N936AS
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.
58 reports on file, 1995-05-01 – 2000-02-02.
Part: SKIN — CRACKED (RT WING)
INSPECTION FOUND A 2 INCH CRACK IN RT WING FIXED LEADING EDGE SKIN AT SLAT TRACK NR 8 CUTOUT. THE SKIN WAS REPAIRED IAW ECRA 5721-01049.
Part: RIB — CRACKED (TE FLAP)
INSPECTION FOUND LT WING O/B NR 1 FLAP L/E INTERIOR RIB CRACKED AT FASTENER HOLES. THE RIB WAS REMOVED AND A NEW RIB WAS INSTALLED IAW SRM 57-50-14 AND 51-30-02.
Part: FLOORBEAM — CRACKED (BS 1098)
INSPECTION FOUND FLOOR SUPPORT CRACKED AT FS 1098, L24L, IN AFT CARGO PIT. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-70-01 AND 51-30-02.
Part: ANGLE — CRACKED (APU SHROUD)
INSPECTION FOUND A 3 INCH CRACK IN APU SHROUD CUTOUT AREA FORWARD RIGHT SUPPORT ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-04, AND 51-10-03.
Part: FRAME — CRACKED (BS 1418)
INSPECTION FOUND A 2 INCH CRACK IN TAIL COMPARTMENT FRAME JUST ABOVE THE WATER SEPARATORS AT STA 1418, LONGERON 2R. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-04, 53-01, FIGURE 2, AND 51-30-05.
Part: BRACKET — CRACKED (BS 875)
INSPECTION FOUND A 1.5 CRACK IN LOWER FUSELAGE LT FILLET PANEL SUPPORT BRACKET AT FS 875, S19L. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-05.
Part: ANGLE — CRACKED (CARGO DOOR)
INSPECTION FOUND ANGLE CRACKED AT FORWARD CARGO DOOR UPPER SIDE JUST FORWARD OF AFT HINGE. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-02.
Part: INTERCOSTAL — CRACKED (BS 769 - 807)
INSPECTION FOUND INTERCOSTAL CRACKED IN CABIN UNDER CENTER FLOORBOARD AT FS 769-807. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-05 AND 51-30-02.
Part: ANGLE — CRACKED (BS 1309)
INSPECTION FOUND FORWARD FACE OF LAV BULKHEAD FRAME TO FUSELAGE ATTACH ANGLE CRACKED AT STA 1309. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 29.
Part: SEAT TRACK — CORRODED (BS 1155)
INSPECTION FOUND LT O/B SEAT TRACK CORRODED AT STA 1155. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION OF TRACK WAS INSTALLED IAW SRM 51-30-2, 53-05, FIGURE 4F, 51-10-4, 51-10-3, AND 51-30-05.
Part: BULKHEAD — CRACKED (BS 1309)
INSPECTION FOUND A CRACK IN BULKHEAD AT STA 1309 BETWEEN LONGERONS 15R AND 16R. THE CRACK WAS STOP DRILLED IAW SRM 53-14-03, FIGURE3 AND A REPAIR WAS INSTALLED IAW SRM 51-10-04, 51-10-03, AND 51-30-05.
Part: FRAME — CORRODED (BS 1401)
INSPECTION FOUND FRAME IN TAIL COMPARTMENT CORRODED AT FS 1401, S21R. THE FRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW SRM 51-30-21 AND 51-30-05.
Part: ANGLE — CORRODED (CABIN)
INSPECTION FOUND LOWER AND TOP SURFACES OF ATTACH ANGLE CORRODED AND GOUGED AT FORWARD ENTRY DOOR JAMB LOWER THRESHOLD. THE ATTACH ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 53-11-1, AND 51-30-5.
Part: SEAT TRACK — CORRODED (BS 200 - 237)
INSPECTION FOUND RT I/B SEAT TRACK CORRODED FROM STA 200-237. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-5.
Part: ANGLE — CORRODED (CABIN)
INSPECTION FOUND THE R-1 DOOR SLIDE ATTACH ANGLE CORRODED. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3.
Part: SEAT TRACK — CORRODED (BS 1079 - 1193)
INSPECTION FOUND LT I/B SEAT TRACK CORRODED AT STA 1079-1193. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-5 AND 51-10-4.
Part: SKIN — CRACKED (BS 946)
INSPECTION FOUND A .5 INCH CRACK IN BOTH THE LT AND RT MLG DOOR CUTOUTS AT STA 946, LBL 8 AND RBL 8, RESPECTIVELY. THE CRACKED AREAS WERE REMOVED AND ANGLE REPAIRS WERE INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-2, 51-80-5, 53-14-0, FIGURE 2, 51-10-3, AND 51-30-09.
Part: WEB — CORRODED (BS 1140)
INSPECTION FOUND FLOOR WEB CORRODED INSIDE CABIN ATSTA 1140 JUST INSIDE L-2 DOOR. THE CORROSION WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2 AND 51-10-3.
Earlier reports · 1995–1998 · 40 reports
1998
Part: LINK — BROKEN (RT MLG UPLOCK)
THE RT MLG LIGHT AND GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION LEAVING MIA. THE AIRCRAFT WAS DIVERTED TO MCO WHERE IT LANDED SAFELY. MAINTENANCE FOUND THE RT MLG UP ACTUATOR LOWER LINK BROKEN. THE LINK WAS REMOVED AND REPLACED IAW MM 32-10-00. A GEAR SWING WAS PERFORMED IAW MM 07-11-00 AND OPERATION CHECKED GOOD.
Part: AIR DISTRIBUTION — SMOKE (CABIN)
THE FLIGHT ATTENDANTS REPORTED HAZE IN CABIN WHILE ON DESCENT. BOTH PACKS WERE RUN ON AIR CART WITH CABIN AND PACKS CHECKING GOOD. THE APU WAS RUN ALL NIGHT WITH PACKS ON. NO SMOKE IN CABIN OR LEAKS AT APU WERE NOTED.
Part: CABLE — DAMAGED (TAIL CONE)
INSPECTION FOUND TAILCONE RELEASE CABLE KINKED AT TOP LEFT PULLEY. THE CABLE WAS REMOVED AND REPLACED AND RIGGED IAW MM 53-53-00.
Part: BRACKET — CRACKED (CARGO COMPT)
INSPECTION FOUND BRACKET ANGLE CRACKED IN MID BAG BIN ABOVE LT OUTBOARD FORWARD CORNER OF FUEL TANK. A NEW BRACKET WAS INSTALLED IAW SRM 51-30-5.
Part: CABLES — OUT OF ADJUST (TAIL CONE)
PULL FROM THE TAIL CONE INTERIOR RELEASE HANDLE WAS EXCESSIVE AT 40 POUNDS. THE LATCH CABLES WERE RIGGED IAW MM 53-53-00.
Part: JAMB — CORRODED (CARGO DOOR)
INSPECTION FOUND Z-ANGLE BEAM REPAIR STRAP CORRODED AT AFT CARGO BIN LOWER DOOR JAMB. THE REPAIR STRAP WAS REPLACED IAW SRM 53-05, FIGURE 63.
1997
Part: BATTERIES — DISCHARGED (CABIN)
INSPECTION FOUND EMERGENCY OVERHEAD LIGHTS AT L-1 AND R-1 DOORS INOPERATIVE. THE POWER SUPPLY BATTERIES WERE REPLACED AND OPERATION CHECKED GOOD.
1996
Part: BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M)
Part: BATTERIES — DISCHARGED (CABIN)
SFO - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHT IN THE FORWARD CABIN WERE FOUND DIM. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M)
Part: LIGHT — DEFECTIVE (CABIN)
PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND DIM. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (X)
Part: DOOR MECHANISM — OUT OF ADJUST (L1 DOOR)
SEA - FLT 191 - PRIOR TO DEPARTURE, CREW REPORTED THE L1 DOOR HANDLE WOULD NOT REMAIN IN THE LOCKED POSITION AND THE DOOR WARNING LIGHT WOULD NOT EXTINGUISH. RERIGGED THE L1 DOOR MECHANISM PER MM AND OPERATED NORMALLY. (X)
Part: DOWNLOCK SENSOR — DEFECTIVE (NLG)
SEA - FLT 467 - CREW REPORTED THE NOSE LANDING GEAR LIGHT REMAINED ILLUMINATED AFTER TAKEOFF OAK. FOLLOWED ABNORMAL GEAR INDICATION CHECKLIST, RECYCLED LANDING GEAR AND INDICATION SYSTEM OPERATED NORMALLY. LANDED IN SEA WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR UP/DOWNLOCK SENSOR AND CONNECTOR, ADJUSTED UPLOCK SENSOR AND THE NOSE LANDING GEAR INDICATION SYSTEM OPERATED NORMALLY DURING GEAR RETRACTION. (M)
Part: FLOOR COVERING — EXCESS MATERIAL (FWD GALLEY)
SEA - FLT 511 - AFTER ARRIVAL, CREW REPORTED R1 DOOR HANDLE WAS DIFFICULT TO MOVE. FOUND GIRT BAR FITTING CONTACTING BOTTOM OF DOOR. REMOVED PORTION OF FORWARD GALLEY FLOOR COVERING MATERIAL, REINSTALLED GIRT BAR, AND RESEALED FLOOR. DOOR AND GIRT BAR OPERATE NORMALLY. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 2 TO 6 WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (M)
Part: MECHANISM — OUT OF ADJUST (L1 DOOR)
SEA - PRIOR TO DEPARTURE OF FLIGHT 370, CREW REPORTED THE L1 DOOR WOULD NOT CLOSE AND LOCK NORMALLY. ADJUSTED DOOR MECHANISM PER MAINTENANCE MANUAL AND OPERATED NORMALLY. (M)
Part: SEAL — RUBBING (R1 DOOR)
SEA - DURING MAINTENANCE CHECK, THE R1 DOOR WAS FOUND DIFFICULT TO OPEN. REMOVED EXCESS INTERIOR TRIM SEAL FROM FORWARD UPPER CORNER OF FRAME AND OPERATED NORMALLY. (M)
Part: DOOR — OUT OF ADJUST (L1)
SEA - DURING MAINTENANCE CHECK, THE L1 DOOR GUST LOCK WAS FOUND INOPERATIVE. RERIGGED DOOR PER MAINTENANCE MANUAL AND OPERATED NORMALLY. (M)
Part: DOOR FRAME — CORRODED (CARGO COMPT)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT DOOR FRAME PAN AT Y370 TO Y427, X-15 TO X-18, Z-18. REPLACED DOOR FRAME PAN IAW DC-9 SRM 51-30-02, AND 53-05. (M)
Part: LONGERON — CORRODED (BS 1245-1271)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 30 FROM Y1245 TO Y1271, X-0, Z-50. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, 51-30-02, 53-14-03 AND 53-02. (M)
Part: CUSP — CORRODED (BS 200)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON CUSP AT Y200, X-56, Z-0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, 51-30-03, 51-30-05 AND 53-05. (M)
Part: INTERCOSTAL — CORRODED (BS 1307-1322)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON INTERCOSTAL FROM Y1307 TO Y1322. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-30-02 AND 51-30-05. (M)
Part: LONGERON — CORRODED (BS 1117-1136)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 29R FROM Y1117 TO Y1136. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW ASA EA 5310-01396. (M)
Part: FRAME — CORRODED (BS 1271)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME AT Y1271, Z-50, LONGERON 26L TO 27R. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, 51-30-02 AND 53-03. (M)
Part: LONGERON — CORRODED (BS 769-788)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 30L AT Y769 TO Y788. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-30-05. (M)
Part: SUPPORT — CRACKED (BS 1287-1307)
PAE - DURING 30K CHECK, CRACK WAS FOUND ON FLOOR SUPPORT AT Y1287 TO Y1307, X0, Z0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, 51-30-02 AND 53-14-03. (M)
Part: SPLICE — CORRODED (BS 598)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 28L SPLICE AT Y598. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-30-05 AND 53-01. (M)
Part: SEAT TRACK — CORRODED (BS 232-239)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON SEAT TRACK AT Y232 TO Y239, X MINUS 44, Z0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 53-05. (M)
Part: SUPPORT — CORRODED (BS 169-174)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FLOOR SUPPORT AT Y169 TO Y174, X MINUS 52, Z PLUS 1. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-30-02, 53-10-01 AND 53-01. (M)
Part: SEAT TRACK — CORRODED (BS 1174)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON SEAT TRACK AT Y1174, X PLUS 22, Z0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-30-01 AND 53-05. (M)
Part: LONGERON — CORRODED (BS 210-236)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 29L AT Y210 TO Y236. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC9-SRM 51-10-03, 51-30-02 AND 53-14-01. (M)
Part: THRESHOLD — CORRODED (CARGO COMPT)
PAE - DURING 30K CHECK, FOUND CORROSION WAS FOUND ON THE UPPER SURFACE OF THE LOWER FLANGE ON THE AFT CARGO COMPARTMENT DOOR THRESHOLD BEAM AT Y1155, LONGERON 28R. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM AND ASA EA 5310-01395. (M)
Part: SUPPORT — CORRODED (BS 200)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FLOOR BOARD SUPPORT AT Y200, X PLUS 56, Z0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 53-10-01. (M)
Part: SKIN — CORRODED (BS 712-731)
PAE - DURING 30K CHECK, FOUND CORROSION ON THE FUSELAGE SKIN AND INTERNAL DOUBLER AT Y712 TO Y731, LONGERON 28L TO 28R. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM AND ASA EA 5330-01223. (M)
Part: HAT CHANNEL — CORRODED (BS 1129/1138)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON HAT CHANNEL AT Y1129 AND Y1138, X PLUS 3, Z0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, 53-14-03 AND 53-01. (M)
Part: SEAT TRACK — CORRODED (BS 239)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON SEAT TRACK AT Y239, X-22, Z0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03 AND 53-05. (M)
Part: SUPPORT — CORRODED (FS 200-220)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FLOOR BOARD SUPPORT AT Y200 TO Y220, X PLUS 15, Z0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 53-10-01. (M)
1995
Part: MECHANISM — BINDING (L1 DOOR)
SEA - FLT 530 - PRIOR TO DEPARTURE, CREW REPORTED THE L1 DOOR WOULD NOT LOCK CLOSED. FREED AND LUBRICATED THE INTERLOCK MECHANISM AND DOOR OPERATED NORMALLY. (W)
Part: EEL BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 24 TO 27 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M)
Part: STRUT — LOW PRESS (NLG)
SEA - ON ARRIVAL OF FLT 443, CREW REPORTED THE LANDING GEAR HANDLE WOULD NOT GO TO RETRACT POSITION. HAD TO PUSH INTERLOCK BUTTON TO RAISE HANDLE. FOUND NOSE LANDING GEAR STRUT PRESSURE LOW AND TORQUE LINK APEX BOLT OVER TORQUED. SERVICED NOSE LANDING GEAR STRUT TO PROPER DIMENSION AND RETORQUED APEX BOLT. ACCOMPLISHED GEAR SWING AND OPERATED NORMALLY. REFERENCE ASAA9580108.
Part: TORQUE LINK BOLT — OVER TORQUED (NLG)
SEA - ON ARRIVAL OF FLT 443, CREW REPORTED THE LANDING GEAR HANDLE WOULD NOT GO TO RETRACT POSITION. HAD TO PUSH INTERLOCK BUTTON TO RAISE HANDLE. FOUND NOSE LANDING GEAR STRUT PRESSURE LOW AND TORQUE LINK APEX BOLT OVER TORQUED. SERVICED NOSE LANDING GEAR STRUT TO PROPER DIMENSION AND RETORQUED APEX BOLT. ACCOMPLISHED GEAR SWING AND OPERATED NORMALLY. REFERENCE 95ZZZM60.