# N92874: 1982 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: 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: 49122 - Year built: 1982 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard - Airworthiness date: August 24, 1984 - Certificate issued: December 24, 1992 - Last registry action: January 23, 2013 - Mode S code: ACDF4C - 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/N92874 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=92874 - Page: https://openairdocs.org/deregistered/N92874-2013-03-21 From the FAA registry file of November 5, 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 (100, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0300589](https://openairdocs.org/sdr/CALA0300589), Oct 12, 2003: DOUBLER. CORRODED. INSPECTION FOUND INTERNAL DOUBLER FOR OUTFLOW VALVE CORRODED AT STA 1325 BETWEEN L21L AND L22L. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-02. - [SDR CALA0300333](https://openairdocs.org/sdr/CALA0300333), Jun 23, 2003: BATTERY PACK. INOPERATIVE. INSPECTION FOUND THE OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. THE BATTERY PACK WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD IAW MM 33-53-00, PAGE 407. - [SDR CALA0300270](https://openairdocs.org/sdr/CALA0300270), May 28, 2003: SLIDE. DISCHARGED. INSPECTION FOUND THE R-1 DOOR SLIDE PRESSURE LOW. THE EMERGENCY DOOR SLIDE WAS REMOVED AND REPLACED IAW MM 25-62-00. - [SDR CALA0200430](https://openairdocs.org/sdr/CALA0200430), Jul 25, 2002: SKIN. CRACKED. INSPECTION FOUND A 1/4" CRACK AT RIVET IN L-1 DOOR SKIN AND THE CORNER WAS BENT. THE CRACK WAS LOCATED AT THE UPPER AFT CORNER OF DOOR. A REPAIR DOUBLER WAS INS - [SDR CALA0200421](https://openairdocs.org/sdr/CALA0200421), Jul 19, 2002: SEAT TRACK. CORRODED. INSPECTION FOUND R/H I/B SEAT TRACK CORRODED AT STA 200-228. THE SEAT TRACK SECTION WAS REPLACED IAW SRM 53-05, FIGURE 4F, SHEET 1. - [SDR CALA0200405](https://openairdocs.org/sdr/CALA0200405), Jul 17, 2002: SEAT TRACK. CORRODED. INSPECTION FOUND L/H CENTER SEAT TRACK CORRODED AROUND FLOOR PANEL MOUNT HOLES BETWEEN STA 1136 AND 1174. A NEW SEAT TRACK SECTION WAS INSTALLED IAW SRM 53-05. - [SDR CALA0200401](https://openairdocs.org/sdr/CALA0200401), Jul 15, 2002: SEAT TRACK. CORRODED. INSPECTION FOUND R/H I/B SEAT TRACK CORRODED AT STA 200-228. THE CORRODED SECTION OF SEAT TRACK WAS REPLACED IAW SRM 53-05, FIGURE 4F, SHEET 1. - [SDR CALA0200141](https://openairdocs.org/sdr/CALA0200141), Mar 19, 2002: FAN. OVERHEATED. THE FLIGHT ATTENDANT REPORTED AN ELECTRICAL SMOKE ODOR APPARENTLY COMING FROM THE RIGHT AFT LAV AREA AFTER TAKEOFF FROM MIA. THE AIRCRAFT WAS RETURNED TO MIA WH - [SDR CALA0100655](https://openairdocs.org/sdr/CALA0100655), Jul 14, 2001: CHARGER. INOPERATIVE. INSPECTION FOUND EMERGENCY AISLE PATH LIGHTING IN CENTER OF AIRCRAFT INOPERATIVE. THE EMERGENCY BATTERY CHARGER NEAR TOP BEACON WAS REMOVED AND REPLACED AND OPE - [SDR CALA0100566](https://openairdocs.org/sdr/CALA0100566), Jun 21, 2001: INTERCOSTAL. CORRODED. INSPECTION FOUND FIVE INTERCOSTALS CORRODED INSIDE TORQUE BOX AT AFT CARGO PIT AREA, FS 1165 - 1203. THE INTERCOSTALS WERE REMOVED AND NEW INTERCOSTALS WERE INS - [SDR CALA0100565](https://openairdocs.org/sdr/CALA0100565), Jun 21, 2001: SKIN. GOUGED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN GOUGED AFT OF R-1 DOOR GUST LOCK. THE GOUGED AREA WAS REMOVED. SKIN FILLER AND REPAIR DOUBLERS WERE INSTALLED IAW SRM 53 - [SDR CALA0100540](https://openairdocs.org/sdr/CALA0100540), Jun 12, 2001: SKIN. DENTED. INSPECTION FOUND LEFT I/B FLAP LOWER SKIN SURFACE DENTED. THE LEFT I/B FLAP PANEL WAS REMOVED AND NEW SKIN WAS INSTALLED IAW SRM 51-50-14, 51-10-3, 51-50-20, AN - [SDR CALA0100539](https://openairdocs.org/sdr/CALA0100539), Jun 12, 2001: INTERCOSTAL. CORRODED. INSPECTION FOUND MID CARGO INTERCOSTAL CORRODED AT FS 769-788 BETWEEN LONGERONS 27R AND 28R. PANEL 2214C WAS REMOVED IAW SRM 51-30-01. THE INTERCOSTAL WAS REMOV - [SDR CALA0100537](https://openairdocs.org/sdr/CALA0100537), Jun 10, 2001: WEB. CORRODED. INSPECTION FOUND AFT CARGO PIT TORQUE BOX WEB CORRODED. THE TORQUE BOX WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-5. - [SDR CALA0100536](https://openairdocs.org/sdr/CALA0100536), Jun 7, 2001: DOOR FRAME. CORRODED. INSPECTION FOUND FORWARD CARGO DOOR FORWARD JAMB UPPER WEB CORRODED. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-30-5. - [SDR CALA0100534](https://openairdocs.org/sdr/CALA0100534), Jun 6, 2001: ANGLE. CORRODED. INSPECTION FOUND CUSP ANGLE CORRODED AT FS 200, RBL 54. THE R-1 DOOR, FRAME FITTING, AND CUSP ANGLE WERE REMOVED IAW MM 52-41-00, SRM 51-30-05, AND 53-05, FIGUR - [SDR CALA0100533](https://openairdocs.org/sdr/CALA0100533), Jun 3, 2001: FRAME. CORRODED. INSPECTION FOUND TAIL COMPARTMENT LT SIDE CANTED FRAME GOUGED AT FS 1463. THE CORROSION WAS REMOVED AND REPAIR ANGLES WERE INSTALLED IAW SRM 51-30-5, 53-01, FIG - [SDR CALA0100532](https://openairdocs.org/sdr/CALA0100532), Jun 3, 2001: WEB. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN L1 DOOR TORQUE BOX WEB AFT OF TANG AT LONGERON 15L. THE FASTENERS WERE REMOVED, TANGS TRIMMED, AND FILLER AND DOUBLER WERE IN - [SDR CALA0100531](https://openairdocs.org/sdr/CALA0100531), Jun 3, 2001: FLOORBEAM. CORRODED. INSPECTION FOUND AFT CARGO FLOORBEAM AND NUT PLATES CORRODED AT FS 1338. THE UPPER L-ANGLE ON FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-05, 51-30-01, 51-30- - [SDR CALA0100530](https://openairdocs.org/sdr/CALA0100530), Jun 3, 2001: SKIN. DENTED. INSPECTION FOUND RT WING EXTERNAL SURFACE OF ZERO SLAT SKIN DENTED I/B OF THE DRIVE TRACK. THE SLAT WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-80-01, EA 9 - [SDR CALA0100529](https://openairdocs.org/sdr/CALA0100529), Jun 2, 2001: STRAP. CORRODED. INSPECTION FOUND AFT CARGO DOOR JAMB TORQUE BOX FWD STRAP CORRODED. THE FORWARD STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 53-01, FIGURE 1, 51-10-4 - [SDR CALA0100528](https://openairdocs.org/sdr/CALA0100528), Jun 2, 2001: FLOORBEAM. CORRODED. INSPECTION FOUND AFT CARGO CABIN FLOORBEAM AND NUT PLATES CORRODED AT FS 1322. THE FLOORBEAM WAS REPAIRED IAW SRM 53-05 AND 53-05, FIGURE 20A. - [SDR CALA0100527](https://openairdocs.org/sdr/CALA0100527), Jun 2, 2001: BEAM. CORRODED. INSPECTION FOUND AFT CARGO DOOR JAMB BEAM CORRODED. THE LOWER DOOR JAMB BEAM WAS REMOVED AND A NEW LOWER DOOR JAMB BEAM WAS INSTALLED USING A DOUBLER AND SPACER - [SDR CALA0100524](https://openairdocs.org/sdr/CALA0100524), May 31, 2001: FRAME. CORRODED. INSPECTION FOUND MID CARGO FRAME CORRODED AT FS 541 BETWEEN LONGERONS 26R AND 26L. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGUR - [SDR CALA0100523](https://openairdocs.org/sdr/CALA0100523), May 30, 2001: FRAME. CORRODED. INSPECTION FOUND MID CARGO FRAME CORRODED AT FS 560 BETWEEN LONGERONS 26R AND 26L. THE CORRODED SECTION OF FRAME WAS REMOVED AND A Z-FRAME REPAIR SPLICE WAS INS - [SDR CALA0100522](https://openairdocs.org/sdr/CALA0100522), May 30, 2001: SUPPORT. CRACKED. INSPECTION FOUND AFT CARGO FALSE BULKHEAD LOWER SUPPORTS CORRODED AND CRACKED AT FS 1007, LONGERON 28L AND 28R. BOTH SUPPORTS WERE REMOVED AND NEW SUPPORTS WERE - [SDR CALA0100521](https://openairdocs.org/sdr/CALA0100521), May 30, 2001: SKIN. DAMAGED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN CREASED AT FS 230 BETWEEN LONGERON 17L AND 18L. THE SKIN WAS REPAIRED IAW ECRA 5330-02445. - [SDR CALA0100520](https://openairdocs.org/sdr/CALA0100520), May 29, 2001: FLOORBEAM. CORRODED. INSPECTION FOUND AFT CARGO OVERHEAD FLOORBEAM CORRODED ON NUT PLATES AND EXFOLIATION CORROSION ON RT SIDE AT FS 1309. THE FLOORBEAM WAS REMOVED AND A NEW FLOORB - [SDR CALA0100519](https://openairdocs.org/sdr/CALA0100519), May 29, 2001: SUPPORT. CORRODED. INSPECTION FOUND MID CARGO SUPPORT CORRODED AT FS 750 BETWEEN LONGERONS 29L AND 29R. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW 51-30-5, 51-10- - [SDR CALA0100518](https://openairdocs.org/sdr/CALA0100518), May 29, 2001: FRAME. CORRODED. INSPECTION FOUND AFT CARGO FRAME CORRODED AT FS 1117, LONGERON 30. THE CORRODED SECTION OF FRAME WAS REMOVED AND A NEW FRAME SECTION WAS INSTALLED IAW SRM 51-30 - [SDR CALA0100517](https://openairdocs.org/sdr/CALA0100517), May 29, 2001: CARGO TRACK. CORRODED. INSPECTION FOUND MID CARGO RT TIE DOWN TRACK CORRODED BETWEEN FS 693 AND 788. THE CARGO TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-01, 51-10- - [SDR CALA0100516](https://openairdocs.org/sdr/CALA0100516), May 29, 2001: DOOR FRAME. CORRODED. INSPECTION FOUND MID CARGO DOOR LOWER JAMB BEAM CORRODED AROUND RIVNUTS. THE DOOR JAMB WAS REPAIRED IAW ECRA 5310-03027. - [SDR CALA0100512](https://openairdocs.org/sdr/CALA0100512), May 26, 2001: WEB. CORRODED. INSPECTION FOUND CUSP WEB CORRODED AT FS 200 - 207, RBL 56. THE CUSP WEB WAS REMOVED AND A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-01, FIGURE 1, 51- - [SDR CALA0100511](https://openairdocs.org/sdr/CALA0100511), May 26, 2001: WEB. CRACKED. INSPECTION FOUND MAIN CABIN CUSP WEB CRACKED IN SEVERAL PLACES AT FS 1280, RBL 54. THE CRACKS WERE APPROXIMATELY 1 INCH LONG. FLOOR PANELS WERE REMOVED TO GAIN - [SDR CALA0100510](https://openairdocs.org/sdr/CALA0100510), May 26, 2001: WEB. CORRODED. INSPECTION FOUND MAIN CABIN CUSP WEB CORRODED AT FS 160 - 200, RBL 56. THE CORRODED AREA WAS CUT OUT IAW SRM 53-01, FIGURE 3. A REPAIR DOUBLER AND FILLER WERE I - [SDR CALA0100509](https://openairdocs.org/sdr/CALA0100509), May 26, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED ON UPPER AND LOWER SURFACE IN MID CARGO AREA AT FS 636, LONGERON 28R-29R. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR - [SDR CALA0100508](https://openairdocs.org/sdr/CALA0100508), May 26, 2001: SUPPORT. CORRODED. INSPECTION FOUND SUPPORT CORRODED AT AFT LT SIDE OF WEB AT CUSP AREA, STA 1309. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-1 - [SDR CALA0100506](https://openairdocs.org/sdr/CALA0100506), May 25, 2001: SKIN. DENTED. INSPECTION FOUND LT EXTERNAL FUSELAGE SKIN DENTED AT FS 195, LONGERON 23L. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38. - [SDR CALA0100505](https://openairdocs.org/sdr/CALA0100505), May 25, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND MAIN CABIN FLOOR SUPPORT CORRODED AT FS 160-200, RBL 56. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-4, 51-30-3 - [SDR CALA0100504](https://openairdocs.org/sdr/CALA0100504), May 25, 2001: SKIN. GOUGED. INSPECTION FOUND RT INTERNAL FUSELAGE SKIN GOUGED AT FS 1429. THE AREA WAS BLENDED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, 51-10-3, 51-10-4, AND 51-30 - [SDR CALA0100503](https://openairdocs.org/sdr/CALA0100503), May 24, 2001: SKIN. DENTED. INSPECTION FOUND RT MLG DOOR EXTERNAL SKIN DENTED IN TWO PLACES 7 INCHES APART I/B OF DOOR SKID. A REPAIR PATCH WAS INSTALLED IAW SRM 52-01, FIGURE 2 AND 51-30- - [SDR CALA0100502](https://openairdocs.org/sdr/CALA0100502), May 24, 2001: SKIN. DENTED. INSPECTION FOUND RT EXTERNAL FUSELAGE SKIN DENTED BETWEEN FS 313 - 332, LONGERON 20-21R. THE EXISTING DOUBLER WAS REMOVED IAW SRM 51-30-05 AND 51-30-02. THE DEN - [SDR CALA0100501](https://openairdocs.org/sdr/CALA0100501), May 24, 2001: SKIN. DENTED. INSPECTION FOUND LT EXTERNAL FUSELAGE SKIN DENTED AT FS 233, LONGERON 23L. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-4 AND 51-30-2. - [SDR CALA0100493](https://openairdocs.org/sdr/CALA0100493), May 22, 2001: SKIN. DENTED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AND CREASED AT FS 322, LONGERON 25R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, 51-10-4, AND 51-10- - [SDR CALA0100492](https://openairdocs.org/sdr/CALA0100492), May 22, 2001: SKIN. DENTED. INSPECTION FOUND THE EXTERNAL FUSELAGE SKIN DENTED AT FS 340, LONGERON 24L. THE DENTED AREA WAS REFORMED AND A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38. - [SDR CALA0100491](https://openairdocs.org/sdr/CALA0100491), May 22, 2001: SKIN. DAMAGED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN CREASED AT FS 312, LONGERON 24L. THE SKIN WAS COLD WORKED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-2, 53-04, FIGURE 38, - [SDR CALA0100489](https://openairdocs.org/sdr/CALA0100489), May 21, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND CABIN CENTER FLOOR PANEL DELAMINATED AT FS 905 - 946. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW ECRA 5100-01844. - [SDR CALA0100486](https://openairdocs.org/sdr/CALA0100486), May 21, 2001: FLOOR PANEL. CRACKED. INSPECTION FOUND CABIN CENTER FLOOR PANEL CRACKED AT FS 905-946. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-2 AND 51-30-8. - [SDR CALA0100484](https://openairdocs.org/sdr/CALA0100484), May 20, 2001: WEB. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN CUSP WEB AT FS 237, RBL 56. THE CUSP WEB WAS REMOVED AND THE CRACK WAS STOP DRILLED IAW SRM 51-30-2 AND 53-01, FIGURE 2. A RE - [SDR CALA0100482](https://openairdocs.org/sdr/CALA0100482), May 20, 2001: FLOOR SUPPORT. CRACKED. INSPECTION FOUND CABIN RT I/B FLOOR SUPPORT CORRODED WITH A 1.5 INCH EDGE CRACK AT FS 210. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED I All 100: https://openairdocs.org/deregistered/N92874-2013-03-21/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 19960807030759I](https://openairdocs.org/incident/19960807030759I), Aug 7, 1996: Doug DC982 (N92874), Cleveland, OH, Minor damage. Narrative: aircraft lost hydraulic pressure in cruise flight on right system. Flight crew manually extended the landing gear and landed in Cleveland without… ## Other aircraft with N92874 - [Cancelled 1990-04-25](https://openairdocs.org/deregistered/N92874-1990-04-25): Cessna A188B, S/N 18802074T. N-number assigned, not yet registered --- 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.