# Boeing DHC-8-102 - Type: Aircraft model (FAA registry) - Registry code: 1386002 - Manufacturer (registry): BOEING - Model: DHC-8-102 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-prop - Seats: 39 - 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: 3 - Page: https://openairdocs.org/model/boeing-dhc-8-102 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 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 2013-16-12](https://openairdocs.org/ad/2013-16-12): Nacelles/pylons · Bombardier DHC-8-102, DHC-8-103 and DHC-8-106. Effective Sep 24, 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 2012-05-07](https://openairdocs.org/ad/2012-05-07): Engine Controls · Bombardier DHC-8-102, DHC-8-103 and DHC-8-106. Effective Apr 4, 2012 - [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 2010-05-12](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 - [AD 2005-11-10](https://openairdocs.org/ad/2005-11-10): Brake shuttle valves · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Jul 12, 2005 Historical (superseded or no longer in force): - [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 163: https://openairdocs.org/model/boeing-dhc-8-102/ads.md ## Registered aircraft (3) - [N807EX](https://openairdocs.org/aircraft/N807EX): [Frontera Flight Holdings Inc](https://openairdocs.org/faa-owner/FRONTERA%20FLIGHT%20HOLDINGS%20INC), [Dover, DE](https://openairdocs.org/faa-place/DE/Dover), built 1991, S/N 292 - [N837EX](https://openairdocs.org/aircraft/N837EX): [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), S/N 217 - [N839EX](https://openairdocs.org/aircraft/N839EX): [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 1990, S/N 226 ## NTSB investigations (9) 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 DCA14CA031](https://openairdocs.org/ntsb/DCA14CA031), Nov 25, 2013: De Havilland DHC8 - 102 (N808EX), Philadelphia, PA, substantial damage. Probable cause: an inadvertent encounter with several birds during approach that resulted in substantial damage to the airplane. - [NTSB DCA13FA094](https://openairdocs.org/ntsb/DCA13FA094), May 18, 2013: Bombardier DHC8 (N934HA), Newark, NJ, substantial damage. Probable cause: the frozen left main landing gear (MLG) uplock roller due to lack of lubrication and the uplock latch that had worn beyond acceptable tolerances, which prevented the flight crew from extending the… - [NTSB ERA12LA147](https://openairdocs.org/ntsb/ERA12LA147), Jan 16, 2012: Boeing DHC-8-102 (N839EX), Huntington, WV, substantial damage. Probable cause: The inadequate communication among ground crew personnel, which resulted in the airplane’s collision with a deice truck. - [NTSB SEA01IA161](https://openairdocs.org/ntsb/SEA01IA161), Aug 28, 2001: de Havilland DHC-8-102 (N827PH), Portland, OR, incident, no damage. Probable cause: Improper tension of the right control yoke chain; a worn right aileron spring tab hinge bearing; improper tension of the left aileron spring tab aft spring and worn contact stud; improper tension of… - [NTSB IAD00IA026](https://openairdocs.org/ntsb/IAD00IA026), Mar 12, 2000: Boeing - Canada DHC-8-102 (N838EX), Baltimore, MD, incident, minor damage. Probable cause: the missing elevator stop bumper that resulted in elevator over-travel and damage to the elevator. A factor in the incident was the abrupt release of the elevator control lock in windy conditions. - [NTSB NYC00LA007](https://openairdocs.org/ntsb/NYC00LA007), Oct 7, 1999: Boeing - Canada DHC-8-102 (N818EX), Philadelphia, PA, substantial damage. Probable cause: An in flight collision with birds. - [NTSB SEA97LA077](https://openairdocs.org/ntsb/SEA97LA077), Mar 26, 1997: de Havilland DHC-8 (N826PH), Wenatchee, WA, substantial damage. Probable cause: failure of the ground marshaller to marshal the airplane into a correct parking place on the ramp, her failure to verify clearance between the right wing of the airplane and the ground de-ice cart,… - [NTSB ATL94IA048](https://openairdocs.org/ntsb/ATL94IA048), Feb 11, 1994: Boeing DHC-8-102 (N882CC), Charlotte, NC, incident, no damage. Probable cause: AN INFLIGHT ENCOUNTER WITH TURBULENCE, AND THE FLIGHT ATTENDANT'S FAILURE TO FASTEN HER SEATBELT. - [NTSB MIA93LA090](https://openairdocs.org/ntsb/MIA93LA090), Mar 23, 1993: de Havilland DHC-8-102 (N928HA), Jacksonville, FL, no damage. Probable cause: THE OPERATOR'S LACK OF ADEQUATE INSTRUCTIONS TO CREWMEMBERS AS TO WHEN FLIGHT ATTENDANTS CAN RESUME CABIN DUTIES AFTER BEING TOLD TO BE SEATED BY THE CAPTAIN. ## FAA accident and incident reports (100, newest 50) 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 20141112020569I](https://openairdocs.org/incident/20141112020569I), Nov 12, 2014: Boeing DHC-8-102 (N806EX), Charlotte, NC, Minor damage. On pushback aircraft struck a catering truck. The aircraft sustained damage to the bottom of the rudder, tailcone,and rear navigation light. The rudder was… - [Accident 20131124024339A](https://openairdocs.org/incident/20131124024339A), Nov 24, 2013: Bombardier, DHC-8-102 (N808EX), Philadelphia, PA, Substantial damage. On November 24, 2013 aircraft N808EX piedmont airlines flight #4314 encountered several bird strikes on approach five miles east of the Philadelphia… - [Accident 20130518008759A](https://openairdocs.org/incident/20130518008759A), May 18, 2013: Dehavilland DHC-8-102 (N934HA), Newark, NJ, Substantial damage. After an uneventful flight from kphl to kewr, crew selected gear down on final to rwy 4R at kewr. Gear indication was left gear not down and locked. Crew… - [Accident 20120116000849A](https://openairdocs.org/incident/20120116000849A), Jan 16, 2012: Boeing DHC-8-102 (N839EX), Huntington, WV, Substantial damage. A piedmont flight 4117, in aircraft N839EX, struck a deicing truck boom with the left horizontal stabilizer, elevator and elevator trim tab, while taxiing on… - [Incident 20100314029179I](https://openairdocs.org/incident/20100314029179I), Mar 14, 2010: Dehavilland DHC-8-102 (N938HA), Harrisburg, PA, Minor damage. Aircraft returned to gate due to dragging right brake. Right inboard brake caught fire and was immediately extinguished by mechanic. - [Incident 20071203829369I](https://openairdocs.org/incident/20071203829369I), Dec 3, 2007: Dhav DHC8102 (N839EX), Pittsburgh, PA, No damage. (-23) After take-off from 28C, the left main landing gear door open light remained illuminated after gear retraction. The landing gear was then extended to… - [Incident 20070715019159I](https://openairdocs.org/incident/20070715019159I), Jul 15, 2007: Dhav DHC8102 (N812EX), Lititz, PA, No damage. (-23) Piedmont flight H318 in route from MDT to phi diverted to lns with smoke in cabin. Aircraft was evacuated on taxiway with no injuries. Aircraft ferried… - [Incident 20060509006759I](https://openairdocs.org/incident/20060509006759I), May 9, 2006: Dhav DHC8102 (N806EX), Latrobe, PA. (-23) On flight 4518 (pit-avp) about 10 min. After departure the crew started getting smoke in the cockpit from what they described as the windshield area.… - [Incident 20060412005639I](https://openairdocs.org/incident/20060412005639I), Apr 12, 2006: Dhav DHC8102 (N808EX), Pittsburgh, PA, Minor damage. (-23) Air carrier incident, Pittsburgh int'l airport, PA, 4/12/06 at 1547E, piedmont airlines flight 4532, a DHC-8-102, N808EX, returned to land on runway 28R… - [Incident 20040505033669I](https://openairdocs.org/incident/20040505033669I), May 5, 2004: Dhav DHC8102 (N817EX), Rochester, NY. (-23) On may 5, 2004 at approx 1015 local, an allegheny airlines DHC-8, N817EX, had a right gear door light illuminate while landing at Rochester, NY. The… - [Incident 20030912032119I](https://openairdocs.org/incident/20030912032119I), Sep 12, 2003: Dhav DHC8102 (N811AW), Buffalo, NY. (-23) On September 12, 2003 at approx 06:37 EST a DHC-8-102, operated by pcaa, registration number N81AW, was descending into buf when the crew reported the… - [Incident 20030508007129I](https://openairdocs.org/incident/20030508007129I), May 8, 2003: Dhav DHC8102 (N804EX), Pittsburgh, PA. (-23) Allegheny airlines flight #3899 enroute from abe on approach to pit encountered an "airframe vibration" that "occurred three times in flight". The… - [Incident 20030408017289I](https://openairdocs.org/incident/20030408017289I), Apr 8, 2003: Dhav DHC8102 (N811AW), Syracuse, NY. (-23) On April 8, 2003, flt. 9382, a DHC-8, N811AW, took off and returned to Syracuse airport (syr), Syracuse, NY for a landing gear problem. Crew reported… - [Incident 20030402017279I](https://openairdocs.org/incident/20030402017279I), Apr 2, 2003: Dhav DHC8102 (N804EX), Middletown, PA. (-23) Flight controls did not respond as expected after initial climb/turn. Removed and replaced aileron. Test flight was satisfactory and aircraft was… - [Incident 20030312007869I](https://openairdocs.org/incident/20030312007869I), Mar 12, 2003: Dhav DHC8102 (N807EX), Syracuse, NY, Minor damage. (-23) Approximately 10-15 miles out on approach to syr first officer smelled fumes in cockpit. After the smell grew worse the crew donned oxygen masks. At… - [Incident 20030203001479I](https://openairdocs.org/incident/20030203001479I), Feb 3, 2003: Dhav DHC8102 (N814EX), Pittsburgh, PA. (-23) Windshield cracked about 50 miles from pit declared emergency 15 miles from pit. Crew proceeded with checklist and landed without incident. Crews actions… - [Incident 20030126000949I](https://openairdocs.org/incident/20030126000949I), Jan 26, 2003: Dhav DHC8102 (N805EX), Pittsburgh, PA. (-23) At 1137E on January 26, 2003, allegheny airlines flight #3569, a DH8 landed on runway 28R with #1 engine shut down for unknown reasons. Emergency was… - [Incident 20030101000119I](https://openairdocs.org/incident/20030101000119I), Jan 1, 2003: Dhav DHC8102 (N804EX), Pittsburgh, PA. (-23) Abe-pit flight #3511. Crew reported while on descent through 8000 ft. unknown smell was noticed in cockpit and cabin. Smell was suspected to be smoke… - [Incident 20021231034219I](https://openairdocs.org/incident/20021231034219I), Dec 31, 2002: Dhav DHC8102 (N806EX), Pittsburgh, PA, Minor damage. (-23) During pushback, the tow bar disengaged from the tug. Pilot was instructed by ground crew to apply brakes since the plane was rolling backwards.… - [Incident 20021003029729I](https://openairdocs.org/incident/20021003029729I), Oct 3, 2002: Dhav DHC8102 (N804EX), Middletown, PA. (-23) During enroute cruise between rochester, NY (roc) to Washington, DC (dca) at 17,000MSL, #2 hydraulic system isolation visual warning illuminated. #2… - [Incident 20021002029759I](https://openairdocs.org/incident/20021002029759I), Oct 2, 2002: Dhav DHC8102 (N811AW), Albany, NY. (-23) Aircraft departed alb at 10:45AM, all indications were normal during t/o phase of flt. During climb approximately 2000 MSL crew noticed an oil smell in… - [Incident 20020913037099I](https://openairdocs.org/incident/20020913037099I), Sep 13, 2002: Dhav DHC8102 (N839EX), Binghamton, NY. (-23) On September 13, a DHC-8-102, N839EX, a loud vibration was discovered while in level cruise at 12,000 ft. the crew described a grinding sound.… - [Incident 20020905037089I](https://openairdocs.org/incident/20020905037089I), Sep 5, 2002: Dhav DHC8102 (N831EX), Syracuse, NY. (-23) The aircraft was enroute from roc to lga but diverted to syr after the crew reported that the #2 hydraulic isolation valve caution light illuminated.… - [Incident 20020708017969I](https://openairdocs.org/incident/20020708017969I), Jul 8, 2002: Dhav DHC8102 (N818EX), Buffalo, NY. (-23) After the gear was selected up the RH gear door amber light illuminated. The buf FAA tower dispatched the CFR vehicles however the crew did not declare… - [Incident 20020422018079I](https://openairdocs.org/incident/20020422018079I), Apr 22, 2002: Dhav DHC8102 (N817EX), Rochester, NY. (-23) On Monday, April 22, 2002, after selecting the gear-up after takeoff, the left and right amber gear lights and red nose gear light remained illuminated… - [Incident 20020212004599I](https://openairdocs.org/incident/20020212004599I), Feb 12, 2002: Dhav DHC8102 (N811AW), Syracuse, NY. (-23) On Tuesday, February 12, 2002, at 0635 EST, a DHC-8, N811AW, discovered a problem with right torque system (indication erratic) during takeoff in… - [Incident 20020104000659I](https://openairdocs.org/incident/20020104000659I), Jan 4, 2002: Dhav DHC8102 (N838EX), Buffalo, NY. (-23)On Friday, January 4, 2002, the captain of allegheny airlines, flight 3585, a DHC-8, N838EX, noticed sparks coming from his windshield during climb out.… - [Incident 20011209036649I](https://openairdocs.org/incident/20011209036649I), Dec 9, 2001: Dhav DHC8102 (N837EX), Syracuse, NY. (-23) On Sunday, December 9, 2001, a DHC-8, N837EX, operated by allegheny airlines, inc., returned to land on runway 28 at the Syracuse Hancock International… - [Incident 20011203034239I](https://openairdocs.org/incident/20011203034239I), Dec 3, 2001: Dhav DHC8102 (N838EX), Middletown, PA, Minor damage. (-23) Incident report har fdso-13 (IEA1320020006) reported by operations center eastern region (cruz) allegheny (pcaa) flight 3900 diverted into Harrisburg,… - [Incident 20011107031709I](https://openairdocs.org/incident/20011107031709I), Nov 7, 2001: Dhav DHC8102 (N838EX), Philadelphia, PA. (-23) Aircraft hit pocket of turb, px without seat belt hit head on oerhead compartment, no injury. Flight attendant robert schegber while asking pax to put… - [Incident 20010828027239I](https://openairdocs.org/incident/20010828027239I), Aug 28, 2001: Dhav DHC8102 (N827PH), Portland, OR. (-23) On August 28, 2001, at 1515 PDT, a horizon air flight 2185 experienced a "stiffness" in the roll control of the aircraft shortly after departing klamath… - [Incident 20010814028249I](https://openairdocs.org/incident/20010814028249I), Aug 14, 2001: Dhav DHC8102 (N818EX), Syracuse, NY. (-23) On Tuesday, August 14, 2001, a DHC-8, N818EX, shows the following logbook entry: during climb #1 oil pressure rose to 90 and stabilized. Oil pressure… - [Incident 20010809028229I](https://openairdocs.org/incident/20010809028229I), Aug 9, 2001: Dhav DHC8102 (N808EX), Buffalo, NY. (-23) On August 9, 2001, at 08:36 local time, a Dehavilland dash 8 series 102 aircraft, bearing registration number N808EX, serial number 299, operating as… - [Incident 20010713016059I](https://openairdocs.org/incident/20010713016059I), Jul 13, 2001: Dhav DHC8102 (N837EX), Pittsburgh, PA. (-23) On July 13, 2001, at 0842 EST, allegheny airlines flight #3923, a DH8 landed on runway 28L, due to a gear problem. The ARFF responded and the aircraft… - [Incident 20010602018459I](https://openairdocs.org/incident/20010602018459I), Jun 2, 2001: Dhav DHC8102 (N825PH), Vancouver Bc, CN, Minor damage. (-23) Number 4 brake assembly overheated and caught fire due to failure of filter fitting p/n 20011-4-10W. Filter assembly became dislodged and blocked the… - [Incident 20010322007809I](https://openairdocs.org/incident/20010322007809I), Mar 22, 2001: Dhav DHC8102 (N808EX), Syracuse, NY. (-23)On March 22, 2001 at 0936 local time, a Dehavilland dash 8 series 102 aircraft, bearing registration number N808EX, serial number 229, operating as… - [Incident 20010309003319I](https://openairdocs.org/incident/20010309003319I), Mar 9, 2001: Dhav DHC8102 (N940HA), Pittsburgh, PA. (-23) On March 9, 2001, at 2222E, a DHC-8, s/n 156, registered as N940HA and operating as hnaa flight #3316, landed at pit after reporting a hydraulic problem.… - [Incident 20010128001769I](https://openairdocs.org/incident/20010128001769I), Jan 28, 2001: Dhav DHC8102 (N828PH), Portland, OR. (-23) During climb after take off from pdx, #1 engine lost all oil quantity and subsequently lost oil pressure. The crew shut down the engine and returned to… - [Incident 20001216037709I](https://openairdocs.org/incident/20001216037709I), Dec 16, 2000: Dhav DHC8102 (N841EX), Binghamton, NY. (-23) On Saturday December 16, 2000 at 08:23 hours local time, a Dehavilland dash 8 series 100 aircraft, bearing registration number N841EX, serial number 249,… - [Incident 20000630034929I](https://openairdocs.org/incident/20000630034929I), Jun 30, 2000: Dhav DHC8102 (N937HA), Pittsburgh, PA. (-23) On 6/30/2000, at 1626E, a U.S. Registered piedmont airlines DHC-8-102, aborted taxi on the ramp at Pittsburgh international airport (pit) due to a nose… - [Incident 20000608032949I](https://openairdocs.org/incident/20000608032949I), Jun 8, 2000: Dhav DHC8102 (N804EX), Binghamton, NY. (-23)On Thursday, June 8, 2000 at 0843 local, an allegheny airlines (d/b/a usair express) DHC-8, N804EX, reported smoke in the cockpit inbound from bgm. The… - [Incident 20000328001919I](https://openairdocs.org/incident/20000328001919I), Mar 28, 2000: Dhav DHC8102 (N822EX), Pittsburgh, PA. (-23) On March 28, 2000, at 0959E, DHC-8, s/n 187, registered as N822EX, landed at pit after the crew reported the elevator manual trim had jammed in cruise… - [Incident 20000214002669I](https://openairdocs.org/incident/20000214002669I), Feb 14, 2000: Dhav DHC8102 (N808EX), Newburgh, NY. On feb 14, 2000 flight 3957 departed the gate at swf at approximately 1010 hrs local time and taxiing to the active runway when the flight attendant reported… - [Incident 20000213003309I](https://openairdocs.org/incident/20000213003309I), Feb 13, 2000: Dhav DHC8102 (N817EX), Pittsburgh, PA. On February 13, 2000, at 2126E, DHC-8, regristered as N817EX and operated by "pcaa" as flight 3779, landed at Pittsburgh, PA (pit) on runway 10L after… - [Incident 20000112001079I](https://openairdocs.org/incident/20000112001079I), Jan 12, 2000: Dhav DHC8102 (N809EX), Buffalo, NY. (-23) On Wednesday, January 12, 2000, at 0737 local, an allegheny airlines d/b/a us air express, DHC-8, N809EX, performed an air turnback to buf due to an… - [Incident 20000111001089I](https://openairdocs.org/incident/20000111001089I), Jan 11, 2000: Dhav DHC8102 (N839EX), Binghamton, NY. (-23) On 1/11/00 pcaa flight 3863, DH-8, N839EX, pilot shut down the #1 engine due to a low oil pressure indication. The low oil pressure light did not… - [Incident 20000110001199I](https://openairdocs.org/incident/20000110001199I), Jan 10, 2000: Dhav DHC8102 (N937HA), Asheville, NC. (-23) The aircraft was cruising at 9000 feet when the number two engine shut itself down. The number 2 engine elctronic control unit (ecu) had gone into… - [Incident 20000101001159I](https://openairdocs.org/incident/20000101001159I), Jan 1, 2000: Dhav DHC8102 (N841EX), Binghamton, NY. (-23) On Saturday, January 1, 2000, at 1206 local, allegheny airlines d/b/a us air express, DHC-8-102, N841EX, diverted into bgm due to a possible vibration in… - [Incident 19991215034869I](https://openairdocs.org/incident/19991215034869I), Dec 15, 1999: Dhav DHC8102 (N807EX), Providence, RI, Minor damage. (-23) Allegheny flight 3637 struck a ramp boundary fence with the left wing while taxiing in a non-movement area at pvd. Visibility was marginal and the pilot… - [Incident 19991127030899I](https://openairdocs.org/incident/19991127030899I), Nov 27, 1999: Dhav DHC8102 (N804EX), Buffalo, NY. (-23)On Saturday, November 27, 1999 at 1410 local, an allegheny airlines (d/b/a usair express) DHC-8-102, N804EX shut down the nbr 2 engine due to the oil… All 100: https://openairdocs.org/model/boeing-dhc-8-102/incidents.md ## Service difficulty reports (9,272, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR CA190802005](https://openairdocs.org/sdr/CA190802005), Jul 30, 2019: BEARING. SEIZED. (CAN) FLIGHT CREW REPORTED AILERON CONTROL HAD AN ODD FEELING IN FLIGHT, SOMEWHAT STIFF AND HEAVY. UPON AN UNEVENTFUL LANDING, MAINTENANCE PERSONNEL CARRIED OUT - [SDR CA190821005](https://openairdocs.org/sdr/CA190821005), Jul 25, 2019: UNKNOWN. SMOKE. (CAN) WHILE TAXIING THE CREW HEARD A CLUNKING SOUND AND THEN OBSERVED SMOKE IN THE FLIGHT DECK AND CABIN AREAS. THE AIRCRAFT RETURNED TO THE GATE. . (TC# 201908 - [SDR CA190726022](https://openairdocs.org/sdr/CA190726022), Jul 25, 2019: ACM. SEIZED. (CAN) THE CREW MADE A GATE RETURN AS CABIN TEMP COULD NOT BE CONTROLLED IN MANUAL OR AUTO MODE. AFTER A SYSTEM RESET AND ENGINE START THEY BEGAN TO LEAVE THE AP - [SDR CA190729013](https://openairdocs.org/sdr/CA190729013), Jul 17, 2019: PRESSURE SWITCH. FAILED. (CAN) #2 BLEED HOT ILLUMINATED DURING CRUISE. SYSTEM GOT TURNED OFF, AFTER THAT #1 SYSTEM FAILED. EMERGENCY DECENT WAS EXECUTED, PLANE DIVERTED TO YQT FOR MAINT - [SDR CA190711001](https://openairdocs.org/sdr/CA190711001), Jul 8, 2019: VALVE. DAMAGED. (CAN) DURING CRUISE FLIGHT, #2 ENGINE WAS SHUTDOWN DUE TO HIGH ENGINE OIL TEMPS. THE OIL COOLER THERMO VALVE WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. (TC# - [SDR CA190730010](https://openairdocs.org/sdr/CA190730010), Jul 8, 2019: OIL SYSTEM. OVERTEMP. (CAN) DURING THE FLIGHT, THE FLIGHT CREW NOTICED A HIGH OIL TEMPERATURE ON THE NUMBER 2 ENGINE. AS THE TEMPERATURE CONTINUED TO INCREASE, THE FLIGHT CREW ELECTE - [SDR CA190625001](https://openairdocs.org/sdr/CA190625001), Jun 22, 2019: LEVER. BINDING. (CAN) WHILE CARRYING AILERON ROLL DISCONNECT, FOUND CLUNKING NOISE COMING FROM UNDERFLOOR QUADRANT. FOUND COPILOT AILERON PULLEY QUADRANT BEARING CAUSING THE NO - [SDR CA190704001](https://openairdocs.org/sdr/CA190704001), Jun 20, 2019: ENGINE. SURGES. (CAN) PILOT REPORTED THAT #2 ENGINE STARTED SURGING IMMEDIATELY AFTER THE AIRCRAFT WAS AIRBORNE AND WITH THE GEAR SELECTED UP. PILOT INITIALLY HEARD THE CYCLING - [SDR CA190604014](https://openairdocs.org/sdr/CA190604014), Jun 2, 2019: EEC. MALFUNCTIONED. (CAN) AFTER DEPARTURE #2 ENGINE TORQUE ROLLED BACK 16 % TWO SEPARATE TIMES WITH NO ECU LIGHT. TORQUE INDICATION RETURNED TO NORMAL AFTER A FEW SECONDS. MOMENTAR - [SDR CA190531011](https://openairdocs.org/sdr/CA190531011), May 30, 2019: HMU. FAILED. (CAN) DURING CRUISE THE CREW REPORTED A #2 PROP OVER SPEED INDICATION AND SHUT DOWN THE ENGINE. THE CREW DECLARED AN EMERGENCY AND CONTINUED TO BASE, LANDING WI - [SDR CA190523003](https://openairdocs.org/sdr/CA190523003), May 21, 2019: CONTROL BOX. SHORTED. (CAN) MULTIPLE INVERTER FAILURE `PRI INV`, `SEC INV`, `AUX INV`, `LVAC26` AND `R26VAC` CAUTION LIGHTS ILLUMINATED. LOST ALL FLIGHT INSTRUMENTS ON CAPT, F/O SIDE - [SDR CA190521032](https://openairdocs.org/sdr/CA190521032), May 18, 2019: FITTING. LEAKING. (CAN) DURING POST FLIGHT INSPECTION, OIL WAS NOTED LEAKING FROM #1 ENGINE. MAINTENANCE FOUND THAT A FITTING WAS LOOSE ON THE ACCESSORY OIL PUMP DRIVE COVER. THE - [SDR CA190517008](https://openairdocs.org/sdr/CA190517008), May 16, 2019: RELAY. MALFUNCTIONED. (CAN) AFTER BOTH ENGINES WERE STARTED AT THE GATE FOR DEPARTURE, SMOKE WAS OBSERVED COMING FROM THE RHS ENGINE BY RAMP CREW. CAPTAIN WAS ADVISED TO SHUT DOWN EN - [SDR CA190703018](https://openairdocs.org/sdr/CA190703018), May 15, 2019: FUEL HEATER. MALFUNCTIONED. (CAN) DURING INSTALL OF FUEL HEATER ON #1 ENGINE IT WAS DISCOVERED THAT THERE WAS WHAT APPEARED TO BE MEDIA BLAST (GLASS BEAD) IN THE FILTER BOWL. THE UNIT WAS - [SDR CA190516006](https://openairdocs.org/sdr/CA190516006), May 15, 2019: GCU. FAILED. (CAN) ON DESCENT THE AIRCRAFT SUSTAINED A LIGHTNING STRIKE. BOTH DC GENERATORS TRIPPED BUT WERE ABLE TO RESET. THIS WAS FOLLOWED BY A LOSS OF THE DC BUS AND THE - [SDR CA190425024](https://openairdocs.org/sdr/CA190425024), Apr 22, 2019: TORQUE TUBE. CHAFED. (CAN) WHILE PERFORMING UNRELATED MAINTENANCE, AN AME OBSERVED THAT A FLAP DRIVE TORQUE TUBE LOCATED ON THE LEFT WING, INBOARD OF THE OUTER FLAP ACTUATOR HAD SEV - [SDR CA190422003](https://openairdocs.org/sdr/CA190422003), Apr 20, 2019: SWITCH. FAILED. (CAN) NR 1 ENGINE ECU MANUAL CAUTION ILLUMINATED AT 50FT AGL, TORQUE SPLIT IN CRUISE NOT WITHIN MEL CRITERIA, SOC ELECTED TO RETURN AC TO DEPARTURE AIRPORT. MAI - [SDR CA190424005](https://openairdocs.org/sdr/CA190424005), Apr 19, 2019: SWITCH. MALFUNCTIONED. (CAN) CREW RECEIVED PACK HOT CAUTION MESSAGE, FOLLOWED QRH AND DESCENDED TO 14,000 FEET. DECLARED AN EMERGENCY WITH ATC AND LANDED WITHOUT INCIDENT. NO PASSENGE - [SDR CA190410016](https://openairdocs.org/sdr/CA190410016), Apr 9, 2019: WIRE. CHAFED. (CAN) AFTER GROUND CREW HAD CONNECTED AC POWER THE RH AC CONTACTOR BOX AREA BEGAN TO EMIT SMOKE AND VISIBLE ARCHING. MAINTENANCE DISCOVERED THAT A 20GAUGE AC WI - [SDR CA190409009](https://openairdocs.org/sdr/CA190409009), Apr 8, 2019: BEARING RACE. FRACTURED. (CAN) WHILE TROUBLESHOOTING A LH PROP LEAK MAINTENANCE DISCOVERED THE INNER BEARING RACE FOR THE #2 BLADE TO HAVE BROKEN AND FAILED. LH PROP HUB AND BLADES HAVE - [SDR CA190402006](https://openairdocs.org/sdr/CA190402006), Mar 31, 2019: CONTROL PANEL. ODOR. (CAN) ON INITIAL CLIMB OUT FLIGHT CREW REPORTED LIGHT ELECTRICAL BURN SMELL. MAINTENANCE IDENTIFIED THAT THE SMELL WAS COMING FROM #1 AUDIO CONTROL PANEL. PANEL - [SDR CA190326008](https://openairdocs.org/sdr/CA190326008), Mar 24, 2019: IMPELLER. DAMAGED. (CAN) DURING MAINTENANCE THE #2 ENGINE WAS DISCOVERED TO HAVE IMPELLER DAMAGE. AFTER A BOROSCOPE WAS CARRIED OUT FURTHER DAMAGE WAS FOUND ON THE DIFFUSER CHANNE - [SDR CA190325017](https://openairdocs.org/sdr/CA190325017), Mar 24, 2019: TRANSDUCER. FAILED. (CAN) IMMEDIATELY AFTER TAKEOFF THE STICK SHAKER ACTIVATED. IT REMAINED ON UNTIL THE CREW RETURNED TO BASE. THE AIRCRAFT LANDED WITHOUT INCIDENT AND NO EMERGENC - [SDR CA190301005](https://openairdocs.org/sdr/CA190301005), Feb 28, 2019: CASE. CRACKED. (CAN) ENGINE WAS REMOVED DUE TO HIGHER THAN NORMAL ITT. AN APPROXIMATELY 4 INCH CRACK WAS FOUND ADJACENT TO THE NO. 1 FUEL NOZZLE IN THE GAS GENERATOR CASE. - [SDR CA190227007](https://openairdocs.org/sdr/CA190227007), Feb 25, 2019: TUBE. CHAFED. (CAN) AIRCRAFT DEPARTED AND LOST ALL HYDRAULIC FLUID FROM #1 HYDRAULIC SYSTEM AFTER 45 MINUTES IN CRUISE. THEY CAME BACK TO LAND AND DECLARED EMERGENCY. THEY HA - [SDR CA190226007](https://openairdocs.org/sdr/CA190226007), Feb 23, 2019: BEARING RACE. FRACTURED. (CAN) DURING REMOVAL OF LH2 BLADE FOR RESTORATION A TECHNICIAN FOUND ONE OF THE TWO PIECE INNER BEARING RACES FRACTURED. THE PROP HUB AND BLADE SHOWED SIGNS OF - [SDR CA190409007](https://openairdocs.org/sdr/CA190409007), Jan 18, 2019: SMOKE DETECTOR. FAILED. (CAN) INTERNAL FAILURE OF PART (SMOKE DETECTOR TYPE II) CAUSING `SMOKE WARNING` ANNUNICATOR TO ILLUMINATE (TC# 20190409007) - [SDR CA180706015](https://openairdocs.org/sdr/CA180706015), Jul 4, 2018: CONTROL UNIT. NO TEST. (CAN) AIRCRAFT TAXIED FOR DEPARTURE AND WAS HOLDING SHORT OF RUNWAY FOR TAKE OFF, FLIGHT CREW REPORTED TO MAINTENANCE CONTROL THAT THE AIRCRAFT WOULDN`T MOVE WH - [SDR CA180723012](https://openairdocs.org/sdr/CA180723012), Jun 18, 2018: CONDENSER. CRACKED. (CAN) DURING FLIGHT, FLIGHT CREW REPORTED AN INTERMITTENT AIR COND PACK HOT AMBER CAUTION LIGHT. DURING TROUBLESHOOTING, THE CONDENSER MIXER WAS FOUND CRACKED A - [SDR CA180404019](https://openairdocs.org/sdr/CA180404019), Apr 1, 2018: OIL COOLER. LEAKING. (CAN) ON APPROACH THE NR 1 ENGINE OIL PRESSURE DROPPED TO APPROXIMATELY 40PSI WITH ASSOCIATED NR 1 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. WHILE TAXIING - [SDR CA180103007](https://openairdocs.org/sdr/CA180103007), Dec 30, 2017: PUMP. FAILED. (CAN) SHORTLY AFTER TAKE-OFF THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP FAILED. THE CREW TURNED BACK TO BASE AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. - [SDR HNAA2017103000364](https://openairdocs.org/sdr/HNAA2017103000364), Oct 29, 2017: LIGHT. INOPERATIVE. EMERGENCY LIGHTS AT ROW 17DF DIM. REMOVE AND REPLACED THE EMERGENCY LIGHT ASSEMBLIES AT ROW 7DF. - [SDR HNAA2017103000361](https://openairdocs.org/sdr/HNAA2017103000361), Oct 29, 2017: INDICATOR. MALFUNCTIONED. ON TAKEOFF, NR 2 ITT INDICATOR STUCK AT 1050. ALL OTHER ENGINE PARAMETERS AND INDICATIONS WERE NORMAL. POWERED AIRCRAFT DOWN AND REAPPLIED POWER. TESTED NR 2 IT - [SDR HNAA2017101000347](https://openairdocs.org/sdr/HNAA2017101000347), Oct 8, 2017: LIGHT. INOPERATIVE. FLOOR EMERGENCY LIGHT AT SEAT 7DF INOPERATIVE. R & R THE EMERGENCY LIGHT. - [SDR HNAA2017101000346](https://openairdocs.org/sdr/HNAA2017101000346), Oct 6, 2017: BULB. BURNED OUT. CABIN FLOOR EMERGENCY LIGHT THIRD RED LIGHT BULB INOPERATIVE AT SEAT 1DF. REMOVED & REPLACED THE BULB. - [SDR HNAA2017092900336](https://openairdocs.org/sdr/HNAA2017092900336), Sep 27, 2017: SWITCH. INOPERATIVE. FLOOR EMERGENCY LIGHTS WILL NOT TURN OFF USING F/A SWITCH. SIDE WALL LIGHTS WILL NOT RESPOND TO THE SWITCH. R & R THE F/A LIGHTS CONTROL PANEL IAW 33-20-00, AND - [SDR HNAA2017092900339](https://openairdocs.org/sdr/HNAA2017092900339), Sep 26, 2017: UNKNOWN. ODOR. CREW REPORTED AN ODD ODOR IN THE ACFT AROUND SEAT 5AC. DROPPED LT PSU AND CENTER AISLE PANEL INSPECTED, NO FAULTS FOUND. REINSTALLED PSU AND CENTER PANEL. OPS C - [SDR HNAA2017091801](https://openairdocs.org/sdr/HNAA2017091801), Sep 16, 2017: POWER SUPPLY. BURNED. DURING TROUBLESHOOTING OF SEQ 3, FOUND THE POWER SUPPLY BASE AT 3351-P4 HAS A BURNED ODOR AND APPEARS TO HAVE A BURNED RESISTOR. R & R THE EMERGENCY LIGHT POWER - [SDR HNAA20170918317](https://openairdocs.org/sdr/HNAA20170918317), Sep 16, 2017: BATTERY PACK. INOPERATIVE. LEFT FUSELAGE MOUNTED EMERGENCY LIGHTS INOPERATIVE. R & R THE POWER SUPPLY AND BATTERY AT 3351-PS3 IAW AMM 33-51-00. - [SDR HNAA20170918316](https://openairdocs.org/sdr/HNAA20170918316), Sep 16, 2017: WARNING LIGHT. UNKNOWN. RIGHT AC BUSS CAUTION LIGHT ILLUMINATED DURING CLIMB OUT, WITH ASSOCIATED CAUTION LIGHTS. REMOVED AND REINSTALLED THE LT AC GCU FOR TROUBLESHOOTING. REPLACED RT - [SDR HNAA2017091400304](https://openairdocs.org/sdr/HNAA2017091400304), Sep 9, 2017: SWITCH. LACK OF LUBE. REJECTED TAKE OFF DUE TO AT 60 PERCENT TORQUE AUTOFEATHER ARM LIGHT ILLUMINATED WITH TAKEOFF WARNING HORN. CLEANED AND LUBRICATED THE SWITCHES. R & R FLAP POSIT - [SDR HNAA2017090500299](https://openairdocs.org/sdr/HNAA2017090500299), Sep 3, 2017: LIGHT. INOPERATIVE. MIDDLE CEILING EMERGENCY LIGHT INOP. - [SDR HNAA2017082500288](https://openairdocs.org/sdr/HNAA2017082500288), Aug 24, 2017: CONTACTOR. INOPERATIVE. LEFT MAIN GEAR INDICATION FAILED IN THE DIM AND BRIGHT MODE. GREEN DOWNLOCK INDICATION. INSPECTION FOUND CONTACTS NOT CONNECTING TO BULBS. - [SDR HNAA2017082500286](https://openairdocs.org/sdr/HNAA2017082500286), Aug 24, 2017: AUTOFEATHER SYS. MALFUNCTIONED. REJECTED TAKEOFF DUE TO AUTOFEATHER NOT ARMING UP TO 90% TORQUE. R & R THE NR 1 TSEU. GROUND RAN ACFT. AUTO-FEATHER SYSTEM OPS NORMAL IAW RUNUP MANUAL,. OK FOR - [SDR HNAA2017080200259](https://openairdocs.org/sdr/HNAA2017080200259), Aug 2, 2017: SIGN. INOPERATIVE. EMERGENCY LIGHT INOPERATIVE ON FWD RT FUSELAGE, FWD AISLE OVERHEAD EMERGENCY EXIT SIGN. - [SDR HNAA2017073100253](https://openairdocs.org/sdr/HNAA2017073100253), Jul 30, 2017: LIGHT. INOPERATIVE. EMERGENCY AISLE LIGHT INOPERATIVE AT ROW 7 - [SDR HNAA2017073100254](https://openairdocs.org/sdr/HNAA2017073100254), Jul 29, 2017: LIGHT. INOPERATIVE. THE THIRD RED AFT EMERGENCY AISLE LIGHT IS INOPERATIVE. - [SDR HNAA2017073100251](https://openairdocs.org/sdr/HNAA2017073100251), Jul 25, 2017: LIGHT. INOPERATIVE. THIRD RED FLOOR EMERGENCY LIGHT INOPERATIVE. - [SDR HNAA2017072500247](https://openairdocs.org/sdr/HNAA2017072500247), Jul 21, 2017: BATTERY. DISCHARGED. FWD RT EXTERNAL EMERGENCY LIGHT INOPERATIVE, GALLEY CEILING, RT FWD EMERGENCY EXIT TOP, NOT WORKING . CHANGED THE BATTERY AT 3351 PS2 LOCATION IAW AMM 33-51-00, - [SDR HNAA2017071200238](https://openairdocs.org/sdr/HNAA2017071200238), Jul 11, 2017: CONNECTOR. DIRTY. NR 2 ITT AND TORQUE GAUGES CIRCUIT BREAKERS TRIPPED INFLT. REMOVED AND CLEANED THE ENGINE SPIDER HARNESS CONNECTOR AT THE FIRE WALL. RESET CIRCUIT BREAKERS AND All 9,272: https://openairdocs.org/model/boeing-dhc-8-102/reports.md ## STCs that may be installed (OpenAirDocs) (138, 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 SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight 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 ST04559CH](https://openairdocs.org/stc/ST04559CH): Installation of L3Harris Aviation Products SRVIVR25 Model 7100 Cockpit Voice Recorder (CVR) System. Acron Aviation 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 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 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 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 ST00015NY](https://openairdocs.org/stc/ST00015NY): 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 SA2916SO](https://openairdocs.org/stc/SA2916SO): Installation of dual TRA-67 Mode S transponder system. Honeywell International Inc - [STC SA2917SO](https://openairdocs.org/stc/SA2917SO): Installation of CAS-81 TCAS II system. 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 SA9086SC-D](https://openairdocs.org/stc/SA9086SC-D): Recore of Hamilton Standard Heat Exchangers 778683-2 for Installation on deHavilland DHC-8 Series Aircraft and 778683-2 for Installation on Fokker F27 Mark 050 Aircraft, in accordance with Honeywell LORI Sealed Drawing List SDL3545-1, Revision C, dated 11 October 2005 or later FAA approved revision. Honeywell International Inc - [STC SA9080SC-D](https://openairdocs.org/stc/SA9080SC-D): Replace 30E94-2 Sensing Element in Janitrol Valve 45E04-1 used on DHC-8 Oil Coolers 28E99-6 and 28E99-7 in accordance with Honeywell LORI Specification LR 0201-117 as reflected on Honeywell LORI Sealed Drawing List SDL3709-1, Revision A, dated 11 October 2005 or later FAA approved revision. Honeywell International Inc - [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 ST04449NY](https://openairdocs.org/stc/ST04449NY): Conversion of DHC-8-102/-103/-106 from passenger carrying aircraft into Package Freighter with a Class E Cargo Compartment. Voyageur Aerotech 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 All 138: https://openairdocs.org/model/boeing-dhc-8-102/stcs.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Boeing Of Canada/Dehav Div DHC-8-102](https://openairdocs.org/model/boeing-of-canada-dehav-div-dhc-8-102): 1 registered aircraft, registry code 1385303 - [Dehavilland DHC-8-102](https://openairdocs.org/model/dehavilland-dhc-8-102): 1 registered aircraft, registry code 2809003 - [Boeing Of Canada DHC-8-102](https://openairdocs.org/model/boeing-of-canada-dhc-8-102): 0 registered aircraft, registry code 1385305 - [Bombardier DHC-8-102](https://openairdocs.org/model/bombardier-dhc-8-102): 0 registered aircraft, registry code 1390002 --- 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.