# N625US: 1979 Boeing 747-251B, registration cancelled 2007-09-27 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 27, 2007 - Status when cancelled: Valid registration - Airframe: [Boeing 747-251B](https://openairdocs.org/model/boeing-747-251b) (registry code 1384892) - Engine: [Pratt & Whitney JT9D-3A](https://openairdocs.org/engine/pratt-whitney-jt9d-3a) (registry code 52050) - Data sheets: [TCDS A20WE](https://openairdocs.org/tcds/A20WE), [TCDS E20EA](https://openairdocs.org/tcds/E20EA) (OpenAirDocs) - Serial number: 21707 - Year built: 1979 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 16, 1979 - Certificate issued: August 31, 2007 - Last registry action: August 31, 2007 - Mode S code: A82AA3 - Owner when cancelled: [Evergreen Aircraft Sales & Leasing Co](https://openairdocs.org/faa-owner/EVERGREEN%20AIRCRAFT%20SALES%20%26%20LEASING%20CO) - Location: [Mcminnville, OR](https://openairdocs.org/faa-place/OR/Mcminnville) - Owner type: Corporation - 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/N625US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=625US - Page: https://openairdocs.org/deregistered/N625US-2007-09-27 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 Boeing 747-251B: https://openairdocs.org/model/boeing-747-251b.md ## Service difficulty reports (37) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 0301786625](https://openairdocs.org/sdr/0301786625), Sep 24, 2003: POWER SUPPLY. INOPERATIVE. DURING LINE CHECK, FOUND ZONE-E FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD. - [SDR 0101696625](https://openairdocs.org/sdr/0101696625), May 5, 2001: UNKNOWN. ODOR. DURING CRUISE, A SMOKE ODOR WAS NOTICED AROUND DOOR 5L. THE ODOR DISSIPATED AFTER A FEW MINUTES AND THE AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INC - [SDR 0101676625](https://openairdocs.org/sdr/0101676625), May 5, 2001: WIRE. SHORTED. DURING FLIGHT, THE NR 2 HOT PLATE SPARKED AND EMITTED SMOKE RESULTING IN TRIPPING OF THE CIRCUIT BREAKER. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT I - [SDR 0100226625](https://openairdocs.org/sdr/0100226625), Jan 18, 2001: CONTROLLER. FAILED. DURING CLIMB AT 24,000 FEET, THE PRESSURIZATION AUTO FAIL LIGHT ILLUMINATED ACCOMPANIED WITH THE NR 2 PACK TRIPPING AND THE PRESSURE RELIEF LIGHT ILLUMINATING. - [SDR 0004656625](https://openairdocs.org/sdr/0004656625), Dec 28, 2000: DURING CRUISE, NOTICED FAINT BURNING SMELL. SHUYT DOWN WEATHER RADAR AND SMELL DISAPPEARED. MAINTENANCE FOUND ELECTRICAL CONNECTOR DIRTY. CLEANED CONNECTORS AND - [SDR 0002966625](https://openairdocs.org/sdr/0002966625), Aug 15, 2000: ACM. FAILED. DURING APPROACH, A SMOKE SMELL WAS NOTICED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE NR 1 AIR CYCLE MACHINE. OPERATIONAL CHEC - [SDR 0002976625](https://openairdocs.org/sdr/0002976625), Aug 13, 2000: ACM. FAILED. DURING APPROACH, AN ELECTRICAL SMOKE SMELL WAS NOTICED IN THE CABIN COMPARTMENT. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE NR 3 - [SDR 0002156625](https://openairdocs.org/sdr/0002156625), Jun 11, 2000: CIRCUIT BOARD. DEFECTIVE. DURING FLIGHT, THE NR 4 ENGINE NACELLE TEMPERATURE INDICATED ''A'' FLUCTUATED INTO RED WITH ASSOCIATED FAULT LIGHT AND FIRE DETECTOR LIGHT ILLUMINATING ON ANNUN - [SDR 0002046625](https://openairdocs.org/sdr/0002046625), May 24, 2000: FRAME. CRACKED. DURING M-CHECK, FOUND CRACK ON FRAME, LOCATED AT BS 500, STRINGER 11R. REPAIRED PER EA 66-176689. - [SDR 0002026625](https://openairdocs.org/sdr/0002026625), May 24, 2000: SHEAR TIE. CRACKED. DURING M-CHECK, FOUND CRACK ON FRAME SHEAR TIE, LOCATED AT BS 520, STRINGER 11R. REPAIRED PER EA 66-176687 REV A. - [SDR 0002266625](https://openairdocs.org/sdr/0002266625), May 22, 2000: ANGLE. CORRODED. DURING -M- INSPECTION, FOUND CORROSION ON CABIN FLOOR RT SIDEWALL FLANGE. REPAIRED PER EA 66-176776. - [SDR 0001976625](https://openairdocs.org/sdr/0001976625), May 22, 2000: FRAME. CRACKED. DURING M-CHECK, FOUND CRACK ON FRAME WEB LOCATED AT STATION 1265. REPAIRED PER EA66-175568. - [SDR 0002006625](https://openairdocs.org/sdr/0002006625), May 19, 2000: FRAME. CRACKED. DURING M-CHECK, FOUND CRACKED FRAME WEB AT STRINGER CUTOUT UPPER INBOARD CORNER AT BS 360, STRINGER 10L. REPAIRED PER EA66-176684. - [SDR 0001996625](https://openairdocs.org/sdr/0001996625), May 19, 2000: FRAME. CRACKED. DURING M-CHECK, FOUND CRACK ON FRAME WEB AT STRINGER CUTOUT UPPER INBOARD CORNER, AT BS 380, STRINGER 10R. REPAIRED PER EA 66-176683 REV A. - [SDR 0002036625](https://openairdocs.org/sdr/0002036625), May 18, 2000: FRAME. CRACKED. DURING M-CHECK, FOUND CRACK ON FRAME, LOCATED AT BS 420, STRINGER 14R. REPAIRED PER EA66-176688. - [SDR 0002016625](https://openairdocs.org/sdr/0002016625), May 18, 2000: FRAME. CRACKED. DURING M-CHECK, FOUND CRACK ON INBOARD EDGE OF FRAME WEB, LOCATED AT STATION 360, STRINGER 2R. REPAIRED PER EA 66-176686 REV A. - [SDR 0001986625](https://openairdocs.org/sdr/0001986625), May 18, 2000: FRAME. CRACKED. DURING M-CHECK, FOUND CRACK AT CANTED BULKHEAD FRAME LOCATED AT STATION 260, STRINGER 32L. REPAIRED PER EA66-176190. - [SDR 0002056625](https://openairdocs.org/sdr/0002056625), May 13, 2000: FRAME. CRACKED. DURING M-CHECK, FOUND CRACK ON FRAME, LOCATED AT BS 460, STRINGER 11 TO 12R. REPAIRED PER EA 66-176727. - [SDR 9902096625](https://openairdocs.org/sdr/9902096625), Jun 16, 1999: ACTUATOR. FAILED. DURING APPROACH, THE NOSE LANDING GEAR WOULD NOT EXTEND. RECYCLED THE LANDING GEAR AND GEAR EXTENDED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE NOSE LANDIN - [SDR 9900466625](https://openairdocs.org/sdr/9900466625), Feb 9, 1999: ACTUATOR. LEAKING. DURING CRUISE (TPE), NR 1 HYDRAULIC SYSTEM QUANTITY WENT TO ZERO. TURNED NR 1 HYDRAULIC PUMP OFF AND AIRCRAFT CONTINUED TO NRT AND LANDED WITHOUT INCIDENT. AIRC - [SDR 9811166625](https://openairdocs.org/sdr/9811166625), Sep 26, 1998: BATTERY. DISCHARGED. DURING LINE CHECK, FOUND B ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY, OPERATIONAL CHECK GOOD. - [SDR 9723526625](https://openairdocs.org/sdr/9723526625), Nov 25, 1997: SPAR WEB. CORRODED. DURING PERIODIC CHECK, FOUND CORROSION ON THE LEFT WING FORWARD SPAR WEB (P/N 65B225851-2) BETWEEN FSS 950-980. REPAIRED PER EA 66-152345. - [SDR 9722826625](https://openairdocs.org/sdr/9722826625), Nov 25, 1997: SPAR WEB. CORRODED. DURING PERIODIC CHECK, FOUND CORROSION ON LEFT WING FORWARD SPAR WEB BETWEEN FSSI 1050 TO 1078. REPAIRED PER EA 66-153654. - [SDR 9721396625](https://openairdocs.org/sdr/9721396625), Nov 13, 1997: POWER SUPPLY. INOPERATIVE. DURING LINE CHECK, FOUND 7 EMERGENCY EXIT SIGNS THROUGHOUT THE AIRCRAFT THAT FAILED THE 10 MINUTE CAPACITY CHECK. REPLACED THE POWER SUPPLIES, OPERATIONAL CHECK - [SDR 9721426625](https://openairdocs.org/sdr/9721426625), Nov 11, 1997: PRESS DECK. CORRODED. DURING PERIODIC CHECK, FOUND CORROSION ON CEILING PRESSURE DECK I BEAM IN THE RIGHT WHEEL WELL FS 1265, RBL 105 TO 117. REPAIRED PER EA 66-152533. - [SDR 9716656625](https://openairdocs.org/sdr/9716656625), Sep 2, 1997: PUMP. LEAKING. DURING CRUISE, THE NR 4 HYDRAULIC SYSTEM INDICATED A LOSS OF FLUID AND PRESSURE. AIRCRAFT DIVERTED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE NR 4 ENGINE - [SDR 9701866625](https://openairdocs.org/sdr/9701866625), Jan 27, 1997: ENGINE. BIRD STRIKE. DURING CLIMB AFTER DEPARTURE, CREW REPORTED POSSIBLE BIRD STRIKE ON RIGHT WING. DURING CRUISE FLIGHT, NR 3 ENGINE HAD A LOW FREQUENCY VIBRATION AT LOWER POWER S - [SDR 9701406625](https://openairdocs.org/sdr/9701406625), Jan 18, 1997: AURAL WARN. MALFUNCTIONED. DURING TAKEOFF, THE AURAL WARNING HORN SOUNDED. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE COULD NOT DUPLICATE FAULT, OPERATIONAL CHECK OF A - [SDR 9700826625](https://openairdocs.org/sdr/9700826625), Jan 3, 1997: SEAT TRACK. CORRODED. DURING PERIODIC CHECK, FOUND CORROSION ON SEAT TRACK FLANGE. REPAIRED PER EA 66-121308. - [SDR 9623076635](https://openairdocs.org/sdr/9623076635), Oct 26, 1996: COMPRESSOR. STALLED. DURING TAKEOFF ROTATION, THE NR 3 ENGINE EXPERIENCED TWO COMPRESSOR STALLS. AT THE TIME OF STALL, EGT ROSE TO 850 DEGREES CELSIUS FOR APPROXIMATELY FIVE MINUTES - [SDR 9618976625](https://openairdocs.org/sdr/9618976625), Aug 30, 1996: CONTROL HANDLE. LACK OF LUBE. DURING APPROACH THE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR EXTENSION. RECYCLED LANDING GEAR AND LIGHT EXTINGUISHED. AIRCRAFT LANDED W - [SDR 9601056625](https://openairdocs.org/sdr/9601056625), Jan 17, 1996: PACK. MALFUNCTIONED. AFTER TAKEOFF AND SUBSEQUENTLY TURNING OFF PACKS, SMOKE FILLED THE ENTIRE AIRCRAFT. WITH ALL PACKS SHOWING NORMAL OPERATING TEMPERATURE, THE SMOKE DISSIPATED WI - [SDR 9600436625](https://openairdocs.org/sdr/9600436625), Jan 10, 1996: POWER SUPPLY. INOPERATIVE. DURING LINE CHECK, FOUND THE STATE ROOM EMERGENCY TRACK LIGHT INOPERATIVE. REPLACED THE POWER SUPPLY AND BATTERY PACK AND FUNCTIONAL CHECK WAS NORMAL. - [SDR 9508226625](https://openairdocs.org/sdr/9508226625), May 20, 1995: RETRACT MECH. REQD SERVICE. DURING CLIMB, THE RIGHT BODY GEAR TILT LIGHT ILLUMINATED AND GEAR WOULD NOT RETRACT IN BOTH PRIMARY AND ALTERNATE. CREW FOLLOWED COCKPIT OPERATING MANUAL AND PR - [SDR 9508216625](https://openairdocs.org/sdr/9508216625), May 20, 1995: LINE. CHAFED. DURING CLIMB, THE RIGHT BODY GEAR TILT LIGHT ILLUMINATED AND BOTH PRIMARY AND ALTERNATE GEAR WOULD NOT RETRACT. CREW FOLLOWED COCKPIT OPERATING MANUAL PROCEDURE - [SDR 9506156625](https://openairdocs.org/sdr/9506156625), Apr 18, 1995: BLEED VALVE. MALFUNCTIONED. DURING TAKEOFF, THE NR 4 ENGINE EXPERIENCED EGT RISE AND POWER WAS REDUCED TO KEEP WITHIN LIMITS. DURING CLIMB THE FAULT LIGHT CAME ON INDICATING IN THE 8 TO 10 - [SDR 9505466625](https://openairdocs.org/sdr/9505466625), Apr 9, 1995: CONTROL CABLE. DISCONNECTED. DURING TAKEOFF ROLL, THE NR 4 ENGINE WOULD NOT RESPOND TO POWER LEVER MOVEMENT AND THE TAKEOFF WAS ABORTED. THE CONTROL CABLE IN THE PYLON WAS FOUND TO HAVE DIS ## 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 19930728030819I](https://openairdocs.org/incident/19930728030819I), Jul 28, 1993: Boeing 747251B (N625US), Honolulu, HI, Minor damage. NR3 engine lost power on climb. Shut engine down. Dumped fuel. Returned. Found 6th stage turbine blades damaged. - [Incident 19920516021029I](https://openairdocs.org/incident/19920516021029I), May 16, 1992: Boeing 747251B (N625US), Seattle, WA, Minor damage. Right overwing escape slide deployed and separated on approach. Slide improperly secured. - [Incident 19880525039249I](https://openairdocs.org/incident/19880525039249I), May 25, 1988: Boeing 747251B (N625US), Chicago, IL. Passenger attacked flight attendant en route. Passenger restrained and monitored until removed by police at ord. ## Other aircraft with N625US - [Cancelled 2019-03-13](https://openairdocs.org/deregistered/N625US-2019-03-13): DJI PHANTOM 3 ADVANCED, S/N P76DCD23012004. Registration expired, pending cancellation. Owner: [Airleaf LLC](https://openairdocs.org/faa-owner/AIRLEAF%20LLC), [Encinitas, CA](https://openairdocs.org/faa-place/CA/Encinitas) --- 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.