# N914HA: 1986 Dehavilland DHC-8-102, registration cancelled 2019-04-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 8, 2019
- Status when cancelled: Valid registration
- Airframe: [Dehavilland DHC-8-102](https://openairdocs.org/model/dehavilland-dhc-8-102) (registry code 2809003)
- Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999)
- Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM) (OpenAirDocs)
- Serial number: 53
- Year built: 1986
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, transport
- Airworthiness date: November 13, 1986
- Certificate issued: September 11, 2017
- Last registry action: June 13, 2018
- Mode S code: ACA637
- 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/N914HA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=914HA
- Page: https://openairdocs.org/deregistered/N914HA-2019-04-08

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

## Service difficulty reports (190, newest 50)

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

- [SDR HNAA2015042700144](https://openairdocs.org/sdr/HNAA2015042700144), Apr 27, 2015: BATTERY PACK. INOPERATIVE. PASSENGER DOOR OVERHEAD EMERGENCY LIGHT IS OUT. R & R EMERGENCY LIGHT BATTERY 3351-PS1 IAW 33-51-00. OPS CHECKED GOOD.
- [SDR HNAA2015042700143](https://openairdocs.org/sdr/HNAA2015042700143), Apr 27, 2015: BATTERY PACK. INOPERATIVE. RIGHT EMERGENCY EGRESS LIGHT IS OUT. R & R EMERGENCY LIGHT BATTERY AT 3351-PS2 IAW MM 33-51-00. OPS CHECKED GOOD.
- [SDR HNAA2015030400076](https://openairdocs.org/sdr/HNAA2015030400076), Mar 4, 2015: BULB. INOPERATIVE. EMERGENCY CEILING LIGHT IS INOPERATIVE AT ROW 7. REMOVED LENS PANEL, R & R BULB. OPS CHECKED GOOD, REINSTALLED LIGHT LENS PANEL.
- [SDR HNAA2015010700006](https://openairdocs.org/sdr/HNAA2015010700006), Jan 7, 2015: AUTOFEATHER SYS. MALFUNCTIONED. REJECTED TAKEOFF, AUTO-FEATHER DID NOT ARM. AUTO-FEATHER TESTS NORMALLY. CYCLED POWER LEVERS. GROUND RAN ACFT. OPS CHECKED GOOD. AUTO-FEATHER ARMED AT 62 AND 63
- [SDR HNAA2014122300376](https://openairdocs.org/sdr/HNAA2014122300376), Dec 23, 2014: CONTROL WHEEL. BINDING. AFTER TAKEOFF, TRIMS WERE SET. TRIM WHEEL AND INDICATOR OPERATED NORMALLY, HOWEVER ACFT WAS FLYING TAIL HEAVY REGARDLESS OF TRIM SETTINGS. INSPECTED AND FOUND L
- [SDR HNAA2014110500305](https://openairdocs.org/sdr/HNAA2014110500305), Nov 5, 2014: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS ARE INOPERATIVE. R & R EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD.
- [SDR HNAA2014110500304](https://openairdocs.org/sdr/HNAA2014110500304), Nov 5, 2014: BULB. DIM. EMERGENCY EXIT LIGHT IS DIM AT ROW 4DF. R & R THE BULB. OPS CHECKED GOOD.
- [SDR HNAA2014102900303](https://openairdocs.org/sdr/HNAA2014102900303), Oct 29, 2014: BULB. INOPERATIVE. SIDEWALL EMERGENCY EXIT LIGHT HAS ONE BULB INOPERATIVE AT ROW 4. R & R THE BULB. OPS CHECKED GOOD.
- [SDR HNAA2014102900302](https://openairdocs.org/sdr/HNAA2014102900302), Oct 29, 2014: BULB. INOPERATIVE. EMERGENCY LIGHT INOPERATIVE. R & R THE BULB. OPS CHECKED GOOD.
- [SDR HNAA2014082700250](https://openairdocs.org/sdr/HNAA2014082700250), Aug 27, 2014: BULB. DIM. FORWARD RT EMERGENCY SIGN ABOVE EMERGENCY EXIT IS DIM. R & R BULBS. OPS CHECKED GOOD.
- [SDR HNAA201408100236](https://openairdocs.org/sdr/HNAA201408100236), Aug 15, 2014: INDICATOR. MALFUNCTIONED. NR 1 ENGINE OIL PRESSURE FLUCTUATED BETWEEN 80-100 PSI IN FLIGHT. INDICATION WENT TO MAX ON THE GROUND. PRESSURE REMAINED AT 40 PSI AFTER ENGINE SHUTDOWN. R & R
- [SDR HNAA2014063000194](https://openairdocs.org/sdr/HNAA2014063000194), Jun 30, 2014: LOCK. DEPLOYED. AFTER GEAR RETRACTION, LT, RT, AND NOSE DOOR AMBER LIGHT AND NOSE GREEN AND RED LIGHTS REMAINED ILLUMINATED. AFTER ALTERNATE EXTENSION, RED UNSAFE LIGHT WENT OU
- [SDR HNAA2014061800185](https://openairdocs.org/sdr/HNAA2014061800185), Jun 18, 2014: MONITOR. INOPERATIVE. AC POWER MONITOR IS BLANK. R & R AC POWER MONITOR IAW 24-29-05. OPS CHECKED GOOD.
- [SDR HNAA2014031400088](https://openairdocs.org/sdr/HNAA2014031400088), Mar 14, 2014: AUTOFEATHER SYS. MALFUNCTIONED. AUTOFEATHER DID NOT ARM DURING TAKEOFF ROLL, CYCLED CIRCUIT BREAKER Q4 NO FIX. GROUND RAN ACFT AND PERFORMED OPS CHECK OF AUTO FEATHER SYS IAW MANUAL. SYS OPERA
- [SDR HNAA2014010300654](https://openairdocs.org/sdr/HNAA2014010300654), Jan 3, 2014: CONTROLLER. MALFUNCTIONED. EMERGENCY LIGHTS CAME ON ENROUTE. RIGHT SECONDARY BUSS VOLTAGE STEADY AT 26.6 VOLTS. PROPELLER HEAT OFF. NO WARNING OR CAUTIONS. R & R EMERGENCY LIGHT CONTROL B
- [SDR HNAA2013123000645](https://openairdocs.org/sdr/HNAA2013123000645), Dec 29, 2013: RELAY. FAILED. AUTOFEATHER DID NOT ARM, DOES STATIC TEST OK. COULD NOT DUPLICATE. R & R RELAY 6121-K5 FOR TROUBLESHOOTING. GROUND RAN, OPS CHECKED GOOD AT THIS TIME.
- [SDR HNAA2013110600565](https://openairdocs.org/sdr/HNAA2013110600565), Nov 6, 2013: BULB. FAILED. FOURTH RED EMERGENCY FLOOR LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.
- [SDR HNAA2013102800552](https://openairdocs.org/sdr/HNAA2013102800552), Oct 28, 2013: BULB. INOPERATIVE. FLOOR EMERGENCY ESCAPE PATH LIGHT HAS ONE BULB INOPERATIVE AT ROW 1. R & R BULB. OPS CHECKED GOOD.
- [SDR HNAA2013091700499](https://openairdocs.org/sdr/HNAA2013091700499), Sep 15, 2013: INDICATOR. INACCURATE. FLAP POSITION INDICATOR READS 2.5 DEG W/ FLAP SELECTED TO ZERO. R & R FLAP POSITION INDICATOR IAW -8MM, 27-53-05. OPS CK GOOD.
- [SDR HNAA2013091000491](https://openairdocs.org/sdr/HNAA2013091000491), Sep 10, 2013: GROUND WIRE. BROKEN. AFTER TAKEOFF, ON GEAR RETRACTION, ALL GEAR REMAINED DOWN. ALL THREE GREEN, RED AND HANDLE LIGHTS REMAINED ILLUMINATED IAW CHECKLIST, SELECTED GEAR DOWN THEN HA
- [SDR HNAA2013091000490](https://openairdocs.org/sdr/HNAA2013091000490), Sep 10, 2013: WARNING LIGHT. MALFUNCTIONED. WHEN GEAR SELECTED UP, THE THREE GREEN LIGHTS STAYED ON AND THE THREE RED UNSAFE LIGHTS ILLUMINATED. AFTER APPROX 90 SECONDS, GEAR RETRACTED AND LIGHTS WENT OUT
- [SDR HNAA201307220419](https://openairdocs.org/sdr/HNAA201307220419), Jul 22, 2013: CONTROL HEAD. INTERMITTENT. NR 2 COMM HEAD BLANK AND INTERMITTENTLY SHOWS TEST MESSAGE ON SCREEN. R & R NR 2 COMM CONTROL HEAD. OPS CHECKED GOOD IAW MM 23-21-04.
- [SDR HNAA2013070500393](https://openairdocs.org/sdr/HNAA2013070500393), Jul 5, 2013: PUMP. MALFUNCTIONED. ON TAXI OUT TO RUNWAY, NR 2 STANDBY HOT CAUTION LIGHT ILLUMINATED. GOOD HYD QTY AND PRESSURE. SWAPPED NR 2 STANDBY HYD PUMP TO SPAR TEMP SENSOR IAW SP29.5. OPS 
- [SDR HNAA2013050300249](https://openairdocs.org/sdr/HNAA2013050300249), May 3, 2013: BULB. FAILED. EMERGENCY SIDEWALL LIGHTS ARE INOP AT ROW 4AC. REMOVED LENS. R & R ONE BULB. OPS CHECKED GOOD. REINSTALLED LENS.
- [SDR HNAA2013032900190](https://openairdocs.org/sdr/HNAA2013032900190), Mar 29, 2013: GENERATOR. SLOW. NR 1 AC GENERATOR IS SLOW TO COME ON LINE WHEN SELECTED ON WITH PROP AT 785. REQUIRES SEVERAL RESETS. COULD NOT DUPLICATE. GROUND RAN ACFT IAW RUN UP MANUAL. OK
- [SDR HNAA2013032600183](https://openairdocs.org/sdr/HNAA2013032600183), Mar 26, 2013: GENERATOR. WARNING LIGHT. RT AC BUSS CAUTION LIGHT ILLUMINATED AFTER NR 2 AC GENERATOR WAS BROUGHT ON LINE. CYCLED NR 2 AC GENERATOR. CAUTION LIGHT AND BUSS FAULT LIGHT WENT OUT. R & R N
- [SDR HNAA2013030100098](https://openairdocs.org/sdr/HNAA2013030100098), Mar 1, 2013: WIRE. CHAFED. F/A REPORTED EMERGENCY LIGHTS ILLUMINATED DURING CLIMBOUT FOR A FEW SECONDS AND REMAINED OFF FOR REST OF THE FLIGHT WITH NO OTHER ASSOCIATED LIGHTS. INSPECTED W
- [SDR HNAA2013022500091](https://openairdocs.org/sdr/HNAA2013022500091), Feb 25, 2013: CONTROL BOX. INTERMITTENT. ALL EMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY. MX INSPECTED BOTH BRUSH BLOCKS AND ADJACENT WIRE HARNESS. NO DEFECTS NOTED. GROUND RAN ACFT AND COULD NOT DUPLI
- [SDR HNAA2013020800036](https://openairdocs.org/sdr/HNAA2013020800036), Feb 8, 2013: LEAD. BURNED. EMERGENCY LIGHTS FLICKERED ON IN CRUISE FLIGHT WITH PROP HEAT ON. INSPECTED WIRING AND CHECKED RESISTANCE FOR NR 1 AND NR 2 BRUSH BLOCKS AND SLIP RINGS. CHECKED
- [SDR HNAA2013012500014](https://openairdocs.org/sdr/HNAA2013012500014), Jan 25, 2013: WIRE HARNESS. SATURATED. EMERGENCY LIGHTS FLICKERS WITH PROP HEAT ON. OK WITH OFF. OK AT 1050 NP. UNABLE TO DUPLICATE PROBLEM ON GROUND RUN. INSPECTED BOTH PROP BLADE LEADS CHECKED GOOD
- [SDR HNAA2013012500013](https://openairdocs.org/sdr/HNAA2013012500013), Jan 25, 2013: BRUSH BLOCK. INTERMITTENT. EMERGENCY LIGHTS FLICKER WITH PROP HEAT ON. OK AT 1050 NP. R & R NR 1 AND NR 2 BRUSH BLOCK ASSY'S IAW DASH 8 MM 61-10-11. GROUND RAN ACFT WITH NO DEFECTS NOTED.
- [SDR HNAA2013012500012](https://openairdocs.org/sdr/HNAA2013012500012), Jan 25, 2013: BRUSH BLOCK. DIRTY. ALL CABIN EMERGENCY LIGHTS FLICKERING, WHEN PROP AT 1050, OP HEAT ON AND PHASE 2A. EMERGENCY LIGHTS DO NOT FLICKER WHEN SELECTED TO 900. CLEANED AND INSPECTED P
- [SDR HNAA2013010401142](https://openairdocs.org/sdr/HNAA2013010401142), Jan 4, 2013: CONTROL CABLE. OUT OF ADJUST. ELEVATOR CONTROLS VERY SLOPPY AND DIFFICULT TO MAINTAIN PITCH ATTITUDE ON APPROACH AND LANDING. ADJUSTED ELEVATOR CABLE TENSIONS IAW MM 27-00-00. COMPLETED RII 
- [SDR HNAA2012122401130](https://openairdocs.org/sdr/HNAA2012122401130), Dec 24, 2012: BRUSH BLOCK. MALFUNCTIONED. EMERGENCY FLOOR LIGHT FLICKER DURING CLIMB OUT WITH ASSOCIATED WARNINGS. NR 2 AC GENERATOR VOLTS DROP ON "B" PHASE. INSPECTED NR 2 PROP R & R BRUSH BLOCK AND OP
- [SDR HNAA2012121901115](https://openairdocs.org/sdr/HNAA2012121901115), Dec 19, 2012: CONTROLLER. INTERMITTENT. EMERGENCY LIGHTS FLICKER WITH NR 2 PROP A PHASE ACTIVE. R & R EMERGENCY CONTROL BOX IAW -8 MM 33-51-00. GROUND RAN ACFT. OPS CHECKED GOOD.
- [SDR HNAA2012112701074](https://openairdocs.org/sdr/HNAA2012112701074), Nov 27, 2012: SWITCH. SHORTED. EMERGENCY LIGHTS FLICKERED ON CLIMBOUT WITH PROP HEAT AND IGNITERS ON. LIGHTS DID NOT FLICKER DURING CRUISE OR IN DECENT. R & R F/A EMERGENCY LIGHT SWITCH. SYS 
- [SDR HNAA2012112101063](https://openairdocs.org/sdr/HNAA2012112101063), Nov 21, 2012: BRUSH BLOCK. UNKNOWN. EMERGENCY LIGHTS FLICKERED ON CLIMBOUT WITH NR 2 PROPELLER A PHASE. REMOVED FWD UPPER COWL PANEL ON NR 2 ENGINE. INSPECTED BRUSH BLOCK ASSY SLIP RINGS AND HEATE
- [SDR HNAA2012111201036](https://openairdocs.org/sdr/HNAA2012111201036), Nov 12, 2012: BULB. FAILED. EMERGENCY LIGHT IS INOPERATIVE. REMOVED PLASTIC COVERING. R & R BULB. REINSTALLED PLASTIC COVERING. OPS CHECKED GOOD.
- [SDR HNAA2012081700921](https://openairdocs.org/sdr/HNAA2012081700921), Aug 17, 2012: BULB. FAILED. EMERGENCY FLOOR RED LIGHT IS INOPERATIVE AT ROW 1. REMOVED LENS, REMOVED AND REPLACED BULB. OPS CHECKED GOOD.
- [SDR HNAA2012060400814](https://openairdocs.org/sdr/HNAA2012060400814), Jun 4, 2012: HMU. FAILED. DURING TAKEOFF, NR 1 POWER LEVER HAD 2 KNOB SPLIT. WHEN SWITCH SET TO NORM, THE NR 1 ENGINE TORQUE SURGED TO 96 PERCENT MOMENTARILY, THEN DROPPED TO 80 PERCENT.
- [SDR HNAA2012043000758](https://openairdocs.org/sdr/HNAA2012043000758), Apr 30, 2012: CONTACTOR. INOPERATIVE. EMERGENCY LIGHTS FLICKERED INFLIGHT. R & R 2431-K18 SECONDARY BUSS CONTACTOR IAW STD PRACTICES, OPS CHECKED GOOD
- [SDR HNAA2012042007401](https://openairdocs.org/sdr/HNAA2012042007401), Apr 20, 2012: CONTROL BOX. MALFUNCTIONED. EMERGENCY LIGHTS FLICKERED THE ENTIRE FLIGHT. ALL FLOOR EMERGENCY AND ROW 1DF LOWER EXIT SIGN. R & R NR 2 BRUSH BLOCK. OPS CHECKED GOOD IAW MM 30-61-00. R & R E
- [SDR HNAA2012030200631](https://openairdocs.org/sdr/HNAA2012030200631), Mar 2, 2012: HYDRAULIC SYSTEM. DISCHARGED. LOSS OF NR 2 HYD FLUID IN FLIGHT. PRESSURE AT ZERO FOR MORE THAN 20 MINUTES. NR 1 HYD QUANITY DROPPED TO ZERO WHEN PARK BRAKE APPLIED. ACFT WAS BEING POSITION F
- [SDR HNAA2011120100411](https://openairdocs.org/sdr/HNAA2011120100411), Dec 1, 2011: BRUSH BLOCK. FAILED. EMERGENCY LIGHTS FLICKERED DURING CLIMB. R & R NR1 AND NR 2 PROP BRUSH BLOCK IAW MM 61-10-11. COMPLIED WITH WORKCARD 33-50-03Q. EMERGENCY LIGHT SYS OPS CHECKED 
- [SDR HNAA2011120100409](https://openairdocs.org/sdr/HNAA2011120100409), Dec 1, 2011: CONTROL BOX. FAILED. FLOOR EMERGENCY LIGHTS FLICKERED DURING CLIMB OUT. R & R LIGHT CONTROL BOX IAW WORKCARD 33-50-03Q.
- [SDR HNAA2011081700254](https://openairdocs.org/sdr/HNAA2011081700254), Aug 12, 2011: UNKNOWN. ODOR. STRONG ODOR IN COCKPIT IN FLIGHT. CYCLED BLEEDS OFF, NO DIFFERENCE NOTED (NO ODOR IN CABIN). INSPECTED ACFT FOR ODORS, NONE FOUND. INSPECTED AVIONICS RACK, TRU'
- [SDR HNAA2011072600223](https://openairdocs.org/sdr/HNAA2011072600223), Jul 26, 2011: MODULE. INOPERATIVE. MIDCABIN FLOOR EMERGENCY LIGHT AT ROW 2DF WILL NOT ILLUMINATE. INSTALLED NEW LIGHT MODULE AS REQUIRED.
- [SDR HNAA2011072600222](https://openairdocs.org/sdr/HNAA2011072600222), Jul 25, 2011: SPLICE. FAILED. RIGHT FORWARD EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE. FOUND DIODED MATRIX SPLICE 3352-CR6 BROKEN. R & R DIODED. EXIT LIGHT OPERATED NORMALLY ON GROUND.
- [SDR HNAA2011071400210](https://openairdocs.org/sdr/HNAA2011071400210), Jul 8, 2011: PANEL. CORRODED. PANEL 622AT HAS PITTING IN MARKED COUNTERSINKS. REMOVED PITTING IAW RD8-57-1686.
- [SDR HNAA20110400209](https://openairdocs.org/sdr/HNAA20110400209), Jul 8, 2011: PANEL. CORRODED. PANEL 523AT HAS PITTING IN NUMEROUS COUNTERSINKS. REMOVED PITTING IAW RD8-57-1686.

All 190: https://openairdocs.org/deregistered/N914HA-2019-04-08/reports.md

## 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.

- [Incident 20031113035869I](https://openairdocs.org/incident/20031113035869I), Nov 13, 2003: Dhav DHC8102 (N914HA), Charlottesville, VA, Minor damage. (-23) Aircraft landed hard due to gusty wind and turbulence. Damage to landing gear and fuselage sustained.

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