# N35836: 1986 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2005-06-29 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 29, 2005 - Exported to: Thailand - Status when cancelled: Valid registration - 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 series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 49441 - Year built: 1986 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: July 12, 1988 - Certificate issued: November 6, 1989 - Last registry action: August 23, 2004 - Mode S code: A40565 - Owner when cancelled: [Boeing Capital Corporation](https://openairdocs.org/faa-owner/BOEING%20CAPITAL%20CORPORATION) - Location: [Renton, WA](https://openairdocs.org/faa-place/WA/Renton) - Owner type: Corporation - Owner's area on the map: 47.4475° N, 122.2016° W: Placed by OpenAirDocs at the center of ZIP code 98055, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N35836 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=35836 - Page: https://openairdocs.org/deregistered/N35836-2005-06-29 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 (46) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0500042](https://openairdocs.org/sdr/CALA0500042), Feb 6, 2005: SEAT TRACK. CORRODED. INSPECTION FOUND F/O'S AFT O/B SEAT TRACK CORRODED. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-40-01. - [SDR CALA0500041](https://openairdocs.org/sdr/CALA0500041), Feb 3, 2005: PANEL. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN UPPER TRAILING EDGE PANEL LOCATED FORWARD OF O/B SIDE OF GROUND SPOILER, LEFT UPPER WING, XRS 91.0 TO 111.5. A NEW PANEL WAS - [SDR CALA0500040](https://openairdocs.org/sdr/CALA0500040), Feb 3, 2005: DOOR FRAME. CRACKED. INSPECTION FOUND A 1.75 INCH CRACK IN NWW LT DOOR JAMB AT UPPER LOCK FASTENER FOR SPRAY DEFLECTOR GUARD, STA 45. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INS - [SDR CALA0500036](https://openairdocs.org/sdr/CALA0500036), Feb 1, 2005: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK BELOW LOWER FORWARD LATCH OF MID CARGO DOOR SKIN. THE DOOR SKIN WAS REPAIRED IAW SRM 52-05, FIGURE 26A. - [SDR CALA0500035](https://openairdocs.org/sdr/CALA0500035), Jan 31, 2005: PAN. CRACKED. INSPECTION FOUND A .75 INCH CRACK AT CORNER OF LOWER FORWARD INNER PAN OF FORWARD CARGO DOOR. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW - [SDR CALA0500031](https://openairdocs.org/sdr/CALA0500031), Jan 29, 2005: FLOOR PANEL. DELAMINATED. INSPECTION FOUND LT CENTER FLOOR PANEL DELAMINATED AND HOLES PUNCHED IN PANEL AT STA 465-541, LBL 20 TO LBL 40. A NEW PANEL WAS INSTALLED IAW SRM 53-05, PAGE 12 - [SDR CALA0500028](https://openairdocs.org/sdr/CALA0500028), Jan 28, 2005: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 1322 UNDER RT LAV, RBL 20. THE CORRODED SECTION OF FLOORBEAM WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-05, FI - [SDR CALA0500025](https://openairdocs.org/sdr/CALA0500025), Jan 27, 2005: FLOOR SUPPORT. CRACKED. INSPECTION FOUND A 1 INCH CRACK AT FORWARD O/B END OF FORWARD ENTRY FLOOR SUPPORT TEE AT STA 180, RBL 43. A REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2. - [SDR CALA0500024](https://openairdocs.org/sdr/CALA0500024), Jan 26, 2005: SEAT TRACK. CORRODED. INSPECTION FOUND LT MIDDLE SEAT TRACK CORRODED FROM STA 1022-1250, S18L. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM - [SDR CALA0500022](https://openairdocs.org/sdr/CALA0500022), Jan 26, 2005: STRUCTURE. CORRODED. INSPECTION FOUND SUBFLOOR CORRODED UNDER LEFT O/B SEAT TRACK AT STA 1174, LBL 60. THE CORRODED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-70-4. - [SDR CALA0500021](https://openairdocs.org/sdr/CALA0500021), Jan 24, 2005: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT I/B CABIN SEAT TRACK CORRODED FROM STA 1022-1250, LBL 25. THE SEAT TRACK WAS REPLACED IAW SRM 53-05, FIGURE 4. - [SDR CALA0500020](https://openairdocs.org/sdr/CALA0500020), Jan 22, 2005: SEAT TRACK. CORRODED. INSPECTION FOUND CAPTAIN'S AFT I/B SEAT TRACK CORRODED AT STA 83.55 - 101.55, LBL 10. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-01. - [SDR CALA0500017](https://openairdocs.org/sdr/CALA0500017), Jan 21, 2005: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 180, LBL 12 TO LBL 37. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-3 AND 51-30-2. - [SDR CALA0500016](https://openairdocs.org/sdr/CALA0500016), Jan 21, 2005: RIB. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN RIB AND DOUBLER AT LT WING LEADING EDGE INTERNALLY BETWEEN NR 9 AND NR 10 SLAT TRACK CUTOUTS, STA XRS 324. THE CRACKED RIB - [SDR CALA0500057](https://openairdocs.org/sdr/CALA0500057), Jan 20, 2005: CUSP WEB. CORRODED. INSPECTION FOUND RT CUSP CORRODED AT STA 200. A SMALL SECTION OF THE UPPER CUSP CHORD WAS TRIMMED OUT TO REMOVE LOCAL CORROSION AND A REPAIR DOUBLER WAS INSTALL - [SDR CALA0500012](https://openairdocs.org/sdr/CALA0500012), Jan 17, 2005: LONGERON. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN LONGERON 4L AT STA 160. A NEW LONGERON SECTION WAS SPLICED IN IAW SRM 53-02 FIGURE 18. - [SDR CALA0500009](https://openairdocs.org/sdr/CALA0500009), Jan 16, 2005: FLOOR SUPPORT. CORRODED. INSPECTION FOUND CENTER FLOOR SUPPORT BETWEEN I/B AND MIDDLE SEAT TRACKS CORRODED AROUND SCREW HOLES AT LT SIDE STA 1155, BL 0 TO LBL 30. THE FLOOR SUPPORT WAS - [SDR CALA0100894](https://openairdocs.org/sdr/CALA0100894), Sep 23, 2001: CLIP. OUT OF ADJ. THE TAILCONE EXTERIOR RELEASE HANDLE PULL FROM CLIPS WAS LOW. THE CLIPS WERE ADJUSTED IAW MM 53-53-00. - [SDR CALA0100893](https://openairdocs.org/sdr/CALA0100893), Sep 21, 2001: FRAME. CRACKED. INSPECTION FOUND A CRACK IN TAIL COMPARTMENT CANTED FRAME AT STA 1446, L3R AN L26L. THE CRACKED FRAME CAP WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5. - [SDR CALA0100891](https://openairdocs.org/sdr/CALA0100891), Sep 20, 2001: FITTING. CRACKED. INSPECTION FOUND A 2.5" CRACK IN R/H WING GROUND SPOILER ACTUATOR FITTING. A DOUBLER WAS INSTALLED IAW ECRA 5740-01317 AND DRAWING SRO9570010. - [SDR CALA0100890](https://openairdocs.org/sdr/CALA0100890), Sep 20, 2001: FITTING. CRACKED. INSPECTION FOUND A 2.25" CRACK IN L/H WING LEFT I/B GROUND SPOILER ACTUATOR SUPPORT FITTING. REPAIRED IAW ECRA 5740-01317 AND DRAWING SR09570010. - [SDR CALA0100887](https://openairdocs.org/sdr/CALA0100887), Sep 19, 2001: DOOR FRAME. CORRODED. INSPECTION FOUND MID BAGGAGE BIN LOWER DOOR JAMB CORRODED AROUND H-SHEAR AT STA 636-693. A REPAIR DOUBLER AND SPACER WERE INSTALLED IAW SRM 53-05, FIGURE 63. - [SDR CALA0100886](https://openairdocs.org/sdr/CALA0100886), Sep 19, 2001: DOOR FRAME. CORRODED. INSPECTION FOUND AFT BAGGAGE BIN LOWER DOOR JAMB CORRODED BETWEEN STA 1155-1211. A Z-ANGLE BEAM REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 63. - [SDR CALA0000502](https://openairdocs.org/sdr/CALA0000502), Apr 18, 2000: ACM. LEAKING. WHEN THROTTLES WERE BROUGHT UP FOR TAKEOFF (DURING TAKEOFF ROLL) A NOXIOUS FOUL ODOR ENTERED THE AIRCRAFT THROUGH THE AIR CONDITIONING PACKS. THE CREW AND PASSE - [SDR CALA0000141](https://openairdocs.org/sdr/CALA0000141), Feb 8, 2000: POWER SUPPLY. INOPERATIVE. INSPECTION FOUND BOTH OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. A NEW POWER SUPPLY AND BATTERY PACK WERE INSTALLED IAW MM 33-53-00, PAGE 407. - [SDR CALA9900538](https://openairdocs.org/sdr/CALA9900538), May 13, 1999: FAIRING. GOUGED. LEFT WING NR 4 SLAT TRACK CAN GOUGED. WELDED CAN PER DRWG 5935801 AND INSTALLED PER MM 27-80-01. - [SDR CALA9900527](https://openairdocs.org/sdr/CALA9900527), May 11, 1999: TAIL CONE. OUT OF ADJUST. TAIL COMPARTMENT INTERIOR TAIL CONE RELEASE HANDLE PULL TOO HIGH (45 LBS). RIGGED TAIL CONE RELEASE MECHANISM PER MM 53-53-00. - [SDR CALA9900525](https://openairdocs.org/sdr/CALA9900525), May 11, 1999: BRACKET. CRACKED. LEFT FORWARD EMERGENCY EXIT DOOR SEAL RETAINER SUPPORT BRACKET CRACKED AT RIVET (.5). REPLACED FORWARD LOWER RETAINER BRACKET PER SRM 51-30-2. - [SDR CALA9900523](https://openairdocs.org/sdr/CALA9900523), May 11, 1999: SKIN. GOUGED. FUSELAGE SKIN IS GOUGED UNDER AFT END OF ADF ANTENNA. BLENDED GOUGE AND INSTALLED REPAIR PER SRM 53-04 FIG 38 VIEW G. - [SDR CALA9900492](https://openairdocs.org/sdr/CALA9900492), May 8, 1999: RETAINER. CORRODED. LEFT FORWARD EMERGENCY EXIT DOOR CORROSION FOUND AT LOWER AFT CORNER SEAL RETAINER. REMOVED AND REPLACED SEAL RETAINER PER SRM 51-30-2. - [SDR CALA990497](https://openairdocs.org/sdr/CALA990497), May 7, 1999: JAMB. CORRODED. FORWARD CORGO DOOR JAMB PAN LOWER SECTION IS CORRODED. INSTALLED SPLICE REPAIR ON DOOR JAMB PER SRM 53-05 FIG 44. - [SDR CALA9900500](https://openairdocs.org/sdr/CALA9900500), May 7, 1999: DOUBLER. CRACKED. AFT SERVICE DOOR DOUBLER AROUND HOLD OPEN HOOK CRACKED (1) OUTER SKIN. INSTALLED DOUBLER REPAIR PER EC/RA 5205-01008. - [SDR CALA9900496](https://openairdocs.org/sdr/CALA9900496), May 7, 1999: SEAT TRACK. CORRODED. SEAT TRACK NR 2 CORROSION AT NUT PLATE HOLES FROM STA 1136 - 1174. REPLACED SEAT TRACK LEFT CENTER STA 1079 - 1305 PER SRM 51-30-01. - [SDR CALA9900487](https://openairdocs.org/sdr/CALA9900487), May 5, 1999: SEAT TRACK. CORRODED. LEFT MOST INBOARD SET TRACK HAS CORROSION AT CENTER CHANNEL STA 1105. REMOVED AND REPLACED SEAT TRACK PER SRM 53-05 FROM STA 1041 - 1309. - [SDR CALA9900484](https://openairdocs.org/sdr/CALA9900484), May 4, 1999: SEAT TRACK. CORRODED. RIGHT CENTER SEAT TRACK CORRODED STA 200 AND 237. REMOVED AND REPLACED SEAT TRACK STA 200 - 247 PER SRM 51-30-1. - [SDR CALA9900470](https://openairdocs.org/sdr/CALA9900470), May 3, 1999: BULKHEAD DOUBLER. CORRODED. CORROSION AT AFT PRESSURE BULKHEAD AND VERTICAL BULKHEAD INTERSECTION AT STA 1338 FROM L-29LT TO L-29RT. REMOVED CORROSION AND INSTALLED SERVICEABLE JACK PAD DO - [SDR CALA9900469](https://openairdocs.org/sdr/CALA9900469), May 3, 1999: SKIN. HOLE. TEMPORARY REPAIR APPROXIMATELY STA 383 L-29LT WHERE PREVIOUS PHONE ANTENNA INSTALLED. INSTALLED DOUBLERS PER SRM 53-04 FIG 38. - [SDR CALA9900467](https://openairdocs.org/sdr/CALA9900467), Apr 30, 1999: BEAM. CRACKED. HOU - FORWARD SERVICE DOOR NR 4 BEAM IS CRACKED AT FORWARD END 1.5 INCH. INSTALLED NEW BEAM PER SRM 51-30-2 AND 51-30-1. (M) - [SDR CALA9900466](https://openairdocs.org/sdr/CALA9900466), Apr 30, 1999: BEAM. CRACKED. HOU - MAIN CABIN DOOR NR 1 BEAM IS CRACKED AT BOTH ENDS .625 INCH FORWARD AND 1 INCH AFT. REMOVED AND REPLACED BEAM PER SRM 51-30-0. (M) - [SDR CALA9900465](https://openairdocs.org/sdr/CALA9900465), Apr 30, 1999: ANGLE. CRACKED. HOU - RIGHT INNER ATTACH ANGLE CRACKED 1 INCH, DORSAL FIN. REMOVED AND REPLACED ATTACH ANGLE PER SRM 51-30-2. (M) - [SDR CALA9900464](https://openairdocs.org/sdr/CALA9900464), Apr 30, 1999: ANGLE. CRACKED. HOU - LEFT INNER ATTACH ANGLE CRACKED 1 INCH, DORSAL FIN. REMOVED AND REPLACED ANGLE PER SRM 51-30-2. (M) - [SDR CALA9900453](https://openairdocs.org/sdr/CALA9900453), Apr 29, 1999: ESCAPE LINE. FRAYED. RIGHT OVERWING EXIT ESCAPE LINE IS FRAYED AT ATTACH HOOK. REPLACED ESCAPE LINE PER MM 25-61-00. - [SDR CALA9900452](https://openairdocs.org/sdr/CALA9900452), Apr 29, 1999: ESCAPE LINE. FRAYED. LEFT OVERWING EMERGENCY EXIT ESCAPE LINE IS FRAYED AT ATTACH HOOK. REPLACED ESCAPE LINE PER MM 25-61-00. - [SDR CALA9900223](https://openairdocs.org/sdr/CALA9900223), Mar 4, 1999: FUSE. BLOWN. INSPECTION FOUND MIDDLE SECTION OF SEAT MOUNTED EMERGENCY PATH LIGHTING INOPERATIVE. MAINTENANCE FOUND MOST OUTBOARD FUSE OF MIDDLE POWER SUPPLY PACK BLOWN. THE - [SDR CALA9601479](https://openairdocs.org/sdr/CALA9601479), Oct 17, 1996: SLIDE. FELL OFF. FORWARD ENTRY DOOR SLIDE FELL OFF DOOR. REINSTALLED SLIDE PACK PER MAINTENANCE MANUAL. - [SDR CAL950187](https://openairdocs.org/sdr/CAL950187), Mar 9, 1995: T/R CNTL VALVE. RUPTURED. SFO - FLT 0165 - THE MAIN CABIN BEGAN TO FILL WITH SMOKE DURING TAXI TO TERMINAL AFTER LANDING AT SFO. THE AIRCRAFT WAS STOPPED ON THE TAXIWAY, THE L-1 DOOR AND ## FAA accident and incident reports (2) 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 19990908027319I](https://openairdocs.org/incident/19990908027319I), Sep 8, 1999: Doug DC982 (N35836), Houston, TX. (-23) Hydraulic system malfunction/smoke in the cabin; emergency evacuation slides deployed. 1. Reason: hydraulic system malfunction and smoke/fumes in the… - [Incident 19950310005009I](https://openairdocs.org/incident/19950310005009I), Mar 10, 1995: Doug DC9 (N35836), San Francisco, CA. Narrative: when cala F165/9 landed at sfo the a/c filled with smoke. Crew stopped a/c on runway, shutdown engines and notified cala ground control declared an… ## Other aircraft with N35836 - [Cancelled 1975-06-16](https://openairdocs.org/deregistered/N35836-1975-06-16): Cessna U206F, S/N U20602748. Exported to Mexico. Owner: [Airflite Inc Couth](https://openairdocs.org/faa-owner/AIRFLITE%20INC%20COUTH), [Long Beach, CA](https://openairdocs.org/faa-place/CA/Long%20Beach) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.