# N71828: 1987 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2005-10-31 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 31, 2005 - 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: 49488 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: March 20, 1987 - Certificate issued: June 9, 1993 - Last registry action: November 13, 2002 - Mode S code: A99C84 - 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/N71828 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=71828 - Page: https://openairdocs.org/deregistered/N71828-2005-10-31 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 (99, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0400419](https://openairdocs.org/sdr/CALA0400419), Apr 25, 2004: CHARGER. INOPERATIVE. COCKPIT, GALLEY AND FWD ENTRY EMERGENCY LIGHTS FAILED TO ILLUMINATE DURING TEST. REPLACED BATTERY CHARGER AND PACK PER AMM 33-53-00. - [SDR CALA0300681](https://openairdocs.org/sdr/CALA0300681), Dec 2, 2003: CHARGER. INOPERATIVE. THE BATTERY CHARGER FOR EMERGENCY EXIT LIGHTS AT THE L-2 DOOR WAS FOUND INOPERATIVE. THE CHARGER WAS REMOVED AND REPLACED IAW MM 33-53-00, PAGE 401. - [SDR CALA0200454](https://openairdocs.org/sdr/CALA0200454), Sep 7, 2002: CONTROL CABLE. OUT OF ADJUST. THE EXTERIOR TAIL CONE RELEASE HANDLE PULLED LOW AT 10 POUNDS. THE TAIL CONE CABLE TENSION WAS ADJUSTED AND THE HANDLE CLIPS WERE REPLACED. - [SDR CALA0200450](https://openairdocs.org/sdr/CALA0200450), Aug 31, 2002: LONGERON. CRACKED. INSPECTION FOUND A 1.5" CRACK IN LONGERON 2R AT STA 1418. REPAIRED LONGERON IAW SRM 53-02, FIGURE 18. - [SDR CALA0200449](https://openairdocs.org/sdr/CALA0200449), Aug 31, 2002: FRAME. CRACKED. INSPECTION FOUND A 2" CRACK IN TAIL COMPARTMENT BELTFRAME AT STA 1418, LONGERON 2R AND 2L. REPAIRED BELTFRAME IAW SRM 53-03-31A. - [SDR CALA0100759](https://openairdocs.org/sdr/CALA0100759), Aug 13, 2001: BATTERY. DEFECTIVE. THE FORWARD ENTRY PORTABLE EMERGENCY LIGHT ASSEMBLY BATTERIES WOULD NOT CHARGE. THE LIGHT ASSEMBLY NICAD BATTERIES WERE REPLACED AND OPERATION CHECKED GOOD. - [SDR CALA0001864](https://openairdocs.org/sdr/CALA0001864), Dec 6, 2000: BALLAST. BURNED. SMOKE ENTERED THE COCKPIT FROM BEHIND THE F/O'S SEAT WHILE ON FINAL APPROACH TO IAH. THE AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE UNDER ITS OWN POWER. THE - [SDR CALA000981](https://openairdocs.org/sdr/CALA000981), Jun 23, 2000: VALVE. LEAKING. WHEN THE LANDING GEAR WAS EXTENDED ON APPROACH TO SJC, THE MAIN GAER INDICATED DOWN AND LOCKED, BUT THE NOSE GEAR INDICATED UNSAFE. QRH PROCEDURES WERE COMPLIED - [SDR CALA0000675](https://openairdocs.org/sdr/CALA0000675), May 13, 2000: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED JUST INSIDE R-1 DOOR AT STA 200, RBL 54. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 53-05, FIGURE 55 AND EA 9-5311-2-AD67B. - [SDR CALA0000666](https://openairdocs.org/sdr/CALA0000666), May 10, 2000: ANGLE. CORRODED. INSPECTION FOUND SIDEWALL SUPPORT ANGLE CORRODED AT STA 1117 - 1136. THE SUPPORT ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-01. - [SDR CALA0000665](https://openairdocs.org/sdr/CALA0000665), May 10, 2000: WEB. CORRODED. INSPECTION FOUND LT CUSP WEB CORRODED AT STA 1130 - 1270, LBL 45 TO LBL 55. THE CUSP WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-04, 51-10-03 AND - [SDR CALA0000664](https://openairdocs.org/sdr/CALA0000664), May 10, 2000: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 200, RBL 44 TO RBL 54. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-05. - [SDR CALA0000663](https://openairdocs.org/sdr/CALA0000663), May 10, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND TWO FLOOR SUPPORT WEBS CORRODED FROM STA 140 - 200, RBL 54. THE FLOOR SUPPORT WEBS WERE REMOVED AND REPLACED IAW SRM 51-30-01. - [SDR CALA0000662](https://openairdocs.org/sdr/CALA0000662), May 10, 2000: SHEAR TIE. CORRODED. INSPECTION FOUND CORROSION UNDER SEALANT AT SHEAR TIE IN AFT CARGO AREA AT FS 1079 BETWEEN LONGERON 29R AND 30. THE SHEAR TIE WAS REMOVED AND A REPAIR WAS INSTA - [SDR CALA0000661](https://openairdocs.org/sdr/CALA0000661), May 10, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT STA 1136, LBL 54 (LOWER LEG OF TRACK AT CUSP WEB). THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-01. - [SDR CALA0000643](https://openairdocs.org/sdr/CALA0000643), May 8, 2000: ANGLE. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN LT SIDE DORSAL FIN TO FUSELAGE ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-4 AND 51-10-4. - [SDR CALA0000637](https://openairdocs.org/sdr/CALA0000637), May 6, 2000: WEB. CORRODED. INSPECTION FOUND LOWER SURFACE OF LT CUSP WEB IN AFT CARGO AREA CORRODED AT STA 1309. THE CORRODED AREA WAS REMOVED AND A NEW SECTION OF CUSP WEB WAS INSTALLED - [SDR CALA0000636](https://openairdocs.org/sdr/CALA0000636), May 6, 2000: PAN. CORRODED. INSPECTION FOUND MID CARGO DOOR LOWER PAN CORRODED. THE CORROSION WAS REMOVED AND A DOUBLER AND SPACER WERE INSTALLED IAW EA 9-5310-2-A0665 AND ECRA 5310-03027. - [SDR CALA0000635](https://openairdocs.org/sdr/CALA0000635), May 6, 2000: ACCESS PANEL. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN NR 1 RIGHT SLAT LOWER CUTOUT DOOR. THE CUTOUT DOOR WAS REMOVED AND REPLACED. - [SDR CALA0000634](https://openairdocs.org/sdr/CALA0000634), May 6, 2000: PAN. BENT. INSPECTION FOUND AFT CARGO DOOR BOTTOM LIP BENT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 4. - [SDR CALA0000633](https://openairdocs.org/sdr/CALA0000633), May 6, 2000: WEB. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN AFT AIRSTAIRS TOP STEP SUPPORT WEB. THE CRACKED AREA WAS CUT OUT AND BLENDED IAW SRM 53-01, FIGURE 2. A REPAIR WAS INSTALLED - [SDR CALA0000632](https://openairdocs.org/sdr/CALA0000632), May 6, 2000: WEB. CORRODED. INSPECTION FOUND LT CUSP WEB CORRODED AT STA 465 - 712 AS SEEN FROM MID AND FORWARD CARGO BAYS. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE - [SDR CALA0000631](https://openairdocs.org/sdr/CALA0000631), May 6, 2000: TAB. DENTED. INSPECTION FOUND LT AILERON CONTROL TAB AFT EDGE DENTED AND DELAMINATED. THE CONTROL TAB WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-10-02, SRM 57-03, AND - [SDR CALA0000630](https://openairdocs.org/sdr/CALA0000630), May 6, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LT SEAT TRACK CORRODED AT STA 1110 - 1220, LBL 44. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-04, 51-10-03, 51-30-01, AN - [SDR CALA0000629](https://openairdocs.org/sdr/CALA0000629), May 6, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 427 - 788, RBL 54. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-04, 51- - [SDR CALA0000628](https://openairdocs.org/sdr/CALA0000628), May 6, 2000: FLOORBOARD. DELAMINATED. INSPECTION FOUND CABIN RIGHT O/B FLOOR PANEL DELAMINATED AT STA 275 TO 313. THE CABIN FLOOR PANEL WAS REMOVED IAW SRM 51-30-04. A DOUBLER REPAIR WAS INSTALLED I - [SDR CALA0000627](https://openairdocs.org/sdr/CALA0000627), May 6, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 1140, LBL 54. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-02 AND 51-10 - [SDR CALA0000626](https://openairdocs.org/sdr/CALA0000626), May 6, 2000: WEB. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN CUSP WEB AT FS 112, RBL 47. THE CRACK WAS STOP DRILLED IAW 53-01, FIGURE 2 AND A DOUBLER WAS INSTALLED IAW SRM 53-01, 51-10- - [SDR CALA0000608](https://openairdocs.org/sdr/CALA0000608), May 2, 2000: CLIP. CRACKED. VERTICAL STAB LOWER AFT SPAR LEFT SIDE CLIP IS CRACKED (1). REMOVED AND REPLACED CLIP PER SRM 51-30 AND 51-30-05. - [SDR CALA0000607](https://openairdocs.org/sdr/CALA0000607), May 2, 2000: WEB. CORRODED. CUSP WEB IS CORRODED AT STA 1079 TO 1098 AT RBL 55. REMOVED AND REPLACED DAMAGED WEB SECTION PER SRM 51-30-01, 51-10-04, 51-10-03, AND 53-01 FIG 4. - [SDR CALA0000606](https://openairdocs.org/sdr/CALA0000606), May 2, 2000: SEAT TRACK. CORRODED. LEFT INBOARD SEAT TRACK IS CORRODED AT STA 1210 TO 1240 LBL 22. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK PER SRM 51-10-03, 53-05 FIG 4B-1, 51-10-04, 5 - [SDR CALA0000605](https://openairdocs.org/sdr/CALA0000605), May 2, 2000: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT CORRODED AT STA 1165 LBL 54. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-30-02, 51-10-03, 51-10-04, AND 51-30-02. - [SDR CALA0000604](https://openairdocs.org/sdr/CALA0000604), May 2, 2000: ATTACH FITTING. CORRODED. LEFT OUTBOARD GALLEY FITTING ATTACH OUTBOARD OF TRACK CORRODED AT FS 1174. REMOVED AND REPLACED FITTING PER SRM 51-10-04, 51-360-02, AND 51-30-05. - [SDR CALA0000603](https://openairdocs.org/sdr/CALA0000603), May 2, 2000: WEB. CORRODED. MAIN CABIN RIGHT SIDE STATION 237 CUSP WEB CRACKED AND CORRODED. REMOVED AND REPLACED CUSP WEB AND FRAME FOOT PER SRM 51-30-01 AND 51-30-05. - [SDR CALA0000602](https://openairdocs.org/sdr/CALA0000602), May 2, 2000: CARGO TRACK. CORRODED. MID CARGO RIGHT SIDE TIE DOWN TRACK CORRODED. REMOVED AND REPLACED DAMAGED SECTION OF TRACK PER SRM 51-10-03, 51-30-02, AND 51-30-01. - [SDR CALA0000601](https://openairdocs.org/sdr/CALA0000601), May 2, 2000: WEB. CORRODED. CUSP WEB IS CORRODED AT STA 1041 LBL 54 ON UPPER SURFACE OF FRAME. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER PER SRM 51-10-03, 51-30-02, AND 53-01 FIG 4 - [SDR CALA0000600](https://openairdocs.org/sdr/CALA0000600), May 2, 2000: FLOOR SUPPORT. CORRODED. MID CARGO RIGHT SIDE FLOOR SUPPORT ATTACH TO TIEDOWN TRACK CORRODED. REMOVED CORRODED SECTION AND REPLACED PER SRM 51-10-03, 51-10-04, AND 51-30-01. - [SDR CALA0000599](https://openairdocs.org/sdr/CALA0000599), May 2, 2000: SKIN. CRACKED. FORWARD CARGO DOOR OUTER SKIN IS CRACKED (5). STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER SRM 53-01, 52-05 FIG 32, AND 51-10-03. - [SDR CALA0000598](https://openairdocs.org/sdr/CALA0000598), May 2, 2000: PAN. CRACKED. FORWARD CARGO DOOR FORWARD LOWER SIDE PAN T/E BENT AND CRACKED (3). INSTALLED REPAIR DOUBLER PER SRM 52-01, 51-30-02, AND EC/RA5330-02819. - [SDR CALA0000597](https://openairdocs.org/sdr/CALA0000597), May 2, 2000: STRUCTURE. CRACKED. RIGHT MAIN LANDING GEAR DOOR UPPER CORNER CRACKED (1). REMOVED AND INSTALLED NEW CORNER PER SRM 52-84-0, 51-10-03, AND 51-30-02. - [SDR CALA0000593](https://openairdocs.org/sdr/CALA0000593), May 2, 2000: FITTING. CRACKED. FRAME FITTING UNDER SEAT TRACK CRACKED (1) AT STA 905 RBL 42. REMOVED AND REPLACED DAMAGED SECTION PER SRM 51-30-05, 51-10-03, AND 51-10-04. - [SDR CALA0000592](https://openairdocs.org/sdr/CALA0000592), May 2, 2000: SEAT TRACK. CORRODED. MAIN CABIN LEFT O/B SEAT TRACK AT LBL 54 IS CORRODED AT STA 1174 TO 1387. REMOVED AND REPLACED SEAT TRACK SECTION PER SRM 53-01 FIG 1, 51-10-03, AND 51-30-01. - [SDR CALA0000591](https://openairdocs.org/sdr/CALA0000591), May 2, 2000: WEB. CORRODED. STATION 896 TO 905 LEFT CUSP WEB AT LBL 55 IS CORRODED. REMOVED SEAT TRACK SECTION, FABRICATED AND INSTALLED FILLER PER SRM 51-30-01 AND 53-01 FIG 4. - [SDR CALA0000590](https://openairdocs.org/sdr/CALA0000590), May 2, 2000: WEB. CRACKED. STATION 807 LEFT CUSP HAS A VISIBLE 2 INCH CRACK O/B OF SEAT TRACK AT LBL 56. REPAIRED LT CUSP WEB PER SRM 53-01 FIG 4 AND 51-30-02. - [SDR CALA0000589](https://openairdocs.org/sdr/CALA0000589), May 2, 2000: SKIN. GOUGED. AFT CARGO DOOR FWD LIP OF DOOR FASTENER HOLES DAMAGED AND SKIN GOUGED. REPAIRED PER EA 9-5231-2-A0659 AND REMOVED AND REPLACED PER SRM 51-30-02. - [SDR CALA0000588](https://openairdocs.org/sdr/CALA0000588), May 2, 2000: FLOOR SUPPORT. DAMAGED. AFT CARGO FWD BULKHEAD LOWER FLOOR SUPPORT HAS SEVERAL TOOL MARKS BETWEEN LONG 28 RIGHT AND 28 LEFT. REMOVED AND REPLACED FLOOR SUPPORT AND INSTALLED SPLICE PER - [SDR CALA0000596](https://openairdocs.org/sdr/CALA0000596), May 1, 2000: WEB. CORRODED. CUSP WEB RIGHT SIDE IS CORRODED FROM STA 503 TO 750. REPLACED CUSP WEB PER SRM 51-30-02. - [SDR CALA0000595](https://openairdocs.org/sdr/CALA0000595), May 1, 2000: CARGO TRACK. CORRODED. AFT CARGO RIGHT AFT TIE DOWN TRACK IS CORRODED BETWEEN FS 1211 AND 1320. REMOVED AND REPLACED DAMAGED SECTION OF TRACK PER SRM 51-30-01, 51-10-01, AND 51-10-03. - [SDR CALA0000580](https://openairdocs.org/sdr/CALA0000580), Apr 27, 2000: CARGO TRACK. CORRODED. FORWARD CARGO RT TIE DOWN TRACK CORRODED BETWEEN FS 218 AND 370. REMOVED AND REPLACED TIE TRACK PER SRM 51-30-01. - [SDR CALA0000579](https://openairdocs.org/sdr/CALA0000579), Apr 27, 2000: DOOR. CRACKED. FORWARD CARGO BARRIER DOOR SUPPORT BEAM IS CRACKED AT FASTENER HOLE (1). STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER SRM 53-01 FIG 1, FIG 2, AND 51-30-0 All 99: https://openairdocs.org/deregistered/N71828-2005-10-31/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 19951005042199I](https://openairdocs.org/incident/19951005042199I), Oct 5, 1995: Doug DC982 (N71828), Omaha, NE. Narrative: on October 5, 1995, N71828, a DC-9-82 operated by Continental airlines, inc., as flt 723, was enroute from cleveland, oh to las vegas, NV when the… ## Other aircraft with N71828 - [Cancelled 1970-09-16](https://openairdocs.org/deregistered/N71828-1970-09-16): Luscombe 8A, S/N 3255. Owner: [Orland F Poage](https://openairdocs.org/faa-owner/ORLAND%20F%20POAGE), [Kansas City, MO](https://openairdocs.org/faa-place/MO/Kansas%20City) --- 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.