# N907HA: 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: 011
- Type of aircraft: Fixed wing multi engine
- Engine type: None
- Airworthiness: Standard, transport
- Airworthiness date: May 22, 1985
- Certificate issued: August 7, 2015
- Last registry action: August 7, 2015
- Mode S code: AC89DD
- 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/N907HA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=907HA
- Page: https://openairdocs.org/deregistered/N907HA-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 (145, newest 50)

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

- [SDR HNAA2014010300656](https://openairdocs.org/sdr/HNAA2014010300656), Jan 3, 2014: BULB. INOPERATIVE. NR 1 EMERGENCY LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.
- [SDR HNAA2013122500635](https://openairdocs.org/sdr/HNAA2013122500635), Dec 25, 2013: BULB. INOPERATIVE. EMERGENCY CEILING LIGHT IS INOPERATIVE AT ROW 5DF. R & R EMERGENCY CEILING LIGHT BULB AT ROW 5DF. OPS CHECKED GOOD.
- [SDR HNAA2013121600617](https://openairdocs.org/sdr/HNAA2013121600617), Dec 16, 2013: CONNECTOR. DIRTY. RUDDER TRIM INOPERATIVE. INSPECTED AND CLEANED ACTUATOR CONNECTOR. OPS CHECKED GOOD.
- [SDR HNAA2013101100533](https://openairdocs.org/sdr/HNAA2013101100533), Oct 11, 2013: HOSE. KINKED. F/O`S ASI READS HIGHER THAN CAPTAIN'S AFTER TAKEOFF AND FOR DURATION OF FLIGHT IAW CHECKLIST. SWITCHED TO ALT SOURCE. NO FIX, FOUND RT PITOT HOSE KINKED. REPLAC
- [SDR HNAA2013092000504](https://openairdocs.org/sdr/HNAA2013092000504), Sep 18, 2013: WIRE. DAMAGED. -ESCAPE PATH EMERGENCY LIGHT BULB IS INOPERATIVE AT ROW 8 . R & R LIGHT, AISLE MARKER DUE TO BAD WIRE CONNECTION.
- [SDR HNAA2013092000503](https://openairdocs.org/sdr/HNAA2013092000503), Sep 18, 2013: BULB. DIM. CABIN, CEILING EXIT SIGN AT CENTER ISLE OF ROW 1 IS DIM, R & R DIM LIGHTS OF CEILING EXIT SIGN AT CENTER ISLE OF ROW 1 OPS CHECKED GOOD, REINSTALLED CEILING COV
- [SDR HNAA2013080200441](https://openairdocs.org/sdr/HNAA2013080200441), Aug 2, 2013: CONTROL BOX. INOPERATIVE. NR 1 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED CONTINUOUSLY ON CLIMB. OIL PRESSURE INDICATED NORMAL- IN GREEN ARC. ENGINE WAS SHUTDOWN IN FLIGHT. CREW REPOR
- [SDR HNAA2013072200417](https://openairdocs.org/sdr/HNAA2013072200417), Jul 22, 2013: GARLOCK SEAL. DAMAGED. NR 1 OIL PRESSURE FLUCTUATED AND STEADILY FELL. FEATHERED NR 1 ENGINE AFTER PRESSURE FELL BELOW 55 PSI AND SHUTDOWN AFTER CONTINOUS ILLUMINATION OF CAUTION LIGH
- [SDR HNAA2013072200416](https://openairdocs.org/sdr/HNAA2013072200416), Jul 22, 2013: LINKAGE. MALFUNCTIONED. PSCS SHOWS RT INBD SPOILER DEPLOYED. FOUND RT INBD SPOILER SYNCRO TRANSMITTER LINKAGE OVER CENTERED. REPOSITION AND CHECKED SECURITY. GROUND RAN AND OPS CHECKED
- [SDR HNAA2013071500409](https://openairdocs.org/sdr/HNAA2013071500409), Jul 15, 2013: BULB. FAILED. ONE EMERGENCY FLOOR LIGHT IS INOPERATIVE AT ROW 9. R & R BULB AT ROW 9 EMERGENCY FLOOR PATH LIGHTING. OPS CHECKED GOOD.
- [SDR HNAA2013071000404](https://openairdocs.org/sdr/HNAA2013071000404), Jul 10, 2013: NONE. NONE. AISLE EMERGENCY LIGHT IS INOPERATIVE AT ROW 7. CYCLED SWITCH, FOUND LIGHT TO BE OPERATIONAL, OPS CHECKED GOOD.
- [SDR HNAA2013071000403](https://openairdocs.org/sdr/HNAA2013071000403), Jul 10, 2013: NONE. NONE. LEFT AFT EGRESS LIGHT BULB IS INOPERATIVE. CYCLED SWITCH, FOUND LIGHTS TO BE OPERATIONAL. OPS CHECKED GOOD.
- [SDR HNAA2013062600364](https://openairdocs.org/sdr/HNAA2013062600364), Jun 26, 2013: PSEU. MALFUNCTIONED. WOW CAUTION LIGHT ILLUMINATED ON LANDING ROLL FOR APPROX THREE SECONDS, THEN EXTINGUISHED. R & R PSEU IAW MM 32-61-50. CHECKED WOW SENSOR GAPS IAW MM 32-10-11.
- [SDR HNAA2013050100243](https://openairdocs.org/sdr/HNAA2013050100243), May 1, 2013: WIRE. DAMAGED. RT MLG ALTERNATE INDICATION IS INOPERATIVE. FOUND BROKEN WIRE. INSTALLED ENVIRONMENTAL SPLICE IAW STANDARD PRACTICE. OPS CHECKED GOOD. OK FOR SERVICE. LAST NIGH
- [SDR HNAA2013021900080](https://openairdocs.org/sdr/HNAA2013021900080), Feb 19, 2013: RELAY. FAILED. LT AC BUSS FAILURE IN FLIGHT WITH EMERGENCY LIGHTS FLICKERING. ALSO ASSOCIATED CAUTION LIGHTS ON. R & R 2421-S2 AND 2421-K2. RAN ENGINES FOR OVER 10 MINUTES. OP
- [SDR HNAA2013021500061](https://openairdocs.org/sdr/HNAA2013021500061), Feb 15, 2013: BULB. FAILED. 12TH EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE. R & R BULB FOR EMERGENCY FLOOR PATH LIGHT. OPS CHECKED GOOD.
- [SDR HNAA2013021500058](https://openairdocs.org/sdr/HNAA2013021500058), Feb 15, 2013: UNKNOWN. WARNING LIGHT. RT AC BUSS CAUTION LIGHT ILLUMINATED IN FLIGHT WITH ASSOCIATED CAUTION LIGHTS. PROBLEM OCCURED TWO MINUTES AFTER SELECTING PROP HEAT ON. ON PREVIOUS THREE LEGS,
- [SDR HNAA2013021100046](https://openairdocs.org/sdr/HNAA2013021100046), Feb 11, 2013: UNKNOWN. UNKNOWN. ON CLIMB OUT, LT AC BUSS, LT TRU AND LT ELEVATOR HORN HEAT CAUTION LIGHTS ILLUMINATED. RETURN TO FIELD. INSPECTED BOTH 1 AND 2 ENGINES PROP BRUSH BLOCKS AND CLE
- [SDR HNAA2013021100045](https://openairdocs.org/sdr/HNAA2013021100045), Feb 11, 2013: BRUSH BLOCK. SATURATED. ON CLIMBOUT, RT AC BUSS, RT TRU AND RT ELEVATOR HORN HEAT CAUTION LIGHTS CAME ON. STAYED ON FOR ENTIRE FLIGHT. NR 2 BRUSH BLOCK WAS OILED SOAKED. R & R NR 2 PRO
- [SDR HNAA2013021100043](https://openairdocs.org/sdr/HNAA2013021100043), Feb 11, 2013: GENERATOR. INOPERATIVE. ON CLIMB OUT, RT AC BUSS, RT TRU AND RT ELEVATOR HORN HEAT CAUTION LIGHTS ILLUMINATED. ACFT WAS AIR TURNBACK. R & R NR 2 AC GENERATOR, GCU IAW WC 24-20-11R. OPS
- [SDR HNAA2013020400031](https://openairdocs.org/sdr/HNAA2013020400031), Feb 4, 2013: CONNECTOR. SATURATED. DURING CRUISE FLIGHT AT 12K, SELECTED PROP HEAT ON AND RT AC BUSS FAULT OCCURED. INSPECTED BOTH PROP BRUSH BLOCKS, FOUND NR 2 PROP BRUSH BLOCK CONNECTOR PLUG SO
- [SDR HNAA2012111201041](https://openairdocs.org/sdr/HNAA2012111201041), Nov 12, 2012: WARNING LIGHT. FALSE ACTIVATION. RIGHT WINDSHIELD HOT LIGHT ILLUMINATED. INSPECTED SENSOR WIRING ARRANGEMENT. FOUND TO BE ON PRIMARY SENSOR. CHECKED SENSORS RESISTANCE. FOUND TO BE WITHIN LIMIT
- [SDR HNAA201210100110](https://openairdocs.org/sdr/HNAA201210100110), Oct 10, 2012: DOOR. OUT OF RIG. LEFT DOOR AMBER LIGHT REMAINED ILLUMINATED WITH GEAR UP. RECYCLED GEAR STILL ILLUMINATED. FORWARD DOOR REMAINED OPEN. ACFT RETURNED TO FIELD. RERIGGED NR 1 FORW
- [SDR HNAA2012100901009](https://openairdocs.org/sdr/HNAA2012100901009), Oct 9, 2012: BATTERY. FAILED. LEFT FORWARD EXTERIOR EMERGENCY LIGHT IS DIM. R & R BATTERY. OPS CHECKED GOOD.
- [SDR HNAA2012100901005](https://openairdocs.org/sdr/HNAA2012100901005), Oct 9, 2012: CONNECTOR. DAMAGED. FORWARD CENTER CEILING EMERGENCY EXIT SIGN IS INOP. FOUND FORWARD CENTER CEILING LIGHT WIRE UNPLUGGED AND MATRIX CONNECTOR DAMAGED. R & R MATRIX CONNECTOR AND P
- [SDR HNAA2012100300995](https://openairdocs.org/sdr/HNAA2012100300995), Oct 3, 2012: BOLT. CORRODED. RT WING TO FUSELAGE STRUT HAD RUSTED BOLT AND BORE INSIDE OF PANEL 264CR. CLEANED BORE WITH BARREL BRUSH. CORROSION WAS TRANSFERED FROM CORRODED BOLT. INSTALLED
- [SDR HNAA2012100300994](https://openairdocs.org/sdr/HNAA2012100300994), Oct 3, 2012: BOLT. CORRODED. AFT OTBD BOLT AND BORE IF LT AFT WING TO FUSELAGE STRUT IS RUSTED INSIDE OF PANEL 263CL. REAMED HOLE IAW DWG 85320339. CLEANED CORRSION, R & R BOLT AND PLI WASH
- [SDR HNAA2012100300993](https://openairdocs.org/sdr/HNAA2012100300993), Oct 3, 2012: BOLT. CORRODED. FORWARD INBD BOLT IS PITTED ON AFT STRUT, LT WING TO FUSELAGE ATTACH POINT. R & R BOLT AND PLI WASHERS.
- [SDR HNAA2012100300997](https://openairdocs.org/sdr/HNAA2012100300997), Oct 3, 2012: FLOORBEAM. CORRODED. UPPER BAG BAY FLOORBEAM ABOVE STR 31S AT BS 600 HAS CORROSION. REMOVED CORROSION FROM UPPER BAGBAY FLOORBEAM. ALODINED AND PRIMED AREA.
- [SDR HNAA2012100300996](https://openairdocs.org/sdr/HNAA2012100300996), Oct 3, 2012: BRACKET. CORRODED. SURFACE CORROSION AT ANGLE BRACKET JUST BELOW FLOOR AT STA X600 FRONT OF UPPER BAG BAY FLOOR. CORROSION WAS REMOVED, APPLIED ALODINE AND PRIMER TO ANGLE BRACKET
- [SDR HNAA2012100100991](https://openairdocs.org/sdr/HNAA2012100100991), Oct 1, 2012: BOLT. RUSTED. LEFT AFT STEEL STRUT TO WING RIB BOLT IS RUSTED AND BORE OF STRUT. REAMED HOLE TO .541 IAW DWG 85320229. CLEANED CORROSION AND R & R BOLT AND NEW PLI WASHERS.
- [SDR HNAA2012100100990](https://openairdocs.org/sdr/HNAA2012100100990), Oct 1, 2012: SEAT TRACK. CORRODED. MINOR CORROSION AT RIGHT OTBD SEAT TRACK AT BS 424. SEAT TRACK OUT OF LIMITS IAW RD8-53-1342. REMOVED & INSTALLED NEW SEAT TRACK IAW DWG 85320777.
- [SDR HNAA2012092800986](https://openairdocs.org/sdr/HNAA2012092800986), Sep 28, 2012: SEAT TRACK. CORRODED. SURFACE CORROSION AT LT OTBD SEAT TRACK AT BS 501. REMOVED CORROSION ON LT SEAT TRACK IAW RD8-53-1342. COMPLIED WITH HFEC INSPECTION. NO DEFECTS NOTED.
- [SDR HNAA2012092800985](https://openairdocs.org/sdr/HNAA2012092800985), Sep 28, 2012: SEAT TRACK. CORRODED. SURFACE CORROSION AT LT OTBD SEAT TRACK BS 387 THRU 366. SEAT TRACK DAMAGE IS OUT OF LIMITS. R & R SEAT TRACK IAW DWG 85320777.
- [SDR HNAA2012092800984](https://openairdocs.org/sdr/HNAA2012092800984), Sep 28, 2012: THRESHOLD. CORRODED. AIRSTAIR DOOR OPENING THRESHOLD HAS SURFACE CORROSION AROUND NUT PLACES ON TOP AND BOTTOM SIDES OF THRESHOLD. REMOVED AIRSTAIR DOOR OPENING THRESHOLD AND INSTAL
- [SDR HNAA2012092800983](https://openairdocs.org/sdr/HNAA2012092800983), Sep 28, 2012: SHEAR TIE. CORRODED. CORROSION ON FRAME LEG AT STA X270.500 BETWEEN STR 32P AND 31P. CLEANED CORROSION, APPLIED ALODINE AND PRIMER.
- [SDR HNAA2012092800982](https://openairdocs.org/sdr/HNAA2012092800982), Sep 28, 2012: SEAT TRACK. CORRODED. SURFACE CORROSION AT LT INBD SEAT TRACK AT BS 330. BLENDED AFFECTED AREA TO WITHIN LIMITS OF RD8-53-1339. HFEC INSPECTION COMPLIED WITH. NO DEFECTS NOTED.
- [SDR HNAA2012092800981](https://openairdocs.org/sdr/HNAA2012092800981), Sep 28, 2012: FLOORBEAM. CORRODED. SURFACE CORROSION AT BS 467 FLOORBEAM JUST BELOW LT AND RT INBD SEAT TRACK. CLEANED CORROSION . APPLIED ALODINE AND PRIMER.
- [SDR HNAA2012092600976](https://openairdocs.org/sdr/HNAA2012092600976), Sep 26, 2012: SHEAR TIE. CORRODED. FRAME LEG AT STATION X222 HAS SURFACE CORROSION BETWEEN STR 28S AND 29S. REMOVED CORROSION AT FRAME LEG STA X222 BETWEEN STR 28S AND 29S. APPLIED ALODINE AND PR
- [SDR HNAA2012092600975](https://openairdocs.org/sdr/HNAA2012092600975), Sep 26, 2012: FRAME. CORRODED. STRINGER 31S AND FRAME LEG IS CORRODED AT STATION X222. CLEANED CORROSION FROM FRAME LEG AND STRINGER 31S AT STA X222. APPLIED ALODINE AND PRIMED AREA.
- [SDR HNAA2012092600974](https://openairdocs.org/sdr/HNAA2012092600974), Sep 26, 2012: SHEAR TIE. CORRODED. CORROSION AT FRAME LEG X240.500 BETWEEN STR. 28P AND 27P. REMOVED BRACKET FROM FRAME AT STA.X240.500. REMOVED FRAME SECTION AT STA X240.500, FORMED AND HEAT TRE
- [SDR HNAA2012092600973](https://openairdocs.org/sdr/HNAA2012092600973), Sep 26, 2012: STRINGER. CORRODED. CORROSION AT STRINGER 28P WHERE IT MEETS MAIN FRAME X387 .350. REMOVED BRACKET ON STRINGER 28P ATTACH POINT TO MAIN FRAME X387.350. CLEANED MINOR SURFACE CORROS
- [SDR HNAA2012092600972](https://openairdocs.org/sdr/HNAA2012092600972), Sep 26, 2012: SHEAR TIE. CORRODED. FRAME LEG AT STATION X242 BETWEEN STR 31S AND 30S HAS SURFACE CORROSION. REMOVED CORROSION FROM FRAME LEG AT STA X242 BETWEEN STR 31S AND 30S. APPLIED ALODINE A
- [SDR HNAA2012092600971](https://openairdocs.org/sdr/HNAA2012092600971), Sep 26, 2012: STRINGER. CORRODED. STRINGER 31S HAS CORROSION BETWEEN FRAME X242 AND X201. REPAIRED IAW RD8-53-3044. PERFORMED HFEC INSPECTION. NO DEFECTS NOTED. APPLIED ALODINE AND EPOXY PRIMER 
- [SDR HNAA2012092600970](https://openairdocs.org/sdr/HNAA2012092600970), Sep 26, 2012: FLOOR SUPPORT. CORRODED. SEVERAL AREAS OF LIGHT CORROSION ON OTBD FLOOR SUPPORT, AROUND AFT ATTACH HOLE FOR WARDROBE FLOOR. CLEANED CORROSION FROM OTBD FLOOR SUPPORT. ALODINED AND PRIME
- [SDR HNAA2012092600969](https://openairdocs.org/sdr/HNAA2012092600969), Sep 26, 2012: DOOR. CORRODED. LAVATORY SERVICE DOOR IS CORRODED. REMOVED CORRODED LAVATORY DOOR. INSTALLED NEW LAVATORY DOOR ASSY IAW DWG 85320983.
- [SDR HNAA2012092600968](https://openairdocs.org/sdr/HNAA2012092600968), Sep 26, 2012: DOUBLER. CORRODED. LAVATORY MACHINED DOUBLER ON CUTOUT IS CORRDED. REMOVED MACHINE DOUBLER, INSTALLED NEW MACHINED DOUBLER IAW DWG 85320983.
- [SDR HNAA2012092500967](https://openairdocs.org/sdr/HNAA2012092500967), Sep 25, 2012: FRAME. CORRODED. CORROSION AT FRAME STA X434.500 AND STR 22P. REMOVED 1 AFT ANGLE AT MAIN FRAME, STRINGER TO SEAT RAIL WEB AND ANGLE FROM STA 443, STRINGER TIE. CLEANED, BLENDED
- [SDR HNAA2012092500966](https://openairdocs.org/sdr/HNAA2012092500966), Sep 25, 2012: FRAME. CORRODED. CORROSION AT FRAME BS 445.500 AND STR. 22P. REMOVED CLEAT AND BLENDED TO WITHIN LIMITS IAW SRM 51-20-11. ALODINE AND PRIMED. REINSTALLED IAW DWG 85320511.
- [SDR HNAA2012092500965](https://openairdocs.org/sdr/HNAA2012092500965), Sep 25, 2012: FRAME. CORRODED. CORROSION AT "L" BRACKET ON BOTH SIDES OF MAIN FRAME STA X383, STR 22P. REMOVED FORWARD AND AFT ANGLE ON MAIN FRAME AT STA.X387. BLENDED LIGHT CORROSION TO WITH

All 145: https://openairdocs.org/deregistered/N907HA-2016-09-20/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 20070429008119I](https://openairdocs.org/incident/20070429008119I), Apr 29, 2007: Dhav DHC8102 (N907HA), Charlotte, NC, Minor damage. (-23) After departure at 2117 a bad smell was noticed in the cabin of hnaa flight 4242 by passengers and the fa, shortly after, hyd fluid (skydrol) leaked into…

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