# N72821: 1986 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2005-05-17 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 17, 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: 49481 - Year built: 1986 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: September 22, 1986 - Certificate issued: April 21, 1998 - Last registry action: November 13, 2002 - Mode S code: A9C3FC - 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/N72821 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=72821 - Page: https://openairdocs.org/deregistered/N72821-2005-05-17 From the FAA registry file of November 12, 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 CALA0400628](https://openairdocs.org/sdr/CALA0400628), Sep 4, 2004: BEAM. CORRODED. INSPECTION FOUND BULKHEAD BEAM WEB CORRODED AT STA 110, S30L. THE BEAM WEB WAS REPAIRED IAW ECRA 5310-04387. - [SDR CALA0300697](https://openairdocs.org/sdr/CALA0300697), Nov 20, 2003: BEAM. CORRODED. INSPECTION FOUND STA 110 BULKHEAD BEAM WEB CORRODED AT MAIN BATTERY GROUND STUD HOLE. THE BEAM WEB WAS REPAIRED IAW ECRA 5310-04387. - [SDR CALA0200438](https://openairdocs.org/sdr/CALA0200438), Aug 9, 2002: SEAT TRACK. CORRODED. INSPECTION FOUND L/H CENTER SEAT TRACK CORRODED BETWEEN STA 1079 AND 1136. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-5. - [SDR CALA0200437](https://openairdocs.org/sdr/CALA0200437), Aug 9, 2002: WEB. CORRODED. INSPECTION FOUND E&E COMPARTMENT SUBFLOOR CORRODED AT VENTRAL STAIR MECHANISM, STA 162-168, X = 54.000. A DOUBLER WAS INSTALLED IAW SRM 51-70-4. - [SDR CALA0200436](https://openairdocs.org/sdr/CALA0200436), Aug 7, 2002: SEAT TRACK. CORRODED. INSPECTION FOUND R/H CENTER AND R/H I/B SEAT TRACKS CORRODED AT STA 228. THE CORRODED SEAT TRACK SECTIONS WERE REMOVED AND NEW SECTIONS WERE SPLICED IN IAW SRM - [SDR CALA0100757](https://openairdocs.org/sdr/CALA0100757), Aug 10, 2001: SKIN. DENTED. THE R/H FUSELAGE SKIN WAS DENTED BETWEEN FORWARD CARGO DOOR AND RIGHT TURN OFF LIGHT AT STA 435-510 BETWEEN LONGERONS 20R AND 21R. A FLUSH SKIN PANEL REPAIR WAS - [SDR CALA0100756](https://openairdocs.org/sdr/CALA0100756), Aug 10, 2001: LONGERON. CRACKED. INSPECTION FOUND A 10" CRACK AT END OF LONGERON 2L AT STA 1418. A HAT SECTION REPAIR SPLICE WAS INSTALLED IAW SRM 53-02, FIGURE 18. - [SDR CALA0100755](https://openairdocs.org/sdr/CALA0100755), Aug 10, 2001: ANGLE. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN TAIL COMPARTMENT LEFT VENTRAL BOX SUPPORT ANGLE AT CANTED FRAME STA 1474. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SR - [SDR CALA0100753](https://openairdocs.org/sdr/CALA0100753), Aug 9, 2001: FITTING. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN TAIL COMPARTMENT SUPPORT FITTING BETWEEN CANTED FRAMES 1463 AND 1485 AT LOWER AFT SIDE. THE SUPPORT FITTING WAS REMOVED AND A - [SDR CALA0100752](https://openairdocs.org/sdr/CALA0100752), Aug 9, 2001: PLATE. CORRODED. INSPECTION FOUND HORIZONTAL STABILIZER PIVOT PLATE CORRODED AT LEFT I/B LUG BORES. THE PIVOT PLATES WERE REMOVED AND REPLACED IAW EA 5530-01238. - [SDR CALA0100751](https://openairdocs.org/sdr/CALA0100751), Aug 9, 2001: PLATE. CORRODED. INSPECTION FOUND HORIZONTAL STABILIZER PIVOT PLATES CORRODED AT RIGHT O/B AND RIGHT I/B LUG BORES. THE PIVOT PLATES WERE REMOVED AND REPLACED IAW EA 5530-01238. - [SDR CALA0100750](https://openairdocs.org/sdr/CALA0100750), Aug 9, 2001: FRAME. CRACKED. INSPECTION FOUND A 2" CRACK IN TAIL COMPARTMENT CANTED FRAME AT STA 1474, LEFT LOWER SIDE, BY VENT BOX DRAIN HOSE. REPAIRED IAW ECRA 5310-04173. - [SDR CALA0100747](https://openairdocs.org/sdr/CALA0100747), Aug 8, 2001: ATTACH ANGLE. CRACKED. INSPECTION FOUND A 3/4" CRACK COMING FROM RIVET HOLE IN R/H SIDE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT STA 1463. THE CRACKED AREA WAS CUT OUT AND A RE - [SDR CALA0100743](https://openairdocs.org/sdr/CALA0100743), Aug 7, 2001: PAN. CRACKED. INSPECTION FOUND A 1" CRACK IN L/H MLG I/B DOOR PAN AT LEADING EDGE. THE DOOR PAN WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-3, 51-30-8, AND 51-10-2. - [SDR CALA9901487](https://openairdocs.org/sdr/CALA9901487), Nov 12, 1999: SKIN. CRACKED. INSPECTION FOUND A 3 CRACK IN RT WING LEADING EDGE UPPER SKIN AT STA XOS 286. A DOUBLER WAS INSTALLED IAW ECRA 5720-01773 AND A DIP WAS INITIATED TO REINSPECT T - [SDR CALA9900245](https://openairdocs.org/sdr/CALA9900245), Mar 11, 1999: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN AFT SERVICE DOOR SKIN AT TOP AFT EDGE OF HOLD OPEN HOOK CUTOUT. REPAIRED IAW ECRA 5205-01008. - [SDR CALA9900243](https://openairdocs.org/sdr/CALA9900243), Mar 10, 1999: BAYONET. WORN. THE FORCE REQUIRED TO RELEASE TAIL CONE USING EXTERNAL HANDLE WAS LOW. THE LEFT LOWER TAIL CONE BAYONET WAS REMOVED AND REPLACED DUE TO WEAR. AN ADJUSTMENT/TEST - [SDR CALA9900236](https://openairdocs.org/sdr/CALA9900236), Mar 9, 1999: PAN. CRACKED. INSPECTION FOUND A 2.25 INCH CRACK IN AFT CARGO DOOR PAN AT FORWARD HOLD OPEN LATCH AND A .75 INCH CRACK IN AFT CARGO DOOR PAN AT AFT HOLD OPEN LATCH. INSTALLED - [SDR CALA9900228](https://openairdocs.org/sdr/CALA9900228), Mar 6, 1999: BEAM. CRACKED. INSPECTION FOUND TWO CRACKS IN THE NR 1 BEAM OF MAIN CABIN DOOR. THE BEAM HAD A .75 INCH CRACK ON AFT END AND A .375 INCH CRACK ON FORWARD END. - [SDR CALA9900227](https://openairdocs.org/sdr/CALA9900227), Mar 5, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND SEAT TRACK CORRODED AROUND SCREW HOLES AT LT I/B POSITION, STA 1117-1174 AFT GALLEY AREA. NEW SEAT TRACK SECTIONS WERE INSTALLED IAW SRM 53-05. - [SDR CALA9900224](https://openairdocs.org/sdr/CALA9900224), Mar 5, 1999: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 237 ABOVE CUSP. A NEW SKIN SECTION WAS INSTALLED BETWEEN LONGERON 15L AND 18L IAW ECRA 5330-02445. - [SDR CALA9900221](https://openairdocs.org/sdr/CALA9900221), Mar 4, 1999: PAN. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN MID CARGO BIN DOOR PAN. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 52-05, FIGURE 26A. - [SDR CALA9900220](https://openairdocs.org/sdr/CALA9900220), Mar 4, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT CENTER SEAT TRACK CORRODED AROUND SCREW HOLES FROM GALLEY NR 3 TO GALLEY NR 4 AREA, STA 1117 TO 1174. THE SEAT TRACK WAS REMOVED AND REPLA - [SDR CALA9900212](https://openairdocs.org/sdr/CALA9900212), Mar 3, 1999: ANGLE. CORRODED. INSPECTION FOUND AFT CARGO COMPARTMENT Z-ANGLE CORRODED. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 63 AND 51-30-5. - [SDR CALA9800659](https://openairdocs.org/sdr/CALA9800659), Apr 15, 1998: SENSOR. INOPERATIVE. THE AIRCRAFT HAD A BRIEF HISTORY OF THE NOSE GEAR UNSAFE LIGHT REMAINING ILLUMINATED AFTER TAKEOFF. CYCLING THE GEAR WOULD EXTINGUISH THE LIGHT. THE NOSE GEAR L - [SDR CALA9700365](https://openairdocs.org/sdr/CALA9700365), Mar 12, 1997: SKIN. DAMAGED. FINGER DOUBLERS WERE INSTALLED TO FUSELAGE SKIN AT STA 427 TO 507, LONGERON 20L IAW SRM 53-04, FIGURE 12B. THE SKIN DAMAGE HAD BEEN REPAIRED PREVIOUSLY AND DEFE - [SDR CALA9700363](https://openairdocs.org/sdr/CALA9700363), Mar 12, 1997: CHANNEL. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN RT MLG INBOARD DOOR FORWARD JAMB CHANNEL. A REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2. - [SDR CAL950872](https://openairdocs.org/sdr/CAL950872), Sep 25, 1995: SKIN. TORN. TUS - FLT 0425 - INSPECTION FOUND A 1.5 INCH TEAR IN FUSELAGE SKIN AND DAMAGE TO TWO SKIN CLIPS DUE TO GROUND DAMAGE. THE DAMAGE WAS LOCATED AT STA 427-STA 507 - [SDR CAL950464](https://openairdocs.org/sdr/CAL950464), Jun 7, 1995: EEL PWR SUPPLY. INOPERATIVE. FLT NR 0305 - EWR - BOTH OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. THE POWER SUPPLY WAS REPLACED AND OPERATION OF THE OVERWING EMERGENCY EXIT LIGHT ## Other aircraft with N72821 - [Cancelled 1953-04-15](https://openairdocs.org/deregistered/N72821-1953-04-15): Cessna 140, S/N 10007. Owner: [Pipes David](https://openairdocs.org/faa-owner/PIPES%20DAVID), [Centerville, TX](https://openairdocs.org/faa-place/TX/Centerville) --- 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, except the copies of manufacturers’ service documents, which belong to their rights holders.