# N14839: 1987 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2008-07-16 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 16, 2008 - 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: 49635 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: November 4, 1987 - Certificate issued: September 19, 2006 - Last registry action: September 19, 2006 - Mode S code: A0C34B - 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/N14839 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14839 - Page: https://openairdocs.org/deregistered/N14839-2008-07-16 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 (74, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0300499](https://openairdocs.org/sdr/CALA0300499), Aug 26, 2003: STRUT. LOW. THE NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM LAS. RECYCLING THE GEAR DID NOT HELP. THE AIRCRAFT WAS RETURNED TO LAS WHERE IT LANDED WITHOUT INCIDENT. MAIN - [SDR CALA0200581](https://openairdocs.org/sdr/CALA0200581), Dec 11, 2002: BATTERY PACK. INOPERATIVE. THE TAILCONE SLIDE EMERGENCY LIGHTS WOULD NOT TEST. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-53-00. - [SDR CALA0200389](https://openairdocs.org/sdr/CALA0200389), Jul 2, 2002: LATCH. OUT OF RIG. THE TAILCONE INTERIOR RELEASE HANDLE PULL WAS EXCESSIVE. THE TAILCONE LATCH LOCKPINS WERE ADJUSTED AND OPERATION CHECKED GOOD IAW MM 53-53-00. - [SDR CALA0200369](https://openairdocs.org/sdr/CALA0200369), Jun 28, 2002: LONGERON. CRACKED. INSPECTION FOUND A 1/4" CRACK IN LONGERON 2L AT BELTFRAME STA 1418. THE CRACKED SECTION OF LONGERON WAS CUT OUT AND A NEW SECTION WAS SPLICED IN IAW SRM 53-02, - [SDR CALA0000143](https://openairdocs.org/sdr/CALA0000143), Feb 8, 2000: PANEL. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN RT WING TRANSVERSE PANEL. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3. - [SDR CALA0000142](https://openairdocs.org/sdr/CALA0000142), Feb 8, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND AFT CARGO RT TIEDOWN TRACK CORRODED AT FS 1003-1155. THE TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-4, 51-10-03, 51-30-01, AND 51-30-02. - [SDR CALA0000140](https://openairdocs.org/sdr/CALA0000140), Feb 7, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND MID AND AFT CARGO LT TIE DOWN TRACKS CORRODED AT FS 636-736 AND FS 1003-1212, LBL 24. THE CORRODED SECTIONS OF TRACK WERE REMOVED AND NEW TRACK - [SDR CALA0000138](https://openairdocs.org/sdr/CALA0000138), Feb 5, 2000: DOOR PAN. GOUGED. INSPECTION FOUND AFT CARGO DOOR AFT STOP POSITIONS ON FRAME GOUGED. A DOUBLER REPAIR WAS INSTALLED IAW SRM 52-03, FIGURE 8 AND ECRA5230-01519. - [SDR CALA0000137](https://openairdocs.org/sdr/CALA0000137), Feb 5, 2000: WEB. CORRODED. INSPECTION FOUND CABIN FLOOR WEB CORRODED AT SUPPORTS BETWEEN FS 1136 AND 1212. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10- - [SDR CALA0000135](https://openairdocs.org/sdr/CALA0000135), Feb 4, 2000: FLOORBEAM. CORRODED. INSPECTION FOUND AFT CARGO FLOOR PANEL SUPPORT CORRODED AT FS 1155, LBL 16 TO RBL 8. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-4, 51-30-2, AND 51-30-5. - [SDR CALA0000128](https://openairdocs.org/sdr/CALA0000128), Feb 2, 2000: INTERCOSTAL. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL AT FS 1022-1041, BL 0. THE INTERCOSTAL WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, - [SDR CALA0000127](https://openairdocs.org/sdr/CALA0000127), Feb 2, 2000: STOP PAD. CHAFED. INSPECTION FOUND MID CARGO DOOR FORWARD STOP PADS ON FRAME CHAFED. REPAIR DOUBLERS WERE INSTALLED IAW SRM 52-03, FIGURE 8, 51-10-03, AND EA 9-5233-A0988. - [SDR CALA0000126](https://openairdocs.org/sdr/CALA0000126), Feb 1, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND RT CARGO TIEDOWN TRACK IN MID CARGO COMPARTMENT CORRODED AT STA 769-786. A NEW CARGO TIEDOWN TRACK WAS INSTALLED IAW SRM 51-10-4, 51-30-1, AND - [SDR CALA0000125](https://openairdocs.org/sdr/CALA0000125), Feb 1, 2000: FITTING. CORRODED. INSPECTION FOUND LEFT O/B GALLEY FITTING CORRODED AT FS 1140. THE GALLEY FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-02 AND 51-30-05. - [SDR CALA0000124](https://openairdocs.org/sdr/CALA0000124), Feb 1, 2000: SKIN. CHAFED. INSPECTION FOUND LOWER EXTERNAL SKIN FORWARD AND AFT CORNERS OF FORWARD CARGO DOOR CHAFED. A TWO DOUBLER REPAIR WAS INSTALLED WITH SHIMS IAW SRM 52-05, FIGURE 4 - [SDR CALA0000123](https://openairdocs.org/sdr/CALA0000123), Feb 1, 2000: SKIN. DENTED. INSPECTION FOUND FUSELAGE BELLY SKIN DENTED AT STA 636, LONGERON 30. THE SKIN WAS COLD WORKED AND A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, 53-01, FIGUR - [SDR CALA0000122](https://openairdocs.org/sdr/CALA0000122), Feb 1, 2000: BRACKET. CRACKED. INSPECTION FOUND RT FORWARD ADF FAIRING SUPPORT BRACKET CRACKED AT L/E WING ROOT. THE SUPPORT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-5. - [SDR CALA0000121](https://openairdocs.org/sdr/CALA0000121), Feb 1, 2000: SKIN. CRACKED. INSPECTION FOUND RT SIDE TAIL COMPARTMENT SKIN CRACKED JUST FORWARD OF RUDDER TRIM ACTUATOR AT STA 1485. THE CRACKED AREA OF SKIN WAS REMOVED AND A DOUBLER WAS - [SDR CALA0000120](https://openairdocs.org/sdr/CALA0000120), Feb 1, 2000: SKIN. DENTED. INSPECTION FOUND LT ELEVATOR LOWER SKIN SURFACE DENTED. THE DENTED AREA WAS REMOVED AND REPAIRED IAW ECRA 5520-01231. - [SDR CALA0000119](https://openairdocs.org/sdr/CALA0000119), Feb 1, 2000: INTERCOSTAL. GOUGED. INSPECTION FOUND AFT CARGO COMPARTMENT INTERCOSTAL GOUGED ON TOP AND BOTTOM FLANGE AT STA 1007, LONGERON 22R. REPAIR ANGLES WERE INSTALLED IAW SRM 51-10-4, 51-1 - [SDR CALA0000118](https://openairdocs.org/sdr/CALA0000118), Feb 1, 2000: STOP PAD. CHAFED. INSPECTION FOUND AFT CARGO DOOR UPPER STOP AND FORWARD STOP PADS ON FRAME CHAFED. ANGLE REPAIRS WERE INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2, 51-30-5, 52-03 - [SDR CALA0000116](https://openairdocs.org/sdr/CALA0000116), Feb 1, 2000: SKIN. CORRODED. INSPECTION FOUND AFT CARGO DOOR UPPER FORWARD WEB SKIN CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-3. A DOUBLER WAS INSTALLED IAW SRM 52-01, FIGURE 1, 51- - [SDR CALA0000115](https://openairdocs.org/sdr/CALA0000115), Feb 1, 2000: FRAME. CHAFED. INSPECTION FOUND MID CARGO DOOR UPPER FORWARD STOP AREA CHAFED. A DOUBLER WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 52-03, FIGURE 8 AND ECRA 5230-01518. - [SDR CALA0000114](https://openairdocs.org/sdr/CALA0000114), Feb 1, 2000: FLANGE. CHAFED. INSPECTION FOUND FORWARD PIT DOOR SEAL ATTACH FLANGE CHAFED UNDER STOP PADS AT ALL SIDES OF DOOR. REPAIR ANGLES WERE INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2 - [SDR CALA0000105](https://openairdocs.org/sdr/CALA0000105), Jan 27, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND RT TIEDOWN TRACK IN AFT CARGO COMPARTMENT CORRODED AT STA 1212-1322, RBL 24. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-05, - [SDR CALA0000089](https://openairdocs.org/sdr/CALA0000089), Jan 26, 2000: RIB. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN I/B TOP END OF FORWARD RIB ON LT MLG I/B DOOR. THE SKIN WAS REMOVED AND THE CRACK WAS STOP DRILLED. A REPAIR ANGLE WAS INSTAL - [SDR CALA0000088](https://openairdocs.org/sdr/CALA0000088), Jan 26, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LT CENTER SEAT TRACK CORRODED FROM STA 1098 TO 1231. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51- - [SDR CALA0000087](https://openairdocs.org/sdr/CALA0000087), Jan 26, 2000: CLIP. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN CLIP AT VERTICAL STABILIZER LOWER LT AFT CORNER JUST FORWARD OF RUDDER LEADING EDGE. THE CLIP WAS REMOVED AND A NEW CLIP WAS - [SDR CALA0000082](https://openairdocs.org/sdr/CALA0000082), Jan 25, 2000: COWL. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN INTERNAL DOUBLER STRAP OF NR 2 ENGINE NOSE COWL THROUGH ACCESS PANEL NR 7403 UPPER RT SIDE. THE NR 2 ENGINE NOSE COWL WAS REM - [SDR CALA0000081](https://openairdocs.org/sdr/CALA0000081), Jan 25, 2000: BEAM. CORRODED. INSPECTION FOUND MID CARGO DOOR JAMB BEAM CORRODED AROUND RIVETS. A DOUBLER AND SPACER WERE INSTALLED IAW SRM 51-30-5 AND ECRA 5310-03027. - [SDR CALA0000075](https://openairdocs.org/sdr/CALA0000075), Jan 24, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND RT O/B SEAT TRACK CORRODED AT GALLEY FITTING FS 218. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53- - [SDR CALA0000074](https://openairdocs.org/sdr/CALA0000074), Jan 24, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LT O/B SEAT TRACK CORRODED AT STA 1140 GALLEY FITTING. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION OF TRACK WAS INSTALLED - [SDR CALA0000073](https://openairdocs.org/sdr/CALA0000073), Jan 24, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND RT INBD AND RT CENTER SEAT TRACKS CORRODED AT STA 207. THE SEAT TRACKS WERE REMOVED AND NEW TRACKS WERE INSTALLED IAW SRM 51-30-1, 51-10-4, 51- - [SDR CALA0000072](https://openairdocs.org/sdr/CALA0000072), Jan 24, 2000: SKIN. GOUGED. INSPECTION FOUND MID CARGO DOOR SKIN GOUGED. THE AREA WAS REPAIRED IAW SRM 52-05, FIGURE 1. - [SDR CALA0000071](https://openairdocs.org/sdr/CALA0000071), Jan 24, 2000: DOOR PAN. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN FORWARD CARGO DOOR PAN AT T/E SEAL RETAINER HOLES FLANGE, LOWER FORWARD SECTION, 12 INCHES FROM BOTTOM. THE CRACK WAS STOP - [SDR CALA0000070](https://openairdocs.org/sdr/CALA0000070), Jan 24, 2000: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 168-200, RBL 47. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-5 AND 53-14-1. - [SDR CALA0000069](https://openairdocs.org/sdr/CALA0000069), Jan 23, 2000: DOOR PAN. CORRODED. INSPECTION FOUND FORWARD CARGO DOOR JAMB PAN CORRODED AROUND RIVETS. THE DOOR JAMB PAN WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 44. - [SDR CALA0000068](https://openairdocs.org/sdr/CALA0000068), Jan 23, 2000: SKIN. CRACKED. INSPECTION FOUND .5 INCH CRACKS IN REPAIR DOUBLER AT LOWER AFT O/B CORNER OF LT MLG I/B DOOR. THE CRACKED DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IA - [SDR CALA0000067](https://openairdocs.org/sdr/CALA0000067), Jan 23, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT STA 218. THE SEAT TRACK WAS REMOVED AND REPLACED USING A SPLICE IAW SRM 51-30-2,53-05, AND 51-30-3. - [SDR CALA0000066](https://openairdocs.org/sdr/CALA0000066), Jan 23, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LT I/B SEAT TRACK CORRODED FROM STA 1079-1271. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-5, 51-10-4, 51-10-3, - [SDR CALA0000065](https://openairdocs.org/sdr/CALA0000065), Jan 21, 2000: SKIN. CRACKED. INSPECTION FOUND AFT ACCESSORY CATWALK SHROUD RT AND LT FWD END SKIN CRACKED AT FS 1345. THE CRACKS WERE 2 AND 1 LONG, RESPECTIVELY. THE CRACKS WERE STOP DRILLE - [SDR CALA0000064](https://openairdocs.org/sdr/CALA0000064), Jan 21, 2000: FITTING. CORRODED. INSPECTION FOUND GALLEY SUPPORT FITTING CORRODED ATSTA 157, RBL 4. A NEW GALLEY SUPPORT FITTING WAS INSTALLED IAW SRM 51-30-2. - [SDR CALA0000063](https://openairdocs.org/sdr/CALA0000063), Jan 21, 2000: WEB. CRACKED. INSPECTION FOUND AFT AIRSTAIRS LEFT AND RIGHT LOWER WEB CRACKED ABOVE GROUND ROLLER. THE CRACKS WERE 2 AND 1 LONG RESPECTIVELY. REPAIR DOUBLERS WERE INSTALLED A - [SDR CALA0000062](https://openairdocs.org/sdr/CALA0000062), Jan 21, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND SEAT TRACK CORRODED AT FS 157-200, LBL 14. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3. - [SDR CALA0000061](https://openairdocs.org/sdr/CALA0000061), Jan 21, 2000: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 180-200, RBL 37. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 53-14-1, 51- - [SDR CALA0000060](https://openairdocs.org/sdr/CALA0000060), Jan 21, 2000: SKIN. CREASED. INSPECTION FOUND FUSELAGE SKIN CREASED AT STA 120-150 BETWEEN LONGERON 24 AND 25R. REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-04, FIGURE 12B, 51-30-2, AND 51-30- - [SDR CALA0000059](https://openairdocs.org/sdr/CALA0000059), Jan 21, 2000: BRACKET. CORRODED. INSPECTION FOUND CORROSION AROUND FASTENER HOLE AT RT LOWER CORNER OF RT AFT EMERGENCY EXIT DOOR. THE CORROSION WAS REMOVED IAW SRM 51-10-3 AND 51-30-2. A BRACK - [SDR CALA0000053](https://openairdocs.org/sdr/CALA0000053), Jan 21, 2000: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT AT FORWARD ENTRANCE THRESHOLD CORRODED. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-14-1 AND 51-3-0. - [SDR CALA0000052](https://openairdocs.org/sdr/CALA0000052), Jan 21, 2000: PANEL. CORRODED. INSPECTION FOUND FORWARD UPPER PANEL OF Rt MLG DOOR CORRODED. A NEW PANEL WAS INSTALLED IAW SRM 52-84-0. - [SDR CALA0000051](https://openairdocs.org/sdr/CALA0000051), Jan 21, 2000: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT AT FORWARD ENTRY AREA, STA 180, LBL 25, CORRODED. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, All 74: https://openairdocs.org/deregistered/N14839-2008-07-16/reports.md ## Other aircraft with N14839 - [Registered now](https://openairdocs.org/aircraft/N14839): Ea Vision J-150, S/N JMZKJ150UAV602595250 - [Cancelled 1972-10-10](https://openairdocs.org/deregistered/N14839-1972-10-10): Bell 47G3B2A, S/N 6844. Exported to Canada. Owner: [Bell Helicopter Co](https://openairdocs.org/faa-owner/BELL%20HELICOPTER%20CO), [Ft Worth, TX](https://openairdocs.org/faa-place/TX/Ft%20Worth) --- 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.