# N906HA: Dehavilland DHC-8-102, registration cancelled 2016-09-20

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 20, 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: 9
- Type of aircraft: Fixed wing multi engine
- Engine type: None
- Airworthiness: Standard, transport
- Airworthiness date: April 3, 1985
- Certificate issued: August 7, 2015
- Last registry action: August 7, 2015
- Mode S code: AC8626
- 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/N906HA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=906HA
- Page: https://openairdocs.org/deregistered/N906HA-2016-09-20

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 (85, newest 50)

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

- [SDR HNAA2013053100315](https://openairdocs.org/sdr/HNAA2013053100315), May 31, 2013: BULB. INOPERATIVE. CENTER CEILING MID EMERGENCY LIGHT IS INOPERATIVE. R & R BULB IAW 33-51-00. OPS CHECKED GOOD.
- [SDR HNAA2013041700223](https://openairdocs.org/sdr/HNAA2013041700223), Apr 16, 2013: HOSE. DETACHED. CREW REPORTS SMOKE FROM TAILCONE AND APU DOOR VENT. APU OPS OK WITH NO FIRE INDICATIONS. INSPECTION APU COMPARTMENT, ATTACHED HOSE AT APU EXHAUST.
- [SDR HNAA2013041000215](https://openairdocs.org/sdr/HNAA2013041000215), Apr 10, 2013: CONNECTOR. CONTAMINATED. LOST BRAKES DURING TAXI. FOUND NR 1 S/B HYD PUMP CIRCUIT BREAKER OUT. INSPECTED AND FOUND CONNECTOR PLUG CONTAMINATED WITH OIL FROM ENGINE BREATHER. CLEANED AND
- [SDR HNAA2013031200123](https://openairdocs.org/sdr/HNAA2013031200123), Mar 13, 2013: GENERATOR. INOPERATIVE. NR 2 AC GENERATOR HOT CAUTION LIGHT ILLUMINATED IN FLIGHT. R & R NR 2 AC GENERATOR IAW WC 24-20-11. OPS AND LEAKED CHECKED GOOD.
- [SDR HNAA2012113001082](https://openairdocs.org/sdr/HNAA2012113001082), Nov 30, 2012: BULB. FAILED. OVERHEAD EMERGENCY LIGHT AT ROW 2 IS INOPERATIVE. REMOVED LENS PANEL, R & R BULB. OPS CHECKED GOOD.
- [SDR HNAA2012111201042](https://openairdocs.org/sdr/HNAA2012111201042), Nov 12, 2012: WIRE. BROKEN. NR 1 HYDRAULIC STANDBY PUMP INOPERATIVE, ZERO PRESSURE. FOUND WIRE 10009B22 BROKEN AT P4 CONNECTOR PLUG. REPAIRED WIRE USING STD MTC PRACTICE. OPS CHECKED GOOD.
- [SDR HNAA2012052100791](https://openairdocs.org/sdr/HNAA2012052100791), May 17, 2012: PSEU. FAULTED. LEFT MLG AMBER DOOR LIGHT REMAINED ILLUMINATED AFTER MLG RETRACTION, CYCLED GEAR IAW CHECK LIST, ALL INDICATIONS ARE NORMAL. PERFORMED PSEU TEST FOUND CODE 54 C
- [SDR HNAA2012042600753](https://openairdocs.org/sdr/HNAA2012042600753), Apr 26, 2012: PITOT HEAD. FAILED. CAPTAIN LOST AIRSPEED, HEADING DATA AND YAW DAMPER FAILED. REPLACED RUBBER PITOT HOSE BETWEEN CAPTS PITOT TUBE AND FLOOR V THROUGH. R & R CAPT'S PITOT TUBE. OPS
- [SDR HNAA2012031400690](https://openairdocs.org/sdr/HNAA2012031400690), Mar 14, 2012: WARNING LIGHT. ILLUMINATED. SUSPECTED LIGHTNING STRIKE, FOLLOWED BY ILLUMINATION OF NR 2 DC GEN CAUTION LIGHT. CAUTION LIGHT EXTINGUSHED AFTER CYCLING NR 2 DC GENERATOR. COMPLIED WITH LIGH
- [SDR HNAA2011110200343](https://openairdocs.org/sdr/HNAA2011110200343), Oct 28, 2011: ACTUATOR. OUT OF ADJUST. LT MAIN GEAR DOOR AMBER LIGHT ILLUMINATED AFTER GEAR RETRACTION. RECYCLED GEAR IAW CHECK LIST. AMBER LIGHT RE-ILLUMINATED. ADJUSTED FORWARD LT GEAR DOOR ACTUATO
- [SDR HNAA2011062900199](https://openairdocs.org/sdr/HNAA2011062900199), Jun 23, 2011: BULB. FAILED. (1) OVERHEAD EMERGENCY LIGHT AT ROW 6 IS INOP. R & R BULB. OPS CHECKED GOOD.
- [SDR HNAA2011062100180](https://openairdocs.org/sdr/HNAA2011062100180), Jun 19, 2011: DRAG STRUT. INOPERATIVE. REJECTED TAKEOFF DUE TO NOSE GEAR UNSAFE LIGHT, GEAR SELECT HANDLE LIGHTS AND NOSE STEERING CAUTION LIGHT ILLUMINATED AT 75 KNOTS ON TAKEOFF ROLL. LIGHTS EXTING
- [SDR HNAA2011060100160](https://openairdocs.org/sdr/HNAA2011060100160), May 28, 2011: WIRE HARNESS. MISWIRED. PANEL 143BZ (CTR FLOOR) EMERGENCY LIGHTS DO NOT COME ON AND DIM ALL OTHER EMERGENCY LIGHTS WHEN PLUGGED IN. R & R POWER SUPPLY BASE AND BATTERY, NO FIX. FOUND L
- [SDR HNAA2011060100157](https://openairdocs.org/sdr/HNAA2011060100157), May 27, 2011: FRAME. CORRODED. RIB AT X222, STRINGER 30-31 HAS CORROSION. REMOVED VERTICAL FLOOR SUPPORT FRAME. REMOVED RIB SECTION AT X222 BETWEEN STRINGERS 32P AND 28S. COMPLIED WITH HFEC I
- [SDR HNAA2011060100156](https://openairdocs.org/sdr/HNAA2011060100156), May 27, 2011: FRAME. CORRODED. RIB AT X240.5, STA. 31S HAS CORROSION. REMOVED RIB SECTION AT X240.5 BETWEEN STRINGER 32P AND STRINGER 28S. COMPLIED WITH HFEC IAW EO8-53-11-0289. NO DEFECTS NO
- [SDR HNAA2011051700135](https://openairdocs.org/sdr/HNAA2011051700135), May 3, 2011: FLAP TRACK. CORRODED. RT NR 2 FLAP TRACK HAS PITTING AND CORROSION ON MATING SURFACE AND HEAVY WEAR AND PITTING ON ROLLER SURFACE. R & R FLAP TRACK WITH NEW HARDWARE IAW AMM57-50-26.
- [SDR HNAA2011052300145](https://openairdocs.org/sdr/HNAA2011052300145), May 2, 2011: THRESHOLD. CORRODED. PAX DOOR THRESHOLD IS CORRODED. R & R THRESHOLD ASSY, INSTALLED THRESHOLD ASSY IAW ENG DRAWING 85321241.
- [SDR HNAA2011051700130](https://openairdocs.org/sdr/HNAA2011051700130), May 2, 2011: FITTING. CORRODED. RT NR1 FLAP TRACK THROUGH BOLT FITTING IS CORRODED. R & R NECESSARY HARDWARE WITH NEW HARDWARE.
- [SDR HNAA2011051700134](https://openairdocs.org/sdr/HNAA2011051700134), May 2, 2011: SKIN. CORRODED. SEVERAL AREAS OF CORROSION AT UPPER END OF PAX DOOR SKIN. R & R PAX DOOR SKIN.
- [SDR HNAA2011051700133](https://openairdocs.org/sdr/HNAA2011051700133), May 2, 2011: FLOOR SUPPORT. CORRODED. LAV FLOOR ANGLE BRACKET IS CORRODED. REMOVED LOWER AND UPPER ANGLE. FABRICATED NEW ANGLES FROM 2024-T3 .040 ALUMINUM, ALODINED, PRIMED AND INSTALLED IAW DWG 825
- [SDR HNAA2011051700132](https://openairdocs.org/sdr/HNAA2011051700132), May 2, 2011: STRUCTURE. CRACKED. INTERNAL STRUCTURE HAS SMALL CRACKS EMINATING FROM A RIVET AT LOWER AFT CORNER ON LT MID EMERGENCY EXIT. FURTHER INSP FOUND STRUCTURE AT HOLE BOWED OUT, CAUSING
- [SDR HNAA2011051700131](https://openairdocs.org/sdr/HNAA2011051700131), May 2, 2011: FLAP TRACK. CORRODED. RT NR 1 FLAP TRACK HAS CORROSION ON THE MATING SURFACE AND HEAVY WEAR AND PITTING ON THE ROLLER SURFACE. R & R FLAP TRACK WITH NEW HARDWARE IAW AMM 57-50-11.
- [SDR HNAA2011042400078](https://openairdocs.org/sdr/HNAA2011042400078), Apr 14, 2011: MODULE. INOPERATIVE. EMERGENCY FLOOR PATH LIGHT IS INOP AT ROW 7. R & R LIGHT MODULE AS REQUIRED. OPS CHECKED GOOD.
- [SDR HNAA2011030900037](https://openairdocs.org/sdr/HNAA2011030900037), Mar 4, 2011: BULB. LOOSE. FIRST RED EMERGENCY FLOOR LIGHT INOP. .RESEATED EMERGENCY LIGHT IN SOCKET. OPS CHECKED GOOD.
- [SDR HNAA2011021500026](https://openairdocs.org/sdr/HNAA2011021500026), Feb 8, 2011: PRESSURE SWITCH. MALFUNCTIONED. ROLL SPOILER OTBD HYD CAUTION LIGHT ILLUMINATED ON CLIMB OUT AT 9000 FT AT 140 KNOTS. R & R PRESSURE SWITCH, GROUND RAN, OPS CHECKED GOOD. INSP, FOUND HYD QTY'S
- [SDR HNAA2010122100285](https://openairdocs.org/sdr/HNAA2010122100285), Dec 17, 2010: BULB. INOPERATIVE. EMERGENCY FLOOR PATH LIGHT IS INOP AT SEAT 5DF. R & R BULB IN EMERGENCY FLOOR PATH LIGHT AT ROW 5. OPS CKD GOOD.
- [SDR HNAA2010112200247](https://openairdocs.org/sdr/HNAA2010112200247), Nov 17, 2010: COMPUTER. MALFUNCTIONED. ON ROTATION, STICK SHAKER ACTIVATED FOR REMAINDER OF FLIGHT. R & R NR 1 COMPUTER AND CALIBRATED IAW MM 27-33-00. RECONNECTED SHAKERS, OPS CHECKED GOOD.
- [SDR HNAA2010063000158](https://openairdocs.org/sdr/HNAA2010063000158), Jun 6, 2010: OIL COOLER. LEAKING. IN FLIGHT, NR 1 ENGINE OIL PRESSURE DROPPED TO 40PSI FOR 3 MINUTES. SHUT NR1 ENGINE DOWN IAW CHECK LIST, LANDED NORMALLY WITH 1 ENGINE. INVESTIGATED, FOUND HELI
- [SDR HNAA2010042300119](https://openairdocs.org/sdr/HNAA2010042300119), Apr 19, 2010: BULB. INOPERATIVE. EMERGENCY LIGHT 26 BULBS INOP LOCATED AT CEILING ROW 4. R & R BULBS IAW 33-51-00.
- [SDR HNAA2010042300118](https://openairdocs.org/sdr/HNAA2010042300118), Apr 19, 2010: BULB. INOPERATIVE. EMERGENCY LIGHT, ONE BULB IN OP LOCATED AT ROW 1 FLOOR. R & R BULB IAW 33-51-00.
- [SDR HNAA2010042300117](https://openairdocs.org/sdr/HNAA2010042300117), Apr 19, 2010: BULB. INOPERATIVE. EMERGENCY LIGHT 8 BULBS IN OP LOCATED AT ROW 1 CEILING. R & R BULB IAW 33-51-00.
- [SDR HNAA2010042300116](https://openairdocs.org/sdr/HNAA2010042300116), Apr 19, 2010: BULB. INOPERATIVE. EMERGENCY LIGHT 12 BULBS IN OP ON ROW 1AC ON TOP OF PAX DOOR. R & R BULBS IAW 33-51-00.
- [SDR HNAA2010042300115](https://openairdocs.org/sdr/HNAA2010042300115), Apr 19, 2010: BULB. INOPERATIVE. EMERGENCY LIGHT BULB IN OP AT ROW 4AC ON SIDEWALL. R & R BULB IAW 33-51-00.
- [SDR HNAA 200909290029](https://openairdocs.org/sdr/HNAA%20200909290029), Sep 25, 2009: COVER. MISSING. EMERGENCY FLOOR PATH TRANSPARENT COVER IS MISSING. FORWARD MOST COVER. REMOVED AND REPLACED EMERGENCY FLOOR LIGHTING TRIM COVER AS REQUIRED. OPERATIONAL CHECK G
- [SDR HNAA2009092900205](https://openairdocs.org/sdr/HNAA2009092900205), Sep 25, 2009: COVER. MISSING. EMERGENCY FLOOR PATH TRANSPARENT COVER IS MISSING, FWD MOST COVER. REMOVED AND REPLACED FLOOR LIGHT TRIM COVER AS REQUIRED.
- [SDR HNAA2009090600281](https://openairdocs.org/sdr/HNAA2009090600281), Sep 5, 2009: BATTERY PACK. FAILED. RIGHT AFT EMERGENCY DITCHING LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT LOCATION/IDENT ROW 7DF (RIGHT SIDE)/ PS6, BATTERY REFERENCE DESI
- [SDR HNA2008F00018](https://openairdocs.org/sdr/HNA2008F00018), Jun 27, 2008: UNKNOWN. ODOR. UNKNOWN ELECTRICAL ODOR ACCOMPANIED BY LIGHT SMOKE. MAINT WAS ON AC FOR APPROX 2.5 HOURS, SUSPECT WATER GOT ON TOP OF ADVISORY DISPLAY PANEL WHICH WAS CURRENTLY
- [SDR HNAA0800121](https://openairdocs.org/sdr/HNAA0800121), Mar 30, 2008: HYDRAULIC LINE. CRACKED. ON TAXI OUT LOST HYDRAULIC QTY ON NR 2 SYSTEM WENT DOWN TO .6 QTS. RETURNED TO GATE. UPON INVESTIGATION FOUND LEFT OUTBOARD SPOILER ACTUATOR LINE LEAKING, MECHA
- [SDR HNAA0800094](https://openairdocs.org/sdr/HNAA0800094), Feb 21, 2008: TSCU. MALFUNCTIONED. ON TAKEOFF ROLE NR 2 PROP FEATHERED AT 30% TORQUE. ARM LIGHT WAS NOT ILLUMINATED. ABORTED TAKEOFF. UNABLE TO DUPLICATE PROBLEM. REPLACED NR 2 TSCU.
- [SDR HNAA0800060](https://openairdocs.org/sdr/HNAA0800060), Feb 6, 2008: CONTROL MODULE. FAILED. WHEN TESTED, THE NR 1 ENGINE FIRE EXTINGUISHER 'T' HANDLE WOULD NOT ILLUMINATE. MAINTENANCE CLEANED THE ELECTRICAL CONNECTOR BETWEEN THE 'T' HANDLE AND SHAFT, T
- [SDR HNAA0800052](https://openairdocs.org/sdr/HNAA0800052), Jan 27, 2008: SWITCH. FAILED. AS THE POWER LEVERS WERE BEING ADVANCED TO START THE TAKEOFF ROLL, THE AUTOFEATHER SYSTEM DID NOT ACTIVATE AND THE NR 2 ENGINE TORQUE INDICATION WENT TO 105% FO
- [SDR HNAA0800040](https://openairdocs.org/sdr/HNAA0800040), Jan 25, 2008: CONNECTOR. CONTAMINATED. WHEN PILOT ADVANCED POWER FOR TAKEOFF, THE NR 2 PROPELLER WENT INTO FEATHER UNCOMMANDED. THE PROP SPEED WAS APPROXIMATELY 1200 RPM AND REACHED A TORQUE OF 100-1
- [SDR HNAA0800024](https://openairdocs.org/sdr/HNAA0800024), Jan 2, 2008: LEVER. WORN. IN FLIGHT AIRCRAFT IS DIFFICULT TO TURN LEFT AND SPOILER NR 1 PUSH OFF LIGHT ILLUMINATES WHEN MAKING RIGHT TURNS. FOUND WIRES ON RIGHT HAND SPOILER CLUTCH UPPER
- [SDR HNAA0700161](https://openairdocs.org/sdr/HNAA0700161), Jul 30, 2007: WINDSHIELD. DAMAGED. THERE WAS A BIRD STRIKE NEAR THE F/O WINDSHIELD ON CLIMBOUT. THE FLIGHT WAS 20 MINUTES OUT OF CLT. THE FLIGHT CREW WAS HEARING A NOISE AND THEN IT WENT AWAY. FL
- [SDR HNAA0700155](https://openairdocs.org/sdr/HNAA0700155), Jul 25, 2007: LINE. LEAKING. HYD LEAK IN NR 2 GEAR WELL LEFT SIDE ABOVE JET PIPE. ROA MX CANNOT REACH LEAK, CREW WILL TAKE A/C TO HANGAR, LOOKING TO TAKE A/C 980 AS A SPARE WILL HAVE TO USE
- [SDR HNAA0700129](https://openairdocs.org/sdr/HNAA0700129), Jun 28, 2007: TRANSDUCER. MALFUNCTIONED. JUST AFTER ROTATION FROM LGA, THE STICK SHAKER WENT OFF. CAPTAIN QUICKLY RETURNED TO THE FIELD. CAPTAIN'S STALL WARNING HAS A PROBLEM. REMOVED AND REPLACED NR 1
- [SDR HNAA0700071](https://openairdocs.org/sdr/HNAA0700071), Apr 16, 2007: CONTROL HEAD. CONTAMINATED. NR 2 TRANSPONDER SMOKED THEN MADE POPPING NOISE THEN FAIL TO OPERATE, SUSPECT WATER IN NR 2 TRANSPONDER. REMOVED NR 2 TRANSPONDER CONTROLLER C/P. REMOVED AND RE
- [SDR HNAA0700070](https://openairdocs.org/sdr/HNAA0700070), Apr 16, 2007: VHF COMM. CONTAMINATED. 16APR07 - EXPERIENCE SMOKE IN COCKPIT, SMOKE COMING FROM NR 2 COMM DURING RUN UP, SUSPECT WATER IN NR 2 COMM. 17APR07 - REMOVED AND REPLACED NR 2 COM R/T, CONTR
- [SDR HNAA0600108](https://openairdocs.org/sdr/HNAA0600108), Aug 31, 2006: TRANSDUCER. FAILED. BOTH STICK SHAKERS ACTIVATED ON ROTATION AND STAYED ON UNTIL RETURN TO FIELD. REMOVED AND REPLACED LT TRANSDUCER. PART INFO TO FOLLOW
- [SDR HNAA0600085](https://openairdocs.org/sdr/HNAA0600085), Aug 12, 2006: STICK SHAKER. ACTIVATED. STICK SHAKER ACTIVATED ON TAKEOFF WITH OUT ASSOCIATED CAUTION LIGHTS. SYSTEM PLACED ON MEL....MORE TO FOLLOW.

All 85: https://openairdocs.org/deregistered/N906HA-2016-09-20/reports.md

## FAA accident and incident reports (4)

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 20030822018579I](https://openairdocs.org/incident/20030822018579I), Aug 22, 2003: Dhav DHC8102 (N906HA), Charlotte, NC, Minor damage. (-23) Due to impending weather, a piedmont aircraft (N906HA) was holding off taxiway charlie with both engines shut down and APU running. Thunderstorm hit the…
- [Incident 20020222001829I](https://openairdocs.org/incident/20020222001829I), Feb 22, 2002: Dhav DHC8102 (N906HA), Pittsburgh, PA. (-23) On February 22, 2002, at 1427E piedmont airlines flight 3310 returned to pit after reporting a gear retraction problem. The DHC-8 landed on runway 32,…
- [Incident 19930915041589I](https://openairdocs.org/incident/19930915041589I), Sep 15, 1993: Dhav DHC8102 (N906HA), Cleveland, OH, Minor damage. Unsafe landing gear indication. Made a tower fly by. Landed safely. Found pivot tube broken in nose gear assembly.
- [Incident 19911014052589I](https://openairdocs.org/incident/19911014052589I), Oct 14, 1991: Dhav DHC8102 (N906HA), White Plains, NY. Pilot had a TCAS alert on descent. Climbed to 5300 feet. Crew acted properlly. According to TCAS alert.

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