# Bombardier DHC-8-202 - Type: Aircraft model (FAA registry) - Registry code: 1390007 - Manufacturer (registry): BOMBARDIER INC - Model: DHC-8-202 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-prop - Seats: 40 - Weight class: 20,000 lb and over - Certification: Type certificated - Data sheet: [TCDS A13NM](https://openairdocs.org/tcds/A13NM) (OpenAirDocs) - Holder: De Havilland Aircraft of Canada Limited - Registered aircraft: 14 - Page: https://openairdocs.org/model/bombardier-dhc-8-202 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [AD 2026-11-06](https://openairdocs.org/ad/2026-11-06): Hardware; Standard practices/structures · De Havilland Aircraft of Canada DHC-8-101, DHC-8-102, DHC-8-103 and 9 more. Effective Jul 9, 2026 - [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026 - [AD 2022-15-08](https://openairdocs.org/ad/2022-15-08): Information systems · Airbus A318-111, A318-112, A319-111 and 49 more. Effective Aug 12, 2022 - [AD 2021-19-11](https://openairdocs.org/ad/2021-19-11): Flight controls · De Havilland Aircraft of Canada DHC-8-102, DHC-8-103, DHC-8-106 and 8 more. Effective Nov 18, 2021 - [AD 2019-12-17](https://openairdocs.org/ad/2019-12-17): Stabilizers · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Aug 12, 2019 - [AD 2018-23-04](https://openairdocs.org/ad/2018-23-04): Engine Controls · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Mar 15, 2019 - [AD 2018-20-12](https://openairdocs.org/ad/2018-20-12): Ice and rain protection · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Nov 23, 2018 - [AD 2017-15-11](https://openairdocs.org/ad/2017-15-11): Landing Gear · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Sep 5, 2017 - [AD 2017-08-02](https://openairdocs.org/ad/2017-08-02): Ignition · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective May 17, 2017 - [AD 2016-24-06](https://openairdocs.org/ad/2016-24-06): Ice and rain protection · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Jan 12, 2017 - [AD 2016-24-01](https://openairdocs.org/ad/2016-24-01): Electrical Power · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Dec 30, 2016 - [AD 2016-10-07](https://openairdocs.org/ad/2016-10-07): Electrical power · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Jun 23, 2016 - [AD 2015-21-02](https://openairdocs.org/ad/2015-21-02): Electrical Power · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Nov 24, 2015 - [AD 2015-14-03](https://openairdocs.org/ad/2015-14-03): Fuel · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Aug 21, 2015 - [AD 2015-04-08](https://openairdocs.org/ad/2015-04-08): Landing Gear · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Apr 27, 2015 - [AD 2013-15-06](https://openairdocs.org/ad/2013-15-06): Electrical Power · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Oct 20, 2014 - [AD 2014-15-07](https://openairdocs.org/ad/2014-15-07): Wings · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Sep 2, 2014 - [AD 2014-13-18](https://openairdocs.org/ad/2014-13-18): Instruments, Engine Controls · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Aug 19, 2014 - [AD 2014-05-17](https://openairdocs.org/ad/2014-05-17): Fuel · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective May 2, 2014 - [AD 2013-22-04](https://openairdocs.org/ad/2013-22-04): Flight controls · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 8 more. Effective Dec 5, 2013 - [AD 2013-14-09](https://openairdocs.org/ad/2013-14-09): Landing gear · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Sep 10, 2013 - [AD 2013-04-07](https://openairdocs.org/ad/2013-04-07): Electrical Power · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Apr 9, 2013 - [AD 2012-15-16](https://openairdocs.org/ad/2012-15-16): Landing gear · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 8 more. Effective Sep 12, 2012 - [AD 2012-04-08](https://openairdocs.org/ad/2012-04-08): Flight controls · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 8 more. Effective Apr 10, 2012 - [AD 2011-24-10](https://openairdocs.org/ad/2011-24-10): Equipment/Furnishings · Bombardier DHC-8-201 and DHC-8-202. Effective Dec 16, 2011 - [AD 2011-21-08](https://openairdocs.org/ad/2011-21-08): Equipment/Furnishings · ATR - GIE Avions de Transport Régional ATR42-200, ATR42-300, ATR42-320 and 202 more. Effective Nov 23, 2011 - [AD 2011-21-04](https://openairdocs.org/ad/2011-21-04): Doors · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Nov 16, 2011 - [AD 2011-09-12](https://openairdocs.org/ad/2011-09-12): Windows · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 8 more. Effective Jun 6, 2011 - [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011 - [AD 2010-21-02](https://openairdocs.org/ad/2010-21-02): Landing gear · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 9 more. Effective Nov 12, 2010 - [AD 2010-19-02](https://openairdocs.org/ad/2010-19-02): Fuel · Bombardier DHC-8-201, DHC-8-202, DHC-8-301 and 2 more. Effective Oct 18, 2010 - [AD 2010-05-12](https://openairdocs.org/ad/2010-05-12): Wings · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 2 more. Effective Apr 13, 2010 - [AD 2010-04-12](https://openairdocs.org/ad/2010-04-12): Landing Gear, Standard Practices/Structures, Doors, Fuselage, Nacelles/Pylons, Stabilizers and Wings. · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Apr 8, 2010 - [AD 2008-09-25 R1](https://openairdocs.org/ad/2008-09-25-R1): Fuel · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Dec 10, 2009 - [AD 2009-21-03](https://openairdocs.org/ad/2009-21-03): APU full- authority digital controller (FADEC) · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 10 more. Effective Nov 20, 2009 - [AD 2009-06-21](https://openairdocs.org/ad/2009-06-21): Fuselage spoiler cable · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 8 more. Effective Apr 28, 2009 - [AD 2008-26-03](https://openairdocs.org/ad/2008-26-03): Electronic strike system of the cockpit doo · Cockpit door electro-mechanical strike (Jazz Air STC ST02014NY). Effective Apr 13, 2009 - [AD 2008-13-09](https://openairdocs.org/ad/2008-13-09): Fuel tank bonding jumpers · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Sep 17, 2008 - [AD 2008-04-17](https://openairdocs.org/ad/2008-04-17): Observer utility light system · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 8 more. Effective Apr 3, 2008 - [AD 2007-23-04](https://openairdocs.org/ad/2007-23-04): Elevator spring tab mechanism · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Dec 11, 2007 - [AD 2007-21-16](https://openairdocs.org/ad/2007-21-16): Spolier cable · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Nov 21, 2007 - [AD 2007-12-01](https://openairdocs.org/ad/2007-12-01): Main landing gear (MLG) shock strut · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Jul 10, 2007 - [AD 2007-06-19](https://openairdocs.org/ad/2007-06-19): Main landing gear (MLG) and nose landing gear (NLG) handle assemblies for alternate release and the MLG retaining plate. · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Apr 27, 2007 - [AD 2007-04-22](https://openairdocs.org/ad/2007-04-22): Electrical cable harness assembly. · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Apr 3, 2007 - [AD 2007-01-11](https://openairdocs.org/ad/2007-01-11): Flight compartment door · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 9 more. Effective Mar 5, 2007 - [AD 2006-20-04](https://openairdocs.org/ad/2006-20-04): Inspection of chain assemblies of elevator trim system · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Nov 2, 2006 - [AD 2006-17-17](https://openairdocs.org/ad/2006-17-17): Rivets on left and right control column torque tube assemblies · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 8 more. Effective Sep 29, 2006 - [AD 2006-17-10](https://openairdocs.org/ad/2006-17-10): Fluorescent light tube assemblies of the cabin, lavatory, and sidewall · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Sep 27, 2006 - [AD 2005-13-35](https://openairdocs.org/ad/2005-13-35): Flight idle stop · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Sep 26, 2005 - [AD 2005-13-38](https://openairdocs.org/ad/2005-13-38): Longitudinal skin joints in the fuselage pressure shell · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Aug 9, 2005 Historical (superseded or no longer in force): - [AD 2019-20-03](https://openairdocs.org/ad/2019-20-03) (historical): Information systems · Airbus A340-312, A340-313, A318-111 and 48 more. Effective Nov 19, 2019 - [AD 2014-06-08](https://openairdocs.org/ad/2014-06-08) (historical): Landing gear · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Apr 14, 2014 - [AD 2012-14-04](https://openairdocs.org/ad/2012-14-04) (historical): Landing gear · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Aug 27, 2012 - [AD 2006-12-16](https://openairdocs.org/ad/2006-12-16) (historical): Structural testing of the cockpit door · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Jul 18, 2006 - [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996 All 122: https://openairdocs.org/model/bombardier-dhc-8-202/ads.md ## Registered aircraft (14) - [N359PH](https://openairdocs.org/aircraft/N359PH): [Bighorn Airways Inc](https://openairdocs.org/faa-owner/BIGHORN%20AIRWAYS%20INC), [Sheridan, WY](https://openairdocs.org/faa-place/WY/Sheridan), built 1998, S/N 514 - [N360PH](https://openairdocs.org/aircraft/N360PH): [Umb Bank Na Trustee](https://openairdocs.org/faa-owner/UMB%20BANK%20NA%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 1998, S/N 515 - [N363PH](https://openairdocs.org/aircraft/N363PH): [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE), [Columbia, MD](https://openairdocs.org/faa-place/MD/Columbia), built 1998, S/N 520 - [N365PH](https://openairdocs.org/aircraft/N365PH): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 1998, S/N 526 - [N367PH](https://openairdocs.org/aircraft/N367PH): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 1998, S/N 511 - [N637CC](https://openairdocs.org/aircraft/N637CC): [Bank To Utah Trustee](https://openairdocs.org/faa-owner/BANK%20TO%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), S/N 637 - [N646CC](https://openairdocs.org/aircraft/N646CC): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2007, S/N 646 - [N649CC](https://openairdocs.org/aircraft/N649CC): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2007, S/N 649 - [N801MR](https://openairdocs.org/aircraft/N801MR): [US Department Of Homeland Security](https://openairdocs.org/faa-owner/US%20DEPARTMENT%20OF%20HOMELAND%20SECURITY), [Washington, DC](https://openairdocs.org/faa-place/DC/Washington), built 2004, S/N 606 - [N802MR](https://openairdocs.org/aircraft/N802MR): [Department Of Homeland Security](https://openairdocs.org/faa-owner/DEPARTMENT%20OF%20HOMELAND%20SECURITY), [Washington, DC](https://openairdocs.org/faa-place/DC/Washington), built 2005, S/N 612 - [N803MR](https://openairdocs.org/aircraft/N803MR): [Department Of Homeland Security](https://openairdocs.org/faa-owner/DEPARTMENT%20OF%20HOMELAND%20SECURITY), [Washington, DC](https://openairdocs.org/faa-place/DC/Washington), built 2006, S/N 626 - [N805MR](https://openairdocs.org/aircraft/N805MR): [US Department Of Homeland Security](https://openairdocs.org/faa-owner/US%20DEPARTMENT%20OF%20HOMELAND%20SECURITY), [Washington, DC](https://openairdocs.org/faa-place/DC/Washington), built 2008, S/N 655 - [N986HA](https://openairdocs.org/aircraft/N986HA): [645 Aeronautical Systems Group (Aesg)](https://openairdocs.org/faa-owner/645%20AERONAUTICAL%20SYSTEMS%20GROUP%20(AESG)), [Wpafb, OH](https://openairdocs.org/faa-place/OH/Wpafb), built 1996, S/N 421 - [N993BH](https://openairdocs.org/aircraft/N993BH): [Bighorn Airways Inc](https://openairdocs.org/faa-owner/BIGHORN%20AIRWAYS%20INC), [Sheridan, WY](https://openairdocs.org/faa-place/WY/Sheridan), built 1998, S/N 524 ## NTSB investigations (4) 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. - [NTSB ENG15IA024](https://openairdocs.org/ntsb/ENG15IA024), Jun 5, 2015: Bombardier DHC 8 (N363PH), Windsor Locks, CT, incident, minor damage. Probable cause: The arcing failure of the windshield heat power wire on the right windshield due to unknown reasons. Contributing to the severity of the fire was the lack of training or guidance provided to the crew… - [NTSB ERA09LA529](https://openairdocs.org/ntsb/ERA09LA529), Aug 29, 2009: Bombardier DHC-8-202 (N367PH), Sterling, VA, substantial damage. Probable cause: Undetermined. - [NTSB SEA05LA184](https://openairdocs.org/ntsb/SEA05LA184), Aug 29, 2005: Bombardier DHC-8-202 (N363PH), Portland, OR, substantial damage. Probable cause: The failure of the flightcrew of the other airplane to maintain clearance while taxiing. ## FAA accident and incident reports (28) 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 20170814017969I](https://openairdocs.org/incident/20170814017969I), Aug 14, 2017: Bombardier Inc DHC-8-202 (N359PH), Albany, NY, No damage. The pilot reported the aircraft took off and encountered the #2 engine unresponsive to power lever input and experienced torque fluctuations. This lead to the… - [Incident 20170517009699I](https://openairdocs.org/incident/20170517009699I), May 17, 2017: Bombardier Inc DHC-8-202 (N361PH), Latham, NY, Minor damage. On may 17th, 2017 at 13:45Z a commutair DHC-8-202 aircraft operating as united express flight 4915 from ewr to alb experienced a nose gear door unsafe… - [Incident 20161228023599I](https://openairdocs.org/incident/20161228023599I), Dec 28, 2016: Bombardier Inc DHC-8-202 (N379PH), Newark, NJ, No damage. Newark, NJ (ewr): N379PH, DH8, returned and landed on runway 4L after reporting a number 2 engine shutdown on 12/28/16 at 1921Z. The original event was… - [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 20160726011579I](https://openairdocs.org/incident/20160726011579I), Jul 26, 2016: Bombardier Inc DHC-8-202 (N362PH), Chantilly, VA, No damage. On July 26 2016 at approximately 1830 EST, a DHC-8-200, N362PH, united express flight 4979 operated by champlain enterprises LLC, d.b.a. commutair departed the… - [Incident 20160221001749I](https://openairdocs.org/incident/20160221001749I), Feb 21, 2016: Bombardier Inc DHC-8-202 (N367PH), Dulles, VA, No damage. On 02/21/2016, at approximately 13:20 EST, a commutair DHC-8-202 aircraft flying as united express flight 4944 experienced a left engine failure and associated… - [Incident 20160210001739I](https://openairdocs.org/incident/20160210001739I), Feb 10, 2016: Bombardier Inc DHC-8-202 (N367PH), Latham, NY, No damage. On 2/10/2016, at approximately 0855 EST, a commutair DHC-8-202 aircraft while flying as united express flight 4775, on departure from Albany international(alb)… - [Incident 20160129001729I](https://openairdocs.org/incident/20160129001729I), Jan 29, 2016: Bombardier Inc DHC-8-202 (N360PH), Newark, NJ, No damage. On 1/29/2016 at approximately 15:40 EST flight 5008 returned to ewr and landed on rwy 29 after reporting an engine oil pressure problem. Further investigation… - [Incident 20151202019179I](https://openairdocs.org/incident/20151202019179I), Dec 2, 2015: Bombardier Inc DHC-8-202 (N368PH), Pittsburgh, PA, No damage. On decemember 2, 2015 commutair flight 4772 departed Washington dulles intl airport at approximately 1312Z headed for fayitville, NC. Shortly after departure,… - [Incident 20150621007989I](https://openairdocs.org/incident/20150621007989I), Jun 21, 2015: Bombardier Inc DHC-8-202 (N363PH), Canandaigua, NY, No damage. Canandaigua airport, NY (D38):commutair flight 770, a DH8, diverted and landed on runway 31 due to a fire in the lavatory and smoke in the cockpit. The pilot… - [Incident 20150605008489I](https://openairdocs.org/incident/20150605008489I), Jun 5, 2015: Bombardier Inc DHC-8-202 (N363PH), Windsor Locks, CT, Minor damage. On June 5, 2015, about 1215 eastern daylight time (EDT), a Bombardier DHC-8-202 airplane, N363PH, had an in-flight cockpit fire during approach into Bradley… - [Incident 20150302001789I](https://openairdocs.org/incident/20150302001789I), Mar 2, 2015: Bombardier Inc DHC-8-202 (N360PH), Newark, NJ, No damage. At 500 feet AGL the #2 prop feathered automatically. The autofeather system was armed at the time of the incident. The f.o. reported that the #2 engine torque… - [Incident 20110310003429I](https://openairdocs.org/incident/20110310003429I), Mar 10, 2011: Bombardier DHC-8-202 (N359PH), Newark, NJ, No damage. During climb, the aircraft experienced a left wing down aileron trim tab runaway. Aircraft did not respond to right wing down selection. The crew performed the… - [Incident 20100919051549I](https://openairdocs.org/incident/20100919051549I), Sep 19, 2010: Bombardier DHC-8-202 (N369PH), Newark, NJ, Minor damage. Company statement alleges ground crew gave innacurate marshalling guidance and failed to visually clear both sides of aircraft during taxi in to gate. - [Incident 20081217855979I](https://openairdocs.org/incident/20081217855979I), Dec 17, 2008: Dhav DHC8202 (N362PH), Newark, NJ, Minor damage. (-23) At approximately 3:40 am on 12/17/08, N362PH, a DHC-8 operated by Continental connection was struck in the left hand elevator by a de-ice truck boom… - [Incident 20080918850919I](https://openairdocs.org/incident/20080918850919I), Sep 18, 2008: Dhav DHC8202 (N363PH), IN, No damage. (-23) An air carrier aircraft on an IFR flight plan at 14,000 feet MSL responded to a terminal collision advisory system (TCAS) resolution advisory (ra)… - [Incident 20060128000939I](https://openairdocs.org/incident/20060128000939I), Jan 28, 2006: Dhav DHC8202 (N368PH), Seattle, WA. (-23) At approx 1830 LCL, horizon flt 223 enroute from yvr to pdx encountered reduced cabin pressure causing thru FL 180 approx 50NM from sea. Crew made an… - [Accident 20050829019919A](https://openairdocs.org/incident/20050829019919A), Aug 29, 2005: Dhav DHC8202 (N363PH), Portland, OR, Substantial damage. (-23) While taxiing for takeoff NWA5 struck HORIZON66. The impact resulted in substantial damage to the horizon DHC-8 aircraft. Horizon 66 was holding short of… - [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 20021119033789I](https://openairdocs.org/incident/20021119033789I), Nov 19, 2002: Dhav DHC8202 (N367PH), Portland, OR. (-23) Horizon air flight 2056 rdm to sea diverted to Portland or. When they experienced smoke in cabin and cockpit. Maintenance at Portland or. Ran both… - [Incident 20020312004279I](https://openairdocs.org/incident/20020312004279I), Mar 12, 2002: Dhav DHC8202 (N361PH), Portland, OR. (-23) During taxi #2 engine fire warning system activated. Flight crew performed engine fire checklist and called for CFR. Engine fire warning ceased at… - [Incident 20020107002819I](https://openairdocs.org/incident/20020107002819I), Jan 7, 2002: Dhav DHC8202 (N367PH), Seattle, WA. (-23) On flight 2331 from lewiston Idaho to Seattle Washington crew noted noise and vibration on approach to seatac. On postflight inspection crew noted that… - [Incident 20011106031219I](https://openairdocs.org/incident/20011106031219I), Nov 6, 2001: Dhav DHC8202 (N374PH), Arcata - Eureka, CA, Minor damage. (-23) On takeoff the aircraft struck a deer. - [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… - [Incident 20010129000859I](https://openairdocs.org/incident/20010129000859I), Jan 29, 2001: Dhav DHC8202 (N363PH), Seattle, WA, Minor damage. (-23) Noise heard at rotation, notified enroute by yakima (ykm) tower metal had separated from aircraft (a/c). On descent in Seattle/Tacoma (sea) second noise… - [Incident 20001227030649I](https://openairdocs.org/incident/20001227030649I), Dec 27, 2000: Dhav DHC8201 (N986HA), Pittsburgh, PA. (-23) On 12/27/00 at 15:27E, while on approach to Pittsburgh international airport, piedmont airlines flight 3403 reported a landing gear problem (piedmont may… - [Incident 20000223016089I](https://openairdocs.org/incident/20000223016089I), Feb 23, 2000: Dhav DHC8202 (N363PH), Redding, CA. (-23)Enroute @ flight level 210 elevator trim frozen. Trim was operable after landing. Maintenance lubed both screw jack assemblies. - [Incident 20000209019549I](https://openairdocs.org/incident/20000209019549I), Feb 9, 2000: Dhav DHC8202 (N359PH), Seattle, WA. (-23)Aileron trim was observed by the crew to be moving left without any crew input. Crew pulled circuit beaker and continued the flight without further… ## Service difficulty reports (8,233, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR BIGA20260824001](https://openairdocs.org/sdr/BIGA20260824001), Aug 24, 2026: AIR DUCT. DETACHED. AIRCRAFT WAS ENROUTE TO RESPOND TO A FIRE MISSION. WHILE ENROUTE THE SMOKE-JUMPER CREW SAW WHAT APPEARED TO BE SMOKE COMING FROM RIGHT AFT CABIN FLOORBOARDS. TH - [SDR 2023FA0000702](https://openairdocs.org/sdr/2023FA0000702), Oct 5, 2023: ENGINE. POWER LOSS. 10/5/2023 AT AROUND 4:25 PM CST, D8-200 N805MR WAS DEPARTING MIAMI EXECUTIVE AIRPORT. AIRCRAFT WAS SET UP FOR CRUISE CLIMB WITH AUTOPILOT ENGAGED. PROP RPM 1064 - [SDR 2022FA0000214](https://openairdocs.org/sdr/2022FA0000214), Apr 15, 2022: NONE. NONE. UNDETECTED, STANDING FUEL IN A WING DRY BAY WITH A BLEED AIR TUBE HAS PROMPTED THIS REPORT. THE AIRCRAFT HAS BEEN MODIFIED WITH STC ST03382NY, WHICH CONVERTS A - [SDR HKGA20220314004](https://openairdocs.org/sdr/HKGA20220314004), Mar 13, 2022: SPACER. CRACKED. BLEED SYSTEM PRSOV SPACE MOUNTING EARS FOUND CRACKED. REMOVED SPACER, REPLACED CRACKED ANGLES P/N 85531139-101 & 85531139-105. RE-INSTALLED REPAIRED SPACER. - [SDR HKGA20220314003](https://openairdocs.org/sdr/HKGA20220314003), Mar 13, 2022: SPACER. CRACKED. BLEED SYSTEM PRSOV SPACE MOUNTING EARS FOUND CRACKED. REMOVED SPACER, REPLACED CRACKED ANGLES P/N 85531139-101 & 85531139-105. RE-INSTALLED REPAIRED SPACER. - [SDR HKGA20220314002](https://openairdocs.org/sdr/HKGA20220314002), Mar 13, 2022: SPACER. CRACKED. BLEED SYSTEM PRSOV SPACE MOUNTING EARS FOUND CRACKED. REMOVED SPACER, REPLACED CRACKED ANGLES P/N 85531139-101 & 85531139-105. RE-INSTALLED REPAIRED SPACER. - [SDR HKGA20190821742](https://openairdocs.org/sdr/HKGA20190821742), Aug 16, 2019: TRIM TAB. CRACKED. RH ELEVATOR SPRING TAB CRACKED @ TRAILING EDGE. REMOVED AND REPLACED RH ELEVATOR SPRING TAB IAW DHC-8 MM 27-34-11. - [SDR HKGA201908217041](https://openairdocs.org/sdr/HKGA201908217041), Aug 16, 2019: TRIM TAB. DAMAGED. DURING INSPECTION IT WAS FOUND THAT THE LH ELEVATOR SPRING TAB HAS A BULLET HOLE @ TRAILING EDGE. REMOVED AND REPLACED LH ELEVATOR SPRING TAB IAW DHC-8 MM 27-34 - [SDR CA190628008](https://openairdocs.org/sdr/CA190628008), Jun 21, 2019: SWITCH. BROKEN. (CAN) WE HAD AN ENGINE IFSD ON MSN 522 DUE TO THE RH ENGINE SURGE BETWEEN 80% AND 120% ON FRIDAY 21/JUNE/19. PRECAUTION ENGINE SHUT DOWN WAS PERFORMED AND THE A - [SDR CA190605008](https://openairdocs.org/sdr/CA190605008), May 30, 2019: ELEVATOR SYSTEM. MALFUNCTIONED. (CAN) WHEN THE CREW ROTATED THE AIRCRAFT, THERE WERE NO RESPONSE TO PITCH CONTROL INPUT AND THE CREW ELECTED TO EXECUTE A REJECTED TAKEOFF. THE AIRCRAFT IS CONF - [SDR CA190507007](https://openairdocs.org/sdr/CA190507007), May 2, 2019: TAB. DENTED. (CAN) DURING TAXI, WHILE PREFORMING THE BEFORE TAKEOFF CHECKS PRIOR TO FLIGHT, THE CREW REPORTED THE PITCH CONTROL WAS JAMMED AND THE FLIGHT WAS CANCELLED. AFTE - [SDR CA190503014](https://openairdocs.org/sdr/CA190503014), Apr 30, 2019: CHECK VALVE. CRACKED. (CAN) DIVERSION CARRIED OUT DUE TO #2 HYDRAULIC FLUID LOSS. MAINTENANCE REPLACED BROKEN HYDRAULIC CHECK VALVE P/N: 3-1582-2-3 LOCATED IN THE TAIL SECTION AND RE - [SDR CA190415014](https://openairdocs.org/sdr/CA190415014), Apr 15, 2019: STARTER GEN. MALFUNCTIONED. (CAN) UNIT SLOW TO START. LH STARTER GENERATOR VENT HAD INDICATIONS OF SMOKE OR OIL ON COWL. FOUND DRIVE SHAFT LOOSE AND UNIT WAS MAKING SMOKE. TEAR DOWN REPORT - [SDR CA190411016](https://openairdocs.org/sdr/CA190411016), Apr 10, 2019: BOLT. LOOSE. (CAN) DURING PILOT PRE TAKE OFF FLIGHT CONTROL CHECK, WITH CONTROL LOCK DISENGAGED, ELEVATOR MOVEMENT RESTRICTED, UNABLE TO MOVE AFT OF NEUTRAL POSITION. AIRCRA - [SDR A8ZR20181113003](https://openairdocs.org/sdr/A8ZR20181113003), Nov 12, 2018: FIREWALL. CRACKED. ACCOMPLISHED DOUBLER INSTALLATION FOR CRACK ON UPPER FIREWALL WEB PN 85410554 OF #1 NACELLE RH IB SIDE AT XN 127.00 REF BOMBARDIER DEHAVILLAND RD 8-54-1565 ISSU - [SDR A8ZR20181113002](https://openairdocs.org/sdr/A8ZR20181113002), Nov 12, 2018: STRUCTURE. CRACKED. ACCOMPLISHED REPLACEMENT OF CRACKED CLOSING MEMBER PN 85410449 OF NR 1 NACELLE RT IB SIDE FIREWALL REF RD 8-54-611 ISSUE 4 DTD 12 APR, 2001. - [SDR A8ZR20181113001](https://openairdocs.org/sdr/A8ZR20181113001), Nov 12, 2018: FIREWALL. CRACKED. ACCOMPLISHED DOUBLER INSTALLATION FOR CRACK ON UPPER FIREWALL WEB PN 85410554 OF NO 1 NACELLE RT IB SIDE REF RD 8-54-3940 ISSUE 1 DTD 24 MAY, 2017. - [SDR A8ZR20181106001](https://openairdocs.org/sdr/A8ZR20181106001), Nov 5, 2018: FIREWALL. CRACKED. ACCOMPLISHED DOUBLER INSTALLATION FOR CRACK ON UPPER FIREWALL WEB PN 85410554 OF NR 2 NACELLE RT OB SIDE REF RD 8-54-3940 ISSUE 1 DTD 24 MAY, 2017. - [SDR A8ZR20181106002](https://openairdocs.org/sdr/A8ZR20181106002), Nov 5, 2018: STRUCTURE. CRACKED. ACCOMPLISHED REPLACEMENT OF CRACKED CLOSING MEMBER PN 85410449 OF NR 2 NACELLE RT OB SIDE FIREWALL REF RD 8-54-611 ISSUE 4 DTD 12 APR, 2001. - [SDR 2018FA0000393](https://openairdocs.org/sdr/2018FA0000393), Sep 20, 2018: HYDRAULIC LINE. LEAKING. DURING CLIMB IN VVI-SRE LEG, THE AIRCRAFT SUFFERED TOTAL LOOS OF SYSTEM NR.2 HYDRAULIC FLUID, QRF TO DEPARTURE STATION. CORRECTIVE ACTION: HYDRAULIC FLUID LOOS - [SDR 2019F00058](https://openairdocs.org/sdr/2019F00058), Aug 12, 2018: SIGNAL COND UNIT. FAILED. PROPELLER OVERSPEED INDICATION ENG#1. AIRCRAFT TURN BACK TO AIRPORT AFTER SHUTTING DOWN AFFECTED ENGINE ACCORDING TO PROCEDURE. CORRECTIVE ACTION: SIGNAL CONDIT - [SDR A8ZR20180817001](https://openairdocs.org/sdr/A8ZR20180817001), Aug 11, 2018: SKIN. DENTED. DENT FOUND AT BS331, STRINGER 31L. REFORMED THE DENT AND CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 42-2018-061, REV. A. - [SDR A8ZR20180921001](https://openairdocs.org/sdr/A8ZR20180921001), Aug 10, 2018: LIGHT. DEFECTIVE. RT FWD EMERGENCY EXIT DOOR, LT & RT UNDER WING EMERGENCY EXIT DOOR BETA LIGHTS P/N 1971001 FAILED BRIGHTNESS CHECK REF TASK CARD 3350/02 AND REPLACED REF AMM 33 - [SDR A8ZR201809121005](https://openairdocs.org/sdr/A8ZR201809121005), Jul 19, 2018: SKIN. GOUGED. ACCOMPLISHED RE-SKIN ON AFT BAGGAGE DOOR UPPER SECTION THAT MEASURES 5.7" X 49.70" FOR GOUGES IN SKIN REF RD 8-52-029 ISSUE 2 DATED 2014-06-05. - [SDR A8ZR20180924003](https://openairdocs.org/sdr/A8ZR20180924003), Jul 18, 2018: LIGHT. DEFECTIVE. RT FWD EMERGENCY EXIT DOOR, LT & RT UNDER WING EMERGENCY EXIT DOOR BETA LIGHTS P/N 1971001 FAILED BRIGHTNESS CHECK REF TASK CARD 3350/02 AND REPLACED REF AMM 33 - [SDR A8ZR20180924002](https://openairdocs.org/sdr/A8ZR20180924002), Jul 18, 2018: LIGHT. DEFECTIVE. RT FWD EMERGENCY EXIT DOOR, LT & RT UNDER WING EMERGENCY EXIT DOOR BETA LIGHTS P/N DSC543-1 FAILED BRIGHTNESS CHECK REF TASK CARD 3350/02 AND REPLACED REF AMM 3 - [SDR A8ZR20180921003](https://openairdocs.org/sdr/A8ZR20180921003), Jul 17, 2018: LIGHT. DEFECTIVE. RT FWD EMERGENCY EXIT DOOR, LT & RT UNDER WING EMERGENCY EXIT DOOR BETA LIGHTS P/N 1971001 FAILED BRIGHTNESS CHECK REF TASK CARD 3350/02 AND REPLACED REF AMM 33 - [SDR A8ZR20180921002](https://openairdocs.org/sdr/A8ZR20180921002), Jul 12, 2018: LIGHT. DEFECTIVE. RT FWD EMERGENCY EXIT DOOR, LT & RT UNDER WING EMERGENCY EXIT DOOR BETA LIGHTS P/N 1971001 FAILED BRIGHTNESS CHECK REF TASK CARD 3350/02 AND REPLACED REF AMM 33 - [SDR A8ZR20180920001](https://openairdocs.org/sdr/A8ZR20180920001), Jul 10, 2018: LIGHT. DEFECTIVE. RT FWD EMERGENCY EXIT DOOR, LT & RT UNDER WING EMERGENCY EXIT DOOR BETA LIGHTS P/N 1971001 FAILED BRIGHTNESS CHECK REF TASK CARD 3350/02 AND REPLACED REF AMM 33 - [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 A8ZR20180911002](https://openairdocs.org/sdr/A8ZR20180911002), Jul 2, 2018: STRUCTURE. DENTED. ACCOMPLISHED DOUBLER REPAIR AT STA 315.80 & BETWEEN S30S AND S31S FOR DENT WITH CREASE REF EA 45-2018-080 REV ORIGINAL ISSUE DATED 06/20/2018. - [SDR A8ZR20180823007](https://openairdocs.org/sdr/A8ZR20180823007), Jun 27, 2018: STRIKER. OUT OF LIMITS. ACCOMPLISHED RE-CONTOUR OF NR 2 ENGINE I/B COWL DOOR NACELLE STRIP-STRIKER FOR THE UPPER EDGE OF THE DOOR IAW EA 43-2018-083, REV A. - [SDR A8ZR20180911004](https://openairdocs.org/sdr/A8ZR20180911004), Jun 20, 2018: STRUCTURE. DENTED. ACCOMPLISHED DOUBLER REPAIR AT STA 213.8 & BETWEEN S16S AND S17S FOR DENT REF EA 48-2018-042 REV ORIGINAL ISSUE DATED 06/20/2018. - [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 A8ZR20180924001](https://openairdocs.org/sdr/A8ZR20180924001), Jun 11, 2018: LIGHT. DEFECTIVE. RT FWD EMERGENCY EXIT DOOR, LT & RT UNDER WING EMERGENCY EXIT DOOR BETA LIGHTS P/N DSC543-1 FAILED BRIGHTNESS CHECK REF TASK CARD 3350/02 AND REPLACED REF AMM 3 - [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 A8ZR20180911001](https://openairdocs.org/sdr/A8ZR20180911001), Jun 6, 2018: TAIL CONE. DELAMINATED. ACCOMPLISHED COMPOSITE REPAIR ON LWR TAILCONE FWD AT TAIL BUMPER FOR DELAMINATION STA X806 & Z130.43 REF SRM 53-70-28 REV 6 DATED SEP 17, 2017. - [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 2018FA0000170](https://openairdocs.org/sdr/2018FA0000170), May 30, 2018: GENERATOR. FAILED. NR 1 GENERATOR FAILURE, CYCLING ON AND OFF. CAUSED MULTIPLE SYSTEM FAILURES, TO INCLUDE AUTO PRESSURIZATION SYSTEM FAILURE. THE NR 1 DC GENERATOR LIGHT ILLUMINA - [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 JJBA2018061910007](https://openairdocs.org/sdr/JJBA2018061910007), May 10, 2018: WIRE. OUT OF POSITION. LEFT EMERGENCY EXIT FORWARD EMERGENCY LIGHT WAS UNSERVICEABLE. TROUBLESHOT AND FOUND WIRES IN CONNECTORS J12 ON SIDEWALL PANEL SWAPPED. SWAPPED WIRES BACK. OPS - [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 A8ZR20180821002](https://openairdocs.org/sdr/A8ZR20180821002), May 7, 2018: SKIN. DENTED. DENT ON FUSELAGE AT STA 328.5 & S13P+6" THAT MEASURES .50"L X .9"W X .006"D SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR WITH NO OFFSETS TO MATERIAL THICKNESS. CON All 8,233: https://openairdocs.org/model/bombardier-dhc-8-202/reports.md ## STCs that may be installed (OpenAirDocs) (143, first 50) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [STC ST00153IB](https://openairdocs.org/stc/ST00153IB): Installation of Static Line Provisions. Voyageur Aviation Corp - [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center - [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc - [STC ST04328NY](https://openairdocs.org/stc/ST04328NY): The Manufacture and Installation of Exterior Placards, Labels and Signs is to be performed, installed. Libellule Monde Inc - [STC ST03875NY](https://openairdocs.org/stc/ST03875NY): Installation of interior placards, signs and markings. Libellule Monde Inc - [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF - [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc - [STC ST03472NY](https://openairdocs.org/stc/ST03472NY): Installation of the Cabin LED Lighting. Avmax Aviation Services Inc - [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc - [STC ST01255SE](https://openairdocs.org/stc/ST01255SE): Installation of a center console extended fairing. Metal Innovations Inc. dba MII Aero - [STC ST02050NY](https://openairdocs.org/stc/ST02050NY): Installation of U.S. Customs Special Mission Modifications. Field Aviation East Limited - [STC ST03795NY](https://openairdocs.org/stc/ST03795NY): Installation of the TB44 Lithium-Ion Battery System. Avmax Aviation Services Inc - [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH - [STC ST01909NY](https://openairdocs.org/stc/ST01909NY): Installation of Hawker 9750W0370-6 (24V 43Ah) sealed lead-acid batteries. Securaplane Technologies Inc - [STC ST02028WI](https://openairdocs.org/stc/ST02028WI): Installation of Bighorn CASEVAC Interior System. Bighorn Airways Inc - [STC ST03065NY](https://openairdocs.org/stc/ST03065NY): The installation of Dual Universal UNS-1F Flight Management System WAAS Up-grade. Field Aviation East Limited - [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH - [STC ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC - [STC ST02311AT](https://openairdocs.org/stc/ST02311AT): Installation of Saf-T-Glo Inc photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc - [STC ST00213MC](https://openairdocs.org/stc/ST00213MC): Installation of means to disable ADS-B Out. Sierra Nevada Corporation - [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH - [STC ST00109IB](https://openairdocs.org/stc/ST00109IB): Installation of the Flight Compartment Stowage Box. Infinion Certification Engineering Inc - [STC ST04788NY](https://openairdocs.org/stc/ST04788NY): Installation of the Terrain Awareness and Warning System. Mid Canada Mod Center - [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited - [STC ST00089IB](https://openairdocs.org/stc/ST00089IB): Installation of SNC Mission Systems. Field Aviation East Limited - [STC ST03354NY](https://openairdocs.org/stc/ST03354NY): Installation of the Dual Auxiliary Air Condintioning system. Field Aviation Company Inc - [STC ST04783NY](https://openairdocs.org/stc/ST04783NY): Installation of the provisions for the Mark II Laser Airborne Depth Sounder (LADS) in the Standard Passenger Carrying Configuration. Field Aviation East Limited - [STC ST00886NY](https://openairdocs.org/stc/ST00886NY): Installation of Flight Deck Manual Stowage Box, in accordance with Aero Consulting Services Modification Data Summary Number B78600, Revision H, dated November 9, 2006, or later TCCA approved revision. B/E Aerospace Limited - [STC ST00428NY](https://openairdocs.org/stc/ST00428NY): Installation of a Sundstrand Turbomach T-62T-40C7B gas turbine auxiliary power unit with a Lear Siegler Model 23088-002 DC starter-generator. Avmax Aviation Services Inc - [STC ST01689WI](https://openairdocs.org/stc/ST01689WI): Installation of Crane Aerospace & Electronics SmartStem Wireless Tire Pressure Sensing System. ELDEC Corporation - [STC SA1220NW](https://openairdocs.org/stc/SA1220NW): Installation of Universal flight data recorder. Honeywell International Inc - [STC ST04667NY](https://openairdocs.org/stc/ST04667NY): Installation of the Honeywell MK VIII Enhanced Ground Proximity Warning System (EGPWS) Override Control. Field Aviation East Limited - [STC ST04652NY](https://openairdocs.org/stc/ST04652NY): Installation of the ACSS TCAS 7.1. Avmax Aviation Services Inc - [STC ST02722SE](https://openairdocs.org/stc/ST02722SE): Installation of LT-4098 series Integrated LED Display Panel and/or associated LT-2201 series LED Pushbutton Switches. Luma Technologies LLC - [STC ST03261NY](https://openairdocs.org/stc/ST03261NY): Installation of Dual Universal UNS-1E Flight Management System WAAS Up-grade. Field Aviation East Limited - [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc - [STC ST02448SE](https://openairdocs.org/stc/ST02448SE): Installation of a Supplemental Lighting System. Aviation Specialties Unlimited Inc - [STC ST00782LA](https://openairdocs.org/stc/ST00782LA): Installation of Chadwick Helmuth Propeller Balance Monitoring System (Vibration Management System II, VMS II). Diagnostic Solution International LLC - [STC ST01226NY](https://openairdocs.org/stc/ST01226NY): Installation of Environmental Control System Performance Improvement Modification. Cascade Aerospace Inc - [STC ST10977SC](https://openairdocs.org/stc/ST10977SC): Installation of Dual Universal Avionics Flight Management Systems (FMS) with Global Positioning System (GPS). DAC International Inc - [STC ST04480NY](https://openairdocs.org/stc/ST04480NY): Installation of the Traffic Collision Avoidance System (TCAS) II Version 7.1 and Elementary Surveillance (ELS) Transponder Upgrade. Genesys Certification Services Inc - [STC ST02729NY](https://openairdocs.org/stc/ST02729NY): Sky Connect Tracking System to be installed. Honeywell International Inc - [STC ST04445NY](https://openairdocs.org/stc/ST04445NY): Installation of the Collins TDR-94D Transponder / Traffic Collision Avoidance System (TCAS) 4100 Upgrade. Mid Canada Mod Center - [STC ST02635LA](https://openairdocs.org/stc/ST02635LA): Modification to replace the existing Mode S Transponder system with the ACSS NXT-600 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit. Med-Pac Inc - [STC ST04372NY](https://openairdocs.org/stc/ST04372NY): Installation of saf-Tglo® SSUL23 Photoluminescent Aisle Path Marking System. STG Aerospace Ltd - [STC ST01900WI](https://openairdocs.org/stc/ST01900WI): Heated (LH) Side Canopy Window Assembly replacement installation. Lee Aerospace Inc - [STC ST04344NY](https://openairdocs.org/stc/ST04344NY): Installation of the Universal Avionics EFI-890R MFD. Avmax Aviation Services Inc - [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS - [STC ST04324NY](https://openairdocs.org/stc/ST04324NY): Installation of the Honeywell Solid State Cockpit Voice Recorder (SSVR) system. Avmax Aviation Services Inc All 143: https://openairdocs.org/model/bombardier-dhc-8-202/stcs.md ## PMA parts (OpenAirDocs) (470, first 50) Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first. - [AF300P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149363258220260717175325.0001): Repair Kit. AkroFire, Inc. · PMA PQ3730CE · Modification part · May 11, 2026 - [MDL DOC-SNC-000385739](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169490213520240801144256.0001): ADS-B Disable. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · May 21, 2024 - [MDL DOC-SNC-000375576](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117578205620240801144258.0001): BLOS X-Band Antenna. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · May 21, 2024 - [MDL 0208-0200-2014](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104565969920240801144257.0001): Mission Systems. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · May 21, 2024 - [MDL-0208-00-9307](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173729114220240308150028.0001): Mission Communication Equipment and Mission Interior Modifications. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Jan 22, 2024 - [MDL-0208-00-9307](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126394400520240123183202.0001): Mission Communication Equipment and Mission Interior Modifications. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Dec 20, 2023 - [SG8504](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199133518520231026161527.0001): Coloured Insert (14.5mm). STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8504 · Oct 24, 2023 - [SG9901](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194884506120231026161816.0001): SuperSeal Stop End. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG9901 · Oct 24, 2023 - [SG8857](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191393429420231026161651.0001): Track SSUL Overcarpet 1.5-3mm. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8857 · Oct 24, 2023 - [SG8607](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189031167420231026161603.0001): Self-adhesive Insert Marker Chevron (White). STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8607 · Oct 24, 2023 - [SG8859](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184796275020231026161701.0001): Track Overcarpet SSL 6.5-10.5mm. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8859 · Oct 24, 2023 - [SG8502](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180885316920231026161516.0001): SuperSeal Lite Angled Stop End. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8502 · Oct 24, 2023 - [SG9954](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179992042920231026161843.0001): Self-Adhesive Insert Marker Chevron. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG9954 · Oct 24, 2023 - [SG9422](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179571282220231026161802.0001): Photoluminescent Insert. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG9422 · Oct 24, 2023 - [SG9905](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177843013220231026161830.0001): Angled Stop End, 21 - 30 Degrees. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG9905 · Oct 24, 2023 - [SG8851](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169830943520231026161637.0001): Track Sleeve SSUL Coated. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8851 · Oct 24, 2023 - [SG8930](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168678075220231026161752.0001): Double Dot Marker, White. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8930 · Oct 24, 2023 - [SG8898](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168351533820231026161705.0001): Track SSL Overcarpet 1.5-6mm. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8898 · Oct 24, 2023 - [SG8503](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167822328120231026161521.0001): Photoluminescent Insert. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8503 · Oct 24, 2023 - [SG8695](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167511670920231026161616.0001): End Cap, SuperSeal (36º-45º). STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8695 · Oct 24, 2023 - [SG8513](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164962464220231026161546.0001): SuperSeal Lite Angled Stop End. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8513 · Oct 24, 2023 - [SG8512](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163904003620231026161541.0001): SuperSeal Lite Angled Stop End. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8512 · Oct 24, 2023 - [SG8844](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157098224120231026161623.0001): SuperSeal Lite Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8844 · Oct 24, 2023 - [SG8519](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID153166689820231026161551.0001): SuperSeal Lite Chevron Marker Insert. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8519 · Oct 24, 2023 - [SG8908](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152257428720231026161710.0001): White Narrow Double Dot Marker Insert. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8908 · Oct 24, 2023 - [SG8642](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID150433317520231026161609.0001): SSL Galley Photoluminescent Insert. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8642 · Oct 24, 2023 - [SG8845](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143008711120231026161630.0001): SuperSeal Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8845 · Oct 24, 2023 - [SG8501](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID138984158920231026161508.0001): SuperSeal Stop End. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8501 · Oct 24, 2023 - [SG8500](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID138270494020231026161459.0001): SuperSeal Lite Track Sleeve. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8500 · Oct 24, 2023 - [SG8854](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137261187020231026161644.0001): Assembly: SuperSeal UltraLite. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8854 · Oct 24, 2023 - [SG9903](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133364886120231026161823.0001): Angled Stop End, 8 - 20 Degrees. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG9903 · Oct 24, 2023 - [SG8925](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127195871320231026161727.0001): PL Insert, Blue Emitting. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8925 · Oct 24, 2023 - [SG8858](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119203010320231026161656.0001): Track Overcarpet SSUL 3-5mm. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8858 · Oct 24, 2023 - [SG9900](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119121999220231026161809.0001): Track SS Coated. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG9900 · Oct 24, 2023 - [SG9999](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117856411520231026161849.0001): Coloured Insert (30.8mm). STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG9999 · Oct 24, 2023 - [SG8924](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115557720220231026161720.0001): Assembly: SuperSeal UltraLite (Blue Emitting). STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8924 · Oct 24, 2023 - [SG9952](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103662445320231026161837.0001): Self-Adhesive Insert Marker Double Dot. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG9952 · Oct 24, 2023 - [SG8505](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102826196620231026161534.0001): SuperSeal Lite Double Dot Marker Insert. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8505 · Oct 24, 2023 - [SG8606](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID100126661520231026161557.0001): SuperSeal Lite Chevron Marker Insert (White). STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8606 · Oct 24, 2023 - [130522-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173562032620230727204633.0001): Cabin Press Control. Honeywell International Inc. · PMA PQ1222NM · Replaces 130522-1 · Apr 20, 2023 - [131410-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157829435520230727204634.0001): Ejector. Honeywell International Inc. · PMA PQ1222NM · Replaces 131410-1 · Apr 20, 2023 - [130522-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140647336720230727204635.0001): Cabin Press Control. Honeywell International Inc. · PMA PQ1222NM · Replaces 130522-2 · Apr 20, 2023 - [2117804-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136861475320230727204632.0001): Computer. Honeywell International Inc. · PMA PQ1222NM · Replaces 2117804-1 · Apr 20, 2023 - [147240-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135081847020230727204636.0001): Air Filter. Honeywell International Inc. · PMA PQ1222NM · Replaces 147240-1 · Apr 20, 2023 - [103672-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125135353220230727204631.0001): Outflow Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 103672-2 · Apr 20, 2023 - [28B262-77A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130029158120231227185351.0001): APU Generator. Honeywell International Inc. · PMA PQ1222NM · Replaces 28B262-77A · Jan 7, 2023 - [103068-14](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137751795520230731171143.0001): Outflow Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 103068-14 · Jul 26, 2022 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165382423920220809130847.0001): Aviation Devices & Electronic Components LLC (Av-DEC) · PMA PQ3846SW · May 10, 2022 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102960505620220809102522.0001): Aviation Devices & Electronic Components LLC (Av-DEC) · PMA PQ3846SW · Apr 18, 2022 - [AG844000-15](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157157650520220408135740.0001): Gasket – UHF/VHF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Feb 8, 2022 All of them: https://openairdocs.org/model/bombardier-dhc-8-202/pma.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Dehavilland DHC-8-202](https://openairdocs.org/model/dehavilland-dhc-8-202): 17 registered aircraft, registry code 2809007 --- 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.