# N9336: 1968 Douglas DC-9-31, registration cancelled 2008-07-02 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 2, 2008 - Status when cancelled: Sale reported - Airframe: [Douglas DC-9-31](https://openairdocs.org/model/douglas-dc-9-31) (registry code 3022065) - 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: 47338 - Year built: 1968 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard - Last registry action: May 29, 2008 - Mode S code: ACF3F8 - Location: [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale) - Owner type: Individual - Owner's area on the map: 26.1860° N, 80.1727° W: Placed by OpenAirDocs at the center of ZIP code 33309, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N9336 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=9336 - Page: https://openairdocs.org/deregistered/N9336-2008-07-02 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-9-31: https://openairdocs.org/model/douglas-dc-9-31.md ## Service difficulty reports (36) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 0201569972](https://openairdocs.org/sdr/0201569972), May 12, 2002: VALVE. FAILED. DURING CLIMBOUT WITH THE ENGINE AND AIRFOIL ANTI-ICE SYSTEM ACTIVATED, THE FORWARD AND LEFT REAR LAV SMOKE DETECTOR ALARMS SOUNDED. THE RIGHT AIR CONDITION SUPP - [SDR 0003919972](https://openairdocs.org/sdr/0003919972), Oct 14, 2000: BATTERY PACK. INOPERATIVE. DURING LINE CHECK, FOUND THE EMERGENCY LIGHTS IN THE TAIL COMPARTMENT WOULD NOT EXTINGUISH WHEN POWER REMOVED FROM THE AIRCRAFT. MAINTENANCE INSPECTED FURTHER A - [SDR 0003909972](https://openairdocs.org/sdr/0003909972), Oct 12, 2000: BATTERY PACK. INOPERATIVE. DURING LINE CHECK, FOUND EMERGENCY LIGHTS IN THE COCKPIT AND THE ENTRYWAY INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONAL CHECK NORMAL. - [SDR 0002959972](https://openairdocs.org/sdr/0002959972), Aug 18, 2000: WARNING LIGHT. ILLUMINATED. SLAT DISAGREEMENT LIGHT CAME ON AND BLUE SLAT EXTEND LIGHT DID NOT ILLUMINATE DURNG APPROACH TO MBS. EXPERIENCED SLIGHT AIRCRAFT ROLL TO THE RIGHT. COMPLIED WIT - [SDR 0000679972](https://openairdocs.org/sdr/0000679972), Mar 30, 2000: FLOORBEAM. CORRODED. CORROSION ON FLOOR SUPPORT BETWEEN STA 200 AND 218 INBD OF RT SEAT TRACK. REPAIRED PER EA 99-172295 LOG PAGE 1419182. - [SDR 9809509972](https://openairdocs.org/sdr/9809509972), Jun 9, 1998: T-DUCT. LACK OF LUBE. SLAT DISAGREEMENT LIGHT ILLUMINATED ACCOMPANIED BY AIRCRAFT ROLL ON SLAT EXTENSION DURING APPROACH INTO JAN. FLIGHT CREW DECLARED AN EMERGENCY AND THE AIRCRAFT - [SDR 9718949972](https://openairdocs.org/sdr/9718949972), Oct 5, 1997: BATTERY PACK. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS AT ROWS 12 THRU 14 INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY, OPERATIONAL CHECK NO - [SDR 9712999972](https://openairdocs.org/sdr/9712999972), Jul 2, 1997: BATTERIES. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. - [SDR 9710499972](https://openairdocs.org/sdr/9710499972), May 28, 1997: EPR INDICATOR. MALFUNCTIONED. AS TAKEOFF POWER WAS APPLIED, THE LEFT ENGINE EPR INDICATION WOULD NOT REACH TARGET EPR. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE - [SDR 9709419972](https://openairdocs.org/sdr/9709419972), May 12, 1997: CLIPS. OUT OF ADJUST. DURING M-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL EXTERIOR TAIL CONE RELEASE HANDLE FROM CLIPS. ALSO, FOUND THE LEFT TAIL CONE CABLE FRAYED BELOW - [SDR 9709599972](https://openairdocs.org/sdr/9709599972), May 8, 1997: FRAME. CORRODED. DURING 'M' CHECK, FOUND CORROSION ON T-CAP UPPER SURFACE 6 INCHES TO THE RIGHT OF THE KEEL BEAM FS 756. REPAIRED PER EA 99-112865. - [SDR 9708619972](https://openairdocs.org/sdr/9708619972), Apr 29, 1997: BULKHEAD. CRACKED. DURING M-CHECK, FOUND A CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE BULKHEAD FS 105, LEFT SIDE, 22 INCHES INBOARD OF FUSELAGE SKIN. REPAIRED PER E - [SDR 9708609972](https://openairdocs.org/sdr/9708609972), Apr 29, 1997: BULKHEAD. CRACKED. DURING M-CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE BULKHEAD FS 105 ABOVE RIGHT OUTBOARD VERTICAL BEAM. REPAIRED PER EA 99-112 - [SDR 9708699972](https://openairdocs.org/sdr/9708699972), Apr 27, 1997: FITTING. CORRODED. DURING M-CHECK, FOUND CORROSION ON BOTTOM INBOARD AFT KEEL FITTING IN THE RIGHT WHEEL WELL FS 740 TO 755. REPLACED FITTING PER SRM 51-30-2. - [SDR 9708689972](https://openairdocs.org/sdr/9708689972), Apr 27, 1997: FITTING. CORRODED. DURING M-CHECK, FOUND CORROSION ON BOTTOM INBOARD AFT KEEL FITTING IN THE LEFT WHEEL WELL FS 750 TO 755. REPLACED FITTING PER SRM 51-30-2. - [SDR 9708729972](https://openairdocs.org/sdr/9708729972), Apr 25, 1997: FITTING. CORRODED. DURING M-CHECK, FOUND CORROSION IN BOLT HOLES OF LONGERON 30 END FITTING FS 756. REPLACED END FITTING PER SRM 53-02, FIG 12. - [SDR 9708719972](https://openairdocs.org/sdr/9708719972), Apr 25, 1997: FITTING. CORRODED. DURING M-CHECK, FOUND CORROSION IN BOLT HOLES OF LONGERON 29R END FITTING FS 756. REPLACED END FITTING PER SRM 53-02, FIG 12. - [SDR 9708709972](https://openairdocs.org/sdr/9708709972), Apr 25, 1997: FITTING. CORRODED. DURING M-CHECK, FOUND CORROSION IN BOLT HOLES OF LONGERON 29L END FITTING AT FS 756. REPLACED END FITTING PER SRM 53-02 FIG 12. - [SDR 9700179972](https://openairdocs.org/sdr/9700179972), Jan 6, 1997: POWER SUPPLY. INOPERATIVE. DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL. - [SDR 9627539972](https://openairdocs.org/sdr/9627539972), Dec 31, 1996: BATTERIES. DISCHARGED. DURING PERIODIC CHECK, FOUND FORWARD OVERWING UPPER EMERGENCY LIGHTS ON BOTH LEFT AND RIGHT SIDES INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY, OPERATIONAL C - [SDR 9622739972](https://openairdocs.org/sdr/9622739972), Oct 24, 1996: POWER SUPPLY. MALFUNCTIONED. DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL. - [SDR 9622719972](https://openairdocs.org/sdr/9622719972), Oct 22, 1996: COUPLING. LOOSE. EN ROUTE, AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED WITH WING ANTI-ICE ACTIVATED. FLIGHT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENAN - [SDR 9622359972](https://openairdocs.org/sdr/9622359972), Oct 20, 1996: ANTI-ICE VALVE. FAILED. AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED AFTER TAKEOFF. WING ANTI-ICE BLUE LIGHT WAS NOT ON. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDEN - [SDR 9620019972](https://openairdocs.org/sdr/9620019972), Sep 13, 1996: LIGHT. INOPERATIVE. DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS AT ROWS 8 THROUGH 15 INOPERATIVE. REPLACED POWER SUPPLIES AND BATTERY PACKS, OPERATIONAL CHE - [SDR 9618269972](https://openairdocs.org/sdr/9618269972), Aug 19, 1996: WIRE. BROKEN. DURING LINE MAINTENANCE INSPECTION, FOUND LEFT OVERWING EMERGENCY EXIT LIGHTS DIM. REPAIRED GROUND WIRE TO LEFT OVERWING UPPER DOOR EMERGENCY LIGHTS. OPERATIONA - [SDR 9617009972](https://openairdocs.org/sdr/9617009972), Aug 3, 1996: PRESS REGULATOR. FAILED. AUTO PRESSURIZATION SYSTEM FAILED AFTER TAKEOFF. CABIN ALTITUDE CLIMBED IN CONJUNCTION WITH AIRCRAFT ALTITUDE. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDEN - [SDR 9616999972](https://openairdocs.org/sdr/9616999972), Aug 3, 1996: RELAY. MALFUNCTIONED. AUTO PRESSURIZATION SYSTEM FAILED AFTER TAKEOFF, OUTFLOW VALVE REMAINED OPEN. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE COULD NOT DUPLICAT - [SDR 9611949972](https://openairdocs.org/sdr/9611949972), May 26, 1996: BATTERIES. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS AT TAIL COMPARTMENT CATWALK INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL - [SDR 9601339972](https://openairdocs.org/sdr/9601339972), Jan 21, 1996: BATTERY PACK. DISCHARGED. DURING LINE CHECK, FOUND CEILING AND MID CABIN EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK GOOD. - [SDR 9521269972](https://openairdocs.org/sdr/9521269972), Dec 20, 1995: CONTROLLER. MALFUNCTIONED. ON THE FIRST TWO ATTEMPTS TO ENGAGE THE AUTOPILOT SYSTEM, THE AIRCRAFT EXPERIENCED A SLIGHT ROLL. AIRCRAFT OPERATED NORMALLY AFTER ENGAGING THE AUTOPILOT SYSTEM - [SDR 9520909972](https://openairdocs.org/sdr/9520909972), Dec 6, 1995: JAMB. CRACKED. DURING LINE CHECK, FOUND A CRACK IN THE FORWARD AIRSTAIR DOOR JAMB, AFT LOWER CORNER. REPAIRED JAMB PER EA 99-103377. - [SDR 9520869972](https://openairdocs.org/sdr/9520869972), Dec 5, 1995: INTERCOSTAL. CORRODED. DURING LINE CHECK, FOUND CORROSION ON THE FORWARD AIRSTAIR CUT OUT LOWER DOOR JAMB INTERCOSTAL. REPAIRED INTERCOSTAL (P/N 9957839-3) PER EA 99-103384. - [SDR 9517689972](https://openairdocs.org/sdr/9517689972), Oct 29, 1995: SKIN. CORRODED. DURING L-CHECK, FOUND CORROSION IN THE FUSELAGE SKIN AT FS 604, LONGERON 30. REPAIRED SKIN (P/N 5911418-503), PER EA 99-103309. - [SDR 9517269972](https://openairdocs.org/sdr/9517269972), Oct 29, 1995: BLKHD PANEL. CRACKED. DURING L-CHECK, FOUND A 2.5 INCH CRACK IN THE FS 83 PRESSURE PANEL, LEFT SIDE. REPAIRED PER EO 5310-01134. - [SDR 9514209972](https://openairdocs.org/sdr/9514209972), Sep 11, 1995: CONTROL VALVE. MALFUNCTIONED. DURING CLIMBOUT, RIGHT AIR CONDITIONING PACK BEGAN SMOKING AND THEN WENT TO FULL HOT. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED TEMPERATURE C - [SDR 9504719972](https://openairdocs.org/sdr/9504719972), Feb 21, 1995: OIL CAP. NOT SECURE. NR 1 ENGINE OIL QUANTITY DECREASED TO 7 QUARTS ON TAKEOFF. REPORTS FROM THE TOWER INDICATED FLUID LEAKING FROM THE LEFT ENGINE. THE AIRCRAFT RETURNED TO MSP AND ## FAA accident and incident reports (3) 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 19961230043919I](https://openairdocs.org/incident/19961230043919I), Dec 30, 1996: Doug DC931 (N9336), Columbus, OH, Minor damage. Narrative: aircraft left wing tip struck runway prior to or during a go-around. Damage was to LH landing light, position light and leading edge slat. Lower… - [Incident 19930828037959I](https://openairdocs.org/incident/19930828037959I), Aug 28, 1993: Doug DC931 (N9336), Kansas City, MO. Right engine quit in flight. Diverted to Kansas City. Replaced csd and generator. - [Incident 19870823058049I](https://openairdocs.org/incident/19870823058049I), Aug 23, 1987: Doug DC931 (N9336), Memphis, TN. Ac emergency buss light came on in flight. Replaced R2-46. ## Other aircraft with N9336 - [Cancelled 1938-08-20](https://openairdocs.org/deregistered/N9336-1938-08-20): Arrow Aircraft & Motors ARROW SPORT, S/N 352. Owner: [Howard Fletcher](https://openairdocs.org/faa-owner/HOWARD%20FLETCHER), [Kerrville, TX](https://openairdocs.org/faa-place/TX/Kerrville) --- 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.