# N8914E: 1966 Douglas DC-9-14, registration cancelled 2013-03-11 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 11, 2013 - Status when cancelled: Sale reported, canceled - Airframe: [Douglas DC-9-14](https://openairdocs.org/model/douglas-dc-9-14) (registry code 3022034) - 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: 45831 - Year built: 1966 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: December 28, 1966 - Last registry action: February 7, 2012 - Mode S code: AC4BF4 - Location: [Mcminnville, OR](https://openairdocs.org/faa-place/OR/Mcminnville) - Owner type: Individual - Owner's area on the map: 45.2117° N, 123.2817° W: Placed by OpenAirDocs at the center of ZIP code 97128, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N8914E - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8914E - Page: https://openairdocs.org/deregistered/N8914E-2013-03-11 From the FAA registry file of November 5, 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-9-14: https://openairdocs.org/model/douglas-dc-9-14.md ## Service difficulty reports (31) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 0400339155](https://openairdocs.org/sdr/0400339155), Feb 28, 2004: LINE. BROKEN. AT FL330, THE CABIN BEGAN TO CLIMB AT 500 FPM AND COULD NOT BE CORRECTED. CREW INITIATED AN EMERGENCY DESCENT TO 10,000 FT AND THEN WAS ABLE TO CLIMB BACK TO A - [SDR 0104819155](https://openairdocs.org/sdr/0104819155), Nov 27, 2001: PAN. CRACKED. During HCK, the forward cargo door inner pan was found to be cracked between stops #1 and #2. The outer pan was also found cracked. Material .050" 2024-t4. Repa - [SDR 0003929155](https://openairdocs.org/sdr/0003929155), Oct 11, 2000: BATTERY PACK. INOPERATIVE. DURING LINE CHECK, FOUND EMERGENCY LIGHTS IN CEILING OF FIRST CLASS SECTION AND ESCAPE PATH LIGHTS IN TAIL COMPARTMENT INOPERATIVE. MAINTENANCE REPLACED THE BAT - [SDR 9904029155](https://openairdocs.org/sdr/9904029155), Sep 23, 1999: BATTERIES. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. - [SDR 9902829155](https://openairdocs.org/sdr/9902829155), Jul 20, 1999: BATTERIES. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. - [SDR 9902419155](https://openairdocs.org/sdr/9902419155), Jul 5, 1999: BATTERY. DISCHARGED. DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING ON CATWALK INOPERATIVE. MAINTENANCE REPLACED BATTERIES. OPERATIONAL CHECK NORMAL. - [SDR 9902119155](https://openairdocs.org/sdr/9902119155), Jun 17, 1999: BATTERY. DISCHARGED. DURING LINE CHECK, FOUND CATWALK EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. - [SDR 9901079155](https://openairdocs.org/sdr/9901079155), Mar 12, 1999: BATTERIES. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN PACK, OPERATIONAL CHECK NORMAL. - [SDR 9900859155](https://openairdocs.org/sdr/9900859155), Mar 10, 1999: BATTERY. DISCHARGED. DURING LINE CHECK, FOUND CATWALK EMERGENCY EXIT LIGHTING INOPEATIVE AND WIRING PULLED BACK. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERIES AND REPOSITIONED WIRI - [SDR 9806059155](https://openairdocs.org/sdr/9806059155), Apr 6, 1998: TR UNIT. INOPERATIVE. DURING CLIMBOUT, THE RADAR SYSTEM WAS UNRELIABLE. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RADAR TRANSCEIVER, OPERATIONAL CH - [SDR 9723479155](https://openairdocs.org/sdr/9723479155), Nov 25, 1997: SKIN. CRACKED. DURING LINE CHECK, FOUND CRACK IN FUSELAGE SKIN AT FS 69.5, RBL 20.5. REPAIRED PER EA 91-154146. - [SDR 9723469155](https://openairdocs.org/sdr/9723469155), Nov 25, 1997: SKIN. CRACKED. DURING LINE CHECK, FOUND CRACK IN FUSELAGE SKIN AT FS 76.5, RBL 26. REPAIRED PER EA 91-154146. - [SDR 9718759155](https://openairdocs.org/sdr/9718759155), Oct 2, 1997: BATTERY PACK. DISCHARGED. DURING LINE CHECK, FOUND A SECTION OF THE EMERGENCY LIGHTS WOULD NOT COME ON. REPLACED BATTERY PACK B5-091. OPERATIONAL CHECK OK. - [SDR 9719729155](https://openairdocs.org/sdr/9719729155), Oct 1, 1997: SKIN. CORRODED. DURING L CHECK, FOUND CORROSION ON FUSELAGE SKIN FS 758-817, LONGERON 24R-23R. REPAIRED PER EA 91-151723. - [SDR 9719409155](https://openairdocs.org/sdr/9719409155), Oct 1, 1997: DOUBLER. CORRODED. DURING L-CHECK, FOUND CORROSION ON THE AFT CARGO DOOR JAMB DOUBLER LOCATED AT THE LOWER FORWARD CORNER. REPAIRED PER EA 91-151721. - [SDR 9719399155](https://openairdocs.org/sdr/9719399155), Sep 28, 1997: LONGERON. CORRODED. DURING L-CHECK, FOUND CORROSION ON LONGERON 29L, FS 604. REPAIRED PER EA 91-151724. - [SDR 9718469155](https://openairdocs.org/sdr/9718469155), Sep 25, 1997: FITTING. CORRODED. DURING L CHECK, FOUND CORROSION ON LONGERON 26L END FITTING AT FS 817. REPLACED FITTING (P/N 3914590-501) PER SRM 51-30-2. - [SDR 9718459155](https://openairdocs.org/sdr/9718459155), Sep 25, 1997: FITTING. CORRODED. DURING L CHECK, FOUND CORROSION ON LONGERON 28L END FITTING FS 817. REPLACED FITTING (P/N 3915134-503) PER SRM 51-30-2. - [SDR 9708389155](https://openairdocs.org/sdr/9708389155), Apr 26, 1997: WIRE. BROKEN. DURING LINE CHECK, FOUND SECOND FROM MOST FORWARD FLOOR PROXIMITY LIGHT INOPERAITVE. REPAIRED WIRING, OPERATIONAL CHECK OK. - [SDR 9707099155](https://openairdocs.org/sdr/9707099155), Apr 4, 1997: LATCH PINS. LACK OF LUBE. DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE TAILCONE AND EXCESSIVE FORCE WAS REQUIRED TO REMOVE INTERIOR HANDLE FROM CLIPS. CLEANED AN - [SDR 9620819155](https://openairdocs.org/sdr/9620819155), Sep 29, 1996: ENGINE. BIRD STRIKE. DURING CLIMB AT 1,000 FEET, THE AIRCRAFT ENCOUNTERED A FLOCK OF GEESE AT WHICH TIME THE RIGHT ENGINE INGESTED ONE BIRD. RIGHT ENGINE EPR DROPPED FROM 2 TO 1.8. - [SDR 9612899155](https://openairdocs.org/sdr/9612899155), Jun 11, 1996: BATTERY PACK. DISCHARGED. DURING LINE CHECK, FOUND RIGHT TAILCONE EMERGENCY SLIDE LIGHT AND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK IN POWER SUPPLY, OPERATIONAL - [SDR 9612889155](https://openairdocs.org/sdr/9612889155), Jun 11, 1996: BATTERY PACK. DISCHARGED. DURING LINE CHECK, FOUND LEFT TAILCONE EMERGENCY SLIDE LIGHT AND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK IN POWER SUPPLY, OPERATIONAL CH - [SDR 9604379155](https://openairdocs.org/sdr/9604379155), Jan 25, 1996: BULKHEAD. CORRODED. DURING H-CHECK, FOUND CORROSION ON THE HORIZONTAL PRESSURE PANEL AT FS 110, RIGHT SIDE BETWEEN THE TWO VERTICAL FITTINGS. REPAIRED PANEL PER EA 91-106633. - [SDR 9604369155](https://openairdocs.org/sdr/9604369155), Jan 25, 1996: SUPPORT. CORRODED. DURING H-CHECK, FOUND CORROSION ON THE FLOOR SUPPORTS AT FS 160, LBL 12 TO 56 AND AT LBL 12, FS 160 TO 164. REPAIRED SUPPORTS PER EA 91-106634. - [SDR 9604359155](https://openairdocs.org/sdr/9604359155), Jan 24, 1996: FRAME. CORRODED. DURING H-CHECK, FOUND CORROSION IN THE FS 817 FRAME AT THE RIGHT CUSP. REPAIRED FRAME (P/N 5910163-73) PER EA 91-102643. - [SDR 9602009155](https://openairdocs.org/sdr/9602009155), Jan 24, 1996: FITTING. CORRODED. DURING H-CHECK, FOUND CORROSION IN THE FORWARD SERVICE DOOR JAMB FLOOR TO FRAME SUPPORT FITTING, FS 200. REPLACED FITTING PER SRM 51-30-5. - [SDR 9604349155](https://openairdocs.org/sdr/9604349155), Jan 14, 1996: DOUBLER. CRACKED. DURING H-CHECK, FOUND CRACKS IN THE FORWARD ENTRY DOOR JAMB, SID PSE 53.09.031 DOOR STOP DOUBLERS AFT SIDE, 4TH AND 5TH STOPS FROM THE BOTTOM. REPAIRED JAMB PER - [SDR 9521399155](https://openairdocs.org/sdr/9521399155), Dec 25, 1995: STRUT. DEFLATED. LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF DUE TO GROUND SHIFT FAILURE. NOSE WHEEL WAS STEERABLE. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPACKED - [SDR 9517849155](https://openairdocs.org/sdr/9517849155), Nov 12, 1995: BATTERY PACK. DISCHARGED. DURING LINE CHECK, THE RIGHT OVERWING EXIT AND RIGHT CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY PACKS. OPERATIONAL CHECK GOOD. - [SDR 9502699155](https://openairdocs.org/sdr/9502699155), Feb 11, 1995: STICK SHAKER. MALFUNCTIONED. STALL INDICATION FAILURE LIGHT AND STICK SHAKER ACTIVATED ON FINAL APPROACH INTO DTW. PERFORMED STALL RECOVERY AND ACCOMPLISHED GO-AROUND PROCEDURES. NORMAL IND ## 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 19871104073539I](https://openairdocs.org/incident/19871104073539I), Nov 4, 1987: Doug DC914 (N8914E), Memphis, TN. Oil quanity dropped. Returned. Oil tank cap was off. Mechanic received a 3 day suspension. - [Incident 19860127004029I](https://openairdocs.org/incident/19860127004029I), Jan 27, 1986: Doug DC914 (N8914E), Memphis, TN. Right main gear had unsafe indication. Visually checked gear down. Landed and gear pinned. Replaced micro switch. - [Incident 19850515022939I](https://openairdocs.org/incident/19850515022939I), May 15, 1985: Doug DC914 (N8914E), Memphis, TN, Minor damage. Aircraft was pulling from ramp with wing walkers when wingtip struck N9355, other aircraft standing still. --- 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.