# Dehavilland DHC-8-102 - Type: Aircraft model (FAA registry) - Registry code: 2809003 - Manufacturer (registry): DEHAVILLAND - 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: 1 - Page: https://openairdocs.org/model/dehavilland-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/dehavilland-dhc-8-102/ads.md ## Registered aircraft (1) - [N8100V](https://openairdocs.org/aircraft/N8100V): [Dynamic Avlease Inc](https://openairdocs.org/faa-owner/DYNAMIC%20AVLEASE%20INC), [Bridgewater, VA](https://openairdocs.org/faa-place/VA/Bridgewater), built 1985, S/N 024 ## NTSB investigations (7) 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 DCA14CA147](https://openairdocs.org/ntsb/DCA14CA147), Aug 10, 2014: Dehavilland DHC 8 102 (N815EX), Harrisburg, PA, substantial damage. Probable cause: the airplanes collision with geese during the takeoff roll. - [NTSB SEA01FA059](https://openairdocs.org/ntsb/SEA01FA059), Mar 6, 2001: de Havilland DHC-8-102 (N822PH), Portland, OR, substantial damage. Probable cause: The failure of the number 5 engine bearing assembly followed by the disconnection of the P2.5/P3 switching valve to rear inlet case sealing air tube and the melting of the NL probe port (sealing… - [NTSB CHI97IA075](https://openairdocs.org/ntsb/CHI97IA075), Jan 22, 1997: de Havilland DHC-8-102 (N852MA), Charleston, WV, incident, no damage. Probable cause: a fractured fusion weld in the piston of the roll spoiler servoactuator, which allowed the plug at the base of the piston to separate and jam the piston. A factor relating to the incident was: the… - [NTSB CHI93IA068](https://openairdocs.org/ntsb/CHI93IA068), Jan 8, 1993: de Havilland DHC-8-102 (N826MA), Detroit, MI, incident, no damage. Probable cause: THE MANUFACTURER'S INADEQUATE DESIGN OF THE FUEL TRANSFER TUBE SYSTEM, WHICH LOOSENED/DISCONNECTED DURING ENGINE OPERATION. - [NTSB ATL91IA134](https://openairdocs.org/ntsb/ATL91IA134), Jul 17, 1991: de Havilland DHC-8-102 (N922HA), Savannah, GA, incident, minor damage. Probable cause: THE INADEQUATE INSPECTION PROCEDURES WHICH ALLOWED THE LOSS OF TORQUE ON THE TOP RETRACTION FITTING ATTACHMENT BOLT WHICH SUBSEQUENTLY FAILED IN FATIGUE. FACTORS WERE THE LOSS OF HYDRAULIC FLUID… - [NTSB MIA90IA159](https://openairdocs.org/ntsb/MIA90IA159), Jul 25, 1990: de Havilland DHC-8-100 (N800MX), Panama City, FL, incident, no damage. Probable cause: FAILURE OF SEAL IN THE HYDRAULIC ACTUATOR FOR THE RIGHT OUTBOARD WING SPOILER PANEL FOR UNKNOWN REASONS. - [NTSB ATL87IA034](https://openairdocs.org/ntsb/ATL87IA034), Dec 3, 1986: de Havilland DHC-8-101 (N802MX), Atlanta, GA, incident, minor damage ## FAA accident and incident reports (74, 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. - [Accident 20140810014459A](https://openairdocs.org/incident/20140810014459A), Aug 10, 2014: Dehavilland DHC-8-102 (N815EX), Harrisburg, PA, Substantial damage. During take off roll at approx 40 knots IAS aircraft encountered a flock of geese striking several causing approx 17 inches of 1 propeller blade to separate… - [Incident 20080316012429I](https://openairdocs.org/incident/20080316012429I), Mar 16, 2008: Dhav DHC8102 (N815EX), Allentown, PA, Minor damage. (-23) Shortly after take off from Allentown, PA (abe) the crew noted a hydraulic problem. They elected to return to abe. Maintenance discovered a hydraulic… - [Incident 20070429008119I](https://openairdocs.org/incident/20070429008119I), Apr 29, 2007: Dhav DHC8102 (N907HA), Charlotte, NC, Minor damage. (-23) After departure at 2117 a bad smell was noticed in the cabin of hnaa flight 4242 by passengers and the fa, shortly after, hyd fluid (skydrol) leaked into… - [Incident 20050119000869I](https://openairdocs.org/incident/20050119000869I), Jan 19, 2005: Dhav DHC8102 (N816EX), Pittsburgh, PA, Minor damage. (-23) Desk audit: on January 19, 2005, at approximately 2100 eastern standard time, a Dehavilland DHC-8-102, N816EX, flight number 3742 conducted under 14 CFR… - [Incident 20040616011429I](https://openairdocs.org/incident/20040616011429I), Jun 16, 2004: Dhav DHC8102 (N827EX), Burlington, VT, Minor damage. (-23) Suspicious package was found in ROW9 after parking at gate in btv. The package was lodged in such a manner making it impossible to investigate. Package… - [Incident 20040128002239I](https://openairdocs.org/incident/20040128002239I), Jan 28, 2004: Dhav DHC8102 (N827EX), Syracuse, NY. (-23) On January 28, 2004, flt. 3843, DHC-8, N827EX, departed ithaca airport, ithaca, NY, crew observed the #1 oil pressure indication was 85-95 PSI on… - [Incident 20031113035869I](https://openairdocs.org/incident/20031113035869I), Nov 13, 2003: Dhav DHC8102 (N914HA), Charlottesville, VA, Minor damage. (-23) Aircraft landed hard due to gusty wind and turbulence. Damage to landing gear and fuselage sustained. - [Incident 20031011032639I](https://openairdocs.org/incident/20031011032639I), Oct 11, 2003: Dhav DHC8102 (N980HA), Syracuse, NY. (-23) On October 11, 2003, a DHC-8, flt. 3629, crew reported that the #2 engine power uptrim partially activated during takeoff. Crew experienced repeated #2… - [Incident 20031010032199I](https://openairdocs.org/incident/20031010032199I), Oct 10, 2003: Dhav DHC8102 (N846EX), Middletown, PA. (-23) During cruise flight @ 5000 ft. the #2 engine started to vibrate and oil pressure dropped to 40 PSI. #2 engine was shut down, emergency declared,… - [Incident 20030822018579I](https://openairdocs.org/incident/20030822018579I), Aug 22, 2003: Dhav DHC8102 (N906HA), Charlotte, NC, Minor damage. (-23) Due to impending weather, a piedmont aircraft (N906HA) was holding off taxiway charlie with both engines shut down and APU running. Thunderstorm hit the… - [Incident 20030319007949I](https://openairdocs.org/incident/20030319007949I), Mar 19, 2003: Dhav DHC8102 (N982HA), Binghamton, NY. (-23) Crew reported the #2 hyd isolation valve caution light illuminated after gear extension. 1.4 quarts remaining in #2 system. The aircraft landed on runway… - [Incident 20030201007879I](https://openairdocs.org/incident/20030201007879I), Feb 1, 2003: Dhav DHC8102 (N825EX), Binghamton, NY. (-23) On February 1, 2003, flt. 3577, N825EX, DHC-8, on climb-out, gear was selected "up", and hydraulic quantity on #2 system went to "0". Aircraft landed… - [Incident 20030112000129I](https://openairdocs.org/incident/20030112000129I), Jan 12, 2003: Dhav DHC8102 (N846EX), Pittsburgh, PA. (-23) Pcaa flight 3856 landed on 28R with the #1 engine shutdown due to fluctuating oil pressure indication. Maintenance complied with unscheduled maintenance… - [Incident 20020630016339I](https://openairdocs.org/incident/20020630016339I), Jun 30, 2002: Dhav DHC8102 (N980HA), Pittsburgh, PA. (-23) On June 30, 2002 allegheny airlines flight #3731 aborted take-off on runway 28R due to #1 engine low oil pressure annunciator illuminating. The pilot… - [Incident 20020529019299I](https://openairdocs.org/incident/20020529019299I), May 29, 2002: Dhav DHC8102 (N980HA), Binghamton, NY. (-23) On Wednesday, may 29, 2002, the crew of DHC-8, N980HA, reported a right gear unsafe and nose yellow door light illuminated on climbout. Both gear… - [Incident 20020512008419I](https://openairdocs.org/incident/20020512008419I), May 12, 2002: Dhav DHC8102 (N820EX), Windsor Locks, CT. (-23) After landing at kbdl, N820EX was taxiing to the gate. The crew started the APU. The APU started normally. It was noted that the generator warning light… - [Incident 20020222001829I](https://openairdocs.org/incident/20020222001829I), Feb 22, 2002: Dhav DHC8102 (N906HA), Pittsburgh, PA. (-23) On February 22, 2002, at 1427E piedmont airlines flight 3310 returned to pit after reporting a gear retraction problem. The DHC-8 landed on runway 32,… - [Incident 20020119001599I](https://openairdocs.org/incident/20020119001599I), Jan 19, 2002: Dhav DHC8102 (N846EX), Binghamton, NY. (-23) On Saturday, January 19, 2002, a DHC-8 aircraft, N846EX, operated by allegheny airlines, inc., was enroute from ith to lga and diverted to bgm due to… - [Incident 20020109000459I](https://openairdocs.org/incident/20020109000459I), Jan 9, 2002: Dhav DHC8102 (N982HA), Norfolk, VA, Substantial damage. (-23) At 20:45 hrs, at the Norfolk International Airport (orf) an aircraft was stationary at gate 9 with both engines powered up. Two piedmont mechanics were… - [Incident 20011214034289I](https://openairdocs.org/incident/20011214034289I), Dec 14, 2001: Dhav DHC8102 (N980HA), Middletown, PA. (-23) After takeoff there was a heading mismatch. Crew returned to MDT with no further incident. There was no fire or injuries resulting from this incident.… - [Incident 20010517014939I](https://openairdocs.org/incident/20010517014939I), May 17, 2001: Dhav DHC8102 (N827EX), Binghamton, NY. (-23) On may 17, 2001 at 1949 EDT, N827EX, a Dehavilland, DHC-8-102, s/n 390, operated by allegheny airlines, landed on runway 16 at Edwin a. Link/broome… - [Incident 20010306005709I](https://openairdocs.org/incident/20010306005709I), Mar 6, 2001: Dhav DHC8102 (N822PH), Portland, OR, Substantial damage. (-23) A/c enroute from sea to pdx, crew noticed vibration on #2 engine and smell of smoke in cabin. Crew declared an emergency and landed at pdx. During… - [Incident 20000919037729I](https://openairdocs.org/incident/20000919037729I), Sep 19, 2000: Dhav DHC8102 (N845EX), Binghamton, NY. (-23)On Tuesday, September 19, 2000 at 1730 local, an allegheny airlines d/b/a usair express, flight 3860, N845EX, a DHC-8-102 reported to the Binghamton ATCT… - [Incident 20000915027219I](https://openairdocs.org/incident/20000915027219I), Sep 15, 2000: Dhav DHC8102 (N820EX), Ithaca, NY. (-23)On Friday, September 15, 2000 at 1034 local, a Dehavilland DHC-8-102, N820EX, flight 3707, operated by allegheny airlines, departed from binghamton, NY to… - [Incident 20000905027259I](https://openairdocs.org/incident/20000905027259I), Sep 5, 2000: Dhav DHC8102 (N917HA), Columbia, SC. (-23)The pilot relayed to jacksonville approach control that while in the vicinity of Columbia,SC (cae), descending out of 18,000 feet for 16,000 feet, he… - [Incident 20000616034139I](https://openairdocs.org/incident/20000616034139I), Jun 16, 2000: Dhav DHC8102 (N819EX), New York, NY. (-23)At La Guardia Airport, allegheny-flt. 3676 captain, wtih assistance from first officer had difficulty turning control column to right to move aileron.… - [Incident 20000211002929I](https://openairdocs.org/incident/20000211002929I), Feb 11, 2000: Dhav DHC8102 (N819EX), Buffalo, NY. On Friday, February 11, 2000 at 1236 EST, allegheny airlines flight 3594, DHC-8, N819EX, landed on runway 31 at Buffalo niagara international airport due to a… - [Incident 20000111000409I](https://openairdocs.org/incident/20000111000409I), Jan 11, 2000: Dhav DHC8102 (N982HA), Elmira, NY. (-23) On Tuesday, 1/11/2000 at 1116 local, a piedmont airlines (d/b/a usair express) reported a captain's side window cracked. The aircraft landed on runway 28… - [Incident 19990826024749I](https://openairdocs.org/incident/19990826024749I), Aug 26, 1999: Dhav DHC8102 (N713M), Erie, PA, Minor damage. Pilot stated that while on an IFR flight from stewart international (swf) to detroit metro (dtw) and while in cruise flight at 14,000 feet, between dunkirk… - [Incident 19990513014319I](https://openairdocs.org/incident/19990513014319I), May 13, 1999: Dhav DHC8102 (N814PH), Portland, OR. After reaching 3000 ft, while departing from pdx, the flight crew was given a left turn by ATC. The fo noticed very still aileron control while in the left… - [Incident 19990315016839I](https://openairdocs.org/incident/19990315016839I), Mar 15, 1999: Dhav DHC8102 (N827EX), Syracuse, NY. (-5)On March 15, 1999, at 1626 EST, a Dehavilland, DHC-8-102, S/N390, N827EX, operated by allegheny airlines inc., returned to land on runway 32 at Syracuse… - [Incident 19990313016979I](https://openairdocs.org/incident/19990313016979I), Mar 13, 1999: Dhav DHC8102 (N816EX), Rochester, NY. (-5)On saturdy, March 13, 1999, at 1914 EST, a Dehavilland DHC-8-102, N816EX, flight 3944, operated by allegheny airlines, on departure from Rochester, new… - [Incident 19981217041429I](https://openairdocs.org/incident/19981217041429I), Dec 17, 1998: Dhav DHC8102 (N924HA), Charleston, WV, Minor damage. (-23)N924HA began to taxi from the crw gate area, where it had been parked overnight, and had two (2) us airways ramp personnel marshaling the aircraft. The… - [Incident 19980623017829I](https://openairdocs.org/incident/19980623017829I), Jun 23, 1998: Dhav DHC8102 (N816EX), Middletown, PA. Returned to MDT when landing gear was slow to retract. Hydraulic line was cracked. - [Incident 19980121004969I](https://openairdocs.org/incident/19980121004969I), Jan 21, 1998: Dhav DHC8102 (N819EX), Rochester, NY. Narrative: on Wednesday, January 21, 1998, a Dehavilland DHC-8-102, N819EX, s/n 016, operated by allegheny airlines, experienced an unsafe gear indication in… - [Incident 19970816028539I](https://openairdocs.org/incident/19970816028539I), Aug 16, 1997: Dhav DHC8102 (N922HA), Philadelphia, PA. Narrative: on August 16, 1997, piedmont airlines aircraft N922HA, experienced an uncommanded roll control disconnect when landing at phl. The disconnect was… - [Incident 19970716022789I](https://openairdocs.org/incident/19970716022789I), Jul 16, 1997: Dhav DHC8102 (N827EX), Albany, NY. Diverted to airport due smoke in cockpit. Removed and replaced auxiliary converter. - [Incident 19970114005099I](https://openairdocs.org/incident/19970114005099I), Jan 14, 1997: Dhav DHC8102 (N713M), Stuart, NY. Narrative: on climb out from utica, number one channel of the autopilot failed. Number two was engaged and programmed for 160 knot climb. During this climb,… - [Incident 19970110002309I](https://openairdocs.org/incident/19970110002309I), Jan 10, 1997: Dhav DHC8102 (N820EX), Binghamton, NY. Narrative: on 1/10/97 at 1713 EST a Dehavilland DHC-8 operated by allegheny airlines as flight 3925, landed at Broome county airport, Binghamton, NY after… - [Incident 19961228043909I](https://openairdocs.org/incident/19961228043909I), Dec 28, 1996: Dhav DHC8102 (N852MA), Lincoln, NE. Narrative: N852MA, a Dehavilland DHC-8, operating as northwest airlink flight 3223, departed Lincoln, NE enroute minneapolis, MN on 12/28/96. During climbout,… - [Incident 19961109040479I](https://openairdocs.org/incident/19961109040479I), Nov 9, 1996: Dhav DHC8102 (N861MA), Detroit, MI. Narrative: after departure from cmh mesaba 3082 experienced a "stuck" elevator and declared an emergency. The flight continued to dtw and landed without… - [Incident 19960918032839I](https://openairdocs.org/incident/19960918032839I), Sep 18, 1996: Dhav DHC8102 (N825EX), Syracuse, NY. Narrative: on September 18, 1996 at 0655 EDT, a Dehavilland DHC-8-102, N825EX, flight 3853, operated by allegheny commuter airlines, inc., during takeoff from… - [Incident 19960102002949I](https://openairdocs.org/incident/19960102002949I), Jan 2, 1996: Dhav DHC8102 (N865MA), Benton Harbor, MI. Narrative: flight crew reported that just shortly after rotation, the number 2 engine began to surge. Even with a power reduction the surging continued and was… - [Incident 19951013041289I](https://openairdocs.org/incident/19951013041289I), Oct 13, 1995: Dhav DHC8102 (N825EX), Middletown, PA. Narrative: on October 13, 1995, during an IFR scheduled flight from boston (bos) to Harrisburg (MDT), allegheny airlines flight 3714, a Dehavilland DHC-8, on a… - [Incident 19950209005489I](https://openairdocs.org/incident/19950209005489I), Feb 9, 1995: Dhav DHC8102 (N815EX), Middletown, PA. Narrative: the crew stated in cruise flight both main and aux. Battery temperature lights illuminated. The crew diverted to Middletown and made an uneventful… - [Incident 19950207003999I](https://openairdocs.org/incident/19950207003999I), Feb 7, 1995: Dhav DHC8102 (N820EX), Albany, NY. Narrative: after departing from Albany County Airport, crew tried to retract landing gear. Left main landing gear failed to retract. Crew manually extended the… - [Incident 19950203005499I](https://openairdocs.org/incident/19950203005499I), Feb 3, 1995: Dhav DHC8102 (N820EX), Middletown, PA. Narrative: pilot stated on takeoff #2 hydraulic pump light illuminated. The crew returned the aircraft to the airport and landed with no further incident.… - [Incident 19940512023069I](https://openairdocs.org/incident/19940512023069I), May 12, 1994: Dhav DHC8102 (N819EX), State College, PA. NR2 engine reverted to manual and lost power. Replaced electronic control unit. Torque sensor hydro unit. Fuel pump. - [Incident 19940511016549I](https://openairdocs.org/incident/19940511016549I), May 11, 1994: Dhav DHC8102 (N920HA), Lynchburg, VA. Fire warning NR1 engine. Shut engine down. Returned. No external fire noted. Found compressor turbine damage. - [Incident 19940407010039I](https://openairdocs.org/incident/19940407010039I), Apr 7, 1994: Dhav DHC8102 (N819EX), White Plains, NY. Oil pressure light on in flight. NR2 engine shutdown. Landed at White Plains. Replaced fuel control and pump. All 74: https://openairdocs.org/model/dehavilland-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/dehavilland-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/dehavilland-dhc-8-102/stcs.md ## PMA parts (OpenAirDocs) (532, 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 - [AAI- 150SG1070](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188895262520240320173348.0001): Friction Disc. Augusta Aero Innovations LLC · PMA PQ04441CE · Replaces 150SG1070 · Jan 31, 2024 - [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 - [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 - [103068-14](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167950019720230727204719.0001): Safety Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 103068-14 · Mar 8, 2022 - [2117804-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178024660420230724173959.0001): Computer. Honeywell International Inc. · PMA PQ1222NM · Replaces 2117804-1 · Feb 28, 2022 - [130522-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119790966720230724174001.0001): Cabin Pressure. Honeywell International Inc. · PMA PQ1222NM · Replaces 130522-1 · Feb 28, 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 - [AG728000-52](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169189394620220408135708.0001): Gasket – Satcom Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Jan 26, 2022 - [AG627000-23](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169325110020220408135638.0001): Gasket – Marker Beacon. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Dec 15, 2021 All of them: https://openairdocs.org/model/dehavilland-dhc-8-102/pma.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Boeing DHC-8-102](https://openairdocs.org/model/boeing-dhc-8-102): 3 registered aircraft, registry code 1386002 - [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 - [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.