# N9347: 1967 Mcdonnell Douglas DC-9-32, registration cancelled 2013-11-19 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 19, 2013 - Status when cancelled: Third renewal notice - Airframe: [Mcdonnell Douglas DC-9-32](https://openairdocs.org/model/mcdonnell-douglas-dc-9-32) (registry code 302206C) - Engine: [Pratt & Whitney JT8D-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 45827 - Year built: 1967 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: February 16, 1973 - Certificate issued: December 31, 2009 - Last registry action: December 31, 2009 - Mode S code: ACF7D2 - Owner when cancelled: [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC) - Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta) - Owner type: Corporation - Owner's area on the map: 33.6604° N, 84.3865° W: Placed by OpenAirDocs at the center of ZIP code 30354, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N9347 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=9347 - Page: https://openairdocs.org/deregistered/N9347-2013-11-19 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-9-32: https://openairdocs.org/model/mcdonnell-douglas-dc-9-32.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 0203069951](https://openairdocs.org/sdr/0203069951), Aug 12, 2002: DOOR. CRACKED. During HCK in DHN, crack damage was found on the lower forward cargo door inner and outer flange. Repaired per EA 99-191322. - [SDR 0203059951](https://openairdocs.org/sdr/0203059951), Aug 8, 2002: BULKHEAD. CRACKED. During HCK in DHN, the aft pressure bulkhead web was found cracked under Z=63.5 stiffener approx. 10" outboard of the ventral door jamb. Repaired per EA 99-1913 - [SDR 0201909951](https://openairdocs.org/sdr/0201909951), Jun 5, 2002: DUCT. DAMAGED. UPON SLAT EXTENSION, THE SLAT DISAGREEMENT ANNUNCIATOR LIGHT ILLUMINATED AND THE AIRCRAFT ROLLED. COMPLIED WITH COM PROCEDURES AND THE AIRCRAFT LANDED IN MSP WI - [SDR 0201919951](https://openairdocs.org/sdr/0201919951), May 25, 2002: DOOR. DAMAGED. DURING APPROACH FOR LANDING WHEN SLATS EXTENDED, THE AIRCRAFT ROLLED TO THE LEFT. THE SLAT DISAGREEMENT LIGHT WAS ON AND THE SLATS RETRACTED LIGHT WAS OUT. CREW - [SDR 9905399951](https://openairdocs.org/sdr/9905399951), Dec 20, 1999: BATTERY. DISCHARGED. DURING PERIODIC CHECK, FOUND FORWARD CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY. OPERATIONAL CHECK NORMAL. - [SDR 9904409951](https://openairdocs.org/sdr/9904409951), Oct 21, 1999: BATTERY PACK. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT ESCAPE PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. - [SDR 9901609951](https://openairdocs.org/sdr/9901609951), Apr 16, 1999: WIRE. LOOSE. DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS IN TAILCONE AND LIGHT ABOVE TAILCONE RELEASE HANDLE INOPERATIVE. MAINTENANCE FOUND BAD CONNEC - [SDR 9809919951](https://openairdocs.org/sdr/9809919951), Aug 16, 1998: PROX SENSOR. BROKEN. NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR EXTENSION. CREW RECYCLED GEAR TWICE WITH SAME RESULTS. EMERGENCY GEAR EXTENSION PRODUCERS WERE UTILIZED AN - [SDR 9807679951](https://openairdocs.org/sdr/9807679951), Apr 28, 1998: BATTERY PACK. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. - [SDR 9802019951](https://openairdocs.org/sdr/9802019951), Feb 1, 1998: BULB. BURNED OUT. LEFT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. CREW ABORTED APPROACH AND NORMAL INDICATIONS WERE ACHIEVED DURING GO-AROUND. AIRCRAF - [SDR 9724389951](https://openairdocs.org/sdr/9724389951), Dec 28, 1997: BATTERIES. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. - [SDR 9718569951](https://openairdocs.org/sdr/9718569951), Oct 1, 1997: BATTERY PACK. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS BETWEEN ROWS 8, 9, AND 10 INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. - [SDR 9714159951](https://openairdocs.org/sdr/9714159951), Jul 24, 1997: CSD. MALFUNCTIONED. AFTER TAKEOFF FROM DFW, LEFT CSD OIL PRESSURE ANNUNCIATOR CAME ON AND OIL TEMP PEGGED OFF SCALE. VOLTS INDICATED NORMAL BUT FREQUENCY READ VERY HIGH. CSD WOULD - [SDR 9624739951](https://openairdocs.org/sdr/9624739951), Nov 14, 1996: SWITCH PACK. FAILED. UPON RAISING GEAR AFTER TAKEOFF, GEAR WARNING HORN SOUNDED CONTINUOUSLY. RECYCLED GEAR SEVERAL TIMES, BOTH CLEAN AND FLAPS 15. CYCLED THROTTLES UP AND PUSHED HO - [SDR 9614739951](https://openairdocs.org/sdr/9614739951), Nov 14, 1996: SWITCH. FAILED. UPON RAISING GEAR AFTER TAKEOFF, GEAR WARNING HORN SOUNDED CONTINUOUSLY. RECYCLED GEAR SEVERAL TIMES, BOTH CLEAN AND FLAPS 15. CYCLED THROTTLES UP AND PUSHED HO - [SDR 9624249951](https://openairdocs.org/sdr/9624249951), Nov 6, 1996: FRAME. CORRODED. DURING H-CHECK, FOUND CORROSION ON THE FS 218 FRAME LOWER CHORD AT LONGERON 30. REPAIRED FRAME (P/N S 2777930-5) PER EA 99-109580. - [SDR 9624239951](https://openairdocs.org/sdr/9624239951), Nov 5, 1996: SKIN. CORRODED. DURING H-CHECK, FOUND CORROSION ON THE FUSELGE SKIN AND FINGER DOUBLER AT FS 510 FROM LONGERON 29L TO 29R. REPAIRED SKIN (P/N 5911412-191, -55). - [SDR 9624229951](https://openairdocs.org/sdr/9624229951), Nov 5, 1996: LONGERON. CORRODED. DURING H-CHECK, FOUND CORROSION AT LONGERONS 29L AND 29R AT FS 579. REPAIRED LONGERONS (P/N 3920596-1) PER EA 99-120176, 99-120174. - [SDR 9624209951](https://openairdocs.org/sdr/9624209951), Oct 31, 1996: FITTING. CORRODED. DURING H-CHECK, FOUND CORROSION ON THE NR 2 PYLON LOWER FORWARD SURFACE BEAVER TAIL FITTING AND LOWER SPAR CHORD. REPLACED FITTING AND REMOVED SPAR CORROSION PE - [SDR 9624189951](https://openairdocs.org/sdr/9624189951), Oct 29, 1996: FRAME. CORRODED. DURING H-CHECK, FOUND CORROSION ON THE FS 756 BULKHEAD FRAME T-CHORD AT LONGERON 29L. REPAIRED FRAME (P/N 9958212-3) PER EA 99-109572. - [SDR 9624169951](https://openairdocs.org/sdr/9624169951), Oct 28, 1996: SKIN. DELAMINATED. DURING H-CHECK, FOUND DELAMINATION IN THE LEFT WING FLAP TRAILING EDGE UPPER SKIN AT XFLS 187-235. REPAIRED SKIN (P/N 9957578-503) PER EA 99-120171. - [SDR 9622939951](https://openairdocs.org/sdr/9622939951), Oct 26, 1996: FITTING. CORRODED. DURING H-CHECK, FOUND CORROSION ON BOTH THE LEFT AND RIGHT OUTBOARD BATHTUB FITTINGS IN THE MAIN LANDING GEAR WHEELWELLS. REPLACED FITTINGS PER SRM 51-01, PAR.1 - [SDR 9622259951](https://openairdocs.org/sdr/9622259951), Oct 17, 1996: FITTING. CORRODED. DURING H-CHECK, FOUND CORROSION ON THE LEFT WHEEL WELL ATTACH FITTING FS 690 AT THE KEEL SKIN. REPLACED FITTING PER SRM 53-01 FIG 1. - [SDR 9620949951](https://openairdocs.org/sdr/9620949951), Sep 29, 1996: LIGHTS. INOPERATIVE. DURING LINE MAINTENANCE INSPECTION, FOUND ALL OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BOTH BATTERY PACKS AND POWER SUPPLIES, OPERATIONAL CHECK NORM - [SDR 9619509951](https://openairdocs.org/sdr/9619509951), Sep 7, 1996: IND SWITCH. MALFUNCTIONED. DURING APPROACH INTO MSP, NOSE LANDING GEAR GREEN DOWNLOCK LIGHT DID NOT ILLUMINATE AFTER GEAR WAS EXTENDED. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. - [SDR 9606279951](https://openairdocs.org/sdr/9606279951), Mar 18, 1996: BATTERY PACK. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT ENGINE NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. - [SDR 9604889951](https://openairdocs.org/sdr/9604889951), Feb 28, 1996: UPLOCK LATCH. BINDING. DURING CLIMBOUT, RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FREED - [SDR 9521129952](https://openairdocs.org/sdr/9521129952), Dec 18, 1995: GENERATOR. FAILED. DURING CRUISE, THE RIGHT AC BUS, RIGHT GENERATOR, AND DC BUS OFF LIGHTS ILLUMINATED. THE RIGHT DC BUS WAS RESTORED BY DC BUS CROSSTIE. AIRCRAFT CONTINUED TO MSP - [SDR 9513409951](https://openairdocs.org/sdr/9513409951), Aug 27, 1995: RMI COMPASS. MALFUNCTIONED. LOSS OF NR 2 COMPASS INDICATOR OCCURRED DURING INITIAL SPOOL UP ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. REPLACED NR 2 RMI. OPERATIONAL CHECK OK, AIRCR - [SDR 9510679951](https://openairdocs.org/sdr/9510679951), Jul 4, 1995: FUEL CONTROL. REQD SERVICE. NR 1 ENGINE EPR FLUCTUATED WHILE ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AT 70 KTS, FLIGHT RETURNED TO THE GATE. MAINTENANCE DRAINED THE F.C.U. MOISTURE TRAP A - [SDR 9510019951](https://openairdocs.org/sdr/9510019951), Jun 21, 1995: THERMOSTAT. LEAKING. TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF AT 60 KNOTS AND RETURNED TO GATE. FOUND SMALL AIR LEAK AT THERMOSTAT, TIGHT - [SDR 9506569951](https://openairdocs.org/sdr/9506569951), Apr 21, 1995: VENT VALVE. MALFUNCTIONED. FUEL BEGAN LEAKING FROM RIGHT WING TANK EN ROUTE PVD-DTW. LEAK WAS APPROXIMATELY 1600 LBS IN ONE HOUR. FLIGHT DIVERTED TO BUF AND LANDED WITHOUT INCIDENT. REPLA - [SDR 9502609951](https://openairdocs.org/sdr/9502609951), Feb 12, 1995: CABLE. FRAYED. DURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE USING THE INTERIOR HANDLE. ALSO, FOUND THE TAILCONE CABLE FRAYED BETWEEN - [SDR 9502269951](https://openairdocs.org/sdr/9502269951), Feb 9, 1995: SKIN. OIL CANNED. DURING PERIODIC CHECK, FOUND OIL CANNING IN THE FUSELAGE SKIN FS 1056 - 1080 BETWEEN LONGERONS 17R - 18R. REPAIRED PER EA 99-096893. - [SDR 9502219951](https://openairdocs.org/sdr/9502219951), Feb 7, 1995: LONGERON. CRACKED. DURING PERIODIC CHECK, FOUND CRACKS IN LONGERON 17R AT FS 389 AND FS 408 AND IN LONGERON 17L AT FS 435. REPAIRED ALL THREE LOCATIONS PER EA 99-096899. - [SDR 9502159951](https://openairdocs.org/sdr/9502159951), Feb 4, 1995: SKIN. OIL CANNED. DURING PERIODIC CHECK, FOUND OIL CANNING IN FUSELAGE SKIN BETWEEN LOWER LEFT PYLON ATTACH ANGLE AND LONGERON 17L AT FS 1002 AND BETWEEN LONGERONS 17L - 18L AT F ## 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 19950421012739I](https://openairdocs.org/incident/19950421012739I), Apr 21, 1995: Doug DC932 (N9347), Buffalo, NY. Fuel leak. Diverted to buf. Landed safe. Replaced climb vent valve and drain float valve. - [Incident 19880226011049I](https://openairdocs.org/incident/19880226011049I), Feb 26, 1988: Doug DC932 (N9347), Memphis, TN. Fluctuating right EGT and fuel flow fluctuating on climb. Returned to airport. Replaced right EGT indicator. ## Other aircraft with N9347 - [Cancelled 1930-05-21](https://openairdocs.org/deregistered/N9347-1930-05-21): Moth 60-GM, S/N 30. Owner: [Moth Aircraft Corp](https://openairdocs.org/faa-owner/MOTH%20AIRCRAFT%20CORP), [Lowell, MA](https://openairdocs.org/faa-place/MA/Lowell) --- 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.