# N816EX: Dehavilland DHC-8-102, registration cancelled 2022-02-14

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 14, 2022
- Exported to: Canada
- Status when cancelled: Second renewal notice
- 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: 329
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: June 16, 1992
- Certificate issued: March 11, 2019
- Last registry action: April 16, 2019
- Mode S code: AB2020
- Owner when cancelled: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%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/N816EX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=816EX
- Page: https://openairdocs.org/deregistered/N816EX-2022-02-14

From the FAA registry file of October 31, 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 (103, newest 50)

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

- [SDR HNAA2017010400002](https://openairdocs.org/sdr/HNAA2017010400002), Jan 4, 2017: BATTERY PACK. INOPERATIVE. RIGHT AFT EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE BATTERY. OPS CHECKED GOOD.
- [SDR HNAA2017010400001](https://openairdocs.org/sdr/HNAA2017010400001), Jan 4, 2017: BULB. INOPERATIVE. F/A PANEL EMERGENCY LIGHT SWITCH ON IS INOPERATIVE. REMOVED AND REPLACED THE F/A EMERGENCY LIGHT SWITCH BULB. OPS CHECKED GOOD.
- [SDR HNAA2016102400330](https://openairdocs.org/sdr/HNAA2016102400330), Oct 24, 2016: AHRS. INACCURATE. DURING TAXI, AFTER PUSH BACK, ADI MISMATCH APPEARED ON BOTH 802 PANELS. F/O ADI ROLLS TO THE RIGHT. CORRECTED WITH SAHS. REMOVED AND REPLACED THE AHRS IAW MM 34
- [SDR HNAA2016061500177](https://openairdocs.org/sdr/HNAA2016061500177), Jun 13, 2016: STEERING SYS. OUT OF ADJUST. UPON LANDING, ACFT PULLED TO THE LT AND REQUIRED FULL RIGHT RUDDER TO STAY ON CENTERLINE. ACFT PULLS TO THE LT DURING NORMAL TAXI. MDT ADJUSTED LVDT IAW MM 32-5
- [SDR HNAA2016060100161](https://openairdocs.org/sdr/HNAA2016060100161), May 31, 2016: LIGHT. INOPERATIVE. INOPERATIVE EMERGENCY FLOOR LIGHT AT ROW 3. REMOVED PLASTIC COVER. R & R BULB ON ROW 3 FLOOR LIGHT INSTALLED PLASTIC POWER, OPS CK GOOD, PN OL3071BPEGPL.
- [SDR HNAA2016041800108](https://openairdocs.org/sdr/HNAA2016041800108), Apr 15, 2016: SPOILER SYS. MALFUNCTIONED. ON TAKE OFF ROLL, SPOILERS DID NOT RETRACT. ABORTED TAKE OFF IAW MAINTENANCE CONTROL CREW CYCLED PUSHOFF SWITCHES AND FLT/TAXI SWITCH GROUND RUN A/C SYSTEM NORM
- [SDR HNAA2015120900364](https://openairdocs.org/sdr/HNAA2015120900364), Dec 9, 2015: BULB. INOPERATIVE. EMERGENCY FLOOR LIGHT IS INOPERATIVE AT ROW 7. R & R BULBS. OPS CHECKED GOOD.
- [SDR HNAA2015112500352](https://openairdocs.org/sdr/HNAA2015112500352), Nov 25, 2015: BATTERY PACK. INOPERATIVE. LEFT EMERGENCY EXIT LIGHT AND LEFT FORWARD EGRESS LIGHTS ARE INOPERATIVE. FOUND BATTERY A, PS1 O BE OF SHELF FAILURE. R & R PS1 BATTERY IAW WC 33-50-0R. OPS CHE
- [SDR HNAA2015101900306](https://openairdocs.org/sdr/HNAA2015101900306), Oct 19, 2015: BULB. INOPERATIVE. EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT ROW 9. R & R BULB AT EMERGENCY FLOOR PATH LIGHT IN ROW 9. OPS CHECKED GOOD.
- [SDR HNAA2015100500289](https://openairdocs.org/sdr/HNAA2015100500289), Oct 4, 2015: CIRCUIT BREAKER. FAULTED. NR 1 ENGINE AC GENERATOR ILLUMINATED UPON TAKEOFF. INSPECTED NR 1 AC CONTACTOR BOX FOUND CIRCUIT BREAKERS FAULTY. R & R CB'S 2421CB3, 2421CB5, 2421CB7 & 2421CB9
- [SDR HNAA2015081400254](https://openairdocs.org/sdr/HNAA2015081400254), Aug 14, 2015: CONNECTOR. UNSECURE. EMERGENCY LIGHTS AFT OF OUTER WING 4AC ARE INOPERATIVE, SIDEWALL LIGHT WITH ARROW POINTING TOWARD THE DOOR. FOUND CONNECTOR PLUG TO EMERGENCY LIGHT UNSECURED. R
- [SDR HNAA2015061200193](https://openairdocs.org/sdr/HNAA2015061200193), Jun 12, 2015: BULB. INOPERATIVE. 5TH FROM FRONT, FORWARD EMERGENCY PATH LIGHT IS INOPERATIVE, BETWEEN ROWS 1 AND 2. R & R BULBS A FORWARD EMERGENCY PATH LIGHTS. OPS CHECKED GOOD.
- [SDR HNAA2015061200192](https://openairdocs.org/sdr/HNAA2015061200192), Jun 12, 2015: BULB. MALFUNCTIONED. RT SIDE, FORWARD EMERGENCY LIGHT IS DIM. R & R EMERGENCY LIGHT BULB IAW MM 33-51-00. OPS CHECKED GOOD.
- [SDR HNAA2015040300118](https://openairdocs.org/sdr/HNAA2015040300118), Apr 3, 2015: STRUCTURE. CHAFED. 2 MEMBERS CHAFED ON OTBD SIDE OF NR 2 NACELLE AT 3 O'CLOCK POSITION. REPAIRED IAW EO 8-54-14-0060.
- [SDR HNAA2015032700111](https://openairdocs.org/sdr/HNAA2015032700111), Mar 27, 2015: BATTERY. INOPERATIVE. 2ND AND 4TH EMERGENCY LIGHTS WILL NOT ILLUMINATE. R & R EMERGENCY LIGHT BATTERY AT PS6 IAW 33-52-00. OPS CHECKED GOOD.
- [SDR HNAA2014040900124](https://openairdocs.org/sdr/HNAA2014040900124), Apr 9, 2014: CONNECTOR. DISCONNECTED. EMERGENCY EXIT LIGHT AT RT SIDE IS INOPERATIVE. FOUND WIRE CONNECTOR TO LIGHT ASSY NOT CONNECTED. CONNECTED WIRING HARNESS, OPS CHECKD GOOD.
- [SDR HNAA2014030300065](https://openairdocs.org/sdr/HNAA2014030300065), Mar 2, 2014: BOOT. FAILED. NR 2 BOOT ON RT WING WOULD NOT INFLATE OR INDICATE. R & R L/E 613BR IAW AMM 57-00-00. OPS CHECKED GOOD.
- [SDR HNAA2013122300634](https://openairdocs.org/sdr/HNAA2013122300634), Dec 23, 2013: BULB. INOPERATIVE. EMERGENCY SIDEWALL LIGHT IS DIM AT ROW 4DF. R & R BULBS IN EMERGENCY SIDEWALL LIGHT. OPS CHECKED GOOD.
- [SDR HNAA2013121800622](https://openairdocs.org/sdr/HNAA2013121800622), Dec 18, 2013: BULB. INOPERATIVE. FOUR EMERGENCY FLOOR PATH LIGHTS ARE INOPERATIVE. R & R BULBS. OPS CHECKED GOOD.
- [SDR HNAA2013050600254](https://openairdocs.org/sdr/HNAA2013050600254), May 4, 2013: ACTUATOR. INOPERATIVE. AFTER TAKE OFF, DURING GEAR RETRACTION, NLG INDICATED UNSAFE AND ALL GEAR DOORS STAYED OPEN. R & R NLG RETRACT ACTUATOR. OPS CHECKED GOOD ON GROUND IAW AMM 32-3
- [SDR HNAA2013030100099](https://openairdocs.org/sdr/HNAA2013030100099), Mar 1, 2013: TRANSMITTER. FAILED. NR 2 MAIN HYD PRESSURE INDICATION DROPPED TO 0 PSI ON TAKEOFF ROLL. NO CAUTION LIGHTS ILLUMINATED AND HYD QUANTITY IS GOOD. R & R HYDRAULIC PRESSURE TRANSMITTER
- [SDR HNAA2013012800023](https://openairdocs.org/sdr/HNAA2013012800023), Jan 28, 2013: APU. SMOKE. WITH APU BLEEDS TURNED ON, FLIGHT DECK FILLED WITH SMOKE. ALL OTHER APU INDICATIONS AND OPERATIONS NORMAL AT THIS TIME. VERIFY FUEL VALVE CLOSED. PULLED AND COL
- [SDR HNAA2012123101136](https://openairdocs.org/sdr/HNAA2012123101136), Dec 31, 2012: BLADE. SPARKS. SPARKS OBSERVED COMING FROM NR 2 PROPELLER AFT OF THE SPINNER. NO VIBRATION AND PROP HEAT INDICATED NORMAL. FOUND RT PROPELLER NR 4 BLADE HEATER MAT BURNED. R &
- [SDR HNAA2012121001094](https://openairdocs.org/sdr/HNAA2012121001094), Dec 10, 2012: TERMINAL. LOOSE. CAPTAIN'S WINDSHIELD HEAT INOPERATIVE. REPLACED LOOSE RING TERMINAL ON TERMINAL "B", PRIMARY HEAT ELEMENT AND ALTERNATE HEAT ELEMENT OHM`D OUT NORMALLY. GROUND 
- [SDR HNAA2012121001093](https://openairdocs.org/sdr/HNAA2012121001093), Dec 10, 2012: CONTROLLER. INOPERATIVE. CAPTAIN`S WINDSHIELD HEAT INOPERATIVE. NO LOADS AND COLD TO THE TOUCH. REMOVED AND REPLACED CAPTAIN'S WINDSHIELD HEAT CONTROLER (P3) IAW 30-41-00. GROUND OPS CH
- [SDR HNAA2012030900680](https://openairdocs.org/sdr/HNAA2012030900680), Mar 9, 2012: LAMP. FAILED. ROW 1DF SIDEWALL EMERGENCY LIGHT LAMP INOPERATIVE. RELAMPED.
- [SDR HNAA2012022700622](https://openairdocs.org/sdr/HNAA2012022700622), Feb 27, 2012: SMOKE DETECTOR. INTERMITTENT. LAVATORY SMOKE DETECTOR SOUNDS INTERMITTENTLY WITH APU BLEEDS ON.
- [SDR HNAA2012021400575](https://openairdocs.org/sdr/HNAA2012021400575), Feb 11, 2012: SMOKE DETECTOR. ACTIVATED. LAVATORY SMOKE DETECTOR GOES OFF WITH APU BLEED SELECTED ON. NORMAL WITH BLEED OFF.
- [SDR HNAA2012010600453](https://openairdocs.org/sdr/HNAA2012010600453), Jan 5, 2012: UNKNOWN. ODOR. EXHAUST ODOR PRESENT WHEN APU BLEED USED. OK WITH ENGINE BLEEDS. APU HAS BEEN MEL'D.
- [SDR HNAA2011122000430](https://openairdocs.org/sdr/HNAA2011122000430), Dec 20, 2011: LAMP. FAILED. NR 2 FROM FRONT EMERGENCY FLOOR PATH LIGHT IS INOP. RELAMPED NR 2 FROM THE FRONT EMERGENCY FLOOR PATH LIGHT. OPS CHECKED GOOD.
- [SDR HNAA2011111000364](https://openairdocs.org/sdr/HNAA2011111000364), Nov 10, 2011: SEAT TRACK. CORRODED. CORROSION ON RT INBD SEAT TRACK AT BS 215 AROUND NUT PLATE HOLE. AREA IS REMOVED DUE TO SEAT TRACK SPLICE, IAW RD8-53-3074.
- [SDR HNAA2011111000361](https://openairdocs.org/sdr/HNAA2011111000361), Nov 10, 2011: SEAT TRACK. CORRODED. LIGHT CORROSION AT RT OTBD SEAT TRACK AT BS 295. BLENDED AREA TO WITHIN LIMITS IAW RD8-53-1342.
- [SDR HNAA2011111000380](https://openairdocs.org/sdr/HNAA2011111000380), Nov 10, 2011: SKIN. CRACKED. PAX DOOR SKIN NR5 BEAM CRACKED AT FORWARD INBD MOUNT AREA. R & R PAX DOOR SKIN.
- [SDR HNAA2011111000379](https://openairdocs.org/sdr/HNAA2011111000379), Nov 10, 2011: FRAME. CORRODED. CORROSION ON BACK SIDE OF FRAME JOINT STRAP BELOW LT MID EMERGENCY EXIT DOOR AT STA X370.80. CLEANED CORROSION, INSPECTED AND ALODINED JOINT STRAP. PRIMED AS RE
- [SDR HNAA2011111000378](https://openairdocs.org/sdr/HNAA2011111000378), Nov 10, 2011: FRAME. CORRODED. CORROSION ON FRAME MEMBER BELOW RT FORWARD EMERGENCY EXIT DOOR AT STA X252.30. REMOVED VERY MINOR CORROSION. CORROSION NOT PASSED THE PROTECTIVE COATING. ALODIN
- [SDR HNAA2011111000377](https://openairdocs.org/sdr/HNAA2011111000377), Nov 10, 2011: SEAT TRACK. CORRODED. LT INBD SEAT TRACK CORRODED OUT OF LIMITS IAW RD8-53-4936 AT AFT CARGO FITTING ATTACH AREA. CUT SEAT TRACK IAW RD8-53-1599. INSTALLED NEW SPLICE SECTION OF SEAT
- [SDR HNAA2011111000376](https://openairdocs.org/sdr/HNAA2011111000376), Nov 10, 2011: FITTING. CORRODED. LIGHT CORROSION ON TENSION FITTING AT STR 31P AND STA X201.3. REMOVED CORROSION. ALODINED, PRIMED AND APPLIED CORROSION PREVENTITIVE COMPOUND IAW SRM 51-20-11.
- [SDR HNAA2011111000374](https://openairdocs.org/sdr/HNAA2011111000374), Nov 10, 2011: SEAT TRACK. CORRODED. CORROSION ON LT INBD SEAT TRACK AT STA X330.00. BLENDED AREA. FOUND TO BE OUT OF LIMITS IAW RD8-53-1339. R & R SEAT TRACK IAW DWG 85320490
- [SDR HNAA2011111000373](https://openairdocs.org/sdr/HNAA2011111000373), Nov 10, 2011: SEAT TRACK. CORRODED. LIGHT CORROSION ON LT INBD SEAT TRACK AT STA X360.00. R & R LT INBD SEAT TRACK.
- [SDR HNAA2011111000372](https://openairdocs.org/sdr/HNAA2011111000372), Nov 10, 2011: SEAT TRACK. CORRODED. LIGHT CORROSION ON LT INBD SEAT TRACK AT STA X455.00. BLENDED CORROSION AWAY IAW RD8-53-1339. FOUND TO BE WITHIN LIMITS. NDT'D AND NO CRACKS NOTED. ALODINED AND
- [SDR HNAA2011111000371](https://openairdocs.org/sdr/HNAA2011111000371), Nov 10, 2011: SEAT TRACK. CORRODED. LIGHT CORROSION ON LT INBD SEAT TRACK AT STA X488.00. BLENDED AWAY CORROSION TO WITHIN LIMITS OF RD8-53-1339. NDT'D AND NO CRACKS NOTED. ALODINED AND PRIMED.
- [SDR HNAA2011111000370](https://openairdocs.org/sdr/HNAA2011111000370), Nov 10, 2011: SEAT TRACK. CORRODED. LIGHT CORROSION ON LT INBD SEAT TRACK AT STA X501.00. BLENDED CORROSION AWAY WITHIN LIMITS OF RD8-53-1339. NDT AND NO CRACKS NOTED. ALODINE AND PRIMED.
- [SDR HNAA2011111000369](https://openairdocs.org/sdr/HNAA2011111000369), Nov 10, 2011: SEAT TRACK. CORRODED. LIGHT CORROSION ON LT INBD SEAT TRACK AT STA X519.00. BLENDED CORROSION AWAY WITHIN LIMITS OF RD8-53-1339. NDT AND NO CRACKS NOTED. ALODINED AND PRIMED.
- [SDR HNAA2011111000368](https://openairdocs.org/sdr/HNAA2011111000368), Nov 10, 2011: SEAT TRACK. CORRODED. LIGHT CORROSION ON LT OTBD SEAT TRACK AT STA X 539.00. BLENDED AREA OF CORROSION TO WITHIN LIMITS OF RD8-53-3644. ALODINED AND PRIMED.
- [SDR HNAA2011111000367](https://openairdocs.org/sdr/HNAA2011111000367), Nov 10, 2011: SEAT TRACK. CORRODED. LT INBD SEAT TRACK CORRODED AT SEVERAL SPOTS FROM STAX 201.3 THRU X 222.7. R & R SEAT TRACK.
- [SDR HNAA2011111000365](https://openairdocs.org/sdr/HNAA2011111000365), Nov 10, 2011: SEAT TRACK. CORRODED. CORROSION AT LT AND INBD SEAT TRACK FROM STA X251 THRU X 265. R & R SEAT TRACK.
- [SDR HNAA2011111000363](https://openairdocs.org/sdr/HNAA2011111000363), Nov 10, 2011: SEAT TRACK. CORRODED. CORROSION AT RT INBD SEAT TRACK AT STA X268.00. BLENDED AREA IAW RD8-53-1339. FOUND TO BE OUT OF LIMITS. R & R RT INBD FORWARD SEAT TRACK IAW DWG 85320079.
- [SDR HNAA2011111000362](https://openairdocs.org/sdr/HNAA2011111000362), Nov 10, 2011: SEAT TRACK. CORRODED. CORROSION AT RT INBD SEAT RAIL AT STA X280.00. BLENDED AREA TO WITHIN LIMITS IAW RD8-53-1339.
- [SDR HNAA2011111000360](https://openairdocs.org/sdr/HNAA2011111000360), Nov 10, 2011: SEAT TRACK. CORRODED. LIGHT CORROSION AT RT INBD AND OTBD SEAT TRACK AT STA X312.350. BLENDED AREAS TO WITHIN LIMITS IAW RD8-53-1339 FOR INBD AND RD8-53-1342 FOR OTBD.
- [SDR HNAA2011111000359](https://openairdocs.org/sdr/HNAA2011111000359), Nov 10, 2011: SEAT TRACK. CORRODED. LIGHT CORROSION AT RT INBD AND OTBD SEAT SEAT TRACK AT STA X330.00. BLENDED AREAS TO WITHIN LIMITS IAW RD8-53-1339 INBD AND RD8-53-1342 FOR OTBD.

All 103: https://openairdocs.org/deregistered/N816EX-2022-02-14/reports.md

## 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 20050119000869I](https://openairdocs.org/incident/20050119000869I), Jan 19, 2005: Dhav DHC8102 (N816EX), Pittsburgh, PA, Minor damage. (-23) Desk audit: on January 19, 2005, at approximately 2100 eastern standard time, a Dehavilland DHC-8-102, N816EX, flight number 3742 conducted under 14 CFR…
- [Incident 19990313016979I](https://openairdocs.org/incident/19990313016979I), Mar 13, 1999: Dhav DHC8102 (N816EX), Rochester, NY. (-5)On saturdy, March 13, 1999, at 1914 EST, a Dehavilland DHC-8-102, N816EX, flight 3944, operated by allegheny airlines, on departure from Rochester, new…
- [Incident 19980623017829I](https://openairdocs.org/incident/19980623017829I), Jun 23, 1998: Dhav DHC8102 (N816EX), Middletown, PA. Returned to MDT when landing gear was slow to retract. Hydraulic line was cracked.

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