N064SW
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.
88 reports on file, 1998-07-07 – 2001-11-13.
Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 69,284 hrs · 77,122 cycles
DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 68,986 hrs · 76,796 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY & FWD SVC DOOR'S EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 68,766 hrs · 76,536 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740, STR 17R. REPAIRED SKIN PER SRM.
Part: SLIDE — OUT OF POSITION (AFT DOOR) · airframe 68,741 hrs · 76,504 cycles
BOTH AFT DOOR EMERGENCY EVAC SLIDES PRESS IND OUT OF VIEW. REPOSITIONED SLIDES PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,545 hrs · 76,288 cycles
DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT BOTH OVERWING EXITS. RELAMPED EXIT LIGHTS PER MM.
Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 68,534 hrs · 76,274 cycles
DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM.
Part: LENS — LOOSE (SERVICE DOOR) · airframe 68,456 hrs · 76,185 cycles
DURING SCHEDULED RON CHECK, FOUND FWD SVC DOOR EMERGENCY EXTERIOR EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER MM.
Part: LIGHT — LOOSE (ENTRY DOOR) · airframe 68,432 hrs · 76,155 cycles
AFT ENTRY DOOR EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT ASSY PER MM.
Part: BEAM — CRACKED (FUSELAGE NOSE) · airframe 68,414 hrs · 76,133 cycles
DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM CRACKED APRROX 2 LONG, RBL 5.7, WL 183. REPAIRED BEAM PER SWA RA.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,414 hrs · 76,133 cycles
DURING SCHEDULED 1/4D CHECK, FOUND 3 EEPLS INOP. REMOVED AND REPLACED LIGHT ASSY'S PER MM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 68,414 hrs · 76,133 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 663, BL 0. REMOVED AND REPLACED CHORD PER SWA ACO.
Part: TAB — DELAMINATED (RH WING) · airframe 68,414 hrs · 76,133 cycles
DURING SCHEDULED 1/4D CHECK, FOUND RH AILERON TAB DELAMINATED. R&R TAB PER MM.
Part: WEB — CRACKED (FUSELAGE) · airframe 68,414 hrs · 76,133 cycles
DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 179, RBL 17.1 & WL 231. R&R VERTICAL BEAM WEB PER SRM.
Part: WEB — CRACKED (MAIN W/W) · airframe 68,414 hrs · 76,133 cycles
DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS WEB CRACKED AT BS 663+10, RBL 37. REPAIRED WEB PER SRM.
Part: LENS — CRACKED (CABIN) · airframe 68,414 hrs · 76,133 cycles
DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS CRACKED AT ROW 3. R&R EXIT LIGHT LENS PER MM.
Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 67,902 hrs · 75,574 cycles
AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM.
Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 67,771 hrs · 75,423 cycles
DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY & AFT SVC DOORS EMERGENCY EVAC SLIDES PRES IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDES PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 67,771 hrs · 75,423 cycles
DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 745, ABOVE STR 16R. REPAIRED SKIN PER SRM.
Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 67,718 hrs · 75,365 cycles
AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE ASSY PER MM.
Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 67,522 hrs · 75,131 cycles
AFT ENTRY AND SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY''S PER MM.
Part: SLIDE — OUT OF TOLERANCE (ENTRY DOOR) · airframe 67,102 hrs · 74,671 cycles
FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM.
Part: LIGHT — LOOSE (CABIN) · airframe 66,994 hrs · 74,546 cycles
DURING SCHEDULED C1 CHECK, FOUND EEPLS LOOSE & END CAP MISSING AT AFT END. SECURED EEPLS AND REPLACED END CAP PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,986 hrs · 74,536 cycles
DURING SCHEDULED PM CHECK, FOUND 2 EEPLS BULBS INOP AT ROW 3. RELAMPED EEPLS PER MM.
Earlier reports · 1998–2000 · 65 reports
2000
Part: INDICATOR — OUT OF POSITION (SLIDE) · airframe 66,726 hrs · 74,241 cycles
AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.
Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 66,583 hrs · 74,088 cycles
AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM.
Part: BRACKET — LOOSE (DOOR SLIDE) · airframe 66,147 hrs · 73,595 cycles
DURING SCHEDULED C4 CHECK, FOUND FWD SERVICE DOOR FWD GIRT BAR BRACKET LOOSE ON FLOOR. SECURED BRACKET PER MM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 65,677 hrs · 73,060 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAMES CRACKED, BS 440, STRINGER 24R AND STRINGER 23R, BS 492, STRINGER 20R. REPAIRED FRAMES PER ERO''S.
Part: FRAME — CRACKED (FUSELAGE) · airframe 65,677 hrs · 73,060 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD RT SIDE CHORD CRACKED. REPAIRED CHORD SECTION PER ACO.
Part: FLOORBEAM — CORRODED (CABIN) · airframe 65,677 hrs · 73,060 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND CABIN FLOORBEAM CORRODED, BS 985, RBL 43 - 46. REPAIRED BEAM PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,677 hrs · 73,060 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIP CRACKED, BS 663, STRINGER 5R. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,677 hrs · 73,060 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER 4R CRACKED, BS 749. REPAIRED STRINGER SECTION PER SRM.
Part: BATTERY PACK — INOPERATIVE (RT OVERWING) · airframe 65,644 hrs · 73,025 cycles
DURING SCHEDULED A2 CHECK, FOUND EXTERNAL EMERGENCY LIGHT INOP AFT OF RT OVERWING EXIT. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY — INOPERATIVE (CABIN) · airframe 54,473 hrs · 72,835 cycles
DURING SCHEDULED SERVICE CHECK, FOUND BOTH LT AND RT AFT EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 65,187 hrs · 72,518 cycles
AFT SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.
Part: SKIN — CRACKED (BS 993)
DURING SCHEDULED SERVICE CHECK, FOUND 2 FUSELAGE EXTERNAL SKIN CRACKS, BS 762, STRINGER 17R, AND BS 993, STRINGER 26R. REPAIRED SKIN PER SRM.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT MID CABIN. R&R BATTERY PACK PER MM.
1999
Part: SKIN — CRACKED (FUSELAGE)
FUSELAGE SKIN CRACKED ON RT SIDE, 24 INCHES BELOW NR 24 WINDOW. REPAIRED FUSELAGE SKIN PER SRM.
Part: FRAME — CRACKED (BS 663)
DURING SCHEDULED 1/2D CHECK, FOUND BS 663 FRAME CRACKED AT S2L AND S3L. REPAIRED PER BOEING SRM.
Part: SKIN — GOUGED (LT WING)
DURING SCHEDULED D-CHECK, FOUND FIXED L/E SKIN WAS GOUGED AT CENTER UPSTOP CUTOUT FOR NR 5 SLAT, I/B AND O/B SIDE'S. CUT OUT DAMAGED FIXED LEADING EDGE SKIN, FABRICATED NEW LEADING EDGE SKIN AND SPLICE PLATES, TREATED REPAIR PARTS, INSTALLED NEW SKIN AND SEALED AS PER TRAMCO EWO 98-1175.
Part: SPLICE — DAMAGED (BS 360)
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE DAMAGED AT BS 360, S14R. REMOVED AND REPLACED SPLICE PER BOEING SRM.
Part: SKIN — CRACKED (NR 5 LE SLAT)
DURING SCHEDULED D-CHECK, FOUND NR 5 SLAT LOWER T/E SKIN LOWER SURFACE CRACKED AT FASTENER LOCATION 39 INCHES FROM I/B END. REPAIRED PER TRAMCO EWO 98-1191.
Part: FRAME — CRACKED (BS 727)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727, AT S14R. REPAIRED PER TRAMCO EWO 98-1166.
Part: SKIN — DENTED (BS 727)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 727A + 12 BETWEEN S23-24R.
Part: STRAP — CRACKED (BS 1138)
DURING SCHEDULED D CHECK, FOUND BS 1138 LT DOUBLER STRAP CRACKED AT 12L. REPLACED STRAP PER BOEING SRM.
Part: FRAME — DENTED (BS 827)
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME DENTED BEYOND LIMITS AT BS 827, LBL 28, WL 162. REPAIRED PER BOEING SRM.
Part: STRINGER — CRACKED (BS 1140)
DURING SCHEDULED D CHECK, FOUND STRINGER 5R UPPER AFT CHORD CRACKED AT BS 1140. REPLACED DAMAGED SECTION PER BOEING SRM AND BOEING DRAWING 65C35130.
Part: SKIN — DENTED (BS 290)
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AT 290, AT S20R. REPAIRED PER BOEING SRM.
Part: CHORD — CORRODED (BS 270)
DURING SCHEDULED D CHECK, FOUND Z-CHORD BODY CORRODED AT BS 270, LBL 5. REPAIRED PER BOEING SRM.
Part: STRAP — CRACKED (BS 1140)
DURING SCHEDULED D CHECK, FOUND BS 1140 RT DOUBLER STRAP CRACKED AT S5R. REPLACED STRAP PER BOEING SRM AND BOEING DRAWING 65C35130.
Part: SKIN — CRACKED (SERV DOORWAY)
DURING SCHEDULED D CHECK, FOUND CRACK IN LOWER HINGE CUTOUT OF AFT SERV DOOR. REPAIRED PER BOEING SRM.
Part: FLOORBEAM — CORROSION (BS 380-520)
DURING SCHEDULED D CHECK, FOUND FWD CARGO FLOORBEAM CORRODED FROM 380-520, RBL 2 AND LBL 3. REPAIRED PER BOEING SRM.
Part: STRAP — CRACKED (BS 1139)
DURING SCHEDULED D CHECK, FOUND S5L LT DOUBLER STRAP CRACKED AT BS 1139. REPLACED STRAP PER BOEING SRM AND BOEING DRAWING 65C35130.
Part: STRINGER — CRACKED (BS 1139-1142)
DURING SCHEDULED D CHECK, FOUND STRINGER 5L UPPER CHORD CRACKED FROM BS 1139 TO 1142. REPLACED DAMAGED SECTION PER BOEING SRM AND BOEING DRAWING 65C35130.
Part: STRINGER — CRACKED (BS 520)
DURING SCHEDULED D CHECK, FOUND STRINGER 19R AT BS 520 CRACKED ON LOWER SIDE. REPLACED DAMAGED SECTION PER BOEING SRM.
Part: SHEAR TIE — CRACKED (BS 1138)
DURING SCHEDULED D CHECK, FOUND UPPER SHEAR TIE AT BS 1138 CRACKED AT S5R. REPLACED SHEAR TIE PER BOEING SRM AND BOEING DRAWING 65C35824
Part: STRINGER — CRACKED (BS 1154)
DURING SCHEDULED D CHECK, FOUND STRINGER 5L LOWER CHORD CRACKED AT BS 1154. REPLACED DAMAGED SECTION PER BOEING SRM AND BOEING DRAWING 65C35130.
Part: STRAP — CRACKED (BS 1138)
DURING SCHEDULED D CHECK, FOUND BS 1138 RT DOUBLER STRAP CRACKED AT S12R. REPLACED STRAP PER BOEING SRM.
Part: STRINGER — CRACKED (BS 1006)
DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 1006, AT S12L. REPLACED DAMAGED SECTION PER BOEING SRM.
Part: SKIN — DENTED (BS 258)
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AT 258, 3.5 BELOW S24R. REPAIRED PER BOEING SRM.
Part: CHORD — CRACKED (BS 1155)
DURING SCHEDULED D CHECK, FOUND BS 1155 RT LOWER CHORD CRACKED AT 5R. REPLACED CHORD PER BOEING SRM.
Part: BULKHEAD — GOUGED (BS 727)
DURING SCHEDULED D CHECK, FOUND RT WHEEL WELL WALL BULKHEAD BS 727 GOUGED AT RBL 5, APPROX WL 180, AFT OF FLAP DRIVE MOTOR. REPAIRED PER BOEING SRM AND TRAMCO EWO 98-1188.
1998
Part: FRAME — CRACKED (BS 360)
DURING SCHEDULED D CHECK, FOUND FUSE FRAME CRACKED AT BS 360, BETWEEN S14 AND 13R. REPAIRED PER BOEING SRM.
Part: SKIN — DENTED (BS 997)
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AT BS 997, BELOW S13L. INSTALLED REPAIR DOUBLERS PER BOEING SRM.
Part: SPLICE — CORRODED (BS 900-917)
DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CORRODED AT BS 900 TO 917 AT S26L. INSTALLED REPAIR DOUBLERS PER BOEING SRM.
Part: FRAME — CRACKED (BS 747)
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, ABOVE S14L. INSTALLED REPAIR DOUBLERS PER BOEING SRM.
Part: STRINGER — CORRODED (BS 913-925)
DURING SCHEDULED D CHECK, FOUND STRINGER CORRODED AT BS 913 TO 925, S26R. REPAIRED PER BOEING SRM.
Part: SKIN — DENTED (BS 267)
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AT BS 267, BELOW S24R. INSTALLED REPAIR DOUBLERS PER BOEING SRM.
Part: SKIN — CREASED (BS 1018)
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CREASED AT BS 1018, 2 ABOVE S16R. INSTALLED REPAIR DOUBLER PER BOEING SRM.
Part: FLOORBEAM — CORRODED (BS 727-947)
DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORROSION AT BS 727 TO 947, RBL 3, WL 159. REPAIRED PER BOEING SRM.
Part: WEB — CRACKED (BS 178)
DURING SCHEDULED D CHECK, FOUND BS 178 WEB CRACKED AT WL 234. INSTALLED REPAIR DOUBLER PER BOEING SRM.
Part: SKIN — DENTED (BS 853)
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AT BS 853. REPAIRED PER BOEING SRM.
Part: SKIN — GOUGED (BS 307)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 307, WL 242, LBL 71. REPAIRED PER BOEING SRM.
Part: SKIN — CORRODED (BS 470/500)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORRODED AROUND NUTPLATE HOLES AT BS 470 AND BS 500A +14. REPAIRED PER BOEING SRM.
Part: SPLICE — CRACKED (BS 908)
DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER SPLICE AND CLIP CRACKED AT BS 908, AT S4L. REPAIRED PER BOEING SRM.
Part: STRINGER — CRACKED (BS 1016)
DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER CRACKED AT BS 1016, AT S5R. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (BS 536)
DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 536, 6 UP FROM S10L. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (BS 727-908)
DURING SCHEDULED SPECIAL VISIT CHECK, FOUND SKIN LAP CRACKS AT BS 908 TO 1016, AT S4 LT, S10 RT AND LT. REPAIRED PER SWA ACO 6717-53.
Part: SKIN — CRACKED (BS 908-947)
DURING SCHEDULED SPECIAL VISIT CHECK, FOUND SKIN LAP CRACKS AT BS 908 TO 947, AT S10R AND S14R. REPAIRED PER DALFORT XEA X2-53-226.
Part: SKIN LAP — CRACKED (BS 360-540)
DURING SCHEDULED SPECIAL VISIT CHECK, FOUND SKIN LAP CRACKS AT BS 360 TO 540, AT S10 RT AND LT, S4 LT AND RT AND S14 LT. REPAIRED PER SWA ACO 6717-53.
Part: SHEAR TIE — CRACKED (BS 360)
DURING SCHEDULED SPECIAL VISIT CHECK, FOUND SHEAR TIE CRACKED AT RT BS 360 JUST BELOW S15R. REPAIRED PER BOEING SRM.
Part: STRINGER — CRACKED (BS 410)
DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER CRACKED AT BS 410, S4L. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (BS 727-908)
DURING SCHEDULED SPECIAL VISIT CHECK, FOUND SKIN LAP CRACKS AT BS 727 TO 908, AT S4 L AND RT, S10 RT AND LT. REPAIRED PER SWA ACO 6717-53.
Part: FRAME — CRACKED (BS 663)
DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FUSELAGE FRAME AT STRINGER SPLICE CRACKED AT BS 663, AT S4L. REPAIRED PER BOEING SRM.
Part: LIGHT — INOPERATIVE (PAX DOOR)
DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY AND FWD SERVICE DOOR EMERGENCY SLIDE LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY PER BOEING MM.
Part: LIGHT — INOPERATIVE (CABIN)
DURING WALKAROUND CHECK, FOUND LT AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER BOEING MM.
Part: LIGHT — LOOSE (CABIN)
DURING WALKAROUND CHECK, FOUND EXIT LIGHT ABOVE FWD SERVICE DOOR LOOSE AND ILLUMINATES FREQUENTLY. REPOSITIONED LIGHT ASSY INTO LOCKS OF LIGHT ASSY HOUSING AS PER BOEING MM.
Part: STRINGER — CORRODED (BS 967-1006)
DURING SCHEDULED C4 CHECK, FOUND CORRODED AFT LOWER LOBE 5-27L, ON STRINGER FROM BS 967-1006. REPAIRED PER BOEING MM.
Part: SKIN — CRACKED (BS 766)
DURING SCHEDULED C4 CHECK, FOUND CRACKED RT FUSELAGE SKIN AT BS 766 ABOVE S-19R. REPAIRED PER BOEING SRM.