# N912HA: Dehavilland DHC-8-102, registration cancelled 2016-09-21

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 21, 2016
- Status when cancelled: Valid registration
- Airframe: [Dehavilland DHC-8-102](https://openairdocs.org/model/dehavilland-dhc-8-102) (registry code 2809003)
- Engine: [NONE](https://openairdocs.org/engine/none) (registry code 00000)
- Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM) (OpenAirDocs)
- Serial number: 040
- Type of aircraft: Fixed wing multi engine
- Engine type: None
- Airworthiness: Standard, transport
- Airworthiness date: June 5, 1986
- Certificate issued: August 14, 2015
- Last registry action: August 14, 2015
- Mode S code: AC9EC9
- Owner when cancelled: [Southern Aircraft Consultancy Inc Trustee](https://openairdocs.org/faa-owner/SOUTHERN%20AIRCRAFT%20CONSULTANCY%20INC%20TRUSTEE)
- Location: Bungay Suffolk, United Kingdom
- Owner type: Corporation
- The mark today: https://openairdocs.org/aircraft/N912HA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=912HA
- Page: https://openairdocs.org/deregistered/N912HA-2016-09-21

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

## Service difficulty reports (90, newest 50)

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

- [SDR HNAA2014071600207](https://openairdocs.org/sdr/HNAA2014071600207), Jul 16, 2014: BATTERY PACK. MALFUNCTIONED. ALL CABIN EMERGENCY LIGHTS ON POWER SUPPLY, 3351PS2, COME ON FOR ONE OR TWO SECONDS AND THEN SHUTOFF. ALL OTHER EMERGENCY LIGHTS FUNCTION NORMAL. SLAVED IN POWE
- [SDR HNAA2014050200146](https://openairdocs.org/sdr/HNAA2014050200146), May 2, 2014: RELAY. MALFUNCTIONED. AFTER TAKEOFF, NOSE GEAR RED UNSAFE LIGHT REMAINED ON AFTER SELECTED UP. R & R RELAY 3261-510.
- [SDR HNAA2014050200144](https://openairdocs.org/sdr/HNAA2014050200144), May 2, 2014: TRANSCEIVER. INTERMITTENT. WEATHER RADAR INTERMITTENT WITH ANT-FLIGHT MESSAGE. R & R WEATHER RADAR R/T IAW MM 34-41-04. OPS CHECKED GOOD, OK FOR SERVICE.
- [SDR HNAA2014032400106](https://openairdocs.org/sdr/HNAA2014032400106), Mar 24, 2014: BULB. INOPERATIVE. EMERGENCY LIGHT INOPERATIVE BETWEEN ROWS 3 AND 4. R & R BULB. OPS CHECKED GOOD.
- [SDR HNAA2013111500574](https://openairdocs.org/sdr/HNAA2013111500574), Nov 15, 2013: UNKNOWN. ODOR. EXHAUST ODOR IN COCKPIT. RAN BOTH ENGINES AND BLEEDS. RAN ALL DEICE SYSTEMS. CHECKED ALL CIRCUIT BREAKERS. CHECKED ALL AVIONICS SYSTEMS. ALL CHECKED GOOD. NO EV
- [SDR HNAA2013070900400](https://openairdocs.org/sdr/HNAA2013070900400), Jul 7, 2013: CONTROL PANEL. FAILED. RT MLG DOOR AMBER LIGHT AFTER TAKE OFF (AFT DOOR). CYCLED GEAR IAW CHECKLIST, LIGHT EXTINGUISHED FOR A MOMENT AND THEN RETURNED. R & R GEAR DOOR ACTUATOR AND LA
- [SDR HNAA2013061700345](https://openairdocs.org/sdr/HNAA2013061700345), Jun 17, 2013: CONTROL SWITCH. INOPERATIVE. LT WINDSHIELD HEAT HOT CAUTION LIGHT CAME ON WHEN SELECTED TO NORM. NO LOAD. R & R WINDSHIELD HEAT CONTROL SWITCH IN COCKPIT 3041-S1. HEAT OPS CHECKED GOOD AT T
- [SDR HNAA2013041000216](https://openairdocs.org/sdr/HNAA2013041000216), Apr 10, 2013: SELECTOR VALVE. MALFUNCTIONED. SELECTED GEAR DOWN ON APPROACH. LT MAIN UNSAFE LIGHT ILLUMINATED AND PASSENGER REPORTED LT GEAR NOT EXTENDED. EXECUTED GO AROUND AND GEAR EXTENDED ON ITS OWN AF
- [SDR HNAA2013032700187](https://openairdocs.org/sdr/HNAA2013032700187), Mar 27, 2013: DUMP VALVE. MALFUNCTIONED. CIRCUIT BREAKER G6 RT OTBD ROLL SPOILER INDICATION WILL NOT RESET. R & R NR1 SYSTEM, NR 2 ROLL LIFT DUMP VALVE IAW MM 27. OPS AND LEAK CHECKED GOOD.
- [SDR HNAA2013031900137](https://openairdocs.org/sdr/HNAA2013031900137), Mar 19, 2013: BULB. INOPERATIVE. ROW 4 EMERGENCY LIGHT BULBS ARE INOPERATIVE. R & R EMERGENCY LIGHTS. OPS CHECKED GOOD.
- [SDR HNAA2013031900136](https://openairdocs.org/sdr/HNAA2013031900136), Mar 19, 2013: BULB. FAILED. ROW 8, EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE. R & R BULB . OPS CHECKED GOOD.
- [SDR HNAA2013030100097](https://openairdocs.org/sdr/HNAA2013030100097), Mar 1, 2013: CURRENT LIMITER. BLOWN. DC BUSS CAUTION LIGHT CAME ON DURING TAKEOFF ROLL. REJECTED TAKEOFF. CLEARED RUNWAY. ATTEMPED TO RESET. WILL NOT RESET. MX FOUND CURRENT LIMITERS BLOWN. R & R C
- [SDR HNAA2012062000830](https://openairdocs.org/sdr/HNAA2012062000830), Jun 20, 2012: LIGHT. MISSING. ONE FLOOR EMERGENCY FLOOR PATH LIGHT IS MISSING. INSTALLED LIGHT IN CORRECT LOCATION.
- [SDR HNAA2012061100822](https://openairdocs.org/sdr/HNAA2012061100822), Jun 11, 2012: SEAT TRACK. CRACKED. LEFT SEAT TRACK FLANGE IS CRACKED ON FWD END AT BS X222. REMOVED FLANGE. INSTALLED NEW FLANGE IAW DWG 85320079.
- [SDR HNAA2012061100821](https://openairdocs.org/sdr/HNAA2012061100821), Jun 11, 2012: STRINGER FITTING. CORRODED. AREA OF HEAVY CORROSION AT STA X222 AND STR 26S. FOUND STRINGER END CLEAT CORRODED. REMOVED CLEAT. INSTALLED NEW CLEAT IAW DWG 85320983.
- [SDR HNAA2012061100820](https://openairdocs.org/sdr/HNAA2012061100820), Jun 11, 2012: STRUCTURE. CORRODED. AREA OF CORROSION AT BS X488 AND STR 31S. REMOVED 2 RIVETS, CLEANED AREA AND REPAIRED IAW SRM 51-20-11 AND 51-20-36. INSTALLED NEW RIVETS.
- [SDR HNAA2012061100819](https://openairdocs.org/sdr/HNAA2012061100819), Jun 11, 2012: STRUCTURE. CORRODED. AREA OF CORROSION AT STA X510 AND STR 31S. R & R 3 RIVETS, CLEANED AREA AND REPAIRED IAW SRM 51-20-11 AND 51-20-36. INSTALLED NEW RIVETS.
- [SDR HNAA2012060100808](https://openairdocs.org/sdr/HNAA2012060100808), Jun 1, 2012: SKIN. CORRODED. POSSIBLE CORROSION BUILDUP UNDER BOTH RADIO ALTIMETER ANTENNA. REMOVED MINOR CORROSION FROM SKIN SURFACE AT BOTH FORWARD AND AFT ALTIMETER ANTENNA AREA IAW CORR
- [SDR HNAA2012060100807](https://openairdocs.org/sdr/HNAA2012060100807), Jun 1, 2012: STRINGER FITTING. CORRODED. AREA OF HEAVY CORROSION AT STR 26S AND FRAME X222. FOUND STRINGER END CLEAT CORRODED. REMOVED CLEAT. INSTALLED NEW CLEAT IAW DWG 85320983.
- [SDR HNAA2012052100793](https://openairdocs.org/sdr/HNAA2012052100793), May 17, 2012: BATTERY. WEAK. RT EXIT SIGN (TOP) & FWD CENTER EXIT SIGN INOP. T/S FOUND BAD BATTERY IN BOTTOM COAT CLOSET LOCATION R & R BATTERY. OPS CK GOOD IAW AMM 33-52-00 & W/C 33-50-03Q
- [SDR HNAA2012041600735](https://openairdocs.org/sdr/HNAA2012041600735), Apr 16, 2012: LAMP. FAILED. EMERGENCY FLOOR PATH LIGHTS ARE INOPERATIVE AT ROW 1. R & R EMERGENCY FLOOR PATH LIGHT LAMPS AT ROW 1 AND CLOSED ACCESS PANEL.
- [SDR HNAA2012040500719](https://openairdocs.org/sdr/HNAA2012040500719), Apr 5, 2012: BULB. BURNED OUT. EMERGENCY OVERHEAD LIGHT IS INOPERATIVE AT ROW 7. REMOVED LENS, R & R BULB AT SAID LOCATION, REINSTALLED LENS.
- [SDR HNAA2012021400576](https://openairdocs.org/sdr/HNAA2012021400576), Feb 12, 2012: WIRE. BROKEN. ONE RED FLOOR EMERGENCY LIGHT AT ROW 4 IS INOP. MX FOUND WIRES BROKEN. ROA VERIFIED DISCREPANCY REPAIRED BROKEN WIRE, OPS CHECKS.
- [SDR HNAA2011122700438](https://openairdocs.org/sdr/HNAA2011122700438), Dec 27, 2011: LIGHT. DAMAGED. MISSING EMERGENCY LIGHT ARROW ON LOWER LIGHT. R & R LIGHT MODULE WITH NEW. OPS CHECKED GOOD.
- [SDR HNAA2011110900352](https://openairdocs.org/sdr/HNAA2011110900352), Nov 9, 2011: BULB. FAILED. SECOND FLOOR PATH LIGHT IS INOPERATIVE. R & R LAMP IAW 33-51-00.
- [SDR HNAA2011091100274](https://openairdocs.org/sdr/HNAA2011091100274), Sep 3, 2011: BULB. BURNED OUT. EMERGENCY PATH LIGHTING AT ROWS 4DF AND 7DF NOT WORKING. R & R EMERGENCY LOWER LEVEL FLOOR LIGHT BULBS IN ROWS 4DF AND 7DF.
- [SDR HNAA2011052300150](https://openairdocs.org/sdr/HNAA2011052300150), May 17, 2011: TRU. FAILED. RIGHT AC BUSS CAUTION LIGHT ILLUMINATED INFLIGHT ASSOCIATED WITH OTHER CAUTION LIGHTS. REMOVED AND REPLACED RT TRU IAW 24-31-00, OPS CHECKED GOOD.
- [SDR HNAA2011033000062](https://openairdocs.org/sdr/HNAA2011033000062), Mar 24, 2011: BRUSH BLOCK. BURNED. ON APPROACH, NR 1 ENG WAS SPARKING FROM PROP SPINNER WITH PROP HEAT ON AND NR 1 AC GENERATOR "A" PHASE AT 85 VOLTS. SELECTED PROP HEAT OFF AND SPARKS STOPPED. O
- [SDR HNAA2011032000058](https://openairdocs.org/sdr/HNAA2011032000058), Mar 17, 2011: LAMP. INOPERATIVE. EMERGENCY FLOOR PATH LIGHT IS INOP AT ROW 1. R & R FLOOR PATH LIGHT LAMP AT ROW 1 AND CLOSED ACCESS PANEL.
- [SDR HNAA2011032000057](https://openairdocs.org/sdr/HNAA2011032000057), Mar 10, 2011: CONNECTOR. SHORTED. NOTICE TRACE OF SMOKE IN FLIGHT DECK, DISCOVERED CAPT'S WINDSHIELD ELECTRICAL CONNECTION WITH SMALL TRACE OF SMOKE. SELECTED WINDSHIELD HEAT OFF AND SMOKE DISSI
- [SDR HNAA2011030900038](https://openairdocs.org/sdr/HNAA2011030900038), Mar 6, 2011: TRANSCEIVER. MALFUNCTIONED. RADAR HAS STAB OFF MESSAGE AND WILL NOT PAINT KNOWN WEATHER. R & R RADAR RT IAW 34-41-02.OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR HNAA2011022000031](https://openairdocs.org/sdr/HNAA2011022000031), Feb 19, 2011: LIGHT. MISSING. 1 EMERGENCY FLOOR PATH LIGHT IS MISSING. FOUND MISSING EMERGENCY LIGHT UNDER CENTER FLOOR PANEL AND PLACED IN IT'S PROPER POSITION, OPS CHECKED GOOD.
- [SDR HNAA2011021500025](https://openairdocs.org/sdr/HNAA2011021500025), Feb 7, 2011: WARNING HORN. FALSE ACTIVATION. TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL, ABORTED TAKEOFF, CYCLED FLAPS AND CHECKED ACFT CONFIGURATION. CHECKED GOOD. PERFORMED TAKEOFF WARNING HORN OPS CHE
- [SDR HNAA2011021500019](https://openairdocs.org/sdr/HNAA2011021500019), Jan 31, 2011: UNKNOWN. ODOR. ELECTRICAL ODOR EMINATING IN CABIN AT ROW 2 AND 3. INSPECTED CABIN LIGHTS AND ASSOCIATED AREAS WITH NO OBVIOUS DEFECTS OR ODOR NOTED.
- [SDR HNAA2010120300263](https://openairdocs.org/sdr/HNAA2010120300263), Nov 30, 2010: WINDSCREEN. SMOKE. POPPING SOUND AND LIGHT SMOKE FROM LOWER PORTION OF CAPTAIN'S WINDSCREEN FOLLOWED BY BURNING RUBBER AND ELECTRICAL ODOR. R & R F/O'S RT WINDSCREEN IAW WC 56-00-
- [SDR HNAA2010120300262](https://openairdocs.org/sdr/HNAA2010120300262), Nov 29, 2010: BLEED VALVE. FAILED. INTERMITTENT STRONG ODOR IN FRONT CABIN AND FLIGHT DECK. IN FLIGHT AND GROUND, STRONG SOUR BURNED TOAST ODOR MORE PREVALENT WITH ENGINE BLEEDS. OPERATED BLEED, 
- [SDR HNAA2010082600198](https://openairdocs.org/sdr/HNAA2010082600198), Aug 26, 2010: WIRE. BROKEN. ROW 13 EMERGENCY FLOOR PATH LIGHT INOP, WITH BROKEN WIRE. SPLICE WIRE AT ROW 13 RED EMERGENCY FLOOR LIGHT IAW AMM 20-45-07.
- [SDR HNAA2010042300120](https://openairdocs.org/sdr/HNAA2010042300120), Apr 22, 2010: WIRE. LOOSE. LOOSE WIRE FOUND AT LT HANDHOLD ON CAPTAINS YOKE CAUSED SMOKE AND SPARKS WHEN TOUCHED. AUTOPILOT DISENGAGED ON CAPTAINS YOKE. DISABLED IAW EO8-22-10-10-0141. NE
- [SDR HNAA2010042000090](https://openairdocs.org/sdr/HNAA2010042000090), Apr 7, 2010: TRIM SYSTEM. OUT OF ADJUST. TAKEOFF WAS ABORTED DUE TO NP REACHING 1215 ON NR 2 ENGINE. ADJUSTED RIGHT ENGINE SPEED TRIM SCREW IN ACCORDANCE WITH HAMILTON STD MM 61-22-00. OPERATIONAL CHEC
- [SDR HNAA2010042000081](https://openairdocs.org/sdr/HNAA2010042000081), Mar 29, 2010: GENERATOR. MALFUNCTIONED. FLIGHT DECK REPORTS AC BUS CAUTION LIGHT ILLUMINATED IN FLIGHT WITH OTHER ASSOCIATED CAUTION LIGHTS. REMOVED AND REPLACED GENERATOR IN ACCORDANCE WITH WORK CARD
- [SDR HNAA2010042000080](https://openairdocs.org/sdr/HNAA2010042000080), Mar 29, 2010: CONNECTOR. CONTAMINATED. RIGHT AC BUS CAUTION LIGHT ILLUMINATED IN FLIGHT FOLLOWED BY RIGHT TRU/STALL WARNING/ELEVATOR HORN HEAT CAUTION LIGHT. REMOVED AND REPLACED AC CONTACTOR K-2 IN 
- [SDR HNAA2010012200014](https://openairdocs.org/sdr/HNAA2010012200014), Jan 3, 2010: LONGERON. CRACKED. INBD UPPER LONGERON IS CRACKED AT THE FWD END. CRACK IS 1.3 INCH LONG AND IS IN THE INBD RADIUS. IT TRAVELS FROM THE FWD END, BELOW THE FIRST RIVET AND TO THE S
- [SDR HNAA2009102700321](https://openairdocs.org/sdr/HNAA2009102700321), Oct 23, 2009: BULB. INOPERATIVE. FLOOR EMERGENCY LIGHTS 3 AND 4 FROM FRONT NOT OPERATING. REMOVED AND REPLACED EMERGENCY LIGHT BULBS IN ACCORDANCE WITH AMM 33-52-00
- [SDR HNAA2009081100250](https://openairdocs.org/sdr/HNAA2009081100250), Aug 8, 2009: TRANSFER TUBE. OUT OF POSITION. ON TAKEOFF NR 2 PROPELLER INCREASED TO 1224 RPM WITH SUBSEQUENT PROPELLER FLUX AND TORQUE FLUX OF 5 TO 10 PERCENT. CAPTAIN WAS ABLE TO STABILIZE BY REDUCING POW
- [SDR HNAA2009033100101](https://openairdocs.org/sdr/HNAA2009033100101), Mar 27, 2009: BRAKE. MALFUNCTIONED. SMOKE COMING FROM RIGHT BRAKES. REMOVED AND REPLACED NR 4 BRAKE ASSY IN ACCORDANCE WITH MAINTENANCE MANUAL 32-42-11, LEAK AND OPS CHECKED GOOD.
- [SDR HNAA200903010008A](https://openairdocs.org/sdr/HNAA200903010008A), Mar 2, 2009: PRESSURE SWITCH. DEFECTIVE. AFTER TAKEOFF RIGHT INBOARD TAIL DEICE BOOT DID NOT ILLUMINATE, LIGHT DOES TEST. REMOVED AND REPLACED TAIL DEICE BOOT PRESS SWITCH. GROUND RAN BOTH ENGINES, OPS
- [SDR HNAA2008121000346](https://openairdocs.org/sdr/HNAA2008121000346), Dec 13, 2008: LIGHT. INOPERATIVE. FIRST FLOOR EMERGENCY LIGHT INOP. RELAMPED 1ST EMERGENCY LIGHT BULB.
- [SDR HNA2008F00038](https://openairdocs.org/sdr/HNA2008F00038), Aug 11, 2008: WIRE. BROKEN. ABORTED TAKEOFF DUE TO AUTOFEATHER ARM LIGHT DID NOT ILLUMINATE. FERRIED TO SBY. MAINTENANCE REPAIRED WIRE AT POWER LEVER MICROSWITCH 6121S13. OPS CHECK GOOD. (
- [SDR HNAA0800093](https://openairdocs.org/sdr/HNAA0800093), Feb 20, 2008: PSEU. MALFUNCTIONED. AT 10,000 FT AND 210 KNOTS NOSE GEAR EXTENDED UNCOMMANDED FOR APPROXIMATELY 5 SECONDS THEN RETRACTED. THEN NOSE GEAR CYCLED DOWN AND UP BRIEFLY WITH MAIN GEAR D
- [SDR HNAA0800005](https://openairdocs.org/sdr/HNAA0800005), Dec 19, 2007: MASTER CAUTION. SPARKS. MASTER CAUTION PUSH TO RESET SPARKED WHEN PUSHED AND WILL NOT TEST. REPLACED MASTER CAUTION SWITCH AND CAUTION PANEL.

All 90: https://openairdocs.org/deregistered/N912HA-2016-09-21/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 19910108004479I](https://openairdocs.org/incident/19910108004479I), Jan 8, 1991: Dhav DHC8102 (N912HA), New York, NY, Minor damage. Left wing tip hit parked aircraft while taxiing. Under direction of two marshallers.

---
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.
