# N943HA: 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: 167
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: August 30, 1989
- Certificate issued: November 16, 2017
- Last registry action: June 15, 2018
- Mode S code: AD18FD
- 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/N943HA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=943HA
- Page: https://openairdocs.org/deregistered/N943HA-2019-03-04

From the FAA registry file of November 3, 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 HNAA2017042500138](https://openairdocs.org/sdr/HNAA2017042500138), Apr 27, 2017: BULB. INOPERATIVE. F/A PANEL EMERGENCY LIGHT SWITCH NORM INDICATING BULB INOPERATIVE. R & R THE BULB.
- [SDR HNAA2017032300094](https://openairdocs.org/sdr/HNAA2017032300094), Mar 21, 2017: WARNING LIGHT. ACTIVATED. LEFT AMBER DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION, CYCLED GEAR IAW CHECK LIST AND LIGHT EXTINGUISHED.
- [SDR HNAA2017022400064](https://openairdocs.org/sdr/HNAA2017022400064), Feb 24, 2017: ACTUATOR. OUT OF ADJUST. LEFT AMBER GEAR DOOR LIGHT REMAINED ON AFTER GEAR RETRACTION. ADJUSTED THE NR 1 FORWARD GEAR DOOR ACTUATOR AND OPS CHECKED GOOD.
- [SDR HNAA2017020800049](https://openairdocs.org/sdr/HNAA2017020800049), Feb 3, 2017: BULB. BURNED OUT. EMERGENCY LIGHTS INOPERATIVE. REMOVED & REPLACED THE BULBS. OPS CHECKED GOOD.
- [SDR HNAA2017020800048](https://openairdocs.org/sdr/HNAA2017020800048), Feb 3, 2017: BULB. INOPERATIVE. PAX DOOR EMERGENCY LIGHT DIM. REMOVED & REPLACED THE BULBS, OPS CHECKED GOOD.
- [SDR HNAA2017011600018](https://openairdocs.org/sdr/HNAA2017011600018), Jan 16, 2017: BULB. INOPERATIVE. EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD.
- [SDR HNAA2016121300388](https://openairdocs.org/sdr/HNAA2016121300388), Dec 12, 2016: BATTERY PACK. INOPERATIVE. EMERGENCY CEILING LIGHT AT ROW 4 INOPERATIVE. R & R THE BATTERY AT ROW 3AC IAW 33-51-00.
- [SDR HNAA2016042700123](https://openairdocs.org/sdr/HNAA2016042700123), Apr 25, 2016: BATTERY PACK. DISCHARGED. SEVERAL EMERGENCY LIGHTS OUT DUE TO SWITCH LEFT ON. R & R EMERGENCY LIGHT BATTERIES IAW W/C 33-50-05R.
- [SDR HNAA2016042100111](https://openairdocs.org/sdr/HNAA2016042100111), Apr 18, 2016: PLATE. CORRODED. PASSENGER DOOR AFT GOOSE NECK HARDWARE RENTION PLATE BADLY CORRODED, LOCATED ADJACENT TO TOP STEP 12668. FABRICATED PLATE AND R & R PAX DOOR AFT GOOSE NECK HARD
- [SDR HNAA2015110400324](https://openairdocs.org/sdr/HNAA2015110400324), Nov 4, 2015: BULB. INOPERATIVE. FORWARD LT FUSELAGE EMERGENCY LIGHT IS INOPERATIVE. R & R BULB, OPS CHECKED GOOD.
- [SDR HNAA2015092300284](https://openairdocs.org/sdr/HNAA2015092300284), Sep 23, 2015: BULB. INOPERATIVE. ROW 9DF FLOOR EMERGENCY LIGHT IS OUT. REMOVED LENS, R & R ROW 9DF FLOOR EMERGENCY LIGHT, RESECURED LENS WITH RETAINED HARDWARE.
- [SDR HNAA2015090200269](https://openairdocs.org/sdr/HNAA2015090200269), Sep 2, 2015: UNKNOWN. UNKNOWN. EMERGENCY LIGHTS IN THE CABIN AND BOTH INTAKE BYPASS AMBER LIGHTS FLICKERING IN FLIGHT. ONLY WITH BOTH PROPELER RPM AT 1050. PROPELLER HEAT WAS OFF. CLEANED BOT
- [SDR HNAA2015082100260](https://openairdocs.org/sdr/HNAA2015082100260), Aug 21, 2015: BULB. DIM. DIM LT AFT FUSELAGE EMERGENCY LIGHT. R & R BULB FOR LT AFT FUSELAGE LIGHT. OPS CHECKED GOOD.
- [SDR HNAA2015070600213](https://openairdocs.org/sdr/HNAA2015070600213), Jul 6, 2015: WARNING LIGHT. ILLUMINATED. RIGHT AC BUSS AND RT TRU ILLUMINATED DURING FLIGHT. R & R NR 2 AC GENERATOR IAW WORK CARD 24-20-11R. OPS CHECKED GOOD.
- [SDR HNAA2015060100177](https://openairdocs.org/sdr/HNAA2015060100177), Jun 1, 2015: BULB. INOPERATIVE. MIDDLE OVERHEAD CABIN EMERGENCY EXIT LIGHT IS INOPERATIVE. R & R BULB IN OVERHEAD EMERGENCY EXIT LIGHT. OPS CHECKED GOOD.
- [SDR HNAA2014102000294](https://openairdocs.org/sdr/HNAA2014102000294), Oct 20, 2014: VALVE. MALFUNCTIONED. NR 2 OIL TEMP DROPS TO 45-50 DEGREES IN CLIMB WITH SAT OF -4 DEGREES C WITH LOW ALT SAT OF +15 DEGREES C IN CRUISE. NR 2 OIL TEMP IS 50-55 DEGREES C. RETURN TO 
- [SDR HNAA2014032800111](https://openairdocs.org/sdr/HNAA2014032800111), Mar 28, 2014: BULB. INOPERATIVE. PAX DOOR FLOOR EMERGENCY LIGHT BULB IS INOPERATIVE. R & R BULB, OPS CHECKED GOOD.
- [SDR HNAA2014022400056](https://openairdocs.org/sdr/HNAA2014022400056), Feb 24, 2014: LAMP. INOPERATIVE. EMERGENCY LIGHT INOPERATIVE AT ROW 1. R & R EMERGENCY LIGHT LAMP AT ROW 1. OPS CHECKED GOOD.
- [SDR HNAA2014012700021](https://openairdocs.org/sdr/HNAA2014012700021), Jan 27, 2014: BATTERY PACK. INOPERATIVE. EMERGENCY FLOOR LIGHTS ARE INOPERATIVE. R & R EMERGENCY LIGHT BATTERIES IAW WC 33-50-05R AND 33-50-03Q. OPS CHECKED GOOD.
- [SDR HNAA2014010300652](https://openairdocs.org/sdr/HNAA2014010300652), Jan 3, 2014: CONTROLLER. FAILED. RIGHT WINDSHIELD HOT CAUTION LIGHT ILLUMINATED WITH WINDSHIELD SELECTED TO NORMAL. R & R RIGHT WINDSHIELD CONTROLLER. GROUND RAN ACFT. OPS CHECKED GOOD IAW MM 3
- [SDR HNAA2013060500325](https://openairdocs.org/sdr/HNAA2013060500325), Jun 5, 2013: BULB. INOPERATIVE. RED EMERGENCY PATHWAY LIGHT IS INOPERATIVE. R & R BULB IAW AMM 33-51-00.
- [SDR HNAA2013051000261](https://openairdocs.org/sdr/HNAA2013051000261), May 10, 2013: TRANSCEIVER. INOPERATIVE. RADAR INOPERATIVE, PAINTS INACCURATE WEATHER BEYOND 20 MILES. R & R RADAR TRANSCEIVER IAW MM 34-41-04 AND BULLETIN 34-18. OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR HNAA2013041500220](https://openairdocs.org/sdr/HNAA2013041500220), Apr 14, 2013: BRUSH BLOCK. MALFUNCTIONED. EMERGENCY LIGHTS FLICKERING IN FLT (PROP HEAT OFF) F/A PANEL LIGHTING INTERMITTENT IN FLT ALSO, CLEANED AND RESEATED BRUSH BLOCKS ON NR 1 AND NR 2 ENGINES. UPPE
- [SDR HNAA2013021900077](https://openairdocs.org/sdr/HNAA2013021900077), Feb 19, 2013: WIRE. BROKEN. AFTER GEAR EXTENSION, CREW HEARD A SINGLE POP NOISE, THEN AFTER ROLL OUT, WHEN FLAPS WHERE SELECTED TO 5 DEGREES FROM 15 DEGREES, FLAPS DID NOT MOVE. BUT WHEN Z
- [SDR HNAA2013020800037](https://openairdocs.org/sdr/HNAA2013020800037), Feb 8, 2013: BULB. FAILED. EMERGENCY CEILING LIGHT IS INOPERATIVE AT ROW 3. R & R BULB. OPS CHECKED GOOD.
- [SDR HNAA2013011400008](https://openairdocs.org/sdr/HNAA2013011400008), Jan 14, 2013: BULB. INOPERATIVE. SIDEWALL LIGHT IS DIM AT ROW 4DF. R & R BULB.
- [SDR HNAA2013010701151](https://openairdocs.org/sdr/HNAA2013010701151), Jan 7, 2013: LAMP. INOPERATIVE. EMERGENCY CEILING LIGHT AT ROW 10 IS DIM. REPLACED LAMP, INSTALLED COVER. OPS CHECKED GOOD.
- [SDR HNAA2012112701075](https://openairdocs.org/sdr/HNAA2012112701075), Nov 27, 2012: ACTUATOR. LEAKING. HYDRAULIC QTY DROPPED TO 1QT. JUST BEFORE TAKEOFF AND ISO VALVE CAUTION LIGHT ILLUMINATED. SERVICED NR 1 HYD AND OPERATED NR1 HYD SYS AND FOUND RT INBD SPOILER 
- [SDR HNAA2012082000922](https://openairdocs.org/sdr/HNAA2012082000922), Aug 20, 2012: BULB. FAILED. SECOND MOST FORWARD EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE. R & R FLOOR PATH LIGHT BULB. OPS CHECKED GOOD.
- [SDR HNAA2012071600867](https://openairdocs.org/sdr/HNAA2012071600867), Jul 16, 2012: BULB. FAILED. ROW 5, OVERHEAD EMERGENCY LIGHT IS INOPERATIVE. REMOVED LIGHT LENS PANEL, R & R BULB. OPS CHECKED GOOD. INSTALLED PANEL WITH RETAINED HARDWARE.
- [SDR HNAA2012071300858](https://openairdocs.org/sdr/HNAA2012071300858), Jul 13, 2012: SEAT TRACK. CORRODED. CORROSION ON RT INBD SEAT TRACK AROUND ATTACH POINT FOR GALLEY. REMOVED CORRODED PORTION OF SEAT TRACK IAW RD8-53-3074. SPLICE IN NEW PORTION OF SEAT TRACK IAW 
- [SDR HNAA2012071300863](https://openairdocs.org/sdr/HNAA2012071300863), Jul 13, 2012: FITTING. CORRODED. BOTTOM OF AIRSTAIR DOOR OPENING THRESHOLD FITTING IS CORRODED. R & R THRESHOLD MEMBER IAW ENG DWG 85321241.
- [SDR HNAA2012071300862](https://openairdocs.org/sdr/HNAA2012071300862), Jul 13, 2012: STRINGER. CORRODED. CORROSION AT STR 31P AND FRAME X201.300 ON THE LT SIDE OF TENSION FITTING. BLENDED CORROSION IAW SRM 51-20-11, ALODINED AND PRIMED AREA IAW SRM 51-20-16 AND 51-
- [SDR HNAA2012071300861](https://openairdocs.org/sdr/HNAA2012071300861), Jul 13, 2012: STRINGER SPLICE. CORRODED. CORROSION AT STRINGER 32S AND AFT OF FRAME 488.500. REMOVED STRINGER SPLICE AT BS 488.5. REMOVED STRINGER SECTION FROM BS 488.5 THROUGH 528. REINSTALLED STRINGE
- [SDR HNAA2012071300860](https://openairdocs.org/sdr/HNAA2012071300860), Jul 13, 2012: STRINGER. CORRODED. CORROSION ON STRINGER 31S BETWEEN BS 445.500 AND 467.000. BLENDED CORROSION IAW SRM 51-20-11, ALODINE AND PRIMED IAW SRM 51-20-16, 51-20-36.
- [SDR HNAA2012071300859](https://openairdocs.org/sdr/HNAA2012071300859), Jul 13, 2012: FRAME. CORRODED. MINOR CORROSION ON FRAME LEG AT BS 436.500 AND STR 31S. BLENDED CORROSION IAW SRM 51-20-11, ALODINED AND PRIMED IAW SRM 51-20-16, 51-20-36.
- [SDR HNAA2012071200856](https://openairdocs.org/sdr/HNAA2012071200856), Jul 12, 2012: FRAME. CORRODED. MINOR CORROSION AT BOTTOM OF VERTICAL FRAME MEMBER AT STA X510.00 BETWEEN STR 32S AND 31S. BLENDED CORROSION IAW SRM 51-20-11, ALODINED, PRIMED AREA IAW SRM 51-
- [SDR HNAA2012071200855](https://openairdocs.org/sdr/HNAA2012071200855), Jul 12, 2012: FRAME. CORRODED. CORROSION AT FRAME LEG STA X531.5 BETWEEN STR 32S AND 31S. BLENDED CORROSION IAW SRM 51-20-11, ALODINED, PRIMED AREA IAW SRM 51-20-16, 51-20-36.
- [SDR HNAA2012071200854](https://openairdocs.org/sdr/HNAA2012071200854), Jul 12, 2012: STRINGER. CORRODED. CORROSION ON STR 31S, JUST AFT OF FRAME BS 445.5.
- [SDR HNAA2012071200850](https://openairdocs.org/sdr/HNAA2012071200850), Jul 12, 2012: HINGE FITTING. CORRODED. LAVATORY SERVICE AREA DOUBLER HINGE AND DOOR ARE CORRODED. R & R LAVATORY DOUBLER AND DOOR ASSY IAW DWG 85320983.
- [SDR HNAA2012071100849](https://openairdocs.org/sdr/HNAA2012071100849), Jul 11, 2012: SKIN. DEBONDED. SKIN DISBONDED ALONG STR 32S FROM X506 TO X520 AND AT FRAME X510 AT FRAME LEGS INBD AND OTBD OF STR 32S. REMOVED RIVETS IN FRAME X510 FROM STR 30S TO 31P, FROM 
- [SDR HNAA2012051400773](https://openairdocs.org/sdr/HNAA2012051400773), May 14, 2012: WIRE. LOOSE. ROLL SPOILER INBD HYD CAUTION LIGHT ILLUMINATED IN FLIGHT. REPLACED CONNECTOR ON INBD ROLL SPOILER HYD PRESSURE SWITCH IN NR 1 NACELLE. GROUND RAN ACFT. COULD N
- [SDR HNAA2012040200716](https://openairdocs.org/sdr/HNAA2012040200716), Apr 2, 2012: RELAY. FAILED. APU FAILED AFTER RUNNING APPROX.30 MINUTES, FAULT LIGHT CAME ON FOLLOWED BY CHECK FIRE DETECT LIGHT COMING ON. APU FIRE DETECTION SYS DEACTIVATED IAW S/P APPEND
- [SDR HNAA2011122300437](https://openairdocs.org/sdr/HNAA2011122300437), Dec 23, 2011: LAMP. FAILED. AFT EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT ROW 9. R & R LAMP MODULE. OPS CHECKED GOOD.
- [SDR HNAA2011090100265](https://openairdocs.org/sdr/HNAA2011090100265), Aug 23, 2011: LAMP. INOPERATIVE. ROW 4 WALL EMERGENCY LIGHTS ARE INOPERATIVE. RELAMPED ROW 4 SIDEWALL EMERGENCY LIGHTS. OPS CHECKED GOOD.
- [SDR HNAA2011061300171](https://openairdocs.org/sdr/HNAA2011061300171), Jun 9, 2011: BATTERY. FAILED. LEFT AFT EMERGENCY EGRESS LIGHT INOP. R & R BULB, PN 81. NO FIX. R & R EMERGENCY LIGHT BATTERY AT POSITION PS3. OPS CHECKED GOOD.
- [SDR HNAA2011061300165](https://openairdocs.org/sdr/HNAA2011061300165), Jun 4, 2011: BULB. BURNED OUT. ROW 9 EMERGENCY FLOOR ESCAPE PATH LIGHT INOP. R & R BULB, OPS CHECKED GOOD.
- [SDR HNAA2011021500012](https://openairdocs.org/sdr/HNAA2011021500012), Feb 3, 2011: LIGHT. INOPERATIVE. EMERGENCY FLOOR PATH LIGHT IS INOP AT ROW 1. R & R MARKER AS REQUIRED, OPS CHECKED.
- [SDR HNAA20122100287](https://openairdocs.org/sdr/HNAA20122100287), Dec 17, 2010: BULB. INOPERATIVE. ROW 4DF AND 4AC EMERGENCY EXIT LIGHTS HAVE 1 BULB INOP. R & R BULB IN ROW 4 EMERGENCY EXIT LIGHTS. OPS CHECKED GOOD.
- [SDR HNAA2010042300114](https://openairdocs.org/sdr/HNAA2010042300114), Apr 19, 2010: BULB. INOPERATIVE. EMERGENCY LIGHT BULB IN OP ON ROW 4A SIDEWALL. R & R LIGHT BULB IAW 33-51-00.

All 80: https://openairdocs.org/deregistered/N943HA-2019-03-04/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 19970822028579I](https://openairdocs.org/incident/19970822028579I), Aug 22, 1997: Dhav DHC8102 (N943HA), Baltimore, MD. Narrative: on Friday, 08-22-97, this aircraft experienced a roll control disconnect on landing at bwi. This is the 5th occurrence of this type at piedmont…

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