# N835EX: 1991 Boeing DHC-8-102, registration cancelled 2007-05-30 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 30, 2007 - Exported to: Canada - Status when cancelled: Triennial form not returned - Airframe: [Boeing DHC-8-102](https://openairdocs.org/model/boeing-dhc-8-102) (registry code 1386002) - Engine: [Pratt & Whitney Canada PW120](https://openairdocs.org/engine/pratt-whitney-canada-pw120) (registry code 52114) - Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs) - Serial number: 289 - Year built: 1991 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: October 21, 1991 - Certificate issued: January 29, 2001 - Last registry action: November 15, 2005 - Mode S code: AB6B67 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%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/N835EX - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=835EX - Page: https://openairdocs.org/deregistered/N835EX-2007-05-30 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 DHC-8-102: https://openairdocs.org/model/boeing-dhc-8-102.md ## Service difficulty reports (21) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR HNAA0400109](https://openairdocs.org/sdr/HNAA0400109), Aug 10, 2004: WIRE HARNESS. CHAFED. FLIGHT NR 3822 HAD TO RETURN TO FIELD DUE TO THE RT PROP RPM SURGING ON CLIMB OUT. AIRCRAFT LANDED WITHOUT INCIDENT. CONDITION DID NOT EXIST WITH THE PROP SYNCH - [SDR HNAA0408106](https://openairdocs.org/sdr/HNAA0408106), Aug 1, 2004: SOCKET. BURNED. FLIGHT 3980 REPORTED A HOT ELECTRICAL SMELL IN THE CABIN WITH OVERHEAD LIGHTS ON. MAINTENANCE FOUND THE OVERHEAD LIGHT SOCKET BAD. THEN REMOVED AFFECTED BULB AN - [SDR HNAA0408107](https://openairdocs.org/sdr/HNAA0408107), Jul 31, 2004: POWER SUPPLY. INOPERATIVE. FLIGHT REPORTED THE EMERGENCY EXIT LIGHT OVER THE CABIN DOOR AS BEING INOPERATIVE. MAINTENANCE TROUBLESHOT SYSTEM AND REMOVED AND REPLACED THE BATTERY POWER SUP - [SDR PCAA0404192](https://openairdocs.org/sdr/PCAA0404192), Apr 17, 2004: HANDLE. BENT. REPORTED THAT THE OUTSIDE AIRSTAIR DOOR HANDLE WAS BENT AND WOULD NOT ALLOW THE DOOR TO BE CLOSED. MAINTENANCE REOMVED AND REPLACED THE HANDLE AS REQUIRED AND T - [SDR PCAA0402172](https://openairdocs.org/sdr/PCAA0402172), Feb 21, 2004: SMOKE DETECTOR. FAULTY. FLIGHT 3982 CREW REPORTED THAT THE NR 2 BAGGAGE BAY SMOKE DETECTOR WOULD NOT TEST. ITEM WAS DEFERRED AFTER VERIFICATION THAT THE NR 1 WAS IN OPERATING ORDER. ON - [SDR PCAA0303056](https://openairdocs.org/sdr/PCAA0303056), Mar 16, 2003: BRAKE. FAILED. PHL-FLIGHT 3503 CREW REPORTED NORMAL BRAKES FAILED WHEN TAXIING IN WITH ONLY NR 2 ENGINE OPERATING AND STANDBY PUMPS ON. MAINTENANCE BLED ALL BRAKES, TAXIED AIR - [SDR PCAA0301011](https://openairdocs.org/sdr/PCAA0301011), Jan 7, 2003: WIRE. DAMAGED. DURING ROUTINE MAINTENANCE VISIT 6TH RED FLOOR LEVEL EMERGENCY LIGHT FOUND INOPERATIVE. LEAD WIRE REPAIRED AT ATTACH POINT TO BULB. OPERATIONAL CHECK GOOD. AIRC - [SDR PCAA0212145](https://openairdocs.org/sdr/PCAA0212145), Dec 31, 2002: WINDSHIELD. CRACKED. FLIGHT#3636 BTV-LGA. WHILE IN CRUISE FLIGHT FIRST OFFICERS WINDSHIELD BEGAN TO CRACK IN SEVERAL PLACES AND SPARK DUE TO WINDSHIELD HEAT BEING TURNED ON. WINDSHI - [SDR PCAA0208091](https://openairdocs.org/sdr/PCAA0208091), Aug 9, 2002: WIRE. CRUSHED. DURING ROUTINE MAINTENANCE VISIT FIRST FLOOR LEVEL EMERGENCY LIGHT FOUND INOPERATIVE. CRUSHED WIRE FOUND AND REPAIRED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED - [SDR PCAA0208085](https://openairdocs.org/sdr/PCAA0208085), Aug 2, 2002: ACTUATOR. CRACKED. PHL-FLIGHT#3686. CREW REPORTED LOSS OF #1 HYDRAULIC SYSTEM FLUID JUST AFTER TAKEOFF.EMERGENCY DECLARD, AND AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED AIR - [SDR PCAA0207074](https://openairdocs.org/sdr/PCAA0207074), Jul 14, 2002: CONNECTOR. LOOSE. PHL- FLIGHT 3643. CREW REPORTED FORWARD SEGMENT OF FLOOR EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE RESECURED FORWARD SEGMENT OF EMERGENCY LIGHT PLUGS. AIRCRAF - [SDR PCAA0201015](https://openairdocs.org/sdr/PCAA0201015), Jan 16, 2002: POWER SUPPLY. INOPERATIVE. DURING ROUTINE MAINTENANCE VISIT RIGHT AFT EMERGENCY LIGHTS FOUND TO BE INOPERATIVE. POWERSUPPLY BOX AT POSITION #400 AND 2 BATTERIES WERE REPLACED, POSITION #4 - [SDR PCAA0201010](https://openairdocs.org/sdr/PCAA0201010), Jan 9, 2002: WIRE. BROKEN. DURING ROUTINE MAINTENANCE VISIT THE FURTHEST AFT EMERGENCY FLOOR LIGHT WAS FOUND INOPERATIVE. TWO BROKEN WIRES FOUND AND INSULATION PULLED AWAY FROM LIGHT SOCK - [SDR PCAA0111157](https://openairdocs.org/sdr/PCAA0111157), Oct 16, 2001: LINK. WORN. DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, FOUND PISTON CAP PIN GOUGED BEYOND LIMITS, TRAILING ARM WORN, AND TRAILING ARM ASSE - [SDR PCAA0101002](https://openairdocs.org/sdr/PCAA0101002), Jan 9, 2001: BULB. FAILED. BGM FLIGHT 3555. ROW 1 RIGHT SIDE EMERGENCY LIGHT INOP ONE BULB. MAINTENANCE REPAIRED WIRING ON FLOOR EMERGENCY LIGHTS. AIRCRAFT RETURNED TO SERVICE. - [SDR PCAA0011073](https://openairdocs.org/sdr/PCAA0011073), Nov 15, 2000: SKIN. CRACKED. BGM- DURING ROUTINE MAINTENANCE INSPECTION STARBOARD SIDE OF FORE RUDDER FOUND TO HAVE A 10 INCH C-SHAPE CRACK. FORE RUDDER ASSEMBLY REPLACED IN ACCORDANCE WITH - [SDR PCAA0002012](https://openairdocs.org/sdr/PCAA0002012), Feb 2, 2000: WINDSHIELD. CRACKED. EN ROUTE TO ABE, THE CAPTAINS WINDSHIELD CRACKED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW DHC PROCEDURES. - [SDR PCAA9800765](https://openairdocs.org/sdr/PCAA9800765), Mar 23, 1998: WINDOW. CRACKED. DURING CRUISE FLIGHT OUT OF SYR, THE CAPTAINS SIDE WINDOW CRACKED. AIRCRAFT RETURNED TO SYR AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE SI - [SDR PCAA9800718](https://openairdocs.org/sdr/PCAA9800718), Feb 8, 1998: WIRE. BROKEN. TWO LIGHTS INOPERATIVE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM. REPAIRED BROKEN WIRE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM. REPAIRED BROKEN WIRE IN - [SDR PCAA9700569](https://openairdocs.org/sdr/PCAA9700569), Oct 6, 1997: STRUT. FAILED. LEFT ENGINE OUTBOARD AFT VERTICLE MOUNT STRUT CRACKED COMPLETELY THROUGH ENTIRE STRUT. REMOVED AND REPLACED LEFT ENGINE AFT OUTBOARD VERTICLE MOUNT STRUT WITH S - [SDR PCAA9700362](https://openairdocs.org/sdr/PCAA9700362), Apr 6, 1997: O-RING. FAILED. PHL - DURING CLIMB-OUT, NR 2 ENGINE OIL PRESURE DROPPED TO 40 PSI. THE ENGINE WAS SHUT DOWN AND ACFT LANDED IN ABE WITHOUT INCIDENT. MAINTENANCE INSPECTED ENGIN ## FAA accident and incident reports (1) 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 19980323017219I](https://openairdocs.org/incident/19980323017219I), Mar 23, 1998: Dhav DHC8102 (N835EX), Syracuse, NY, Minor damage. Captains side window outer pane cracked during flight. Returned to syr and landed without further incident. --- 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.