# N936AS: 1986 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2013-03-21

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 21, 2013
- Status when cancelled: Second renewal notice
- Airframe: [Mcdonnell Douglas DC-9-82(MD-82)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82) (registry code 3022082)
- Engine: [Pratt & Whitney JT8D-5](https://openairdocs.org/engine/pratt-whitney-jt8d-5) (registry code 52046)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 49363
- Year built: 1986
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: January 24, 1998
- Certificate issued: November 29, 1996
- Last registry action: November 20, 2007
- Mode S code: ACFC04
- Owner when cancelled: [Continental Airlines Inc](https://openairdocs.org/faa-owner/CONTINENTAL%20AIRLINES%20INC)
- Location: [Houston, TX](https://openairdocs.org/faa-place/TX/Houston)
- Owner type: Corporation
- Owner's area on the map: 29.7568° N, 95.3657° W: Placed by OpenAirDocs at the center of ZIP code 77002, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N936AS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=936AS
- Page: https://openairdocs.org/deregistered/N936AS-2013-03-21

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Mcdonnell Douglas DC-9-82(MD-82): https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82.md

## Service difficulty reports (58, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR CALA0000129](https://openairdocs.org/sdr/CALA0000129), Feb 2, 2000: SKIN. CRACKED. 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.
- [SDR CALA0000107](https://openairdocs.org/sdr/CALA0000107), Jan 28, 2000: FLOORBEAM. CRACKED. 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 
- [SDR CALA0000106](https://openairdocs.org/sdr/CALA0000106), Jan 28, 2000: RIB. CRACKED. 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
- [SDR CALA0000093](https://openairdocs.org/sdr/CALA0000093), Jan 27, 2000: FRAME. CRACKED. 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 DOUB
- [SDR CALA0000092](https://openairdocs.org/sdr/CALA0000092), Jan 27, 2000: ANGLE. CRACKED. 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, 51-1
- [SDR CALA0000091](https://openairdocs.org/sdr/CALA0000091), Jan 27, 2000: BRACKET. CRACKED. 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.
- [SDR CALA0000086](https://openairdocs.org/sdr/CALA0000086), Jan 26, 2000: ANGLE. CRACKED. 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.
- [SDR CALA0000078](https://openairdocs.org/sdr/CALA0000078), Jan 24, 2000: ANGLE. CRACKED. 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 
- [SDR CALA0000077](https://openairdocs.org/sdr/CALA0000077), Jan 24, 2000: INTERCOSTAL. CRACKED. 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.
- [SDR CALA0000076](https://openairdocs.org/sdr/CALA0000076), Jan 24, 2000: SEAT TRACK. CORRODED. 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
- [SDR CALA0000057](https://openairdocs.org/sdr/CALA0000057), Jan 21, 2000: FRAME. CORRODED. 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.
- [SDR CALA0000056](https://openairdocs.org/sdr/CALA0000056), Jan 21, 2000: BULKHEAD. CRACKED. 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 
- [SDR CALA0000040](https://openairdocs.org/sdr/CALA0000040), Jan 18, 2000: SEAT TRACK. CORRODED. 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.
- [SDR CALA0000039](https://openairdocs.org/sdr/CALA0000039), Jan 18, 2000: ANGLE. CORRODED. 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 A
- [SDR CALA0000038](https://openairdocs.org/sdr/CALA0000038), Jan 18, 2000: SEAT TRACK. CORRODED. 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.
- [SDR CALA0000037](https://openairdocs.org/sdr/CALA0000037), Jan 18, 2000: ANGLE. CORRODED. 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.
- [SDR CALA0000036](https://openairdocs.org/sdr/CALA0000036), Jan 18, 2000: WEB. CORRODED. 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 
- [SDR CALA0000034](https://openairdocs.org/sdr/CALA0000034), Jan 18, 2000: SKIN. CRACKED. 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 REPA
- [SDR CALA9801856](https://openairdocs.org/sdr/CALA9801856), Sep 23, 1998: LINK. BROKEN. 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. MAINT
- [SDR CALA9800144](https://openairdocs.org/sdr/CALA9800144), Jan 31, 1998: AIR DISTRIBUTION. SMOKE. 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 WIT
- [SDR CALA9800098](https://openairdocs.org/sdr/CALA9800098), Jan 21, 1998: CABLE. DAMAGED. INSPECTION FOUND TAILCONE RELEASE CABLE KINKED AT TOP LEFT PULLEY. THE CABLE WAS REMOVED AND REPLACED AND RIGGED IAW MM 53-53-00.
- [SDR CALA9800014](https://openairdocs.org/sdr/CALA9800014), Jan 10, 1998: BRACKET. CRACKED. 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.
- [SDR CALA9800013](https://openairdocs.org/sdr/CALA9800013), Jan 10, 1998: CABLES. OUT OF ADJUST. PULL FROM THE TAIL CONE INTERIOR RELEASE HANDLE WAS EXCESSIVE AT 40 POUNDS. THE LATCH CABLES WERE RIGGED IAW MM 53-53-00.
- [SDR CALA9800009](https://openairdocs.org/sdr/CALA9800009), Jan 7, 1998: JAMB. CORRODED. 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.
- [SDR CALA9701396](https://openairdocs.org/sdr/CALA9701396), Sep 29, 1997: BATTERIES. DISCHARGED. INSPECTION FOUND EMERGENCY OVERHEAD LIGHTS AT L-1 AND R-1 DOORS INOPERATIVE. THE POWER SUPPLY BATTERIES WERE REPLACED AND OPERATION CHECKED GOOD.
- [SDR ASAA9680196](https://openairdocs.org/sdr/ASAA9680196), Sep 8, 1996: BATTERIES. DISCHARGED. SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M)
- [SDR ASAA9680120](https://openairdocs.org/sdr/ASAA9680120), May 22, 1996: BATTERIES. DISCHARGED. SFO - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHT IN THE FORWARD CABIN WERE FOUND DIM. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M)
- [SDR ASAA9680104](https://openairdocs.org/sdr/ASAA9680104), Apr 23, 1996: LIGHT. DEFECTIVE. PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND DIM. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (X)
- [SDR ASAA9680100](https://openairdocs.org/sdr/ASAA9680100), Apr 16, 1996: DOOR MECHANISM. OUT OF ADJUST. 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. RE
- [SDR ASAA9680078](https://openairdocs.org/sdr/ASAA9680078), Mar 24, 1996: DOWNLOCK SENSOR. DEFECTIVE. SEA - FLT 467 - CREW REPORTED THE NOSE LANDING GEAR LIGHT REMAINED ILLUMINATED AFTER TAKEOFF OAK. FOLLOWED ABNORMAL GEAR INDICATION CHECKLIST, RECYCLED LANDING 
- [SDR ASAA9680074](https://openairdocs.org/sdr/ASAA9680074), Mar 12, 1996: FLOOR COVERING. EXCESS MATERIAL. 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 
- [SDR ASAA9680035](https://openairdocs.org/sdr/ASAA9680035), Jan 24, 1996: BATTERY PACK. DISCHARGED. SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 2 TO 6 WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (M)
- [SDR ASAA9680034](https://openairdocs.org/sdr/ASAA9680034), Jan 23, 1996: MECHANISM. OUT OF ADJUST. 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
- [SDR ASAA9680033](https://openairdocs.org/sdr/ASAA9680033), Jan 21, 1996: SEAL. RUBBING. 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 NORMA
- [SDR ASAA9680032](https://openairdocs.org/sdr/ASAA9680032), Jan 21, 1996: DOOR. OUT OF ADJUST. SEA - DURING MAINTENANCE CHECK, THE L1 DOOR GUST LOCK WAS FOUND INOPERATIVE. RERIGGED DOOR PER MAINTENANCE MANUAL AND OPERATED NORMALLY. (M)
- [SDR ASAA9680031](https://openairdocs.org/sdr/ASAA9680031), Jan 20, 1996: DOOR FRAME. CORRODED. 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 SR
- [SDR ASAA9680030](https://openairdocs.org/sdr/ASAA9680030), Jan 20, 1996: CUSP. CORRODED. 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 
- [SDR ASAA9680029](https://openairdocs.org/sdr/ASAA9680029), Jan 20, 1996: INTERCOSTAL. CORRODED. 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
- [SDR ASAA9680028](https://openairdocs.org/sdr/ASAA9680028), Jan 20, 1996: LONGERON. CORRODED. 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)
- [SDR ASAA9680027](https://openairdocs.org/sdr/ASAA9680027), Jan 20, 1996: LONGERON. CORRODED. 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, 
- [SDR ASAA9680026](https://openairdocs.org/sdr/ASAA9680026), Jan 20, 1996: FRAME. CORRODED. 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, 5
- [SDR ASAA9680021](https://openairdocs.org/sdr/ASAA9680021), Jan 15, 1996: SUPPORT. CRACKED. 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, 51-30-0
- [SDR ASAA9680020](https://openairdocs.org/sdr/ASAA9680020), Jan 15, 1996: SUPPORT. CORRODED. 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 5
- [SDR ASAA9680019](https://openairdocs.org/sdr/ASAA9680019), Jan 15, 1996: SEAT TRACK. CORRODED. 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)
- [SDR ASAA9680018](https://openairdocs.org/sdr/ASAA9680018), Jan 15, 1996: SEAT TRACK. CORRODED. 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
- [SDR ASAA9680017](https://openairdocs.org/sdr/ASAA9680017), Jan 15, 1996: SPLICE. CORRODED. 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)
- [SDR ASAA9680016](https://openairdocs.org/sdr/ASAA9680016), Jan 15, 1996: LONGERON. CORRODED. 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)
- [SDR ASAA9680015](https://openairdocs.org/sdr/ASAA9680015), Jan 15, 1996: LONGERON. CORRODED. 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
- [SDR ASAA9680169](https://openairdocs.org/sdr/ASAA9680169), Jan 5, 1996: THRESHOLD. CORRODED. 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 2
- [SDR ASAA9680168](https://openairdocs.org/sdr/ASAA9680168), Jan 3, 1996: SKIN. CORRODED. 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 P

All 58: https://openairdocs.org/deregistered/N936AS-2013-03-21/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19990812042599I](https://openairdocs.org/incident/19990812042599I), Aug 12, 1999: Doug DC982 (N936AS), Newark, NJ. (-23)An air carrier aircraft departed the gate and then returned due to mechanical problems. All passengers deplaned from the aircraft during a plane change.…

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