# N10834: 1987 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: 49494 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: May 21, 1987 - Certificate issued: September 3, 1997 - Last registry action: October 18, 2005 - Mode S code: A0254A - 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/N10834 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=10834 - Page: https://openairdocs.org/deregistered/N10834-2007-06-01 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 (66, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0200495](https://openairdocs.org/sdr/CALA0200495), Oct 12, 2002: LONGERON. CRACKED. INSPECTION FOUND A 1" CRACK IN TAIL COMPARTMENT LONGERON 2R AT STA 1418. REPAIRED LONGERON IAW SRM 53-02, FIGURE 18. - [SDR CALA0200494](https://openairdocs.org/sdr/CALA0200494), Oct 12, 2002: FRAME. CRACKED. INSPECTION FOUND A 2" CRACK IN TAIL COMPARTMENT BELTFRAME AT STA 1418, L2R. REPAIRED FRAME IAW SRM 53-03, FIGURE 31A. - [SDR CALA0200490](https://openairdocs.org/sdr/CALA0200490), Oct 9, 2002: SKIN. DENTED. INSPECTION FOUND A DENT IN L/H FUSELAGE SKIN AFT OF FORWARD ENTRY DOOR. THE DENTED SKIN WAS REMOVED AND NEW SKIN WAS INSTALLED IAW SRM 53-04. - [SDR CALA0000957](https://openairdocs.org/sdr/CALA0000957), Jun 21, 2000: PAN. GOUGED. INSPECTION FOUND FORWARD CARGO DOOR TOP PAN FLANGE GOUGED AT STOP. THE GOUGED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW 51-10-02, 51-30-02, 51-10-03, AND - [SDR CALA0000953](https://openairdocs.org/sdr/CALA0000953), Jun 21, 2000: RETAINER. CRACKED. INSPECTION FOUND NR 1 ENGINE APRON FORWARD UPPER SUPPORT (RETAINER) BENT WITH A SIX INCH CRACK. THE RETAINER WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA0000952](https://openairdocs.org/sdr/CALA0000952), Jun 21, 2000: STRINGER. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN HORIZONTAL STABILIZER DOG HOUSE STRINGER. THE CRACKED AREA WAS REMOVED AND A NEW STRINGER WAS INSTALLED IAW SRM 51-30-2, 53-0 - [SDR CALA0000949](https://openairdocs.org/sdr/CALA0000949), Jun 20, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT FS 1174 - 1207, LBL 54. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 53-05, F - [SDR CALA0000948](https://openairdocs.org/sdr/CALA0000948), Jun 20, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 180, LBL 16 - 36. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-5. - [SDR CALA0000947](https://openairdocs.org/sdr/CALA0000947), Jun 20, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 180 - 208, LONGERON 18L. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-2, 51-1 - [SDR CALA0000946](https://openairdocs.org/sdr/CALA0000946), Jun 20, 2000: ATTACH ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN L-1 DOOR UPPER AFT INNER ATTACH ANGLE. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA0000945](https://openairdocs.org/sdr/CALA0000945), Jun 20, 2000: PANEL. CORRODED. INSPECTION FOUND LT LOWER FUEL PANEL NR 1363 CORRODED ON MOUNT FACE AND IN COUNTERSINK. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW MM 51-30-2. - [SDR CALA0000944](https://openairdocs.org/sdr/CALA0000944), Jun 20, 2000: SKIN. CRACKED. INSPECTION FOUND TWO 3 INCH CRACKS IN MID CARGO DOOR I/B SKIN. THE CRACKED AREA WAS REMOVED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 1 AND 51-10 - [SDR CALA0000942](https://openairdocs.org/sdr/CALA0000942), Jun 20, 2000: NUT PLATE. CORRODED. INSPECTION FOUND CORROSION AROUND AND UNDER NUT PLATES INSIDE AFT CARGO LOWER TORQUE BOX AT FS 1183, LONGERON 27R AND 28R. THE TORQUE BOX WAS REPAIRED IAW ECRA - [SDR CALA0000929](https://openairdocs.org/sdr/CALA0000929), Jun 20, 2000: SHEAR TIE. CORRODED. INSPECTION FOUND SHEAR TIE CORRODED AT STA 1287, LONGERON 30 TO 29R. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA0000928](https://openairdocs.org/sdr/CALA0000928), Jun 20, 2000: FRAME. CORRODED. INSPECTION FOUND AFT SIDE OF FRAME CORRODED AT STA 1309, LONGERON 30. THE CORRODED SECTION OF FRAME WAS REMOVED AND REPLACED IAW SRM 53-03, FIGURE 2A, SHEET 1, - [SDR CALA0000927](https://openairdocs.org/sdr/CALA0000927), Jun 20, 2000: STRUCTURE. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN RT MLG I/B DOOR AFT LOWER CORNER AT REPAIR DOUBLER. REMOVED AND REPLACED DOUBLER IAW SRM 51-30-1. - [SDR CALA0000920](https://openairdocs.org/sdr/CALA0000920), Jun 19, 2000: STRUCTURE. BENT. INSPECTION FOUND THE AFT LOWER CORNER OF AFT CARGO DOOR BENT. REPAIRED AREA IAW ECRA 5230-01557. - [SDR CALA0000919](https://openairdocs.org/sdr/CALA0000919), Jun 19, 2000: STOP. GOUGED. INSPECTION FOUND FORWARD CARGO DOOR FORWARD SEAL FLANGE DOOR STOPS A-E GOUGED. REPAIRED AREAS IAW ECRA 5330-02819. - [SDR CALA0000918](https://openairdocs.org/sdr/CALA0000918), Jun 19, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND LT CARGO TIE DOWN TRACK IN AFT PIT CORRODED AROUND CLIP NUT HOLES AT FS 1155 - 1320, LONGERON 27L. THE TIE DOWN TRACK WAS REMOVED AND REPLACED - [SDR CALA0000917](https://openairdocs.org/sdr/CALA0000917), Jun 19, 2000: PAN. GOUGED. INSPECTION FOUND AFT CARGO DOOR PAN GOUGED AT STOP NR 5 ON FORWARD EDGE AND AT STOP NR 4 ON AFT EDGE. BOTH AREAS WERE REPAIRED IAW ECRA 5330-02819. - [SDR CALA0000916](https://openairdocs.org/sdr/CALA0000916), Jun 19, 2000: SUPPORT BRACKET. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN SUPPORT AT TAIL COMPARTMENT RT SIDE IN CEILING JUST AFT OF FRAME STA 1380. THE CRACK WAS STOP DRILLED AND A STACKED ANGLE RE - [SDR CALA0000911](https://openairdocs.org/sdr/CALA0000911), Jun 16, 2000: SKIN. DENTED. INSPECTION FOUND AFT CARGO DOOR OUTER SKIN DENTED JUST ABOVE AFT ACCESS PANEL. THE DENTED AREA WAS CUT OUT IAW SRM 52-05, FIGURE 1 AND A REPAIR DOUBLER WAS INST - [SDR CALA0000906](https://openairdocs.org/sdr/CALA0000906), Jun 15, 2000: CHANNEL. CRACKED. INSPECTION FOUND SUPPORT CHANNELS CRACKED AT CENTER FLOOR PANEL BETWEEN FS 886 AND 946. THE CRACKS WERE 2 INCHES LONG. THE FLOOR PANEL WAS REMOVED IAW SRM 51-30 - [SDR CALA0000905](https://openairdocs.org/sdr/CALA0000905), Jun 15, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND MID CARGO RT TRACK AFT OF DOOR CORRODED UNDER NUT CLIPS AT FS 683 - 786, LONGERON 27R. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW - [SDR CALA0000904](https://openairdocs.org/sdr/CALA0000904), Jun 15, 2000: RIB. CRACKED. INSPECTION FOUND A 6 INCH CRACK IN RT WING L/E RIB AT TRACK NR 8, XRS 248. THE CRACK WAS STOP DRILLED IAW SRM 57-01, FIGURE 3. A REPAIR ANGLE WAS INSTALLED IAW - [SDR CALA0000902](https://openairdocs.org/sdr/CALA0000902), Jun 15, 2000: SKIN. DENTED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT STA 389, LONGERON 24L. THE SKIN WAS REPAIRED IAW SRM 53-04, SHEETS 12 & 20. - [SDR CALA0000901](https://openairdocs.org/sdr/CALA0000901), Jun 14, 2000: SKIN. CANNING. INSPECTION FOUND RIGHT FUSELAGE SKIN OIL CANNING AT STA 484, LONGERON 23R-24R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38. - [SDR CALA0000900](https://openairdocs.org/sdr/CALA0000900), Jun 14, 2000: SUPPORT BRACKET. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN EXTERNAL FUSELAGE LOWER SURFACE WING TO BODY FAIRING SUPPORT TEE AT FS 916. THE SUPPORT WAS REMOVED AND A REPLACEMENT SUPPOR - [SDR CALA0000897](https://openairdocs.org/sdr/CALA0000897), Jun 13, 2000: VANE. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN NR 2 RT FIXED VANE I/B LOWER SURFACE. REPAIRED AND BONDED DOUBLER WITH RIVETS IAW SRM 57-04 AND 51-71-00. - [SDR CALA0000896](https://openairdocs.org/sdr/CALA0000896), Jun 13, 2000: PAN. GOUGED. INSPECTION FOUND FORWARD CARGO DOOR FORWARD PAN FLANGE STOPS H-L GOUGED. THE GOUGED AREAS WERE TRIMMED OUT AND REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5330-0281 - [SDR CALA0000873](https://openairdocs.org/sdr/CALA0000873), Jun 13, 2000: SKIN. DENTED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED WITH A .5 INCH CRACK AT FS 315 BETWEEN LONGERON 22L AND 23L. THE DENT WAS BLENDED OUT IAW SRM 53-04, FIGURE 38. T - [SDR CALA0000865](https://openairdocs.org/sdr/CALA0000865), Jun 10, 2000: SKIN. CORRODED. INSPECTION FOUND LT AFT UPPER FUSELAGE SKIN CORRODED AROUND FASTENERS JUST BELOW DORSAL FIN AT STA 1429 - 1435. A REPAIR STRAP WAS INSTALLED IAW SRM 53-05, 51-1 - [SDR CALA0000864](https://openairdocs.org/sdr/CALA0000864), Jun 10, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND MID CARGO TIE DOWN TRACK CORRODED AT FS 595 - 785, LONGERON 27L. THE TIE DOWN TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, - [SDR CALA0000863](https://openairdocs.org/sdr/CALA0000863), Jun 10, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND SEAT TRACK CORRODED AT FS 1032 - 1309, RBL 24. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-2, 53-05, AND 51-10- - [SDR CALA0000850](https://openairdocs.org/sdr/CALA0000850), Jun 8, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND SEAT TRACK CORRODED AT FS 670, RBL 22.5. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-2, 53-05, FIGURE 4F, AND 51-10- - [SDR CALA0000849](https://openairdocs.org/sdr/CALA0000849), Jun 8, 2000: PAN. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN AFT CARGO DOOR PAN AT FORWARD DOOR CAM AREA. THE OLD DOUBLER WAS REMOVED AND A NEW DOOR PAN DOUBLER WAS INSTALLED IAW SRM 51- - [SDR CALA0000848](https://openairdocs.org/sdr/CALA0000848), Jun 8, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT FS 218 - 238. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4, 51-10-3, - [SDR CALA0000847](https://openairdocs.org/sdr/CALA0000847), Jun 8, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT FS 1088 - 1231. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 51-30-2, 51-30- - [SDR CALA0000842](https://openairdocs.org/sdr/CALA0000842), Jun 7, 2000: WEB. PUNCTURED. INSPECTION FOUND HOLE PUNCTURED IN RT CUSP WEB UNDER FLOOR SUPPORT AT FS 200, RBL 44. THE FLOOR SUPPORT WAS REMOVED IAW SRM 51-30-2. A DOUBLER AND FILLER WERE I - [SDR CALA0000841](https://openairdocs.org/sdr/CALA0000841), Jun 7, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT FS 1174 - 1207, LBL 54. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 53-05, F - [SDR CALA0000840](https://openairdocs.org/sdr/CALA0000840), Jun 7, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND SEAT TRACK LUGS CORRODED AT FS 378, RBL 22.5. THE SEAT TRACK WAS REMOVED AND NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 51-30-2, 51-10-4, AN - [SDR CALA0000839](https://openairdocs.org/sdr/CALA0000839), Jun 7, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 160 - 200, LBL 44.5 AND STA 180, LBL 16 - 36. THE FLOOR SUPPORTS WERE REMOVED AND NEW FLOOR SUPPORTS WERE INSTAL - [SDR CALA0000838](https://openairdocs.org/sdr/CALA0000838), Jun 7, 2000: MOUNT. CORRODED. INSPECTION FOUND G-2 GALLEY I/B FORWARD MOUNT FITTING CORRODED. THE FITTING WAS REMOVED AND AND NEW FITTING WAS INSTALLED IAW SRM 51-30-5. - [SDR CALA0000817](https://openairdocs.org/sdr/CALA0000817), Jun 2, 2000: ATTACH ANGLE. CRACKED. INSPECTION FOUND R-1 DOOR THRESHOLD AFT ATTACH ANGLE CRACKED AND CORRODED. THE ANGLE AND DOUBLER WERE REMOVED AND A NEW ANGLE AND DOUBLER WERE INSTALLED IAW SRM - [SDR CALA0000816](https://openairdocs.org/sdr/CALA0000816), Jun 2, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN STA 200 AND 250, LBL 18. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-3, - [SDR CALA0000815](https://openairdocs.org/sdr/CALA0000815), Jun 2, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT AT L-2 DOOR, STA 1155. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3. - [SDR CALA0000788](https://openairdocs.org/sdr/CALA0000788), Jun 1, 2000: RIB. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN I/B RIB OF RIGHT FLAP WEDGE ASSEMBLY NR 6. THE CRACK WAS DRILLED OUT AND A NEW RIB WAS INSTALLED IAW SRM 51-10-3, 51-30-2, AN - [SDR CALA9801347](https://openairdocs.org/sdr/CALA9801347), Jul 24, 1998: TAIL CONE. WARPED. THE FORCE REQUIRED TO RELEASE TAIL CONE DURING FUNCTIONAL CHECK WAS EXCESSIVE. THE TAIL CONE HUNG UP ON RIGHT SIDE LATCH PINS. A SERVICEABLE TAIL CONE WAS INSTA - [SDR CALA9801323](https://openairdocs.org/sdr/CALA9801323), Jul 23, 1998: SKIN. DENTED. INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 229-237 ABOVE CUSP LINE. A REPAIR WAS INSTALLED IAW ECRA 5330-02687. - [SDR CALA9801322](https://openairdocs.org/sdr/CALA9801322), Jul 22, 1998: BEAM. CORRODED. INSPECTION FOUND CORROSION ON MID BAG BIN Z BEAM AT THRESHOLD, STA 636-693. CORROSION WAS ALSO FOUND ON AFT BAG BIN Z BEAM AT THRESHOLD STA 1155-1212. REPAIRS W All 66: https://openairdocs.org/deregistered/N10834-2007-06-01/reports.md ## 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 19931231050279I](https://openairdocs.org/incident/19931231050279I), Dec 31, 1993: Doug DC982 (N10834), Boise, ID. NE2 engine shut down due to compressor stall. Diverted to Boise. Landed safely. - [Incident 19930402021749I](https://openairdocs.org/incident/19930402021749I), Apr 2, 1993: Doug DC982 (N10834), Seattle, WA. Engine flameout on NR2 engine. Center fuel tank pumps in off position. Turned pumps on. Restarted engine. ## Other aircraft with N10834 - [Cancelled 2010-03-04](https://openairdocs.org/deregistered/N10834-2010-03-04): Mooney M20, S/N 1189. Exported to Canada. Owner: Xxxx - [Cancelled 1939-05-17](https://openairdocs.org/deregistered/N10834-1939-05-17): Stinson JR. S, S/N 8028. Owner: [Denny Daitz Flying Corp](https://openairdocs.org/faa-owner/DENNY%20DAITZ%20FLYING%20CORP), [Long Island, NY](https://openairdocs.org/faa-place/NY/Long%20Island) - [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N10834-undated): Bell 412, S/N 33074 --- 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.