# N831EX: Boeing DHC-8-102, registration cancelled 2004-06-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 2, 2004
- Exported to: Canada
- Status when cancelled: Valid registration
- 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: 160
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: July 11, 1989
- Certificate issued: November 18, 2003
- Last registry action: November 18, 2003
- Mode S code: AB5C8B
- 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/N831EX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=831EX
- Page: https://openairdocs.org/deregistered/N831EX-2004-06-02

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 (28)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR PCAA0401155](https://openairdocs.org/sdr/PCAA0401155), Jan 15, 2004: DEICE SYSTEM. ARCED. FLIGHT 3841 ON CLIMBOUT FROM SYRACUSE HAD TO RETURN TO FIELD DUE TO SPARKS BEING OBSERVED COMING FROM THE NR 2 PROP. NO EMERGENCY DECLARED AND THE FLIGHT LANDED
- [SDR PCAA0309112](https://openairdocs.org/sdr/PCAA0309112), Sep 21, 2003: WIRE. BROKEN. DURING ROUTINE MAINTENANCE VISIT, AN EMERGENCY PATH LIGHT AT ROW 8 WAS FOUND TO HAVE A BROKEN WIRE. MAINTENANCE SPLICED THE WIRE USING AN ENVIROMENTAL BUTT SPLI
- [SDR PCAA0309104](https://openairdocs.org/sdr/PCAA0309104), Sep 3, 2003: WIRE. BROKEN. DURING ROUTINE MAINTENANCE VISIT, AN EMERGENCY FLOOR LIGHT WAS FOUND TO BE INOPERATIVE AT ROW 9DF. A WIRE WAS FOUND BROKEN AT THE LIGHT ASSEMBLY. A NEW FLOOR LI
- [SDR PCAA0305075](https://openairdocs.org/sdr/PCAA0305075), May 17, 2003: PRESSURE PANEL. CRACKED. SYR-LGA FLIGHT 3994. CREW REPORTED GEAR WOULD NOT RETRACT NORMALLY. LT AND RT AMBER DOOR ADVISORY LIGHTS ILLUMINATED AND RED DOOR ADVISORY LIGHT ILLUMINATED WHE
- [SDR PCAA0302043](https://openairdocs.org/sdr/PCAA0302043), Feb 19, 2003: WIRE. BROKEN. DURING ROUTINE MAINTENANCE VISIT THE LAST TWO EMERGENCY LIGHTS ON FLOOR LIGHTING STRIP WERE FOUND INOPERATIVE. A BROKEN WIRE WAS REPAIRED NEAR ROW 9 ON FLOOR TR
- [SDR PCAA0301028](https://openairdocs.org/sdr/PCAA0301028), Jan 30, 2003: BULB. BURNED OUT. DURING ROUTINE MAINTENANCE VISIT FLOOR TRACK EMERGENCY LIGHTING HAD 1 BULB INOPERATIVE AT SEAT 8DF. SOCKET FOR BULB WAS REPLACED ON FLOOR TRACK EMERGENCY LIGHT 
- [SDR PCAA0210127](https://openairdocs.org/sdr/PCAA0210127), Oct 26, 2002: POWER SUPPLY. DISCHARGED. DURING ROUTINE MAINTENANCE VISIT LEFT SIDE OF FUSELAGE AFT EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. EMERGENCY LIGHT POWER SUPPLY AND BATTERY WERE REPLACED. O
- [SDR PCAA0209102](https://openairdocs.org/sdr/PCAA0209102), Sep 8, 2002: HYDRAULIC LINE. LEAKING. ROC-LGA FLIGHT#3905. CREW REPORTED #2 HYDRAULIC ISOLATION VALVE CAUTION LIGHT ILLUMINATED IN FLIGHT DURING CLIMBOUT. AIRCRAFT DIVERTED TO SYR WITHOUT INCIDENCE.
- [SDR PCAA0205055](https://openairdocs.org/sdr/PCAA0205055), May 9, 2002: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE VISIT RIGHT FORWARD AND LEFT AFT EXTERIOR EMERGENCY EXIT LIGHTS FOUND TO BE INOPERATIVE. RIGHT FORWARD LIGHT BULB, LENS AND SOCKET WE
- [SDR PCAA0107076](https://openairdocs.org/sdr/PCAA0107076), Jul 31, 2001: NUT. BROKEN. BWI- FLIGHT 3806. CREW REPORTED NOSE LANDING GEAR SHOCK STRUT GLAND NUT TIGHTENING RING BROKEN OFF. MAINTENANCE REPLACED NOSE LANDING GEAR SHOCK STRUT GLANDNUT 
- [SDR PCAA0101001](https://openairdocs.org/sdr/PCAA0101001), Jan 1, 2001: WINDSHIELD. FAILED. LGA-ALB FLIGHT 3551. LEFT WINDSCREEN SHATTERED IN FLIGHT. AIRCRAFT LANDED IN ALB. MAINTENANCE REPLACED CAPTAINS WINDSHIELD AND 15 NUTPLATES ALONG BOTTOM OF WIND
- [SDR 99ZZZX4529](https://openairdocs.org/sdr/99ZZZX4529), Nov 1, 1999: ENGINE. MALFUNCTIONED. ENGINE REMOVED FROM AIRCRAFT DUE TO MODERATE VIBRATION AT 900 RPM.
- [SDR PCAA9900029](https://openairdocs.org/sdr/PCAA9900029), Aug 23, 1999: RETRACT MECH. MALFUNCTIONED. BOS- UPON DESCENT INTO BOS, ALL THREE GEAR DOORS REMAINED OPEN AFTER GEAR EXTENSION THEN CLOSED AFTER TOUCHDOWN. MAINTENANCE INSPECTED GEAR DOORS, NO DEFECTS NO
- [SDR PCAA9800730](https://openairdocs.org/sdr/PCAA9800730), Feb 13, 1998: BULB. FAILED. LEFT AFT EXTERIOR EMERGENCY EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED BULB AND CLEANED SOCKET. OPERATION TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (X)
- [SDR PCAA9700648](https://openairdocs.org/sdr/PCAA9700648), Dec 9, 1997: BULB. FAILED. AFT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR PCAA9700640](https://openairdocs.org/sdr/PCAA9700640), Dec 4, 1997: BULB. FAILED. EMERGENCY EXIT SIGN AT ROW FOUR HAS ONE BULB INOPERATIVE. REMOVED AND REPLACED EXIT SIGN LIGHT BULB. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR PCAA9700573](https://openairdocs.org/sdr/PCAA9700573), Oct 12, 1997: FITTING. CRACKED. NOSE LANDING GEAR RETRACTION ACTUATOR FITTING CRACKED THROUGH INBOARD ATTACH BOLT BORE. REMOVED AND REPLACED NOSE LANDING GEAR RETRACTION ACTUATOR FITTING WITH 
- [SDR PCAA9700544](https://openairdocs.org/sdr/PCAA9700544), Sep 13, 1997: WIRE. LOOSE. ON SHUTDOWN WITH EMERGENCY LIGHT SWITCH OFF EMERGENCY LIGHTS CAME ON, FLICKERED AND WENT OFF. FOUND WIRE NR 20113A22 ON RELAY K20 RECEPTICAL POS B1 TO HAVE BAD 
- [SDR PCAA9700542](https://openairdocs.org/sdr/PCAA9700542), Sep 13, 1997: LIGHT. INOPERATIVE. COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT WITH SERVICEABLE UNIT. OPERATIONAL CHECK NORMAL. AIRCR
- [SDR PCAA9700513](https://openairdocs.org/sdr/PCAA9700513), Aug 11, 1997: HOSE. FAILED. AFTER TAKEOFF OUT OF ALB, THE NR 2 HYDRAULIC CONTENTS DROPPED TO ZERO FOR APPROXIMATELY 5 MINUTES. AIRCRAFT RETURNED TO FIELD. TROUBLESHOT, FOUND FLEX LINE AT N
- [SDR PCAA9700501](https://openairdocs.org/sdr/PCAA9700501), Jul 25, 1997: LIGHT. INOPERATIVE. COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT WITH SERVICEABLE UNIT. OPERATIONAL CHECK N
- [SDR PCAA9700483](https://openairdocs.org/sdr/PCAA9700483), Jul 10, 1997: BULB. FAILED. FLT 3968 - ON APPROACH TO EWR UPON LANDING GEAR EXTENSION, LEFT MAIN GEAR DOWN INDICATION WAS IN OPERATIVE. CREW VERIFIED GEAR POSITION WITH ALTERNATE INDICATIO
- [SDR PCAA9600301](https://openairdocs.org/sdr/PCAA9600301), Aug 24, 1996: PROX CONTL BOX. FAILED. ELECTRICAL SMELL WAS NOTICED 10 MINUTES INTO FLIGHT, RETURNED TO FIELD. TROUBLESHOT AND FOUND PROXIMITY SENSOR ELECTRONIC UNIT AT FAULT. REMOVED AND REPLACED PS
- [SDR PCAA9600296](https://openairdocs.org/sdr/PCAA9600296), Jun 18, 1996: TURBINE BLADE. SEPARATED. FLT 3859 - EXPERIENCED A TORQUE FLUCTUATION OF THE NR 1 ENGINE AND INCREASE OF ITT TO APPROX 780 DEGREES. TORQUES DROPPED TO 50 PECENT FOLLOWED BY A LOUD GRINDI
- [SDR PCAA9600286](https://openairdocs.org/sdr/PCAA9600286), Apr 26, 1996: LIGHT. FAILED. EMERGENCY LIGHTS CIRCUIT BREAKER POPPED IN FLIGHT. TROUBLESHOT, FOUND FAULTY COCKPIT OVERHEAD EMERGENCY LIGHT ASSY. REPLACED EMERGENCY LIGHT ASSEMBLY, OPERATION
- [SDR PCAA9500254](https://openairdocs.org/sdr/PCAA9500254), Dec 14, 1995: TUBE ASSY. CRACKED. NR 1 HYDRAULIC SYSTEM CONTENTS WENT TO ZERO IN-FLIGHT. TROUBLESHOT, FOUND LINE AT PRESSURE MANIFOLD CRACKED, INSTALLED FLEX LINE IAW MM. RAN AIRCRAFT, OPERATION
- [SDR PCAA9500232](https://openairdocs.org/sdr/PCAA9500232), Jul 17, 1995: HYD LINE. FAILED. NR 1 HYD SYSTEM QUANTITY INDICATION DROPPED TO 0 FOLLOWED BY NR 1 PRESS INDICATION SYSTEM DROPPING TO 0. TROUBLESHOT, FOUND LINE FROM ANTI-SKID CONTROL VALVE TO
- [SDR PCAA9500231](https://openairdocs.org/sdr/PCAA9500231), Jun 27, 1995: VHF UNIT. LOOSE. CREW REPORTED LOSS OF ALL VHF COMMUNICATIONS. AIRCRAFT LANDED IN BOS WITHOUT INCIDENT. BOS MAINTENANCE FOUND RADIO ELECTRONICS UNIT UNSECURED. SECURED UNIT IN R

## 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 20020905037089I](https://openairdocs.org/incident/20020905037089I), Sep 5, 2002: Dhav DHC8102 (N831EX), Syracuse, NY. (-23) The aircraft was enroute from roc to lga but diverted to syr after the crew reported that the #2 hydraulic isolation valve caution light illuminated.…
- [Incident 19970503011479I](https://openairdocs.org/incident/19970503011479I), May 3, 1997: Dhav DHC8102 (N831EX), Syracuse, NY. Narrative: on Saturday, may 3, 1997, at 7:41 EST, a Dehavilland dash 8, N831EX, s/n 160, operated by alleghany airlines, inc., returned and landed on runway 10…
- [Incident 19951214043949I](https://openairdocs.org/incident/19951214043949I), Dec 14, 1995: Dhav DHC8102 (N831EX), Rochester, NY. Narrative: on December 14, 1995, at 1620 EST, a Dehavilland, DHC-8-102, N831EX, flight 3597, operated by allegheny commuter airlines, inc. during cruise flight…

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