECK, FOUND CORROSION AT STRINGER 27R, BS 968. REPAIRED STRINGER PER SRM.
Part: CLIP — CRACKED (BS 380)
DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER CLIP CRACKED, BS 380, STRINGER 5L. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER — CRACKED (BS 907)
DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER 4L CRACKED, BS 907. REPAIRED STRINGER PER SRM.
Part: STRINGER — CRACKED (BS 276 & 310)
DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER 19R 2 EACH CRACKS, BS 276, AND BS 310. REPAIRED STRINGER PER SRM.
Part: SHEAR TIE — CRACKED (BS 380)
DURING SCHEDULED SPECIAL VISIT CHECK, FOUND SHEAR TIE CRACKED, BS 380, STRINGER 14L. REPAIRED SHEAR TIE PER SRM.
Part: SHEAR TIE — CRACKED (BS 360)
DURING SCHEDULED SPECIAL VISIT CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STRINGERS 14R-15R. REPAIRED SHEAR TIE PER SRM.
1998
Part: SKIN — CORRODED (BS 727)
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN BULGE AT BS 727, S28R. REPAIRED PER BOEING SWA RA 1-253-1895.
Part: SKIN — BULGED (BS 727)
DURING SCHEDULED C4 CHECK, FOUND SKIN BULGED AT BS 727, STR 28R. REPAIRED PER SWA RA NR 1-253-1895.
Part: LIGHT — INOPERATIVE (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR OVERHEAD EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AND OPS CKD OK PER BOEING MM. REPAIRED PER BOEING SRM.
Part: STRAP — CRACKED (SERVICE DOORWAY)
DURING SCHEDULED RON CHECK, HFEC INDICATES BEAR STRAP CRACKED AT LOWER FUSELAGE MOUNTED HINGE FITTING AT FWD SERVICE DOOR. REPAIRED PER SWA RA NR 1-253-1871.
Part: FRAME — CRACKED (BS 294.5)
DURING SCHEDULED RON CHECK, FOUND BODY FRAME AT BS 294.5 CRACKED AT LOWER SERVICE DOOR HINGE CUTOUT, ON AFT SIDE OF FRAME. REPAIRED PER BOEING SRM.