# N57837: 1987 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2005-07-05 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 5, 2005 - Exported to: Indonesia - 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: 49582 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: October 1, 1987 - Certificate issued: April 22, 1998 - Last registry action: November 7, 2002 - Mode S code: A76F02 - 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/N57837 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=57837 - Page: https://openairdocs.org/deregistered/N57837-2005-07-05 From the FAA registry file of October 31, 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 (29) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0100658](https://openairdocs.org/sdr/CALA0100658), Jul 17, 2001: BATTERY. DISCHARGED. INSPECTION FOUND THE OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 22-26. THE EMERGENCY LIGHT BATTERIES WERE REMOVED AND REPLACED IAW MM 33-53-00 AND OPERATION - [SDR CALA9900686](https://openairdocs.org/sdr/CALA9900686), Jun 16, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND THE LEFT O/B SEAT TRACK CORRODED FROM STA 1174-1202, LBL 48. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 53-05-04. - [SDR CALA9900685](https://openairdocs.org/sdr/CALA9900685), Jun 16, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT CENTER SEAT TRACK CORRODED FROM STA 1200-1215, LBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1. - [SDR CALA9900684](https://openairdocs.org/sdr/CALA9900684), Jun 16, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND THE LEFT I/B SEAT TRACK CORRODED FROM STA 1117-1136, LBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-30-2. - [SDR CALA9900683](https://openairdocs.org/sdr/CALA9900683), Jun 16, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND THE RIGHT O/B SEAT TRACK CORRODED IN TWO PLACES AT STA 210 & 229, RBL 48. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND SRM 53-05 - [SDR CALA9900682](https://openairdocs.org/sdr/CALA9900682), Jun 16, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED IN TWO PLACES AT STA 210 AND 229, RBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 53-05, FIGU - [SDR CALA9900681](https://openairdocs.org/sdr/CALA9900681), Jun 15, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED FROM STA 1271-1300, LBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1. - [SDR CALA9900680](https://openairdocs.org/sdr/CALA9900680), Jun 15, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND THE RIGHT O/B SEAT TRACK CORRODED FROM STA 598-760, RBL 48. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4, VIEW E. - [SDR CALA9900679](https://openairdocs.org/sdr/CALA9900679), Jun 15, 1999: CARGO TRACK. CORRODED. INSPECTION FOUND AFT CARGO RT FRAME TRACK CORRODED AT FS 1022-1155, LONGERON 27R. THE CARGO TRACK WAS REMOVED AND REPLACED IAW SRM 53-24-0. - [SDR CALA9900678](https://openairdocs.org/sdr/CALA9900678), Jun 15, 1999: JAMB. CORRODED. INSPECTION FOUND AFT CARGO COMPARTMENT LOWER DOOR JAMB AT THRESHOLD CORRODED THE ENTIRE LENGTH AT FS 1111-1251, LONGERON 28R. THE BEAM WAS REMOVED AND REPLACED - [SDR CALA9900677](https://openairdocs.org/sdr/CALA9900677), Jun 15, 1999: FRAME. CRACKED. INSPECTION FOUND THE LEFT I/B MLG DOOR CRACKED AT FORWARD AND LOWER FRAME. THE CRACKS WERE .5 ICNH LONG. THE DOOR FRAME WAS REPAIRED IAW ECRA 5280-01200. - [SDR CALA9900676](https://openairdocs.org/sdr/CALA9900676), Jun 15, 1999: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 239 BETWEEN LONGERON 17L AND 18L. A NEW DOUBLER WAS INSTALLED IAW SRM 53-30-05. - [SDR CALA9900661](https://openairdocs.org/sdr/CALA9900661), Jun 9, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND SEAT TRACK CORRODED AT STA 1212, LBL 60. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-20-3. - [SDR CALA9900660](https://openairdocs.org/sdr/CALA9900660), Jun 9, 1999: FRAME. GOUGED. INSPECTION FOUND FRAME GOUGED AT FS 1437 BETWEEN LONGERON 2L AND 2R. REPAIRED IAW SRM 51-30-5. - [SDR CALA9900658](https://openairdocs.org/sdr/CALA9900658), Jun 8, 1999: BEAM. CORRODED. INSPECTION FOUND MID CARGO DOOR BEAM CORRODED AT FS 617-674 LONGERON 28R. THE MID CARGO DOOR BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-05. - [SDR CALA9900003](https://openairdocs.org/sdr/CALA9900003), Jan 2, 1999: SWITCH. INOP. THE LT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF. THE GEAR WAS CYCLED, BUT THE LIGHT DID NOT EXTINGUISH. THE FLIGHT WAS CONTINUED TO EWR WHERE IT - [SDR CALA9801598](https://openairdocs.org/sdr/CALA9801598), Sep 1, 1998: HYD LINE. LEAKING. THE RT HYDRAULIC PRESSURE LOW LIGHT AND MANUAL RUDDER CONTROL LIGHT ILLUMINATED DURING CLIMB OUT OF ANC. THE RT HYDRAULIC PUMP PRESSURE WAS ZERO WITH QUANTITY D - [SDR CALA9700976](https://openairdocs.org/sdr/CALA9700976), Jun 28, 1997: LAMP. FAILED. THE RT MLG GREEN INDICATION LIGHT DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED ON APPROACH. THE ALTERNATE GEAR EXTENSION HANDLE WAS PULLED, BUT THE LIGHT DID NOT C - [SDR CALA9700740](https://openairdocs.org/sdr/CALA9700740), May 8, 1997: STRAP. CORRODED. INSPECTION FOUND STRAP OVER BELTFRAME CORRODED AT STA 1231. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-30-5. - [SDR CALA9700739](https://openairdocs.org/sdr/CALA9700739), May 8, 1997: SUPPORT. CORRODED. INSPECTION FOUND CENTER FLOOR SUPPORT CORRODED AT STA 1212. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA9700280](https://openairdocs.org/sdr/CALA9700280), Feb 25, 1997: DOOR. IMPACTED. THE LEFT LOWER CORNER OF L-1 DOOR WAS DAMAGED WHEN STRUCK BY JETWAY. THE DOOR WAS REPAIRED IAW SRM 52-05, FIGURE 32. - [SDR CALA9601264](https://openairdocs.org/sdr/CALA9601264), Sep 4, 1996: HYD LINE. LEAKING. THE AIRCRAFT LOST RT HYDRAULIC SYSTEM QUANTITY AND PRESSURE ON APPROACH TO SEA. ALTERNATE GEAR EXTENSION WAS USED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAIN - [SDR CALA9600939](https://openairdocs.org/sdr/CALA9600939), Jul 1, 1996: GENERATOR. INOPERATIVE. THE APU GENERATOR FAILED, WHILE OPERATING THE APU WITH THE NR 1 GENERATOR PLACARDED INOPERATIVE, EN ROUTE. THE FAILURE WAS ACCOMPANIED BY ILLUMINATION OF THE FE - [SDR CAL960621](https://openairdocs.org/sdr/CAL960621), May 20, 1996: SEALS. LEAKING. FLT NR 1891 - MSY - THE NR 2 ENG OIL QTY INDICATOR DROPPED TO ZERO WHILE EN ROUTE FROM TPA TO IAH. THE OIL PRESSURE DROPPED BELOW 35 SPI. THE NR 2 ENGINE WAS SH - [SDR CAL960335](https://openairdocs.org/sdr/CAL960335), Mar 18, 1996: ANTIICE DUCT. BLOWN. OCA - FLT 0611 - THE NR 2 ENGINE HAD A FIRE WARNING SHORTLY AFTER TAKEOFF FROM DCA. ACFT WAS RETURNED TO DCA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND - [SDR CAL960184](https://openairdocs.org/sdr/CAL960184), Feb 20, 1996: DNLOCK SENSOR. INOPERATIVE. FLT NR 498 - BOS - THE A/C HAD A BRIEF HISTORY OF THE RIGHT MLG RED LIGHT REMAINING ILLUMINATED AFTER GEAR RETRACTION. WHEN GEAR WAS EXTENDED FOR LANDING THE GR - [SDR CAL950871](https://openairdocs.org/sdr/CAL950871), Oct 1, 1995: SKIN. PUNCTURED. CLE - FLT 0286 - THE JETWAY PUNCTURED FUSELAGE SKIN AFT OF FORWARD ENTRY DOOR ATER ARRIVAL AT CLE. THE PUNCTURE WAS LOCATED AT STA 207, LONGERON 17L, AND WAS AP - [SDR CAL950311](https://openairdocs.org/sdr/CAL950311), Apr 22, 1995: SLIDE. FELL OFF. FLT NR 0274 - IAH - L-1 DOOR SLIDE FELL OFF. MAINTENANCE REINSTALLED PRIOR TO DISPATCH. NO FURTHER DISCREPANCIES. OK FOR DEPARTURE. (W) - [SDR CAL950295](https://openairdocs.org/sdr/CAL950295), Apr 18, 1995: POWER SUPPLY. INOPERATIVE. DCA - FLT 0799 - INSPECTION FOUND BOTH OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK AND OPERATION OF THE OVERWING E ## 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 19891205061599I](https://openairdocs.org/incident/19891205061599I), Dec 5, 1989: Doug DC982 (N57837), San Francisco, CA, Minor damage. Tail cone fell off aircraft on landing. Escape slide failed to deploy. ## Other aircraft with N57837 - [Cancelled 1955-10-11](https://openairdocs.org/deregistered/N57837-1955-10-11): Cessna T-50, S/N 5854. Owner: [Bouslog Bryant M](https://openairdocs.org/faa-owner/BOUSLOG%20BRYANT%20M), [Marion, IN](https://openairdocs.org/faa-place/IN/Marion) --- 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.