N938AS
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.
54 reports on file, 1995-02-17 – 2000-08-03.
Part: ACTUATOR — BURNED (SPOILER) · airframe 42,249 hrs · 26,318 cycles
BOTH CREW MEMBERS NOTICED A STRONG ELECTRICAL ODOR IN THE COCKPIT DURING CLIMB OUT OF TPA. CREW WAS UNABLE TO ISOLATE THE SOURCE AND THE AIRCRAFT WAS RETURNED TO TPA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AUTO SPOILER ACTUATOR IN FORWARD PEDESTAL AT FAULT. THE AUTO SPOILER ACTUATOR WAS REMOVED AND REPLACED IAW MM 27-62-05, PAGE 201-205.
Part: FRAME — WORN (FUSELAGE) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND A HOLE WORN THROUGH FRAME WEB AT STA 1380, LONGERON 4L. THE FRAME WAS REPAIRED IAW SRM 53-01, FIGURE 4.
Part: PAN — CORRODED (E/E DOOR) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND E&E DOOR PAN CORRODED BETWEEN THE PAN AND THE E&E DOOR SWITCH AT STA 143, RBL 28. THE CORROSION WAS REMOVED IAW SRM 51-10-03. THE SWITCH BRACKET AND FITTINGS WERE REMOVED IAW SRM 51-30-01 AND 51-30-05. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-30-02. THE SWITCH BRACKET AND FITTINGS WERE INSTALLED IAW SRM 51-30-01 AND 51-30-05.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND LEFT O/B CABIN SEAT TRACK GOUGED AT STA 1245, LBL 54.5. THE SEAT TRACK SECTION WAS REMOVED AND REPLACED IAW SRM 51-10-03.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,266 hrs
INSPECTION FOUND AFT PRESSURE BULKHEAD SIDE LOWER JACK PAD SUPPORT ANGLE CORRODED AT STA 1138, LONGERON 29R. THE JACK PAD HAT ANGLE JACK SUPPORT, STIFFENERS, AND LONGERON FITTINGS WERE REMOVED AND NEW PARTS WERE INSTALLED IAW SRM 51-30-05, 51-30-02.
Part: WEB — CORRODED (FUSELAGE) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND LT O/B CUSP WEB CORRODED AT FS 1250, LBL 60. THE CORRODED AREAS WERE REMOVED IAW SRM 53-01, FIGURE 4. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-01, FIGURE 4 AND 53-10-03.
Part: FITTING — CORRODED (FUSELAGE) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND FLOOR FITTING JUST I/B OF AFT CORNER OF R-1 DOOR, FS 208, RBL 48 CORRODED. THE FLOOR FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-01, 51-10-03, 51-10-04, AND 51-30-02.
Part: STRAP — CORRODED (FUSELAGE) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND AFT CARGO DOOR LOWER JAMB REPAIR STRAP CORRODED AT FS 1193 - 1212, LONGERON 27R. THE REPAIR STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-4, 51-30-05, AND ECRA 5310-03027.
Part: STRAP — CRACKED (PAX DOOR) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND A 1.3 INCH CRACK IN LOWER FORWARD CORNER L-1 DOOR TIE STRAP. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-30-02.
Part: FITTING — CRACKED (FUSELAGE) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND A 2 INCH CRACK IN FLOOR FITTING AND INTERCOSTAL CORRODED IN FORWARD PIT AT STA 427, L29R. THE FITTING AND INTERCOSTAL WERE REMOVED IAW SRM 51-30-01 AND 51-20-01. A NEW INTERCOSTAL AND FITTING WERE INSTALLED IAW SRM 51-30-02, 51-10-03, AND 51-30-05.
Part: PAN — CORRODED (PAX DOOR) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND E & E DOOR PAN CORRODED AROUND AND BETWEEN FWD AND AFT DOOR LOCK FITTINGS AT STA 138 & 148, RBL 28. THE DOOR PAN WAS REPAIRED IAW ECRA 5310-03995.
Part: PAN — CRACKED (CARGO DOOR) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND AFT CARGO DOOR FORWARD END INNER PAN CRACKED BY CARGO DOOR LATCHES. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-04, 51-30-05, 51-10-03, AND 52-05, FIGURE 26A.
Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND LEFT AFT EMERGENCY EXIT DOOR LOWER AFT CORNER SUPPORT ANGLE CRACKED AROUND FASTENER HOLES AND SURFACE CORROSION WAS PRESENT. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-10 AND 51-70-04.
Part: FITTING — CRACKED (CARGO DOOR) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND MID PIT DOOR INTERIOR FITTING JUST AFT OF FORWARD HINGE CRACKED. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-01, 51-10-04, AND 51-30-12.
Part: WEB — CRACKED (FUSELAGE) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND A 3 INCH CRACK AT FASTENER HOLE OF LT O/B CUSP WEB NEAR SEAT TRACK SPLICE FOR LT O/B SEAT TRACK, FS 1220. THE CRACKED AREA OF CUSP WEB WAS REMOVED IAW SRM 53-01. DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-01, 51-10-03, AND 53-01-04.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND LEFT I/B CABIN SEAT TRACK CORRODED FROM STA 1155 - 1212. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK AND SPLICE WERE INSTALLED IAW SRM 51-30-05 AND 51-30-01.
Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND EXTERNAL FUSELAGE SUPPORT BRACKET CRACKED AT STA 798, LONGERON 20R. THE BRACKET WAS REMOVED AND REPAIR WAS INSTALLED IAW SRM 51-30-01, 51-10-04, 51-10-03, AND 51-30-05.
Part: PAN — CRACKED (CARGO DOOR) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND AFT CARGO DOOR AFT END INNER PAN CRACKED AT CARGO DOOR LATCH. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-04, 51-10-03, 51-30-05, AND 52-05, FIGURE 26A.
Part: SKIN — DENTED (CARGO DOOR) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND AFT CARGO DOOR SKIN DENTED. THE DOOR SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 38 AND 51-30-01.
Part: FRAME — CORRODED (FUSELAGE) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND LONGERON FORMER CORRODED IN AFT CARGO BAY AT STA 1041, LONGERON 29L-30. THE LONGERON FORMER WAS REMOVED AND A NEW LONGERON FORMER WAS INSTALLED IAW SRM 51-30-05 AND 51-10-03.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND AFT CARGO BAY LT UPPER AND LOWER GILL LINER SUPPORT FRAMES CRACKED AT STA 1212. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-30-02 AND 51-30-05.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND SHEAR TIE CORRODED IN AFT CARGO BAY AT STA 1231, LONGERON 29L-30. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-30-02.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND RT O/B CABIN SEAT TRACK CORRODED FROM STA 220 - 237. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-02, 51-10-04, 51-10-03, AND 51-30-05.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 146 - 200 JUST LEFT OF CENTERLINE. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-01, 51-10-01, AND 51-10-03.
Part: FLANGE — DAMAGED (CARGO DOOR) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND AFT CARGO DOOR FORWARD AFT LOWER AND UPPER FLANGES DAMAGED AT STOP POSITION. DOUBLERS WERE INSTALLED IAW SRM 51-30-01, 51-30-02, 51-10-03, AND ECRA 5330-02819.
Part: SKIN — DENTED (CARGO DOOR) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND THREE SHARP DENTS IN MID CARGO DOOR OUTER SKIN. THE DENTED AREA WAS REPAIRED BY INSTALLING DOUBLERS IAW SRM 53-04, FIGURE 38.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND RT SIDE FLOOR SUPPORT CORRODED AT STA 180 - 200. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-01, FIGURE 1, 51-10-03, 51-30-02, AND 51-30-05.
Part: FLOOR SUPPORT — BROKEN (FUSELAGE) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND SUB FLOOR MEMBRANE BROKEN AT FS 196, LBL 44 JUST FORWARD OF LT O/B SEAT TRACK. THE SUB FLOOR MEMBRANE WAS REPAIRED IAW SRM 53-01, FIGURE 4 AND 51-30-02.
Part: ANGLE — CRACKED (CARGO BAY) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND LT GILL LINER SUPPORT FRAME CRACKED IN AFT CARGO BAY AT STA 1271. THE SUPPORT ANGLE WAS REMOVED, REPAIRED, AND INSTALLED IAW SRM 51-30-02, 51-10-04, AND 51-30-05.
Part: SKIN — BENT (CARGO DOOR) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND AFT CARGO DOOR SKIN AROUND HANDLE BENT AND CHAFED. THE DAMAGED AREA WAS CUT OUT IAW SRM 52-05, FIGURE 3. REPAIR DOUBLERS, FILLER, AND SHIMS WERE INSTALLED IAW SRM 52-05.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 41,266 hrs · 25,815 cycles
INSPECTION FOUND RT GILL LINER SUPPORT FRAME CRACKED IN AFT CARGO BAY AT STA 1136. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-02, 51-10-04, AND 51-30-05.
Part: STOP — WORN (CARGO DOOR)
INSPECTION FOUND MID CARGO DOOR FORWARD AND AFT LOWER FLANGE AND STOP PADS WORN. THE AREAS WERE REPAIRED USING A DOUBLER IAW ECRA 5330-02819 AND SRM 51-10-03.
Part: FRAME — CRACKED (BS 1041)
INSPECTION FOUND A 3 CRACK IN AFT CARGO BAY RT GILL LINER SUPPORT FRAME AT STA 1041, RBL24. THE ANGLE SUPPORT WAS REMOVED AND A NEW ANGLE SUPPORT WAS INSTALLED IAW SRM 51-30-05 AND 51-10-04.
Part: SUPPORT — CORRODED (BS 1117 - 1155)
INSPECTION FOUND UPPER AND LOWER SURFACES OF FLOOR SUPPORT ANGLE CORRODED IN AFT CARGO BAY AT STA 1117-1155. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-01, 51-10-04, AND 51-10-03.
Part: STOP — WORN (CARGO DOOR)
INSPECTION FOUND FORWARD CARGO DOOR FORWARD AND AFT LOWER FLANGE AND STOP PADS WORN. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02819.
Part: ANGLE — CHAFED (RT MLG DOOR)
INSPECTION FOUND RT MLG DOOR AFT LOWER INNER CORNER REPAIR ANGLE DEEPLY CHAFED. AN INNER CORNER DOUBLER REPAIR WAS INSTALLED IAW SRM 52-05, FIGURE 28, 51-10-04, AND 51-10-03.
Part: INTERCOSTAL — CORRODED (BS 1136 - 1155)
INSPECTION FOUND INTERCOSTAL CORRODED IN AFT CARGO BAY AT STA 1136-1155, LONGERON 29L. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.
Part: BRACKET — CRACKED (BS 864)
INSPECTION FOUND LT FORWARD EMERGENCY EXIT DOOR BINDING DUE TO A CRACKED FORWARD SIDE LT BRACKET. THE CRACK WAS 1.5 INCH LONG AND THE BRACKET WAS LOCATED AT FS 864, LONGERON 13L. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-08 AND 51-10-03.
Earlier reports · 1995–1999 · 16 reports
1999
Part: STRUT — DEFLATED (NLG)
THE NOSE GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION DEPARTING DEN AND THE AIRCRAFT WOULD NOT PRESSURIZE UNTIL PULLING THE RIGHT GROUND CONTROL RELAY. THE ABNORMAL CHECKLIST WAS COMPLETED AND THE NOSE GEAR LIGHT EXTINGUISHED. THE AIRCRAFT WAS RETURNED TO DEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE STRUT UNDER INFLATED. A COMPLETE NOSE STRUT SERVICING WITH FLUID AND NITROGEN WAS PERFORMED. THE GEAR WAS RETRACTED IAW MM 32-30-09 AND GROUND CHECK WAS NORMAL.
1998
Part: OVEN — FAILED (GALLEY)
AN ELECTRICAL BURNING ODOR WAS NOTICED IN THE FORWARD CABIN AREA WHILE EN ROUTE TO ATL. NO VISIBLE SMIKE WAS PRESENT. THE AIRCRAFT LANDED AT ATL WITHOUT INCIDENT. MAINTENANCE FOUND THE FORWARD GALLEY NR 2 OVEN HAD A BURNED MOTOR. THE OVEN WAS PLACARDED INOPERATIVE.
Part: VALVE — LEAKING (RT ANTISKID)
THE RT HYDRAULIC SYSTEM QUANTITY DECREASED DURING CLIMBOUT. QRH PROCEDURES WERE FOLLOWED FOR HYDRAULIC QUANTITY LOSS AND ALTERNATE GEAR EXTENSION WAS USED FOR RETURN TO MCO WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT INBOARD ANTI-SKID DUAL CONTROL VALVE LEAKING. THE ANTI-SKID DUAL CONTROL VALVE WAS REMOVED AND REPLACED IAW MM 32-43-03, PAGE 202A. LEAK AND OPERATIONAL CHECKS WERE GOOD.
Part: PROX SENSOR — INOPERATIVE (NLG)
THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND THE RED LIGHT EXTINGUISHED. THE FLIGHT WAS CONTINUED TO ORD WHERE IT LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE FOUND THE NLG UPLOCK PROXIMITY SENSOR AT FAULT. THE SENSOR WAS REPLACED AND RESHIMMED. THE NOSE GEAR WAS SWUNG WITH OPERATION AND INDICATIONS CHECKING GOOD.
Part: BEAM — CORRODED (BAGGAGE COMPT)
INSPECTION FOUND MID BAGGAGE BIN Z-ANGLE BEAM CORRODED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 63.
Part: DOUBLER — CORRODED (NR 2 RADIO ALT)
INSPECTION FOUND NR 2 RADIO ALT RECEIVER ANTENNA RETAINING DOUBLER CORRODED. THE RETAINING DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-00 AND 51-30-2.
1997
Part: COMPRESSOR — DAMAGED (NR 1 ENGINE)
THE AIRCRAFT WAS DIVERTED TO DEN WITH THE NR 1 ENGINE SHUTDOWN WHILE EN ROUTE. THE AIRCRAFT LANDED IN DEN WITHOUT INCIDENT. AN ENGINE CHANGE IS IN PROGRESS. *S/D* INVESTIGATION REVEALED THAT THE ENGINE FAILURE WAS CAUSED BY INGESTION OF BLUE ICE ORIGINATING FROM THE FORWARD LAVATORY SERVICING PORT. SHOP FINDINGS REVEALED TRACES OF BLUE FLUID ON THE FRONT ACCESSORY DRIVE COVER. ALL FAN BLADES WERE DAMAGED AND ONE WAS BROKEN OFF ABOUT ONE-THIRD LENGTH FROM THE BASE. ADDITIONAL DAMAGE WAS FOUND ON ALL STAGES OF THE LOW PRESSURE COMPRESSOR AND 7TH STAGE OF THE HIGH PRESSURE COMPRESSOR.
1996
Part: EVAC SLIDE — BROKEN (R1 DOOR)
SEA - PRIOR TO DEPARTURE OF FLIGHT 598 - CREW REPORTED THE R1 DOOR EMERGENCY EVACUATION SLIDE DEPLOY LANYARD WAS BROKEN AND DETACHED. REPLACED THE EMERGENCY EVACUATION SLIDE. (M)
Part: BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 13 THROUGH 18 WERE FOUND INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY AND LIGHT OPERATED NORMALLY. (M)
Part: COALESCERS — CONTAM CHECK (CABIN)
LAS - FLT NR 9000, AIRCRAFT WAS RELEASED FOR MAINTENANCE FERRY FLIGHT TO SEA (REF MRR ASAA9680080). AFTER TAKEOFF, BOTH PILOTS DETECTED AND ODOR IN THE COCKPIT WHICH MAINTENANCE TECH FOREMAN OCCUPYING THE OBSERVERS SEAT ATTRIBUTED TO A HOT DUCT ODOR. AIRCRAFT RETURNED TO LAS AND THE AIR CONDITIONING PACKS WERE INSPECTED FOR HYDRAULIC AND PNEUMATIC LEAKS, NO LEAKS WERE FOUND. ODOR DIMINISHED AFTER EXTENDED PACK OPERATIONS. REPLACED BOTH COALESCERS AND RELEASED AIRCRAFT. NO ODORS WERE DETECTED DURING FERRY FLIGHT TO SEA. (M)
Part: TR RETURN LINE — LEAKING (LT ENGINE)
LAS - FLT NR 624 - CREW REPORTED AN ELECTRICAL OR HOT PLASTIC ODOR IN THE CABIN DURING DESCENT AND LANDING. INSPECTION OF ALL LAVATORY WASTE CONTAINERS, OVENS, BUN WARMERS AND COFFEE MAKERS REVEALED NO PLASTIC RESIDUE OR OVERHEAT CONDITION, ODOR HAS DISSIPATED. HOWEVER, DURING BOARDING OF OUTBOUND FLIGHT 651, THE ODOR RETURNED WITH THE AIR CONDITIONING PACKS OPERATING. FOUND THE LEFT THRUST REVERSER RETURN LINE LEAKING SKYDROL. TIGHTENED THE 'B' NUT AND SYSTEM LEAK CHECKED GOOD. CLEANED TAIL COMPARTMENT AREA, PERFORMED HIGH PRESSURE BURNOUT OF HIGH PRESSURE DUCTING AND REPLACED BOTH COALESCERS. SYSTEM OPERATED NORMALLY WITH NO ODORS DETECTED. (M)
Part: COALESCERS — DIRTY (CABIN)
LAS - FLT NR 624 - CREW REPORTED AN ELECTRICAL OR HOT PLASTIC ODOR IN THE CABIN DURING DESCENT AND LANDING. INSPECTION OF ALL LAVATORY WASTE CONTAINERS, OVENS, BUN WARMERS AND COFFEE MAKERS REVEALED NO PLASTIC RESIDUE OR OVERHEAT CONDITION, ODOR HAS DISSIPATED. HOWEVER, DURING BOARDING OF OUTBOUND FLIGHT 651, THE ODOR RETURNED WITH THE AIR CONDITIONING PACKS OPERATING. FOUND THE LEFT THRUST REVERSER RETURN LINE LEAKING SKYDROL. TIGHTENED THE 'B' NUT AND SYSTEM LEAK CHECKED GOOD. CLEANED TAIL COMPARTMENT AREA, PERFORMED HIGH PRESSURE BURNOUT OF HIGH PRESSURE DUCTING AND REPLACED BOTH COALESCERS. SYSTEM OPERATED NORMALLY WITH NO ODORS DETECTED. REFERENCE ASAA9680080.
Part: FRAME — CORRODED (BS 1271)
OAK - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME AT Y1271, X PLUS 20 TO X-15, Z-50. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-0 SRM 51-10-03, 51-30-02, 53-01 AND 53-03. (M)
1995
Part: EEL — INOPERATIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT NEON LAMP WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)
Part: EEL WIRING — DISCONNECTED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 1 TO 3 WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (W)
Part: TURBINE — FAILED (NR 1 ENGINE)
OAK - FLT 439 - CREW REPORTED NR 1 ENGINE FAILED AFTER TAKEOFF, NR 1 ENGINE SHUTDOWN AND LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE DUE TO TURBINE FAILURE. VENDOR TEARDOWN REVEALED 8TH STAGE STATOR SUPPORT FLANGE FAILED. (W)