# N14810: 1984 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2015-05-20

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 20, 2015
- Status when cancelled: Sale reported, canceled
- 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-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 49264
- Year built: 1984
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: December 6, 1984
- Last registry action: June 25, 2013
- Mode S code: A0C2FC
- Location: [Marana, AZ](https://openairdocs.org/faa-place/AZ/Marana)
- Owner type: Individual
- Owner's area on the map: 32.3988° N, 111.3863° W: Placed by OpenAirDocs at the center of ZIP code 85653, within about 10 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N14810
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14810
- Page: https://openairdocs.org/deregistered/N14810-2015-05-20

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 (79, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR CALA0100854](https://openairdocs.org/sdr/CALA0100854), Sep 9, 2001: WEB. CRACKED. INSPECTION FOUND A 1" CRACK IN R/H MLG WHEEL WELL DOOR LOWER WEB. A REPAIR WAS INSTALLED IAW EA 9-5281-2-A0920 AND ECRA 5281-01017.
- [SDR CALA0100853](https://openairdocs.org/sdr/CALA0100853), Sep 9, 2001: SHEAR TIE. CRACKED. INSPECTION FOUND A 1" CRACK IN SHEAR TIE AT STA 1418 BETWEEN LONGERON 1R AND 2R. THE SHEAR TIE WAS REMOVED AND A NEW SHEAR TIE WAS INSTALLED IAW SRM 53-03, 51-3
- [SDR CALA0100852](https://openairdocs.org/sdr/CALA0100852), Sep 9, 2001: SEAT TRACK. CORRODED. INSPECTION FOUND SEAT TRACK CORRODED AT FS 200-218, LBL 45. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK, SPLICE, AND TAB WERE INSTALLED 
- [SDR CALA0100851](https://openairdocs.org/sdr/CALA0100851), Sep 9, 2001: WEB. CRACKED. INSPECTION FOUND A 4" CRACK IN FRAME TO LONGERON ATTACH WEB IN AFT ACCESSORY AREA AT FS 1430, R/H SIDE. THE CRACK WAS STOP DRILLED IAW SRM 53-01, FIGURE 2. A DO
- [SDR CALA0100850](https://openairdocs.org/sdr/CALA0100850), Sep 9, 2001: SKIN. GOUGED. INSPECTION FOUND L/H FUSELAGE SKIN GOUGED AFT OF L-1 DOOR AT STA 218. THE GOUGED SKIN SECTION WAS REMOVED AND A NEW SECTION OF SKIN WAS INSTALLED IAW SRM 51-30-
- [SDR CALA0100843](https://openairdocs.org/sdr/CALA0100843), Sep 8, 2001: SKIN. CORRODED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN HAD TWO SHEARED FASTENERS AT FS 1183 WITH CORROSION ON INSIDE. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-10-4, 51-
- [SDR CALA0100841](https://openairdocs.org/sdr/CALA0100841), Sep 7, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND AFT LT LAV FLOOR SUPPORT CORRODED AT STA 1309-1338, L18L. THE CORROSION WAS REMOVED IAW SRM 51-10-3 AND THE SUPPORT WAS REPAIRED IAW EA 9-5314-
- [SDR CALA0100839](https://openairdocs.org/sdr/CALA0100839), Sep 7, 2001: ANGLE. CORRODED. INSPECTION FOUND CUSP ANGLE CORRODED AT FS 207, LBL 54. THE CUSP ANGLE WAS REMOVED AND A NEW CUSP ANGLE WAS INSTALLED IAW SRM 51-30-1 AND EA 9-5310-2-A0917.
- [SDR CALA0100825](https://openairdocs.org/sdr/CALA0100825), Aug 31, 2001: PAN. CORRODED. INSPECTION FOUND FORWARD CARGO DOOR FRAME PAN CORRODED AROUND 10 EACH NUTS. THE PAN AND SPLICES WERE REMOVED IAW SRM 53-05, FIGURE 44. A NEW PAN AND SPLICE WERE
- [SDR CALA0100813](https://openairdocs.org/sdr/CALA0100813), Aug 27, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND CABIN FLOOR PANEL DELAMINATED AT FS 927-1003. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100812](https://openairdocs.org/sdr/CALA0100812), Aug 27, 2001: SEAT TRACK. CORRODED. INSPECTION FOUND MAIN DECK R/H SEAT TRACK CORRODED AT FS 250-788. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-5 AND 53-05, FIGUR
- [SDR CALA0100809](https://openairdocs.org/sdr/CALA0100809), Aug 27, 2001: WEB. CRACKED. INSPECTION FOUND WEB CRACKED IN FOUR PLACES AT CANTED FRAME STA 1463, I/B OF LONGERON 7L. THE WEB AND STIFFENERS WERE REMOVED AND A NEW WEB WAS INSTALLED IAW SR
- [SDR CALA0100800](https://openairdocs.org/sdr/CALA0100800), Aug 24, 2001: FLOOR PANEL. CORRODED. INSPECTION FOUND FORWARD ENTRY FLOOR PANELS WITH BROKEN AND CORRODED INSERTS AT FS 160-200, LBL 8 TO RBL 6 AND AT FS 200-256.
- [SDR CALA0100795](https://openairdocs.org/sdr/CALA0100795), Aug 24, 2001: WEB. CORRODED. INSPECTION FOUND CUSP WEB CRACKED AND CORRODED AT FS 218-239, LBL 44 TO LBL 55. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2, 51-10-3, AND 51
- [SDR CALA0100794](https://openairdocs.org/sdr/CALA0100794), Aug 24, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND CABIN FORWARD ENTRY FLOOR PANEL DELAMINATED. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100793](https://openairdocs.org/sdr/CALA0100793), Aug 24, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND CABIN R/H FLOOR PANEL DELAMINATED AT FS 245-313 AND A CREASE IN FLOOR PANEL AT FS 313-390. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100792](https://openairdocs.org/sdr/CALA0100792), Aug 24, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND CABIN CENTER FLOOR PANEL DELAMINATED AT FS 1003-1079. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100791](https://openairdocs.org/sdr/CALA0100791), Aug 24, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND CABIN CENTER AND L/H FLOOR PANELS DELAMINATED AT FS 769-807 AND FS 769-826. A R/H FLOOR PANEL AT FS 769-807 WAS FOUND TORN AT EDGES. NEW FLOOR 
- [SDR CALA0100790](https://openairdocs.org/sdr/CALA0100790), Aug 24, 2001: FLOOR PANEL. DAMAGED. INSPECTION FOUND RT CABIN FLOOR PANEL CREASED AT FS 466-542. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100789](https://openairdocs.org/sdr/CALA0100789), Aug 24, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND CABIN R/H FLOOR PANELS DELAMINATED AT FS 1193-1250 AND FS 1250-1309. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100788](https://openairdocs.org/sdr/CALA0100788), Aug 24, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND R/H CABIN FLOOR PANEL DELAMINATED AT FS 826-864 AND R/H CABIN FLOOR PANEL CRACKED AT FS 889-927. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-
- [SDR CALA0100787](https://openairdocs.org/sdr/CALA0100787), Aug 24, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND CABIN CENTER AND R/H FLOOR PANELS DELAMINATED AT FS 1079-1117 AND R/H FLOOR PANEL DELAMINATED AT FS 1117-1174. NEW FLOOR PANELS WERE INSTALLED 
- [SDR CALA0100786](https://openairdocs.org/sdr/CALA0100786), Aug 24, 2001: SKIN. DENTED. INSPECTION FOUND L/H FORWARD FUSELAGE EXTERIOR SKIN DENTED BELOW #2 CABIN WINDOW AT FS 264-285, LONGERON 16-18L. THE DENTED SECTION OF SKIN WAS REMOVED AND NEW 
- [SDR CALA0100783](https://openairdocs.org/sdr/CALA0100783), Aug 23, 2001: FLOOR PANEL. PUNCTURED. INSPECTION FOUND CABIN L/H AND R/H FLOOR PANELS PUNCTURED AT FS 1003-1079. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100782](https://openairdocs.org/sdr/CALA0100782), Aug 23, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND CABIN R/H FLOOR PANEL DELAMINATED AT FS 693-765. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100781](https://openairdocs.org/sdr/CALA0100781), Aug 23, 2001: FLOOR PANEL. PUNCTURED. INSPECTION FOUND CABIN L/H FLOOR PANEL PUNCTURED AT FS 927-1003. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100779](https://openairdocs.org/sdr/CALA0100779), Aug 23, 2001: FLOOR PANEL. TORN. INSPECTION FOUND CABIN CENTER FLOOR PANEL TORN BY INSERT HOLE AT FS 945-1003. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100778](https://openairdocs.org/sdr/CALA0100778), Aug 23, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND CABIN L/H FLOOR PANEL DELAMINATED AT FS 1250-1309. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100777](https://openairdocs.org/sdr/CALA0100777), Aug 23, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND CABIN CENTER FLOOR PANEL DELAMINATED AT FS 254-313. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100776](https://openairdocs.org/sdr/CALA0100776), Aug 23, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND COCKPIT CENTER FLOOR PANEL DELAMINATED AT FS 120-160. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100775](https://openairdocs.org/sdr/CALA0100775), Aug 23, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND CABIN CENTER FLOOR PANELS DELAMINATED AT FS 1250-1309 AND FS 1309-1347. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100774](https://openairdocs.org/sdr/CALA0100774), Aug 23, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND CABIN FORWARD ENTRY FLOOR PANEL C & J DELAMINATED. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100773](https://openairdocs.org/sdr/CALA0100773), Aug 23, 2001: FLOOR PANEL. CORRODED. INSPECTION FOUND FORWARD ENTRY FLOOR PANEL CORRODED AT FS 160-200, LBL 8-44. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100772](https://openairdocs.org/sdr/CALA0100772), Aug 23, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND CABIN CENTER FLOOR PANEL DELAMINATED AT FS 826-886. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100771](https://openairdocs.org/sdr/CALA0100771), Aug 23, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND CENTER CABIN FLOOR PANELS AT FS 1117-1174 AND FS 1174-1250 DELAMINATED. LEFT HAND CABIN FLOOR PANELS WERE FOUND DELAMINATED AT FS 1079-1155 AND
- [SDR CALA0100770](https://openairdocs.org/sdr/CALA0100770), Aug 23, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND COCKPIT FLOOR PANEL DELAMINATED AT FS 150-160, LBL 8-12. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100769](https://openairdocs.org/sdr/CALA0100769), Aug 23, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND CABIN L/H FLOOR PANEL DELAMINATED AROUND INSERT HOLES AT FS 673-763. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100763](https://openairdocs.org/sdr/CALA0100763), Aug 16, 2001: INTERCOSTAL. CORRODED. INSPECTION FOUND INTERCOSTAL CORRODED AT FS 1308-1322, LONGERONS 27L-28L. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA0001965](https://openairdocs.org/sdr/CALA0001965), Dec 19, 2000: STRUT. DISCHARGED. THE NLG WOULD NOT RETRACT AFTER TAKEOFF FROM IND. THE AIRCRAFT WAS RETURNED TO IND WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE STRUT PRESSURE L
- [SDR CALA9901295](https://openairdocs.org/sdr/CALA9901295), Sep 24, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND RT SEAT TRACK CORRODED AT FS 1007-1320, RBL 24. THE SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-30-2 AND 51-30-1.
- [SDR CALA9901294](https://openairdocs.org/sdr/CALA9901294), Sep 24, 1999: PANEL. CRACKED. INSPECTION FOUND A 3 CRACK IN VERTICAL STABILIZER PANEL ON LT SIDE. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-01, FIGURE 2, SHEET 2, 51-60-0, PAGE 5, 51-30-5, A
- [SDR CALA9901277](https://openairdocs.org/sdr/CALA9901277), Sep 22, 1999: SKIN. DENTED. INSPECTION FOUND LT SLAT 0 DENTED. THE DENTED AREA WAS CUT OUT IAW SRM 57-6, FIGURE 1. A REPAIR WAS INSTALLED IAW ECRA 5720-01170.
- [SDR CALA9901266](https://openairdocs.org/sdr/CALA9901266), Sep 19, 1999: FAIRING. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN RT HORIZONTAL STABILIZER FAIRING. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA9901265](https://openairdocs.org/sdr/CALA9901265), Sep 19, 1999: DOUBLER. CORRODED. INSPECTION FOUND DOUBLER AT SILL OF DOOR JAMB CORRODED AT FS 1174-1183, LONGERON 27R (AFT PIT). THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 
- [SDR CALA9901264](https://openairdocs.org/sdr/CALA9901264), Sep 19, 1999: VANE. GOUGED. INSPECTION FOUND RT WING O/B NR 2 FIXED VANE GOUGED. THE FIXED VANE WAS REMOVED AND REPAIRED IAW DRAWING NR SR09570025. THE VANE WAS REINSTALLED IAW MM 27-51-03
- [SDR CALA9901263](https://openairdocs.org/sdr/CALA9901263), Sep 19, 1999: SKIN. DELAMINATED. INSPECTION FOUND RT GROUND SPOILER DELAMINATED. THE SPOILER WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-62-01.
- [SDR CALA9901262](https://openairdocs.org/sdr/CALA9901262), Sep 19, 1999: VANE. PUNCTURED. INSPECTION FOUND LT WING I/B FIXED VANE PUNCTURED ON TOP CENTER. THE VANE WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-51-03.
- [SDR CALA9901261](https://openairdocs.org/sdr/CALA9901261), Sep 19, 1999: PAN. CORRODED. INSPECTION FOUND FORWARD CARGO DOOR PAN LOWER SIDE CORRODED AROUND RIB NUTS. THE PAN WAS REMOVED AND A NEW PAN WAS INSTALLED IAW SRM 51-30-2, 51-30-5, 51-30-1, 
- [SDR CALA9901260](https://openairdocs.org/sdr/CALA9901260), Sep 19, 1999: SUPPORT. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN MID CARGO PIT LEFT CEILING SUPPORT AT STA 731, LBL 24. THE CRACK WAS STOP DRILLED IAW SRM 53-01, FIGURE 2. A REPAIR DOUBLER W
- [SDR CALA9901259](https://openairdocs.org/sdr/CALA9901259), Sep 18, 1999: FITTING. CORRODED. INSPECTION FOUND RT GALLEY SUPPORT FITTING CORRODED AT FS 200, RBL 48. THE GALLEY SUPPORT FITTING WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-30-2.

All 79: https://openairdocs.org/deregistered/N14810-2015-05-20/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 19910730043909I](https://openairdocs.org/incident/19910730043909I), Jul 30, 1991: Doug DC982 (N14810), New York, NY, Substantial damage. Ground personnel repositioning aircraft to overnight parking spot was struck by fuel truck. No lights on aircraft.

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