# N739DH: 1995 Boeing 767-324, registration cancelled 2022-06-09 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 9, 2022 - Exported to: United Kingdom - Status when cancelled: Valid registration - Airframe: [Boeing 767-324](https://openairdocs.org/model/boeing-767-324) (registry code 1385203) - Engine: [GE CF6-80C2B7F](https://openairdocs.org/engine/ge-cf6-80c2b7f) (registry code 30114) - Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM), [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (OpenAirDocs) - Serial number: 27392 - Year built: 1995 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: April 27, 2019 - Certificate issued: July 5, 2018 - Last registry action: May 7, 2021 - Mode S code: A9ECCD - Owner when cancelled: [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N739DH - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=739DH - Page: https://openairdocs.org/deregistered/N739DH-2022-06-09 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 Boeing 767-324: https://openairdocs.org/model/boeing-767-324.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 KCSA202206021070](https://openairdocs.org/sdr/KCSA202206021070), Jun 2, 2022: ATTACH ANGLE. CRACKED. LEFT WING INTERNAL TANK RIB 28 AFT SPAR ATTACH ANGLE AT WS 905.2 CRACKED AT LOWEST FASTENER NO. 19 - [SDR KCSA202205191066](https://openairdocs.org/sdr/KCSA202205191066), May 19, 2022: SEAT TRACK. CRACKED. CAPTIAN'S SEAT AFT OUTBOARD SEAT TRACK CRACKED - [SDR KCSA202205191065](https://openairdocs.org/sdr/KCSA202205191065), May 19, 2022: SEAT TRACK. CRACKED. CAPTAIN'S SEAT FWD INBD SEAT TRACK CRACKED - [SDR KCSA202205191064](https://openairdocs.org/sdr/KCSA202205191064), May 19, 2022: STIFFENER. CORRODED. CORROSION ON AFT L-ANGLE UPPER SURFACE INSIDE WING CENTER SECTION FORWARD ACCESS HOLE - [SDR KCSA2022042308](https://openairdocs.org/sdr/KCSA2022042308), Apr 23, 2022: ENGINE. STALLED. RIGHT ENGINE COMPRESSOR STALL, FOLLOWED BY EXHAUST GAS TEMPERATURE INCREASE, RIGHT ENGINE UNRESPONSIVE. RIGHT ENGINE LEFT AT IDLE FOR REMAINDER OF FLIGHT, EMERG - [SDR KCSA2022041505](https://openairdocs.org/sdr/KCSA2022041505), Apr 15, 2022: NONE. NONE. DECLARED EMERGENCY FOR LEFT ENGINE FUEL FILTER ENGINE INDICATING AND CREW ALERTING SYSTEM MESSAGE - [SDR KCSA202007201710](https://openairdocs.org/sdr/KCSA202007201710), Jul 17, 2020: ENGINE. VIBRATION. DURING TAKEOFF AS NOSE GEAR LIFTED OFF SIGNIFICANT NOSE GEAR VIBRATION FELT. REMOVED NOSE WHEEL ASSYS IAW B767-300 AMM 32-45-02. PERFORMED WHEEL EXAMINATION IAW - [SDR KCSA20200619806](https://openairdocs.org/sdr/KCSA20200619806), Jun 18, 2020: CONNECTOR. DIRTY. MASTER MESSAGE: CABIN ALTITUDE MASTER CAUTION MESSAGE: CABIN AUTO INOP STATUS MESSAGE: CABIN ALT AUTO 1 + 2. PERFORMED BITE TEST ON CABIN ALT AUTO 1 IAW FIM 21- - [SDR KCSA20200609702](https://openairdocs.org/sdr/KCSA20200609702), Jun 7, 2020: EADI. FAILED. CA ADI TURNED BRIGHT, THEN FUZZY, THEN OFF. ACRID BURNING WIRE SMELL ASSOCIATED. REMOVED AND REPLACED CAPT EADI IN ACCORDANCE WITH B767-300 AMM 34-22-03. ALL CH - [SDR KCSA2020060952603](https://openairdocs.org/sdr/KCSA2020060952603), May 26, 2020: EADI. FAILED. ADI INOP LIGHT SMOKE AND FUMES OBSERVED. REMOVED AND REPLACED CAPTAINS EADI IAW B767 AMM 34-22-03 OPS CHECK GOOD. PERFORMED AIRCRAFT SYSTEM OIL SMOKE/FUME CONTA - [SDR KCSA20191011002](https://openairdocs.org/sdr/KCSA20191011002), Oct 1, 2019: EADI. FAILED. CAPTAIN ATTITUDE DIRECTIONAL INDICATOR WENT BLANK ON THE ARRIVAL WITH THE SMELL OF ELECTRICAL SMOKE AND A POPPING SOUND. LEFT ATTITUDE DIRECTIONAL INDICATOR CIR - [SDR KCSA2019101192611](https://openairdocs.org/sdr/KCSA2019101192611), Sep 26, 2019: SYMBOL GENERATOR. FAILED. CAPTAINS SIDE EXPERIENCED ELECTRICAL BURNING SMELL AFTER ELECTRONIC FLIGHT INSTRUMENT SWITCH WAS SELECTED DUE TO POSSIBLE SYMBOL GENERATOR FAILURE. REMOVED AND - [SDR KCSA201908012408](https://openairdocs.org/sdr/KCSA201908012408), Jul 24, 2019: CIRCUIT BREAKER. FAILED. DECLARED EMERGENCY DURING LANDING, DUE TO LOSS OF LEFT AC BUSS INFLIGHT. REMOVED AND REPLACED LEFT BUSS TIE CIRCUIT BREAKER. - [SDR KCSA2019072408](https://openairdocs.org/sdr/KCSA2019072408), Jul 24, 2019: CONTROL VALVE. MALFUNCTIONED. AT 1800 FT ON FINAL APPROACH INTO CVG, WHEN SELECTING FLAPS 30, THE LEFT AL BUS FAILED. REMOVED AND REPLACED APU SURGE CONTROL VALVE IAW AMM 49-53-01 ALL CHECKS - [SDR KCSA201903291065](https://openairdocs.org/sdr/KCSA201903291065), Mar 29, 2019: SUPPORT. CRACKED. FWD PIT PALLET SUPPORT HAS AREAS OF CORROSION AND POSSIBLE CRACK STA 538 - 595 RBL 38 APPROX. - [SDR KCSA201902141035](https://openairdocs.org/sdr/KCSA201902141035), Feb 14, 2019: STRINGER CLIP. CORRODED. RT MAIN DECK INTERIOR GROUNDING STUD STATION 1285, STRINGER APPROX 12 IS CORRODED (NOTE: CORROSION FOUND TO BE ON STRINGER CLIP) - [SDR KCSA201902131034](https://openairdocs.org/sdr/KCSA201902131034), Feb 13, 2019: FLOOR SUPPORT. CORRODED. FWD PIT AT STA 485 RBL APPROX 24" FLOOR SUPPORT HAS EVIDENCE OF CORROSION ON TOP SURFACE. - [SDR KCSA201902131033](https://openairdocs.org/sdr/KCSA201902131033), Feb 13, 2019: SUPPORT BEAM. CORRODED. RIGHT I/B FLAP, O/B SUPPORT BEAM AFT I/B BOLT HOLE PITTED. - [SDR KCSA201902131032](https://openairdocs.org/sdr/KCSA201902131032), Feb 13, 2019: SUPPORT BEAM. CORRODED. RIGHT INBOARD FLAP, OUTBOARD SUPPORT BEAM, AFT OUTBOARD BOLT HOLE IS PITTED. - [SDR KCSA201902131031](https://openairdocs.org/sdr/KCSA201902131031), Feb 13, 2019: FILL PORT. CORRODED. L/W OVERWING FILLPORT HAS EVIDENCE OF CORROSION. - [SDR KCSA201902051028](https://openairdocs.org/sdr/KCSA201902051028), Feb 5, 2019: SHEAR TIE. CORRODED. FWD PIT AT STA 610 LBL APPROX 1" SHEAR TIE HAS EVIDENCE OF CORROSION. - [SDR KCSA201902051027](https://openairdocs.org/sdr/KCSA201902051027), Feb 5, 2019: STRUCTURE. CORRODED. FWD PIT AT STA 654 LBL APPROX 48" TOP OF CHORD & UNDERNEATH FLANGE AROUND NUT PLATE HAS EVIDENCE OF CORROSION. - [SDR KCSA201902051026](https://openairdocs.org/sdr/KCSA201902051026), Feb 5, 2019: TORQUE BOX. CORRODED. FORWARD CARGO COMPARTMENT RIGHT HAND TORQUE BOX WEB HAS EVIDENCE OF CORROSION FS 478 TO 495 RBL 40 TO 65. - [SDR KCSA201902041025](https://openairdocs.org/sdr/KCSA201902041025), Feb 4, 2019: HINGE FITTING. CRACKED. RIGHT INBOARD MAIN FLAP INBOARD HINGE FITTING, OUTBOARD TAB IS CRACKED. - [SDR KCSA201902041024](https://openairdocs.org/sdr/KCSA201902041024), Feb 4, 2019: SKIN PANEL. CORRODED. LEFT INBOARD MAIN FLAP PANEL 555 EB IS CORRODED ON THE AFT EDGE NEAR THE OUTBOARD FITTING. - [SDR KCSA201902041023](https://openairdocs.org/sdr/KCSA201902041023), Feb 4, 2019: BULKHEAD WEB. CORRODED. NR 2 PYLON FWD TORQUE BOX WEB CUTOUT FOR HYDRAULIC LINE HAS CORROSION ON AFT SIDE OF HOLE. - [SDR KCSA201902041022](https://openairdocs.org/sdr/KCSA201902041022), Feb 4, 2019: SEAT TRACK. CRACKED. PILOTS O/B FWD SEAT TRACK HAS EVIDENCE OF CORROSION ON AFT END OF TRACK. UPON FURTHER INVESTIGATION FOUND TRACK CRACKED, NO CORROSION NOTED. - [SDR KCSA201901161010](https://openairdocs.org/sdr/KCSA201901161010), Jan 16, 2019: STRINGER CLIP. CORRODED. CORRODED STRINGER CLIP IN MAIN CARGO COMPARTMENT LT SIDE @ APPROX STA 1153, S12 L. - [SDR KCSA201901161009](https://openairdocs.org/sdr/KCSA201901161009), Jan 16, 2019: STRINGER CLIP. CORRODED. EVIDENCE OF CORROSION ON STRINGER CLIP IN MAIN CARGO COMPARTMENT LT SIDE @ APPROX STA 1219 S19 L. - [SDR KCSA201901161008](https://openairdocs.org/sdr/KCSA201901161008), Jan 16, 2019: STRINGER CLIP. CORRODED. EVIDENCE OF CORROSION ON STRINGER CLIP IN MAIN CARGO COMPARTMENT LT SIDE @ APPROX STA 1241 S18 L. - [SDR KCSA201901161007](https://openairdocs.org/sdr/KCSA201901161007), Jan 16, 2019: STRUCTURE. CORRODED. EVIDENCE OF CORROSION ON LT OVERWING EMERGENCY EXIT CUTOUT @ APPROX STA 933 S17 L. - [SDR KCSA201901161006](https://openairdocs.org/sdr/KCSA201901161006), Jan 16, 2019: FITTING. CORRODED. RT MAIN DECK STATION 1153, STRINGER 10, HAS STRINGER TO FRAME CLIP WITH CORROSION. - [SDR KCSA201901161005](https://openairdocs.org/sdr/KCSA201901161005), Jan 16, 2019: FITTING. CORRODED. RT MAIN DECK STRINGER TO FRAME CLIP HAS AREA OF CORROSION AT STRINGER 11 AND STATION 1197 + 22. - [SDR KCSA201901161004](https://openairdocs.org/sdr/KCSA201901161004), Jan 16, 2019: SKIN. CRACKED. RT WING LWR SKIN AT STA 995 STR R 9.5 HAS 2 CRACKS COMING FROM FASTENERS. END OF CRACKS MARKED. - [SDR KCSA201901161003](https://openairdocs.org/sdr/KCSA201901161003), Jan 16, 2019: SKIN. CORRODED. RIGHT WING INBD FLAP AT INBD HINGE ON AFT SPAR OF FLAP ON LOWER SURFACE, APPROX. 66 INCHES - 78 INCHES OUTBD OF FLAP INBD END, (W. BL 164 - 176) SKIN IS BULGED - [SDR KCSA201901161002](https://openairdocs.org/sdr/KCSA201901161002), Jan 16, 2019: WEB. CRACKED. LT L/E CAVITY WEB CRACKED ON AFT SIDE NEAR WS 668.2. ## Other aircraft with N739DH - [Cancelled 1979-07-03](https://openairdocs.org/deregistered/N739DH-1979-07-03): Cessna 172N, S/N 17270457. Exported to Canada. Owner: [Dunn Richard L](https://openairdocs.org/faa-owner/DUNN%20RICHARD%20L), [Lima, OH](https://openairdocs.org/faa-place/OH/Lima) --- 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.