N082SW
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.
100 reports on file, 1997-12-23 – 2004-12-05.
Part: SKIN — CRACKED (FUSELAGE) · airframe 70,812 hrs · 78,256 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 747 + 14, STRINGER 19R, CRACKED. REPAIRED SKIN SECTION PER SRM.
Part: GIRT BAR — INOPERATIVE (R2 DOOR SLIDE) · airframe 70,559 hrs · 77,914 cycles
R2 DOOR EVACUATION SLIDE GIRT BAR WOULD NOT ARM AT FLOOR BRACKETS. REMOVED AND REPLACED SLIDE ASSY PER MM.
Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 70,463 hrs · 77,791 cycles
ON APPROACH TOWER REPORTED NLG TO BE PARTIALLY EXTENDED, HAD THREE GREEN GEAR IND. WENT AROUND CYCLED GEAR, THREE GREEN LIGHTS, VISUAL CHECK THRU GEAR INSP WINDOW ALL NORMAL. VISUALLY INSP NLG AND PROX SWITCHES. NO DEFECTS PER MM.
Part: SKIN — DELAMINATED (ELEVATOR) · airframe 70,415 hrs · 77,727 cycles
DURING SCHEDULED A1 CHECK, FOUND RT ELEVATOR T/E SKIN DELAMINATED. REPAIRED ELEVATOR SKIN PER EA.
Part: LIMITER — BINDING (MLG WW) · airframe 70,029 hrs · 77,209 cycles
WITH FLAPS EXTENDED INFLIGHT, CONTROLS BIND IN ROLL IN BOTH DIRECTIONS. WITH FLAPS UP ROLL IS NORMAL (AUTOPILOT WILL STAY ENGAGED WITH FLAPS DOWN) FELT BINDING AGAIN IN BANK WHEN FLAPS EXTENDED FOR LANDING. REMOVED AND REPLACED AILERON FORCE LIMITER PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 69,931 hrs · 77,079 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 24L, CRACKED. REPAIRED SKIN PER EA.
Part: ROD END — OUT OF ADJUST (LT WING SLAT) · airframe 69,877 hrs · 77,007 cycles
DURING TAKEOFF UNTIL APPROX 10 TO 15 SECONDS AFTER GEAR RETRACTION ABNORMAL RIGHT ROLLING TENDENCY, REQUIRING APPROX 30 DEGREES YOKE DEFLECTION. DURING FLAP EXTENSION ON GROUND TOOK SEVERAL CYCLES OF FLAPS TO EXTINGUISH, SLAT NR 3 AND 4 AMBER LIGHTS ON OVERHEAD PANEL, AMBER LIGHT ON FWD PANEL. ADJUSTED NR 3 L/E SLAT ACTUATOR ROD END PER MM.
Part: PCU — LEAKING (LT WHEEL WELL) · airframe 69,624 hrs · 76,673 cycles
EXCESSIVE PLAY IN THE AILERONS. REMOVED AND REPLACED A-SYSTEM AILERON PCU PER MM.
Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 68,863 hrs · 75,682 cycles
DURING SCHEDULED SPV, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,863 hrs · 75,682 cycles
DURING SCHEDULED SPV, FOUND FLOORBEAMS CORRODED AT BS 1006, LBL 14 TO LBL 38, WL 208 AND BS 1016, LBL 3 TO LBL 8, WL 208. REPAIRED FLOORBEAMS PER ER.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,859 hrs · 75,681 cycles
DURING SCHEDULED SPV, FOUND FLOORBEAM CHORD CORRODED AT BS 986, RBL 38, WL 208. REPAIRED FLOORBEAM CHORD PER ER.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 68,863 hrs · 75,682 cycles
DURING SCHEDULED SPV, FOUND FLOORBEAM CRACKED AT BS 947, LBL 53, WL 208. REPAIRED FLOORBEAM PER ER.
Part: FRAME — CRACKED (FUSELAGE) · airframe 68,859 hrs · 75,681 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND CRACKS INDICATION AT BS 727 FRAME FASTENERS HOLES, STR 18A LT AND STR 18A RT. REPAIRED FRAME PER SRM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 68,834 hrs · 75,654 cycles
DURING SCHEDULED PM CHECK, FOUND BULKHEAD WEB CRACKED AT BS 727, LBL 13.5 AND LBL 14.5, 25 BELOW CEILING IN MAIN WHEEL WELL. REPAIRED WEB PER EA.
Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 68,672 hrs · 75,449 cycles
DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CORRODED AT BS 1016, RBL 1. REPAIRED WEB PER AD.
Part: WEB — CRACKED (FUSELAGE) · airframe 68,543 hrs · 75,289 cycles
DURING SCHEDULED PM CHECK, FOUND CRACK UNDER NOSE WHEELWELL BELOW RT SIDE FWD ACCESS PANEL AT BS 243. REPAIRED PER EA.
Earlier reports · 1997–2003 · 84 reports
2003
Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 68,200 hrs · 74,844 cycles
EEPLS COVERS BROKEN BETWEEN ROWS 4 AND 5. REPAIRED EEPLS PER MM
Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 68,095 hrs · 74,710 cycles
R2 DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.
Part: INDICATOR — OUT OF POSITION (SLIDE) · airframe 67,592 hrs · 74,054 cycles
AFT ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.
Part: SLIDE — OUT OF POSITION (AFT CABIN) · airframe 67,656 hrs · 74,136 cycles
DURING SCHEDULED PM CHECK, FOUND BOTH AFT DOOR EVAC SLIDES OUT OF POSITION. REPOSITIONED BOTH SLIDES PER MM.
Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 67,345 hrs · 73,743 cycles
FWD SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.
Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 66,078 hrs · 72,226 cycles
DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.
Part: INDICATOR — OUT OF POSITION (SERVICE DOOR) · airframe 67,171 hrs · 73,521 cycles
DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE PER MM.
Part: TRANSMISSION — FAULTY (TE FLAPS) · airframe 67,072 hrs · 73,395 cycles
T/E FLAPS WOULD NOT EXTEND PAST 15 DEGREES. REMOVED AND REPLACED NR 7, NR 5 AND NR 4 FLAP TRANSMISSIONS PER MM.
Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 67,017 hrs · 73,327 cycles
DURING SCHEDULED SERVICE CHECK, FOUND COCKPIT OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT ASSY PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 65,757 hrs · 71,741 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 1010 AT STR 4L & BETWEEN BS 354 TO BS 360 AT STR 4L. REPAIRED SKIN PER SRM.
Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 65,985 hrs · 72,041 cycles
DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.
2002
Part: CABLE — MISROUTED (AFT ENTRY DOOR) · airframe 65,299 hrs · 71,174 cycles
DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY CABLE MISROUTED. REROUTED CABLE PER MM.
Part: COVER — MISSING (CABIN) · airframe 65,299 hrs · 71,174 cycles
DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER MISSING IN AFT CABIN. INSTALLED COVER PER MM.
Part: CABLE — STIFF (NR 1 ENGINE) · airframe 64,926 hrs · 70,703 cycles
NR 1 ENGINE THRUST LEVER DIFFICULT TO MOVE. REMOVED AND REPLACED NR 1 ENG THROTTLE TELEFLEX CABLE PER MM.
Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 64,669 hrs · 70,388 cycles
DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 64,543 hrs · 70,229 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 341, ABOVE STR 22L. REPAIRED SKIN PER SWA EA.
Part: SPOILER — DELAMINATED (LT WING) · airframe 64,543 hrs · 70,229 cycles
DURING SCHEDULED 1/4D CHECK, FOUND NR 1 SPOILER DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED NR 1 SPOILER PER MM.
Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 64,543 hrs · 70,229 cycles
DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.
Part: LIGHT — OUT OF POSITION (CABIN) · airframe 64,058 hrs · 69,619 cycles
FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT ASSY FELL OUT. REINSTALLED LIGHT ASSY PER MM.
Part: CAP — MISSING (CABIN) · airframe 63,875 hrs · 69,387 cycles
DURING SCHEDULED C1 CHECK, FOUND EEPLS END CAP MISSING IN FWD CABIN. INSTALLED END CAP PER MM.
Part: SLIDE — OUT OF ADJUST (AFT ENTRY DOOR) · airframe 63,809 hrs · 69,305 cycles
AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.
Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 63,740 hrs · 69,211 cycles
DECLARED EMERGENCY, AIR TURNBACK. DURING CLIMB ALTITUDE HORN SOUNDED, CABIN CLIMBING 1000 FPM. STBY NO HELP, WORKED IN MANUAL. REMOVED AND REPLACED AFT OUTFLOW VALVE PER MM.
Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 63,635 hrs · 69,078 cycles
AFT CARGO DOOR CRACKED AT AFT UPPER CORNER OF HANDLE CUTOUT. REPAIRED DOOR PER SWA RA.
Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 63,214 hrs · 68,561 cycles
DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.
Part: SIGN — LOOSE (CABIN) · airframe 63,214 hrs · 68,561 cycles
DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT SIGN LOOSE ABOVE ROW 20. SECURED EXIT SIGN PER MM.
Part: BATTERY — DISCHARGED (CARGO BAY) · airframe 62,871 hrs · 68,148 cycles
DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT BATTERY PACK INOP IN FWD CARGO. REMOVED AND REPLACED BATTERY PACK PER MM.
2001
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 62,091 hrs · 67,265 cycles
ENGINE SHUT DOWN, DECLARED EMERGENCY, AIR TURNBACK. NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED AFTER T/O. REMOVED AND REPLACED OIL FILTER AND RAN ENGINE. CK'D FILTER, NO CONTAMINANTS FOUND. OPS CK GOOD PER MM.
Part: SLIDE — OUT OF ADJ (AFT ENTRY DOOR) · airframe 61,843 hrs · 66,992 cycles
DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE PER MM.
Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 61,843 hrs · 66,992 cycles
DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE PER MM.
Part: SPLICE — CRACKED (FUSELAGE) · airframe 61,797 hrs · 66,940 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND STR SPLICE CRACKED ( 2 EA ) AT BS 908, STR'S 4L & 4R. R&R STR SPLICE PER SRM.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 61,797 hrs · 66,940 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND FRAME SHEAR TIE CRACKED AT BS 360, STR 14L. R&R SHEAR TIE PER SRM.
Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 60,968 hrs · 65,871 cycles
DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.
Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 61,140 hrs · 66,177 cycles
DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 61,067 hrs · 66,095 cycles
DURING SCHEDULED A2 CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 920, STR 23L. REPAIRED SKIN PER SRM.
Part: CONNECTOR — LOOSE (EPR INDICATOR) · airframe 60,845 hrs · 65,853 cycles
ABORTED TAKEOFF AT 40 KNOTS, NR 2 ENG EPR INDICATOR INOP. CLEANED CONNECTOR AT EPR INDICATOR PER MM. OPS CHECK GOOD.
Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 60,838 hrs · 65,847 cycles
WHEN CLOSING AFT ENTRY DOOR, EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.
Part: BATTERY PACK — DISCHARGED (COCKPIT) · airframe 60,674 hrs · 65,664 cycles
DURING SCHEDULED SERVICE CHECK, FOUND COCKPIT OVERHEAD EMERGENCY EXIT LIGHT BATTERY CHARGE LOW. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 60,490 hrs · 65,448 cycles
FWD OTBD FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT AND BATTERIES PER MM.
Part: SKIN — CRACKED (RT WING) · airframe 60,407 hrs · 65,356 cycles
DURING SCHEDULED C4 CHECK, FOUND RT WING UPPER WING SKIN CRACKED AT STA 160, AFT SPAR. REPAIRED SKIN PER T1-257-014.
Part: BULB — INOPERATIVE (CABIN FLOOR) · airframe 60,407 hrs · 65,356 cycles
DURING SCHEDULED C4 CHECK, FOUND 1 RED EEPLS BULB INOP. RELAMPED EEPLS BULB PER MM.
Part: SLIDE — DISCHARGED (FWD ENTRY) · airframe 60,235 hrs · 65,165 cycles
DURING SCHEDULED A1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR LOW. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM.
2000
Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 60,106 hrs · 65,018 cycles
FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS LOW. R&R EVAC SLIDE ASSY PER MM.
Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 60,097 hrs · 65,008 cycles
DURING SCHEDULED SERVICE CHECK, FOUND BOTH REAR SLIDES GAUGES UNREADABLE. REPOSITIONED SLIDE ASSY'S PER MM.
Part: SLIDE — DISLODGED (AFT PAX DOOR) · airframe 59,888 hrs · 64,768 cycles
AFT ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. RE-INSTALLED SLIDE PER MM.
Part: SLIDE — DISLODGED (AFT PAX DOOR) · airframe 59,879 hrs · 64,761 cycles
AFT ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. RE-INSTALLED SLIDE ASSY PER MM.
Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 59,645 hrs · 64,492 cycles
DURING SCHEDULED C3 CHECK, FOUND AFT SVC AND ENTRY DOOR SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED SLIDE ASSEMBLIES PER MM.
Part: GIRT BAR — OUT OF ADJ (PAX DOOR SLIDE) · airframe 59,464 hrs · 64,301 cycles
AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 59,340 hrs · 64,173 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 940, STR 21L. REPAIRED SKIN PER SRM.
Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 59,101 hrs · 63,914 cycles
BOTH AFT CABIN DOOR EVACUATION SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED BOTH SLIDE ASSY''S PER MM.
Part: SLIDE — DEPLOYED (PAX DOOR) · airframe 58,819 hrs · 63,606 cycles
THIS IS AN AMENDED REPORT ORIGINALLY SUBMITTED 7-15-00, (OPERATOR CONTROL NUMBER SWAA00-1298). INADVERTENTLY DEPLOYED FWD ENTRY DOOR EVACUATION SLIDE. RESECURED SLIDE ASSY TO DOOR PER MM.
Part: SLIDE — DISLODGED (PAX DOOR) · airframe 58,819 hrs · 63,606 cycles
FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER INADVERTENTLY, (STILL ARMED WHEN DOOR OPENED). RE-INSTALLED SLIDE ASSY PER MM.
Part: O-RING — LEAKING (NR 2 ENGINE) · airframe 57,847 hrs · 62,546 cycles
DURING CRUISE, INFLIGHT ENGINE SHUT-DOWN, FLIGHT DIVERTED, NR 2 ENGINE LOW OIL PRESS LIGHT ILLUMINTED AND OIL PRESS INDICATOR INOPERATIVE. C/W NR 2 ENGINE WINDMILLING INSP, R&R MAIN OIL FILTER, R&R CASE SIDE OF BREATHER TUBE O-RING, SERVICE ENGINE WITH OIL AND R&R NR 2 ENGINE N2 INDICATOR PER MM. OPS CK GOOD.
Part: LENS — LOOSE (ESCAPE SLIDE) · airframe 57,847 hrs · 62,546 cycles
DURING SCHEDULED D CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE LIGHT LENS LOOSE. R&R DAMAGE LENS ATTACH NUTPLATE PER MM.
Part: FRAME — CRACKED (BS 294.5)
DURING SCHEDULED D CHECK, FOUND BS 294.5 LOWER STUB FRAME CRACKED, RBL 54, WL 209. REMOVED AND REPLACED STUB FRAME ASSY PER SRM.
Part: FLOORBEAM — CORRODED (BS 294)
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER SURFACE CORRODED, BS 294.5, BL 0 TO RBL 5. REPAIRED BEAM PER SRM.
Part: CLIP — CRACKED (BS 616)
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED, BS 616, STRINGER 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
1999
Part: WIRE — FAILED (GALLEY)
AIR TURNBACK, SMOKE SMELL IN AFT GALLEY. FOUND SHORT BETWEEN COFFEE MAKER POWER WIRE AND WORK LIGHT WIRE BEHIND AFT GALLEY. REPAIRED WIRING PER MM.
Part: LIGHT — INOP (COCKPIT)
DURING SCHEDULED SERVICE CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: SKIN — CRACKED (BS 857)
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED, BS 857, STRINGER 17R. REPAIRED SKIN PER SRM.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND FWD OVERHEAD EXIT LIGHT BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: SKIN — CRACKED (BS 927)
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED, BS 927, BETWEEN STRINGERS 21L-22L. REPAIRED SKIN PER SRM.
Part: STRAP — BROKEN (PAX DOOR LIGHT)
FWD EMERGENCY FLASHLIGHT SECURITY STRAP BROKEN. INSTALLED STRAP PER MM.
Part: STRINGER — CRACKED (BS 500)
DURING SCHEDULED SERVICE CHECK, FOUND THRU EDDY CURRENT INSPECTION .125 INCH LONG CRACK AT STRINGER 4R, BS 500D. REPAIRED PER SRM.
Part: WINDOW — NOT SECURED (AFT SVC DOOR)
DURING SCHEDULED C1 CHECK, FOUND EMERGENCY SLIDE WINDOW NOT SECURED. SECURED WINDOW PER MM.
Part: BRACKET — CRACKED (EMER EXIT DOOR)
DURING SCHEDULED C1 CHECK, FOUND RT OVERWING EXIT FWD SIDE CENTER DOOR CASTING ATTACH BRACKET CRACKED. REPLACED BRACKET PER SRM.
Part: BULB — FAILED (CABIN)
DURING SCHEDULED SC CHECK, FOUND FWD SEGMENT WHITE LIGHT OF FLOOR EMERGENCY EXIT LIGHTS INOP. RELAMPED PER BOEING M/M.
1998
Part: LIGHT — INOP (PAX DOOR)
DURING SCHEDULED A1 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT FWD ENTRY DOOR. REMOVED AND REPLACED LIGHT ASSEMBLY PER BOEING M/M.
Part: FIRE LOOP — MALFUNCTIONED (NR 2 ENGINE)
ON APPROACH, NR 2 ENGINE FIRE WARNING BELL AND HORN SOUNDED. PERFORMED ENGINE SHUTDOWN PROCEDURES AND ACTIVATED FIRE BOTTLES. MADE AN UNEVENTFUL LANDING. INSPECTED WITH NO EVIDENCE OF FIRE OR OVERHEAT CONDITION. REMOVED AND REPLACED LOWER FIRE LOOP. REMOVED AND REPLACED ENGINE AND APU FIRE DETECTION UNITS, AND BOTH FIRE BOTTLES. CLEANED AND REINSTALLED ALL LOOP DISCONNECTS TO UPPER AND LOWER DETECTORS. ALL RESISTANCE CHECKED WITHIN M/M LIMITS. ENGINE RUN CHECKED NORMAL.
Part: LINE — RUPTURED (A HYD SYST)
LOST A SYSTEM HYDRAULIC QUANTITY INBOUND INTO STL. MADE AN UNEVENTFUL LANDING. AIRCRAFT TOWED TO GATE. FOUND PRESSURE LINE LEAKING JUST I/B OF NR 2 ENGINE. REPLACED HYD PRESSURE LINE.
Part: CONNECTOR — SHORTED (NR 2 ENGINE)
INFLIGHT SHUTDOWN DUE TO NR 2 FIRE BLINKED A FEW TIMES WITH BELL, THEN STAYED ON. ALL OTHER INDICATIONS NORMAL. CHECK LIST WAS ACCOMPLISHED, BOTH BOTTLES FIRED, LIGHT REMAINED ILLUMINATED FOR REST OF FLIGHT. NOTHING NOTED ON INSTRUMENTS OR VISUALLY. SUSPECT FALSE FIRE WARNING. AIRCRAFT MADE AN UNEVENTFUL LANDING. FOUND CONECTOR D1098 SHORT TO GROUND. REMOVED AND REPLACED CONECTOR D1098 PER BOEING MM. REMOVED AND REPLACED 1 AND 2 FIRE BOTTLES PER BOEING MM. RAN ENG FOR 20 MINUTES, OP CK OK.
Part: LIGHT — DAMAGED (RT OVERWING)
DURING SCHEDULED SERVICE CHECK, FOUND LIGHT ASSY DAMAGED RT OVERWING DOOR EXIT LIGHT. REMOVED AND REPLACED RT OVERWING EXIT LIGHT ASSY PER BOEING MM.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SCHEDULED A2 CHECK, FOUND EMERGENCY LIGHTS INOPERATIVES IN CABIN. REMOVED AND REPLACED PER BOEING MM.
Part: ANGLE — CORRODED (BS 988)
DURING SCHEDULED 1/4 D CHECK, FOUND CORRODED Z ANGLE AT BS 988. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (BS 336)
DURING SCHEDULED 1/4 D CHECK, FOUND SKIN CRACKED AT BS 336, STR 17L, WITH EXTENSION APPROX 1/4 BEYOND FASTENER HOLE. REPAIRED PER BOEING SRM.
Part: HINGE — CRACKED (SERVICE DOOR)
DURING SCHEDULED 1/4 D CHECK, FOUND AFT SERVICE DOOR UPPER HINGE CUTOUT HAS .25 INCH CRACK AT TOP FWD CORNER. REPAIRED PER SWA RA NR 1-253-1852.
Part: ANGLE — CORRODED (BS 312)
DURING SCHEDULED .25D CHECK, FOUND CRACKED L ANGLE LT SIDE OF 3-2 RACK AT BS 312. REPAIRED PER BOEING MM.
Part: SKIN — CRACKED (BS 178)
DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED SKIN AT BS 178, LBL 5.5 WL 194. REPAIRED PER BOEING SRM.
Part: STRAP — DAMAGED (CARGO DOORWAY)
DURING 1/4 D-CHECK, FOUND STRAP ALONG WEBS AT AFT LOWER SIDE OF CARGO DOOR CUTOUT DAMAGED. REPAIRED PER BOEING SRM.
Part: WEB — DAMAGED (CARGO DOORWAY)
DURING SCHEDULED 1/4 D-CHECK, FOUND LOWER WEB AT FWD SIDE OF CARGO DOOR CUTOUT DAMAGED. REPAIRED PER BOEING SRM.
Part: INTERCOSTAL — CRACKED (BS 178)
DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED INTERCOSTAL BRACKET AT BS 178, RBL 26 WL 195. REMOVED AND REPLACED PER BOEING SRM.
Part: ANGLE — CRACKED (BS 292)
DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED ANGLE AT BS 292 BELOW 511R. REMOVED AND REPLACED PER BOEING SRM.
Part: BULKHEAD — CRACKED (NLG WW)
DURING SCHEDULED RON CHECK, FOUND CRACKED NLG WHEEL WELL CEILING PRESSURE BULKHEAD LOCATED AT FWD RT ACCESS PANEL AT AFT I/B CORNER. REPAIRED PER BOEING TI-A53-001.
Part: SKIN — CRACKED (BS 980)
DURING SCHEDULED RON CHECK, FOUND CRACK IN LT AFT FUSELAGE SKIN AT BS 980, STR 24. REPAIRED PER BOEING SRM.
1997
Part: LIGHT — INOPERATIVE (CABIN)
DURING SCHEDULED CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSEMBLY PER BOEING M/M.