# N958AS: 1991 Mcdonnell Douglas DC-9-83(MD-83), registration cancelled 2012-11-14 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 14, 2012 - Exported to: Venezuela - 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-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: 53024 - Year built: 1991 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: February 15, 1991 - Certificate issued: May 10, 2007 - Last registry action: April 12, 2012 - Mode S code: AD5270 - 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: 40.8659° N, 112.0391° W: Placed by OpenAirDocs at the center of ZIP code 84116, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N958AS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=958AS - Page: https://openairdocs.org/deregistered/N958AS-2012-11-14 From the FAA registry file of October 28, 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 (182, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASAA0882977](https://openairdocs.org/sdr/ASAA0882977), May 21, 2008: DOUBLER. CORRODED. FWD LAV SERVICE PANEL DOUBLER IS CORRODED AT FORWARD LOWER LATCH CUTOUT DAMAGED SECTION. FABRICATED LOCATED DRILLED AND INSTALLED REPAIR STRAP AND FILLER IAW AL - [SDR ASAA0782085](https://openairdocs.org/sdr/ASAA0782085), Oct 5, 2007: DOUBLER. CHAFED. RIGHTHAND WING OUTBOARD FLAP INBOARD FIXED VANE L/E DOUBLER IS CHAFED. REPLACED EXISTING DOUBLER PER SRM 51-70-2. - [SDR ASAA0782084](https://openairdocs.org/sdr/ASAA0782084), Oct 5, 2007: VANE. GOUGED. LEFTHAND WING OUTBOARD FLAP INBOARD VANE L/E DOUBLER REPAIR IS GOUGED. REPLACED EXISTING REPAIR DOUBLER PER SRM 51-70-2. - [SDR ASAA0782083](https://openairdocs.org/sdr/ASAA0782083), Oct 5, 2007: RIB. DAMAGED. LEFTHAND WING NR 5 L/E SLAT OUTBOARD RIB HOLES OVERSIZED. REPLACED WORN RIB PER SRM 51-10-4 AND 51-30-2. - [SDR ASAA0782082](https://openairdocs.org/sdr/ASAA0782082), Oct 5, 2007: ATTACH ANGLE. CRACKED. RIGHTHAND SIDE OF VERTICAL STABILIZER EXTERNAL VERTICAL TO FUSELAGE JOIN STRAP (ATTACH ANGLE) IS CRACKED. REPLACED DAMAGED SECTION OF JOIN STRAP PER SRM 53-05. - [SDR ASAA0782081](https://openairdocs.org/sdr/ASAA0782081), Oct 5, 2007: CUSP WEB. CRACKED. CUSP WEB CRACKED. STOP DRILLED CRACK. INSTALLED REPAIR PARTS PER SRM 53-05. - [SDR ASAA0782076](https://openairdocs.org/sdr/ASAA0782076), Oct 5, 2007: TRACK. CORRODED. CABIN FLOOR FALSE TRACK IS CORRODED. REPLACED FALSE TRACK PER SRM 51-10-3, 51-10-4, 53-14-1 AND 51-30-5. - [SDR ASAA0782075](https://openairdocs.org/sdr/ASAA0782075), Oct 5, 2007: TRACK. CORRODED. CABIN FALSE TRACK IS CORRODED. REPLACED TRACK PER SRM 51-10-3, 51-10-4, 53-14-1, AND 51-30-5. - [SDR ASAA0782074](https://openairdocs.org/sdr/ASAA0782074), Oct 5, 2007: FLOOR PANEL. BROKEN. CABIN FLOOR PANEL HAS DAMAGED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND DAC DWG S4932106. - [SDR ASAA0782073](https://openairdocs.org/sdr/ASAA0782073), Oct 5, 2007: FLOOR PANEL. BROKEN. CABIN FLOOR PANEL HAS DAMAGED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND DAC DWG S4932106. - [SDR ASAA0782072](https://openairdocs.org/sdr/ASAA0782072), Oct 5, 2007: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106. - [SDR ASAA0782071](https://openairdocs.org/sdr/ASAA0782071), Oct 5, 2007: FLOOR PANEL. BROKEN. CABIN FLOOR PANEL HAS DAMAGED INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106. - [SDR ASAA0782070](https://openairdocs.org/sdr/ASAA0782070), Oct 5, 2007: FLOOR PANEL. BROKEN. CABIN FLOOR PANEL HAS BROKEN INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106. - [SDR ASAA0782069](https://openairdocs.org/sdr/ASAA0782069), Oct 5, 2007: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05 AND DAC DWG S4932106. - [SDR ASAA0782068](https://openairdocs.org/sdr/ASAA0782068), Oct 5, 2007: FLOOR PANEL. BROKEN. CABIN FLOOR PANEL HAS BROKEN INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106. - [SDR ASAA0782067](https://openairdocs.org/sdr/ASAA0782067), Oct 5, 2007: FLOOR PANEL. BROKEN. CABIN FLOOR PANEL CRACKED WITH DAMAGED INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106. - [SDR ASAA0782066](https://openairdocs.org/sdr/ASAA0782066), Oct 5, 2007: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106. - [SDR ASAA0782065](https://openairdocs.org/sdr/ASAA0782065), Oct 5, 2007: SEAT TRACK. CORRODED. CABIN SEAT TRACK EXISTING REPAIR SPLICE CORRODED. REMOVED DAMAGED SECTION OF TRACK. INSTALLED REPLACEMENT PER SRM 51-10-4 AND 53-05. - [SDR ASAA0782080](https://openairdocs.org/sdr/ASAA0782080), Oct 5, 2007: LONGERON. CRACKED. LONGERON CRACKED. REMOVED DAMAGED SECTION OF LONGERON. INSTALLED REPLACEMENT SECTION PER SRM 53-02 (SPLICE REPAIR). - [SDR ASAA0782079](https://openairdocs.org/sdr/ASAA0782079), Oct 5, 2007: FRAME. CRACKED. FRAME CRACKED. REPLACED FRAME PER SRM 53-03. - [SDR ASAA0782078](https://openairdocs.org/sdr/ASAA0782078), Oct 5, 2007: STIFFENER. CRACKED. FRAME STIFFENER CRACKED. REPLACED STIFFENER PER SRM 51-30-5, 51-30-2 AND DAC DWG 5913595. - [SDR ASAA0782077](https://openairdocs.org/sdr/ASAA0782077), Oct 5, 2007: SHEAR TIE. CRACKED. SHEAR TIE IS CRACKED. REPLACED SHEAR TIE PER SRM 51-10-4, 51-30-2 AND 51-30-5. - [SDR ASAA0781416](https://openairdocs.org/sdr/ASAA0781416), Jan 19, 2007: FRAME. DENTED. NLG WHEELWELL LEFT FRAME JUST FORWARD OF LEFT INNER BULKHEAD WAS DENTED. REPLACE FRAME PER SRM 51 30 02. - [SDR ASAA0681318](https://openairdocs.org/sdr/ASAA0681318), Dec 9, 2006: WINDOW. STUCK. CAPTAIN SIDE SLIDING WINDOW WOULD NOT OPEN. ADJUSTED WINDOW CAM FOLLOWER. OP CHECKED OK. - [SDR ASAA0681304](https://openairdocs.org/sdr/ASAA0681304), Dec 6, 2006: ENGINE. FAILED. EN ROUTE SAN SEA - RIGHTHAND ENGINE R OIL STRAINER CLOGGING ANNUNCIATED. CREW SHUTDOWN ENGINE AS PRECAUTION AND DIVERTED TO SMF. SUBSEQUENTLY FOUND METAL CONTAM - [SDR ASAA0681217](https://openairdocs.org/sdr/ASAA0681217), Nov 23, 2006: WINDOW. STUCK. DURING TAXI TO GATE, COCKPIT LEFT SLIDING WINDOW WOULD NOT OPEN. ADJUSTED UPPER CAM FOLLOWER. - [SDR ASAA0681216](https://openairdocs.org/sdr/ASAA0681216), Nov 22, 2006: WINDOW. STUCK. ON TAXI TO GATE, COCKPIT LEFT SLIDING WINDOW WOULD NOT OPEN. REALIGNED UPPER FORWARD GUIDE PIN. - [SDR ASAA0680807](https://openairdocs.org/sdr/ASAA0680807), Jul 25, 2006: SKIN. GOUGED. RIGHT OUTBOARD FLAP INBOARD VANE IS GOUGED ON EXISTING REPAIR AT INBOARD LEADING EDGE. REMOVED EXISTING REPAIR DOUBLER. INSTALLED SKIN FILLER AND EXTERNAL DOUBL - [SDR ASAA0680806](https://openairdocs.org/sdr/ASAA0680806), Jul 25, 2006: SKIN. GOUGED. LEFT OUTBOARD FLAP INBOARD VANE IS GOUGED ON EXISTING REPAIR AT INBOARD LEADING EDGE. REMOVED EXISTING REPAIR DOUBLER. INSTALLED SKIN FILLER AND EXTERNAL DOUBLE - [SDR ASAA0680805](https://openairdocs.org/sdr/ASAA0680805), Jul 25, 2006: SHEAR TIE. CORRODED. FOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51 10 4 51 10 3 AND 51 30 5. - [SDR ASAA0680790](https://openairdocs.org/sdr/ASAA0680790), Jul 20, 2006: RIB. GOUGED. THE RT NR 4 SLAT O B FITTING (RIB ASSY) IS GOUGED OUT OF LIMITS. REMOVED DAMAGED RIB ASSY LOCATED DRILLED AND INSTALLED A REPLACEMENT RIB ASSY IAW MD 80 SRM 51 - [SDR ASAA0680789](https://openairdocs.org/sdr/ASAA0680789), Jul 20, 2006: SKIN. MISDRILLED. FUSELAGE SKIN HAS MECHANICAL DAMAGE. (MISDRILLS DUE TO PREVIOUSLY ACCOMPLISHED STOP DRILLS ON THE R H ENGINE PYLON UPPER AFT FAIRING SUPPORT ANGLE) CUT OUT DAMA - [SDR ASAA0680788](https://openairdocs.org/sdr/ASAA0680788), Jul 20, 2006: SHEAR TIE. CORRODED. SHEAR TIE CORRODED OUT OF LIMITS AT FS 1211 BETWEEN LONGERONS 29R AND 30. REMOVED DAMAGED SHEAR TIE FABRICATED AND INSTALLED A REPLACEMENT SHEAR TIE IAW MD 80 S - [SDR ASAA0580253](https://openairdocs.org/sdr/ASAA0580253), May 9, 2005: WIRE. LOOSE. ANC LINE CHECK, FOUND AFT EXIT CATWALK SIDE PANEL EMERGENCY LIGHT INOPERATIVE. RESECURED LOOSE WIRE CONNECTOR. LIGHT THEN OPERATED PROPERLY. (M) - [SDR ASAA0580220](https://openairdocs.org/sdr/ASAA0580220), Apr 25, 2005: SKIN. GOUGED. DURING C-CHECK FOUND, LT WING OUTBOARD FLAP INBOARD FLAP VANE LEADING EDGE GOUGED. REMOVED DAMAGE. INSTALLED REPAIR FILLER AND DOUBLER. (M) - [SDR ASAA0580219](https://openairdocs.org/sdr/ASAA0580219), Apr 25, 2005: SKIN. DENTED. DURING C-CHECK, FOUND RT WING INBOARD FLAP OUTBOARD FLAP VANE UPPER SURFACE DENTED. INSTALLED REPAIR DOUBLER. (M) - [SDR ASAA0580218](https://openairdocs.org/sdr/ASAA0580218), Apr 25, 2005: SKIN. GOUGED. FOUND DURING C-CHECK, FUSELAGE SKIN GOUGED. REMOVED DAMAGE. REPAINTED. (M) - [SDR ASAA0580217](https://openairdocs.org/sdr/ASAA0580217), Apr 25, 2005: SKIN. DELAMINATED. FOUND DURING C-CHECK, LT WING INBOARD FLAP VANE OUTBOARD SEGMENT DELAMINATED. REMOVED DAMAGE. INSTALLED REPAIR FILLERS AND DOUBLERS. (M) - [SDR ASAA0580216](https://openairdocs.org/sdr/ASAA0580216), Apr 25, 2005: RIB. CRACKED. DURING C-CHECK, FOUND LT WING NR 4 SLAT ACCESS CUTOUT RIB CRACKED. INSTALLED REPAIR DOUBLER PER EA 5740-01447. (M) - [SDR ASAA0580213](https://openairdocs.org/sdr/ASAA0580213), Apr 20, 2005: SKIN. DENTED. FOUND DURING C-CHECK, LT ELEVATOR ANTI-FLOAT TAB UPPER SURFACE DENTED. INSTALLED REPAIR DOUBLERS. (M) - [SDR ASAA0580212](https://openairdocs.org/sdr/ASAA0580212), Apr 20, 2005: CUSP WEB. CORRODED. DURING C-CHECK, FOUND CABIN FLOOR PANEL CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER. (M) - [SDR ASAA0580211](https://openairdocs.org/sdr/ASAA0580211), Apr 20, 2005: SKIN. CORRODED. DURING C-CHECK, FOUND FUSELAGE SKIN CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M) - [SDR ASAA0480146](https://openairdocs.org/sdr/ASAA0480146), Mar 1, 2004: MODULE. INOPERATIVE. SEA - PREFILGHT CHECK, FOUND FIRST FIVE EMERGENCY TRACK LIGHTS TESTS INOPERATIVE, TWICE. RECONNECTED MODULE CONNECTOR, TWICE. LIGHTS THEN OPERATED PROPERLY. (M) - [SDR ASAA0480059](https://openairdocs.org/sdr/ASAA0480059), Jan 30, 2004: WEB. CORRODED. OKC - DURING 15K CHECK, FOUND WEB IS CORRODED AT LONGERON 18L NEAR L2 DOOR. REMOVED CORROSION. INSTALLED FILLER AND DOUBLER PER SRM 53-01. (M) - [SDR ASAA0480057](https://openairdocs.org/sdr/ASAA0480057), Jan 30, 2004: TAB. DENTED. OKC - DURING 15K CHECK, FOUND LEFT ANTI-FLOAT TAB UPPER SURFACE IS DENTED. APPLIED FILLER PER SRM 55-04. (M) - [SDR ASAA0480062](https://openairdocs.org/sdr/ASAA0480062), Jan 30, 2004: SEAT TRACK. CORRODED. OKC - DURING 15K CHECK, FOUND RIGHT INBOARD SEAT TRACK IS CORRODED AT FS 200-247. REPLACED SEAT TRACK PER SRM 53-05. (M) - [SDR ASAA0480060](https://openairdocs.org/sdr/ASAA0480060), Jan 30, 2004: SEAT TRACK. CORRODED. OKC - DURING 15K CHECK, FOUND LEFT OUTBOARD SEAT TRACK IS CORRODED AT FS 1106-1185. REPLACED DAMAGED TRACK PER SRM 51-10-4 AND 51-30-5. (M) - [SDR ASAA0480056](https://openairdocs.org/sdr/ASAA0480056), Jan 30, 2004: SKIN. DENTED. OKC - DURNG 15K CHECK, FOUND FUSELAGE SKIN IS DENTED AT FS 237. INSTALLED DOUBLER PER SRM 53-04. (M) - [SDR ASAA0480055](https://openairdocs.org/sdr/ASAA0480055), Jan 30, 2004: SKIN. GOUGED. OKC - DURING 15K CHECK, FOUND FUSELAGE SKIN IS GOUGED AT STATION 235. REMOVED DAMAGED SECTION. REPAIRED WITH FILLER AND DOUBLER PER SRM 53-04. (M) - [SDR ASAA0480054](https://openairdocs.org/sdr/ASAA0480054), Jan 30, 2004: STRINGER. CORRODED. OKC - DURING 15K CHECK, FOUND STRINGER IS CORRODED UNDER LOWER FLANGE AT FS 1212. REMOVED DAMAGED SECTION. REPLACED WITH SPLICE PER SRM 53-02, 51-10-3, AND 51-6 All 182: https://openairdocs.org/deregistered/N958AS-2012-11-14/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 20061206026349I](https://openairdocs.org/incident/20061206026349I), Dec 6, 2006: Doug MD83 (N958AS), Sacramento, CA. (-23) Flight 547, departed san enroute to sea. At approximately 2227 PST, the #2 engine oil strainer light came on. All other engine parameters were normal.… - [Incident 19971127043969I](https://openairdocs.org/incident/19971127043969I), Nov 27, 1997: Doug DC983 (N958AS), Ontario, CA, Minor damage. Narrative: aircraft blew r/h outboard tire on landing. Contract maintenance, mike zimmerman, oas, towed aircraft to parking and determined aircraft r/h engine… --- 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.