# N402QX: 2001 Bombardier DHC-8-402, registration cancelled 2023-08-22

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 22, 2023
- 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: 4032
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: April 29, 2005
- Certificate issued: May 30, 2023
- Last registry action: May 30, 2023
- Mode S code: A4B583
- 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/N402QX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=402QX
- Page: https://openairdocs.org/deregistered/N402QX-2023-08-22

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 (504, newest 50)

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

- [SDR QXEA2023031300036](https://openairdocs.org/sdr/QXEA2023031300036), Sep 1, 2022: UNKNOWN. UNKNOWN. FWD BAGGAGE DOOR, LOWEST CENTRE ANGLE BRACKET CRACKED. REPAIRED FWD BAGGAGE DOOR LWR CENTRE ANGLE BRACKET IAW RD 84-52-2178 ISSUE 1. NDT CARRIED OUT NO CRACKS F
- [SDR QXEA2022062800237](https://openairdocs.org/sdr/QXEA2022062800237), Jun 27, 2022: SCUFF PLATE. DETACHED. AFTER LANDING THERE IS A PIECE OF 8” X 10” PIECE OF METAL WEDGED BETWEEN THE LEFT MAIN GEAR DOORS. REMOVED FROM SERVICE. FOUND TO BE THE LH MLG DOOR SCUFF PLATE
- [SDR QXEA2022062700236](https://openairdocs.org/sdr/QXEA2022062700236), Jun 23, 2022: YOKE. LACK OF LUBE. DURING CLIMBOUT- YOKE HARED TO TURN LEFT AT SPEED 220 KNOTS. YOKE NORMAL FORCE TO TURN RIGHT. REMOVED FROM SERVICE. C/W GVI & TACTILE MOVEMENT OF BOTH AILERONS 
- [SDR QXEA2022061300219](https://openairdocs.org/sdr/QXEA2022061300219), Jun 11, 2022: CARPET. WORN. FWD GALLEY RUBBER FLOORING WHERE IT MEET THE AILE CARPET IS A TRIPPING HAZARD. REMOVED FROM SERVICE. SECURED FWD CARPET AS REQUIRED.NO OTHER DEFECTS NOTED. RETU
- [SDR QXEA2022040800144](https://openairdocs.org/sdr/QXEA2022040800144), Apr 7, 2022: POWER SUPPLY. FAILED. EMERGENCY LIGHTS AT TYPE 2 EXIT DOOR FAIL 10 MINUTE CHECK. R & R'ED EMERGENCY PWR SUPPLY BATTERY PACKS AT POSITIONS RH2 AND RH4 IAW Q400 AMM 33-51-01-000-802 33
- [SDR QXEA2021122000555](https://openairdocs.org/sdr/QXEA2021122000555), Dec 14, 2021: LAMP. MALFUNCTIONED. BETA LAMP LOW OUTPUT. REPLACED LAMP IAW AMM 33-51-00-960-801.
- [SDR QXEA2021082000413](https://openairdocs.org/sdr/QXEA2021082000413), Aug 20, 2021: APU. SMOKE. APU WAS ON WHEN ARRIVING AT AIRCRAFT. SOON AFTER WE ARRIVED THE APU AUTO SHUTDOWN AND APU SHOWED APU FAIL LIGHT. AFTER COMPLETING THE CHECKLIST, WE GAVE THE APU
- [SDR QXEA2021071600364](https://openairdocs.org/sdr/QXEA2021071600364), Jul 15, 2021: LIGHT. LOOSE. ILLUMINATION STRIP IN FORWARD ENTRY IN FRONT OF FORWARD BAGGAGE COMPARTMENT IS LOOSE AND SNAGS ON INTERNAL BAGGAGE DOOR. REMOVED FROM SERVICE. RE-SECURED ILLUMI
- [SDR QXEA2021041200184](https://openairdocs.org/sdr/QXEA2021041200184), Apr 10, 2021: REFLECTOR. DETACHED. REFLECTIVE TAPE ON FLOOR BY MAIN CABIN DOOR IS PEELING UP. REMOVED FROM SERVICE. RE-SECURED EMERGENCY FLOOR LIGHT STRIP BY MAIN CABIN DOOR IN FRONT OF ROW 1AB. 
- [SDR QXEA2021040100168](https://openairdocs.org/sdr/QXEA2021040100168), Mar 31, 2021: LIGHT. LOOSE. PHOTOLUMINESCENT EMERGENCY FLOOR STRIP NEAR MAIN CABIN DOOR IS LIFTING UP CREATING A TRIPPING HAZARD. REMOVED FROM SERVICE. RESECURED PHOTOLUMINESCENT EMERGENCY
- [SDR QXEA2021020800048](https://openairdocs.org/sdr/QXEA2021020800048), Feb 7, 2021: WARNING MESSAGE. FALSE INDICATION. ED MESSAGE MISTRIM (L WING DOWN) APPEARED IN FLIGHT. RAN CHECKLIST. PLANE ROLLED RIGHT WHEN AUTOPILOT DISENGAGED. LEVELED AIRPLANE, DID NOT CHANGE TRIM DUE TO L
- [SDR QXEA2021011700012](https://openairdocs.org/sdr/QXEA2021011700012), Jan 14, 2021: WARNING LIGHT. ILLUMINATED. SPLR OUTBOARD CAUTION ILLUMINATED AT CRUISE FOR ABOUT 8 MINUTES. ROLL CONTROL TO LEFT FELT ABNORMALLY HEAVY DURING DEPARTURE. REMOVED FROM SERVICE. REPLACED THE
- [SDR QXEA2021010400002](https://openairdocs.org/sdr/QXEA2021010400002), Jan 2, 2021: CONTROL UNIT. MALFUNCTIONED. SPLR OUTBOARD CAUTION CAME ON AROUND 8000FT AND 185 KTS. RAN CHECKLIST CAUTION STAYED ON FOR REST OF FLIGHT. ALL FLIGHT CONTROLS FELT NORMAL. REMOVED FROM SERVI
- [SDR QXEA2020121500354](https://openairdocs.org/sdr/QXEA2020121500354), Dec 15, 2020: POWER UNIT. INOPERATIVE. RECEIVED FLAP DRIVE CAUTION ON FINAL. WENT AROUND, ACCOMPLISHED E+A CHECK LIST. FLAPS RETURNED TO 0 DEG AS NORMAL. ACCOMPLISHED FLAPS 35 LANDING, PER THE CHECK 
- [SDR QXEA20200824258](https://openairdocs.org/sdr/QXEA20200824258), Aug 22, 2020: LIGHT. LOOSE. LUMINESCENT ESCAPE STRIP IN FRONT OF SEAT 1B IS PULLED UP. REMOVED FROM SERVICE. RE-SECURED LUMINESCENT ESCAPE STRIP IN FRONT OF SEAT 1B AS REQUIRED. NO FURTHER
- [SDR QXEA2020081300241](https://openairdocs.org/sdr/QXEA2020081300241), Aug 11, 2020: LINE. DAMAGED. #1 HYD QTY DROPPED TO ZERO IN CRUISE. STARTED WITH A #1 HYD ISO VLV CAUTION + ROLL SPLR OUTBD HYD CAUTION WITH ABOUT 15% QUANTITY LEFT THEN SLOWLY BLED TO ZERO.
- [SDR QXEA2020080300228](https://openairdocs.org/sdr/QXEA2020080300228), Aug 1, 2020: SPOILER SYS. MALFUNCTIONED. ON CLIMB OUT ACCELERATING THROUGH APPROX 190KIAS, THE "SPOILER OUTBD" CAUTION LIGHT ILLUMINATED. PER EA CHECKLIST MAINTAINED MAX 200KIAS AFTER LEVEL OFF AT FL24
- [SDR QXEA2020072900226](https://openairdocs.org/sdr/QXEA2020072900226), Jul 29, 2020: BUMPER. DAMAGED. WHEN OPENING THE EMERGENCY EXIT, THE LOWER HANDLE WOULD NOT ROTATE TO THE WATER POSITION (DITCHING DAM). REPLACED THE STOPPER FOR THE EMERGENCY EXIT IAW SRM 51-
- [SDR QXEA2020033000145](https://openairdocs.org/sdr/QXEA2020033000145), Mar 27, 2020: ECU. MALFUNCTIONED. AT APPROX 2500' AGL WE GOT A T/O WARNING HORN. T/O HORN COMES ON ABOVE 50% POWER LEVEL TRAVEL. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. REPLACED FCEC
- [SDR QXEA2020021200089](https://openairdocs.org/sdr/QXEA2020021200089), Feb 9, 2020: BELLCRANK. WORN. AFTER GEAR UP SELECTION THE NOSE GEAR GREEN LIGHT AND NOSE DOOR LIGHT REMAINED ILLUMINATED FOR APPROX 10 SECONDS. THEN BOTH WENT OUT (DARK) AND WE FELT THE GEAR
- [SDR QXEA2020010600008](https://openairdocs.org/sdr/QXEA2020010600008), Jan 5, 2020: TMU. INOPERATIVE. IN CRUISE DEICE BOOTS WOULD NOT INFLATE IN SLOW OR FAST MODES DEICE BOOTS INFLATED NORMALLY N MANUAL MODE. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM S
- [SDR QXEA2019123100490](https://openairdocs.org/sdr/QXEA2019123100490), Dec 29, 2019: LANDING GEAR. MALFUNCTIONED. SELECTED GEAR DOWN ON FINAL AT 4000' LEFT MAIN GEAR EXTENDED AFTER ABOUT 30 SECONDS RIGHT MAIN EXTENDED. CANCELED APPROACH, DECLARED EMERGENCY. ONCE STARTED TO 
- [SDR QXEA2019073000292](https://openairdocs.org/sdr/QXEA2019073000292), Jul 28, 2019: BEAM. CRACKED. AFT PAX DOOR 2 BEAM CRACKED. AFT PAX DOOR 2 BEAM REPLACED IAW SRM 51-40-07-02-01, 51-42-05-02-01, 51-42-75-02-01, 51-40-15-02-01.
- [SDR QXEA2019061700251](https://openairdocs.org/sdr/QXEA2019061700251), Jun 14, 2019: FAULT CODE. FALSE ACTIVATION. AIRFLOW WEAK IN AUTO AND MAN. CABIN DUCT TEMP 18 DEGREE C. DIRTY PACK ODOR. INTERROGATED CDS AND FOUND FAULT CODE 4108,ECU ANLG CH2 PER FIM 21-60-00-810-843, CL
- [SDR QXEA2019042600191](https://openairdocs.org/sdr/QXEA2019042600191), Apr 25, 2019: BRAKE. CONTAMINATED. RT INSIDE WHEEL SMOKING APPARENTLY FROM GREASE ON BRAKE UPON PARKING. REMOVED FROM SERVICE. PERFORMED GVI OF WHEEL AND BRAKE ASSYS. CLEANED RESIDUAL GREASE FROM
- [SDR QXEA2019011100064](https://openairdocs.org/sdr/QXEA2019011100064), Feb 7, 2019: DOOR SEAL. CONTAMINATED. LOUD NOISE COMING FROM AFT PASSENGER DOOR. FLIGHT ATTENDANT REPORTED BEING LIGHT HEADED. NO INDICATION IN COCKPIT OF PRESSURIZATION ISSUE OR ANY CAUTION OR WARN
- [SDR QXEA2018120300447](https://openairdocs.org/sdr/QXEA2018120300447), Dec 3, 2018: CARPET. ODOR. MULTIPLE FLIGHT ATTENDANTS REPORTED AN ELECTRICAL BURNING SMELL IN FLIGHT NEAR THE LEFT SIDE OF ROW 4. THE SMELL WENT AWAY AND THEN CAME BACK AGAIN. TWO FLIGHT 
- [SDR QXEA2018102500385](https://openairdocs.org/sdr/QXEA2018102500385), Oct 24, 2018: NOT REPORTED. MALFUNCTIONED. DURING APPROACH INTO SEA THE RIGHT FUEL INLET TEMP GAUGE SHOWED 87C - 82C. WE RAN THE EA CHECKLIST AND TEMPERATURE DID NOT DECREASE. PERFORMED CONTINUITY AND ME
- [SDR QXEA2018102200377](https://openairdocs.org/sdr/QXEA2018102200377), Oct 20, 2018: HEATER. MALFUNCTIONED. RIGHT SIDE FUEL TEMPERATURE WAS HOT. IT WAS FLUCTUATING BETWEEN NORMAL AND A MAX OBSERVED TEMPERATURE OF 86 DEG C, BUT IT ONLY WAS MOMENTARILY THAT HOT. THE FLU
- [SDR QXEA2018101200363](https://openairdocs.org/sdr/QXEA2018101200363), Oct 9, 2018: BRAKE. MALFUNCTIONED. BRAKES MOMENTARTILY STICK AFTER THE PARKING BRAKE IS RELEASED. REMOVED FROM SERVICE. HOOKED UP AC GPU AND ENERGIZED HYDRAULICS. OPERATED PARK BRAKE SYSTEM REF A
- [SDR QXEA2018092400341](https://openairdocs.org/sdr/QXEA2018092400341), Sep 23, 2018: PUMP. LEAKING. ENG NR 2 DUE TO HIGH OIL CONSUMPTION AND OIL QUANTITY FOUND IN THE FWD COLLECTOR, R&R NR 2 FEATHERING PUMP. R&R NR 2 FEATHERING PUMP IAW AMM 61-20-31-000-801/40
- [SDR QXEA2018091000325](https://openairdocs.org/sdr/QXEA2018091000325), Sep 10, 2018: LIGHT. LOOSE. EMERGENCY LIGHTS AT ROW 9DE ARE LOOSE. RESECURED FLOOR PATH LIGHTING STRIP AT 9DE AND 10AB. NO DEFECTS NOTED. RETURNED TO SERVICE.
- [SDR QXEA2018082000294](https://openairdocs.org/sdr/QXEA2018082000294), Aug 15, 2018: SPRING. LACK OF LUBE. F/A REPORTED THE AFT JUMPSEAT LEFT OF CENTER UNDERSEAT EMERGENCY STOWAGE DOOR DOES NOT SPRING COMPLETELY CLOSED. REMOVED FROM SERVICE. CLEANED AND LUBED THE STO
- [SDR QXEA2018052200184](https://openairdocs.org/sdr/QXEA2018052200184), May 22, 2018: WARNING MESSAGE. MALFUNCTIONED. FLAP POWER CAUTION ILLUMINATED DURING DESCENT. RESET DID NOT SOLVE THE PROBLEM. REMOVED FROM SERVICE. CHECKED CDS FOR FAULT CODES. NO FAULT CODES NOTED IN HISTO
- [SDR QXEA2018052200182](https://openairdocs.org/sdr/QXEA2018052200182), May 19, 2018: FAULT CODE. FALSE INDICATION. NR 1 AUTOFEATHER TEST FAILED. REMOVED FROM SERVICE. INTERROGATED THE CDS, AND FOUND FAULT CODE 400A FOR THE NR 1 PROPELLOER IAW FIM 61-20-09-810-806, CLEARED FA
- [SDR QXEA2018043000164](https://openairdocs.org/sdr/QXEA2018043000164), Apr 30, 2018: WARNING LIGHT. FALSE ACTIVATION. CLIMBING THROUGH 13,000 FT, RECEIVED A FUSELAGE DOOR WARNING, CHECKING THE MFD DOORS PAGE, SAW THE AFT SERVICE DOOR INDICATED RED. FA-B PERFORMED A VISUAL INSPE
- [SDR QXEA2018041300138](https://openairdocs.org/sdr/QXEA2018041300138), Apr 12, 2018: WARNING HORN. FALSE ACTIVATION. TAKEOFF WARNING HORN SOUNDED DURING TAKEOFF. WARNING TEST WAS NORMAL ON TAXI OUT. ABORTED THE TAKEOFF. REMOVED FROM SERVICE. COMPLIED WITH FIM 31-52-00-810-802 
- [SDR QXEA2018040900136](https://openairdocs.org/sdr/QXEA2018040900136), Apr 5, 2018: CONTROLLER. INOPERATIVE. DURING CLIMB, NOTICED AIRCRAFT NOT PRESSURIZING IN AUTO MODE, THE AIRCRAFT DID PRESSURIZE IN MANUAL MODE. REMOVED FROM SERVICE. INTERROGATED CDS AND FOUND CPC/O
- [SDR QXEA2018031900098](https://openairdocs.org/sdr/QXEA2018031900098), Mar 17, 2018: LIGHT. DETACHED. EMERGENCY LIGHT STRIP BECAME DETACHED DURING DEPLANING. REMOVED FROM SERVICE. REINSTALLED THE EMERGENCY LIGHT. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SE
- [SDR QXEA2018030700084](https://openairdocs.org/sdr/QXEA2018030700084), Mar 7, 2018: CONTROL CABLE. OUT OF ADJUST. APPLYING BRAKES THE NOSE SWINGS TO THE RIGHT. HAPPENS ON EVERY BRAKE APPLICATION. REMOVED FROM SERVICE. PERFORMED, RIGGING OF MAIN BRAKE CONTROL CABLES. PERFORM
- [SDR QXEA2018030200082](https://openairdocs.org/sdr/QXEA2018030200082), Mar 2, 2018: DOOR. BINDING. AFT PAX DOOR DIFFICULT TO OPEN AND CLOSE. REMOVED FROM SERVICE. RESET THE AFT PAX DOOR IAW FIM 52-00-00-810-801, LUBRICATED THE DOOR SEAL. OPS CHECKED GOOD. RET
- [SDR QXEA2018020500038](https://openairdocs.org/sdr/QXEA2018020500038), Feb 3, 2018: BEARING. INOPERATIVE. AFT PASSENGER DOOR DIFFICULT TO OPEN. REMOVED FROM SERVICE. FOUND THE AFT DOOR FWD UPPER GUIDE ROLLER BINDING. REMOVED AND REPLACED THE UPPER GUIDE ROLLER IAW A
- [SDR QXEA2018011000011](https://openairdocs.org/sdr/QXEA2018011000011), Jan 9, 2018: CONTROL VALVE. INOPERATIVE. PASSING 10,500 FT, RECEIVED A CABIN PRESSURE WARNING, RAN E & A CHECKLIST AND DESCENDED TO 9,000 FT. PERFORMED THE PRESSURIZATION FAIL CHECKLIST. DURING THE CHE
- [SDR QXEA2017120800695](https://openairdocs.org/sdr/QXEA2017120800695), Dec 7, 2017: WARNING MESSAGE. FALSE ACTIVATION. WHEN T.O. POWER WAS APPLIED THE T.O. WARNING CAME ON. ABORTED TAKEOFF. WE TAXIED CLEAR OF RWY. ALL CONFIGURATIONS WERE SET FOR NORMAL T.O. C/W OPS TEST OF TAKEO
- [SDR QXEA2017091500569](https://openairdocs.org/sdr/QXEA2017091500569), Sep 14, 2017: WARNING LIGHT. FALSE ACTIVATION. FUSELAGE DOORS MASTER WARNING ILLUMINATED SEVRAL TIMES IN FLIGHT. SAW RATE OF CLIMB INCREASE AS SOON AS AFT PAX DOOR SHOWED CLOSED. RETURN TO FIELD. LANDING UNE
- [SDR QXEA2017053000375](https://openairdocs.org/sdr/QXEA2017053000375), May 29, 2017: WIRE HARNESS. DAMAGED. LEFT MAIN GEAR DOOR CAUTION ILLUMINATED DURING DESCENT 5-6 TIMES FOR APPROX 1 SECOND EACH TIME. INTERROGATED PSEU AND FOUND LGDRCL MH BELOW NOMINAL RANGE WITH N
- [SDR QXEA2017053000374](https://openairdocs.org/sdr/QXEA2017053000374), May 26, 2017: PROXIMITY SENSOR. OUT OF RIG. LEFT MAIN GEAR DOOR INTERMITTENT CAUTION ILLUMINATED DURING CLIMB OUT. RETURN TO FIELD. LANDING UNEVENTFUL. INTERROGATED PSEU IAW AMM TASK 32-61-00-742-801. FOU
- [SDR QXEA2017040300206](https://openairdocs.org/sdr/QXEA2017040300206), Mar 30, 2017: LIGHT. UNSECURE. EMERGENCY LIGHT STRIP AT ROW 20 COMING UP AT BOTH SIDES. RE-SECURED THE LIGHT STRIPS. RETURNED TO SERVICE.
- [SDR QXEA2017012700032](https://openairdocs.org/sdr/QXEA2017012700032), Jan 27, 2017: DOOR SEAL. DIRTY. AFT PASSENGER DOOR IS VERY STIFF TO OPEN. RAMP PERSONNEL HAVING TROUBLE OPENING FROM OUTSIDE. DOOR OPERATES NORMAL. DOOR SEAL AND MATING MEMBER WET. DRIED SEAL 
- [SDR QXEA2016120900790](https://openairdocs.org/sdr/QXEA2016120900790), Dec 8, 2016: SENSOR. OUT OF ADJUST. NOSE GEAR DOOR INDICATOR LIGHT CYCLED AFTER GEAR RETRACTION. RETURNED TO FIELD. LANDING UNEVENTFUL. PERFORMED ADJUSTMENT OF NG DR CL SENSOR IAW AMM 32-61-00-280

All 504: https://openairdocs.org/deregistered/N402QX-2023-08-22/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 DCA20CA010](https://openairdocs.org/ntsb/DCA20CA010), Oct 29, 2019: De Havilland DHC8 (N402QX), Boise, ID, substantial damage. Probable cause: a bird strike during climb out.

## FAA accident and incident reports (2)

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.

- [Accident 20191029020499A](https://openairdocs.org/incident/20191029020499A), Oct 29, 2019: Bombardier Inc DHC-8-402 (N402QX), Boise, ID, Substantial damage. Bird strike climbing out of kboi. No abnormal indications. No signs of significant damage. Landed in seattle, maintenance discovered fuel leaking from bird…
- [Incident 20030106000879I](https://openairdocs.org/incident/20030106000879I), Jan 6, 2003: Bombdr DHC8401 (N402QX), Seattle, WA. (-23) At rotation flight crew heard two loud bangs after which an autofeather on #2 engine occurred. Crew returned to the field and landed without incident.…

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