# N935HA: Boeing Of Canada/Dehav Div DHC-8-102, registration cancelled 2021-04-05

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 5, 2021
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing Of Canada/Dehav Div DHC-8-102](https://openairdocs.org/model/boeing-of-canada-dehav-div-dhc-8-102) (registry code 1385303)
- 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: 142
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: March 30, 1989
- Certificate issued: December 11, 2017
- Last registry action: June 15, 2018
- Mode S code: ACF8EC
- Owner when cancelled: [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%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/N935HA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=935HA
- Page: https://openairdocs.org/deregistered/N935HA-2021-04-05

From the FAA registry file of November 5, 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/Dehav Div DHC-8-102: https://openairdocs.org/model/boeing-of-canada-dehav-div-dhc-8-102.md

## Service difficulty reports (86, newest 50)

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

- [SDR HNAA2017011600021](https://openairdocs.org/sdr/HNAA2017011600021), Jan 16, 2017: PRESSURE SWITCH. MALFUNCTIONED. NR 2 ENGINE HYDRAULIC PUMP CAUTION LIGHT FLICKERED, TRIGGERING MASTER CAUTION P.T.R. BOTH MAIN SYSTEM PRESSURES ARE NORMAL. NR 2 HYDRAULIC CAUTION LIGHT DEACTIV
- [SDR HNAA2017011300017](https://openairdocs.org/sdr/HNAA2017011300017), Jan 13, 2017: POWER SUPPLY. INOPERATIVE. FORWARD EMERGENCY EXIT CEILING LIGHT IS INOPERATIVE AT ROW 1AC. REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK. OPS CHECKED GOOD.
- [SDR HNAA2016103100344](https://openairdocs.org/sdr/HNAA2016103100344), Oct 31, 2016: BULB. INOPERATIVE. SECOND FROM FRONT, FLOOR EMERGENCY EXIT LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE BULB. REINSTALLED PROTECTIVE COVER. OPS CHECKED GOOD.
- [SDR HNAA2016081100245](https://openairdocs.org/sdr/HNAA2016081100245), Aug 10, 2016: CIRCUIT BREAKER. TRIPPED. NR 1 STANDBY PUMP CIRCUIT BREAKER TRIPPED. RESET THE CIRCUIT BREAKER. GROUND RAN ACFT AND OPERATED SYSTEMS. SYSTEMS OPS NORMAL.
- [SDR HNAA2016081000243](https://openairdocs.org/sdr/HNAA2016081000243), Aug 8, 2016: ROD. OUT OF ADJUST. LEFT AMBER GEAR LIGHT CONTINUES TO FLICKER ON & OFF AFTER TAKEOFF. PERFORMED SEVERAL GEAR SWINGS. FOUND FWD DOOR SAGGING. ADJUSTED ROD END ON FWD GEAR DOOR. DID
- [SDR HNAA2016081100244](https://openairdocs.org/sdr/HNAA2016081100244), Jul 20, 2016: PROXIMITY SWITCH. INOPERATIVE. CLOSE WOW C/L ILLUMINATED AT 14,000 FT. NO INDICATION ON LANDING GEAR SELECT PANEL. TRANSCRIBED TO HA300 SEQ 5 ON 20JUL16 WORK PACKAGE INSPECTED WOW PROXIMITY S
- [SDR HNAA2016071800222](https://openairdocs.org/sdr/HNAA2016071800222), Jul 17, 2016: BULB. INOPERATIVE. 15TH FLOOR EMERGENCY LIGHT INOPERATIVE. R & R THE BULB.
- [SDR HNAA2016031600086](https://openairdocs.org/sdr/HNAA2016031600086), Mar 18, 2016: BULB. INOPERATIVE. FLOOR EMERGENCY LIGHTS ARE INOPERATIVE AT ROWS 1, 5 AND 9. R & R BULBS AND ROWS 1, 5 AND 9. OPS CHECKED GOOD.
- [SDR HNAA2016030400071](https://openairdocs.org/sdr/HNAA2016030400071), Mar 4, 2016: SUPPORT BRACKET. CORRODED. NR 4 LT, INBD FLAP TRACK SUPPORT BRACKET HAS PITTING ON CAVITY FACE. R & R NR 4 FLAP TRACK SUPPORT BRACKET IAW MM 57-50-42.
- [SDR HNAA2016030400070](https://openairdocs.org/sdr/HNAA2016030400070), Mar 4, 2016: FLAP TRACK. CORRODED. CORROSION ON LT WING, NR 4 FLAP TRACK, INBD SIDE, BEHIND THE TRACK SUPPORT BRACKET. R & R NR 4 FLAP TRACK IAW MM57-50-42.
- [SDR HNAA2015112500351](https://openairdocs.org/sdr/HNAA2015112500351), Nov 25, 2015: SWITCH. OUT OF ADJUST. ON TAKEOFF ROLL, INBD AND OTBD GROUND SPOILER CAUTION LIGHTS ILLUMINATED. SPOILERS DID NOT MOVE. INSPECTED AND FOUND MICROSWITCH 2761 IS OUT OF ADJUSTMENT. RIGG
- [SDR HNAA2015111300337](https://openairdocs.org/sdr/HNAA2015111300337), Nov 13, 2015: SKIN. DEBONDED. DISBOND DISCOVERED AT BS 467 TO 488, STR 32S TO STR 32P. PREVIOUS REPAIRED USING EO8-53-11-0651. REMOVED BOTTOM SKIN SECTION BS X424 TO BS X488.50, STR 32S TO S
- [SDR HNAA2015102300310](https://openairdocs.org/sdr/HNAA2015102300310), Oct 23, 2015: SKIN. CORRODED. MAINTENANCE FOUND SKIN AROUND MARKER BEACON ATENNA CORRODED AND DISBONDED. BOTTOM SKIN SECTION WAS REMOVED FROM BS 434.124 - 488.50, STR 29P TO 29C. SEALED, PRI
- [SDR HNAA2015042700145](https://openairdocs.org/sdr/HNAA2015042700145), Apr 27, 2015: BULB. INOPERATIVE. FLOOR EMERGENCY EXIT SIGN HAD BULBS OUT AT ROWS 4AC AND 4DF. R & R BULBS A ROW 4AC AND 4DF EMERGENCY EXIT FLOOR SIGN. OPS CHECKED GOOD.
- [SDR HNAA2015041500134](https://openairdocs.org/sdr/HNAA2015041500134), Apr 15, 2015: BULB. INOPERATIVE. ROW 1 FLOOR PATH EMERGENCY LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.
- [SDR HNAA2015041500133](https://openairdocs.org/sdr/HNAA2015041500133), Apr 15, 2015: BULB. INOPERATIVE. ROW 4AC SIDEWALL EMERGENCY LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.
- [SDR HNAA2015041500131](https://openairdocs.org/sdr/HNAA2015041500131), Apr 15, 2015: GCU. MALFUNCTIONED. RIGHT A/C BUSS CAUTION LIGHT ILLUMINATED IN FLIGHT. R & R NR 2 AC GEN AND GCU IAW WC 24-20-11R. GROUND RAN ACFT. OPS CHECKED GOOD.
- [SDR HNAA2015040100114](https://openairdocs.org/sdr/HNAA2015040100114), Apr 1, 2015: SWITCH. FAILED. AFTER TAKEOFF AND CREW SELECTED FLAPS O ZERO, FLAP INDICATOR REMAINED AT 5 DEGREES. NO ASSOCIATED CAUTION LIGHTS ON THE GROUND. FLAPS APPEAR TO BE 5 DEGREES. TR
- [SDR HNAA2014121900373](https://openairdocs.org/sdr/HNAA2014121900373), Dec 19, 2014: BULB. DIM. LEFT AFT EXTERIOR EMERGENCY LIGHT IS DIM. R & R THE BULB. OPS CHECKED GOOD.
- [SDR HNAA2014111800330](https://openairdocs.org/sdr/HNAA2014111800330), Nov 19, 2014: SENSOR. FAILED. WOW CAUTION LIGHT ILLUMINATED ON GEAR RETRACTION. REMAINED ON FOR ENTIRE FLIGHT. EXTINGUISHED ON LANDING. CHECKED PSEU MEMORY. FAULT CODE FOR RT NLG SENSOR. SEN
- [SDR HNAA2014100800284](https://openairdocs.org/sdr/HNAA2014100800284), Oct 8, 2014: CONTROL PANEL. MALFUNCTIONED. NAVAGATION SWITCH ANNUNCIATION 2 CIRCUIT BREAKER TRIPPED, AUTO PILOT DISENGAGE ADVANCE LIGHT ILLUMINATED, F/O FLIGHT DIRECTOR FLAGGED. RETURN TO GATE. R & R GC8
- [SDR HNAA2014090800259](https://openairdocs.org/sdr/HNAA2014090800259), Sep 8, 2014: TRANSCEIVER. FAILED. WEATHER RADAR DID NOT PAINT. R & R WEATHER RADAR R/T. OPS CHECKED GOOD IAW 34-41-04 AND BUL. 34-18.
- [SDR HNAA2014081300234](https://openairdocs.org/sdr/HNAA2014081300234), Aug 13, 2014: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT BATTERY INOPERATIVE. R & R BATTERY IAW WC 33-50-05R.
- [SDR HNAA2014042400137](https://openairdocs.org/sdr/HNAA2014042400137), Apr 24, 2014: WIRE. BROKEN. NR 2 ENGINE OIL PRESSURE FLUXUATED BETWEEN 50-60 PSI DURING CRUISE FLIGHT. REDUCE POWER, PRESSURE STABILIZES AT 50 PSI. SWAPPED GAUGES, NO FIX. FOUND BROKEN WIR
- [SDR HNAA2014032400104](https://openairdocs.org/sdr/HNAA2014032400104), Mar 24, 2014: TRANSMITTER. FAILED. NR 2 ENGINE OIL PRESSURE AT 48 PSI. R & R OIL PRESSURE TRANSMITTER IAW MM 79-36-03. OPS AND LEAKED CHECKED GOOD.
- [SDR HNAA2014031900094](https://openairdocs.org/sdr/HNAA2014031900094), Mar 19, 2014: LEAD. DAMAGED. EMERGENCY LIGHTS FLICKERED DURING CLIMBOUT, CYCLED EMERGENCY LIGHT CONTROL SWITCH AND OPS CHECKED NOMAL. INSPECTED AND FOUND BAD PROPELLER LEAD ON NR 2 PROP, NR
- [SDR HNAA2014031000080](https://openairdocs.org/sdr/HNAA2014031000080), Mar 10, 2014: BRUSH BLOCK. MALFUNCTIONED. EMERGENCY LIGHTS FLICKERS ON & OFF INFLIGHT. R & R NR 1 ENGINE BRUSH BLOCK IAW MM 61-10-11. OPS CHECKED GOOD. THE AC CONTACTOR BOXES WERE INSPECTED AND NO DEFEC
- [SDR HNAA2014031000079](https://openairdocs.org/sdr/HNAA2014031000079), Mar 10, 2014: CONTROL BOX. MALFUNCTIONED. EMERGENCY LIGHTS FLICKER ON & OFF INFLIGHT. R & R EMERGENCY LIGHT CONTROL BOX. OPS CHECKED GOOD AT THIS TIME. OK FOR SERVICE.
- [SDR HNAA2014022400054](https://openairdocs.org/sdr/HNAA2014022400054), Feb 24, 2014: BRUSH BLOCK. FAILED. RT AC BUSS FAILURE IN FLIGHT WITH ASSOCIATED CAUTION LIGHTS. GROUND RAN ACFT. COULD NOT DUPLICATE. INSPECTED NR 2 AC CONTACTOR BOX WIRING. NO DISCREPANCES NOTED
- [SDR HNAA2014021200040](https://openairdocs.org/sdr/HNAA2014021200040), Feb 12, 2014: DADC. FAILED. BOTH TRANSPONDERS ARE INOPERATIVE. R & R NR 1 DADC. SYSTEM CHECKS GOOD IAW AMM 34-12-02 AND SB 34-68.
- [SDR HNAA2014021200039](https://openairdocs.org/sdr/HNAA2014021200039), Feb 12, 2014: ADI. FAILED. STANDBY ATTITUDE INDICATOR DID NOT FUNCTION PROPERLY. SLOWLY ROLLS INTO LT BANK AND NOSE DOWN ATTITUDE. R & R STANDBY ADI. OPS CHECKED GOOD IAW 34-22-00.
- [SDR HNAA2014020500034](https://openairdocs.org/sdr/HNAA2014020500034), Feb 5, 2014: THRESHOLD. CORRODED. PAX DOOR THRESHOLD SURFACE IS CORRODED. R & R PAX DOOR THRESHOLD IAW SRM 53-00-16.
- [SDR HNAA2014020500033](https://openairdocs.org/sdr/HNAA2014020500033), Feb 5, 2014: ANGLE. CORRODED. PAX DOOR STAIR FORWARD UPPER INSIDE ANGLE IS CORRODED. R & R PAX DOOR STAIR FWD UPPER ANGLE.
- [SDR HNAA2014020500032](https://openairdocs.org/sdr/HNAA2014020500032), Feb 5, 2014: BRACKET. CRACKED. RT FRONT SPAR TEE DUCT LOWER BRACKET IS CRACKED. REMOVED ANGLE BRACKET.
- [SDR HNAA2014020500031](https://openairdocs.org/sdr/HNAA2014020500031), Feb 5, 2014: BRACKET. CRACKED. FRONT SPAR TEE DUCT LT UPPER BRACKET IS CRACKED. R & R ANGLE BRACKET.
- [SDR HNAA2013121100615](https://openairdocs.org/sdr/HNAA2013121100615), Dec 11, 2013: BULB. INOPERATIVE. CEILING EMERGENCY LIGHT AT ROW 8 IS INOPERATIVE. REMOVED LENS, R & R BULB, REINSTALLED LENS. OPS CHECKED GOOD.
- [SDR HNAA2013121100614](https://openairdocs.org/sdr/HNAA2013121100614), Dec 11, 2013: BULB. DIM. LEFT AFT EXTERIOR FUSELAGE EMERGENCY LIGHT IS DIM. REMOVED LENS, R & R BULB, AT SAID LOCATION, REINSTALLED LENS. OPS CHECKED GOOD.
- [SDR HNAA2013112500591](https://openairdocs.org/sdr/HNAA2013112500591), Nov 25, 2013: BLEED AIR SYS. SMOKE. APU BLEED AIR CAUSED SMOKE IN CABIN, CLEARED WHEN APU BLEED SELECTED OFF. NO SMOKE OFF ENGINE BLEEDS. APU BLEED AIR.
- [SDR HNAA2013081900470](https://openairdocs.org/sdr/HNAA2013081900470), Aug 19, 2013: SOCKET. FAILED. OVERHEAD LIGHT AT ROW 8 IS INOPERATIVE. REMOVED PANEL, FOUND MELTED SOCKET, R & R SOCKET AND BALLAST. REINSTALLED PANEL. OPS CHECKED GOOD IAW CMM 33-21-19.
- [SDR HNAA2013080900457](https://openairdocs.org/sdr/HNAA2013080900457), Aug 9, 2013: BULB. INOPERATIVE. EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT ROW 3. R & R BULB. OPS CHECKED GOOD IAW MM 33-51-11.
- [SDR HNAA2013080900455](https://openairdocs.org/sdr/HNAA2013080900455), Aug 9, 2013: SMOKE DETECTOR. FALSE ACTIVATION. CARGO BAY SMOKE DETECTION WARNING LIGHT ILLUMINATED FOR ABOUT FIVE SECONDS AND EXTINGUISHED. CARGO DOOR WAS OPEN BOTH SYS TESTED NORMAL. R & R FORWARD SMOKE DET
- [SDR HNAA2013062600360](https://openairdocs.org/sdr/HNAA2013062600360), Jun 26, 2013: CLAMP. LOOSE. LOW AIRFLOW AND HOT RECIRCULATION AIR TEMP, CABIN TOO HOT FOR ENTIRE FLIGHT WITH DUCT TEMP OF 10. COCKPIT IS NORMAL. INSPECTED AFT CABIN AND BAG BAY, NO LEAKS F
- [SDR HNAA2013051000262](https://openairdocs.org/sdr/HNAA2013051000262), May 10, 2013: STRUCTURE. DAMAGED. ACFT STRUCK BY LIGHTNING, ENROUTE.
- [SDR HNAA2013041700227](https://openairdocs.org/sdr/HNAA2013041700227), Apr 15, 2013: LAMP. BURNED OUT. EMERGENCY EXIT CEILING LIGHT AT ROW 7 IS INOPERATIVE. RELAMPED EMERGENCY CEILING LIGHT AT ROW 7 SECURED COVER USING ATTACHED HARDWARE, OPS CHECK GOOD.
- [SDR HNAA2013040100194](https://openairdocs.org/sdr/HNAA2013040100194), Apr 1, 2013: BULB. INOPERATIVE. ONE EMERGENCY FLOOR LIGHT IS INOPERATIVE UNDER ROW 9. R & R BULB. REINSTALLED LIGHT ASSY IN FLOOR TRACK. RESECURED WITH CLEAR STRIP.
- [SDR HNAA2013021100049](https://openairdocs.org/sdr/HNAA2013021100049), Feb 11, 2013: BULB. MALFUNCTIONED. FORWARD AFT EMERGENCY SIGN LIGHT IS DIM. REMOVED BULBS AT LOWER RT EMERGENCY SIGNS. OPS CHECKED GOOD.
- [SDR HNAA2012122101124](https://openairdocs.org/sdr/HNAA2012122101124), Dec 21, 2012: BULB. FAILED. FORWARD MOST FLOOR PATH EMERGENCY LIGHT IS INOPERATIVE. R & R BULB, OPS CHECKED GOOD. REINSTALLED FLOOR COVER.
- [SDR HNAA2012121201100](https://openairdocs.org/sdr/HNAA2012121201100), Dec 12, 2012: BULB. FAILED. DRIFT WALL NEAR F/A SEAT HAS 2 EMERGENCY LIGHTS INOPERATIVE. REMOVED LENS, R & R 2 BULBS. REINSTALLED LENS. OPS CHECKED GOOD.
- [SDR HNAA2012110501032](https://openairdocs.org/sdr/HNAA2012110501032), Nov 2, 2012: CONNECTOR. DAMAGED. EMERGENCY LIGHTS COME ON WHEN SELECTED OFF WHEN CYCLING APU GEN OFF TO ON. ALSO COME ON WHEN SHUTTING ENG DOWN POSITIONED SPADE CONNECTOR ON WIRE 4D22 AT BACK S
- [SDR HNAA2012092600978](https://openairdocs.org/sdr/HNAA2012092600978), Sep 26, 2012: ACTUATOR. FAILED. NR 1 HYD SYS LOSS OF CONTENTS AND FAILURE ON LANDING. RUDDER ISOLATION VALVE CAUTION LIGHT ILLUMINATED. R & R RT INBD SPOILER ACTUATOR IAW AMM 27-14-05. FUNCTIO

All 86: https://openairdocs.org/deregistered/N935HA-2021-04-05/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA01MA056](https://openairdocs.org/ntsb/DCA01MA056), Aug 5, 2001: de Havilland Dash 8-100 (N935HA), Washington, DC, minor damage, 1 fatal. Probable cause: The ramp agent's impaired performance due to his hyperthyroidism, which was exacerbated by the heat and was inadequately controlled by medication, and possibly also due to the use of an antianxiety…

## 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.

- [Accident 20010805022819A](https://openairdocs.org/incident/20010805022819A), Aug 5, 2001: N935HA, Washington, DC, No damage. (-23) During the marshalling process, a ramp agent removed chocks from front tires. When it was apparent chocks would interfere with main tires, ramp agent…

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