# N821EX: Boeing Of Canada DHC-8-102, registration cancelled 2006-10-26 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 26, 2006 - Exported to: Australia - Status when cancelled: Valid registration - Airframe: [Boeing Of Canada DHC-8-102](https://openairdocs.org/model/boeing-of-canada-dhc-8-102) (registry code 1385305) - 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: 173 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: September 28, 1989 - Certificate issued: September 21, 2006 - Last registry action: October 26, 2006 - Mode S code: AB350C - 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/N821EX - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=821EX - Page: https://openairdocs.org/deregistered/N821EX-2006-10-26 From the FAA registry file of November 3, 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 Of Canada DHC-8-102: https://openairdocs.org/model/boeing-of-canada-dhc-8-102.md ## Service difficulty reports (34) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR PCAA0402168](https://openairdocs.org/sdr/PCAA0402168), Feb 16, 2004: MANIFOLD. BROKEN. FLIGHT 4072 TO LGA REPORTED COMPLETE LOSS OF NR 2 HYDRAULIC CONTENTS IN FLIGHT. AIRCRAFT RAN FOR 20 MINUTES WITH NO FLUID IN AFFECTED SYSTEM. MAINTENANCE INSPEC - [SDR PCAA0402164](https://openairdocs.org/sdr/PCAA0402164), Feb 12, 2004: AHRS. FAULTY. FLIGHT 3929 CLIMBING OUT OF PHILADELPHIA HAD TO RETURN TO FIELD DUE TO THE AHRS ON THE CAPTAINS SIDE GOING INOP. THE PILOT ELECTED TO RETURN TO FIELD FOR MAINTE - [SDR PCAA0402165](https://openairdocs.org/sdr/PCAA0402165), Feb 10, 2004: PCU. FAULTY. FLIGHT 3998 MIDDLETOWN, PILOT REPORTED THAT THE NR 2 PROP DID NOT FEATHER DURING THE AUTOFEATHER TEST. MAINTENANCE REMOVED AND REPLACED THE NR 2 PROPELLER CONTR - [SDR PCAA0311142](https://openairdocs.org/sdr/PCAA0311142), Nov 19, 2003: ACTUATOR. FAULTY. DURING CLIMB, AIRCRAFT 821EX, FLIGHT 3651 IN MIDDLETOWN HAD LEFT GEAR DOOR LIGHT REMAIN ILLUMINATED AFTER THE GEAR WAS RETRACTED. GEAR WAS CYCLED PER CHECKLIST, - [SDR PCAA0112174](https://openairdocs.org/sdr/PCAA0112174), Dec 30, 2001: LINK. WORN. DURING FLEET INSPECTION OF NOSE LANDING GEAR FOR WEAR IN THE TRAILING ARM LINK ASSEMBLY THE TRAILING ARM ASSEMBLY, LINK, UPPER AND LOWER PINS WERE REPLACED DUE - [SDR PCAA0111137](https://openairdocs.org/sdr/PCAA0111137), Nov 19, 2001: LATCH. LACK OF LUBE. BWI-FLIGHT 3909. CREW REPORTED COCKPIT DOOR LATCH MECHANISM IS BINDING AND HARD TO TURN PREVENTING EGRESS. MAINTENANCE LUBED LATCH. OPERATIONAL CHECK GOOD. AIRC - [SDR PCAA0108103](https://openairdocs.org/sdr/PCAA0108103), Jan 8, 2001: RIVET. LOOSE. DURING FLEET INSPECTION FOR NACELLE RIVETS BEING LOOSE AND MISSING, 2 RIVETS ON RIGHT NACELLE OUTBOARD END FOUND LOOSE JUST BELOW FLAP TRACK. LOOSE RIVETS REPLA - [SDR PCAA0007046](https://openairdocs.org/sdr/PCAA0007046), Jul 22, 2000: ATTACH ANGLE. CRACKED. UPON APPROACH INTO MDT, FLIGHT 3800 EXPERIENCED A LOUD THUMP NOISE WHEN THE GEAR WAS SELECTED DOWN. MAINTENANCE INSPECTED AND FOUND THE NOSE WHEEL WELL AREA WHE - [SDR PCAA0006043](https://openairdocs.org/sdr/PCAA0006043), Jun 23, 2000: CONTROL CABLE. BROKEN. PIT- UPON LANDING, FLIGHT 3949 EXPERIENCED A LOUD BANG AND THE RIGHT BRAKE PEDAL WENT FLUSH AGAINST THE FLOOR, CAPTAINS AND FIRST OFFICERS. MAINTENANCE INSPECTE - [SDR PCAA9900026](https://openairdocs.org/sdr/PCAA9900026), Aug 8, 1999: ACTUATOR. FAILED. BTV - UPON DESCENT, THE LEFT MAIN GEAR DID NOT EXTEND WHEN SELECTED. GEAR EXTENDED 45 SECONDS LATER WITH DOWN AND LOCKED INDICATION. MAINTENANCE REMOVED AND RPE - [SDR PCAA9800754](https://openairdocs.org/sdr/PCAA9800754), Mar 12, 1998: BULB. FAILED. SEVERAL SMALL BULBS INOPERATIVE IN FORWARD OVERHEAD EMERGENCY EXIT SIGN. REMOVED AND REPLACED BULBS. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR PCAA9800715](https://openairdocs.org/sdr/PCAA9800715), Feb 2, 1998: BULB. FAILED. FORWARD CENTER CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) - [SDR PCAA9800694](https://openairdocs.org/sdr/PCAA9800694), Jan 19, 1998: PSEU. FAILED. EN ROUTE TO PHL, UPON SELECTING THE LANDING GEAR DOWN THE GEAR DID NOT EXTEND. CAUTION LIGHT ILLUMINATED MOMENTARILY THEN EXTINGUISHED. THE CONTROL CIRCUIT BREA - [SDR PCAA9800681](https://openairdocs.org/sdr/PCAA9800681), Jan 3, 1998: BULB. FAILED. ONE LIGHT INOPERATIVE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M) - [SDR PCAA9700639](https://openairdocs.org/sdr/PCAA9700639), Dec 3, 1997: BATTERY. DISCHARGED. CENTER CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M) - [SDR PCAA9700638](https://openairdocs.org/sdr/PCAA9700638), Dec 3, 1997: LENS. MISSING. RIGHT SIDEWALL EMERGENCY EXIT SIGN MISSING LENSE AT ROW FOUR. REPLACED LENS. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR PCAA9700627](https://openairdocs.org/sdr/PCAA9700627), Nov 30, 1997: BATTERIES. DISCHARGED. CENTER OVERHEAD CABIN EMERGENCY LIGHT AND AFT OVERHEAD SIGN INOPERATIVE. CHARGED BATTERIES USING A/C SYSTEM OPERATIONAL CHECK GOOD. A/C RETURNED TO SERVICE. (M) - [SDR PCAA9700620](https://openairdocs.org/sdr/PCAA9700620), Nov 14, 1997: BULB. FAILED. CENTER CABIN OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR PCAA9700618](https://openairdocs.org/sdr/PCAA9700618), Nov 14, 1997: BULB. FAILED. RIGHT AFT EXTERIOR EMERGNCY EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M) - [SDR PCAA9700606](https://openairdocs.org/sdr/PCAA9700606), Oct 31, 1997: SEAT TRACK. WORN. CAPTAINS LEFT SEAT TRACK SHOWING WEAR. REPAIRED SEAT RAILS IAW DHC SERVICE BULLETIN 8-53-53 AND RD8-53-2658. A/C RETURNED TO SERVICE. (M) - [SDR PCAA9700595](https://openairdocs.org/sdr/PCAA9700595), Oct 31, 1997: SEAT TRACK. WORN. CAPTAIN'S LEFT SEAT TRACK SHOWING WEAR. MAINTENANCE PERFORMED S/B 8-53-53 TO AIRCRAFT. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR PCAA9700580](https://openairdocs.org/sdr/PCAA9700580), Oct 19, 1997: BULB. FAILED. RIGHT AFT EXTERIOR EMERGENCY EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR PCAA9700575](https://openairdocs.org/sdr/PCAA9700575), Oct 15, 1997: BULB. FAILED. AFT CENTER AISLE OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR PCAA9700552](https://openairdocs.org/sdr/PCAA9700552), Sep 22, 1997: LIGHT. INOPERATIVE. COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT ASSEMBLY WITH SERVICEABLE UNIT. OPERATIONA - [SDR PCAA9700539](https://openairdocs.org/sdr/PCAA9700539), Sep 9, 1997: BATTERY PACK. DISCHARGED. RIGHT CABIN AFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT FORWARD BATTERY PACK. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR PCAA9700500](https://openairdocs.org/sdr/PCAA9700500), Jul 26, 1997: LIGHT. INOPERATIVE. COCKPIT EMERGENCY LIGHT WILL NOT HOLD A CHARGE. REMOVED AND REPLACED COCKPIT OVERHEAD EMERGENCY LIGHT WITH SERVICEABLE UNIT. OPERATIONAL CHECK NORMAL. AIRCRAFT - [SDR PCAA9700490](https://openairdocs.org/sdr/PCAA9700490), Jul 16, 1997: BATTERY PACK. OPEN CIRCUIT. AFT LEFT EMERGENCY EGRESS LIGHT DOES NOT ILLUMINATE WHEN SELECTED ON. FOUND OPEN CIRCUIT AT EMERGENCY LIGHT BATTERY PACK AT POSITION PS3. REPAIRED CIRCUIT. OPER - [SDR PCAA9700379](https://openairdocs.org/sdr/PCAA9700379), Apr 17, 1997: BULB. FAILED. ONE LIGHT INOPERATIVE IN EMERGENCY FLOOR PATH LIGHTING. REMOVED AND REPLACED LAMP. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) - [SDR PCAA9600330](https://openairdocs.org/sdr/PCAA9600330), Dec 12, 1996: HYD HOSE. FAILED. UPON TAKEOFF OUT OF MHT, WHEN LANDING GEAR WAS SELECTED UP, THE NR 2 HYDRAULIC CONTENTS FELL TO ZERO. CREW PERFORMED A MANUAL EXTENSION OF GEAR . THE AIRCRAFT R - [SDR PCAA9600308](https://openairdocs.org/sdr/PCAA9600308), Sep 12, 1996: UPLOCK SWITCH. FAILED. FLT 3827 - AFTER GEAR RETRACTION, NOSE GEAR INDICATED UNSAFE AND NOSE GEAR DOORS INDICATED OPEN. CREW PERFORMED ALTERNATE GEAR EXTENSION AND RETURNED TO SCE WIT - [SDR PCAA9500248](https://openairdocs.org/sdr/PCAA9500248), Nov 13, 1995: LIGHT. INTERMITTENT. THE PORTABLE OVERHEAD EMERGENCY LIGHT FLASHES INTERMITTENTLY, AND SHOWS LOW ILLUMINATION ON GROUND. REMOVED AND REPLACED C/P EMERGENCY LIGHT. AIRCRAFT RETURNED - [SDR PCAA9500235](https://openairdocs.org/sdr/PCAA9500235), Jul 20, 1995: FUEL FILTER. CLOGGED. NR 2 FUEL FILTER BYPASS LIGHT ILLUMINATED ON TAKEOFF. TAKEOFF WAS ABORTED. REMOVED AND REPLACED HIGH AND LOW PRESSURE FILTERS, BYPASS SWITCH, RAN ENGINE, OPS OK - [SDR PCAA9500190](https://openairdocs.org/sdr/PCAA9500190), Jan 30, 1995: EEL COVER. LOOSE. PLASTIC COVER TO EMERGENCY FLOOR LIGHTS IS COMING UP. RESECURED LIGHT COVER. ACFT RETURNED TO SERVICE. (W) - [SDR PCAA9500185](https://openairdocs.org/sdr/PCAA9500185), Jan 8, 1995: ENGINE. FAILED. THE NR 1 ENGINE SHUTDOWN IN FLIGHT. INSPECTED AND FOUND ACCESSORY GEAR DRIVE SHIFTED AND OIL COMTAMINATED WITH METAL. REMOVED AND REPLACED NR 1 ENGINE ASSEMBLY ## FAA accident and incident reports (2) 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 20010525010379I](https://openairdocs.org/incident/20010525010379I), May 25, 2001: Dhav DHC8102 (N821EX), Pittsburgh, PA. (-23)On 5/25/01 at 1310E allegheny airlines flight 3605 a Boeing (dehav) DHC-8 N821EX returned to land at Pittsburgh international airport runway 10L just… - [Incident 19950108002659I](https://openairdocs.org/incident/19950108002659I), Jan 8, 1995: Dhav DHC8301 (N821EX), Middletown, PA. Narrative: during cruise flight at 11,000 feet MSL, the #1 engine shut itself down. The engine was secured and the flight was diverted to MDT where it landed… --- 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.