# N961AS: 1992 Mcdonnell Douglas DC-9-83(MD-83), registration cancelled 2010-05-04 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 4, 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: 53075 - Year built: 1992 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: March 25, 1992 - Certificate issued: April 1, 2010 - Last registry action: April 2, 2010 - Mode S code: AD5FEE - Owner when cancelled: [Alaska Airlines Inc](https://openairdocs.org/faa-owner/ALASKA%20AIRLINES%20INC) - Location: [Seattle, WA](https://openairdocs.org/faa-place/WA/Seattle) - Owner type: Corporation - Owner's area on the map: 47.4466° N, 122.2721° W: Placed by OpenAirDocs at the center of ZIP code 98188, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N961AS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=961AS - Page: https://openairdocs.org/deregistered/N961AS-2010-05-04 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 (154, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASAA0883085](https://openairdocs.org/sdr/ASAA0883085), Jun 24, 2008: FITTING. WORN. F/A REPORTS L 1 DOOR DIFFICULT TO CLOSE FOUND BAYONET FITTING WORN. REMOVED LINER, REMOVED SLIDE, REMOVED REPLACED BAYONET FITTING. FUNCTION CKD L 1 DOOR AS REQ - [SDR ASAA0782386](https://openairdocs.org/sdr/ASAA0782386), Dec 13, 2007: TURBINE. FAILED. EN ROUTE SEA TO DEN RIGHTHAND ENGINE STARTED TO EXPERIENCE WHAT APPEARED TO BE COMPRESSOR STALLS. ENGINE WAS PURPOSELY SHUTDOWN AND THE FLIGHT WAS DIVERTED TO S - [SDR ASAA0782295](https://openairdocs.org/sdr/ASAA0782295), Dec 1, 2007: FRAME. CRACKED. AFT A C BAY FRAME 1418 CRACKED AT LONGERON 2 RIGHT REPAIRED AFT A C BAY FRAME 1418 IAW MD80 SRM 53 03 FIG 31A. STOP DRILLED CRACK, INSTALLED REPAIR ANGLES. LOCA - [SDR ASAA0782296](https://openairdocs.org/sdr/ASAA0782296), Dec 1, 2007: SKIN. DENTED. RAMP REPORTS DENT IN AFT CARGO DOOR EXTERIOR SKIN JUST BELOW THE HANDLE CUTOUT. DAMAGED AREA OF SKIN FABRICATED REPAIR DOUBLERS AND INSTALLED IAW ASA EA 5230 01 - [SDR ASAA0782293](https://openairdocs.org/sdr/ASAA0782293), Nov 29, 2007: SKIN. DELAMINATED. RT AILERON IS DELAMINATED AT THE O/B ATTACH POINT LOWER SURFACE PREPPED AREA. FABRICATED AND BONDED REPAIR PLIES IAW MD80 SRM 51 90 0 8N PG 72. - [SDR ASAA0782292](https://openairdocs.org/sdr/ASAA0782292), Nov 29, 2007: LONGERON. CRACKED. LONGERON 2 RIGHT CRACKED AT STA 1418. REMOVED CRACKED SECTION OF LONGERON, FABRICATED AND INSTALLED REPLACEMENT SECTION OF LONGERON AND SPLICE IAW MD80 SRM 53-0 - [SDR ASAA0782291](https://openairdocs.org/sdr/ASAA0782291), Nov 29, 2007: LONGERON. CRACKED. LONGERON 2 LEFT CRACKED AT STA 1418. REMOVED CRACKED SECTION OF LONGERON, FABRICATED AND INSTALLED REPLACEMENT SECTION ON LONGERON AND SPLICE IAW MD80 SRM 53-02 - [SDR ASAA0782290](https://openairdocs.org/sdr/ASAA0782290), Nov 29, 2007: FRAME. CRACKED. FUSELAGE FRAME STA 1418 FROM LONGERON 5L TO 5R FAILSAFE CHORD IS CRACKED. REMOVED CRACKED CHORD RECEIVED DRILLED AND INSTALLED NEW CHORD IAW MD80 SRM 51-10-4, 5 - [SDR ASAA0782279](https://openairdocs.org/sdr/ASAA0782279), Nov 25, 2007: SKIN. DAMAGED. A 9 INCH J-SHAPED CREASE ON EXTERIOR OF AFT STAIRWAY DOOR LEFT SIDE OF AIRPLANE JUST FORWARD OF EXTERNAL TAIL CONE ACCESS DOOR. CUT OUT DAMAGED SECTION OF SKIN, - [SDR ASAA0680959](https://openairdocs.org/sdr/ASAA0680959), Sep 12, 2006: SKIN. CRACKED. RIGHT WING OUTBOARD FLAP TRAILING EDGE IS CRACKED. REMOVED DAMAGED AREA. APPLIED FOUR REPAIR PLIES PER SRM 51-70-1. - [SDR ASAA0680958](https://openairdocs.org/sdr/ASAA0680958), Sep 12, 2006: VANE. CHAFED. RIGHT WING INBOARD FLAP INBOARD VANE IS CHAFED ON LEADING EDGE. INSTALLED EXTERNAL REPAIR DOUBLER PER SRM 57-03. - [SDR ASAA0680957](https://openairdocs.org/sdr/ASAA0680957), Sep 12, 2006: STRINGER CLIP. CORRODED. TEE CLIP CORRODED. REPLACED TEE CLIP PER SRM 51-10-4 AND 51-30-5. - [SDR ASAA0680956](https://openairdocs.org/sdr/ASAA0680956), Sep 12, 2006: FLOOR PANEL. PUNCTURED. CABIN FLOOR PANEL PUNCTURED. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106. - [SDR ASAA0680955](https://openairdocs.org/sdr/ASAA0680955), Sep 12, 2006: FLOOR PANEL. CRACKED. CABIN FLOOR PANEL IS CRACKED. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106. - [SDR ASAA0680954](https://openairdocs.org/sdr/ASAA0680954), Sep 12, 2006: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND ASA DWG S4932106. - [SDR ASAA0680953](https://openairdocs.org/sdr/ASAA0680953), Sep 12, 2006: SHEAR TIE. CORRODED. SHEAR TIE CORRODED. REMOVED DAMAGED SECTION OF TIE. INSTALLED REPAIR SECTION AND SPLICE PER SRM 53-03. - [SDR ASAA0680952](https://openairdocs.org/sdr/ASAA0680952), Sep 12, 2006: CUSP WEB. CORRODED. CUSP WEB CORRODED. REMOVED DAMAGED CUSP SECTION. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 51-70-4. - [SDR ASAA0680951](https://openairdocs.org/sdr/ASAA0680951), Sep 12, 2006: CUSP WEB. CORRODED. CUSP WEB CORRODED. REPLACED CUSP WEB PER SRM 51-10-4, 51-30-1, 51-30-2 AND 51-30-5. - [SDR ASAA0680921](https://openairdocs.org/sdr/ASAA0680921), Aug 31, 2006: SKIN. DENTED. FUSELAGE SKIN DENTED. REMOVED DAMAGED SECTION INCLUDING EXISTING REPAIR DOUBLER. INSTALLED EXTERNAL REPAIR DOUBLER FINGER DOUBLER LONGERON STRAP AND FILLER IAW - [SDR ASAA0680925](https://openairdocs.org/sdr/ASAA0680925), Aug 31, 2006: CUSP WEB. CORRODED. CUSP WEB CORRODED. REMOVED DAMAGED SECTION OF WEB. INSTALLED REPAIR DOUBLER IAW SRM 53 01. - [SDR ASAA0680924](https://openairdocs.org/sdr/ASAA0680924), Aug 31, 2006: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106. - [SDR ASAA0680923](https://openairdocs.org/sdr/ASAA0680923), Aug 31, 2006: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106. - [SDR ASAA0680922](https://openairdocs.org/sdr/ASAA0680922), Aug 31, 2006: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106. - [SDR ASAA0680915](https://openairdocs.org/sdr/ASAA0680915), Aug 29, 2006: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL IAW SRM 52 05 AND ASA DWG S4932106. - [SDR ASAA0680914](https://openairdocs.org/sdr/ASAA0680914), Aug 29, 2006: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106. - [SDR ASAA0680913](https://openairdocs.org/sdr/ASAA0680913), Aug 29, 2006: FLOOR PANEL. CORRODED. CABIN FLOOR PANEL CORRODED AT INSERTS. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106. - [SDR ASAA0680912](https://openairdocs.org/sdr/ASAA0680912), Aug 29, 2006: INSERT. CORRODED. CABIN FLOOR PANEL HAS CORRODED INSERTS. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106. - [SDR ASAA0680911](https://openairdocs.org/sdr/ASAA0680911), Aug 29, 2006: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106. - [SDR ASAA0680910](https://openairdocs.org/sdr/ASAA0680910), Aug 29, 2006: FLOOR PANEL. CRACKED. CABIN FLOOR PANEL CRACKED AT INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106. - [SDR ASAA0680909](https://openairdocs.org/sdr/ASAA0680909), Aug 29, 2006: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106. - [SDR ASAA0680908](https://openairdocs.org/sdr/ASAA0680908), Aug 29, 2006: FLOOR PANEL. CRACKED. CABIN FLOOR PANEL CRACKED. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106. - [SDR ASAA0680907](https://openairdocs.org/sdr/ASAA0680907), Aug 29, 2006: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106. - [SDR ASAA0680906](https://openairdocs.org/sdr/ASAA0680906), Aug 29, 2006: FLOOR PANEL. CORRODED. CABIN FLOOR PANEL HAS CORRODED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106. - [SDR ASAA0680905](https://openairdocs.org/sdr/ASAA0680905), Aug 29, 2006: FLOOR PANEL. CORRODED. CABIN FLOOR PANEL CORRODED AT INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106. - [SDR ASAA0680902](https://openairdocs.org/sdr/ASAA0680902), Aug 29, 2006: WEB. CRACKED. L1 DOOR JAMB WEB IS CRACKED. REMOVED DAMAGED AREA OF WEB. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-70-4. - [SDR ASAA0680903](https://openairdocs.org/sdr/ASAA0680903), Aug 29, 2006: SHEAR TIE. CORRODED. AFT CARGO BAY SHEAR TIE IS CORRODED. REPLACED SHEAR TIE PER SRM 51-10-4 AND 51-30-5. - [SDR ASAA0680904](https://openairdocs.org/sdr/ASAA0680904), Aug 29, 2006: SKIN. DENTED. MID CARGO BAY DOOR DENTED. COLD FORMED TO ORIGINAL CONTOUR. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53-04. - [SDR ASAA0680901](https://openairdocs.org/sdr/ASAA0680901), Aug 23, 2006: GUSSET. CORRODED. AFT CARGO BAY THRESHOLD WEB GUSSET IS CORRODED. REPLACED GUSSET IAW SRM 53 14 3 51 10 2 51 10 3. 51 30 2. AND 51 30 5. - [SDR ASAA0680759](https://openairdocs.org/sdr/ASAA0680759), Jul 11, 2006: LANYARD. WORN. INADVERTENTLY DEPLOYED TAIL CONE WHICH SHOULD HAVE ALSO CAUSED AFT EMERGENCY SLIDE TO DEPLOY. LANYARD VELCRO AND SNAP PULLED LOOSE FROM THE SLIDE COVER BUT THE - [SDR ASAA0580300](https://openairdocs.org/sdr/ASAA0580300), Jun 4, 2005: VANE. DENTED. OKC - FOUND HV-CHECK, RIGHT FLAP VANE DENTED ON LOWER SURFACE. REMOVED DAMAGED SECTION. INSTALLED FILLER AND DOUBLER. (M) - [SDR ASAA0580299](https://openairdocs.org/sdr/ASAA0580299), Jun 4, 2005: VANE. GOUGED. OKC - FOUND DURING HV-CHECK, RIGHT FLAP VANE GOUGED. REPAIRED DAMAGED SECTION PER SRM 51-70. (M) - [SDR ASAA0580298](https://openairdocs.org/sdr/ASAA0580298), Jun 4, 2005: SKIN. DENTED. OKC - FOUND DURING HV-CHECK, LEFT NR 2 SLAT L/E DENTED. REPAIRED DAMAGED SECTION PER SRM 57-09. (M) - [SDR ASAA0480452](https://openairdocs.org/sdr/ASAA0480452), May 26, 2004: WIRE. MISINSTALLED. SEA - FOUND DURING PREFLIGHT, COCKPIT OVERHEAD FLOOD LIGHT FOUND INOPERATIVE UPON TEST. REROUTED MIS-CONNECTED FLOOR LIGHT WIRE. LIGHT THEN OPERATED PROPERLY. ( - [SDR ASAA0480188](https://openairdocs.org/sdr/ASAA0480188), Mar 14, 2004: WEB. CORRODED. OKC - DURING HV CHECK, FOUND AFT CARGO BAY DOOR CUTOUT INTERNAL WEB IS CORRODED AROUND ATTACH HARDWARE AT FS 1155-1211. REPLACED DAMAGED AREA OF WEB AND INSTALL - [SDR ASAA0480187](https://openairdocs.org/sdr/ASAA0480187), Mar 14, 2004: ATTACH ANGLE. CORRODED. OKC - DURING HV CHECK, FOUND ATTACH ANGLE IS CORRODED AT FS 1007. REPLACED ANGLE PER SRM 51-10-4. (M) - [SDR ASAA0480186](https://openairdocs.org/sdr/ASAA0480186), Mar 14, 2004: SEAT TRACK. CHAFED. OKC - DURING HV CHECK, FOUND CABIN SEAT TRACK IS CHAFED AT FS 1212-1322. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-05. (M) - [SDR ASAA0480153](https://openairdocs.org/sdr/ASAA0480153), Mar 13, 2004: FLOOR PANEL. DELAMINATED. OKC - FOUND FORWARD CABIN FLOOR PANEL STATION 148 TO STATION 168 HAS DELAMINATION AROUND FASTENER HOLES. FABRICATED REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05. - [SDR ASAA0480156](https://openairdocs.org/sdr/ASAA0480156), Mar 13, 2004: FLOORBOARD. CORRODED. OKC - FOUND CABIN FLOORBOARD STATION 200-256 HAS SEVERAL CORRODED INSERTS. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) - [SDR ASAA0480160](https://openairdocs.org/sdr/ASAA0480160), Mar 12, 2004: FLOOR PANEL. CRACKED. OKC - FOUND INSERTS PULLING OFF, CORRODED AND PANEL CRACKED AT LOWER SURFACE, FORWARD CABIN STATION 148-200. FABRICATED REPLACEMENT FLOOR PANEL IAW MD80 SRM 53- - [SDR ASAAO480180](https://openairdocs.org/sdr/ASAAO480180), Mar 10, 2004: SEAT TRACK. CHAFED. OKC - DURING HV CHECK, FOUND SEAT TRACK CHAFED AT FS 1212. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-05. (M) All 154: https://openairdocs.org/deregistered/N961AS-2010-05-04/reports.md ## Other aircraft with N961AS - [Cancelled 2021-04-30](https://openairdocs.org/deregistered/N961AS-2021-04-30): Learjet 45, S/N 404, built 2009. Exported to India. Owner: New Dehi --- 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.