# N76823: 1986 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2005-09-06 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 6, 2005 - Exported to: Ukraine - 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: 49483 - Year built: 1986 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: October 16, 1986 - Certificate issued: April 21, 1998 - Last registry action: November 13, 2002 - Mode S code: AA61FA - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N76823 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=76823 - Page: https://openairdocs.org/deregistered/N76823-2005-09-06 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 (26) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0100703](https://openairdocs.org/sdr/CALA0100703), Jul 27, 2001: DOOR FRAME. CORRODED. INSPECTION FOUND FORWARD CARGO DOOR LOWER JAMB CORRODED UNDER DOOR STOPS AT STA 389-408. THE DOOR JAMB WAS REPAIRED IAW ECRA 5310-04165. - [SDR CALA0100695](https://openairdocs.org/sdr/CALA0100695), Jul 26, 2001: PLATE. CORRODED. INSPECTION FOUND I/B AND O/B LEFT VERTICAL STABILIZER SUPPORT PLATES FOR HORIZONTAL STABILIZER PIVOT BOLT CORRODED IN AND AROUND BOLT HOLES. THE SUPPORT PLATES - [SDR CALA0100694](https://openairdocs.org/sdr/CALA0100694), Jul 26, 2001: SILL. CORRODED. INSPECTION FOUND AFT CARGO DOOR JAMB SILL CORRODED AT STA 1155-1212. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 63. - [SDR CALA0100678](https://openairdocs.org/sdr/CALA0100678), Jul 25, 2001: SPAR. CORRODED. INSPECTION FOUND LT HORIZONTAL STABILIZER FORWARD UPPER SPAR AFT BARREL NUT HOLE AND BOLT HOLE CORRODED. REPAIRS WERE PERFORMED IAW ECRA 5511-01061. - [SDR CALA0100673](https://openairdocs.org/sdr/CALA0100673), Jul 24, 2001: PLATE. CORRODED. INSPECTION FOUND I/B AND O/B RT VERTICAL STABILIZER SUPPORT PLATES CORRODED. THE I/B AND O/B RT VERTICAL STABILIZER SUPPORT PLATES WERE REMOVED AND REPLACED IAW - [SDR CALA0100660](https://openairdocs.org/sdr/CALA0100660), Jul 19, 2001: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 218 JUST ABOVE LONGERON 19L. THE SKIN WAS REPAIRED IAW SRM 53-04, PAGE 218K. - [SDR CALA9901060](https://openairdocs.org/sdr/CALA9901060), Aug 16, 1999: WIRE. BROKEN. INSPECTION FOUND EMERGENCY LIGHT AT ROW 6DEF INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE UNDER SEAT AND OPERATION CHECKED GOOD. - [SDR CALA9900234](https://openairdocs.org/sdr/CALA9900234), Mar 8, 1999: MEMBRANE. CORRODED. INSPECTION FOUND AFT CARGO LEFT TUNNEL CUSP MEMBRANE CORRODED AT STA 1155 TO 1174. THE MEMBRANE WAS REPLACED IAW SRM 51-30-2. - [SDR CALA9900233](https://openairdocs.org/sdr/CALA9900233), Mar 8, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT STA 1079 TO 1231. A NEW SEAT TRACK SECTION WAS INSTALLED IAW SRM 53-05, FIGURE 4F. - [SDR CALA9900232](https://openairdocs.org/sdr/CALA9900232), Mar 8, 1999: WEB. CRACKED. INSPECTION FOUND A 1 INCH CRACK AT AFT WEB PLATE LIGHTENING HOLE BETWEEN NR 6 AND NR 7 BEAMS OF MAIN CABIN DOOR. THE AREA WAS REPAIRED IAW SRM 51-30-1, 51-30-2, - [SDR CALA9900229](https://openairdocs.org/sdr/CALA9900229), Mar 6, 1999: RELEASE MECH. FAILED TEST. THE TAIL CONE RELEASE PULL WAS LOW AT 15 POUNDS DURING TEST. THE TAIL CONE WAS REMOVED AND A NEW TAIL CONE WAS INSTALLED AND RIGGED IAW MM 53-53-00. OPERATIONAL - [SDR CALA9900217](https://openairdocs.org/sdr/CALA9900217), Mar 4, 1999: BEAM. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN RADIUS OF MAIN CABIN DOOR INTERIOR BEAM NR 2 FLANGE AFT END. REPAIRED BEAM IAW SRM 52-05, FIGURE 31, SHEET 3. - [SDR CALA9900213](https://openairdocs.org/sdr/CALA9900213), Mar 3, 1999: LONGERON. CORRODED. INSPECTION FOUND LONGERON 30 CORRODED IN E & E COMPARTMENT AT STA 180. THE CORRODED SECTION OF LONGERON WAS REPLACED IAW SRM 51-10-3. - [SDR CALA9900210](https://openairdocs.org/sdr/CALA9900210), Mar 2, 1999: WEB. CORRODED. INSPECTION FOUND E & E COMPARTMENT WEB MEMBRANE CORRODED AT STA 200, RT SIDE. THE AREA WAS REPAIRED IAW ECRA 5305-01049 AND SRM 53-05, FIGURE 55. - [SDR CALA9900202](https://openairdocs.org/sdr/CALA9900202), Feb 27, 1999: FRAME. CORRODED. INSPECTION FOUND NR 15L CABIN WINDOW FRAME CORRODED AT STA 419. THE WINDOW FRAME SECTION WAS REMOVED AND REPLACED IAW SRM 51-10-3. - [SDR CALA9900191](https://openairdocs.org/sdr/CALA9900191), Feb 24, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND RT INBOARD SEAT TRACK CORRODED AT STA 226 TO 232. THE CORRODED SEAT TRACK SECTION WAS REMOVED AND REPLACED IAW SRM 53-05. - [SDR CALA9900190](https://openairdocs.org/sdr/CALA9900190), Feb 22, 1999: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AFT OF L-1 DOOR BETWEEN STA 229 AND 237 ABOVE LONGERON 18. A REPAIR WAS INSTALLED IAW ECRA 5330-02445. - [SDR CALA9700315](https://openairdocs.org/sdr/CALA9700315), Mar 3, 1997: BULKHEAD TEE CAP. CORRODED. INSPECTION FOUND CORROSION ON BULKHEAD TEE CAP AT STA 110, LONGERON 29L. THE CORRODED AREA OF TEE CAP WAS CUT OUT, A REPAIR WAS INSTALLED IAW ECRA 5310-03443, S - [SDR CALA9700317](https://openairdocs.org/sdr/CALA9700317), Mar 2, 1997: CHANNEL. CORRODED. INSPECTION FOUND MID BAGGAGE BIN THRESHOLD Z-CHANNEL CORRODED. THE CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-30-0. - [SDR CALA9601685](https://openairdocs.org/sdr/CALA9601685), Nov 18, 1996: BATTERIES. DISCHARGED. INSPECTION FOUND THE EMERGENCY CEILING LIGHT INOPERATIVE AT ROW 12 TO 16. THE BATTERIES WERE REPLACED AND OPERATION OF THE LIGHT WAS RESTORED. - [SDR CALA9601684](https://openairdocs.org/sdr/CALA9601684), Nov 18, 1996: BATTERIES. DISCHARGED. INSPECTION FOUND THE CEILING EMERGENCY LIGHT INOPERATIVE AT ROW 28 TO 30. THE BATTERIES WERE REPLACED AND OPERATION OF THE LIGHT WAS RESTORED. - [SDR CALA9601683](https://openairdocs.org/sdr/CALA9601683), Nov 18, 1996: FUSE. BLOWN. INSPECTION FOUND THE EMERGENCY EXIT LOCATOR SIGN AT AFT GALLEY DOOR INOPERATIVE. MAINTENANCE FOUND A BLOWN FUSE IN POWER SUPPLY. THE FUSE WAS REPLACED AND OPERA - [SDR CALA9600840](https://openairdocs.org/sdr/CALA9600840), Jun 16, 1996: OVEN. CONTAMINATED. THE FLIGHT ATTENDANT SAW SMOKE COMING FROM RT OVEN IN FORWARD GALLEY WHILE IN FLIGHT. THE SMOKE CEASED AFTER USING A HALON AND WATER FIRE EXTINGUISHER AND PULLI - [SDR CAL960371](https://openairdocs.org/sdr/CAL960371), Mar 19, 1996: T3 BLADE. BROKEN. THE AIRCRAFT REJECTED TAKEOFF AT HIGH SPEED AFTER THE NR 2 ENGINE FAILED. THE ENGINE FAILURE WAS ACCOMPANIED BY A LOUD POP AND LOW N1. MAINTENANCE FOUND BLADES - [SDR CAL960305](https://openairdocs.org/sdr/CAL960305), Mar 12, 1996: CSD SPLINES. DAMAGED. MSY - FLT 1783 - THE LT GENERATOR TRIPPED OFF WHILE EN ROUTE FROM DCA TO IAH. ACFT DESCENDED TO FL 240 AND CREW MADE AN UNSUCCESSFUL ATTEMPT TO START APU. AT TH - [SDR CAL951037](https://openairdocs.org/sdr/CAL951037), Nov 12, 1995: RETRACT MECH. MALFUNCTIONED. ANC - FLT 0662 - THE LANDING GEAR RED UNSAFE LIGHTS AND THE GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED WITH LANDING GEAR NOISE AND VIBRATION AFTER THE GEAR HANDL ## 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 19960319010079I](https://openairdocs.org/incident/19960319010079I), Mar 19, 1996: Doug DC982 (N76823), Cleveland, OH. Narrative: flight crew aborted takeoff at 50 knots after hearing and feeling a thud from the right side of the aircraft. Abort was normal, reversers deployed… - [Incident 19941020045779I](https://openairdocs.org/incident/19941020045779I), Oct 20, 1994: Doug DC982 (N76823), Seattle, WA, Minor damage. During gate pushback. Tail struck food service truck. Damaged left trailing edge flap. --- 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.