# N15841: 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: 49581 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: July 2, 1987 - Certificate issued: September 19, 2006 - Last registry action: September 19, 2006 - Mode S code: A0EAE5 - 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/N15841 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=15841 - Page: https://openairdocs.org/deregistered/N15841-2008-07-16 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 (95, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0400410](https://openairdocs.org/sdr/CALA0400410), Apr 23, 2004: WEB. CRACKED. WEB CRACKED AT FWD LWR SIDE OF BAG BIN DOOR AT STA 636, LONG 27 LEFT. REMOVED AND REPLACED WEB PER ECRA 5310-04416. - [SDR CALA0400404](https://openairdocs.org/sdr/CALA0400404), Apr 20, 2004: SHEAR TIE. CORRODED. A/B/B SHEAR TIE CORRODED AT LONGERON 30 AND 28 RIGHT AT STATION 1193. FABRICATED AND INSTALLED SHEAR TIE REPAIR SPLICE BETWEEN LONG 30 AND 29 RIGHT PER SRM 53-0 - [SDR CALA0300053](https://openairdocs.org/sdr/CALA0300053), Feb 17, 2003: LONGERON. CRACKED. INSPECTION FOUND LONGERON 2L CRACKED AT STA 1418. REPAIRED IAW ECRA 5311-01132. - [SDR CALA0300048](https://openairdocs.org/sdr/CALA0300048), Feb 15, 2003: LONGERON. CRACKED. INSPECTION FOUND A 2" CRACK IN LONGERON 2R AT STA 1418. A SECTION OF LONGERON WAS SPLICED IN IAW ECRA 5311-01132. - [SDR CALA0001412](https://openairdocs.org/sdr/CALA0001412), Sep 12, 2000: SKIN. CRACKED. INSPECTION FOUND LT WING LEADING EDGE SKIN CRACKED AT APPROXIMATELY STA XIS 60. REPAIR DOUBLERS, SHIMS, ANGLES, AND NUT PLATE STRIPS WERE INSTALLED IAW EA 9-572 - [SDR CALA0001411](https://openairdocs.org/sdr/CALA0001411), Sep 12, 2000: FRAME. CORRODED. INSPECTION FOUND AFT CARGO FRAME AFT SIDE CORRODED UNDER PAINT AT FS 1309, L24R-24L. THE CORRODED SECTION WAS CUT OUT AND A FRAME REPAIR SPLICE WAS INSTALLED IA - [SDR CALA0001410](https://openairdocs.org/sdr/CALA0001410), Sep 11, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND MID CARGO RT CARGO TIE DOWN TRACK CORRODED AT FS 532 - 625 AND FS 693 - 807. THE TIE DOWN TRACK SECTIONS WERE REMOVED AND NEW TRACK SECTIONS WE - [SDR CALA0001409](https://openairdocs.org/sdr/CALA0001409), Sep 11, 2000: SKIN. CRACKED. AN INTERIM REPAIR WAS REMOVED AND A PERMANENT REPAIR WAS INSTALLED WHERE A 1 INCH CRACK EXISTED ON L/E LOWER SURFACE OF LT WING SKIN AT NR 2 SLAT CENTER TRACK C - [SDR CALA0001408](https://openairdocs.org/sdr/CALA0001408), Sep 11, 2000: FAIRING. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN RT WING FLAP HINGE FAIRING NR 3 AFT. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 57-01, FIGURE 3, S - [SDR CALA0001403](https://openairdocs.org/sdr/CALA0001403), Sep 8, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND MID CARGO RT TRACK FLOOR SUPPORT CORRODED AT FS 598 - 636. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-01 - [SDR CALA0001402](https://openairdocs.org/sdr/CALA0001402), Sep 7, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT I/B CABIN SEAT TRACK CORRODED AT FS 1117 - 1309. THE CORROSION WAS REMOVED IAW SRM 53-05, FIGURE 4. CORROSION REMOVAL WAS WITHIN LIMITS FR - [SDR CALA0001400](https://openairdocs.org/sdr/CALA0001400), Sep 5, 2000: SKIN. DENTED. INSPECTION FOUND NR 2 LEFT T/E FLAP DENTED ON LOWER SIDE. THE DENTED AREA WAS TRIMMED OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-01, FIGURE 5 AND FIGURE - [SDR CALA0001399](https://openairdocs.org/sdr/CALA0001399), Sep 5, 2000: ANGLE. CRACKED. INSPECTION FOUND FOUR VERTICAL STABILIZER DOGHOUSE ANGLES CRACKED. LOCATIONS WERE RT AND LT FWD LOWER AND RT AND LT AFT LOWER AREA. THE CRACKS WERE .5 INCH LONG - [SDR CALA0001398](https://openairdocs.org/sdr/CALA0001398), Sep 5, 2000: DOOR FRAME. CORRODED. INSPECTION FOUND AFT CARGO DOOR CUTOUT LOWER JAMB CORRODED. A DOUBLER AND STRAP WERE INSTALLED IAW SRM 51-10-4 AND ECRA 5310-03027. - [SDR CALA0001397](https://openairdocs.org/sdr/CALA0001397), Sep 5, 2000: DOUBLER. CORRODED. INSPECTION FOUND ANTENNA DOUBLER CORRODED ON MOUNTING FLANGE AT FS 700, LONGERON 30. THE ANTENNA DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51- - [SDR CALA0001389](https://openairdocs.org/sdr/CALA0001389), Sep 3, 2000: PAN. CRACKED. INSPECTION FOUND A 1.9 INCH CRACK AT CAM LATCH OF FWD CARGO DOOR FWD EDGE OF INNER PAN. THE CRACKED SECTION WAS REMOVED IAW EA 9-5231-2-A0749. A REPAIR ANGLE AN - [SDR CALA0001388](https://openairdocs.org/sdr/CALA0001388), Sep 3, 2000: ANGLE. CORRODED. INSPECTION FOUND UPPER AND LOWER SURFACE OF DOOR Z-ANGLE CORRODED AT RT SIDE OF AFT PIT. THE Z-ANGLE WAS REMOVED AND A NEW Z-ANGLE WAS INSTALLED IAW SRM 51-30-1 - [SDR CALA0001387](https://openairdocs.org/sdr/CALA0001387), Sep 3, 2000: BRACKET. CORRODED. INSPECTION FOUND L-2 DOOR THRESHOLD SUPPORT BRACKETS CORRODED. THE BRACKETS WERE REMOVED AND NEW BRACKETS WERE INSTALLED IAW SRM 51-30-5. - [SDR CALA0001386](https://openairdocs.org/sdr/CALA0001386), Sep 3, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND RT TIEDOWN TRACK CORRODED FROM STA 1211 - 1309 AND LT TIEDOWN TRACK CORRODED FROM STA 1007 - 1309 IN AFT PIT. THE TRACKS WERE REMOVED AND NEW T - [SDR CALA0001385](https://openairdocs.org/sdr/CALA0001385), Sep 3, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT FS 936 - 1212. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1 AND 53-05, FIGURE - [SDR CALA0001383](https://openairdocs.org/sdr/CALA0001383), Sep 3, 2000: FAIRING. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN RT UPPER HORIZONTAL STABILIZER BANANA FAIRING ON FORWARD END. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-01, FIGURE 2, 55-10-0 - [SDR CALA0001382](https://openairdocs.org/sdr/CALA0001382), Sep 3, 2000: FRAME. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN LT MLG WHEEL WELL DOOR FRAME AT O/B FORWARD CORNER. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-1, AND 51-30-8. - [SDR CALA0001381](https://openairdocs.org/sdr/CALA0001381), Sep 3, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND LT CARGO TIE DOWN TRACK CORRODED IN MID CARGO COMPARTMENT AT FS 522. THE TIE DOWN TRACK WAS REMOVED AND A REPLACEMENT TRACK WAS INSTALLED IAW S - [SDR CALA0001380](https://openairdocs.org/sdr/CALA0001380), Sep 3, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT STA 1126 - 1240. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1, 51-30-2, AND 53-05, FIGURE 4. - [SDR CALA0001379](https://openairdocs.org/sdr/CALA0001379), Sep 3, 2000: SKIN. DENTED. INSPECTION FOUND LOWER FUSELAGE SKIN DENTED AT STA 294, LONGERON 22L. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 38G. - [SDR CALA0001378](https://openairdocs.org/sdr/CALA0001378), Sep 3, 2000: STRUCTURE. CORRODED. INSPECTION FOUND CABIN AREA SUPPORT CORRODED AT STA 200, LBL 10. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 53-14-1, 51-10-4, 51-1 - [SDR CALA0001377](https://openairdocs.org/sdr/CALA0001377), Sep 3, 2000: DOUBLER. GOUGED. INSPECTION FOUND FORWARD CARGO DOOR FORWARD LOWER OUTER SKIN DOUBLER LOWER EDGE GOUGED. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2. - [SDR CALA0001376](https://openairdocs.org/sdr/CALA0001376), Sep 3, 2000: WEB. BENT. INSPECTION FOUND CABIN SUBFLOOR LIGHTENING HOLE DOUBLER BENT AND TORN AT STA 160, LBL 12. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30- - [SDR CALA0001375](https://openairdocs.org/sdr/CALA0001375), Sep 3, 2000: STRUCTURE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE I/B SUPPORT. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-10 - [SDR CALA0001373](https://openairdocs.org/sdr/CALA0001373), Sep 3, 2000: FLOOR PANEL. CORRODED. INSPECTION FOUND COCKPIT RT METAL FLOOR PANEL CORRODED AND DENTED. THE FLOOR PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 53-24-0. - [SDR CALA0001367](https://openairdocs.org/sdr/CALA0001367), Sep 2, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 160, BL 0. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW 51-30-02, 51-10-04, AND 51-30- - [SDR CALA0001366](https://openairdocs.org/sdr/CALA0001366), Sep 2, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND CABIN FLOOR SUPPORTS CORRODED AT STA 160, RBL 45 AND AT STA 200, RBL 51. THE FLOOR SUPPORTS WERE REMOVED AND NEW SUPPORTS WERE INSTALLED IAW SR - [SDR CALA0001365](https://openairdocs.org/sdr/CALA0001365), Sep 2, 2000: BRACKET. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN TWO AFT CARGO PIT L BRACKETS AT FORWARD AND AFT END OF OVERHEAD CARGO DOOR LATCH SUPPORT. THE BRACKETS WERE REMOVED AND REPLA - [SDR CALA0001364](https://openairdocs.org/sdr/CALA0001364), Sep 2, 2000: BRACKET. CRACKED. INSPECTION FOUND TWO L BRACKETS CRACKED IN FORWARD CARGO PIT AT FORWARD AND AFT END OF CARGO DOOR LATCH SUPPORT. THE CRACKS WERE .25 INCH LONG. THE BRACKETS WER - [SDR CALA0001363](https://openairdocs.org/sdr/CALA0001363), Sep 2, 2000: PANEL. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN AFT CARGO CENTER FLOOR TRANSITION PANEL AT STA 1212 - 1231. THE CRACKED AREA WAS TRIMMED OUT IAW SRM 53-01, FIGURE 4, SHEET 3 - [SDR CALA0001361](https://openairdocs.org/sdr/CALA0001361), Sep 2, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND CABIN AREA FLOOR SUPPORTS CORRODED AT STA 200, BL 0 AND AT STA 140 - 200, RBL 7. THE FLOOR SUPPORTS WERE REMOVED AND NEW SUPPORTS WERE INSTALLE - [SDR CALA0001360](https://openairdocs.org/sdr/CALA0001360), Sep 2, 2000: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LT MLG FORWARD KEELBEAM ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-03, 51-30-05, AND 5 - [SDR CALA0001359](https://openairdocs.org/sdr/CALA0001359), Sep 2, 2000: SKIN. DENTED. INSPECTION FOUND L-1 DOOR UPPER AFT I/B EDGE DENTED. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38. - [SDR CALA0001354](https://openairdocs.org/sdr/CALA0001354), Aug 31, 2000: SKIN. DENTED. INSPECTION FOUND LOWER FUSELAGE SKIN DENTED AT STA 294, LONGERON 21L. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 38, VIEW G. - [SDR CALA0001353](https://openairdocs.org/sdr/CALA0001353), Aug 31, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT O/B SEAT TRACK AFT OF L-2 DOOR CORRODED AT FS 1174. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-4 - [SDR CALA0001352](https://openairdocs.org/sdr/CALA0001352), Aug 31, 2000: FLOOR SUPPORT. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LOWER FLOOR PANEL SUPPORT IN FORWARD CARGO AREA AT FS 522. THE FLOOR PANEL SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-02 - [SDR CALA0001351](https://openairdocs.org/sdr/CALA0001351), Aug 31, 2000: WEB. CORRODED. INSPECTION FOUND LOWER SURFACE OF CABIN SUBFLOOR CORRODED AT FS 200 BETWEEN BL 0 AND RT SIDE OF AIRCRAFT. THE SUBFLOOR WAS REMOVED AND REPLACED IAW SRM 53-14-01 - [SDR CALA0001348](https://openairdocs.org/sdr/CALA0001348), Aug 29, 2000: SKIN. DENTED. INSPECTION FOUND LOWER FUSELAGE SKIN DENTED AT FS 465, LONGERON 23R - 24R. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 38, VIEW G. - [SDR CALA0001347](https://openairdocs.org/sdr/CALA0001347), Aug 29, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 168, RBL 28. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA0001346](https://openairdocs.org/sdr/CALA0001346), Aug 29, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200, RBL 29. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 53-14-1, A - [SDR CALA0001345](https://openairdocs.org/sdr/CALA0001345), Aug 29, 2000: SKIN. DENTED. INSPECTION FOUND AFT CARGO DOOR EXTERIOR SKIN DENTED. REPAIRED SKIN IAW SRM 52-05, FIGURE 1 AND 51-10-3. - [SDR CALA0001344](https://openairdocs.org/sdr/CALA0001344), Aug 29, 2000: FITTING. CORRODED. INSPECTION FOUND FORWARD AIRSTAIRS DOOR MOUNT BASE FITTING CORRODED AT STA 180. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-10-4, 51-10-3 - [SDR CALA0001340](https://openairdocs.org/sdr/CALA0001340), Aug 28, 2000: WEB. CRACKED. INSPECTION FOUND TWO 1 INCH CRACKS IN RT CUSP WEB AT FS 218 - 237. THE CUSP WEB WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2. - [SDR CALA0001339](https://openairdocs.org/sdr/CALA0001339), Aug 28, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 160, LBL 52. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-5, 51-10-4, - [SDR CALA0001338](https://openairdocs.org/sdr/CALA0001338), Aug 28, 2000: COVER. CORRODED. INSPECTION FOUND CABIN FLOOR SUPPORT COVER PLATE CORRODED AT FS 160 - 200, RBL 54. THE COVER PLATE WAS REMOVED AND A NEW COVER PLATE WAS INSTALLED IAW SRM 51-30 All 95: https://openairdocs.org/deregistered/N15841-2008-07-16/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 19900416020869I](https://openairdocs.org/incident/19900416020869I), Apr 16, 1990: Doug DC982 (N15841), Boston, MA, Minor damage. Struck the top of the fuel truck while being marshalled to parking area. ## Other aircraft with N15841 - [Cancelled 1973-06-22](https://openairdocs.org/deregistered/N15841-1973-06-22): Piper PA-28-140, S/N 28-7325176. Exported to Belgium. Owner: [Piper Aircraft Corp](https://openairdocs.org/faa-owner/PIPER%20AIRCRAFT%20CORP), [Lock Haven, PA](https://openairdocs.org/faa-place/PA/Lock%20Haven) - [Cancelled 1955-10-19](https://openairdocs.org/deregistered/N15841-1955-10-19): Beech C17B, S/N 84, built 1936. Owner: [Holland Dusting Service Inc](https://openairdocs.org/faa-owner/HOLLAND%20DUSTING%20SERVICE%20INC), [High Springs, FL](https://openairdocs.org/faa-place/FL/High%20Springs) --- 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.