# N407QX: 2001 Bombardier DHC-8-402, registration cancelled 2020-08-10

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 10, 2020
- 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: 4049
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: April 18, 2005
- Certificate issued: October 5, 2001
- Last registry action: May 10, 2018
- Mode S code: A4C816
- 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/N407QX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=407QX
- Page: https://openairdocs.org/deregistered/N407QX-2020-08-10

From the FAA registry file of November 5, 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 (627, newest 50)

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

- [SDR QXEA2019093000370](https://openairdocs.org/sdr/QXEA2019093000370), Sep 29, 2019: UNKNOWN. MALFUNCTIONED. AFTER ADVANCING CONDITION LEVERS FOR LANDING, RIGHT PROP REACHED 1020 AND LEFT REACHED 950 RPM. LANDING UNEVENTFUL. REMOVED FROM SERVICE. PERFORMED FADEC TRIM (
- [SDR QXEA2019060300232](https://openairdocs.org/sdr/QXEA2019060300232), May 30, 2019: GLOWSTRIP. LOOSE. AISLE GLOW IN THE DARK STRIP HAS COME UNATTACHED FROM THE FLOOR AT 3DE. REMOVED FROM SERVICE. RESECURED LUMINESCENT STRIP AT 3DE AS REQUIRED. NO FURTHER DEFECTS
- [SDR QXEA2019043000197](https://openairdocs.org/sdr/QXEA2019043000197), Apr 28, 2019: EXTINGUISHER. MALFUNCTIONED. DURING CRUISE AT FL 240 MASTER WARNING ILLUMINATED INTERMITTENTLLY APPROX 3 SEPARATE TIME WITH ASSOCIATED CHECK FIRE DET AAND APU BTL LOW LIGHT ALSO ILLUMINATIN
- [SDR QXEA2019022800094](https://openairdocs.org/sdr/QXEA2019022800094), Feb 26, 2019: RETURN SPRING. DEFECTIVE. AFT FA STORAGE BIN UNDER JUMPSEAT DOESNT SPRING BACK. REMOVED FROM SERVICE. REPLACED RETURN SPRING ON AFT FA STORAGE BIN. REF CMM 25-21-47. DOOR CLOSES AS NORMA
- [SDR QXEA2018112900436](https://openairdocs.org/sdr/QXEA2018112900436), Nov 26, 2018: STEP. OUT OF LIMITS. FWD TYPE II/III DOOR STILL HAS LOUD SQUEAL IN CLIMB/CRUISE PRESSURIZATION NORMAL. PRESSURIZED AIRCRAFT AND CHECK DOOR FOR LEAKS REF AMM 21-31-00-720-801. FOUND 
- [SDR QXEA2018080700285](https://openairdocs.org/sdr/QXEA2018080700285), Aug 6, 2018: LAMP. INOPERATIVE. AFT EXIT ROW SIGN HAS A BURNED OUT LIGHT ADVISORY. REMOVED FROM SERVICE. REPLACED THE LAMP. OBSERVED NORMAL OPERATION. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURN
- [SDR QXEA2018073100270](https://openairdocs.org/sdr/QXEA2018073100270), Jul 29, 2018: CONNECTOR. DIRTY. NR 1 RUD HYD ILLUMINATED DURING CRUSE FLIGHT AT 14,000. RETURNED TO THE FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. FOUND HI RESISTANCE IN WIRE 2700-P4 PIN
- [SDR QXEA2017101300616](https://openairdocs.org/sdr/QXEA2017101300616), Oct 10, 2017: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS IN MID CABIN AFT, FAILED TO ILLUMINATE DURING AN OPERATIONAL CHECK. REMOVED AND REPLACED THE BATTERY PACKS. OPS CHECKED GOOD IAW AMM 33-51-00-7
- [SDR QXEA2017091900572](https://openairdocs.org/sdr/QXEA2017091900572), Sep 17, 2017: TIMER. MALFUNCTIONED. AIRFRAME DEICE BOOTS WOULD NOT CYCLE IN SLOW OR FAST. NO CAUTION LIGHTS ILLUMINATED. BOOTS WOULD CYCLE IN MANUAL MODE. ALL BOOTS ON LEFT WING APPEARED INFLATED 
- [SDR QXEA2017082100523](https://openairdocs.org/sdr/QXEA2017082100523), Aug 16, 2017: HINGE. BROKEN. FLASHLIGHT AND LIFE VEST COMPARTMENT BELOW FLIGHT ATTENDANT JUMPSEAT WILL NOT SPRING CLOSED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED HINGE ASSEMBLY 
- [SDR QXEA2017071700472](https://openairdocs.org/sdr/QXEA2017071700472), Jul 17, 2017: ESCAPE ROPE. OUT OF POSITION. NYLON ROPE EXPOSED ON THE INSIDE OF THE TYPE III EMERGENCY EXIT.AIRCRAFT REMOVED FROM SERVICE. REPOSITIONED THE ROPE. CHECKS GOOD. RETURNED TO SERVICE. NO PARTS
- [SDR QXEA2017071000459](https://openairdocs.org/sdr/QXEA2017071000459), Jul 7, 2017: PCU. MALFUNCTIONED. NR 1 RUDDER HYD CAUTION ILLUMINATED DURING CRUISE, PUSH OFF LIGHT DID NOT ILLUMINATE. NO OTHER ABNORMALITIES. REMOVED FROM SERVICE. REPLACEMENT OF LOWER RUDDER 
- [SDR QXEA201707050446](https://openairdocs.org/sdr/QXEA201707050446), Jul 2, 2017: CHANNEL. UNKNOWN. AFTER ACCELERATION HEIGHT, FLAPS UP, EXPERIANCED CONSTANT VIBRATION AND NOISE THROUGH ENTIRE FLIGHT REGARDLESS OF AIRSPEED, POWER SETTING, PROP SETTING OR PITCH
- [SDR QXEA2017062800435](https://openairdocs.org/sdr/QXEA2017062800435), Jun 27, 2017: FAIRING. DAMAGED. DURING DESCENT, PASSING THROUGH FL180 A SUDDEN AND PRONOUNCED CHANGE IN AIRCRAFT SOUND (A RUMBLE) WITH AIRFRAME VIBRATION IN THE FLOOR AND POWER LEVER QUADRANT.
- [SDR QXEA2017051900363](https://openairdocs.org/sdr/QXEA2017051900363), May 17, 2017: BEAM. CRACKED. FORWARD BAGGAGE DOOR RT FWD BEAM ABOVE VENT DOOR CRACKED. LOCATED AND DRILLED NEW MACHINED BEAM.
- [SDR QXEA2017051500355](https://openairdocs.org/sdr/QXEA2017051500355), May 13, 2017: BRACKET. BENT. FWD BAGGAGE DOOR LOWER AFT BRACKET IS BENT PN 85217586-103. REMOVED BRACKET FROM FWD BAGGAGE DOOR RT PER SRM 51-42-05 REPAIR01. INSTALLED NEW BRACKET PN 8521758
- [SDR QXEA2017050200338](https://openairdocs.org/sdr/QXEA2017050200338), Apr 28, 2017: RIVET. CORRODED. FUS X 116-136 STR 24L, 25L, & 26L HAVE CORRODED FASTENERS. REMOVED CORRODED RIVETS REF SRM 51-42-05 REPAIR-01. INSTALLED NEW RIVETS REF SRM 51-42-05 REPAIR-01. 
- [SDR QXEA2017050200340](https://openairdocs.org/sdr/QXEA2017050200340), Apr 28, 2017: SEAT TRACK. DAMAGED. REPLACE SEAT TRACK 9 PN 85338210-111. REMOVED SPLICE FITTINGS INBOARD OUTBD COMMON TO SEAT TRACK 9 AND 8 REF SRM 51-40-15-02-01. INSTALLED SPLICE FITTINGS INBD 
- [SDR QXEA2017050300342](https://openairdocs.org/sdr/QXEA2017050300342), Apr 25, 2017: DOOR. CRACKED. SERVICE DOOR RT AFT BEAM ABOVE VENT DOOR CRACKED. REMOVED AFT SERVICE DOOR VENT DOOR. INSTALLED A REPLACEMENT VENT DOOR.
- [SDR QXEA2017050300341](https://openairdocs.org/sdr/QXEA2017050300341), Apr 24, 2017: BEAM. CRACKED. AFT ENTRY DOOR BEAM ABOVE THE VENT DOOR CRACKED. REMOVED VENT DOUBLER PN 85217351-101 AND STIFFENER PN 85217471-102. INSTALLED VENT DOUBLER PN 85217351-101 & ST
- [SDR QXEA2017050200337](https://openairdocs.org/sdr/QXEA2017050200337), Apr 18, 2017: SEAT TRACK. CORRODED. SEAT TRACK 11 REQUIRES REPLACEMENT. REMOVED FASTENERS REF SRM 51-40-07. INSTALLED NEW SEAT TRACK 11 PN 85328210-115 REF SRM 51-41-00-00-01 AND 51-42-05-02-01. L
- [SDR QXEA2017050200339](https://openairdocs.org/sdr/QXEA2017050200339), Apr 18, 2017: SEAT TRACK. DAMAGED. SEAT TRACK 10 REQUIRES REPLACEMENT. REMOVED ALL FASTENERS FROM SEAT TRACK 10 IAW SRM 51-40-07. REMOVED 10 SEAT TRACK REF SRM 51-40-07. INSTALLED NEW SEAT TRACK 
- [SDR QXEA2017050200336](https://openairdocs.org/sdr/QXEA2017050200336), Apr 10, 2017: STIFFENER. CRACKED. LT NACELLE AFT FAIRING PNL 414AR AFT BOTTOM ANGLE CRACKED. REMOVED AFT BOTTOM STIFFENER PN 85414249-102 FROM AFT FAIRING PNL 414AR REF SRM 51-42-05. INSTALLED N
- [SDR QXEA2017031600128](https://openairdocs.org/sdr/QXEA2017031600128), Mar 16, 2017: LIGHT. LOOSE. EMERGENCY LIGHT NEAR THE COCKPIT DOOR IS LOOSE. SECURED THE LIGHT AND RETURNED TO SERVICE.
- [SDR QXEA2017012500026](https://openairdocs.org/sdr/QXEA2017012500026), Jan 24, 2017: POWER SUPPLY. MALFUNCTIONED. FORWARD CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-01-000-801 AND 33-51-01-400-801. NO HELP. PLACED FORW
- [SDR QXEA2016110400703](https://openairdocs.org/sdr/QXEA2016110400703), Nov 3, 2016: COVER. DETACHED. FORWARD EMERGENCY EXIT LIGHT COVER FELL OFF. REATTACHED LIGHT COVER. NO DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.
- [SDR QXEA2016100600645](https://openairdocs.org/sdr/QXEA2016100600645), Oct 3, 2016: CIRCUIT BREAKER. OPEN. DURING AUTOFEATHER TEST, BOTH SIDES SHOW ABORT. FOUND CIRCUIT BREAKER J6 OPEN. RESET AND PERFORMED OPS TEST IAW AMM 61-20-00-710-801. TESTS GOOD. RETURNED TO SE
- [SDR QXEA2016092700614](https://openairdocs.org/sdr/QXEA2016092700614), Sep 27, 2016: LIGHT. INOPERATIVE. FORWARD F/A EMERGENCY LIGHT BULB IS BURNED OUT. RELAMPED THE FORWARD F/A EMERGENCY LIGHT. OPS TESTS GOOD. RETURNED TO SERVICE.
- [SDR QXEA2016082900559](https://openairdocs.org/sdr/QXEA2016082900559), Aug 29, 2016: WIRE HARNESS. DEFECTIVE. PROP DE-ICE CAUTION LIGHT ILLUMINATED A FEW SECONDS EVERY TIME NR 1 PROP DE-ICE, GREEN LIGHT ILLUMINATED. RETURNED TO FIELD. LANDING UNEVENTFUL. CLEARED FAULTS 
- [SDR QXEA2016051100315](https://openairdocs.org/sdr/QXEA2016051100315), May 11, 2016: LINE. LEAKING. ON TAXI TO THE GATE, ACFT LOST HYDRAULIC QTY, DROPPED TO ZERO. ELEVATORS, NOSE WHEEL STEERING, AND SPOILERS BECAME INOPERATIVE. ACFT MADE IT SAFELY TO THE GATE.
- [SDR QXEA2016022000159](https://openairdocs.org/sdr/QXEA2016022000159), Feb 20, 2016: DISPLAY. MALFUNCTIONED. CAPTAIN'S PFD WENT BLANK AS ACFT PULLED ON RUNWAY FOR TAKEOFF. R & R NR 1 PFD WITH NEW FROM STOCK IAW TC 6316104. FOUND AIR FILTER CAKED WITH DUST, R & R WITH N
- [SDR QXEA2016012200055](https://openairdocs.org/sdr/QXEA2016012200055), Jan 22, 2016: HANDLE. LACK OF LUBE. AFT SERVICE DOOR DIFFICULT TO OPEN. CLEANED AND LUBED THE SEAL AND HANDLE. DOOR OPERATES NORMALLY. RETURNED TO SERVICE.
- [SDR QXEA2015102300558](https://openairdocs.org/sdr/QXEA2015102300558), Oct 23, 2015: COFFEEMAKER. OVERHEATED. ELECTRICAL ODOR IN THE AFT GALLEY AN APPROACH. THE GALLEY HOT JUG WAS FOUND TO BE EXTREMELY HOT. FERRIED FOR REPAIRS. FOUND NO DEFECTS WITH HOT JUG CONNECTIONS.
- [SDR QXEA2015092700511](https://openairdocs.org/sdr/QXEA2015092700511), Sep 27, 2015: STARTER GEN. MALFUNCTIONED. APU FAIL DURING START. RAMP AGENTS REPORTED SMOKE COMING FROM EXHAUST, BLOWING SMOKE FROM EXHAUST. STARTED APU WITH EXTERNAL POWER AND APU RAN NORMAL. DEPRESSED
- [SDR QXEA2015060400307](https://openairdocs.org/sdr/QXEA2015060400307), Jun 4, 2015: SPRING. BENT. AFT PASSENGER DOOR WILL NOT CLOSE AND HANDLE WILL NOT TURN. FOUND OVER CENTER SPRING ASSLY ON LIFT AND LATCH ASSEMBLY BENT. REPLACED. RETURNED TO SERVICE.
- [SDR QXEA2015060400308](https://openairdocs.org/sdr/QXEA2015060400308), Jun 4, 2015: BRACKET. DAMAGED. FOUND AFT PASSENGER DOOR LIFT AND LATCH BRACKET WORN AND DAMAGED. REPLACED IAW SRM 51-40-15. RETURNED TO SERVICE.
- [SDR QXEA2015052200278](https://openairdocs.org/sdr/QXEA2015052200278), May 22, 2015: DOOR. OUT OF ADJUST. NLG ALTERNATE EXTENSION RELEASE DOOR DOES NOT SIT FLUSH WITH THE FLIGHT DECK FLOORING AT THE FORWARD END. INSPECTED COMPARTMENT AND FOUND FOD ALONG THE DOOR MAT
- [SDR QXEA2015052200266](https://openairdocs.org/sdr/QXEA2015052200266), May 20, 2015: TEE FITTING. CRACKED. FWD PAX DOOR TEE FITTING IS CRACKED. R & R THE TEE FITTING IAW SRM 51-42-05, REPAIR 01 AND SRM 51-42-45.
- [SDR QXEA2015052100249](https://openairdocs.org/sdr/QXEA2015052100249), May 18, 2015: SKIN. DAMAGED. RIGHT ELEVATOR T/E AT MOST OTBD STATIC WICK HAS LIGHTNING STRIKE DAMAGE. INSTALLED REPAIR DOUBLER AND REPAIR PACKERS ON RT ELEVATOR TRIMING EDGE OTBD SIDE REF S
- [SDR QXEA2015052000247](https://openairdocs.org/sdr/QXEA2015052000247), May 17, 2015: SEAT TRACK. DAMAGED. SEAT TRACK NR 10 DAMAGED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-00, SRM 51-40-15, AND DWG 85328201, REV-E.
- [SDR QXEA2015052000245](https://openairdocs.org/sdr/QXEA2015052000245), May 17, 2015: SEAT TRACK. DAMAGED. SEAT TRACK NR 7 DAMAGED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05 AND 51-41-00.
- [SDR QXEA2015052100254](https://openairdocs.org/sdr/QXEA2015052100254), May 16, 2015: SEAT TRACK. DAMAGED. SEAT TRACK NR 1 DAMAGED. REPAIRED IAW SRM.
- [SDR QXEA2015052100253](https://openairdocs.org/sdr/QXEA2015052100253), May 16, 2015: SEAT TRACK. DAMAGED. SEAT TRACK NR 2 DAMAGED. REPAIRED IAW SRM.
- [SDR QXEA2015052100252](https://openairdocs.org/sdr/QXEA2015052100252), May 16, 2015: SEAT TRACK. DAMAGED. SEAT TRACK NR 3 DAMAGED. INSTALLED NEW SEAT TRACK IAW SRM 51-40-15 AND 51-42-05-02-01.
- [SDR QXEA2015052100251](https://openairdocs.org/sdr/QXEA2015052100251), May 16, 2015: SEAT TRACK. DAMAGED. SEAT TRACK NR 18 DAMAGED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM'S 51-42-45, PARA 6H, 51-42-05 PARA 4E, 51-40-15 PARA 6M.
- [SDR QXEA2015052100250](https://openairdocs.org/sdr/QXEA2015052100250), May 16, 2015: SEAT TRACK. DAMAGED. SEAT TRACK NR 19 DAMAGED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05, 51-42-15, 51-42-45 AND 51-40-15.
- [SDR QXEA2015052100248](https://openairdocs.org/sdr/QXEA2015052100248), May 16, 2015: SEAT TRACK. DAMAGED. SEAT TRACK NR 20 DAMAGED. INSTALLED NEW SEAT TRACK IAW SRM 51-42-05-02-01, STEP 4D, 3-10 AND SRM 51-40-15-02-01, STEP 6H2.
- [SDR QXEA2015052000246](https://openairdocs.org/sdr/QXEA2015052000246), May 12, 2015: SEAT TRACK. DAMAGED. SEAT TRACK NR 8 DAMAGED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-00-00-01, SRM 51-42-05-02-01 STEP 4D (3-10) AND 51-40-15-02-01, STEP 6H2.
- [SDR QXEA2015051400237](https://openairdocs.org/sdr/QXEA2015051400237), May 12, 2015: STRUCTURE. CORRODED. CORROSION UNDERNEATH STRINGER TO FRAME CLIP AT STR 25L BETWEEN FS 664.500 + FS 668.900. 6J, 51-23-00 PAR 2A, FIG 1 AND RD8/4-53-6837, ISSUE 1, SHT 2 AND DWG 853
- [SDR QXEA2015051400234](https://openairdocs.org/sdr/QXEA2015051400234), May 11, 2015: STRINGER. CORRODED. CORROSION ON STRINGER 25P BETWEEN FS X664.5 TO FS X668.90. REMOVED CORROSION FROM STR 25P IAW SRM 51-21-00, PAR 4A ITEM 5. 100 PERCENT MATERIAL LOSS AT FS X667.

All 627: https://openairdocs.org/deregistered/N407QX-2020-08-10/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 20040411004819I](https://openairdocs.org/incident/20040411004819I), Apr 11, 2004: Bombdr DHC8401 (N407QX), Spokane, WA, Minor damage. (-23) The flight officers windshield cracked when in cruise flight sea to mso. The aircraft followed normal procedure and landed without incident at get.…

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