# N962AS: 1992 Mcdonnell Douglas DC-9-83(MD-83), registration cancelled 2010-09-24

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 24, 2010
- Status when cancelled: Valid registration
- Airframe: [Mcdonnell Douglas DC-9-83(MD-83)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83) (registry code 3022083)
- 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: 53076
- Year built: 1992
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: April 6, 1992
- Certificate issued: September 10, 2010
- Last registry action: September 10, 2010
- Mode S code: AD63A5
- Owner when cancelled: [Avioserv San Diego Inc](https://openairdocs.org/faa-owner/AVIOSERV%20SAN%20DIEGO%20INC)
- Location: [San Diego, CA](https://openairdocs.org/faa-place/CA/San%20Diego)
- Owner type: Corporation
- Owner's area on the map: 32.8971° N, 117.2016° W: Placed by OpenAirDocs at the center of ZIP code 92121, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N962AS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=962AS
- Page: https://openairdocs.org/deregistered/N962AS-2010-09-24

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-9-83(MD-83): https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83.md

## Service difficulty reports (187, newest 50)

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

- [SDR ASAA0781782](https://openairdocs.org/sdr/ASAA0781782), Jun 7, 2007: CUSP WEB. CORRODED. RIGHT CUSP WEB CORRODED. REMOVED DAMAGED AREA. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 53-05.
- [SDR ASAA0781781](https://openairdocs.org/sdr/ASAA0781781), Jun 7, 2007: CUSP WEB. CORRODED. RIGHT CUSP WEB CORRODED. REMOVED DAMAGED AREA. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 53-01 AND 53-05.
- [SDR ASAA0781780](https://openairdocs.org/sdr/ASAA0781780), Jun 7, 2007: CUSP WEB. CORRODED. RIGHT CUSP WEB CORRODED. REMOVED DAMAGED AREA. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 53-01, 51-70-4 AND 51-70-4.
- [SDR ASAA0781779](https://openairdocs.org/sdr/ASAA0781779), Jun 7, 2007: CUSP WEB. CORRODED. RIGHT CUSP WEB CORRODED. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER PER SRM 53-05 AND 53-01.
- [SDR ASAA0781778](https://openairdocs.org/sdr/ASAA0781778), Jun 3, 2007: INSERT. CORRODED. CABIN FLOOR PANEL HAS NUMEROUS CORRODED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND DWG 4932106.
- [SDR ASAA0781777](https://openairdocs.org/sdr/ASAA0781777), Jun 3, 2007: SKIN. DENTED. RIGHT INBOARD FLAP INBOARD VANE HAS SEVERAL DENTS ON LOWER SURFACE. PREPARED DAMAGED SURFACE FOR BONDING. INSTALLED REPAIR DOUBLER PER SRM 51-70-2.
- [SDR ASAA0781776](https://openairdocs.org/sdr/ASAA0781776), Jun 3, 2007: SKIN. CHAFED. LEFT OUTBOARD FLAP VANE LEADING EDGE IS CHAFED AT INBOARD SIDE. REMOVED DAMAGED EXISTING DOUBLER. INSTALLED REPLACEMENT DOUBLER PER SRM 51-70-2.
- [SDR ASAA0781775](https://openairdocs.org/sdr/ASAA0781775), Jun 3, 2007: SKIN. DENTED. LEFT INBOARD FLAP OUTBOARD VANE LOWER INBOARD SURFACE HAS MULTIPLE DENTS. PREPARED DAMAGED AREA FOR BONDING. INSTALLED REPAIR DOUBLER PER SRM 51-70-2.
- [SDR ASAA0781774](https://openairdocs.org/sdr/ASAA0781774), Jun 3, 2007: DOUBLER. DEBONDED. EXISTING REPAIR DISBONDED ON LOWER SURFACE OF LEFT ELEVATOR GEARED TAB. PREPARED DAMAGED AREA FOR BONDING. INSTALLED FILLER AND DOUBLER PER SRM 51-70-2.
- [SDR ASAA0781733](https://openairdocs.org/sdr/ASAA0781733), May 30, 2007: WEB. DAMAGED. DOUBLE DRILLED HOLES ON WEB UNDER FWD CABIN FLOORBOARD SUPPORT ANGLE. CUT OUT DAMAGED AREA OF WEB, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM 
- [SDR ASAA0781732](https://openairdocs.org/sdr/ASAA0781732), May 30, 2007: SKIN. DENTED. FUSELAGE SKIN DENTED A PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR. CUT OUT DAMAGED AREA OF SKIN. FABRICATED AND INSTALLED A SKIN FILLER INTERNAL REPAIR DOUBLERS, 
- [SDR ASAA0781731](https://openairdocs.org/sdr/ASAA0781731), May 30, 2007: CHANNEL. DAMAGED. CABIN FLOOR PANEL HAS A DAMAGED HAT CHANNEL. LOCATED AND DRILLED A REPLACEMENT HAT CHANNEL IAW SRM 51-10-4, 51-30-2 AND DAC DWG 9957918.
- [SDR ASAA0781730](https://openairdocs.org/sdr/ASAA0781730), May 30, 2007: FLOOR PANEL. DAMAGED. CABIN FLOOR PANEL HAS EDGE DAMAGE. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-03 PG 122B AND DCA DWG S4932106.
- [SDR ASAA0781729](https://openairdocs.org/sdr/ASAA0781729), May 30, 2007: FLOOR PANEL. DAMAGED. CABIN FLOOR PANEL IS DELAMINATED. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781728](https://openairdocs.org/sdr/ASAA0781728), May 30, 2007: FLOOR PANEL. DAMAGED. CABIN FLOOR PANEL HAS TEN DAMAGED INSERTS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781727](https://openairdocs.org/sdr/ASAA0781727), May 30, 2007: FLOOR PANEL. DETERIORATED. CABIN FLOOR PANEL HAS NUMEROUS DAMAGED INSERTS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781726](https://openairdocs.org/sdr/ASAA0781726), May 30, 2007: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL IS DELAMINATED. FABRICATED A REPLACEMENT PANEL IAW SRM 53-05 PARA 44 AND DCA DWG S4932106.
- [SDR ASAA0781725](https://openairdocs.org/sdr/ASAA0781725), May 30, 2007: FLOOR PANEL. DETERIORATED. CABIN FLOOR PANEL IS BROKEN AT AN INSERT. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781724](https://openairdocs.org/sdr/ASAA0781724), May 30, 2007: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL DELAMINATED. FABRICATED REPLACEMENT FLOOR PANEL IAW SRM 53-05 PG 122B FIGURES 50 AND 50A AND DCA DWG 9936640.
- [SDR ASAA0781723](https://openairdocs.org/sdr/ASAA0781723), May 30, 2007: CUSP WEB. CORRODED. PASSENGER CABIN CUSP WEB IS CORRODED. REMOVED CORRODED WEB LOCATED DRILLED AND INSTALLED A REPLACEMENT WEB IAW SRM 51-30-2.
- [SDR ASAA0781722](https://openairdocs.org/sdr/ASAA0781722), May 30, 2007: CUSP WEB. CORRODED. PASSENGER CABIN FLOOR CUSP WEB IS CORRODED. REMOVED THE CORRODED CUSP WEB LOCATED DRILLED AND INSTALLED A REPLACEMENT CUSP WEB IAW SRM 51-10-4 PG 1 AND 4 FIG 3 
- [SDR ASAA0781721](https://openairdocs.org/sdr/ASAA0781721), May 30, 2007: WEB. CRACKED. PASSENGER CABIN FLOOR WEB IS CRACKED. CUT OUT DAMAGED AREA OF WEB, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM 51-70-4 FIG 2.
- [SDR ASAA0781720](https://openairdocs.org/sdr/ASAA0781720), May 30, 2007: CUSP WEB. CRACKED. PASSENGER CABIN FLOOR RT CUSP WEB IS CRACKED. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781719](https://openairdocs.org/sdr/ASAA0781719), May 30, 2007: FLOOR SUPPORT. CORRODED. PASSENGER CABIN FLOOR SUPPORT IS CORRODED. FABRICATED AND INSTALLED A REPLACEMENT FLOOR SUPPORT IAW SRM 51-10-4 PG 1 AND 51-30-1 PARA 1 AND PARA 11.
- [SDR ASAA0781718](https://openairdocs.org/sdr/ASAA0781718), May 30, 2007: FLOOR SUPPORT. CORRODED. PASSENGER CABIN FLOOR SUPPORT IS CORRODED. FABRICATED AND INSTALLED A REPLACEMENT FLOOR SUPPORT IAW SRM 51-10-4 PG 1 AND 51-30-1 PG 4.
- [SDR ASAA0781746](https://openairdocs.org/sdr/ASAA0781746), May 29, 2007: FRAME. CORRODED. AFT CARGO FRAME AT STA 1307.091 CORRODED. LOCATED AND DRILLED A REPLACEMENT FRAME SECTION AND REPAIR PARTS AND INSTALLED IAW SRM 53-03 FIG 2A AND SRM 51-30-2.
- [SDR ASAA0781745](https://openairdocs.org/sdr/ASAA0781745), May 29, 2007: SKIN. DENTED. EXTERNAL FUSELAGE DENTED AT STA 579 BETWEEN LONG 20L AND 21L. MEASURED DENT AT 4.0 X .015 INCH WITHIN LIMITS PER SRM. REPAIRED IAW SRM 53-04 FIG 38 SHEETS 12 AN
- [SDR ASAA0781744](https://openairdocs.org/sdr/ASAA0781744), May 29, 2007: SKIN. DENTED. AFT CARGO DOOR EXTERIOR SKIN IS DENTED 22 INCHES FROM THE AFT EDGE 14 INCHES FROM THE TOP EDGE. CUT OUT DAMAGED AREA OF SKIN, FABRICATED AND INSTALLED REPAIR DO
- [SDR ASAA0781743](https://openairdocs.org/sdr/ASAA0781743), May 29, 2007: INSERT. CORRODED. CABIN FLOOR PANEL HAS NUMERIOUS INSERTS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781742](https://openairdocs.org/sdr/ASAA0781742), May 29, 2007: INSERT. CORRODED. CABIN FLOOR PANEL HAS NUMEROUS CORRODED INSERTS. FABRICATED A REPLACEMENT PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781741](https://openairdocs.org/sdr/ASAA0781741), May 29, 2007: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL IS DELAMINATED. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781740](https://openairdocs.org/sdr/ASAA0781740), May 29, 2007: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL IS DELAMINATED. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781739](https://openairdocs.org/sdr/ASAA0781739), May 29, 2007: INSERT. CORRODED. CABIN FLOOR PANEL HAS NUMEROUS CORRODED INSERTS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781738](https://openairdocs.org/sdr/ASAA0781738), May 29, 2007: INSERT. CORRODED. CABIN FLOOR PANEL HAS NUMEROUS CORRODED INSERTS. FABRICATED A REPLACEMENT PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781737](https://openairdocs.org/sdr/ASAA0781737), May 29, 2007: FLOOR PANEL. DETERIORATED. CABIN FLOOR PANEL HAS FIBER DAMAGE TO THE UPPER SURFACE. FABRICATED A REPLACEMENT PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781736](https://openairdocs.org/sdr/ASAA0781736), May 29, 2007: FLOOR PANEL. DAMAGED. CABIN FLOOR PANEL HAS DAMAGED INSERTS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781735](https://openairdocs.org/sdr/ASAA0781735), May 29, 2007: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL IS DELAMINATED. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106.
- [SDR ASAA0781734](https://openairdocs.org/sdr/ASAA0781734), May 29, 2007: FLOOR PANEL. CORRODED. CABIN FLOOR PANEL HAS CORRODED INSERTS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53 05 PARA 11 AND DAC DWG S4932106.
- [SDR ASAA0781715](https://openairdocs.org/sdr/ASAA0781715), May 29, 2007: SKIN. DENTED. FUSELAGE SKIN IS DENTED. INSTALLED REPAIR DOUBLER AT RIGHT EXT FUSELAGE. COLD FORMED SKIN BACK TO ORIGINAL BLUEPRINT CONTOUR AND HFEC PRIOR TO DOUBLER INSTALLAT
- [SDR ASAA0781714](https://openairdocs.org/sdr/ASAA0781714), May 29, 2007: CUSP WEB. CORRODED. PASSENGER CABIN FLOOR CUSP WEB CORRODED. REMOVED CORRODED CUSP WEB, LOCATED DRILLED AND INSTALLED A REPLACEMENT CUSP WEB IAW SRM 51-10-4 AND 51-30-2.
- [SDR ASAA0781713](https://openairdocs.org/sdr/ASAA0781713), May 29, 2007: CUSP WEB. CORRODED. PASSENGER CABIN FLOOR CUSP WEB CORRODED. REMOVED CORROSION MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND REPLACED CUSP WEB IAW SRM 51-30-2 AND 51
- [SDR ASAA0781712](https://openairdocs.org/sdr/ASAA0781712), May 29, 2007: SKIN. DENTED. FUSELAGE SKIN IS DENTED AFT OF THE FWD LAVATORY SERVICE PANEL WITHIN 1 INCH OF LONGERON 20L. COLD WORKED SKIN, FABRICATED DOUBLER ,TREATED, PRIMED AND INSTALLED
- [SDR ASAA0680224](https://openairdocs.org/sdr/ASAA0680224), Mar 2, 2006: SKIN. DENTED. LEFT INBOARD FLAP LOWER SURFACE IS DENTED. CUT OUT DAMAGED AREA. INSTALLED FILLER AND DOUBLER PER SRM 57 01 FIG 5 SHT 2.
- [SDR ASAA0680223](https://openairdocs.org/sdr/ASAA0680223), Mar 2, 2006: SKIN. DAMAGED. FOUND RUDDER LEFT SURFACE IS DINGED 23 INCHES FROM T/E 20.5 INCHES AFT OF LOWER DAMPER CUTOUT. APPLIED FILLER PER SRM 51 70 1A PARA 21.
- [SDR ASAA0680258](https://openairdocs.org/sdr/ASAA0680258), Mar 1, 2006: REPAIR. DELAMINATED. RUDDER TAB EXISTING REPAIR DELAMINATED 7 TO 9 INCHES FROM T/E AND 3 TO 9 INCHES ABOVE SECOND HINGE. REPLACED EXISTING REPAIR PER SRM 51-70-1A PARA 21.
- [SDR ASAA0480627](https://openairdocs.org/sdr/ASAA0480627), Dec 29, 2004: POWER SUPPLY. DISCHARGED. DURING LINE CHECK, FOUND OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE. REPLACED ASSOCIATED POWER SUPPLY (BATTERY PACK). LIGHTS THEN OPERATED PROPERLY. (M)
- [SDR ASAA0480615](https://openairdocs.org/sdr/ASAA0480615), Dec 16, 2004: LONGERON. CORRODED. OKC - HV-CHECK, LONGERON 29L IS CORRODED. APPLIED SEALANT PER EA 5310-02430. (M)
- [SDR ASAA0480614](https://openairdocs.org/sdr/ASAA0480614), Dec 16, 2004: LONGERON. CORRODED. OKC - HV-CHECK, FOUND LONGERON 30 IS CORRODED. REMOVED DAMAGED SECTION. INSTALLED U-CHANNEL AND FILLER. (M)
- [SDR ASAA0480612](https://openairdocs.org/sdr/ASAA0480612), Dec 16, 2004: ACCESS PANEL. CHAFED. OKC - HV-CHECK, LEFT WING FUEL PANEL 1303 CHAFED AND PITTED. REPLACED PANEL. (M)
- [SDR ASAA0480616](https://openairdocs.org/sdr/ASAA0480616), Dec 16, 2004: DOOR FRAME. GOUGED. OKC - HV-CHECK, TWO MOUNTING HOLES GOUGED AT BOTTOM FRAME OF LEFT OVERWING EXIT. INSTALLED DOUBLER PER EA 53-20-01679. (M)

All 187: https://openairdocs.org/deregistered/N962AS-2010-09-24/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 19950706044069I](https://openairdocs.org/incident/19950706044069I), Jul 6, 1995: Doug DC983 (N962AS), Portland, OR. Narrative: Alaska flight 336 experienced a generator failure enroute from seattle to ontario. Crew elected to divert into Portland International, since the APU…

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