# N8925E: 1967 Douglas DC-9-31, registration cancelled 2010-08-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 3, 2010 - 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: 45840 - Year built: 1967 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: May 28, 1967 - Last registry action: July 13, 2010 - Mode S code: AC4FCE - 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/N8925E - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8925E - Page: https://openairdocs.org/deregistered/N8925E-2010-08-03 From the FAA registry file of October 31, 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 (41) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DALA105929945](https://openairdocs.org/sdr/DALA105929945), Mar 17, 2010: BATTERY. DISCHARGED. DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 5-8 & 18-21 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE APPROPRIATE - [SDR DALA102449945](https://openairdocs.org/sdr/DALA102449945), Feb 1, 2010: BATTERY PACK. WEAK. DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 5-7 AND THE RT OVERWING EMERGENCY EXIT SIGN WERE WEAK. MX REPLACED THE BATTERIES AND THE - [SDR NWAA094349945](https://openairdocs.org/sdr/NWAA094349945), Dec 16, 2009: BATTERY. DISCHARGED. DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 5-11 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE P - [SDR NWAA091079945](https://openairdocs.org/sdr/NWAA091079945), Apr 4, 2009: POWER SUPPLY. INOPERATIVE. DURING LINE CHECK, MX FOUND THAT ALL THREE OF THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WERE INOPERATIVE. MX REPLACED THE EMERGENCY - [SDR NWAA091069945](https://openairdocs.org/sdr/NWAA091069945), Apr 3, 2009: ACTUATOR. INTERMITTENT. ON APPROACH, AS THE FLIGHT CREW WAS CONFIGURING THE ACFT FOR LANDING, AN UNCOMMANDED ROLL OF THE ACFT TO THE LT OCCURRED WHEN THE SPEED BRAKES WERE USED. THE AC - [SDR 0302109945](https://openairdocs.org/sdr/0302109945), Oct 30, 2003: SKIN. CORRODED. DURING M-CHECK FOUND CRACK IN SKIN AT NR 6 FORWARD STOP OF DOOR 1L. REPAIRED PER EA 99-196420. - [SDR 0103289945](https://openairdocs.org/sdr/0103289945), Mar 29, 2001: SKIN. WRINKLED. DURING AN H-CHECK AT ATLANTA, WAVINESS AND SKIN MISMATCH WERE FOUND IN THE AREA OF THE ALTERNATE STATIC PORT. IN ORDER TO CORRECT THE DISCREPANCY, THE FUSELAGE - [SDR 0002809944](https://openairdocs.org/sdr/0002809944), Jul 27, 2000: BATTERY PACK. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS IN TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. - [SDR 9903819945](https://openairdocs.org/sdr/9903819945), Sep 12, 1999: CONNECTOR. DIRTY. DURING PERIODIC CHECK, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS ON CATWALK INOPERATIVE. CLEANED CORROSION FROM CATWALK STRIP CONNECTOR, OPERATIONAL CHECK NORMAL. - [SDR 9903589945](https://openairdocs.org/sdr/9903589945), Sep 7, 1999: BATTERY PACK. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. - [SDR 9903579945](https://openairdocs.org/sdr/9903579945), Sep 3, 1999: BATTERY PACK. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. - [SDR 9809169945](https://openairdocs.org/sdr/9809169945), May 13, 1998: OVERHEAT SENSOR. FAILED. TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT RETURNED TO MSY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE TAIL COMPARTMENT - [SDR 9804809945](https://openairdocs.org/sdr/9804809945), Mar 22, 1998: WIRE. BROKEN. DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS BETWEEN ROWS 12, 13, AND 14 INOPERATIVE. REPAIRED BROKEN WIRING, OPERATIONAL CHECK NO - [SDR 9805289945](https://openairdocs.org/sdr/9805289945), Mar 4, 1998: BRACKET. CRACKED. DURING H-CHECK, FOUND SHEAR TIE FITTING CRACKED AT FS 639 AT LONGERON 29L. REPLACED SHEAR TIE FITTING PER SRM 51-30-2. - [SDR 9716389945](https://openairdocs.org/sdr/9716389945), Sep 1, 1997: BATTERY PACK. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND AFT CEILING AND TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN PACK, OPERATIONAL CHECK NORMAL. - [SDR 9713709945](https://openairdocs.org/sdr/9713709945), Jul 12, 1997: AIR CYCLE MACH. LEAKING. TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AT 29,000 FEET. CREW SHUT DOWN LEFT PACK AND CABIN PRESSURE BEGAN TO RISE. CREW DECLARED AN EMERGENCY AND DE - [SDR 9713219945](https://openairdocs.org/sdr/9713219945), Jul 3, 1997: GASKET. BLOWN. TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. CAPTAIN DECLARED AN EMERGENCY AND FLIGHT WAS DIVERTED TO BNA. AIRCRAFT LANDED WITHOUT INCIDEN - [SDR 9705579945](https://openairdocs.org/sdr/9705579945), Mar 18, 1997: ANTI ICE VALVE. MALFUNCTIONED. AIRFOIL ICE PROTECTION PRESSURE ABNORMAL AND PRESSURE HIGH LIGHTS ILLUMINATED WITH TAIL DEICE SELECTED AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT - [SDR 9626299945](https://openairdocs.org/sdr/9626299945), Dec 10, 1996: TAILCONE. OUT OF ADJUST. DURING PERIODIC CHECK, TAILCONE RELEASE FORCE EXCEEDED MAXIMUM LIMITS ON FUNCTION DROP CHECK. ADJUSTED PER CITEXT 09-5350-1-0021, SECOND TEST WAS WITHIN LIMITS. - [SDR 9626229945](https://openairdocs.org/sdr/9626229945), Dec 6, 1996: FRAME. ELONGATED HOLE. DURING PERIODIC CHECK, FOUND FRAME AT FS 1038 BETWEEN LONGERONS 13L AND 14L WITH AN ELONGATED HOLE FROM BRACE ROD ATTACH FITTING. REPAIRED FRAME PER EA 99-111-1 - [SDR 9621499945](https://openairdocs.org/sdr/9621499945), Oct 7, 1996: GEN CONTL PNL. FAILED. RIGHT GENERATOR DROPPED OFF LINE ACCOMPANIED BY AC CROSSTIE LOCKOUT AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGH - [SDR 9619819945](https://openairdocs.org/sdr/9619819945), Sep 15, 1996: DOOR TRACK. DIRTY. AFTER TAKEOFF RECEIVED AN E/E DOOR WARNING INDICATION, LIGHT EXTINGUISHED AFT PRESSURIZATION. RETURNED TO SDF WITHOUT FURTHER INCIDENT. RECYCLED THE DOOR, CLEAN - [SDR 9618189945](https://openairdocs.org/sdr/9618189945), Aug 21, 1996: DOOR. NOT SEATED. AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. WIND NOISE WAS ALSO COMING FROM NOSE GEAR AREA. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. NOTE: FORWARD A - [SDR 9615039945](https://openairdocs.org/sdr/9615039945), Jul 11, 1996: BLEED AIR. LEAKING AIR. DURING CLIMBOUT, PASSENGERS REPORTED A FUEL LIKE SMELL IN CABIN. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THAT APU WAS BLEEDING RES - [SDR 9603489945](https://openairdocs.org/sdr/9603489945), Feb 11, 1996: SCHRADER VALVE. FAILED. DURING CLIMBOUT, THE AIRCRAFT WOULD NOT SHIFT FROM GROUND MODE TO FLIGHT MODE. AIRCRAFT WAS UNABLE TO PRESSURIZE AND NOSE WHEEL WAS STEERABLE. FLIGHT RETURNED T - [SDR 9601019945](https://openairdocs.org/sdr/9601019945), Jan 16, 1996: PRESS REG VLV. MALFUNCTIONED. DURING FLIGHT, THE AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED DURING WING ANTI-ICE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LIGHT REMAI - [SDR 9518529945](https://openairdocs.org/sdr/9518529945), Nov 19, 1995: THERMAL SWITCH. FAILED. DURING CLIMB, THE LEFT PACK OVERHEATED AND SMOKE ACCUMULATED IN THE FLIGHT DECK AND CABIN. DEACTIVATED THE LEFT PACK. FLIGHT RETURNED TO ROC AND LANDED WITHOUT - [SDR 9514489945](https://openairdocs.org/sdr/9514489945), Sep 24, 1995: INDICATION. MALFUNCTIONED. DURING APPROACH INTO MSP, AFTER SLATS AND FLAPS WERE EXTENDED FOR LANDING, SLAT DISAGREEMENT LIGHT ILLUMINATED WITH NO BLUE SLAT EXTENDED LIGHT. SLATS WERE VISU - [SDR 9514449945](https://openairdocs.org/sdr/9514449945), Sep 21, 1995: RETRACT MECH. MALFUNCTIONED. DURING SLAT EXTENSION ON APPROACH INTO MSP, SLAT EXTEND LIGHT BEGAN FLICKERING, THEN EXTINGUISHED AND SLAT DISAGREEMENT LIGHT ILLUMINATED. PERFORMED MISSED APPR - [SDR 9509419945](https://openairdocs.org/sdr/9509419945), Jun 9, 1995: WINDSHIELD. DELAMINATED. LEFT COCKPIT WINDSHIELD CRACKED EN ROUTE DFW TO MSP. CAPTAIN DECLARED AN EMERGENCY AND FLIGHT WAS DIVERTED TO STL, AN UNEVENTFUL LANDING WAS ACCOMPLISHED. FOUND - [SDR 9504089945](https://openairdocs.org/sdr/9504089945), Mar 10, 1995: BRACKET. CRACKED. DURING LINE CHECK, FOUND CRACK IN VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE REPAIR, RIGHT SIDE ABOVE THE RUDDER LEADING EDGE. REPAIRED PER XEA X9-53-82. - [SDR 9503179945](https://openairdocs.org/sdr/9503179945), Feb 26, 1995: STRUT. DEFLATED. LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF DUE TO GROUND SHIFT FAILURE. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. INSPECTED GROUND SHIFT LINKAGE AND - [SDR 9502249945](https://openairdocs.org/sdr/9502249945), Feb 8, 1995: STUDS. CORRODED. DURING PERIODIC CHECK, FOUND CORROSION ON NR 2 FLAP HINGE ATTACH STUDS. REPAIRED PER XEA X9-27-9. - [SDR 9502119945](https://openairdocs.org/sdr/9502119945), Feb 2, 1995: HINGE. CORRODED. DURING PERIODIC CHECK, FOUND CORROSION IN NR 3 FLAP HINGE MOUNTING HOLES, WS 251. REPLACED HINGE FITTING PER CITEXT 09-5740-1-9800. - [SDR 9500939945](https://openairdocs.org/sdr/9500939945), Jan 13, 1995: BULKHEAD. CORRODED. DURING PERIODIC CHECK, FOUND CORROSION IN FS 110 BULKHEAD TUNNEL AT LONGERON 27R, 6 INCHES UP FROM BOTTOM CORNER. REPAIRED PER XEA X9-53-50. - [SDR 9500869945](https://openairdocs.org/sdr/9500869945), Jan 12, 1995: HINGE FITT. CORRODED. DURING PERIODIC CHECK, FOUND CORROSION IN THE LEFT WING NR 2 FLAP HINGE FITTING OUTBOARD FASTENER BORES. REPAIRED PER XEA X9-9-27-9. - [SDR 9502449945](https://openairdocs.org/sdr/9502449945), Jan 11, 1995: HINGE. CORRODED. DURING PERIODIC CHECK, FOUND CORROSION IN NR 3 FLAP HINGE FASTENER BORES. REPAIRED PER XEA X9-27-12. - [SDR 9500509945](https://openairdocs.org/sdr/9500509945), Jan 9, 1995: FITTING. CRACKED. DURING PERIODIC CHECK, FOUND CRACK IN CENTER WING TANK FITTING XCW O, BETWEEN WING STRINGERS 17 - 18. REPLACED FITTING PER SRM 51-10-4. - [SDR 9500499945](https://openairdocs.org/sdr/9500499945), Jan 9, 1995: KEEL BEAM. CRACKED. DURING PERIODIC CHECK, FOUND 10 INCH CRACK AND CORROSION IN RIGHT SIDE KEEL BEAM FS 604 - 637 BETWEEN LONGERON 28R - 29R. REPLACED BEAM PER SRM 51-30-2. - [SDR 9500479945](https://openairdocs.org/sdr/9500479945), Jan 7, 1995: SPAR CHORD. CRACKED. DURING PERIODIC CHECK, FOUND CRACKS IN THE HORIZONTAL STABILIZER AFT SPAR 'T' CAPS LEFT SIDE LOWER (XHS 205-211) AND RIGHT SIDE UPPER (XHS 188). REPAIRED BOTH P - [SDR 9500469945](https://openairdocs.org/sdr/9500469945), Jan 7, 1995: FITTING. CRACKED. DURING PERIODIC CHECK, FOUND CRACKS IN ATTACH FITTINGS FS 996 AT LONGERONS 27R, 24L, AND AT INTERCOSTAL BETWEEN LONGERON 27L AND 28L. REPLACED ALL FITTINGS PER ## 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 NYC70IN101](https://openairdocs.org/ntsb/NYC70IN101), Mar 17, 1970: Douglas DC-9 (N8925E), Boston, MA, incident, no damage, 1 fatal ## 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 19951120042289I](https://openairdocs.org/incident/19951120042289I), Nov 20, 1995: Doug DC931 (N8925E), Rochester, NY. Narrative: nwaa flight 1209 departed roc at 7:00 a.m. enroute for detroit. 15 minutes in flight, crew experienced smoke in cockpit. Aircraft returned to roc… - [Incident 19780808049539I](https://openairdocs.org/incident/19780808049539I), Aug 8, 1978: Doug DC931 (N8925E), Boston, MA. Flight returned after loss of oil found oil cap seal blown. --- 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.