# N72829: 1987 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2005-06-15 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 15, 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: 49489 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: March 23, 1987 - Certificate issued: April 22, 1998 - Last registry action: November 13, 2002 - Mode S code: A9C404 - 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/N72829 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=72829 - Page: https://openairdocs.org/deregistered/N72829-2005-06-15 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 (22) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA9900628](https://openairdocs.org/sdr/CALA9900628), Jun 2, 1999: RETAINER. CRACKED. INSPECTION FOUND A 2 INCH CRACK ON FORWARD CARGO DOOR LOWER LEFT PAN SEAL RETAINER UNDER DOOR LATCH MECHANISM. A REPAIR WAS INSTALLED IAW ECRA 5210-01343. - [SDR CALA9900609](https://openairdocs.org/sdr/CALA9900609), Jun 1, 1999: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 218 AT LONGERON 18L. THE DENTED AREA WAS REPAIRED IAW ECRA 5330-02817. - [SDR CALA9900581](https://openairdocs.org/sdr/CALA9900581), May 28, 1999: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 120 ABOVE LONGERON 18L. AN INTERNAL DOUBLER REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38. - [SDR CALA9900579](https://openairdocs.org/sdr/CALA9900579), May 27, 1999: BEAM. CRACKED. INSPECTION FOUND A .375 INCH CRACK IN MAIN CABIN DOOR NR 7 BEAM. THE DOOR BEAM WAS REPAIRED IAW SRM 52-05, FIGURE 31. - [SDR CALA9900578](https://openairdocs.org/sdr/CALA9900578), May 26, 1999: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT STA 389, LONGERON 30. A DOUBLER WAS INSTALLED IAW SRM 53-04 AND ECRA 5330-02812. - [SDR CALA9900577](https://openairdocs.org/sdr/CALA9900577), May 26, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT STA 200. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-05, FIGURE - [SDR CALA9900576](https://openairdocs.org/sdr/CALA9900576), May 26, 1999: SKIN. CRACKED. INSPECTION FOUND A .25 INCH CRACK WITH BEND AT LOCKING HANDLE IN FORWARD CARGO DOOR EXTERIOR SKIN. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 30. - [SDR CALA9900575](https://openairdocs.org/sdr/CALA9900575), May 25, 1999: ANGLE. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN LT INNER ATTACH ANGLE AT FORWARD LOWER ATTACH POINT FOR VERTICAL STABILIZER, FUSELAGE STA 1418. A 1.5 INCH CRACK WAS FOUND I - [SDR CALA9900574](https://openairdocs.org/sdr/CALA9900574), May 25, 1999: LONGERON. CRACKED. INSPECTION FOUND A 1 CRACK IN LONGERON 2R AND FOUND A 1 INCH CRACK IN LONGERON 2L AT STA 1418. THE CRACKED SECTIONS OF LONGERON WERE REMOVED, NEW SECTIONS AND S - [SDR CALA9900573](https://openairdocs.org/sdr/CALA9900573), May 24, 1999: BEAM. CRACKED. INSPECTION FOUND A 1 INCH CRACK AT BOTH ENDS OF MAIN CABIN DOOR NR 1 BEAM. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-1. - [SDR CALA9900572](https://openairdocs.org/sdr/CALA9900572), May 24, 1999: BEAM. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FORWARD SERVICE DOOR NR 4 BEAM. A NEW BEAM WAS INSTALLED IAW SRM 51-30-02 AND 51-30-05. - [SDR CALA9900571](https://openairdocs.org/sdr/CALA9900571), May 24, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT CENTER SEAT TRACK CORRODED FROM STA 1079 TO 1231. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F. - [SDR CALA9900570](https://openairdocs.org/sdr/CALA9900570), May 23, 1999: SKIN. DENTED. INSPECTION FOUND LT FUSELAGE SKIN DENTED BELOW CUSP LINE AT STA 218. THE DENTED AREA WAS ROUTED OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 25. - [SDR CALA9900569](https://openairdocs.org/sdr/CALA9900569), May 22, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND RT INBOARD SEAT TRACK CORRODED AT STA 218 TO 256. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30. - [SDR CALA9900567](https://openairdocs.org/sdr/CALA9900567), May 20, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND RT CENTER SEAT TRACK CORRODED AT STA 218-237. A NEW SECTION OF SEAT TRACK WAS SPLICED IN IAW SRM 53-05, FIGURE 4F. - [SDR CALA9900563](https://openairdocs.org/sdr/CALA9900563), May 20, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT OUTBOARD SEAT TRACK CORRODED AT STA 1136-1128. THE SEAT TRACK WAS REPLACED IAW SRM 51-30-2. - [SDR CALA9900562](https://openairdocs.org/sdr/CALA9900562), May 20, 1999: JAMB. CORRODED. INSPECTION FOUND CORROSION ON FORWARD BAG BIN DOOR JAMB PAN AT STA 370-427. A NEW PAN AND DOUBLERS WERE INSTALLED IAW SRM 53-05. - [SDR CALA9900561](https://openairdocs.org/sdr/CALA9900561), May 20, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT INBOARD SEAT TRACK CORRODED AT STA 1212-1222. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-01. - [SDR CALA9900560](https://openairdocs.org/sdr/CALA9900560), May 19, 1999: ESCAPE LINE. FRAYED. INSPECTION FOUND THE LEFT OVERWING EXIT ESCAPE LINE FRAYED AT ATTACH HOOK. THE ESCAPE LINE WAS REMOVED AND REPLACED IAW MM 25-61-00, PAGE 204-205. - [SDR CALA9900002](https://openairdocs.org/sdr/CALA9900002), Jan 2, 1998: DUCT. RUPTURED. THE NR 2 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED AFTER TAKEOFF. THRUST WAS REDUCED TO IDLE WITH THE FIRE HANDLE AND LOOP LIGHT EXTINGUISHING SHORTLY AFTERW - [SDR CALA970788](https://openairdocs.org/sdr/CALA970788), May 19, 1997: INTERCOSTAL. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN MAIN CABIN DOOR INTERCOSTAL AT AFT HANDLE TORQUE TUBE. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-2 AND 51-10-3. - [SDR CALA9700789](https://openairdocs.org/sdr/CALA9700789), May 17, 1997: INTERCOSTAL. CRACKED. INSPECTION FOUND A .5 AND .75 INCH CRACK IN AFT BAGGAGE BIN INTERCOSTAL BETWEEN FLOORBEAMS AT STA 1271 TO 1294. A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2. ## 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 19940913041069I](https://openairdocs.org/incident/19940913041069I), Sep 13, 1994: Doug DC982 (N72829), Panama City, FL. Deviating around thunderstorm. Hit cat at FL350. Seat belt sign not on. Two passengers minor injuries. ## Other aircraft with N72829 - [Cancelled 1974-09-23](https://openairdocs.org/deregistered/N72829-1974-09-23): Cessna 140, S/N 10015. Owner: [Wenkman Michael J](https://openairdocs.org/faa-owner/WENKMAN%20MICHAEL%20J), [Mcas Cherry Point, NC](https://openairdocs.org/faa-place/NC/Mcas%20Cherry%20Point) --- 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.