N071SW
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.
103 reports on file, 1998-06-01 – 2003-07-08.
Part: INDICATOR — OUT OF POSITION (SLIDE BOTTLE) · airframe 70,713 hrs · 78,906 cycles
DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.
Part: ROLLER — WORN (LT WING TE FLAP) · airframe 70,280 hrs · 78,364 cycles
T/E FLAPS CAUSED SHUDDER DURING EXTENSION. REMOVED AND REPLACED LEFT T/E MID FLAP PIVOT ROLLER PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 70,179 hrs · 78,233 cycles
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT NR 1 RT PAX WINDOW LOWER AFT CUTOUT, BS 360. REPAIRED SKIN PER SWA EA.
Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 70,179 hrs · 78,233 cycles
DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.
Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 70,033 hrs · 78,040 cycles
AFT SERVICE DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.
Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 69,937 hrs · 77,253 cycles
DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM.
Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 69,390 hrs · 77,243 cycles
AFT ENTRY DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.
Earlier reports · 1998–2002 · 96 reports
2002
Part: SKIN — CRACKED (FWD ENTRY DOOR) · airframe 69,224 hrs · 77,031 cycles
DURING WALK AROUND INSPECTION, FOUND FWD ENTRY DOOR SKIN CRACKED AT UPPER AFT CORNER. REMOVED AND REPLACED FWD ENTRY DOOR PER MM.
Part: BEARING — WORN (TAIL) · airframe 69,129 hrs · 76,909 cycles
FLIGHT CONTROLS BINDING IN PITCH HEAVY FEEL. REMOVED AND REPLACED ELEVATOR TORQUE TUBE BEARING PER MM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 69,072 hrs · 76,845 cycles
DURING SCHEDULED PM CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.
Part: BEARING — WORN (LT ELEVATOR) · airframe 69,067 hrs · 76,837 cycles
IN FLIGHT, ELEVATOR VERY STIFF. ON APPROACH ELEVATOR HAS DEAD BAND AREA. REMOVED AND REPLACED LEFT ELEVATOR CONTROL ROD INPUT BEARING.
Part: CABLE — WORN (NR 1 ENGINE) · airframe 69,042 hrs · 76,805 cycles
DURING SCHEDULED RON, FOUND NR 1 ENGINE THRUST CONTROL TELEFLEX CABLE WORN. REMOVED AND REPLACED NR 1 ENGINE THRUST CONTROL TELEFLEX CABLE PER MM.
Part: WIRE — DAMAGED (CABIN) · airframe 69,018 hrs · 76,773 cycles
DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT ROW NR 1. RESPLICED EEPLS PER MM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 68,985 hrs · 76,731 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 68,985 hrs · 76,731 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND BOTH FWD AND AFT EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERIES PER MM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 68,985 hrs · 76,731 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND BOTH LT AND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,738 hrs · 76,436 cycles
DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP AT ROW NR 9. RELAMPED EEPLS PER MM.
Part: CAP — MISSING (CABIN) · airframe 68,738 hrs · 76,436 cycles
DURING SCHEDULED C2 CHECK, FOUND EEPLS END CAP MISSING IN FWD CABIN. INSTALLED END CAP PER MM.
Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 68,495 hrs · 76,124 cycles
DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.
Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 68,044 hrs · 75,544 cycles
DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 67,600 hrs · 74,995 cycles
DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 445, FWD OF AFT RAD ALT ANTENNA, BL 0. REPAIRED SKIN PER SWA RA.
Part: CABLE — FAILED (SPEED BRAKE) · airframe 67,495 hrs · 74,860 cycles
AIR TURNBACK, AIR GROUND SAFETY SENSOR FAILED ON TAKEOFF. REMOVED AND REPLACED GROUND SPEED BRAKE VALVE CABLE PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,039 hrs · 74,304 cycles
DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED LIGHT ASSY DUE TO CRACK AND BATTERY PACK PER MM.
Part: BATTERY — WEAK (AFT CARGO) · airframe 67,039 hrs · 74,304 cycles
DURING SCHEDULED SERVICE CHECK, FOUND AFT EMERGENCY EXIT LIGHT BATTERY VOLTAGE LOW. REMOVED AND REPLACED BATTERY PER MM.
Part: ACTUATOR — LEAKING (RT WING) · airframe 67,603 hrs · 74,461 cycles
DECLARED EMERGENCY, AIR TURNBACK, DURING CLIMB, LOST A HYD SYSTEM, ACCOMPLISHED APPROPIATE CK LIST AND RETURNED TO MSY. REMOVED AND REPLACED NR 6 SPOILER ACTUATOR PLUG PER MM. INSPECTION REMOVED AND REPLACED EDP CASE DRAIN FILTER AND MODULAR PACKAGE FILTER'S ALSO REMOVED AND REPLACED 'A' SYSTEM RETURN FILTER PER MM.
Part: CAP — MISSING (CABIN) · airframe 66,596 hrs · 73,747 cycles
DURING SCHEDULED C3 CHECK, FOUND EEPLS END CAP MISSING IN AFT CABIN. INSTALLED END CAP PER MM.
2001
Part: SKIN — CRACKED (FUSELAGE) · airframe 65,902 hrs · 72,930 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 1.7 INCH LONG AT BS 870, STR 23R. REPAIRED SKIN PER SRM.
Part: ACTUATOR — FAILED (L/E SLAT) · airframe 65,572 hrs · 72,540 cycles
(AIR TURNBACK) NR 4 L/E SLAT WOULD NOT RETRACT. REMOVED AND REPLACED NR 4 SLAT ACTUATOR PER MM.
Part: MODULE — ERRATIC (CABIN) · airframe 65,282 hrs · 72,219 cycles
BOTH FWD DOOR EMERGENCY EXIT LIGHTS REMAIN ILLUMINATED WHEN SWITCH IS IN THE OFF POSITION. R&R DOOR EMERGENCY LIGHT CONTROL MODULE PER MM.
Part: CAP — MISSING (CABIN) · airframe 65,053 hrs · 71,941 cycles
DURING SCHEDULED C1 CHECK, FOUND EEPLS END CAP MISSING AT AFT END. INSTALLED END CAP PER MM.
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 64,313 hrs · 71,079 cycles
DURING SCHEDULED C1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: LIGHT — LOOSE (CABIN) · airframe 64,012 hrs · 70,843 cycles
EMERGENCY EXIT LIGHT ASSY LOOSE AT MID CABIN. SECURED LIGHT ASSY PER MM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 64,048 hrs · 70,783 cycles
DURING SCHEDULED SERVICE CHECK, FOUND BELT FRAME CRACKED AT BS 344, STR 20R. REPAIRED FRAME PER SRM.
Part: DOUBLER — CRACKED (FUSELAGE) · airframe 64,021 hrs · 70,750 cycles
DURING SCHEDULED 1/2D CHECK, FOUND WINDOW BELT DOUBLER UPPER FWD CORNER OF WINDOW CUTOUTS CRACKED AT RT POSITIONS NR 1, 2, 6, 9, 10 & LT POSITIONS 1, 2, 4, 7, 8 & 10. REPAIRED WINDOWS CUTOUTS PER BFG ER, SRM & SWA SI.
Part: DOUBLER — CRACKED (FUSELAGE) · airframe 64,021 hrs · 70,750 cycles
DURING SCHEDULED 1/2D CHECK, FOUND WINDOW BELT DOUBLER UPPER AFT CORNER OF WINDOW CUTOUTS CRACKED AT LT POSITIONS NR 26 & 28. REPAIRED WINDOW CUTOUTS PER BFG ER, SRM & SWA SI.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,021 hrs · 70,750 cycles
DURING SCHEDULED 1/2D CHECK, FOUND STRINGERS CRACKED, STR 13R, BS 417 & 477 & STR 13L, BS 514. REPAIRED STRINGERS PER BFG ER, SRM & SWA SI.
Part: DOUBLER — CRACKED (FUSELAGE) · airframe 64,021 hrs · 70,750 cycles
DURING SCHEDULED 1/2D CHECK, FOUND WINDOW BELT DOUBLER LOWER AFT CORNER OF WINDOW CUTOUTS CRACKED AT RT POSITIONS NR 3, 5, 8, & LT POSITIONS 2, 8 & 9. REPAIRED WINDOW CUTOUTS PER BFG ER, SRM & SWA SI.
Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 64,021 hrs · 70,750 cycles
DURING SCHEDULED 1/2D CHECK, FOUND LT HORIZ STAB CENTER SECTION REAR SPAR UPPER AND LOWER AFT CLEVIS LUGS CORRODED. REPAIRED LUGS PER BFG ER.
Part: FLOORBEAM — CORRODED (CABIN) · airframe 64,021 hrs · 70,750 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 987, LBL 22 TO RBL 55. REPAIRED FLOORBEAM UPPER CHORD PER BFG ER.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,021 hrs · 70,750 cycles
DURING SCHEDULED 1/2D CHECK, FOUND STR CLIP CRACKED AT BS 500, STR 11R. REMOVED AND REPLACED STR CLIP PER BAC DWG.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 64,021 hrs · 70,750 cycles
DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM INBOARD CHORD CORRODED AT BS 915 TO BS 1006, RBL 44 TO RBL 60. REPAIRED CREASE BEAM PER SRM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,021 hrs · 70,750 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 947, RBL 43 TO RBL 47. REPAIRED FLOORBEAM PER BFG ER.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,021 hrs · 70,750 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 270, LBL 10 TO RBL 11. REPAIRED FLOORBEAM PER SRM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,021 hrs · 70,750 cycles
DURING SCHEDULED 1/2D CHECK, FOUND 2 BS 178 BULKHEAD VERTICAL BEAM WEB CRACKS AT RBL 17, WL 230. REPAIRED VERTICAL BEAM WEB PER ER.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,021 hrs · 70,750 cycles
DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT LBL 5.7, WL 205. REPAIRED VERTICAL BEAM WEB PER ER.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,021 hrs · 70,750 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 277, LBL 17 & LBL 24. REPAIRED FLOORBEAM UPPER CHORD PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 64,021 hrs · 70,750 cycles
DURING SCHEDULED 1/2D CHECK, FOUND BS 1142 UPPER FUSELAGE FRAME CHORD CRACKED AT STR 12R. REPAIRED FRAME CHORD PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 64,021 hrs · 70,750 cycles
DURING SCHEDULED 1/2D CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK BETWEEN BS 727 & BS 747, STR 13R. REPAIRED SKIN PER SRM & SWA SI.
Part: CLIP — CRACKED (FUSELAGE) · airframe 64,021 hrs · 70,750 cycles
DURING SCHEDULED 1/2D CHECK, FOUND STR CLIP CRACKED AT STR 24R, BS 493 TO BS 500. REMOVED AND REPLACED STR CLIP PER SRM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,021 hrs · 70,750 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 1016, LBL 15. REPAIRED FLOORBEAM UPPER CHORD PER SRM.
Part: BRACKET — CORRODED (FWD ENTRY) · airframe 64,021 hrs · 70,750 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR AFT GIRT ASSY BRACKET CORRODED. REMOVED AND REPLACED GIRT BRACKET ASSY PER SRM.
Part: DOOR FRAME — CRACKED (FWD CARGO BAY) · airframe 64,021 hrs · 70,750 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FWD CARGO DOOR AFT FUSELAGE FRAME CRACKED AT BS 492.4, LOWER DOOR STOP. REPAIRED FRAME PER SRM.
Part: FITTING — CRACKED (RT WING) · airframe 64,021 hrs · 70,750 cycles
DURING SCHEDULED 1/2D CHECK, FOUND RT WING AILERON FITTING CRACKED, 2ND FROM INBOARD. REMOVED AND REPLACED FITTING PER SRM.
Part: FLOORBEAM — CORRODED (CABIN) · airframe 64,021 hrs · 70,750 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAMS CORRODED AT BS 967, RBL 51, RBL 41, RBL 27, RBL 4 & BS 329, RBL 65. REPAIRED FLOORBEAMS PER SRM.
Part: FLOORBEAM — CORRODED (CABIN) · airframe 64,021 hrs · 70,750 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAMS CORRODED AT BS 294, LBL 13 TO RBL 51, BS 312, LBL 8 TO RBL 8 & BS 328, LBL 30. REPAIRED FLOORBEAMS PER SRM.
Part: FRAME — CRACKED (CABIN) · airframe 64,021 hrs · 70,750 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, BETWEEN STR 13R & STR 14R. REPAIRED FRAME PER SRM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,021 hrs · 70,750 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 1016, LBL 10 TO LBL 20. REPAIRED FLOORBEAM UPPER CHORD PER SRM.
2000
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 63,724 hrs · 70,434 cycles
AFT UPPER EMERGENCY FLASHLIGHT INOP. R&R FLASHLIGHT BATTERY PER MM.
Part: AILERON — DELAMINATED (RT WING) · airframe 63,717 hrs · 70,428 cycles
FOUND RT AILERON DELAMINATED. R&R AILERON PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 63,578 hrs · 70,286 cycles
ON WALKAROUND, FOUND FUSELAGE EXTERNAL SKIN CRACKED AT BS 937, STR 24R. REPAIRED SKIN PER SRM.
Part: LAMP — INOPERATIVE (LT OVERWING) · airframe 63,569 hrs · 70,276 cycles
DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.
Part: LIGHT — INOPERATIVE (FWD PAX DOOR) · airframe 63,569 hrs · 70,276 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.
Part: SKIN — CRACKED (LT WING SLAT) · airframe 63,569 hrs · 70,276 cycles
DURING SCHEDULED SERVICE CHECK, FOUND NR 1 L/E SLAT HAS 2 CRACKS ON LOWER SURFACE. REPAIRED SLAT PER RA 1-257-0555.
Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 63,193 hrs · 69,866 cycles
DURING SCHEDULED SERVICE CHECK, FOUND LT WING INBD T/E FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,110 hrs · 69,775 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CENTER SECTION CRACKED. REMOVED AND REPLACED BS 178 CENTER SECTION PER ERO 00-1032.
Part: FRAME — CRACKED (FUSELAGE) · airframe 63,110 hrs · 69,775 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND BS 847 FRAME CRACKED AT STR S19R. REPAIRED FRAME PER ERO 00-1019.
Part: FRAME — CRACKED (FUSELAGE) · airframe 63,110 hrs · 69,775 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 RT SIDE CHORD CRACKED. REMOVED AND REPLACED SIDE CHORD PER ACO 7342-53.
Part: FRAME — CRACKED (BULKHEAD) · airframe 63,110 hrs · 69,775 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND CRACK IN CHORD AT BS 178, RBL 25, WL 215. REPAIRED CHORD PER SRM.
Part: STRINGER — CRACKED (BULKHEAD) · airframe 66,049 hrs · 73,264 cycles
DURING SCHEDULED SPECIAL VISIT CHECK, FOUND BS 178, STR 17 RT CRACKED. REPAIRED STR PER SRM.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,751 hrs · 69,351 cycles
DURING SCHEDULED C2 CHECK, FOUND STRINGER 25R CORRODED BETWEEN BS 942 - 1116. REMOVED AND REPLACED STRINGER SECTION PER SRM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,923 hrs · 68,435 cycles
DURING SCHEDULED C1 CHECK, FOUND SEVERAL EEPL INOP. RELAMPED EEPLS PER MM.
1999
Part: BATTERY — DISCHARGED (FLASHLIGHT)
DURING SCHEDULED SPECIAL VISIT, FOUND FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.
Part: BRACKET — LOOSE (SERVICE DOORWAY)
DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY AND AFT SERVICE DOOR GIRT BAR FLOOR BRACKETS LOOSE. TIGHTENED BRACKETS PER MM.
Part: LENS — FADED (ROW 10F)
DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT SIGN LENS FADED BY SEAT 10F. REMOVED AND REPLACED LENS PER MM.
Part: LIGHT — INOP (ROW 10)
DURING SCHEDULED C3 CHECK, FOUND EEPLS INOP AT ROW 10. RELAMPED PER MM.
Part: LIGHT — INOP (CABIN)
AFT UPPER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT ASSY PER MM.
Part: SHEAR TIE — CRACKED (BS 360)
DURING SCHEDULED SPECIAL VISIT, FOUND CRACKED FUSELAGE SHEAR TIE, BS 360, BETWEEN STRINGERS 14R-15R. REPAIRED SHEAR TIE PER SRM.
Part: CLIP — CRACKED (FUSELAGE)
DURING SCHEDULED SPECIAL VISIT, FOUND 3 EACH STRINGER CLIPS CRACKED, STRINGER 4R, BS 727A, BS 727B, AND BS 767. REMOVED AND REPLACED STRINGER CLIPS PER SRM.
Part: SHEAR TIE — CRACKED (BS 400)
DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED BS 400, STRINGER 14L. REPAIRED SHEAR TIE PER SRM.
Part: DOOR — AJAR (E & E COMPT)
AIR TURNBACK, NO CONTROL OF CABIN PRESSURE, FWD AIRFLOW VALVE STAYS OPEN AND CAN NOT CONTROL. FOUND E/E DOOR AJAR DUE TO SWITCH INOP, REPAIRED PER MM. OPS CHECK GOOD.
Part: CLIP — CRACKED (BS 727 & 767)
DURING SCHEDULE SPECIAL VISIT CHECK, FOUND 3 EA STRINGER CLIPS CRACKED, STRINGER 4R, BS 727A,727B, AND 767. REMOVED AND REPLACED STRINGER CLIPS PER SRM.
Part: FRAME — CRACKED (BS 951)
DURING SCHEDULED SPECIAL VISIT CHECK, FOUND CRACKED FUSELAGE FRAME, BS 951, STRINGER 19R. REPAIRED FRAME PER SRM.
Part: BOTTLE — LOW PRESSURE (SERVICE DOOR)
DURING SCHEDULED CHECK, FOUND R-2 DOOR SLIDE ASSY HAS LOW BOTTLE PRESS. REPLACED SLIDE ASSY PER MM.
Part: BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED SC CHECK, FOUND MID CABIN CEILING EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY PER M/M.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SCHEDULED SC CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING M/M.
1998
Part: STRINGER — CRACKED (BS 800)
DURING SCHEDULED SC CHECK, FOUND STRINGER CRACK AT BS 800, S10R. REPAIRED PER SRM.
Part: SKIN — CRACKED (BS 460)
DURING SCHEDULED SC CHECK, FOUND SKIN CRACKED AT SKIN LAP BS 460, S14R. REPAIRED PER SRM.
Part: STANCHION — CRACKED (BS 298)
DURING SCHEDULED 1/4D CHECK, FOUND LT FWD STANCHION HAS HFEC INDICATION OF A CRACK AT BS 298, LBL 25 INDB FASTENER 2ND FROM BOTTOM. REPAIRED PER BOEING SRM.
Part: LIGHT — INOPERATIVE (CABIN)
DURING SCHEDULED 1/4D CHECK, FOUND FWD EGRESS FLOOR TRACK HAS ONE RED LIGHT INOP. REPLACED LIGHT ASSY PER BOEING MM.
Part: KEEL BEAM — CRACKED (RT MLG WW)
DURING SCHEDULED 1/4D CHECK, FOUND KEELBEAM AFT PANEL IN W/W CRACKED. REMOVED AND REPLACED PER BOEING SRM.
Part: CHORD — CRACKED (BS 178)
DURING SCHEDULED 1/4D CHECK, FOUND LT SIDE CHORD CRACKED AT BS 178, LBL 32, WL 207. REMOVED AND REPLACED PER BOEING SRM.
Part: SKIN — CRACKED (SERVICE DRWAY)
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER CORNER OF LOWER HINGE CUTOUT. REPAIRED PER TI-A53-056.
Part: SKIN — CRACKED (PAX DOORWAY)
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED WITH PREVIOUS STOP DRILL AT LOWER CORNER OF LOWER HINGE CUTOUT SKIN AND DOUBLER CRACK 1.5 BEAR STRAP CRACK .5. REPAIRED PER SWA RA 1-253-1888.
Part: SKIN — CORRODED (BS 967)
DURING SCHEDULED 1/4D CHECK, FOUND CORRODED BETWEEN SKIN AND STRINGER AT BS 967, STR 25L. REPAIRED PER BOEING SRM.
Part: ANGLE — CRACKED (FUSELAGE)
DURING SCHEDULED 1/4D CHECK, FOUND CRACKED INNER SUPPORT ANGLE UNDER WINDOW. REMOVED AND REPLACED PER BOEING SRM.
Part: BOW TIE — WORN (BS 1156)
DURING SCHEDULED 1/4D CHECK, FOUND LT BOW TIE WORN AT BS 1156. REMOVED AND REPLACED PER BOEING SRM.
Part: SKIN — CRACKED (LT WING)
DURING SCHEDULED 1/4D CHECK, FOUND NR 2 SLAT AT INNER AUX TRACK AREA LOWER SKIN AROUND RIVET CRACKED. REPAIRED PER BOEING SRM.
Part: SKIN — FRAYED (LT WING)
DURING SCHEDULED 1/4D CHECK, FOUND LT W/W CUTOUT OUTER REAR PANEL FWD EDGE IS FRAYED AND WORN. REPAIRED PER BOEING SRM.
Part: SKIN — BENT (SERVICE DOORWAY)
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN BENT AT AFT LOWER CORNER OF LOWER HINGE CUTOUT. REPAIRED PER BOEING SRM.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT FOR AFT SERVICE AND AFT ENTRY WEAK. REMOVED AND REPLACED BATTERY PACK PER BOEING MM.
Part: SKIN — DAMAGED (L1 DOORWAY)
DURING SCHEDULED BC CHECK, FOUND SHEET METAL REPAIR TO AFT ENTRY DOOR AREA L1 DOOR RIG. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (BS 950)
DURING SCHEDULED C2 CHECK, FOUND CRACKED FUSELAGE SKIN AT FASTENER AT BS 950 ABOVE STR 21L. REPAIRED PER BOEING SRM.
Part: INTERCOSTAL — CRACKED (CARGO DOORWAY)
DURING SCHEDULED C 2 CHECK, FOUND CRACKED AFT CARGO DOOR UPLATCH INTERCOSTAL. REPAIRED PER BOEING SRM.