# N410QX: 2001 Bombardier DHC-8-402, registration cancelled 2019-12-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 23, 2019 - Exported to: Peru - Status when cancelled: Valid registration - Airframe: [Bombardier DHC-8-402](https://openairdocs.org/model/bombardier-dhc-8-402) (registry code 1390042) - Engine: [Pratt & Whitney Canada PW150A](https://openairdocs.org/engine/pratt-whitney-canada-pw150a) (registry code 52167) - Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM), [TCDS E00062EN](https://openairdocs.org/tcds/E00062EN) (OpenAirDocs) - Serial number: 4053 - Year built: 2001 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: May 2, 2005 - Certificate issued: October 16, 2019 - Last registry action: November 15, 2019 - Mode S code: A4D594 - Owner when cancelled: [Aviation Marketing Group Inc](https://openairdocs.org/faa-owner/AVIATION%20MARKETING%20GROUP%20INC) - Location: [Fort Mill, SC](https://openairdocs.org/faa-place/SC/Fort%20Mill) - Owner type: Corporation - Owner's area on the map: 35.0110° N, 80.9276° W: Placed by OpenAirDocs at the center of ZIP code 29715, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N410QX - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=410QX - Page: https://openairdocs.org/deregistered/N410QX-2019-12-23 From the FAA registry file of November 7, 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 Bombardier DHC-8-402: https://openairdocs.org/model/bombardier-dhc-8-402.md ## Service difficulty reports (536, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR QXEA2018042000154](https://openairdocs.org/sdr/QXEA2018042000154), Apr 18, 2018: POWER SUPPLY. WEAK. BATTERY PACKS FOR EMERGENCY LIGHTS ARE WEAK. REPLACED THE BATTERY PACK POWER SUPPLY. - [SDR QXEA2018011200014](https://openairdocs.org/sdr/QXEA2018011200014), Jan 12, 2018: CIRCUIT CARD. MALFUNCTIONED. READING LIGHT ABOVE ROW 15 AB OVERHEATING. REMOVED FROM SERVICE. REPLACED THE CIRCUIT CARD, OPS CHECKED GOOD. RETURNED TO SERVICE. - [SDR QXEA2017120800694](https://openairdocs.org/sdr/QXEA2017120800694), Dec 7, 2017: WARNING MESSAGE. FALSE ACTIVATION. PITCH TRIM CAUTION OBSERVED DURING T/O. ABORTED TAKEOFF. RETURN TO GATE. INTERAGATED CDS FOUND CPILTRIM SW FAILURE, ALSO FOUND FAULT FCECU FAILURE E2, C/W FIM T - [SDR QXEA2017101300614](https://openairdocs.org/sdr/QXEA2017101300614), Oct 12, 2017: LIGHT. LOOSE. EMERGENCY LIGHT NEAR THE FWD GALLEY IS COMING LOOSE. SECURED THE LIGHT. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE. - [SDR QXEA2017082800536](https://openairdocs.org/sdr/QXEA2017082800536), Aug 27, 2017: WARNING LIGHT. FALSE ACTIVATION. INTERMITENT FUSELAGE DOOR WARNING LIGHT. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED AIRCRAFT FROM SERVICE. PERFORMED GVI OF AFT BAGGAGE DOOR & NO DEFECTS WE - [SDR QXEA2017061900425](https://openairdocs.org/sdr/QXEA2017061900425), Jun 17, 2017: WARNING MESSAGE. FALSE ACTIVATION. FLAP POWER CAUTION ILLUMINATED AFTER TAKEOFF, FLAPS STUCK AT 15. RETURNED TO FIELD AND LANDING UNEVENTFUL. FLAPS CHECKED GOOD IAW 27-50-00-710-801. COULD NOT DU - [SDR QXEA2017061200410](https://openairdocs.org/sdr/QXEA2017061200410), Jun 11, 2017: LIGHT. MISSING. IN MCD ENTRYWAY, MISSING A PART OF THE EMERGENCY LIGHTING STRIP. INSTALLED AND SEALED MISSING LIGHTNING STRIP AS NECESSARY. - [SDR QXEA2017061300418](https://openairdocs.org/sdr/QXEA2017061300418), May 31, 2017: STRINGER. CORRODED. STRINGER 25L HAS EVIDENCE OF CORROSION FORE & AFT OF FRAME BS 196. REMOVED AND BLENDED CORROSION ON THE FRAME IAW SRM 53-00-00, REPAIR -09. PERF'D E/T AND U/T I - [SDR QXEA2017061300417](https://openairdocs.org/sdr/QXEA2017061300417), May 23, 2017: CHANNEL. CORRODED. FWD PAX DOOR THRESHOLD CHANNEL AT STRINGER 23L HAS EVIDENCE OF CORROSION. REMOVED FWD PAX DOOR THRESHOLD CHANNEL IAW SRM 51-42-05-02-01. INSTALLED NEW FWD PAX D - [SDR QXEA2017061300419](https://openairdocs.org/sdr/QXEA2017061300419), May 13, 2017: SEAT TRACK. CORRODED. SEAT TRACK 9 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-15, 51-42-05, SRM 51-42-05-02-01 AND 51-40-15-02-01. - [SDR QXEA2017051700360](https://openairdocs.org/sdr/QXEA2017051700360), May 13, 2017: FRAME. CORRODED. FRAME FLANGE ON AFT SIDE OF BS 301 BETWEEN STRINGERS 31 AND 32R HAS EVIDENCE OF SURFACE CORROSION. REMOVED & BLENDED ALL CORROSION IAW SRM 53-00-00, REPAIR 09. - [SDR QXEA2017051700359](https://openairdocs.org/sdr/QXEA2017051700359), May 13, 2017: STRAP. CORRODED. INTERNAL FUSELAGE LONGITUDINAL SKIN STRAP BETWEEN STRINGERS. 31 AND 32L HAS EVIDENCE OF SURFACE CORROSION 4 INCHES FORWARD OF FRAME BS 176. REMOVED AND BLENDED - [SDR QXEA2017051200354](https://openairdocs.org/sdr/QXEA2017051200354), May 11, 2017: SEAT TRACK. CORRODED. SEAT TRACK 10 CORRODED. . REMOVED THE SEAT TRACK IAW SRM 51-41-00-00-01. INSTALLED A NEW SEAT TRACK IAW SRM 51-41-00-00-01 & SRM 51-40-15. - [SDR QXEA2017051700358](https://openairdocs.org/sdr/QXEA2017051700358), May 8, 2017: SEAT TRACK. CORRODED. SEAT TRACK BS 670 - 701 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05-02-01, 51-41-00-00-01 AND DWG 85338201. - [SDR QXEA2017050200335](https://openairdocs.org/sdr/QXEA2017050200335), Apr 30, 2017: SEAT TRACK. CORRODED. SEAT TRACK 15 REQUIRES REPLACEMENT DUE TO CORROSION. REMOVED SEAT TRACK 15 REF SRM 51-42-05 REPAIR-01. INSTALLED SEAT TRACK 15 (NEW) REF SRM 51-42-05-02-01 AND - [SDR QXEA2017032200165](https://openairdocs.org/sdr/QXEA2017032200165), Mar 21, 2017: CAM FOLLOWER. MALFUNCTIONED. AFT SERVICE DOOR HARD TO OPEN. REMOVED & REPLACED UPPER AFT CAM FOLLOWER IAW AMM 52-41-11-000-801/400-801. DOOR OPEN & CLOSE FREELY. NO OTHER DEFECTS NOTED. RET - [SDR QXEA2017031700130](https://openairdocs.org/sdr/QXEA2017031700130), Mar 16, 2017: SPRING. WORN. F/A REPORTED THAT THE EMERGENCY ACCESS DOOR BELOW THE JUMPSEAT DOES NOT SPRING CLOSED PROPERLY. REPLACED THE WORN HINGE SPRING IN THE COMPARTMENT DOOR. OPERATIO - [SDR QXEA2016112100734](https://openairdocs.org/sdr/QXEA2016112100734), Nov 19, 2016: TRANSDUCER. DAMAGED. ON TAKEOFF ROLL AT 30-40 KTS, MASTER CAUTION & OUTBD ANTISKID LIGHTS ILLUMINATED. AFTER COMPLYING WITH E&A CHECKLIST ANTISKID LIGHT REMAINED ILLUMINATED THROUGH - [SDR QXEA2016101800652](https://openairdocs.org/sdr/QXEA2016101800652), Oct 14, 2016: PUMP. FAILED. UPON GEAR RETRACTION ON TAKEOFF NR 2 HYD PUMP CAUTION, NR 2 RUD CTRL, NR 2 HYD ISO VALVE CAME ON. THE RT MLG DID NOT RETRACT. THE NR 2 HYD QTY , AND NR 2 HYD PR - [SDR QXEA2016090600573](https://openairdocs.org/sdr/QXEA2016090600573), Sep 7, 2016: ROD. OUT OF ADJUST. AFT GALLEY SERVICE DOOR HARD TO OPEN. CLEANED AFT SERVICE DOOR SEAL IAW MCN:652643-01 ISSUE NR 1, NO HELP. INVESTIGATED AFT SERVICE DOOR IAW Q400 FIM TASK 52-00 - [SDR QXEA2016080800533](https://openairdocs.org/sdr/QXEA2016080800533), Aug 8, 2016: LINK. MALFUNCTIONED. AT 270 KNOTS, 12,000 FEET, SLIP INDICATOR NEUTRAL, RUDDER TRIM NEUTRAL, THE AILERON TRIM INDICATOR WAS INDICATING 1/2 TRIM LWD, ON FINAL APPROACH AT 120 KNOTS S - [SDR QXEA2016063000439](https://openairdocs.org/sdr/QXEA2016063000439), Jun 30, 2016: WIRE. BROKEN. 2 BROKEN WIRES 3351-42B22-2W9 AND 3351-43A, 22N-2, W9, 18" FORWARD OF SOCKET 3351-J8 FOR EMERGENCY LIGHT SOCKET EL3-1. SPLICED WIRES IAW WIRING MANUAL 20-16-10- - [SDR QXEA2016060700376](https://openairdocs.org/sdr/QXEA2016060700376), Jun 7, 2016: DITCHING DAM. LOOSE. AFT PASSENGER DOOR DITCHING DAM IS LOOSE. C/W OPS TEST IAW AMM 25-62-01-710-801. CHECKS GOOD. COMPAIRED TO 2 OTHER ACFT WITH NO DEFECTS FOUND. RETURNED TO SERVI - [SDR QXEA2016060700375](https://openairdocs.org/sdr/QXEA2016060700375), Jun 7, 2016: CONTROLLER. MALFUNCTIONED. PARKING BRAKE CAUTION MESSAGE AFTER SETTING TAKEOFF POWER. ABORTED TAKEOFF AT LESS THEN 20 KNOTS. REPLACED THE PARKING BRAKE CONTROL QUADRANT IAW AMM 32-44-21-0 - [SDR QXEA2016060100373](https://openairdocs.org/sdr/QXEA2016060100373), Jun 1, 2016: LIGHT. UNSECURE. CREW REPORTS THAT THE EMERGENCY LIGHTING AT ROW 2D IS LIFTING UP. SECURED THE EMERGENCY LIGHT STRIP AT 2D. RETURNED TO SERVICE. - [SDR QXEA2016051800342](https://openairdocs.org/sdr/QXEA2016051800342), May 18, 2016: FIRE DETECTOR. MALFUNCTIONED. CHECK FIRE DETECTOR WARNING LIGHT ILLUMINATED CONCURRENTLY WITH HTE FAULT A LIGHT ON NR 1 ENGINE. THERE WERE NO OTHER FIRE OR SMOKE INDICATIONS. NR 1 ENGINE PRI - [SDR QXEA2016042000272](https://openairdocs.org/sdr/QXEA2016042000272), Apr 20, 2016: LEAD. DAMAGED. AT 23,000 FT PROP DEICE CAUTION LIGHT ILLUMINATED. COMPLIED W/E& A CHECKLIST. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. R & R DE-ICE LEAD ON NR 1 PROP, NR 3 - [SDR QXEA2016032400220](https://openairdocs.org/sdr/QXEA2016032400220), Mar 24, 2016: LAMP. INOPERATIVE. NORMAL POSITION OF F/A EMERGENCY LIGHT SWITCH DOES NOT ILLUMINATE. REPLACED BURNED OUT LAMPS OF SWITCH. CHECKS NORMAL. RETURNED TO SERVICE. - [SDR QXEA2016012400048](https://openairdocs.org/sdr/QXEA2016012400048), Jan 24, 2016: LIGHT. DETACHED. EMERGENCY LIGHTING AT ROW 2 D,E AND ROW 1 DETACHED. SECURED THE EMERGENCY LIGHT AND RETURNED TO SERVICE. - [SDR QXEA2015122600666](https://openairdocs.org/sdr/QXEA2015122600666), Dec 26, 2015: LIGHT. LOOSE. FLOOR PATH LIGHTING STRIP AT THE MAIN CABIN DOOR IS LOOSE. RESECURED AS REQUIRED. RETURNED TO SERVICE. - [SDR QXEA2015112100617](https://openairdocs.org/sdr/QXEA2015112100617), Nov 21, 2015: SEAL. DAMAGED. F/A REPORTS AFT PAX DOOR LOUD NOISE. CLIMBING OUT OF 8000 FT MSL STILL DESCENDING TO 10000 FT MSL, NO PRESSURIZATION ISSUES. RETURNED TO FIELD. LANDING UNEVENTF - [SDR QXEA2015103000568](https://openairdocs.org/sdr/QXEA2015103000568), Oct 30, 2015: FITTING. LEAKING. NR 2 ENGINE OIL TEMPERATURE REACHED 128 DEGREES. ENGINE SHUTDOWN AND FLIGHT DIVERTED. LANDING UNEVENTFUL. AIRCRAFT DOWN FOR REPAIRS AND REPLACEMENT OF NR 2 ENGI - [SDR QXEA2015091400485](https://openairdocs.org/sdr/QXEA2015091400485), Sep 14, 2015: SWITCH. BROKEN. FORWARD F/A EMERGENCY LIGHT SWITCH COVER BROKEN. REPLACED SWITCH IAW AMM 33-51-05-000-801. OPS TEST GOOD IAW AMM 33-51-00-710-803. RETURNED TO SERVICE. - [SDR QXEA2015083000444](https://openairdocs.org/sdr/QXEA2015083000444), Aug 30, 2015: OUTFLOW VALVE. MALFUNCTIONED. MASTER WARNING CABIN PRESSURE ILLUMINATED AT 10,000 MSL. ALL CHECKLISTS ACCOMPLISHED. ACFT WILL NOT PRESSURIZE. RETURNED TO FIELD, LANDING UNEVENTFUL. FOUND AFT - [SDR QXEA2015060300290](https://openairdocs.org/sdr/QXEA2015060300290), Jun 3, 2015: SEAT TRACK. DAMAGED. SEAT TRACK NR 5 FOUND OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-00, SRM 51-40-15, STEP 6H - 6J AND SRM 51-42-05, STEP 4, 2, 10. - [SDR QXEA2015060300291](https://openairdocs.org/sdr/QXEA2015060300291), Jun 3, 2015: ANGLE. CORRODED. EVIDENCE OF CORROSION ON MCD MACHINED WEB ANGLE, PN 85329542-115 COMMON TO FUSELAGE SKIN AT X6.70 STR 24P. REMOVED ANGLE, PN 85329542-115 FROM MCD MACHINED WEB - [SDR QXEA2015060300284](https://openairdocs.org/sdr/QXEA2015060300284), Jun 3, 2015: SEAT TRACK. DAMAGED. SEAT TRACK NR 10 FOUND OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-15, 51-41-00 AND DWG 85328210. - [SDR QXEA2015060300283](https://openairdocs.org/sdr/QXEA2015060300283), Jun 3, 2015: SEAT TRACK. CORRODED. SEAT TRACK NR 11 FOUND OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05 AND 51-41-00. - [SDR QXEA2015060300282](https://openairdocs.org/sdr/QXEA2015060300282), Jun 3, 2015: SEAT TRACK. CORRODED. SEAT TRACK, NR 13 FOUND OUT OF LIMITS BS 228 - 570. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05 AND SRM 51-41-00. - [SDR QXEA2015060300281](https://openairdocs.org/sdr/QXEA2015060300281), Jun 3, 2015: INTERCOSTAL. CORRODED. EVIDENCE OF CORROSION ON MCD MACHINED INTERCOSTAL ANGLES, PN 85329576-103 COMMON TO MACHINED WEB AT X6.70, STR 25P AND ANGLE, PN 85329576-104 COMMON TO MACHINED - [SDR QXEA2015060300280](https://openairdocs.org/sdr/QXEA2015060300280), Jun 3, 2015: DOUBLER. CORRODED. LAV SERVICE CUT OUT DOUBLER CORRODED. LAV SERVICE DOOR REMOVED REF SRM 52-42-10. INSTALLED SERVICE DOOR REF AMM 52-44-26-400-801. REMOVED DOUBLER, PN 85307796 F - [SDR QXEA2015060300288](https://openairdocs.org/sdr/QXEA2015060300288), May 30, 2015: SEAT TRACK. CORRODED. SEAT TRACK NR 19, FOUND OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-45, PAR 6H, 51-42-15, PAR 5G, 51-42-05 PAR 4E, AND 51-40-15 PAR 6M. - [SDR QXEA2015060300289](https://openairdocs.org/sdr/QXEA2015060300289), May 27, 2015: SEAT TRACK. CORRODED. SEAT TRACK NR 18 FOUND OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK SRM 51-42-05 STEP 4E, STEP 4,D AND DWG NR 85328251, REV A. - [SDR QXEA2015060300287](https://openairdocs.org/sdr/QXEA2015060300287), May 26, 2015: SEAT TRACK. DAMAGED. SEAT TRACK NR 14 FOUND OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-15 AND SRM 51-42-05. - [SDR QXEA20150603](https://openairdocs.org/sdr/QXEA20150603), May 26, 2015: SEAT TRACK. CORRODED. SEAT TRACK NR 15 FOUND OUT OF LIMITS AND REQUIRES REPLACEMENT PN:85338210-115. REMOVED SEAT TRACK NR 15, PN 85338210-115 IAW SRM 51-40-15 AND SRM 51-42-05. INST - [SDR QXEAA20150603](https://openairdocs.org/sdr/QXEAA20150603), May 24, 2015: SEAT TRACK. CORRODED. SEAT TRACK NR 6, FOUND OUT OF LIMITS AND REQUIRES REPLACEMENT PN:85328210-111. REMOVED SEAT TRACK NR 6, PN 85328210-111, REF SRM 51-40-07. INSTALLED SEAT TRACK - [SDR QXEA2015052600271](https://openairdocs.org/sdr/QXEA2015052600271), May 24, 2015: SEAT TRACK. UNKNOWN. SEAT TRACK NR 8 FOUND OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-00, SRM 51-40-15 AND SRM 51-42-05. - [SDR QXEA2015052600272](https://openairdocs.org/sdr/QXEA2015052600272), May 23, 2015: SEAT TRACK. UNKNOWN. SEAT TRACK NR 9 FOUND OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK SRM 51-42-05 AND SRM 51-40-15. - [SDR QXEA2015052600273](https://openairdocs.org/sdr/QXEA2015052600273), May 18, 2015: SEAT TRACK. UNKNOWN. SEAT TRACK NR 2 FOUND OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-15 AND 51-42-05. - [SDR QXEA2015052600269](https://openairdocs.org/sdr/QXEA2015052600269), May 18, 2015: SEAT TRACK. UNKNOWN. SEAT TRACK NR 3 FOUND OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05, STEP 4E. All 536: https://openairdocs.org/deregistered/N410QX-2019-12-23/reports.md ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB SEA02IA044](https://openairdocs.org/ntsb/SEA02IA044), Mar 2, 2002: Bombardier DHC-8-401 (N410QX), Boise, ID, incident, no damage. Probable cause: The partial failure of one of the number two hydraulic system elevator hydraulic lines, leading to the loss of fluid and pressure in that system during cruise flight. This loss resulted in reliance… ## FAA accident and incident reports (3) 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 20151030018469I](https://openairdocs.org/incident/20151030018469I), Oct 30, 2015: Bombardier Inc DHC-8-402 (N410QX), Pullman, WA, No damage. QXE211, a dhc -8-401 N410QX departed puw on a revenue flight enroute to sea when the #2 engine oil temp climbed above normal. Checklist procedures were… - [Incident 20050102000349I](https://openairdocs.org/incident/20050102000349I), Jan 2, 2005: Bombdr DHC8401 (N410QX), Great Falls, MT. (-23) On 01/02/05, qxea flt 2321 departed hln enroute to gtf, the flight crew experienced aircraft roll to the right. The pilot balanced the fuel in the wings,… - [Incident 20031002027709I](https://openairdocs.org/incident/20031002027709I), Oct 2, 2003: Bombdr DHC8401 (N410QX), Kalispell, MT, Minor damage. (-23) Horizon air, flight 2340 on October 2, 2003 at 2338 MDT from mso to fca, hit an unknown number of ducks, at 7800' MSL approximately 20 NM sse of fca. The… --- 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.