# N405QX: 2001 Bombardier DHC-8-402, registration cancelled 2024-01-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 8, 2024
- Exported to: Canada
- 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: 4047
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: April 26, 2005
- Certificate issued: November 29, 2023
- Last registry action: November 29, 2023
- Mode S code: A4C0A8
- Owner when cancelled: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%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/N405QX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=405QX
- Page: https://openairdocs.org/deregistered/N405QX-2024-01-08

From the FAA registry file of November 4, 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 (555, newest 50)

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

- [SDR QXEA2023092500134](https://openairdocs.org/sdr/QXEA2023092500134), Sep 19, 2023: LAMP. INOPERATIVE. AFT PASSENGER DOOR EMERGENCY LIGHT IS INOP. RELAMPED.
- [SDR QXEA2022120500332](https://openairdocs.org/sdr/QXEA2022120500332), Dec 4, 2022: SIGN. LOOSE. FWD LIGHTED EXIT SIGN IS PEELING BACK & IS LOOSE. REMOVED FROM SERVICE. FOUND FWD EXIT/INFO SIGN HOUSING OUT OF ALIGNMENT CAUSING INFO SIGN LIGHT COVER TO POP O
- [SDR QXEA2022101000305](https://openairdocs.org/sdr/QXEA2022101000305), Oct 6, 2022: ANTENNA. INOPERATIVE. ATTEMPTED CAT III APPROACH INTO SEA, "NO FLARE" MSG IN THE HUD. DIVERTED TO PDX, UPON DESCENT INTO PDX, RECEIVED RA2 FAIL MESSAGE. ( RADIO ALTIMETER - ONE INOP 
- [SDR QXEA2022090600286](https://openairdocs.org/sdr/QXEA2022090600286), Sep 2, 2022: AXLE. CORRODED. CORROSION AND PITTING FOUND ON #2 MLG AXLE. EXCEEDS LIMITES IN TASK CARD 321100202 ITEM 5. REPLACED #2 MLG AXLE IAW AMM 32-11-04-000-801. CHECKS GOOD.
- [SDR QXEA2022052400205](https://openairdocs.org/sdr/QXEA2022052400205), May 23, 2022: INSTRUMENT PANEL. LOOSE. ISI INSTUMENT STARTED TUMBLING DURING FLIGHT THEN BECAME STUCK SHOWING A 60 DEGREE BANK. AIRSPEED AND ALTITUDE INDICATIONS WERE NORMAL. RETURNED TO FILED AND AC
- [SDR QXEA2022022800095](https://openairdocs.org/sdr/QXEA2022022800095), Feb 27, 2022: NONE. NONE. WAS GETTING HOT BLEED LIKE SMELL BUT BLEED AIR WAS COLD AND DUCTS SHOWING COLD. REMOVED FROM SERVICE. PERFORMED BLEED AIR OPERATIONAL CHECK. IAW AMM TASK 36-11-
- [SDR QXEA2022010300573](https://openairdocs.org/sdr/QXEA2022010300573), Dec 30, 2021: SEAL. DAMAGED. ON CLIMBOUT SAW RATE UP TO 3000' AND CABIN ALT TO 4000' THEN NORMAL. CYCLE REPEATED ONCE. ON ROLLOUT NOTICED DIFFERENCE .4 AND RATE TO 1500' FOR A FEW SEC. REMO
- [SDR QXEA2021120700543](https://openairdocs.org/sdr/QXEA2021120700543), Dec 7, 2021: NONE. NONE. CREW REPORTED CARPET PEELING IN FRONT OF EMERGENCY/EXIT DOOR. REMOVED FROM SERVICE. RESECURED CARPET AS REQUIRED. NO FURTHER DEFECTS TO BE NOTED. NO PARTS REPLA
- [SDR QXEA2021111500510](https://openairdocs.org/sdr/QXEA2021111500510), Nov 14, 2021: PITOT HEAD. MALFUNCTIONED. PITOT HEAT #2 MASTER CAUTION INFLIGHT. RETURNED TO FIELD. LANDING UNEVENTFUL. C/W FIM 30-30-00-810-807. PITOT/STATIC ANTI ICE OPS CHECK FAILED. #2 PITOT PROBE F
- [SDR QXEA2021100500465](https://openairdocs.org/sdr/QXEA2021100500465), Oct 5, 2021: BATTERY PACK. FAILED. AFT EMERGENCY LIGHTS BATTERY PACKS ARE FAILING. REPLACED BATTERY PACKS FOR THE AFT EMERGENCY LIGHTS.
- [SDR QXEA2021051100229](https://openairdocs.org/sdr/QXEA2021051100229), May 7, 2021: AXLE. CORRODED. #1 MLG AXLE REQUIRES REPLACEMENT DUE TO CORROSION FINDINGS ON THE PISTON PLUG BORE. REMOVED #1 MLG AXEL IAW AMM TASK 32-11-04-000-801. BEGAN INSTALL OF #1 MLG A
- [SDR QXEA2021050700215](https://openairdocs.org/sdr/QXEA2021050700215), May 6, 2021: WIRE HARNESS. DAMAGED. PROP DEICE CAUTION ILLUMINATES WHEN # 2 PROP CYCLES ON. THE CAUTION EXTINGUISHES AFTER THE # 2 PROP TURNS OFF. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVIC
- [SDR QXEA2021020300045](https://openairdocs.org/sdr/QXEA2021020300045), Feb 2, 2021: GCU. WARNING MESSAGE. R AC BUS CAUTION MESSAGE ILLUMINATED DURING FLIGHT NO MASTER CAUTION ASSOCIATED REMAINED ILLUMINATED UNTIL ENGINE SHUTDOWN. DIVERTED. REMOVED FROM SERVICE. BOAR
- [SDR QXEA2020090700277](https://openairdocs.org/sdr/QXEA2020090700277), Sep 2, 2020: TAB. OUT OF ADJUST. ON CLIMBOUT WITH AP ON THROUGH 8500 MSL, RUDDER TRIM RUNAWAY, FULL RIGHT DEFLECTION. AT CRUISE WITH AP ON MISTRIM LT WING DN CAUTION PFD. THROUGHOUT FLIGHT LT A
- [SDR QXEA2020090200273](https://openairdocs.org/sdr/QXEA2020090200273), Sep 2, 2020: CONTROL PANEL. MALFUNCTIONED. AIRPLANE REQUIRED MORE THAN 3/4 SCALE DEFLECTION OF THE LEFT AILERON TRIM. DURING CRUISE AND DESCENT GOT MISTRIM MESSAGE ON PFD, RAN CHECKLIST. SPOILERS INDICAT
- [SDR QXEA2020062400260](https://openairdocs.org/sdr/QXEA2020062400260), Aug 22, 2020: TRANSDUCER. MALFUNCTIONED. POWERPLANT MESSAGE ILLUMINATED ON ED DURING CLIMB @ 10'000'. RETURNED TO FIELD. LANDING UNEVENTFUL, REMOVED FROM SERVICE. FAULT CODE IN CDS IS #2 ENGINE CHAN. B
- [SDR QXEA2020071300205](https://openairdocs.org/sdr/QXEA2020071300205), Jul 8, 2020: SEAT TRACK. CORRODED. SEAT RAIL 11 FROM FSX 10.50-FSX102.50 CORRODED BEYOND LIMITS. REMOVED SEAT RAIL 11 FROM FSX 10.50 - 102.50 IAW SRM 51-40-07-02-01. REPLACED SEAT RAIL 11 IAW SRM
- [SDR QXEA2020070900204](https://openairdocs.org/sdr/QXEA2020070900204), Jul 8, 2020: SEAT TRACK. CORRODED. SEAT RAIL 10 FROM FSX -39.00 -X10.50 CORRODED BEYOND LIMITS. REMOVED SEAT RAIL 10 FSX - 39.00- X10.50 IAW SRM 51-40-07-02-01. REPLACED SEAT RAIL 10 IAW SRM 51-4
- [SDR QXEA2020031000130](https://openairdocs.org/sdr/QXEA2020031000130), Mar 7, 2020: WIRE HARNESS. MALFUNCTIONED. ON CLIMB OUT THE "PROP DEICE" MASTER CAUTION APPEARED. RAN THE CHECKLIST AND CAUTION CLEARED AND SUBSEQUENTLY REAPPEARED. AC GEN #1. DIVERTED. LANDING UNEVENTFU
- [SDR QXEA2019123100489](https://openairdocs.org/sdr/QXEA2019123100489), Dec 28, 2019: LINE. LEAKING. ON FINAL APPROACH, GEAR DOWN. FLAPS 15 DEGREES, NR 2 HYD ISOLATION VALVE CAUTION ILLUMINATED. NR 2 HYD QUANTITY WAS AT 10%. RAN NR 2 HYD ISOLATION VALVE CAUTION
- [SDR QXEA2019120400444](https://openairdocs.org/sdr/QXEA2019120400444), Dec 4, 2019: DOOR. BINDING. RAMP REPORTS L2 DOOR HARD TO OPEN. REMOVED FROM SERVICE. COMPLIED WITH OPERATIONAL TEST OF L2 DOOR IAW AMM TASK 52-12-00-710-802. OPS TEST GOOD. NO PARTS REPLAC
- [SDR QXEA2019120200442](https://openairdocs.org/sdr/QXEA2019120200442), Nov 29, 2019: SEQUENCE VALVE. MALFUNCTIONED. AFTER T/O WHEN GEAR WAS SELECTED UP, THE L. DOOR AMBER LIGHT REMAINED ILLUMINATED. F.A. CONFIRMED THE LT GEAR DOOR DID NOT RETRACT. ACCOMPLISHED ALT LDG GEAR EX
- [SDR QXEA2019110800410](https://openairdocs.org/sdr/QXEA2019110800410), Nov 8, 2019: FADEC. MALFUNCTIONED. FADEC 1/DU DISPLAYED ON ED AFTER ENGINE SHUTDOWN. A/F TEST CAME BACK WITH ABORT MESSAGE. REMOVED FROM SERVICE. DISPLAY REPLACED, NO HELP. FADEC #1 REPLACED NO H
- [SDR QXEA2019102800396](https://openairdocs.org/sdr/QXEA2019102800396), Oct 26, 2019: SEQUENCE VALVE. MALFUNCTIONED. L DOOR AMBER LIGHT ILLUMINATED DURING CLIMB OUT. WE NOTICED IT AT 2500FT SPEED NEVER WENT ABOVE 185. WE RAN APPROPRIATE CHECKLIST AND ALTERNATE GEAR EXTENSION. 
- [SDR QXEA2019082100324](https://openairdocs.org/sdr/QXEA2019082100324), Aug 20, 2019: SWITCH. MALFUNCTIONED. #1 BLEED HOT CAUTION ILUMINATED INTERMITANATLY. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. REPLACED #1 ENGINE NACELLE DUCT-LEAK OVER TEMP SWIT
- [SDR QXEA2019080100302](https://openairdocs.org/sdr/QXEA2019080100302), Aug 1, 2019: UNKNOWN. UNKNOWN. RAMP REPORTS THAT SPARKS WERE COMING FROM APU DURING STARTUP AND FLUID WAS LEAKING ONCE IT WAS RUNNING, START SEEMED NORMAL EXCEPT STARTER LIGHT STAYED ON LONGE
- [SDR QXEA2019072200273](https://openairdocs.org/sdr/QXEA2019072200273), Jul 20, 2019: UNKNOWN. MALFUNCTIONED. AFTER ENGINE START AND MOVING CONDITION LEVERS TO MAX. THE #2 PROP HUNG AT 450 RPM FOR 10 SECONDS AND THEN SURGED TO 750 RPM AND THEN SETTLED AT 660 RPM. A POWE
- [SDR QXEA2019061100245](https://openairdocs.org/sdr/QXEA2019061100245), Jun 11, 2019: DOOR. OUT OF SEQUENCE. RAMPER ADVISES UNABLE TO OPEN THE AFT PASSENGER DOOR. DOOR IS JAMMED IN ITS CURRENT POSITION. UNABLE TO MOVE. APPEARS OFF TRACK. REMOVED FROM SERVICE. FREED AFT
- [SDR QXEA2019060700241](https://openairdocs.org/sdr/QXEA2019060700241), Jun 6, 2019: SEQUENCE VALVE. INOPERATIVE. "L DOOR" ADVISORY LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. PERFORMED ALTERNATE GEAR EXTENSION. REMOVED FROM SERVICE. INTERROGATED PSEU FOR RELATED FAUL
- [SDR QXEA2019060300235](https://openairdocs.org/sdr/QXEA2019060300235), May 31, 2019: CONNECTOR. CORRODED. DAILY SYSTEMS CHECK OF THE AUTOFEATHER SYSTEM FAILED 3 CONSECUTIVE TIMES. REMOVED FROM SERVICE. FOUND HIGH RESISTANCE SHORT TO GROUND IN WIRE# 7600-42A-20-4 BET
- [SDR QXEA2019052800225](https://openairdocs.org/sdr/QXEA2019052800225), May 26, 2019: LIGHT. INOPERATIVE. F/A EMERGENCY LIGHT "NORMAL" BACKLIGHT IS OUT. REMOVED FROM SERVICE. RELAMPED F/A EMERGENCY "NORMAL" BACK LIGHT AT FWD F/A JUMPSEAT. FUNCTIONS AS REQUIRED. NO F
- [SDR QXEA2019042400187](https://openairdocs.org/sdr/QXEA2019042400187), Apr 24, 2019: FAULT CODE. ILLUMINATED. AFTER BEING CLEARED FOR TAKEOFF BUT PRIOR TO ADDING TAKEOFF POWER #2 PEC CAUTION ILLUMINATED WITH POWERPLANT MSG ON ED. ABORTED TAKE OFF. REMOVED FROM SERVICE. 
- [SDR QXEA2019040800161](https://openairdocs.org/sdr/QXEA2019040800161), Apr 8, 2019: LIGHT. DETACHED. PHOTO-LUMINESCENT STRIP IN FRONT OF 1B DETACHED. REMOVED FROM SERVICE. RE-SECURED LOOSE FLOOR PATH LIGHTING SECTION FWD OF PAX SEAT 1B IAW 33-51-16-400-801. AIR
- [SDR QXEA2019022700092](https://openairdocs.org/sdr/QXEA2019022700092), Feb 26, 2019: LANDING GEAR. SLOW. AT SELECTION OF GEAR UP ON T/O, SEVERAL CAUTION ADV LITS ILLUMINATED MOMENTARILY AND THE LT MAIN LDG GEAR WAS SLOW TO RETRACT. AT SELECTION OF GEAR DN ON LDG. T
- [SDR QXEA2019022700091](https://openairdocs.org/sdr/QXEA2019022700091), Feb 24, 2019: RVDT. OUT OF RIG. AFTER TAKEOFF AND GEAR HANDLE SELECTED UP. GEAR SHOWED 3 RED WITH HANDLE IN UP POSITION. RAN GEAR FAILES OT RETRACT CHECKLIST, THEN ALT GEAR EXT CHECKLIST. DISC
- [SDR QXEA2019021100066](https://openairdocs.org/sdr/QXEA2019021100066), Feb 11, 2019: GLOWSTRIP. LOOSE. FA REPORTS THE PHOTOLUMINESCENCE LIGHT STRIP IN FRONT OF SEAT 2D IS COMING UP. REMOVED FROM SERVICE. RESECURED PHOTOLUMINESCENT LIGHT STRIP IN FRONT OF SEAT 2D,
- [SDR QXEA2019020500060](https://openairdocs.org/sdr/QXEA2019020500060), Feb 4, 2019: LIGHT. LOOSE. FLOOR LIGHTING IN FRONT OF ROW 2 LOOSE. REMOVED FROM SERVICE. EMER STRIP IN FRONT OF ROW 2DE NOT PROPERLY INSTALLED. REINSTALLED/RESECURED EMER STRIP LIGHTING I
- [SDR QXEA2019010700006](https://openairdocs.org/sdr/QXEA2019010700006), Jan 3, 2019: SELECTOR VALVE. MALFUNCTIONED. AFTER SELECTING LANDING GEAR DOWN FOR LANDING, WE RECEIVED 3 GEAR UNSAFE (RED LIGHTS) FOR OVER A MINUTE (APPROX). GEAR THEN CAME DOWN (3 GREEN LIGHTS) WITH NO F
- [SDR QXEA2018121000451](https://openairdocs.org/sdr/QXEA2018121000451), Dec 8, 2018: PSEU. INOPERATIVE. AFTER GEAR RETRACTION L MAIN GEAR DOOR CAUTION N GEAR DOOR CAUTION. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. INTERROGATED PSEU AND FOUND FAU
- [SDR QXEA2018111500420](https://openairdocs.org/sdr/QXEA2018111500420), Nov 15, 2018: DOOR SEAL. DAMAGED. AIRPLANE FAILED TO PRESSURIZE AFTER TAKE OFF. RETURNED TO FIELD. LANDING UNEVENTFUL. FOUND AFT BLOWOUT PANEL DISLODGED INSPECTED PANEL AND SURROUNDING AREA NO D
- [SDR QXEA2018111300416](https://openairdocs.org/sdr/QXEA2018111300416), Nov 12, 2018: FUEL NOZZLE. INOPERATIVE. APU FAILED TO START THE STARTER LIGHT STAYED ON FOR 30 SEC THAN APU FAIL MSG POWERED UP. 2ND START SAME OUTCOME. RAMPER WAS REPORTING SMOKE FROM THE APU. COMPLI
- [SDR QXEA2018062700240](https://openairdocs.org/sdr/QXEA2018062700240), Jun 27, 2018: HOOK AND LOOP. WORN. RT AFT GALLEY SERVICE DOOR OPENING INTERFERES WITH GALLEY SERVICE DOOR TRIM PANEL. REMOVED FROM SERVICE. REPLACED WORN HOOK AND LOOP ON AFT GALLEY SERVICE DOOR,
- [SDR QXEA2018031300087](https://openairdocs.org/sdr/QXEA2018031300087), Mar 11, 2018: LIGHT. DIM. BOTTOM BETA LIGHT ON EMERGENCY EXIT DOOR IS DIM. REPLACED BETA LIGHT IAW AMM 33-51-00-960-801. CHECKS GOOD. RETURNED TO SERVICE.
- [SDR QXEA2017121100702](https://openairdocs.org/sdr/QXEA2017121100702), Dec 9, 2017: LENS. BROKEN. TYPE 2 TYPE 3 DOOR EXIT SIGN COVER BROKE OFF. REMOVED FROM SERVICE. REMOVED AND REPLACED FWD EMERGENCY EXIT LIGHT COVER (LOWER) ASSY REF WM 33-51-00-2,OPS TESTE
- [SDR QXEA2017083100](https://openairdocs.org/sdr/QXEA2017083100), Aug 30, 2017: BUSHING. MISSING. AFTER LANDING, THE MAIN CABIN DOOR WOULD NOT FULLY OPEN OR FULLY CLOSE. REMOVED AIRCRAFT FROM SERVICE. FOUND A NUT MISSING FROM THE REAR HINGE AT THE MAIN CABIN
- [SDR QXEA2017071100464](https://openairdocs.org/sdr/QXEA2017071100464), Jul 8, 2017: SKIN. CRACKED. CRACK ON FWD CARGO DOOR NR 2 BEAM. REPLACED THE BEAM IAW SRM 51-40-07-02-01, 51-40-15-02-01, 51-42-05-02-01, 51-42-45-02-01, AND 51-42-75-02-01. CRACKED LOWER S
- [SDR QXEA2017071000457](https://openairdocs.org/sdr/QXEA2017071000457), Jul 6, 2017: STRINGER. CORRODED. STRINGER 25R HAS CORROSION THREE INCHES AFT OF BS 136. REMOVED DAMAGE IAW RD84-53-8283. NDT CARRIED OUT IAW NDTM 6, 51-00-08-250-801. REPAIRED STRINGER 25R RD84
- [SDR QXEA2017071000456](https://openairdocs.org/sdr/QXEA2017071000456), Jun 30, 2017: SEAT TRACK. CORRODED. SEAT TRACK NR 6 LT INBD FROM BS 102 - 228.50 CORRODED BEYOND LIMITS. THE SEAT TRACK WAS REPLACED IAW SRM 51-41-00, 51-42-05, AND 51-40-15.
- [SDR QXEA2017071000454](https://openairdocs.org/sdr/QXEA2017071000454), Jun 30, 2017: SEAT TRACK. CORRODED. SEAT TRACK NR 13 RT INBOARD CORRODED BEYOND LIMITS FROM BS 228.50 - 570. THE SEAT TRACK WAS REPLACED IAW SRM 51-41-00, 51-42-05, AND 51-40-15.
- [SDR QXEA2017071000453](https://openairdocs.org/sdr/QXEA2017071000453), Jun 30, 2017: SEAT TRACK. CORRODED. SEAT TRACK LEFT INBD, BS 228.5 - 570 CORRODED BEYOND LIMITS. THE SEAT TRACK WAS REPLACED IAW SRM 51-41-00, 51-42-05, AND 51-40-15.

All 555: https://openairdocs.org/deregistered/N405QX-2024-01-08/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 20120103000029I](https://openairdocs.org/incident/20120103000029I), Jan 3, 2012: Bombardier Inc DHC-8-402 (N405QX), Yakima, WA, Minor damage. On January 03, 2012 while on short final to ykm, N405QX struck a flock of 4 or 5 canadian geese at approximately 100 - 200 feet above the runway. Damage was…
- [Incident 20080415831979I](https://openairdocs.org/incident/20080415831979I), Apr 15, 2008: Bombdr DHC8402 (N405QX), Los Angeles, CA, No damage. (-23) Carrier reported runway rudder trim to the right, when applying rudder trim to the left during climb.
- [Incident 20040324003899I](https://openairdocs.org/incident/20040324003899I), Mar 24, 2004: Bombdr DHC8401 (N405QX), Seattle, WA, Minor damage. (-23) On March 24, 2004 a Bombardier DHC-8-401, operated by horizon air industries, inc on a scheduled domestic passenger flight under provisions of title 14…
- [Incident 20030909024459I](https://openairdocs.org/incident/20030909024459I), Sep 9, 2003: Bombdr DHC8401 (N405QX), Portland, OR. (-23) Crew experienced #2 engine fadec caution during approach to land. Copilot was flying at the time. The captain initiated the check list for #2 engine…

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