# N951AS: 1982 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2009-04-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 8, 2009
- Status when cancelled: Valid registration
- 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-5](https://openairdocs.org/engine/pratt-whitney-jt8d-5) (registry code 52046)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 49111
- Year built: 1982
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: July 16, 1982
- Last registry action: April 8, 2009
- Mode S code: AD386F
- Owner when cancelled: [Stewart Industries International LLC](https://openairdocs.org/faa-owner/STEWART%20INDUSTRIES%20INTERNATIONAL%20LLC)
- Location: [Guthrie, OK](https://openairdocs.org/faa-place/OK/Guthrie)
- Owner type: Corporation
- Owner's area on the map: 35.8679° N, 97.4344° W: Placed by OpenAirDocs at the center of ZIP code 73044, within about 9 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N951AS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=951AS
- Page: https://openairdocs.org/deregistered/N951AS-2009-04-08

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-9-82(MD-82): https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82.md

## Service difficulty reports (114, newest 50)

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

- [SDR ASAA0380579](https://openairdocs.org/sdr/ASAA0380579), Sep 5, 2003: LANYARD. DISCONNECTED. PREFLIGHT CHECK, FORWARD SERVICE R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)
- [SDR ASAA0380552](https://openairdocs.org/sdr/ASAA0380552), Aug 12, 2003: BATTERY PACK. INOPERATIVE. PHX PREFLIGHT CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS FOUND INOPERATIVE. REPLACED POWER SUPPLIES, BATTERY PACKS. LIGHTS THEN OPERATED PROPERLY. (M)
- [SDR ASAA0280604](https://openairdocs.org/sdr/ASAA0280604), Nov 19, 2002: MODULE. INOPERATIVE. SEA - DURING LINE CHECK, WHITE EMERGENCY TRACK LIGHT WAS FOUND INOPERATIVE AT ROW 6. REPLACED LIGHT MODULE. LIGHT THEN OPERATED PROPERLY. (M)
- [SDR ASAA0280266](https://openairdocs.org/sdr/ASAA0280266), Aug 16, 2002: WIRE. DAMAGED. PDX - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROWS 26-29. REPAIRED DAMAGED WIRING BETWEEN LIGHT MODULE CONNECTORS. LIGHTS THEN OPERATED P
- [SDR ASAA0280233](https://openairdocs.org/sdr/ASAA0280233), Jul 23, 2002: LONGERON. CORRODED. OAK - DURING C-CHECK, FOUND LONGERON 30, IN MID CARGO AREA, CORRODED BEYOND LIMITS FROM STATION 636 TO 655. REPLACED LONGERON 30 FROM STATION 579-788 PER SRM 51
- [SDR ASAA0280228](https://openairdocs.org/sdr/ASAA0280228), Jul 19, 2002: LONGERON. CORRODED. OAK - DURING C-CHECK, FOUND CORROSION AROUND AND UNDER RIVETS ALONG LONGERON 22R AT FUSELAGE STATION 160-180. CUT OUT DAMAGED SKIN FROM STATION 150 TO 177 BETWE
- [SDR ASAA0280045](https://openairdocs.org/sdr/ASAA0280045), Feb 18, 2002: LANYARD. DETACHED. PDX - DURING PREFLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REPLACED LANYARD. (M)
- [SDR ASAA0180310](https://openairdocs.org/sdr/ASAA0180310), Dec 9, 2001: RIB. CRACKED. PDX - DURING SERVICE CHECK, FOUND 15 INCH CRACK ON RIB STRUCTURE IN TAIL COMPARTMENT AT STATION 1463 CANT, LONGERON 7 ON LEFT SIDE. AIRCRAFT FERRIED TO OAK FOR 
- [SDR ASAA0180236](https://openairdocs.org/sdr/ASAA0180236), Aug 9, 2001: LIGHT. INOPERATIVE. SEA - DURING LINE CHECK, A TRACK LIGHT WAS FOUND TO BE INOPERATIVE AT ROW 1. REPAIRED SOCKET AND RELAMPED. LIGHTS THEN OPERATED PROPERLY. (M)
- [SDR ASAA0180234](https://openairdocs.org/sdr/ASAA0180234), Aug 2, 2001: WIRE. BROKEN. SEA - DURING PRE-FLIGHT CHECK, A TRACK LIGHT WAS FOUND TO BE INOPERATIVE AT ROW 1. SPLICED BROKEN WIRE UNDER TRACK COVER. LIGHTS THEN OPERATED PROPERLY. (M)
- [SDR ASAA0180196](https://openairdocs.org/sdr/ASAA0180196), Jun 9, 2001: BATTERY PACK. DISCHARGED. SEA - DURING PREFLIGHT CHECK, OVERWING EMERGENCY EXIT LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY PACK. LIGHTS THEN OPERATED PROPERLY.
- [SDR ASAA0180183](https://openairdocs.org/sdr/ASAA0180183), May 26, 2001: STUD. LOOSE. PDX - DURING LINE CHECK, AFT CABIN OVERHEAD STANDBY LIGHTS AT ROW 18 AND 19 WERE DETERMINED TO BE INOPERATIVE. TIGHTENED LOOSE GROUND STUD. LIGHTS THEN OPERATED
- [SDR ASAA0180130](https://openairdocs.org/sdr/ASAA0180130), Apr 8, 2001: WIRE. BROKEN. PDX - DURING SERVICE CHECK, EMERGENCY FLOOR TRACK LIGHTING AT ROW 6 WAS DETERMINED TO BE INOPERATIVE. REPAIRED BROKEN CONNECTOR WIRE AND RESECURED. TRACK LIGHTS
- [SDR ASAA0180117](https://openairdocs.org/sdr/ASAA0180117), Mar 28, 2001: LIGHT. INOPERATIVE. PHX - DURING LINE CHECK, EXTERIOR EMERGENCY LIGHTS WERE DETERMINED TO BE INOPERATIVE. REMOVED AND REPLACED EXTERNAL EMERGENCY LIGHT BATTERY. LIGHTS THEN OPERATE
- [SDR ASAA0180116](https://openairdocs.org/sdr/ASAA0180116), Mar 26, 2001: POWER SUPPLY. SEA - DURING PRE-FLIGHT CHECK, THE PORTABLE EMERGENCY LIGHT AND EXTERNAL OVERWING EMERGENCY LIGHTS WERE REPORTED TO HAVE BEEN TURNED ON FOR AT LEAST TEN MINUTES
- [SDR ASAA0180115](https://openairdocs.org/sdr/ASAA0180115), Mar 21, 2001: WINDOW. INOPERATIVE. SEA - DURING PREFLIGHT CHECK, FIRST OFFICERS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. LUBRICATED FORWARD LOCKING MECHANISM. WINDOW THEN OPERATED PROPERLY. (M)
- [SDR ASAA0180096](https://openairdocs.org/sdr/ASAA0180096), Mar 3, 2001: CHANNEL. CRACKED. OAK - DURING C-CHECK, FOUND RT C-CHANNEL, AFT OF MOVEABLE CEILING, CRACKED AT FUS CANT STATION 1485. REMOVED AND REPLACED CRACKED C-CHANNEL. (M)
- [SDR ASAA0180075](https://openairdocs.org/sdr/ASAA0180075), Feb 18, 2001: CABLE. DISCONNECTED. SEA - DURING LANDING, ''TAILCONE MISSING'' ANNUNCIATOR ILLUMINATED. SUBSEQUENT INSPECTION REVEALED THE EXTERNAL RELEASE HANDLE CABLE HAD BECOME DISCONNECTED. RE
- [SDR ASAA0180061](https://openairdocs.org/sdr/ASAA0180061), Feb 12, 2001: HANDLE. NOT CLOSED. SEA - DURING LINE CHECK, EXTERNAL DOOR OVER TAILCONE RELEASE HANDLE WAS FOUND TO NOT CLOSE COMPLETELY. LUBRICATED FLAPPER DOOR HINGE. DOOR THEN CLOSED PROPERLY.
- [SDR ASAA0180054](https://openairdocs.org/sdr/ASAA0180054), Feb 7, 2001: BATTERY PACK. DISCHARGED. PDX - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTS AT OVERWING EXIT LOCATION WERE DETERMINED TO BE INOPERATIVE. REMOVED AND REPLACED ASSOCIATED BATTERY PACK ASS
- [SDR ASAA0180027](https://openairdocs.org/sdr/ASAA0180027), Jan 23, 2001: WINDOW. INOPERATIVE. SEA - DURING PREFLIGHT CHECK, CAPTAINS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. RESEATED LOOSE HINGE PIN AND LUBRICATED WINDOW. WINDOW THEN OPERATED PROPERLY. (
- [SDR ASAA0080614](https://openairdocs.org/sdr/ASAA0080614), Sep 17, 2000: CHARGER. INOPERATIVE. OAK - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTS AND THE EXIT IDENTIFIER AFT OF GALLEY 3 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY CHARGER/POWER 
- [SDR ASAA0080255](https://openairdocs.org/sdr/ASAA0080255), Apr 24, 2000: WIRE. BROKEN. SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHT AT ROW 6 WAS FOUND INOPERATIVE. REPAIRED WIRE IN FLOOR TRACK AND OPERATED NORMALLY. (M)
- [SDR ASAA0080247](https://openairdocs.org/sdr/ASAA0080247), Apr 16, 2000: BATTERY. DISCHARGED. SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 6 TO 9 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED N
- [SDR ASAA0080204](https://openairdocs.org/sdr/ASAA0080204), Mar 21, 2000: BATTERY. DISCHARGED. ODX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. RE-SECURED LOOSE BATTERY PACK CANNON PLUG AND REP
- [SDR ASAA9980065](https://openairdocs.org/sdr/ASAA9980065), Mar 18, 2000: SKIN. CRACKED. OAK - DURING MAINTENANCE CHECK, FOUND CRACK IN FUSELAGE SKIN AT L1 DOOR FORWARD UPPER CUTOUT. INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-05, FIG 25A. (M)
- [SDR ASAA0080043](https://openairdocs.org/sdr/ASAA0080043), Jan 18, 2000: INTERCOSTAL. CORRODED. PHX - DURING 30K CHECK, FOUND CORROSION ON INTERCOSTAL WEB FROM FS 1003 TO 1007, LONGERON 28L. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-
- [SDR ASAA0080048](https://openairdocs.org/sdr/ASAA0080048), Jan 18, 2000: SKIN. CORRODED. PHX - DURING 30K CHECK, FOUND CORROSION ON FUSELAGE SKIN FROM FS 1174 TO 1190, LONGERON 30. REPAIRED IAW ASA EA 5330-01417. (M)
- [SDR ASAA0080047](https://openairdocs.org/sdr/ASAA0080047), Jan 18, 2000: LONGERON. CORRODED. PHX - DURING 30K CHECK, FOUND CORROSION ON LONGERON 29L, FS 665. REPAIRED IAW ASA EA 5310-01796. (M)
- [SDR ASAA0080046](https://openairdocs.org/sdr/ASAA0080046), Jan 18, 2000: FLOORBEAM. CORRODED. PHX - DURING 30K CHECK, FOUND CORROSION ON FLOORBEAM WEB AT FS 1338, RBL 35. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW ASA EA 5310-10797. (M)
- [SDR ASAA0080045](https://openairdocs.org/sdr/ASAA0080045), Jan 18, 2000: FLOORBEAM. CORRODED. PHX - DURING 30K CHECK, FOUND CORROSION ON FLOORBEAM AT FS 1338, FROM RBL 11 TO RBL 44. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW ASA EA 5310-01776.
- [SDR ASAA0080044](https://openairdocs.org/sdr/ASAA0080044), Jan 18, 2000: WEB. DAMAGED. PHX - DURING 30K CHECK, FOUND HOLES WERE TORN AND OVERWORKED ON CABIN SUB FLOOR WEB BETWEEN FS 180 AND 200, LBL 60. REMOVED DAMAGED MATERIAL AND INSTALLED NEW P
- [SDR ASAA0080042](https://openairdocs.org/sdr/ASAA0080042), Jan 18, 2000: SHEAR TIE. CORRODED. PHX - DURING 30K CHECK, FOUND CORROSION ON SHEAR TIE AT FS 788, BETWEEN LONGERON 27L AND 28L. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-0
- [SDR ASAA0080041](https://openairdocs.org/sdr/ASAA0080041), Jan 18, 2000: FLOOR SUPPORT. CORRODED. PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SUB FLOOR WEB AT FS 218, XCW 48.0L. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-10-03 AND 
- [SDR ASAA0080040](https://openairdocs.org/sdr/ASAA0080040), Jan 18, 2000: RIB. DAMAGED. PHX - DURING 30K CHECK, FOUND ON LOWER RIB AT L1 DOOR, BETWEEN STOPS 8 AND 9. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-10-02A, 51-10-03,
- [SDR ASAA0080039](https://openairdocs.org/sdr/ASAA0080039), Jan 18, 2000: STRAP. CRACKED. PHX - DURING 30K CHECK, FOUND CRACK IN RIGHT WING L/E STRAP AT SKIN SPLICE AT XFS 194.85. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-30. (
- [SDR ASAA0080038](https://openairdocs.org/sdr/ASAA0080038), Jan 18, 2000: SKIN. CRACKED. PHX - DURING 30K CHECK, FOUND CRACK IN LEFT WING L/E SKIN SPLICE AND ATTACH CLIP AT XFS 196.236. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 5
- [SDR ASAA0080037](https://openairdocs.org/sdr/ASAA0080037), Jan 18, 2000: SKIN. GOUGED. PHX - DURING 30K CHECK, FOUND GOUGE ON FUSELAGE SKIN AT FS 1084, LONGERON 18L. BLENDED DAMAGED AREA AND INSTALLED INTERNAL DOUBLER IAW DC9 SRM 53-04, FIG 38. (M
- [SDR ASAA0080036](https://openairdocs.org/sdr/ASAA0080036), Jan 18, 2000: SKIN. LIGHTNING STRIKE. PHX - DURING 30K CHECK, FOUND LIGHTNING STRIKE DAMAGE WAS FOUND ON FUSELAGE SKIN AT FS 618, LONGERON 19L. BLENDED DAMAGED AREA AND INSTALLED INTERNAL DOUBLER IA
- [SDR ASAA0080035](https://openairdocs.org/sdr/ASAA0080035), Jan 18, 2000: SKIN. LIGHTNING STRIKE. PHX - DURING 30K CHECK, FOUND LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN AT FS 101, LONGERON 14R. REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER IAW DC9 SR
- [SDR ASAA0080034](https://openairdocs.org/sdr/ASAA0080034), Jan 18, 2000: CARGO TRACK. CORRODED. PHX - DURING 30K CHECK, FOUND CORROSION ON CARGO COMPARTMENT TIEDOWN TRACK FROM FS 1212 TO 1320, RBL 16. REPLACED TRACK SECTION IAW DC9 SRM 51-30. (M)
- [SDR ASAA0080033](https://openairdocs.org/sdr/ASAA0080033), Jan 18, 2000: CARGO TRACK. CORRODED. PHX - DURING 30K CHECK, FOUND CORROSION ON CARGO COMPARTMENT TIEDOWN TRACK FROM FS 1222 TO 1320, LBL 16. REPLACED TRACK SECTION IAW DC9 SRM 53-24. (M)
- [SDR ASAA0080032](https://openairdocs.org/sdr/ASAA0080032), Jan 18, 2000: SEAT TRACK. CORRODED. PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK FROM FS 1125 TO 1205, LBL 51. REPLACED SEAT TRACK SECTION IAW DC9 SRM 53-01 FIG 1. (M)
- [SDR ASAA0080031](https://openairdocs.org/sdr/ASAA0080031), Jan 18, 2000: SEAT TRACK. CORRODED. PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK FROM FS 1003 TO 1079, LBL 51. REPLACED SEAT TRACK SECTION IAW DC9 SRM 53-05. (M)
- [SDR ASAA0080030](https://openairdocs.org/sdr/ASAA0080030), Jan 18, 2000: SEAT TRACK. CORRODED. PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK FROM FS 693 TO 793, LBL 51. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW SRM 53-05. (M)
- [SDR ASAA0080029](https://openairdocs.org/sdr/ASAA0080029), Jan 18, 2000: SEAT TRACK. CORRODED. PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK FROM FS 218 TO 256, RBL 44 TO RBL 46. REPLACED SEAT TRACK SECTION IAW DC9 SRM 51-30-02. (M)
- [SDR ASAA0080028](https://openairdocs.org/sdr/ASAA0080028), Jan 18, 2000: SEAT TRACK. CORRODED. PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK AT FS 237, RBL 24. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-05. (M)
- [SDR ASAA0080027](https://openairdocs.org/sdr/ASAA0080027), Jan 18, 2000: FLOOR SUPPORT. CORRODED. PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SUB FLOOR WEB AT FS 212, RBL 2. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER IAW DC9 SRM 53-14-01, FIG 11. (M
- [SDR ASAA0080026](https://openairdocs.org/sdr/ASAA0080026), Jan 18, 2000: SEAT TRACK. CORRODED. PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK AT FS 206, LBL 51. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-05. (M)
- [SDR ASAA0080025](https://openairdocs.org/sdr/ASAA0080025), Jan 18, 2000: FRAME. CRACKED. PHX - DURING 30K CHECK, FOUND CRACKS IN FRAME AT FS 1446, BETWEEN LONGERON 8L AND 8R. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-10-2A. (M

All 114: https://openairdocs.org/deregistered/N951AS-2009-04-08/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB SEA97FA202](https://openairdocs.org/ntsb/SEA97FA202), Sep 2, 1997: McDonnell Douglas DC-9-82 (MD-82) (N951AS), Seattle, WA, substantial damage. Probable cause: fatigue failure of the nose landing gear upper lock link, due in part to reduced strength after the manufacturing process was changed from forged to machined plate stock; and inadequate…

## 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.

- [Accident 19970901047979A](https://openairdocs.org/incident/19970901047979A), Sep 1, 1997: Doug DC982 (N951AS), Seattle, WA, Substantial damage. (-16) On sept. 1, 1997, upon landing gear extention for landing at Seattle airport, the crew of Alaska airlines flight 255 reported an unsafe gear indication…

---
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.