# N16813: 1981 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2002-11-13

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 13, 2002
- Exported to: Indonesia
- Status when cancelled: Second triennial mailing, no response
- 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: 48066
- Year built: 1981
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: December 17, 1985
- Certificate issued: August 21, 1990
- Last registry action: February 4, 1998
- Mode S code: A111FD
- Owner when cancelled: [Eal Delaware Xi Corp](https://openairdocs.org/faa-owner/EAL%20DELAWARE%20XI%20CORP)
- Location: [Stamford, CT](https://openairdocs.org/faa-place/CT/Stamford)
- Owner type: Corporation
- Owner's area on the map: 41.0593° N, 73.5444° W: Placed by OpenAirDocs at the center of ZIP code 06902, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N16813
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=16813
- Page: https://openairdocs.org/deregistered/N16813-2002-11-13

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 (98, newest 50)

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

- [SDR CALA0200443](https://openairdocs.org/sdr/CALA0200443), Aug 27, 2002: SKIN. CORRODED. INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 275 LONGERON 30 AFT OF LOWER ADF ANTENNA. THE SKIN SECTION WAS REMOVED AND REPLACED IAW SRM 51-30-02.
- [SDR CALA0100712](https://openairdocs.org/sdr/CALA0100712), Jul 29, 2001: FLOOR PANEL. CORRODED. INSPECTION FOUND FORWARD ENTRY FLOOR PANEL AT R-1 DOOR JAMB CORRODED, FS 160-200, RBL 48. THE FLOOR PANEL AND SUPPORT WERE REMOVED AND A NEW FLOOR PANEL AND SUP
- [SDR CALA0100693](https://openairdocs.org/sdr/CALA0100693), Jul 25, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND MAIN CABIN R/H I/B FLOOR PANEL DELAMINATED AT FS 1003-1079. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100657](https://openairdocs.org/sdr/CALA0100657), Jul 16, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND CAPTAIN'S R/H SIDE AFT FLOORBOARD DELAMINATED. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-01.
- [SDR CALA0100653](https://openairdocs.org/sdr/CALA0100653), Jul 12, 2001: DOOR FRAME. DENTED. INSPECTION FOUND R-1 DOOR JAMB DENTED AT AFT LATCHING MECHANISM. THE BAYONET ROLLER ATTACH ARM WAS REMOVED IAW SRM 51-30-01. A REPAIR DOUBLER AND SHIM WERE INST
- [SDR CALA0100638](https://openairdocs.org/sdr/CALA0100638), Jul 7, 2001: SKIN. DENTED. INSPECTION FOUND L/H FORWARD FUSELAGE EXTERNAL SKIN DENTED AT FS 120, LONGERON 18L. THE DENT WAS COLD WORKED AND A REPAIR DOUBLER WAS INSTALLED IAW EA 9-5331-2-
- [SDR CALA0100636](https://openairdocs.org/sdr/CALA0100636), Jul 6, 2001: SLAT. DENTED. INSPECTION FOUND R/H WING #2 SLAT DENTED AT LEADING EDGE. THE DENT WAS FILLED IAW SRM 57-03, FIGURE 20A & B.
- [SDR CALA0100635](https://openairdocs.org/sdr/CALA0100635), Jul 6, 2001: ANGLE. CORRODED. INSPECTION FOUND LT CUSP ANGLE CORRODED ON UPPER SURFACE AT AFT END OF L-1 DOOR ENTRANCE, STA 186. THE AREA WAS REPAIRED IAW EA 9-5310-2-A0895 AND ECRA 5310-041
- [SDR CALA0100632](https://openairdocs.org/sdr/CALA0100632), Jul 3, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND MID CARGO RT BULKHEAD FLOOR SUPPORT CORRODED AT FS 541. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51
- [SDR CALA0100631](https://openairdocs.org/sdr/CALA0100631), Jul 3, 2001: DOOR FRAME. CRACKED. INSPECTION FOUND A 5 INCH CRACK IN DOOR JAMB SKIN TANG AT AFT END OF L-1 DOOR, FS 207, LONGERON 11L. A 1 INCH CRACK WAS FOUND IN THE DOOR JAMB SKIN TANG AT FS 2
- [SDR CALA0100629](https://openairdocs.org/sdr/CALA0100629), Jul 2, 2001: SKIN. DENTED. INSPECTION FOUND AFT CARGO DOOR EXTERIOR SKIN DENTED. THE SKIN WAS REPAIRED IAW SRM 52-05, PAGE 2.
- [SDR CALA0100628](https://openairdocs.org/sdr/CALA0100628), Jul 1, 2001: DOUBLER. CRACKED. INSPECTION FOUND A 3" CRACK IN EXISTING DOUBLER REPAIR AT LOWER FORWARD CARGO DOOR. THE EXISTING DOUBLER WAS REMOVED AND THE CRACK WAS STOP DRILLED IAW SRM 51-1
- [SDR CALA0100627](https://openairdocs.org/sdr/CALA0100627), Jul 1, 2001: WEB. CORRODED. INSPECTION FOUND FORWARD PIT(TORQUE BOX) FWD CLOSEOUT AT LIGHTENING HOLE(SLANT PANEL) CORRODED AT AND AROUND FASTENER HOLES AT FS 336. REMOVED FITTING, WEB, AND
- [SDR CALA0100623](https://openairdocs.org/sdr/CALA0100623), Jun 30, 2001: PAN. CORRODED. INSPECTION FOUND FORWARD PIT DOOR PAN BETWEEN TWO LOWER STOPS AT DRAIN HOLE CORRODED. THE CORRODED AREA WAS CUT OUT IAW SRM 53-05, FIGURE 44. A NEW LOWER PAN AN
- [SDR CALA0100622](https://openairdocs.org/sdr/CALA0100622), Jun 30, 2001: ANGLE. CORRODED. INSPECTION FOUND JACK SUPPORT ANGLE CORRODED IN CHANNEL AREA AT BOTTOM OF APB, FS 1338, LONGERON 30. THE JACK SUPPORT ANGLE AND VERTICAL CHANNEL STRINGER TIE FI
- [SDR CALA0100621](https://openairdocs.org/sdr/CALA0100621), Jun 30, 2001: SKIN. GOUGED. INSPECTION FOUND LOWER SURFACE OF SKIN PANEL #1613 GOUGED AT R/H I/B FLAP T/E AREA. THE PANEL SKIN WAS REMOVED AND NEW SKIN WAS INSTALLED IAW SRM 51-30-2, 57-50
- [SDR CALA0100619](https://openairdocs.org/sdr/CALA0100619), Jun 29, 2001: WEB. CORRODED. INSPECTION FOUND CUSP WEB CORRODED AT LOWER CORNER FORWARD END OF R-1 DOOR JAMB, FS 160 - 238. THE LOWER DOOR PAN, TWO TORQUE BOX WEB PANELS, STRAPS, AND COMPOS
- [SDR CALA0100618](https://openairdocs.org/sdr/CALA0100618), Jun 29, 2001: FLOOR PANEL. PUNCTURED. INSPECTION FOUND R/H CABIN FLOOR PANEL PUNCTURED AT STA 256-313 SIDEWALL SUPPORT STRUCTURE. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51
- [SDR CALA0100617](https://openairdocs.org/sdr/CALA0100617), Jun 29, 2001: WEB. CORRODED. INSPECTION FOUND MAIN CABIN CUSP WEB CORRODED AT FS 202-218, RBL 54. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-02, 51-10-4, AND 51-10-3.
- [SDR CALA0100615](https://openairdocs.org/sdr/CALA0100615), Jun 26, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 160 - 196, LBL 44. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-4, 51-10-3, A
- [SDR CALA0100614](https://openairdocs.org/sdr/CALA0100614), Jun 26, 2001: FLOOR SUPPORT. CRACKED. INSPECTION FOUND A 6 INCH CRACK IN COCKPIT CENTER FLOORBOARD CENTER FLOOR SUPPORT AT FS 140, BL 0. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INS
- [SDR CALA0100613](https://openairdocs.org/sdr/CALA0100613), Jun 26, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 160 - 195, LBL 56. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-4 AND 51-30-2
- [SDR CALA0100612](https://openairdocs.org/sdr/CALA0100612), Jun 26, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 157 - 200, RBL 6. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-4, 51-10-1, AN
- [SDR CALA0100611](https://openairdocs.org/sdr/CALA0100611), Jun 26, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 157 - 198, RBL 45. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-4, 51-10-3, A
- [SDR CALA0100610](https://openairdocs.org/sdr/CALA0100610), Jun 26, 2001: CARGO TRACK. CORRODED. INSPECTION FOUND FORWARD PIT RT SIDE CARGO TIE DOWN TRACK CORRODED AT LOWER SIDE OF FASTENER HOLES FROM FS 218 TO FORWARD DOOR FRAME. THE TIE DOWN TRACK AND ATT
- [SDR CALA0100609](https://openairdocs.org/sdr/CALA0100609), Jun 26, 2001: WEB. CORRODED. INSPECTION FOUND LT FLOOR CUSP WEB BEHIND LAV AREA CORRODED AT FS 218 - 228, LBL 45 - 56. THE CUSP WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2, 
- [SDR CALA0100608](https://openairdocs.org/sdr/CALA0100608), Jun 26, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT IN CENTER CARGO PIT CORRODED ON UPPER SURFACE AT FS 636 FROM LONGERON 29R-28L. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPP
- [SDR CALA0100607](https://openairdocs.org/sdr/CALA0100607), Jun 26, 2001: WEB. CORRODED. INSPECTION FOUND FORWARD ENTRY SUBFLOOR CORRODED AT FS 160 - 200, RBL 56. THE FLOOR SUPPORTS AND WEB SUPPORTS WERE REMOVED TO GAIN ACCESS TO SUBFLOOR. THE SUBFL
- [SDR CALA0100606](https://openairdocs.org/sdr/CALA0100606), Jun 26, 2001: WEB. CRACKED. INSPECTION FOUND CUSP WEB CRACKED IN TWO PLACES AT FS 218 - 238, RBL 54. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2 AND 51-30-4.
- [SDR CALA0100605](https://openairdocs.org/sdr/CALA0100605), Jun 25, 2001: SKIN. DENTED. INSPECTION FOUND L/H FUSELAGE EXTERNAL SKIN CREASED AND DENTED AT FS 389, LONGERON 22L. THE DAMAGED AREA WAS REFORMED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-
- [SDR CALA0100604](https://openairdocs.org/sdr/CALA0100604), Jun 25, 2001: ANGLE. CORRODED. INSPECTION FOUND MAIN CABIN WEB ATTACH ANGLE CORRODED AT FS 200-214, LBL 54. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-3 AND 51-30-5.
- [SDR CALA0100603](https://openairdocs.org/sdr/CALA0100603), Jun 25, 2001: SHEAR TIE. CRACKED. INSPECTION FOUND A 1" CRACK IN FORWARD CARGO SHEAR TIE AT FS 370, LONGERON 22-23L. THE CRACKED AREA WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01
- [SDR CALA0100600](https://openairdocs.org/sdr/CALA0100600), Jun 25, 2001: FLOOR PANEL. CORRODED. INSPECTION FOUND CABIN FLOOR PANEL "F" CORRODED AROUND FASTENER HOLES. THE PANEL WAS REPLACED IAW SRM 53-21-0 AND 51-10-3.
- [SDR CALA0100599](https://openairdocs.org/sdr/CALA0100599), Jun 25, 2001: FLOOR PANEL. CRACKED. INSPECTION FOUND L/H O/B FLOOR PANEL CRACKED AROUND SCREW HOLES AT BOTH ENDS, STA 826-927. A DOUBLER WAS INSTALLED AT EACH END IAW SRM 53-01, FIGURE 4 AND 51-10
- [SDR CALA0100598](https://openairdocs.org/sdr/CALA0100598), Jun 25, 2001: SKIN. DENTED. INSPECTION FOUND R/H FUSELAGE EXTERNAL SKIN DENTED AT FS 579 BETWEEN LONGERONS 20R AND 21R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.
- [SDR CALA0100597](https://openairdocs.org/sdr/CALA0100597), Jun 24, 2001: SKIN. DENTED. INSPECTION FOUND R/H FUSELAGE EXTERNAL SKIN DENTED AT FS 541 BETWEEN LONGERONS 20R AND 21R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.
- [SDR CALA0100596](https://openairdocs.org/sdr/CALA0100596), Jun 24, 2001: SKIN. DENTED. INSPECTION FOUND R/H EXTERNAL FUSELAGE SKIN DENTED AT FS 370 JUST BELOW LONGERON 20R. THE DENTED AREA WAS COLD WORKED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM
- [SDR CALA0100595](https://openairdocs.org/sdr/CALA0100595), Jun 24, 2001: SEAT TRACK. CORRODED. INSPECTION FOUND MAIN CABIN SEAT TRACK CORRODED AT FS 1070-1203, LBL 25. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW S
- [SDR CALA0100594](https://openairdocs.org/sdr/CALA0100594), Jun 24, 2001: WEB. CORRODED. INSPECTION FOUND LT FLOOR CUSP WEB CORRODED ON LOWER SURFACE AT FS 1117. THE CORRODED AREA WAS REMOVED AND A NEW CUSP WEB WAS INSTALLED IAW SRM 51-30-2, 51-10-4
- [SDR CALA0100593](https://openairdocs.org/sdr/CALA0100593), Jun 24, 2001: FITTING. CORRODED. INSPECTION FOUND ATTACH FITTING(FORWARD OF L-2 DOOR) CORRODED AT FS 1136, LBL 56. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-1, 51-30
- [SDR CALA0100592](https://openairdocs.org/sdr/CALA0100592), Jun 24, 2001: WEB. CORRODED. INSPECTION FOUND MAIN CABIN CUSP WEB CORRODED AT FS 1174 - 1193, LBL 54. THE CORRODED AREA WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND
- [SDR CALA0100589](https://openairdocs.org/sdr/CALA0100589), Jun 23, 2001: SEAT TRACK. CORRODED. INSPECTION FOUND SEAT TRACK CORRODED AT FS 1097-1215, LBL 45. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-10-3.
- [SDR CALA0100588](https://openairdocs.org/sdr/CALA0100588), Jun 23, 2001: ANGLE. CORRODED. INSPECTION FOUND L/H MAIN CABIN T-ANGLE CORRODED AT FS 1140. THE T-ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-3, 51-10-4, 51-10-5, AND 51-30-
- [SDR CALA0100587](https://openairdocs.org/sdr/CALA0100587), Jun 23, 2001: ANGLE. CORRODED. INSPECTION FOUND AFT ENTRY DOOR Z-ANGLE COMMON TO CUSP MEMBRANE CORRODED AT FS 1136-1174, LBL 48.5. THE Z-ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SR
- [SDR CALA0100586](https://openairdocs.org/sdr/CALA0100586), Jun 23, 2001: CHANNEL. CORRODED. INSPECTION FOUND AFT ENTRY DOOR SEAL AREA AFT HAT CHANNEL FOR THRESHOLD CORRODED. THE HAT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-30-2 AN
- [SDR CALA0100585](https://openairdocs.org/sdr/CALA0100585), Jun 22, 2001: SKIN. DENTED. INSPECTION FOUND R/H WING SKIN I/B LOWER SURFACE NICKED AND DENTED. NEW SKIN WAS FABRICATED AND INSTALLED IAW SRM 51-60-4 AND 51-30-2.
- [SDR CALA0100584](https://openairdocs.org/sdr/CALA0100584), Jun 22, 2001: FITTING. CORRODED. INSPECTION FOUND CABIN FRAME TO WEB FITTING CORRODED AT FS 160, RBL 56. THE FRAME FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-01, 51-30-05, AND 51-10-4.
- [SDR CALA0100583](https://openairdocs.org/sdr/CALA0100583), Jun 22, 2001: SKIN. DENTED. INSPECTION FOUND L/H FUSELAGE EXTERNAL SKIN DENTED AT FS 474 JUST ABOVE LONGERON 21L. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 3B.
- [SDR CALA0100579](https://openairdocs.org/sdr/CALA0100579), Jun 22, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND CABIN FLOOR PANEL DELAMINATED AT STA 1041-1117. THE FLOOR PANEL WAS REPLACED IAW ECRA 5320-01265.
- [SDR CALA0100578](https://openairdocs.org/sdr/CALA0100578), Jun 22, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND CABIN FLOOR PANELS I & J AT LT FORWARD ENTRY DELAMINATED. THE FLOOR PANELS WERE REPLACED IAW ECRA 5320-01265.

All 98: https://openairdocs.org/deregistered/N16813-2002-11-13/reports.md

## FAA accident and incident reports (2)

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 19970517019119I](https://openairdocs.org/incident/19970517019119I), May 17, 1997: Doug DC982 (N16813), Cleveland, OH. Cabin pressure began uncontrolled climb. Descended. Returned to airport. Replaced right acm.
- [Incident 19930917038009I](https://openairdocs.org/incident/19930917038009I), Sep 17, 1993: Doug DC982 (N16813), Des Moines, IA. Oil pressure dropped to zero. Diverted to Des Moines. Blue ice from leaking forward lav ingested in left engine.

## Other aircraft with N16813

- [Cancelled 2008-04-29](https://openairdocs.org/deregistered/N16813-2008-04-29): Cessna 172R, S/N 17281432, built 2007. Exported to China. Owner: [Aircraft Packaging And Shipping LLC](https://openairdocs.org/faa-owner/AIRCRAFT%20PACKAGING%20AND%20SHIPPING%20LLC), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)
- [Cancelled 1970-06-19](https://openairdocs.org/deregistered/N16813-1970-06-19): Douglas DC3C, S/N 42-93012. Exported to Ecuador. Owner: [Weeks David S](https://openairdocs.org/faa-owner/WEEKS%20DAVID%20S), [Delray Beach, FL](https://openairdocs.org/faa-place/FL/Delray%20Beach)

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