# N366PH: 1998 Bombardier DHC-8-202, registration cancelled 2020-02-11 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 11, 2020 - Exported to: Kenya - Status when cancelled: Valid registration - Airframe: [Bombardier DHC-8-202](https://openairdocs.org/model/bombardier-dhc-8-202) (registry code 1390007) - Engine: [Pratt & Whitney Canada PW123](https://openairdocs.org/engine/pratt-whitney-canada-pw123) (registry code 52129) - Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs) - Serial number: 510 - Year built: 1998 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: September 30, 1998 - Certificate issued: October 27, 2011 - Last registry action: May 9, 2018 - Mode S code: A423E3 - 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/N366PH - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=366PH - Page: https://openairdocs.org/deregistered/N366PH-2020-02-11 From the FAA registry file of October 31, 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-8-202: https://openairdocs.org/model/bombardier-dhc-8-202.md ## Service difficulty reports (262, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR A8ZR20180831001](https://openairdocs.org/sdr/A8ZR20180831001), Jul 5, 2018: LIGHT. DEFECTIVE. AFT RT EMERGENCY BETA LAMP FAILED BRIGHTNESS TEST. BETA LAMP ASSY REMOVED AND REPLACED REF AMM 33-51-00 REV 38 DATED MAY 15/17. - [SDR A8ZR20180830004](https://openairdocs.org/sdr/A8ZR20180830004), Jun 15, 2018: STRUCTURE. CRACKED. ACCOMPLISHED REPLACEMENT ON MAIN AIRSTAIR DOOR AFT EDGE MEMBER UPPER SECTION FOR CRACKS, REF STS EA 32-2018-078 REV IR DATED 06/15/2018. - [SDR A8ZR20180830003](https://openairdocs.org/sdr/A8ZR20180830003), Jun 15, 2018: SKIN. DENTED. ACCOMPLISHED REPLACEMENT OF DOUBLER TO UPPER SKIN ON AIRSTAIR DOOR FOR DENT, REF BOMBARDIER RD 8-52-040 ISSUE 4 DATED 2014-06-05. - [SDR A8ZR20180829007](https://openairdocs.org/sdr/A8ZR20180829007), Jun 7, 2018: SKIN. DENTED. LEFT LOWER SURFACE OF THE HORIZONTAL STABILIZER 15.5 INCHES INBD FROM OTBD EDGE AND 6.5 INCHES FWD OF AFT EDGE WAS DENTED. ACCOMPLISHED DOUBLER REPAIR IAW EA 45 - [SDR A8ZR20180828002](https://openairdocs.org/sdr/A8ZR20180828002), Jun 7, 2018: SKIN. DENTED. THE FUSELAGE SKIN AT BS 240.5 BETWEEN STRINGERS 29P & 30P WAS DENTED. REPAIRED IAW EA 42-2018-040, REV A-P2. - [SDR A8ZR20180829004](https://openairdocs.org/sdr/A8ZR20180829004), Jun 6, 2018: SKIN. DENTED. BS 293 TO 321.85, STRINGER 24S WAS DENTED. ACCOMPLISHED A DOUBLER AND TRIPLER REPAIR IAW EA 42-2018-041, REV B. - [SDR A8ZR20180829006](https://openairdocs.org/sdr/A8ZR20180829006), May 29, 2018: SKIN. DENTED. SKIN DENTED AT BS 321.6, STRINGER 24S-3.5, SUCCESSFULLY REFORMED BACK TO ORIGINAL CONTOUR WITH NO INDICATIONS FOR CRACKS AND CONSIDERED STRUCTURALLY ACCEPTABLE - [SDR A8ZR20180829005](https://openairdocs.org/sdr/A8ZR20180829005), May 29, 2018: SKIN. DENTED. SKIN DENTED AT BS 307.5, STRINGER 26S+1.60/ SUCCESSFULLY REFORMED BACK TO ORIGINAL CONTOUR WITH NO INDICATIONS FOR CRACKS AND CONSIDERED STRUCTURALLY ACCEPTABLE - [SDR A8ZR20180829009](https://openairdocs.org/sdr/A8ZR20180829009), May 25, 2018: SKIN. DENTED. SKIN PANEL DENTED ON THE RT AILERON TRIM TAB. REPAIRED IAW SRM 51-42-45. - [SDR A8ZR20180829008](https://openairdocs.org/sdr/A8ZR20180829008), May 22, 2018: SKIN. DENTED. ACCOMPLISHED A SKIN REPLACEMENT AND SPLICE 10.8 INCH X 1.70 INCH ON THE RT ELEVATOR SPRING TAB UPPER SURFACE, 2.5 INCHES INBD OF HINGE NR 2, 2.8 INCHES FWD OF T - [SDR A8ZR20180827002](https://openairdocs.org/sdr/A8ZR20180827002), May 21, 2018: SKIN. DENTED. THREE DENTS ON THE FUSELAGE AT BS 111.5 & 121.8 AND STRINGERS 21P & 22P. REFORMED TO ORIGINAL CONTOUR, CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 43-2018-066, RE - [SDR A8ZR201808290010](https://openairdocs.org/sdr/A8ZR201808290010), May 9, 2018: SKIN. DENTED. FUSELAGE SKIN AT BS 295, STRINGER 31S+2.8 INCHES DENTED. REPAIRED IAW EA 45-2018-067, REV ORIGINAL. - [SDR A8ZR20180830002](https://openairdocs.org/sdr/A8ZR20180830002), May 7, 2018: SKIN. DENTED. ACCOMPLISHED DOUBLER REPAIR ON L/H AILERON UPPER SURFACE AT YW 474 & 4.7" FWD OF TRIM TAB AND YW 476 & 1" TO 6" FWD OF TRIM TAB FOR MULTIPLE DENTS REF DEHAVILLA - [SDR A8ZR20180829002](https://openairdocs.org/sdr/A8ZR20180829002), Apr 26, 2018: SKIN. DENTED. DENT FOUND ON THE FUSELAGE SKIN AT BS 327.3, STRINGER 14P+5. REFORMED TO ORIGINAL CONTOUR AND FOUND TO BE WITHOUT CRACKING OR MATERIAL LOSS IAW EA 42-2018-042, - [SDR A8ZR20180829001](https://openairdocs.org/sdr/A8ZR20180829001), Apr 26, 2018: SKIN. DENTED. A DENT FOUND ON THE FUSELAGE SKIN AT BS 331.8 & STRINGER 14P+2.5. REFORMED TO ORIGINAL CONTOUR AND FOUND TO BE WITHOUT CRACKING OR MATERIAL LOSS IAW EA 42-2018- - [SDR A8ZR20180827004](https://openairdocs.org/sdr/A8ZR20180827004), Apr 25, 2018: SKIN. DENTED. A DENT WAS FOUND AT BS 120.3, STRINGER 27P+.6. REFORMED TO ORIGINAL CONTOUR WITH NO MATERIAL LOSS OR CRACK INDICATIONS AND CONSIDERED STRUCTURALLY ACCEPTABLE IA - [SDR A8ZR20180827003](https://openairdocs.org/sdr/A8ZR20180827003), Apr 25, 2018: SKIN. DENTED. DENT FOUND ATBS 118, STRINGER 26P-.55. REFORMED TO ORIGINAL CONTOUR WITH NO MATERIAL LOSS OR CRACK INDICATIONS AND CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 301 - [SDR A8ZR20180827005](https://openairdocs.org/sdr/A8ZR20180827005), Apr 25, 2018: SKIN. DENTED. DENT FOUND AT BS 108.5, STRINGER 15P. REFORMED WITH NO MATERIAL LOSS OR CRACK INDICATIONS AND CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 43-2018-067, REV ORIGINA - [SDR A8ZR20180830001](https://openairdocs.org/sdr/A8ZR20180830001), Apr 13, 2018: SKIN. CORRODED. ACCOMPLISHED REPLACEMENT OF DOUBLER FOR R/H FUSELAGE SKIN AROUND TOILET ACCESS DOOR FROM CORROSION, REF DEHAVILLAND DWG 85320983 REV P. - [SDR JJBA20170614009](https://openairdocs.org/sdr/JJBA20170614009), Jun 14, 2017: BATTERY PACK. INOPERATIVE. ALL EMERGENCY LIGHTS INOPERATIVE. R & R THE EMERGENCY LIGHT BATTERIES. OPS CHECKED GOOD. - [SDR JJBA20160924013](https://openairdocs.org/sdr/JJBA20160924013), Sep 24, 2016: LANDING GEAR. FAILED. DURING LANDING NLG FAILED TO EXTEND AND LANDED. OPEN. - [SDR JJBA20160816013](https://openairdocs.org/sdr/JJBA20160816013), Aug 16, 2016: ACTUATOR. INOPERATIVE. NOSE LANDING GEAR FAILED TO EXTEND ON FINAL. R & R NLG RETRACT ACTUATOR. OPS AND LEAK CHECKED GOOD. - [SDR JJBA20160728002](https://openairdocs.org/sdr/JJBA20160728002), Jul 28, 2016: UNKNOWN. SMOKE. AT NR 2 ENGINE START, SMOKE IN THE CABIN WITH BLEEDS ON. COMPLETED FAULT ISOLATION TROUBLESHOOTING IAW 72-00-04. BLEED LINES INSPECTED FOR OIL AND FOD. COULD NO - [SDR JJBA20160726007](https://openairdocs.org/sdr/JJBA20160726007), Jul 26, 2016: BLEED AIR SYS. PILOT ERROR. SMOKE IN THE FLIGHT DECK AND CABIN AFTER ENGINE START. CREW OPERATION ERROR. THEY STARTED THE ENGINES WITH BLEEDS OPEN. THIS WAS CONFIRMED BY THE CREW AND MAINT - [SDR JJBA20160108006](https://openairdocs.org/sdr/JJBA20160108006), Jan 8, 2016: SMOKE DETECTOR. FAULTY. LAVATORY SMOKE DETECTOR ALARM SOUNDED DURING TAXI. R & R SMOKE DETECTOR & OPERATIONS CHECK DONE. OPERATIONS CHECK WAS SATISFACTORY. - [SDR JJBA20160103003](https://openairdocs.org/sdr/JJBA20160103003), Jan 3, 2016: SWITCH. OUT OF ADJUST. EMERGENCY LIGHT SWITCH IS NOT ILLUMINATING GREEN. ADJUSTED EMER LIGHT SWITCH. PERFORMED OPERATIONS CHECK OF SYS, SYS TESTED SATISFACTORY. - [SDR JJBA20151226010](https://openairdocs.org/sdr/JJBA20151226010), Dec 26, 2015: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS DO NOT WORK WHEN TESTED. R & R LIGHT BATTERY PACKS. - [SDR JJBA20151029009](https://openairdocs.org/sdr/JJBA20151029009), Oct 29, 2015: TRIM PANEL. OUT OF ADJUST. TYPE NR 2 EMER EXIT DOOR HITTING THE OVERHEAD BIN WHEN REMOVING. ADJUSTED TYPE NR 2 EMER EXIT DOOR TRIM. - [SDR JJBA20151018006](https://openairdocs.org/sdr/JJBA20151018006), Oct 18, 2015: STUD. LOOSE. WHILE AUTOPILOT WAS OFF, VERY BUFFET IN THE CONTROL COLUMN APPEAR TO BE WORSE AT HIGH SPEEDS, BUFFET WENT AWAY WITH AUTOPILOT ON. PERFORMED GENERAL VISUAL INSPE - [SDR JJBA20150925006](https://openairdocs.org/sdr/JJBA20150925006), Sep 25, 2015: SMOKE DETECTOR. FALSE ACTIVATION. SMOKE WARNING ILLUMINATED IN FLIGHT. R & R FWD & AFT SMOKE DETECTORS. - [SDR JJBA20150602005](https://openairdocs.org/sdr/JJBA20150602005), Jun 2, 2015: BATTERY. DISCHARGED. GROUND POWER CART TRIPPED OFF & THE EMER LIGHTS CAME ON & WON'T GO OUT. EMER BATTERIES ARE DEAD. R & R EMER BATTERIES. - [SDR JJBA20150602013](https://openairdocs.org/sdr/JJBA20150602013), Jun 2, 2015: BATTERY. DISCHARGED. GROUND POWER CART TRIPPED OFF & THE EMER LIGHTS CAME ON & WON'T GO OUT. EMER BATTERIES ARE DEAD. R & R EMER BATTERIES. - [SDR JJBA20150506004](https://openairdocs.org/sdr/JJBA20150506004), May 6, 2015: BATTERY. DISCHARGED. EMERGENCY LIGHTS WILL NOT DISARM. LIGHTS STAY ILLUMINATED WHEN SELECTED OFF. R & R EMER LIGHT BATTERIES. - [SDR JJBA20150504002](https://openairdocs.org/sdr/JJBA20150504002), May 4, 2015: PSEU. MALFUNCTIONED. LANDING GEAR FAILED TO EXTEND NORMALLY. R & R PROX SWITCH ELECTRONICS UNIT DUE TO PAST FAILURE. R & R LANDING GEAR SELECTOR VLV DUE TO HIGH RESISTANCE READINGS. - [SDR JJBA20150422012](https://openairdocs.org/sdr/JJBA20150422012), Apr 22, 2015: CONTROL HANDLE. FAULTY. LANDING GEAR FAILED TO EXTEND NORMALLY. R & R LG SELECTOR HANDLE. EMER DECLARED. - [SDR JJBA20150212010](https://openairdocs.org/sdr/JJBA20150212010), Feb 12, 2015: SKIN. CRACKED. PASSENGER DOOR INNER SKIN WAS FOUND TO BE CRACKED ON THE LOWER PANEL & GOUGED ON THE LOWER FWD SIDE PANEL. R & R PAX DOOR LOWER INNER SKIN & REPAIRED PAX DOOR L - [SDR JJBA20150115001](https://openairdocs.org/sdr/JJBA20150115001), Jan 15, 2015: CONNECTOR. CORRODED. PASSENGER DOOR STEP LIGHT ELEC CONNECTIONS CORRODED & WIRES NOT SECURED TO STEPS IN SEVERAL AREAS. REMOVED & TREATED CORRODED LIGHT ASSEMBLIES. R & R LIGHT ASSE - [SDR JJBA20141122011](https://openairdocs.org/sdr/JJBA20141122011), Nov 22, 2014: BATTERY PACK. DISCHARGED. ALL EMER LIGHTS IN CABIN JUST FLICKER WHEN TURNED ON AT ALL SWITCHES. R & R ALL EMER LIGHT BATTERY PACKS. - [SDR JJBA20140817005](https://openairdocs.org/sdr/JJBA20140817005), Aug 17, 2014: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS INOPERATIVE AT TYPE TWO EXIT, MAIN CABIN DOOR & SECOND OVERHEAD LIGHT. R & R PS1 & PS2 BATTERY PACKS. - [SDR JJBA20140622010](https://openairdocs.org/sdr/JJBA20140622010), Jun 22, 2014: BATTERY. DIRTY. THREE EMERGENCY EXIT SIGN LIGHTS WILL NOT TEST. CLEANED, RESEATED & CHARGED EMERGENCY BATTERIES. - [SDR JJBA20140615007](https://openairdocs.org/sdr/JJBA20140615007), Jun 15, 2014: LIGHT. INOPERATIVE. FORWARD FLOOR EMERGENCY ESCAPE LIGHT HAS INOPERABLE BULBS. R & R FWD FLOOR EMERGENCY ESCAPE LIGHT ASSEMBLY. - [SDR JJBA20140505001](https://openairdocs.org/sdr/JJBA20140505001), May 5, 2014: DOOR. INOPERATIVE. GALLEY CABINET DOOR INOPERABLE. SECURED GALLEY DOOR. - [SDR JJBA20140124014](https://openairdocs.org/sdr/JJBA20140124014), Jan 24, 2014: BATTERY. DISCHARGED. NR 1 & NR 3 CEILING EMERGENCY LIGHTS FAIL TO ILLUMINATE DURING TEST. RAN ENGS & CHARGED SYSTEM. - [SDR JJBA20131031009](https://openairdocs.org/sdr/JJBA20131031009), Oct 31, 2013: WIRE. BROKEN. F/A EMERGENCY CALL BUTTON INOPERATIVE. REPAIRED BROKEN WIRE ON CONTROL PANEL. - [SDR JJBA20130615026](https://openairdocs.org/sdr/JJBA20130615026), Jun 15, 2013: LIGHT. INOPERATIVE. CREW REPORTED THAT DURING PREFLIGHT, OBSERVED A SECTION OF THE FLOOR EMERGENCY LIGHT STRIP WAS INOPERATIVE. MX REPLACED THE STRIP. - [SDR JJBA20130511010](https://openairdocs.org/sdr/JJBA20130511010), May 11, 2013: PUMP. FAILED. CREW REPORTED NR 1 HYD FLUID QTY WAS DROPPED TO ZERO. MX REPLACED THE NR 1 EDP. - [SDR JJBA20130415006](https://openairdocs.org/sdr/JJBA20130415006), Apr 15, 2013: BATTERY. INOPERATIVE. DURING PREFLIGHT CREW REPORTED THE OVERHEAD EMERGENCY LIGHT OVER ROW 9 WAS INOPERATIVE. MX REPLACED THE BATTERY. ALL OPS CHECKS WERE SATISFACTORY. - [SDR JJBA20130414005](https://openairdocs.org/sdr/JJBA20130414005), Apr 14, 2013: BATTERY PACK. INOPERATIVE. DURING PREFLIGHT CREW OBSERVED THE REAR OVER HEAD EMERGENCY LIGHT TO BE INOPERATIVE. GROUND MX CREW R & R THE BATTERY PACK. ALL OPS CHECKS WERE SATISFACTORY. - [SDR JJBA20130128015](https://openairdocs.org/sdr/JJBA20130128015), Jan 28, 2013: BATTERY. FAILED. DURING A LINE CHECK INSPECTION, THE TECH NOTICED SEVERAL INTERIOR EMERGENCY LIGHT BATTERIES HAD FAILED TO ILLUMINATED DURING TESTING. THE TECH REPLACED THE PS-5 - [SDR JJBA20121217007](https://openairdocs.org/sdr/JJBA20121217007), Dec 17, 2012: BATTERY. DISCHARGED. DURING PREFLIGHT THE CREW NOTICED THE EMERGENCY LIGHTING WAS NOT ILLUMINATING DURING TESTING. GROUND MX CREW DISCOVERED THAT THE EMERGENCY LIGHT BATTERIES WERE All 262: https://openairdocs.org/deregistered/N366PH-2020-02-11/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 DCA16CA226](https://openairdocs.org/ntsb/DCA16CA226), Sep 24, 2016: Bombardier DHC 8 202 (N366PH), Dulles, VA, substantial damage. Probable cause: incorrect installation of the frangible towing fuse that prevented the nose landing gear from extending. ## 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 20160924019569I](https://openairdocs.org/incident/20160924019569I), Sep 24, 2016: Bombardier Inc DHC-8-202 (N366PH), Chantilly, VA, Minor damage. Nose landing gear failed to extend. First flight out of "a" check. Nose landing gear frangible fuse was replaced during the "a" check. Frangible fuse was… - [Incident 20021123032089I](https://openairdocs.org/incident/20021123032089I), Nov 23, 2002: Dhav DHC8202 (N366PH), Portland, OR. (-23) On approach to pdx, landing gear handle was selected down and indicated three red (unsafe) lights. Gear did not come out of the wheel wells. Crew… - [Incident 20010304005769I](https://openairdocs.org/incident/20010304005769I), Mar 4, 2001: Dhav DHC8202 (N366PH), Portland, OR, Minor damage. (-23) Horizon air flight 2017 a/c N366PH incurred a birdstrike on takeoff from Portland, Oregon. A/c returned to field without incident. Maintenance at pdx did… --- 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.