# N934HA: Boeing DHC-8-102, registration cancelled 2017-08-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 23, 2017
- Status when cancelled: Second renewal notice
- Airframe: [Boeing DHC-8-102](https://openairdocs.org/model/boeing-dhc-8-102) (registry code 1386002)
- 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: 139
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: March 10, 1989
- Certificate issued: August 1, 2014
- Last registry action: January 30, 2015
- Mode S code: ACF535
- 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/N934HA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=934HA
- Page: https://openairdocs.org/deregistered/N934HA-2017-08-23

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 Boeing DHC-8-102: https://openairdocs.org/model/boeing-dhc-8-102.md

## Service difficulty reports (80, newest 50)

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

- [SDR HNAA2015020600034](https://openairdocs.org/sdr/HNAA2015020600034), Feb 5, 2015: INDICATOR. MALFUNCTIONED. REJECTED T/O DUE TO NR 2 PROPELLER REACHED 1243 RPM FOR APPROX 5-10 SEC. R &R NR 2 PROP INDICATOR & NR 2 NP PROBE AS REQUIRED. R & R NR 2 HORSECOLLAR PANEL. RAN
- [SDR HNAA2013052000299](https://openairdocs.org/sdr/HNAA2013052000299), May 18, 2013: LANDING GEAR. MALFUNCTIONED. LT MAIN GEAR FAILED TO EXTEND WHEN SELECTED, ACFT PERFORMED EMERGENCY GEAR UP LANDING.
- [SDR HNAA2013042600236](https://openairdocs.org/sdr/HNAA2013042600236), Apr 26, 2013: SEAL. LEAKING. WITH APU RUNNING, WITHOUT GROUND POWER UNIT, ELECTRICAL BURNING ODOR AND SMOKE COMING FROM CARGO BAY / APU AREA. INSPECTED AND FOUND APU STARTEF GENERATOR TO BE
- [SDR HNAA201304220023](https://openairdocs.org/sdr/HNAA201304220023), Apr 22, 2013: CONNECTOR. CORRODED. RADAR DOES NOT PAINT WEATHER OR GROUND. RADAR DISPLAY SPOKES, FOUND CORROSION IN CONNECTOR 3441-P1001. R & R CONNECTOR IAW MM 20-45-06
- [SDR HNAA2013041700222](https://openairdocs.org/sdr/HNAA2013041700222), Apr 16, 2013: BULB. BURNED OUT. ROW 7 EMERGENCY LIGHT INOPERATIVE. R & R BULB.
- [SDR HNAA2013030600110](https://openairdocs.org/sdr/HNAA2013030600110), Mar 6, 2013: INDICATOR. INOPERATIVE. NR 1 TORQUE GAUGE ANOLOG AND DIGITAL DID NOT GO ABOVE 10 PERCENT. CLEANED CONNECTOR ON TSCU. R & R NR 1 TORQUE INDICATOR. OPS CHECKED GOOD ON THE GROUND RUN, IA
- [SDR HNAA2013030400105](https://openairdocs.org/sdr/HNAA2013030400105), Mar 4, 2013: BULB. FAILED. SIDEWALL EMERGENCY LIGHTS ARE DIM AT ROWS 1DF AND 4AC. R & R BURNED BULB IN SIDEWALL EMERGENCY LIGHTS. OPS CHECKED GOOD.
- [SDR HNAA2013030400104](https://openairdocs.org/sdr/HNAA2013030400104), Mar 4, 2013: BULB. FAILED. RT AFT FUSELAGE EMERGENCY LIGHT IS INOPERATIVE. R & R BULB IN RT AFT FUSELAGE EMERGENCY LIGHT. OPS CHECKED GOOD.
- [SDR HNAA2013030100100](https://openairdocs.org/sdr/HNAA2013030100100), Mar 1, 2013: BULB. FAILED. LOWER LEVEL EMERGENCY EXIT LIGHT IS INOPERATIVE AT ROW 2 AND ROW 4. R & R EMERGENCY LIGHT BULB IAW 33-51-00.
- [SDR HNAA2013022500093](https://openairdocs.org/sdr/HNAA2013022500093), Feb 25, 2013: BULB. FAILED. 17TH AND 21ST FLOOR EMERGENCY LIGHTS ARE INOPERATIVE. R & R BULBS IN FLOOR EMERGENCY LIGHTS. OPS CHECKED GOOD.
- [SDR HNAA2013022500092](https://openairdocs.org/sdr/HNAA2013022500092), Feb 25, 2013: BULB. INOPERATIVE. LAST CEILING EMERGENCY LIGHT IS INOPERATIVE. R & R EMERGENCY CEILING LIGHT, OPS CHECKED GOOD.
- [SDR HNAA2013020100030](https://openairdocs.org/sdr/HNAA2013020100030), Feb 1, 2013: LIGHT. OUT OF POSITION. EMERGENCY FLOOR LIGHT MODULE IS OFF POSITION AT ROW 9. POSITIONED EMERGENCY FLOOR LIGHT MODULE AT ROW 9.
- [SDR HNAA2012112901077](https://openairdocs.org/sdr/HNAA2012112901077), Nov 29, 2012: BULB. FAILED. ROW TWO CEILING EMERGENCY LIGHT IS INOPERATIVE. R & R BULB.
- [SDR HNAA2012100901004](https://openairdocs.org/sdr/HNAA2012100901004), Oct 9, 2012: TORQUE SENSOR. FAILED. DURING TAKEOFF, NR 2 TORQUE INDICATOR BOTH DIGITAL AND ANOLOG, DID NOT SHOW AN INCREASE. R & R NR 2 TORQUE INDICATOR IAW AMM 77-10-00. INSPECTED ASSOCIATED CONN
- [SDR HNAA2012062700836](https://openairdocs.org/sdr/HNAA2012062700836), Jun 27, 2012: BULB. FAILED. CEILING EMERGENCY LIGHT IS INOPERATIVE AT ROW 2. R & R EMERGENCY LIGHT BULB AT ROW 2. OPS CHECKED GOOD.
- [SDR HNAA2012051100771](https://openairdocs.org/sdr/HNAA2012051100771), May 11, 2012: ENGINE. SURGES. NR 1 ENGINE TORQUE SURGED ON TAKEOFF ROLL UP TO 99 PERCENT. R & R NR 1 ENGINE HMU AND FUEL PUMP IAW 73-20-01. GROUND RAN ACFT IAW SRT MANUAL. OPS CHECKED GOOD.
- [SDR HNAA2012042300745](https://openairdocs.org/sdr/HNAA2012042300745), Apr 23, 2012: INDICATOR. FLUCTUATES. ABORTED TAKEOFF DUE TO NR 1 ENGINE TORQUE FLUX 20-40-PERCENT. OTHER PARAMETERS NORMAL. R & R NR 1 TORQUE INDICATOR IAW MM 77-10-00. GROUND RAN ACFT. OPS CHECKED
- [SDR HNAA2012033000712](https://openairdocs.org/sdr/HNAA2012033000712), Mar 30, 2012: BULB. FAILED. RT FWD EMERGENCY EXIT SIGN HAS BULB INOPERATIVE. R & R BULB. OPS CHECKED GOOD.
- [SDR HNAA2012030700674](https://openairdocs.org/sdr/HNAA2012030700674), Mar 7, 2012: CHECK VALVE. FAILED. WITH BOTH ENGINES SHUTDOWN AND APU BLEEDS OFF. DEICE PRESSURE SHOWS 24 PSI AND BOOTS STILL INFLATED. R & R APU LINK UP PRESSURIZATION CHECK VALVE. RAN APU DEICE
- [SDR HNAA2011110200344](https://openairdocs.org/sdr/HNAA2011110200344), Oct 29, 2011: OIL SYSTEM. LOW. NR 1 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL. LIGHT EXTINGUISHED AFTER ABORTED TAKEOFF. CLEANED OIL PRESSURE SWITCH AND TRANSDUCER. FOUND 
- [SDR HNAA2011091900292](https://openairdocs.org/sdr/HNAA2011091900292), Sep 15, 2011: BULB. FAILED. LT AFT EMERGENCY LIGHT DIM. R & R BULB.
- [SDR HNAA2011091900289](https://openairdocs.org/sdr/HNAA2011091900289), Sep 14, 2011: SELECTOR PANEL. FAILED. PRESSURIZATION FAULT LIGHT ON. WILL NOT GO OUT. R & R CABIN PRESSURE SELECTOR PANEL. OPS CHECKED GOOD IAW MM 21-30-07. CLEARED MEL. REVERSED SP21-1 OUTFLOW RETU
- [SDR HNAA2011071400213](https://openairdocs.org/sdr/HNAA2011071400213), Jul 11, 2011: CONTROLLER. MALFUNCTIONED. ACFT DID NOT PRESSURIZE DURING CLIMBOUT AND NR 1 TRANSPONDER, F/O ALT, F/O IVSI FAILED. MX R & R NR 2 BLEED OVERTEMP SWITCH AND CABIN PRESSURE CONTROLLER AND NR
- [SDR HNAA2011062900202](https://openairdocs.org/sdr/HNAA2011062900202), Jun 24, 2011: BULB. INOPERATIVE. AFT EMERGENCY FLOOR PATH LIGHT IS TOO FAR BACK AND VERY DIM. R & R BULB. REPOSITIONED PATH LIGHT.
- [SDR HNAA2011062900200](https://openairdocs.org/sdr/HNAA2011062900200), Jun 24, 2011: LIGHT. MISINSTALLED. EMERGENCY FLOOR PATH LIGHTS AT ROWS 5 AND 6. THE ARROWS ARE FACING THE WRONG DIRECTION. REPOSITIONED EMERGENCY FLOOR PATH LIGHTSAT ROWS 5 AND 6 TO FACE PROPER D
- [SDR HNAA2010122100288](https://openairdocs.org/sdr/HNAA2010122100288), Dec 18, 2010: LAMP. INOPERATIVE. 2ND RED FLOOR LIGHT IS INOP. RELAMP, OPS CHECKED GOOD IAW MM 33-51-00.
- [SDR HNAA2010122100281](https://openairdocs.org/sdr/HNAA2010122100281), Dec 10, 2010: BULB. INOPERATIVE. OVERHEAD EMERGENCY LIGHT AT ROW 5 IS OUT. REMOVED LENS, R & R BULB, OPS CHECKED GOOD, INSTALLED LENS WITH ATTACHED HARDWARE.
- [SDR HNAA2010122100278](https://openairdocs.org/sdr/HNAA2010122100278), Dec 10, 2010: BULB. BURNED OUT. OVERHEAD EMERGENCY LIGHT AT ROW 5 IS OUT. REMOVED LENS, R & R BULB, OPS CHECKED GOOD. INSTALLED LENS WITH ATTACHED HARDWARE.
- [SDR HNAA2010122100273](https://openairdocs.org/sdr/HNAA2010122100273), Dec 4, 2010: BATTERY. INOPERATIVE. PAX DOOR OVERHEAD EMERGENCY SIGN AND LT FUSELAGE FWD EMERGENCY LIGHT INOP. R & R EMERGENCY LIGHT BATTERY ON PSI IAW WORDCARD 33-51-00.
- [SDR HNAA2010012200005](https://openairdocs.org/sdr/HNAA2010012200005), Jan 22, 2010: BULB. INOPERATIVE. OVERHEAD EMERGENCY LIGHT AT ROW 5 IS INOPERATIVE. R & R LIGHT LENS, R & R LIGHT BULB, OPS CHECKED GOOD. INSTALLED LIGHT LENS WITH ATTACHED HARDWARE.
- [SDR HNAA20091100334](https://openairdocs.org/sdr/HNAA20091100334), Nov 16, 2009: ACTUATOR. LEAKING. DURING TAXI, NR 1 HYD RUDDER ISO CAUTION LIGHT AND ROLL SPOILER INBD CAUTION LIGHT ILLUMINATED. NR1 HYD QUANTITY DROPPED TO .6 QUARTS. REMOVED AND REPLACED INBD
- [SDR HNAA2009090400280](https://openairdocs.org/sdr/HNAA2009090400280), Aug 28, 2009: GARLOCK SEAL. LEAKING. IN CRUISE FLIGHT NR 1 ENGINE OIL PRESSURE INDICATOR FLUXED FOLLOWED BY NR 1 ENGINE WARNING LIGHT ILLUMINATED. FOLLOWED CHECK LIST AND SHUT NR 1 ENGINE. REMOVED 
- [SDR HNAA2009070600216](https://openairdocs.org/sdr/HNAA2009070600216), Jul 3, 2009: DISPLAY. BURNED. ELECTRICAL BURNED ODOR IN FLIGHT, FOUND NR 2 TRANSPONDER DISPLAY SCREEN BLANK AND THE COMPONENT WAS HOT. PULLED ATC2 CIRCUIT BREAKER AND ODOR WENT AWAY AND COMP
- [SDR HNAA2009052100156](https://openairdocs.org/sdr/HNAA2009052100156), May 20, 2009: O-RING. LEAKING. NUMBER 2 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL. REMOVED AND REPLACED O-RING AT FUEL HEATER REDUCTION GEAR BOX OUT PRESS LINE. LEAK AND O
- [SDR HNAA2009052600160](https://openairdocs.org/sdr/HNAA2009052600160), May 17, 2009: FUEL HEATER. BROKEN. IN FLIGHT THE NR 2 FUEL TANK TEMPERATURE WAS ABOVE RED LINE ON THE GAUGE. THE TEMPERATURE DROPPED WHEN PULLING POWER BACK OR SELECTING AUXILIARY PUMP. THERE WAS
- [SDR HNAA2009051300142](https://openairdocs.org/sdr/HNAA2009051300142), May 3, 2009: PSEU. FAULTY. UPON GEAR RETRACTION NOSE GEAR DOOR AMBER LIGHT ILLUMINATED CYCLED GEAR PER EMERGENCY CHECKLIST AND RED UNSAFE LIGHT ILLUMINATED WITH NO ALTERNATE INDICATION, P
- [SDR HNAA2009042900139](https://openairdocs.org/sdr/HNAA2009042900139), Apr 28, 2009: PSEU. FALSE INDICATION. UPON GEAR RETRACTION NOSE GEAR DOOR AMBER LIGHT ILLUMINATED. CYCLED GEAR PER EMERGENCY CHECKLIST AND RED UNSAFE LIGHT ILLUMINATED WITH NO ALTERNATE INDICATION. 
- [SDR HNAA2009032800099](https://openairdocs.org/sdr/HNAA2009032800099), Mar 27, 2009: LIGHT. INOPERATIVE. UPON INSPECTION AT SBY, IT WAS NOTICED THAT AN EMERGENCY LIGHT AT ROW 1 WAS INOPERATIONAL. REPLACED THE LIGHT BULB AND THE OPERATIONAL CHECK WAS GOOD.
- [SDR HNAA0800127](https://openairdocs.org/sdr/HNAA0800127), Apr 6, 2008: LIFT STRUT. WORN. PAX DOOR UNLATCHED ITSELF (HANDLE POPPED TO THE FIRST DETENT) FOLLOWED BY PAX DOOR WARNING LIGHT IN FLIGHT COMPARTMENT. F/A LATCHED DOOR AND DOOR REMAINED LATCH
- [SDR HNAA0800056](https://openairdocs.org/sdr/HNAA0800056), Feb 4, 2008: PROXIMITY SENSOR. INTERMITTENT. GEAR SELECTED DOWN, LEFT MAIN GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED, ALT GEAR IND HAD THREE GREEN. CREW VERIFIED GEAR WAS DOWN.
- [SDR HNAA0800033](https://openairdocs.org/sdr/HNAA0800033), Jan 21, 2008: BRAKE ASSY. DEFECTIVE. WHILE TAXING TO RUNWAY 36L, ANOTHER AIRCRAFT CREW SAID THE LEFT BREAKS WERE GLOWING RED. PULLED AIRCRAFT OFF TAXIWAY TO INSPECT. THE FIRST OFFICER NOTED SMOKE C
- [SDR HNAA0700054](https://openairdocs.org/sdr/HNAA0700054), Mar 23, 2007: ROD. OUT OF ADJUST. FLIGHT ATTENDANT REPORTS FORWARD MAIN LANDING GEAR DOOR SHAKING AND WHEN CLOSED DOOR IS GAPPED. FLIGHT RETURNED TO FIELD, NO EMERGENCY WAS DECLARED BUT RESCUE V
- [SDR HNAA0700048](https://openairdocs.org/sdr/HNAA0700048), Mar 18, 2007: FUEL FILTER. DIRTY. NR 2 FUEL FILTER BYPASS CAUTION LIGHT ILLUMINATED AFTER TAKEOFF. INSPECTED WIRE HARNESS NO DEFECT NOTED. INSPECTED AND REPLACED THE HP FUEL FILTER. INSPECTED AN
- [SDR HNAA0700045](https://openairdocs.org/sdr/HNAA0700045), Feb 27, 2007: LIGHT. INOPERATIVE. EMERGENCY LIGHTING AIRSTAIR DOOR EMERGENCY EXIT SIGN CENTER LAMP IS INOP. RELAMPED LIGHT.
- [SDR HNAA0700044](https://openairdocs.org/sdr/HNAA0700044), Feb 27, 2007: LIGHT. INOPERATIVE. CABIN AISLE ESCAPE PATH LIGHTING IS INOP. RELAMPED LIGHTING.
- [SDR HNAA0700043](https://openairdocs.org/sdr/HNAA0700043), Feb 27, 2007: LIGHT. INOPERATIVE. CABIN AISLE ESCAPE PATH LIGHTING LIGHT NR 21 IS INOP. RELAMPED LIGHT.
- [SDR HNAA0600120](https://openairdocs.org/sdr/HNAA0600120), Oct 17, 2006: PROPELLER. UNKNOWN. DURING CLIMB AND STRAIGHT AND LEVEL FLIGHT THE NR 2 PROP RPM WOULD NOT STABILIZE, FLUXED FROM 940 TO 1050. RAN TEMPORARY WIRE (10008C22) FROM WING ROOT CONNECTO
- [SDR HNAA0600030](https://openairdocs.org/sdr/HNAA0600030), Apr 22, 2006: SWITCH. INTERMITTENT. EMERGENCY LIGHTS INTERMITTANTLY FLASH IN FLIGHT. REPLACED FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH.
- [SDR HNAA0500059](https://openairdocs.org/sdr/HNAA0500059), Jun 19, 2005: PSEU. FAULTY. NOSE GEAR LIGHT WILL NOT EXTINGUISH AFTER TAKEOFF. CYCLED GEAR AND LIGHT REMAINED ON. REMOVED AND REPLACED THE PSEU.
- [SDR HNAA0400030](https://openairdocs.org/sdr/HNAA0400030), Mar 26, 2004: TAPE. DEBONDED. LEFT I/B BOOT LOOSE. PHL WILL SECURE WITH SPEED TAPE WE'LL MEL A/F DEICE AND FLY REVENUE TO SBY. SCURED LOOSE DEICE BOOT WITH SPEED TAPE I/A/W SPECIAL PROCEDURE

All 80: https://openairdocs.org/deregistered/N934HA-2017-08-23/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 DCA13FA094](https://openairdocs.org/ntsb/DCA13FA094), May 18, 2013: Bombardier DHC8 (N934HA), Newark, NJ, substantial damage. Probable cause: the frozen left main landing gear (MLG) uplock roller due to lack of lubrication and the uplock latch that had worn beyond acceptable tolerances, which prevented the flight crew from extending the…

## 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.

- [Accident 20130518008759A](https://openairdocs.org/incident/20130518008759A), May 18, 2013: Dehavilland DHC-8-102 (N934HA), Newark, NJ, Substantial damage. After an uneventful flight from kphl to kewr, crew selected gear down on final to rwy 4R at kewr. Gear indication was left gear not down and locked. Crew…
- [Incident 19931205051249I](https://openairdocs.org/incident/19931205051249I), Dec 5, 1993: Dhav DHC8102 (N934HA), Washington, DC. NR2 engine voltage dropped off line. Returned. Replaced NR2 generator and control unit.

---
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.