# N930HA: Boeing DHC-8-102, registration cancelled 2019-03-04 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 4, 2019 - Status when cancelled: Valid registration - 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: 126 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: December 2, 1988 - Certificate issued: November 16, 2017 - Last registry action: June 13, 2018 - Mode S code: ACE659 - 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/N930HA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=930HA - Page: https://openairdocs.org/deregistered/N930HA-2019-03-04 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 (129, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR HNAA2017042500139](https://openairdocs.org/sdr/HNAA2017042500139), Apr 28, 2017: POWER SUPPLY. INOPERATIVE. GROUND EMERGENCY LIGHT BY FWD EMERGENCY EXIT DIMS AND GOES OUT AFTER A FEW SECONDS R & R THE POWER SUPPLY AT SEAT 7AC IAW AMM 33-50-00. - [SDR HNAA2017020800043](https://openairdocs.org/sdr/HNAA2017020800043), Feb 7, 2017: BULB. INOPERATIVE. EMERGENCY LIGHT INOPERATIVE RT AFT FUSELAGE. R & R THE BULB. - [SDR HNAA2017020800042](https://openairdocs.org/sdr/HNAA2017020800042), Feb 7, 2017: LIGHT. INOPERATIVE. EMERGENCY LIGHTS INOPERATIVE. R & R THE LIGHT ASSY. - [SDR HNAA2016102100325](https://openairdocs.org/sdr/HNAA2016102100325), Oct 21, 2016: BULB. INOPERATIVE. CABIN EMERGENCY EXIT LIGHT AT AIR STAIR DOOR HAS NUMEROUS BULBS THAT WILL NOT ILLUMINATE. REMOVED AND REPLACED THE BULBS. OPS CHECKED GOOD. - [SDR HNAA2016083100264](https://openairdocs.org/sdr/HNAA2016083100264), Aug 30, 2016: BULB. INOPERATIVE. ROW 6DF EMERGENCY LIGHT INOPERATIVE. R & R THE BULB. - [SDR HNAA2016083100265](https://openairdocs.org/sdr/HNAA2016083100265), Aug 29, 2016: LAMP. INOPERATIVE. EMERGENCY LIGHTS DISARM CAUTION LIGHT INOPERATIVE, REPLACED THE LAMP. OPS CHECKED GOOD. OK FOR SERVICE. - [SDR HNAA2016072000223](https://openairdocs.org/sdr/HNAA2016072000223), Jul 19, 2016: BULB. INOPERATIVE. CEILING EMERGENCY LT AT ROW 2 INOPERATIVE. R & R THE BULB. - [SDR HNAA2016071500216](https://openairdocs.org/sdr/HNAA2016071500216), Jul 13, 2016: ROD END. BROKEN. LOUD BANG HEARD WHEN GEAR SELECTED DOWN FROM MAIN GEARS. MLG GEAR DOORS SLOW TO CLOSE. INDICATIONS NORMAL. FOUND NR 1 MLG RETRACTION ACTUATOR ROD END BROKEN. RE - [SDR HNAA2016021700036](https://openairdocs.org/sdr/HNAA2016021700036), Feb 17, 2016: VALVE. INOPERATIVE. RT OUTER DEICE BOOT DOES NOT INDICATE INFLATION AND DOES NOT INFLATE IN MANUAL OR AUTO. NR 4 RT OTBD DISTRIBUTOR VALVE AND OTBD PRESSURE SWITCH IAW MM 30-10-16 - [SDR HNAA2015123000377](https://openairdocs.org/sdr/HNAA2015123000377), Dec 30, 2015: SELECTOR SWITCH. INOPERATIVE. DURING AUTOFEATHER TEST, NR 2 PROP WILL NOT FEATHER. RPM DROPS FROM 650 TO 590. ALL OTHER PARAMETERS OK. R & R RELAYS 6121-K4, K2 AND K10. SLAVED IN NR 2 TSEU, - [SDR HNAA2015122800376](https://openairdocs.org/sdr/HNAA2015122800376), Dec 28, 2015: BULB. INOPERATIVE. EMERGENCY LIGHT ON FORWARD RT SIDE OF FUSELAGE IS INOPERATIVE. R & R BULB FOR RT FORWARD EGRESS LIGHT IAW MM 33-51-05. OPS CHECKED GOOD. - [SDR HNAA2015121600366](https://openairdocs.org/sdr/HNAA2015121600366), Dec 16, 2015: BULB. BURNED OUT. BULBS BURNED AT EMERGENCY EXIT OVERHEAD PANEL. R & R BULBS AT EMERGENCY OVERHEAD PANEL. OPS CHECKED GOOD. - [SDR HNAA2015110400325](https://openairdocs.org/sdr/HNAA2015110400325), Nov 4, 2015: DOWNLOCK SENSOR. MALFUNCTIONED. ON FINAL WITH GEAR EXTENDED, APPROXIMATELY 500 FEET BEFORE TOUCHDOWN, PERFORMED ALTERNATE EXTENSION, ALL INDICATIONS NORMAL AFTER LANDING ROLL OUT. NLG RED LIGH - [SDR HNAA2015101900308](https://openairdocs.org/sdr/HNAA2015101900308), Oct 19, 2015: SKIN. DELAMINATED. WOW CAUTION LIGHT AND NOSE DOOR OPEN LIGHT ILLUMINATED AFTER GEAR RETRACTION, CYCLED GEAR AND BOTH LIGHTS REMAINED ILLUMINATED. MAINTENANCE FOUND RT AFT NOSE DO - [SDR HNAA2015101900305](https://openairdocs.org/sdr/HNAA2015101900305), Oct 19, 2015: WARNING LIGHT. FALSE ACTIVATION. ELEVATOR HORN HEAT CAUTION LIGHT ILLUMINATED ON ROTATION, WOW CAUTION LIGHT ILLUMINATED AFTER GEAR SELECTED UP, NOSE GEAR DOOR CAUTION LIGHT ILLUMINATED AFTER G - [SDR HNAA2015101402960](https://openairdocs.org/sdr/HNAA2015101402960), Oct 14, 2015: SWITCH. CONTAMINATED. SMOKE EMANATED FROM THE SAHS SWITCH. FOUND GYRO NR 1 SWITCH ON GYRO PANEL SCORCHED 3420-SW1. CLEANED DEBRIS FROM OTHER SWITCHES ON PANEL. - [SDR HNAA2015090900277](https://openairdocs.org/sdr/HNAA2015090900277), Sep 9, 2015: UNKNOWN. ODOR. ODOR OF JET FUEL IN COCKPIT WITH APU RUNNING. PULLED AND COLLARED CIRCUIT BREAKER N-8 ON RT MAIN BUS, AUXILIARY POWER UNIT. - [SDR HNAA2015082800265](https://openairdocs.org/sdr/HNAA2015082800265), Aug 28, 2015: PANEL. MALFUNCTIONED. NR 1 ENGINE FUEL PRESSURE CAUTION LIGHT ILLUMINATED WHILE TAKING RUNWAY. REMAINED ON UNTIL ENGINE SHUTDOWN. R & R CAUTION LIGHT PANEL IAW 33-12-01. GROUND RAN A - [SDR HNAA2015052500166](https://openairdocs.org/sdr/HNAA2015052500166), May 25, 2015: BULB. INOPERATIVE. F/A EMERGENCY LIGHT SWITCH GREEN LIGHT IS OUT. R & R BULB IN GREEN LIGHT SWITCH. OPS CHECKED GOOD. - [SDR HNAA2015041300130](https://openairdocs.org/sdr/HNAA2015041300130), Apr 13, 2015: BULB. DIM. RT FORWARD FUSELAGE EMERGENCY LIGHT DIM. R & R FORWARD FUSELAGE EMERGENCY LIGHT BULB. OPS CHECKED GOOD. - [SDR HNAA2015031800102](https://openairdocs.org/sdr/HNAA2015031800102), Mar 18, 2015: BULB. INOPERATIVE. 2ND FLOOR EMERGENCY LIGHT IS INOPERATIVE. R & R BULB FOR 2ND EMERGENCY FLOOR PATH LIGHT. OPS CHECKED GOOD. - [SDR HNAA2014102000293](https://openairdocs.org/sdr/HNAA2014102000293), Oct 20, 2014: HANDLE. MALFUNCTIONED. DURING FERRY FLIGHT WITH GEAR DOWN, NOSE GEAR CYCLED UP/DOWN SEVERAL TIMES WITH INDICATIONS FOLLOWING GEAR POSITION. ALTERNATE EXTENSION WAS REQUIRED TO MAKE A - [SDR HNAA2014100600280](https://openairdocs.org/sdr/HNAA2014100600280), Oct 6, 2014: HMU. MALFUNCTIONED. AT 1500 AGL, SWITCHED FROM TOP TO NORMAL, NR 2 ENGINE TORQUE DROPPED TO ZERO. PROPELLER RPM A 1000. ITT BETWEEN 500 TO 600 DEGREES. PERFORMED EMERGENCY PROCEDUR - [SDR HNAA2014090300255](https://openairdocs.org/sdr/HNAA2014090300255), Sep 3, 2014: BATTERY PACK. INOPERATIVE. FLOOR LEVEL AND CABIN SIDEWALL EMERGENCY LIGHTS FLICKERING WITH COCKPIT SWITCH IN THE OFF AND F/A SWITCH IN NORMAL WITH ENGINES SHUTDOWN ON APU POWER DURING PAS - [SDR HNAA2014082900251](https://openairdocs.org/sdr/HNAA2014082900251), Aug 29, 2014: BULB. INOPERATIVE. TWO EMERGENCY LIGHTS ARE INOPERATIVE AT ROWS 7 AND 8. R & R BULBS. OPS CHECKED GOOD. - [SDR HNAA2014072500215](https://openairdocs.org/sdr/HNAA2014072500215), Jul 25, 2014: CONNECTOR. DAMAGED. EMERGENCY LIGHT IS INOPERATIVE AT ROW 6. R & R 1 PIN IN CONNECTOR IAW MM 20-45-09. OPS CHECKED GOOD. - [SDR HNAA2014072100211](https://openairdocs.org/sdr/HNAA2014072100211), Jul 21, 2014: ACTUATOR. MALFUNCTIONED. AFTER TAKE OFF, SELECTED GEAR UP, RT MLG RED UNSAFE LIGHT ILLUMINATED, AMBER LIGHT ILLUMINATED ON LT MLG AND NLG. R & R NR 2 RETRACT ACTUATOR AND FITTING IAW MM - [SDR HNAA2014071400204](https://openairdocs.org/sdr/HNAA2014071400204), Jul 13, 2014: LAMP. INOPERATIVE. EMERGENCY PATH LIGHT 4TH FROM FRONT INOPERATIVE. REPLACED THE LAMP, OPS CHECKED GOOD, OK FOR SERVICE. - [SDR HNAA2014061600183](https://openairdocs.org/sdr/HNAA2014061600183), Jun 16, 2014: BULB. INOPERATIVE. FIFTH CABIN EMERGENCY LIGHT FROM REAR IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD. - [SDR HNAA2014031700091](https://openairdocs.org/sdr/HNAA2014031700091), Mar 17, 2014: UNKNOWN. SMOKE. CABIN AND FLIGHT DECK HAD SMOKE WITH BLEEDS ON, DISIPATED WITH BLEEDS OFF. ACFT WAS DIVERTED. - [SDR HNAA2014031400085](https://openairdocs.org/sdr/HNAA2014031400085), Mar 14, 2014: BULB. INOPERATIVE. ROW 2 EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT BULB AT ROW 2. - [SDR HNAA2014030700074](https://openairdocs.org/sdr/HNAA2014030700074), Mar 5, 2014: UNKNOWN. ODOR. CREW REPORTED PETROLEUM ODOR, STARTED WHEN ACFT WAS IN STEEP DESCENT AND CLEARED BEFORE LANDING. R & R CONDENSER MIXER, HEAT EXCHANGER, IAW ACM. GROUND RAN, OPS - [SDR HNAA2014030500069](https://openairdocs.org/sdr/HNAA2014030500069), Mar 4, 2014: LIGHT. DIM. RIGHT AFT, RIGHT FORWARD, LEFT AFT BETA LIGHTS DIMMER THAN REFERENCE LIGHT. REMOVED & REPLACED 3 BETA LIGHTS. - [SDR HNAA2014012000013](https://openairdocs.org/sdr/HNAA2014012000013), Jan 20, 2014: INDICATOR. FAILED. GPU HAD 3 VOLTAGE SPIKES. CREW SHUTOFF GROUNDPOWER. CIRCUIT BREAKER P-6 AND CIRCUIT BREAKER C-1 ON LT ESS AND SEC BUSSES FOUND TRIPPED WITH AN ELECTRICAL ODOR. - [SDR HNAA2014011500008](https://openairdocs.org/sdr/HNAA2014011500008), Jan 15, 2014: BULB. INOPERATIVE. ONE EMERGENCY LIGHT IS INOP AT ROW 1DF SIDEWALL. R & R BULB FOR SIDEWALL EMERGENCY LIGHT AT ROW 1DF. OPS CHECKED GOOD. - [SDR HNAA2013122300628](https://openairdocs.org/sdr/HNAA2013122300628), Dec 23, 2013: UNKNOWN. ODOR. ODOR IN FLIGHT DECK DURING DECENT. SELECTED BLEEDS OFF. ODOR DISIPATED, INSPECTED ACM. NO DEFECTS NOTED. GROUND RAN BOTH ENGINES WITH BOTH BLEEDS ON AND THEN ON - [SDR HNAA2013122300625](https://openairdocs.org/sdr/HNAA2013122300625), Dec 23, 2013: UNKNOWN. SMOKE. DURING FLIGHT, OIL ODOR ENTERED THE CABIN AND FLIGHT DECK WITH ASSOCIATED SMOKEY HAZE IN THE CABIN. SWITCHED THE BLEEDS OFF AND ODOR AND SMOKE DISIPATED. INSPEC - [SDR HNAA2013112500588](https://openairdocs.org/sdr/HNAA2013112500588), Nov 25, 2013: SMOKE DETECTOR. ACTIVATED. LAVATORY SMOKE DETECTOR SOUNDED DURING TAXI OUT. SELECTED ENGINE BLEEDS OFF DURING RETURN TO GATE AND LAVATORY ALARM STOPPED. GROUND RAN BOTH ENGINES AND APU. O - [SDR HNAA2013110400562](https://openairdocs.org/sdr/HNAA2013110400562), Nov 4, 2013: VALVE. FAILED. LIGHT SMOKE IN FLIGHT DECK, CABIN AND BAG BAY IN FLIGHT AT 19,000 FT COMPLIED WITH UNKNOWN SMOKE CHECKLIST, RECIRCULATION FAN AND BLEEDS SELECTED OFF. AFTER BLE - [SDR HNAA2013080500447](https://openairdocs.org/sdr/HNAA2013080500447), Aug 5, 2013: WARNING LIGHT. FALSE ACTIVATION. ON ROLL OUT AFTER LANDING, NOSE GEAR INDICATED RED UNSAFE. ACFT WAS STOPPED ASAP AND RED INDICATION SELF CLEARED TO GREEN. DISCREPANCY WAS ASSOCIATED WITH WOW C - [SDR HNAA2013062800372](https://openairdocs.org/sdr/HNAA2013062800372), Jun 28, 2013: RADAR. FAILED. RADAR WILL NOT TEST OR PAINT GROUND. R & R WEATHER RADAR RT IAW MM 34-41-04 AND PB 34-18. OPS CHECKED GOOD. - [SDR HNAA2013051500279](https://openairdocs.org/sdr/HNAA2013051500279), May 15, 2013: STRAP. CORRODED. CORROSION ON FUSELAGE JOINT STRAP AT BS 182 BETWEEN STRINGERS 29 AND 30P. BLENDED AREA OF FUSELAGE STRAP. PERFORMED HFEC INSPECTION. NO DISCREPANCIES FOUND IAW - [SDR HNAA2013051500278](https://openairdocs.org/sdr/HNAA2013051500278), May 15, 2013: SILL. CORRODED. PAX DOOR LOWER SILL HAS CORROSION ON TOP SURFACE AROUND FASTENER HOLES AND UNDER SURFACE NUT PLATES. R & R PAX DOOR LOWER SILL. CLEANED MINOR CORROSION FROM UND - [SDR HNAA2013051500277](https://openairdocs.org/sdr/HNAA2013051500277), May 15, 2013: SEAT TRACK. CORRODED. CENTER LT SEAT TRACK HAS AREA OF MINOR SURFACE PITTING THROUGH OUT THE LENGTH OF THE TRACK. BLENDED LIGHT CORROSION WITHIN LIMITS OF RD8-53-1339. PERFORMED HFEC - [SDR HNAA2013051500276](https://openairdocs.org/sdr/HNAA2013051500276), May 15, 2013: SEAT TRACK. CORRODED. CENTER RT SEAT TRACK HAS AREAS OF MINOR SURFACE PITTING THROUGH OUT THE LENGTH OF THE TRACK. BLENDED AREAS OF CORROSION ON INBD RT SEAT TRACK. CORROSION WAS FOU - [SDR HNAA2013051500275](https://openairdocs.org/sdr/HNAA2013051500275), May 15, 2013: SEAT TRACK. CORRODED. RIGHT OTBD SEAT TRACK HAS MINOR SURFACE CORROSION AFT OF BS 510. BLENDED MINOR SURFACE CORROSION AND FOUND IT TO BE WITHIN LIMITS IAW RD8-53-3644. ALODINED AND - [SDR HNAA2013051500274](https://openairdocs.org/sdr/HNAA2013051500274), May 15, 2013: STRINGER. CORRODED. STRINGER 31S HAS MINOR SURFACE CORROSION JUST AFT OF FRAME BS 240.50. BLENDED MINOR CORROSION IAW THE SRM 51-20-16,51-20-36. - [SDR HNAA2013051500273](https://openairdocs.org/sdr/HNAA2013051500273), May 15, 2013: SEAT TRACK. CORRODED. CENTER LT SEAT TRACK HAS SURFACE CORROSION THROUGHOUT BS 201.15 TO 240.50. BLENDED CORROSION AND FOUND TO BE WITHIN LIMITS IAW RD8-53-4698. - [SDR HNAA2013051300272](https://openairdocs.org/sdr/HNAA2013051300272), May 13, 2013: SEAT TRACK. CORRODED. CENTER RT SEAT TRACK HAS CORROSION THROUGHOUT STA X201.14 TO X252.30. PARTIALLY REMOVED SEAT TRACK. INSTALLED NEW SEAT TRACK AND SPLICE REPAIR. INSTALLED REMAIN - [SDR HNAA2013051300271](https://openairdocs.org/sdr/HNAA2013051300271), May 13, 2013: SKIN. DEBONDED. LOWER FUSELAGE SKIN PANEL IS DEBONDED AT STA X182.00, STR 29P TO 30P. UNRIVETED, DISBONDED AREA FOR FURTHER EVALUATION. CUT OUT DEBONDED SKIN AND WAFFLE DOUBLER All 129: https://openairdocs.org/deregistered/N930HA-2019-03-04/reports.md ## Other aircraft with N930HA - [Registered now](https://openairdocs.org/aircraft/N930HA): DJI AGRAS T100, S/N 1581F8ZLC256A00291JW --- 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.