# N951AX: 1974 Douglas DC-9-41, registration cancelled 2013-07-11

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 11, 2013
- Status when cancelled: Sale reported, canceled
- Airframe: [Douglas DC-9-41](https://openairdocs.org/model/douglas-dc-9-41) (registry code 302207N)
- 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: 47616
- Year built: 1974
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: July 6, 1990
- Last registry action: November 10, 2011
- Mode S code: AD3874
- Location: [Boca Raton, FL](https://openairdocs.org/faa-place/FL/Boca%20Raton)
- Owner type: Individual
- Owner's area on the map: 26.3471° N, 80.1592° W: Placed by OpenAirDocs at the center of ZIP code 33433, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N951AX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=951AX
- Page: https://openairdocs.org/deregistered/N951AX-2013-07-11

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 Douglas DC-9-41: https://openairdocs.org/model/douglas-dc-9-41.md

## Service difficulty reports (83, newest 50)

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

- [SDR ABXA080231](https://openairdocs.org/sdr/ABXA080231), Aug 8, 2008: CIRCUIT BOARD. SHORTED. GPWS FAIL LIGHT AND TERR INOP LIGHT ON TAWS CIRCUIT BRAKE TRIPPED. NR 1 ADC AND NR 1 GS C/B TRIPPED. DEFERRED 61397 FOUND TAWS COMPUTER INOP. CAPPED AND STOWED 
- [SDR ABXA080187](https://openairdocs.org/sdr/ABXA080187), Jul 6, 2008: BATTERY. DISCHARGED. EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-0. (A)
- [SDR ABX2008F00000](https://openairdocs.org/sdr/ABX2008F00000), Jul 6, 2008: POWER SUPPLY. DEFECTIVE. EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY PACK IAW DC9 AMM 33-53-00. (K)
- [SDR ABXA080178](https://openairdocs.org/sdr/ABXA080178), Jun 7, 2008: WIRE. BURNED. WHILE TROUBLE SHOOTING THE INOP LT INBO TAIL LIGHT AND THIS LT AFT WING TIP LIGHT FOUND WIRE L 26AH20N BURNT FROM R5-1051D TO GROUND STUD 713 IAW WDM 33-42-02. 
- [SDR ABXA080124](https://openairdocs.org/sdr/ABXA080124), Apr 16, 2008: BUNGEE CYLINDER. LEAKING. RIGHT HYDRAULIC QUANTITY LOSS TO ZERO. FOUND LEFT MAIN LANDING GEAR HYDRAULIC BUNGEE CYLINDER LEAKING. REPLACED LEFT BUNGEE CYLINDER IAW DC9 AMM 32-32-03-2.
- [SDR ABXA070167](https://openairdocs.org/sdr/ABXA070167), May 10, 2007: INTERCOSTAL. CRACKED. FRAME BETWEEN STA 427 AND 446 CRACKED AT APPROXIMATELY 435. REMOVED AND REPLACED INTERCOSTAL IAW DC9 SRM.
- [SDR ABXA070166](https://openairdocs.org/sdr/ABXA070166), May 10, 2007: FLOOR SUPPORT. CRACKED. LEFT FLOOR TRACK END FITTING/CLIP CRACKED AND ATTACHING INTERCOSTAL WAS CORRODED UNDER NUT PLATES, STA 1056 - 1072, LONGERON 27 - 28 LEFT. REMOVED AND REPLACED 
- [SDR ABXA070165](https://openairdocs.org/sdr/ABXA070165), May 8, 2007: ANGLE. CRACKED. THE TEE ANGLE CRACKED, FORWARD DOOR JAMB, INBOARD MOUNT. REMOVED AND REPLACED TEE ANGLE IAW DC9 SRM 51-30-5.
- [SDR ABXA070091](https://openairdocs.org/sdr/ABXA070091), Apr 9, 2007: POWER SUPPLY. DEFECTIVE. EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW MM 33-53-02-4.
- [SDR ABXA070026](https://openairdocs.org/sdr/ABXA070026), Jan 29, 2007: SKIN. CRACKED. DURING INSPECTION OF FUSELAGE SKIN AT LONGERON 22, FOUND SKIN CRACKED AT LOWER AFT CORNER OF AIR STAIR DOOR, STA 200. REPAIRED CRACK IAW ABX EA 5300001-003-2.
- [SDR ABXA050112](https://openairdocs.org/sdr/ABXA050112), May 4, 2005: CUSP WEB. CRACKED. RIGHT CUSP WEB CRACKED AT EXISTING REPAIR, STA 1021 - 1041, RIGHT BUTT LINE 50. REMOVED AND REPLACED CUSP AT STA 1021 - 1041 IAW DC-9 SRM 53-03 AND 51-30-4.
- [SDR ABXA050108](https://openairdocs.org/sdr/ABXA050108), May 3, 2005: ATTACH ANGLE. CRACKED. UPPER PYLON ATTACH ANGLE CRACKED AT FORWARD END. REPAIRED AREA IAW DC-9 SRM 54-04.
- [SDR ABXA050111](https://openairdocs.org/sdr/ABXA050111), May 3, 2005: STOP FITTING. CRACKED. FORWARD UPPER STOP TEE FITTING CRACKED FORWARD LOWER CARGO DOOR. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-5.
- [SDR ABXA050110](https://openairdocs.org/sdr/ABXA050110), May 3, 2005: STIFFENER. CRACKED. AFT PRESSURE BULKHEAD RIGHT SIDE DOOR JAMB STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER IAW DC-9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA050109](https://openairdocs.org/sdr/ABXA050109), May 2, 2005: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT AT STA 1072 WAS CORRODED TOP AND BOTTOM SIDE LONGERON 28 LEFT - LONGERON 28 RIGHT. REMOVED AND REPLACED FLOOR SUPPORT SECTIONS IAW DC-9 SRM 51-30-
- [SDR ABXA040270](https://openairdocs.org/sdr/ABXA040270), Jul 25, 2004: ENGINE. DEFECTIVE. LEFT ENGINE LOW OIL QUANTITY 0, LOW OIL PRESSURE 35 PSI, OIL PRESSURE LIGHT ON, SHUT DOWN LEFT ENGINE. FROM PDX, MADE DIVERSION TO YAK. REMOVED AND REPLACED LEF
- [SDR ABXA030458](https://openairdocs.org/sdr/ABXA030458), Dec 4, 2003: LIGHT. SHORTED. ODOR OF WIRES BURNING FOLLOWED BY MAP AND BRIEFCASE CIRCUIT BREAKER TRIPPED, AND LOSS OF THOSE LIGHTS. ODOR WENT AWAY. CAPTAIN'S MAP LIGHT LENS ASSEMBLY SHORTED
- [SDR ABXA030372](https://openairdocs.org/sdr/ABXA030372), Sep 12, 2003: CHANNEL. CRACKED. LEFT MAIN LANDING GEAR INBOARD DOOR CRACKED AT FORWARD HINGE. REPLACED PAN SECTION AND REPAIRED AREA, REINSTALLED DOOR IAW DC-9 MM 32-12-01-2 AND SRM 52-05, 53-
- [SDR ABXA030373](https://openairdocs.org/sdr/ABXA030373), Sep 9, 2003: BEAM. CRACKED. AFT LOWER CARGO DOOR BEAM NR 2 END FITTING CRACKED ON AFT SIDE. REPLACED AFT LOWER CARGO DOOR BEAM NR 2 END FITTING IAW DC-9 SRM 51-30-5.
- [SDR ABXA030374](https://openairdocs.org/sdr/ABXA030374), Sep 9, 2003: SHEAR TIE. CRACKED. SHEAR TIE CRACKED, FS 1021 AT LONGERON 14 RIGHT. REPLACED SECTION OF SHEAR TIE IAW DC-9 SRM.
- [SDR ABXA030319](https://openairdocs.org/sdr/ABXA030319), Aug 1, 2003: PIVOT ASSY. LACK OF LUBE. RIGHT MAIN LANDING GEAR CAME OUT ON UPLATCH CHECK. RECYCLED LANDING GEAR AND RECEIVED NORMAL INDICATION. FOUND UPLOCK PIVOT BOLT BOUND UP TO HOOK AND STRUCTURE 
- [SDR ABXA030287](https://openairdocs.org/sdr/ABXA030287), Jul 18, 2003: UPLOCK SWITCH. FAILED. RT GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. LIGHT WENT OUT AFTER GEAR WAS RECYCLED. ALL INDICATIONS WERE NORMAL. REPLACED RIGHT GEAR UPLOCK SWITCH I
- [SDR ABXA030284](https://openairdocs.org/sdr/ABXA030284), Jul 15, 2003: PIN. BENT. AFTER TAKEOFF, RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ON AFTER INITIAL RETRACTION. THERE WAS NO ASSOCIATED YAW OR NOISE. AFTER RECYCLING GEAR, ALL INDICATIONS WE
- [SDR ABXA030076](https://openairdocs.org/sdr/ABXA030076), Feb 18, 2003: DRAIN. FROZEN. DEPLOYING SPOILERS CREATED A LT ROLL OF 5 DEGREES PER SECOND. AILERONS BINDED DURING APPROACH, AILERONS HEAVY DURING APPROACH. FOUND SLAT PANEL DRAINS BLOCKED B
- [SDR ABXA010674](https://openairdocs.org/sdr/ABXA010674), Jan 4, 2002: PANEL. CORRODED. RIGHT SLANT PANEL HAD CORROSION AROUND NUT PLATES, LOWER EDGE FROM INBOARD TO OUTBOARD. REPLACED SLANT PANEL IAW DC-9 SRM 51-30-2, 51-10-4, 51-30-1 AND 51-20-6.
- [SDR ABXA010673](https://openairdocs.org/sdr/ABXA010673), Jan 3, 2002: PANEL. CORRODED. LEFT SLANT PANEL CORRODED AROUND NUTPLATES. REPLACED SLANT PANEL IAW DC-9 SRM 51-30-1.
- [SDR ABXA010672](https://openairdocs.org/sdr/ABXA010672), Jan 3, 2002: ATTACH ANGLE. CORRODED. LEFT WHEEL WELL OUTBOARD SLANT PANEL ATTACH ANGLE EXFOLIATED AT LOWER FASTENER. LOCATED AND DRILLED SLANT PANEL ATTACH ANGLE IAW DC-9 SRM 51-30-5.
- [SDR ABXA010671](https://openairdocs.org/sdr/ABXA010671), Jan 3, 2002: ANGLE. CRACKED. LEFT WHEEL WELL ATTACH ANGLE CRACKED IN RADIUS, JUST OUTBOARD OF THE TRAP PANEL, ABOVE THE HYDRAULIC SERVICE ACCESS. REPLACED ANGLE IAW DC-9 SRM.
- [SDR ABXA010584](https://openairdocs.org/sdr/ABXA010584), Nov 13, 2001: RELAY. MALFUNCTIONED. DURING DESCENT, ALTERNATE LONGITUDINAL TRIM RAN AWAY. AUTOPILOT AND ALTERNATE TRIM CIRCUIT BREAKERS PULLED. COULD NOT DUPLICATE ON GROUND. REPLACED ALTERNATE TR
- [SDR ABXA010235](https://openairdocs.org/sdr/ABXA010235), May 15, 2001: LOCK. DISCONNECTED. THE PILOTS CLEARVIEW WINDOW AFT LOCK WAS DISCONNECTED. MAINTENANCE INSPECTED AND RECONNECTED THE AFT LOCK AS REQUIRED.
- [SDR ABXA010063](https://openairdocs.org/sdr/ABXA010063), Feb 24, 2001: BATTERY PACK. DIRTY. EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE INSPECTED AND CLEANED EMERGENCY LIGHT BATTERY PACK AT FSD AND RETURNED THE A/C TO SERVICE. UPON ARRIVAL AT ILN, MAI
- [SDR ABXA0100016](https://openairdocs.org/sdr/ABXA0100016), Jan 21, 2001: BATTERY. DISCHARGED. EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE EMERGENCY LIGHTS POWER SUPPLY BATTERIES IAW DC-9 MM 33-53-02-4-0001.
- [SDR ABXA000482](https://openairdocs.org/sdr/ABXA000482), Oct 30, 2000: WHEEL. JAMMED. TOP OF DESCENT UPON SETTING LANDING ELEVATION, CABIN CLIMB INDICATOR SHOWED 1500 FPM CLIMB, WENT ON OXYGEN, WENT TO MANUAL. COULD NOT CONTROL. PRESSURIZATION WH
- [SDR ABXA000275](https://openairdocs.org/sdr/ABXA000275), May 11, 2000: SKIN. CORRODED. FUSELAGE SKIN CORRODED UNDER LEFT STATIC PORT PLATE. REPAIRED SKIN IAW DC9 SRM 53-04.
- [SDR ABXA000274](https://openairdocs.org/sdr/ABXA000274), May 11, 2000: SKIN. CORRODED. CENTER KEEL FUSELAGE SKIN EXTERIOR BETWEEN MAIN LANDING GEAR INBOARD WHEEL WELL DOORS CORRODED. REPLACED SKIN IAW DC9 SRM 51-30-2.
- [SDR ABXA000253](https://openairdocs.org/sdr/ABXA000253), May 10, 2000: ANGLE. CRACKED. ATTACH ANGLE CRACKED INSIDE AFT PRESSURE DOME DOOR AT UPPER DOOR HINGE. REPLACED ANGLE (P/N 9915565-157) IAW DC9 SRM 51-30-2.
- [SDR ABXA000257](https://openairdocs.org/sdr/ABXA000257), May 10, 2000: PANEL. DELAMINATED. TRAILING EDGE PANEL FORWARD OF OUTBOARD END OF LEFT AILERON DELAMINATED. REPLACED TRAILING EDGE PANEL IAW DC9 SRM 51-30-1.
- [SDR ABXA000256](https://openairdocs.org/sdr/ABXA000256), May 10, 2000: ANGLE. CRACKED. RIGHT DORSAL FIN ATTACH ANGLE CRACKED FORWARD OF AFT END OF ANGLE, 12 INCHES LONG. REPAIRED ANGLE IAW DC9 SRM 53-05, FIGURE 23.
- [SDR ABXA000255](https://openairdocs.org/sdr/ABXA000255), May 10, 2000: PAN. CRACKED. ELECTRONIC COMPARTMENT DOOR PAN IS CRACKED AT ALL FOUR CORNERS. REPLACED ELECTRONIC COMPARTMENT DOOR.
- [SDR ABXA000254](https://openairdocs.org/sdr/ABXA000254), May 10, 2000: ATTACH FITTING. CRACKED. AFT ENTRY DOOR LEFT LOWER STOP FITTING CRACKED AT FORWARD ATTACH POINT, 19 INCHES ABOVE FLOOR LEVEL. REPLACED FITTING IAW DC9 SRM 51-30-2.
- [SDR ABXA000260](https://openairdocs.org/sdr/ABXA000260), May 9, 2000: HINGE. CRACKED. RIGHT MAIN LANDING GEAR DOOR HINGE CRACKED AT LOBE. REPLACED HINGE IAW DC9 SRM 51-30-1.
- [SDR ABXA000259](https://openairdocs.org/sdr/ABXA000259), May 9, 2000: SKIN. CRACKED. FORWARD LOWER CARGO DOOR EXTERIOR SKIN CRACKED AT CENTER BEAM FORWARD ATTACH FITTING. REPAIRED IAW ABX REA D952-36797.
- [SDR ABXA000258](https://openairdocs.org/sdr/ABXA000258), May 5, 2000: ATTACH FITTING. CRACKED. SEAT TRACK ATTACH FITTING CRACKED AT STA 370. REPLACED FITTING IAW DC9 SRM 51-30-5.
- [SDR ABXA000236](https://openairdocs.org/sdr/ABXA000236), May 5, 2000: ANGLE. CRACKED. FORWARD SERVICE DOOR ATTACH ANGLE CRACKED INSIDE LIGHTENING HOLE, FORWARD UPPER CORNER OF DOOR AT UPPER BEAM TO DOOR PAN. REPLACED ANGLE IAW DC9 SRM 51-30-5.
- [SDR ABXA000235](https://openairdocs.org/sdr/ABXA000235), May 5, 2000: ATTACH FITTING. CRACKED. RIGHT FLOORBEAM TO KEEL ATTACH FITTING AT STATION 737 CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5.
- [SDR ABXA000234](https://openairdocs.org/sdr/ABXA000234), May 5, 2000: INTERCOSTAL. CRACKED. FORWARD LOWER CARGO COMPARTMENT DOOR INTERCOSTAL WEB CRACKED AT UPPER AFT DOOR STOP. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2.
- [SDR ABXA000233](https://openairdocs.org/sdr/ABXA000233), May 5, 2000: WEB. CRACKED. RIGHT CUSP WEB CRACKED AT STATION 1041. REPAIRED IAW DC9 SRM 53-01.
- [SDR ABXA000232](https://openairdocs.org/sdr/ABXA000232), May 5, 2000: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT STATION 1152 AND LONGERON 14 LEFT. REPAIRED SKIN IAW DC9SRM 53-04.
- [SDR ABXA000231](https://openairdocs.org/sdr/ABXA000231), May 5, 2000: WEB. CRACKED. FORWARD SUB FLOOR CRACKED AT STATION 203 AND RBL 22. REPAIRED SUB FLOOR IAW DC9 SRM53-0.
- [SDR ABXA000230](https://openairdocs.org/sdr/ABXA000230), May 1, 2000: FITTING. CRACKED. AFT ENTRY DOOR FRAME LEFT SIDE STOP FITTING CRACKED AT FORWARD END, 36 INCHES ABOVE FLOOR LEVEL. REPLACED FITTING IAW DC9 SRM 51-30-2.

All 83: https://openairdocs.org/deregistered/N951AX-2013-07-11/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 20040725017329I](https://openairdocs.org/incident/20040725017329I), Jul 25, 2004: Doug DC941 (N951AX), Yakutat, AK. (-23) Received report from anc roc that abx 1218, DC-9, pdx to anc, 40 s of yak declared emergency due to low oil pressure in one engine. That engine was shut…

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