# N12811: 1985 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2007-06-01 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 1, 2007 - Status when cancelled: Triennial form not returned - 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: 49265 - Year built: 1985 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: February 23, 1985 - Certificate issued: September 2, 1997 - Last registry action: September 19, 2006 - Mode S code: A073FF - 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/N12811 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=12811 - Page: https://openairdocs.org/deregistered/N12811-2007-06-01 From the FAA registry file of November 4, 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 (40) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0400031](https://openairdocs.org/sdr/CALA0400031), Jan 15, 2004: MEGAPHONE. INOPERATIVE. INSPECTION FOUND THE FORWARD CABIN MEGAPHONE INOPERATIVE. THE MEGAPHONE WAS REMOVED AND REPLACED. - [SDR CALA0300530](https://openairdocs.org/sdr/CALA0300530), Aug 17, 2003: FAN. SEIZED. A/C HAD A CHRONIC INFLT PROBLEM WITH AN ELECTRICAL ODOR AFT. TROUBLESHOOTING PERFORMED. SOURCE OF ODOR APPEARED TO BE COMING FROM AFT GALLEY. COFFEEMAKERS, OVEN - [SDR CALA0200341](https://openairdocs.org/sdr/CALA0200341), Jun 14, 2002: BELTFRAME. CRACKED. INSPECTION FOUND A 1" CRACK IN TAIL COMPARTMENT BELTFRAME AT STA 1418, LONGERON 1. REPAIRED BELTFRAME IAW SRM 53-03, FIGURE 4. - [SDR CALA0200338](https://openairdocs.org/sdr/CALA0200338), Jun 12, 2002: WEB. CRACKED. INSPECTION FOUND TAIL COMPARTMENT BELTFRAME WEB CRACKED AT STA 1463 L18R AND L18L. BOTH CRACKS WERE 2" LONG. THE CRACKS WERE STOP DRILLED AND DOUBLERS WERE INST - [SDR CALA0000459](https://openairdocs.org/sdr/CALA0000459), Apr 11, 2000: PAN. CHAFED. INSPECTION FOUND AFT BAG BIN DOOR PAN CHAFED AT STOP PAD AREAS. REPAIRED IAW ECRA 5230-01540. - [SDR CALA0000457](https://openairdocs.org/sdr/CALA0000457), Apr 11, 2000: PAN. CHAFED. INSPECTION FOUND DOOR PAN CHAFED BY DOOR STOP IN TWO PLACES AT AFT SIDE AND THREE PLACES AT FORWARD SIDE, FORWARD BAGGAGE BIN. REPAIRED IAW ECRA 5230-01540. - [SDR CALA0000455](https://openairdocs.org/sdr/CALA0000455), Apr 11, 2000: LONGERON. CRACKED. INSPECTION FOUND A HALF INCH CRACK IN LONGERON 4 LT AT STA 160. THE LONGERON WAS REPAIRED IAW ECRA 5310-04005. - [SDR CALA0000454](https://openairdocs.org/sdr/CALA0000454), Apr 11, 2000: ANGLE. CRACKED. INSPECTION FOUND LT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CRACKED AT STA 1474 - 1485. THERE WERE FIVE CRACKS TOTALING 8 INCHES IN COMBINED LENGTH. THE AT - [SDR CALA0000413](https://openairdocs.org/sdr/CALA0000413), Apr 6, 2000: CABLE. OUT OF RIG. THE FORCE REQUIRED TO DROP THE TAIL CONE USING INTERIOR AND EXTERIOR RELEASE HANDLES EXCEEDED 35 POUNDS. THE TAIL CONE RELEASE SYSTEM CABLES WERE ADJUSTED IAW M - [SDR CALA0000408](https://openairdocs.org/sdr/CALA0000408), Apr 5, 2000: FRAME. WORN. INSPECTION FOUND A HOLE WORN INTO FRAME WEB AT STA 1380 AT LT AIR CONDITIONING TEMP CONTROL VALVE. REPAIRED FRAME WEB IAW SRM 53-01. - [SDR CALA0000407](https://openairdocs.org/sdr/CALA0000407), Apr 5, 2000: BEAM. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FORWARD SERVICE DOOR LOWER FORWARD BEAM. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA0000406](https://openairdocs.org/sdr/CALA0000406), Apr 5, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND AFT CARGO BIN LEFT AND RIGHT TIEDOWN TRACKS CORRODED AROUND NUT PLATE HOLES AT STA 1022. THE TIEDOWN TRACKS WERE REMOVED AND REPLACED IAW SRM 5 - [SDR CALA0000405](https://openairdocs.org/sdr/CALA0000405), Apr 5, 2000: PAN. CRACKED. INSPECTION FOUND MID CARGO BIN DOOR PAN CRACKED AT FORWARD AND AFT LATCH. REPAIRED IAW SRM 52-05, FIGURE 26A. - [SDR CALA0000404](https://openairdocs.org/sdr/CALA0000404), Apr 5, 2000: SKIN. GOUGED. INSPECTION FOUND FORWARD CARGO DOOR SKIN GOUGED AT DOOR BOTTOM. REPAIRED IAW SRM 52-03, FIGURE 7. - [SDR CALA0000402](https://openairdocs.org/sdr/CALA0000402), Apr 5, 2000: PAN. WORN. INSPECTION FOUND FORWARD CARGO DOOR OUTER PAN WORN AT DOOR STOP PADS. REPAIRED AFT STOPS IAW ECRA 5330-02819. - [SDR CALA0000401](https://openairdocs.org/sdr/CALA0000401), Apr 5, 2000: PAN. WORN. INSPECTION FOUND FORWARD CARGO BIN LOWER DOOR PAN WORN IN TWO PLACES BY DOOR STOPS. TWO STRAPS WERE INSTALLED IAW ECRA 5330-02819. - [SDR CALA0000394](https://openairdocs.org/sdr/CALA0000394), Apr 4, 2000: FLOORBEAM. GOUGED. INSPECTION FOUND A HOLE GOUGED IN CABIN FLOORBEAM AT STA 396. A REPAIR WAS INSTALLED IAW SRM 53-05 SHEETS 1, 2 & 3. - [SDR CALA0000379](https://openairdocs.org/sdr/CALA0000379), Mar 31, 2000: LONGERON. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN LONGERON 2R JUST OVER BELTFRAME AT STA 1429. A NEW SECTION OF LONGERON WAS SPLICED IN IAW SRM 53-02, FIGURE 18, SHEET 2. - [SDR CALA0000375](https://openairdocs.org/sdr/CALA0000375), Mar 30, 2000: PAN. CRACKED. INSPECTION FOUND AFT BAG BIN DOOR EXTERIOR HANDLE PAN GOUGED WITH A 1 INCH CRACK. THE PAN WAS REMOVED AND REPLACED IAW MM 51-30-02. - [SDR CALA0000374](https://openairdocs.org/sdr/CALA0000374), Mar 30, 2000: BELTFRAME. CORRODED. INSPECTION FOUND BELTFRAME CORRODED ON AFT SIDE AT STA 541 FROM LONGERON 29L TO 29R. THE CORROSION WAS REMOVED, TREATED AND PRIMED AREA IAW SRM 51-10-3 AND REIN - [SDR CALA0000373](https://openairdocs.org/sdr/CALA0000373), Mar 30, 2000: BELTFRAME. CORRODED. INSPECTION FOUND AFT BAG BIN BELTFRAME CORRODED AT STA 1238, LONGERON 24L. THE CORROSION WAS REMOVED, TREATED, AND PRIMED IAW SRM 53-01, FIGURE 1. - [SDR CALA0000369](https://openairdocs.org/sdr/CALA0000369), Mar 30, 2000: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 389, LONGERON 29R TO 30. A REPAIR WAS INSTALLED IAW ECRA 5330-02800. - [SDR CALA0000421](https://openairdocs.org/sdr/CALA0000421), Mar 30, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND RT O/B SEAT TRACK CORRODED IN FORWARD GALLEY AREA AT STA 218-266. THE SEAT TRACK WAS REPLACED IAW SRM 53-05, FIGURE 4F. - [SDR CALA0000368](https://openairdocs.org/sdr/CALA0000368), Mar 28, 2000: FLOOR SUPPORT. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN MAIN CABIN FLOOR SUPPORT AT STA 826 UNDER RIGHT I/B SEAT TRACK. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-1. - [SDR CALA0000367](https://openairdocs.org/sdr/CALA0000367), Mar 28, 2000: SEAT TRACK. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN MAIN CABIN FLOOR SUPPORT AT STA 927 BELOW LT O/B SEAT TRACK. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-0. - [SDR CALA0000366](https://openairdocs.org/sdr/CALA0000366), Mar 28, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FORWARD R-1 ENTRY SLIDE ARMING BAR ATTACHED FORWARD AND AFT FLOOR SUPPORTS CORRODED. THE SUPPORTS WERE REMOVED AND NEW ONES WERE INSTALLED IAW - [SDR CALA0000355](https://openairdocs.org/sdr/CALA0000355), Mar 27, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LT CENTER SEAT TRACK CORRODED ON BOTH SIDES OF FLOOR SUPPORT FLANGES FROM FS 1041 - 1309. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30 - [SDR CALA0000332](https://openairdocs.org/sdr/CALA0000332), Mar 22, 2000: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AND GOUGED AT STA 120-133, LONGERON 23R. A REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38. - [SDR CALA0000330](https://openairdocs.org/sdr/CALA0000330), Mar 22, 2000: LINE. FRAYED. INSPECTION FOUND THE LEFT AND RIGHT OVERWING EMERGENCY ESCAPE LINES FRAYED AT ATTACH HOOK. THE EMERGENCY ESCAPE LINES WERE REMOVED AND REPLACED IAW MM 25-60-00. - [SDR CALA0000329](https://openairdocs.org/sdr/CALA0000329), Mar 22, 2000: SKIN. DENTED. INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 712, LONGERON 20L. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38. - [SDR CALA9801857](https://openairdocs.org/sdr/CALA9801857), Sep 26, 1998: ACTUATOR. BURNT. THE CO-PILOT OBSERVED SMOKE COMING FROM THE THROTTLE QUADRANT AFTER TAKEOFF FROM COS. THE ELECTRICAL FIRE/SMOKE OF UNKNOWN ORIGIN EMERGENCY LIST WAS INITIATED A - [SDR CALA9800596](https://openairdocs.org/sdr/CALA9800596), Mar 26, 1998: BEAM. CRACKED. INSPECTION FOUND A 1 INCH CRACK AT FORWARD END AND AFT END OF NR 1 DOOR BEAM OF MAIN CABIN DOOR. A NEW NR 1 MAIN CABIN DOOR BEAM WAS INSTALLED IAW SRM 51-30-1, - [SDR CALA9800589](https://openairdocs.org/sdr/CALA9800589), Mar 25, 1998: INTERCOSTAL. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN RADIUS OF MAIN CABIN DOOR INTERCOSTAL AFT OF HANDLE TORQUE SHAFT. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-02 AND 51-30-05. - [SDR CALA9800588](https://openairdocs.org/sdr/CALA9800588), Mar 25, 1998: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN MAIN CABIN DOOR EXTERIOR SKIN AROUND HOLD OPEN HOOK CUTOUT. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 20A, PAGE 43. - [SDR CALA9800587](https://openairdocs.org/sdr/CALA9800587), Mar 25, 1998: PIVOT PLATES. CORRODED. INSPECTION FOUND LT HORIZONTAL STABILIZER INBOARD AND OUTBOARD SET OF PIVOT PLATES CORRODED. THE PIVOT PLATES WERE REPLACED IAW SRM 51-30-5. - [SDR CALA9701510](https://openairdocs.org/sdr/CALA9701510), Oct 28, 1997: RETRACT MECH. MALFUNCTIONED. THE AIRCRAFT WAS STUCK IN GROUND MODE AND THE GEAR WOULD NOT RETRACT AFTER TAKEOFF. QRH PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO IAH WHERE - [SDR CALA9700188](https://openairdocs.org/sdr/CALA9700188), Feb 17, 1997: BUS CONTROL. MALFUNCTIONED. ALL ELECTRICAL POWER FELL OFF LINE AND ARTS WAS INITIATED AFTER TAKEOFF. EMERGENCY POWER WAS TURNED ON, THE APU GENERATOR WAS PUT ON LINE, PARTIAL POWER WAS RES - [SDR CALA9600967](https://openairdocs.org/sdr/CALA9600967), Jul 6, 1996: AIRSEAL. WORN. THE NR 1 ENGINE SPOOLED DOWN ACCOMPANIED BY A LOUD EXPLOSION WHILE CLIMBING THROUGH FL 310. ABNORMAL PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED - [SDR CAL960033](https://openairdocs.org/sdr/CAL960033), Jan 16, 1996: SKIN. CRACKED. IAH - FLT 1707 - INSPECTION FOUND A 5.25 INCH CRACK IN LEFT WING LEADING EDGE SKIN AT STA 242. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5730-01428. (X) - [SDR CAL950515](https://openairdocs.org/sdr/CAL950515), Jun 21, 1995: EEL BATTERIES. INOPERATIVE. FLT NR 0299 - EWR - INSPECTION FOUND THE INTERIOR EMERGENCY EXIT LIGHTS AT ROW 6-9 AND AT ENTRANCE TO COCKPIT DOOR INOPERATIVE. THE BATTERIES AT ROW 7 AND IN TH ## Other aircraft with N12811 - [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N12811-undated): Cessna 172M, S/N 17262281. Triennial form not returned --- 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.