# N825EX: 1994 Dehavilland DHC-8-102, registration cancelled 2010-08-17

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 17, 2010
- Exported to: Australia
- Status when cancelled: Triennial form not returned
- Airframe: [Dehavilland DHC-8-102](https://openairdocs.org/model/dehavilland-dhc-8-102) (registry code 2809003)
- 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: 388
- Year built: 1994
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: October 28, 1994
- Certificate issued: October 20, 1994
- Last registry action: November 18, 2008
- Mode S code: AB43E8
- 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/N825EX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=825EX
- Page: https://openairdocs.org/deregistered/N825EX-2010-08-17

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 Dehavilland DHC-8-102: https://openairdocs.org/model/dehavilland-dhc-8-102.md

## Service difficulty reports (42)

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

- [SDR HNAA2009091400286](https://openairdocs.org/sdr/HNAA2009091400286), Sep 13, 2009: BULB. BURNED OUT. CABIN ROW 7 HAS ONE FLOOR EMERGENCY LIGHT OUT. REMOVED AND REPLACED ROW 1 FLOOR EMERGENCY LIGHT BULB IAW AMM 33-51-00.
- [SDR HNAA2009041600122](https://openairdocs.org/sdr/HNAA2009041600122), Apr 16, 2009: PIPE. LEAKING. FLIGHT ATTENDANT REPORTS SULFUR ODOR BETWEEN ROWS 2 THRU 5 IN-FLIGHT AND ON GROUND. REMOVED AND REPLACED RIGHT CENTER WING BLEED PIPE. OPS CHECKS GOOD. OK FOR S
- [SDR HNAA2009041700123](https://openairdocs.org/sdr/HNAA2009041700123), Apr 16, 2009: BRAKE. LEAKING. SMOKE COMING FROM NUMBER ONE BRAKE AREA, INSPECT FOUND NUMBER TWO BRAKE TO HAVE A LEAK. REMOVED AND REPLACED NUMBER TWO BRAKE IN ACCORDANCE WITH 32-42-11, LEAK 
- [SDR HNAA2009020700045](https://openairdocs.org/sdr/HNAA2009020700045), Feb 5, 2009: SMOKE DETECTOR. FALSE INDICATION. BAG SMOKE WARNING LIGHT CAME ON IN FLIGHT. NO EVIDENCE OF SMOKE. R&R NR 1 AND NR 2 BAGBAY SMOKE DETECTORS IAW 26-12-01, OPS CHECK GOOD.
- [SDR HNAA0800289](https://openairdocs.org/sdr/HNAA0800289), Sep 14, 2008: PRESSURE SWITCH. STUCK. NR2 ENGINE BLEED HOT CAUTION LIGHT ILLUMINATED DURING FLIGHT. LIGHT GOES OUT WHEN SWITCH SELECTED OFF, FERRYING TO SBY. R&R D BLEED OVERTEMP SWITCH IAW AMM 21-1
- [SDR HNA2008F00049](https://openairdocs.org/sdr/HNA2008F00049), Aug 20, 2008: BULB. INOPERATIVE. MOST REAR OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPS CHECK GOOD. (S)
- [SDR HNA2008F00048](https://openairdocs.org/sdr/HNA2008F00048), Aug 19, 2008: LAMP. BURNED OUT. EMERGENCY BUTTON ON FAS CONTROL PANEL NOT BACKLIT. REPORTED TO MAINTENANCE. RELAMPED FAS EMERGENCY BUTTON ON CONTROL PANEL. OK FOR SERVICE. (S)
- [SDR HNAA0800233](https://openairdocs.org/sdr/HNAA0800233), Jul 15, 2008: CONNECTOR. DIRTY. EMERGENCY LIGHTS WERE FLASHING FOR ABOUT ONE MINUTE AFTER ROTATION. CREW REPORTED. (S)
- [SDR HNAA0800156](https://openairdocs.org/sdr/HNAA0800156), May 9, 2008: MOUNT. WORN. NR 1 INBOARD AFT VERTICAL MOUNT STRUT BEARING WORN. INSP GENERATED BY RII CARD 71-20-03.
- [SDR HNAA0800009](https://openairdocs.org/sdr/HNAA0800009), Dec 22, 2007: WIRE HARNESS. BROKEN. THE CABIN FLOOR EMERGENCY LIGHTING AT ROW 4 WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND A WIRE BROKEN AND CONTACT PIN PULLED FROM CONNECTOR 3352-P5. WIRE WAS
- [SDR HNAA0800001](https://openairdocs.org/sdr/HNAA0800001), Dec 21, 2007: HOT WATER POT. BURNED. BURNING ODOR COMING FROM F/A HANDSET. AFTER INSPECTION, IT WAS DETERMINED THE ODOR TO BE COMING FROM NR 1 HOT WATER BOTTLE RECEPTACLE. REMOVED AND REPLACED RECE
- [SDR HNAA0800008](https://openairdocs.org/sdr/HNAA0800008), Dec 18, 2007: BLEED AIR SYS. CONTAMINATED. DURING OPERATION, AN ODOR THAT WAS BELIEVED TO BE FUEL WAS DETECTED WHEN NR 1 ENGINE BLEED SYSTEM WAS SELECTED ON. BLEED SYSTEM FOR NR 1 AND NR 2 ENGINES, ALONG
- [SDR HNAA0700279](https://openairdocs.org/sdr/HNAA0700279), Nov 29, 2007: ECU. DEFECTIVE. NR 2 ENGINE MANUAL CAUTION LIGHT ILLUMINATED AFTER ENGINE START. MEL'D NR 2 ECU. ON 30 NOVEMBER 2007, NR 2 ECU WAS REPLACED. OPERATIONAL CHECK GOOD. 
- [SDR HNAA0700115](https://openairdocs.org/sdr/HNAA0700115), Jun 17, 2007: RELAY. FAILED. JUST AFTER TAKEOFF, GEAR DID NOT GO UP WHEN SELECTED. ONLY GETTING INDICATION OF 3 GREEN AND 3 RED LIGHTS. GEAR DID NOT GO UP. REMOVED AND REPLACED RELAYS 3261 
- [SDR HNAA0700112](https://openairdocs.org/sdr/HNAA0700112), Jun 7, 2007: SELECTOR VALVE. MALFUNCTIONED. GEAR FAIL TO EXTEND ON LANDING WHEN SLECTED. FERRY AIRCRAFT TO ROA AND SWAP OUT WITH SPARE AC. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE, LEAK AND OPS CH
- [SDR HNAA0700105](https://openairdocs.org/sdr/HNAA0700105), May 27, 2007: BATTERY PACK. DISCHARGED. FIRST TWO FORWARD FLOOR EMERGENCY LIGHTS INOPERATIVE. DEBOARDED PASSENGERS SO MAINTENANCE COULD WORK THE PROBLEM. REMOVED AND REPLACED NR 400 EMERGENCY LIGHT PO
- [SDR HNAA0600125](https://openairdocs.org/sdr/HNAA0600125), Oct 22, 2006: ENGINE. OVERSERVICED. SOON AFTER TAKEOFF CREW SMELLED STRONG ODOR AFTER BLEED WAS TURNED ON. INSPECTED CABIN AND FLIGHT DECK FOUND NOTHING OUT OF THE ORDINARY. CHECKED OIL LEVEL OF B
- [SDR HNAA0500078](https://openairdocs.org/sdr/HNAA0500078), Aug 28, 2005: HMU. FAILED. A 5 INCH POWER LEVER SPLIT IN CRUISE. REMOVED AND REPLACED HYDRO MECHANICAL UNIT AND FUEL PUMP.
- [SDR HNAA0400118](https://openairdocs.org/sdr/HNAA0400118), Sep 1, 2004: LINE. CRACKED. FLIGHT NR 3955, REPORTED THE NR 1 HYDRAULIC CONTENTS DROPPING ON LANDING. RUDDER ISO VALVE LIGHT ILLUMINATED THEN WENT OUT. FLIGHT LANDED WITHOUT INCIDENT. FLUI
- [SDR PCAA0405199](https://openairdocs.org/sdr/PCAA0405199), Apr 30, 2004: INDICATOR. ERRATIC. ABORTED TAKEOFF DUE TO THE NR 1 OIL PRESSURE FLUCTUATING DURING TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE OIL PRESSURE INDICATOR AND PRESSURE TRANSMITTER. S
- [SDR PCAA0403179](https://openairdocs.org/sdr/PCAA0403179), Mar 6, 2004: GAUGE. FAULTY. FLIGHT 3711 REPORTED A HORN SOUNDING DURING TAKEOFF ROLL, POWER WAS AT 82 PERCENT AND SPEED APPROXIMATELY 60 KNOTS. MAINTENANCE FOUND THE FLAP GAUGE TO BE AT FA
- [SDR PCAA0307081](https://openairdocs.org/sdr/PCAA0307081), Jul 10, 2003: DOOR. OUT OF ADJUST. PHL-FLIGHT NR 3556. CREW REPORTED THAT FLIGHT ATTENDANT COULD NOT OPEN THE PASSENGER DOOR. MAINTENANCE ADJUSTED THE PASSENGER DOOR IAW MFG DASH 8 MAINTENANCE MA
- [SDR PCAA0302032](https://openairdocs.org/sdr/PCAA0302032), Feb 1, 2003: FITTING. CRACKED. BGM-PHL FLIGHT#3577. AIRCRAFT RETURNED TO FIELD DUE TO #2 HYDRAULIC QUANTITY GOING TO ZERO ON CLIMB OUT. EMERGENCY WAS DECLARED. MAINTENANCE REPLACED O RINGS ON
- [SDR PCAA0111150](https://openairdocs.org/sdr/PCAA0111150), Oct 17, 2001: LINK. WORN. DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, TRAILING ARM LINK AND PIN FOUND TO HAVE PLAY. REPLACED PISTON CAP TRAILING LINK, AN
- [SDR PCAA0108096](https://openairdocs.org/sdr/PCAA0108096), Aug 28, 2001: GAUGE. INOPERATIVE. PHL-ORH FLIGHT#3692. DURING CLIMB #1 ENGINE OIL PRESSURE GAUGE INDICATED ZERO PSI. #1 ENGINE WAS SHUT DOWN AS A PRECAUTION AND AIRCRAFT RETURNED TO THE FIELD.MA
- [SDR PCAA0008056](https://openairdocs.org/sdr/PCAA0008056), Aug 12, 2000: SKIN. CRACKED. MDT - DURING A FLEET INSPECTION THE REAR FUSELAGE AT FRAME 4 STRINGER 5 WAS FOUND CRACKED. REPAIRS WERE MADE IAW DHC RD8-55-535 AND THE AIRCRAFT WAS RETURNED TO
- [SDR PCAA0002021](https://openairdocs.org/sdr/PCAA0002021), Feb 15, 2000: HARNESS. DAMAGED. NOSE GEAR UNSAFE LIGHT ILLUMINATED IN FLIGHT, WENT OUT WHEN GEAR WAS DOWN AND LOCKED. MAINTENANCE INSPECTED, FOUND NOSE GEAR DRAG STRUT WIRING AND HARNESS DAMAG
- [SDR PCAA0001001](https://openairdocs.org/sdr/PCAA0001001), Dec 30, 1999: GAS STRUT. BROKEN. FLIGHT 3692 IN PHL- PASSENGER DOOR WAS FOUND DIFFICULT TO OPEN AND CLOSE. PASSENGERS WERE DEPLANED NORMALLY. MAINTENANCE INSPECTED AND FOUND THE AFT DOOR STRUT 
- [SDR PCAA9800716](https://openairdocs.org/sdr/PCAA9800716), Feb 6, 1998: BULB. FAILED. ONE LIGHT INOPERATIVE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (X)
- [SDR PCAA9700598](https://openairdocs.org/sdr/PCAA9700598), Nov 2, 1997: CONNECTOR. LOOSE. LEFT SIDE EMERGENCY LIGHT AT EXIT DOOR BASE WILL NOR ILLUMINATE. REMOVED WALL PANEL FOUND MATRIX CONNECTOR LOOSE. SECURED CONNECTOR. OPERATIONAL TEST NORMAL. A/
- [SDR PCAA9700566](https://openairdocs.org/sdr/PCAA9700566), Oct 5, 1997: BRACKET. BENT. COCKPIT PORTABLE EMERGENCY LIGHT COMES ON WHEN AIRCRAFT IS SHUT DOWN. FOUND AFT TAB ON MOUNTING BRACKET TO BE BENT. ADJUSTED AFT TAB AND RESECURED LIGHT ASSEMBL
- [SDR PCAA9700565](https://openairdocs.org/sdr/PCAA9700565), Oct 4, 1997: LIGHT. INOPERATIVE. FLIGHT DECK OVERHEAD PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED COCKPIT PORTABLE EMERGENCY LIGHT ASSEMBLY WITH SERVICEABLE UNIT. OPERATIONAL TEST NORMAL. AI
- [SDR PCAA9700547](https://openairdocs.org/sdr/PCAA9700547), Sep 15, 1997: LIGHT. INOPERATIVE. FLOOR EMERGENCY PATH LIGHT AT ROW 7DF INOPERATIVE. FOUND WIRE PULLED OUT FROM LIGHT SOCKET. REMOVED AND REPLACED LIGHT. OPERATIONAL CHECK NORMAL. AIRCRAFT RETUR
- [SDR PCAA9700530](https://openairdocs.org/sdr/PCAA9700530), Aug 27, 1997: SMOKE DETECTORS. FAILED. SMOKE LIGHT CAME ON IN FLIGHT, AIRCRAFT RETURNED TO FIELD PHL. MAINTENANCE TROUBLESHOT SYSTEM, REMOVED AND REPLACED BOTH DETECTORS. SYSTEM OPERATIONALLY CHECKED
- [SDR PCAA9700523](https://openairdocs.org/sdr/PCAA9700523), Aug 15, 1997: SEAT TRACK. CORRODED. LEFT INBOARD SEAT RAIL FOUND CORRODED UNDER WARDROBE FLOOR DURING C-CHECK FROM STATION X190 TO X210. SPLICED IN NEW SECTION OF SEAT RAIL IAW DHC RD 8-53-1932. A
- [SDR PCAA9600312](https://openairdocs.org/sdr/PCAA9600312), Sep 18, 1996: ACTUATOR. FAILED. NOSE AMBER DOOR ANNUNCIATOR STAYED ILLUMINATED AFTER GEAR RETRACTION. REMOVED AND REPLACED NOSE LANDING GEAR DOOR MECHANICAL SEQUENCE VALVE AND NOSE LANDING GEA
- [SDR 96ZZZM1476](https://openairdocs.org/sdr/96ZZZM1476), Sep 18, 1996: SEQ VALVE. FAILED. NOSE AMBER DOOR ANNUNCIATOR STAYED ILLUMINATED AFTER GEAR RETRACTION. REMOVED AND REPLACED NOSE LANDING GEAR DOOR MECHANICAL SEQUENCE VALVE AND NOSE LANDING GEA
- [SDR PCAA9600311](https://openairdocs.org/sdr/PCAA9600311), Sep 14, 1996: UPLOCK SWITCH. FAILED. FLT 3640 - AFTER GEAR RETRACTION NOSE DOORS INDICATED OPEN. AFTER GEAR WAS CYCLED NOSE GEAR DID NOT SHOW DOWN AND LOCKED. CREW PERFORMED ALTERNATE EXTENSION AND
- [SDR PCAA9500256](https://openairdocs.org/sdr/PCAA9500256), Dec 24, 1995: SIG COND UNIT. FAILED. LGA - UPON CLIMB-OUT, NR 1 ENGINE EXPERIENCED AN UNSCHEDULED FEATHERING OF THE PROPELLER. MAXIMUM ENGINE TORQUE APPROXIMATELY 109 PERCENT FOR 5 SECONDS. CREW SH
- [SDR 96ZZZX215](https://openairdocs.org/sdr/96ZZZX215), Dec 24, 1995: ELEC ENG CONT. FAILED. LGA - UPON CLIMB-OUT, NR 1 ENGINE EXPERIENCED AN UNSCHEDULED FEATHERING OF THE PROPELLER. MAXIMUM ENGINE TORQUE APPROXIMATELY 109 PERCENT FOR 5 SECONDS. CREW SH
- [SDR PCAA9500242](https://openairdocs.org/sdr/PCAA9500242), Oct 13, 1995: O-RINGS. LEAKING. LOST NR 2 HYDRAULIC QUANTITY AND PRESSURE, AFTER 20 MINUTES HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED. INSPECTED, FOUND O-RING ON UNION OF GROUND HYDRAULIC LINE 
- [SDR PCAA9500199](https://openairdocs.org/sdr/PCAA9500199), Feb 20, 1995: HYD LINE. CRACKED. THE NR 2 HYDRAULIC SYSTEM LOST QUANTITY. FOUND HYDRAULIC LINE CRACKED AT FLARE. REPLACED RIGID LINE WITH FLEX LINE AS PER DASH-8 MM 20-50-52. SERVICED HYDRAULIC

## 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 20030201007879I](https://openairdocs.org/incident/20030201007879I), Feb 1, 2003: Dhav DHC8102 (N825EX), Binghamton, NY. (-23) On February 1, 2003, flt. 3577, N825EX, DHC-8, on climb-out, gear was selected "up", and hydraulic quantity on #2 system went to "0". Aircraft landed…
- [Incident 19960918032839I](https://openairdocs.org/incident/19960918032839I), Sep 18, 1996: Dhav DHC8102 (N825EX), Syracuse, NY. Narrative: on September 18, 1996 at 0655 EDT, a Dehavilland DHC-8-102, N825EX, flight 3853, operated by allegheny commuter airlines, inc., during takeoff from…
- [Incident 19951013041289I](https://openairdocs.org/incident/19951013041289I), Oct 13, 1995: Dhav DHC8102 (N825EX), Middletown, PA. Narrative: on October 13, 1995, during an IFR scheduled flight from boston (bos) to Harrisburg (MDT), allegheny airlines flight 3714, a Dehavilland DHC-8, on a…

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