# Bombardier DHC-8-315

- Type: Aircraft model (FAA registry)
- Registry code: 1390043
- Manufacturer (registry): BOMBARDIER INC
- Model: DHC-8-315
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-prop
- Seats: 48
- 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: 15
- Page: https://openairdocs.org/model/bombardier-dhc-8-315

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2026-11-06](https://openairdocs.org/ad/2026-11-06): Hardware; Standard practices/structures · De Havilland Aircraft of Canada DHC-8-101, DHC-8-102, DHC-8-103 and 9 more. Effective Jul 9, 2026
- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2022-15-08](https://openairdocs.org/ad/2022-15-08): Information systems · Airbus A318-111, A318-112, A319-111 and 49 more. Effective Aug 12, 2022
- [AD 2021-19-11](https://openairdocs.org/ad/2021-19-11): Flight controls · De Havilland Aircraft of Canada DHC-8-102, DHC-8-103, DHC-8-106 and 8 more. Effective Nov 18, 2021
- [AD 2019-12-17](https://openairdocs.org/ad/2019-12-17): Stabilizers · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Aug 12, 2019
- [AD 2018-23-04](https://openairdocs.org/ad/2018-23-04): Engine Controls · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Mar 15, 2019
- [AD 2018-20-12](https://openairdocs.org/ad/2018-20-12): Ice and rain protection · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Nov 23, 2018
- [AD 2018-20-11](https://openairdocs.org/ad/2018-20-11): Doors · Bombardier DHC-8-301, DHC-8-311 and DHC-8-315. Effective Nov 23, 2018
- [AD 2017-15-11](https://openairdocs.org/ad/2017-15-11): Landing Gear · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Sep 5, 2017
- [AD 2017-08-02](https://openairdocs.org/ad/2017-08-02): Ignition · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective May 17, 2017
- [AD 2016-24-06](https://openairdocs.org/ad/2016-24-06): Ice and rain protection · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Jan 12, 2017
- [AD 2016-24-01](https://openairdocs.org/ad/2016-24-01): Electrical Power · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Dec 30, 2016
- [AD 2016-10-07](https://openairdocs.org/ad/2016-10-07): Electrical power · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Jun 23, 2016
- [AD 2015-21-02](https://openairdocs.org/ad/2015-21-02): Electrical Power · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Nov 24, 2015
- [AD 2015-14-03](https://openairdocs.org/ad/2015-14-03): Fuel · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Aug 21, 2015
- [AD 2015-04-08](https://openairdocs.org/ad/2015-04-08): Landing Gear · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Apr 27, 2015
- [AD 2013-15-06](https://openairdocs.org/ad/2013-15-06): Electrical Power · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Oct 20, 2014
- [AD 2014-15-07](https://openairdocs.org/ad/2014-15-07): Wings · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Sep 2, 2014
- [AD 2014-13-18](https://openairdocs.org/ad/2014-13-18): Instruments, Engine Controls · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Aug 19, 2014
- [AD 2014-05-17](https://openairdocs.org/ad/2014-05-17): Fuel · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective May 2, 2014
- [AD 2013-22-04](https://openairdocs.org/ad/2013-22-04): Flight controls · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 8 more. Effective Dec 5, 2013
- [AD 2013-14-09](https://openairdocs.org/ad/2013-14-09): Landing gear · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Sep 10, 2013
- [AD 2013-04-07](https://openairdocs.org/ad/2013-04-07): Electrical Power · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Apr 9, 2013
- [AD 2012-15-16](https://openairdocs.org/ad/2012-15-16): Landing gear · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 8 more. Effective Sep 12, 2012
- [AD 2012-04-08](https://openairdocs.org/ad/2012-04-08): Flight controls · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 8 more. Effective Apr 10, 2012
- [AD 2011-26-05](https://openairdocs.org/ad/2011-26-05): Wings · Bombardier DHC-8-301, DHC-8-311 and DHC-8-315. Effective Jan 23, 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 2010-19-02](https://openairdocs.org/ad/2010-19-02): Fuel · Bombardier DHC-8-201, DHC-8-202, DHC-8-301 and 2 more. Effective Oct 18, 2010
- [AD 2010-04-12](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 2006-07-02](https://openairdocs.org/ad/2006-07-02): Pressure control valve of the Type 1 emergency door · Bombardier DHC-8-301, DHC-8-311 and DHC-8-315. Effective May 4, 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

Historical (superseded or no longer in force):

- [AD 2019-20-03](https://openairdocs.org/ad/2019-20-03) (historical): Information systems · Airbus A340-312, A340-313, A318-111 and 48 more. Effective Nov 19, 2019
- [AD 2014-06-08](https://openairdocs.org/ad/2014-06-08) (historical): Landing gear · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Apr 14, 2014
- [AD 2012-14-04](https://openairdocs.org/ad/2012-14-04) (historical): Landing gear · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Aug 27, 2012
- [AD 2006-12-16](https://openairdocs.org/ad/2006-12-16) (historical): Structural testing of the cockpit door · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Jul 18, 2006
- [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996

All 147: https://openairdocs.org/model/bombardier-dhc-8-315/ads.md

## Registered aircraft (15)

- [N539AR](https://openairdocs.org/aircraft/N539AR): [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 539
- [N560WK](https://openairdocs.org/aircraft/N560WK): [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 560
- [N563AW](https://openairdocs.org/aircraft/N563AW): [US Department Of State](https://openairdocs.org/faa-owner/US%20DEPARTMENT%20OF%20STATE), [Melbourne, FL](https://openairdocs.org/faa-place/FL/Melbourne), S/N 563
- [N567WK](https://openairdocs.org/aircraft/N567WK): [US Dept Of State](https://openairdocs.org/faa-owner/US%20DEPT%20OF%20STATE), [Melbourne, FL](https://openairdocs.org/faa-place/FL/Melbourne), S/N 567
- [N568AW](https://openairdocs.org/aircraft/N568AW): [US Department Of State](https://openairdocs.org/faa-owner/US%20DEPARTMENT%20OF%20STATE), [Melbourne, FL](https://openairdocs.org/faa-place/FL/Melbourne), S/N 568
- [N569AW](https://openairdocs.org/aircraft/N569AW): [US Department Of State](https://openairdocs.org/faa-owner/US%20DEPARTMENT%20OF%20STATE), [Melbourne, FL](https://openairdocs.org/faa-place/FL/Melbourne), S/N 569
- [N570AW](https://openairdocs.org/aircraft/N570AW): [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 570
- [N580AR](https://openairdocs.org/aircraft/N580AR): [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 580
- [N589AW](https://openairdocs.org/aircraft/N589AW): [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 589
- [N599AR](https://openairdocs.org/aircraft/N599AR): [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 599
- [N800AW](https://openairdocs.org/aircraft/N800AW): [US Department Of State](https://openairdocs.org/faa-owner/US%20DEPARTMENT%20OF%20STATE), [Melbourne, FL](https://openairdocs.org/faa-place/FL/Melbourne), S/N 573
- [N804MR](https://openairdocs.org/aircraft/N804MR): [US Department Of Homeland Security](https://openairdocs.org/faa-owner/US%20DEPARTMENT%20OF%20HOMELAND%20SECURITY), [Washington, DC](https://openairdocs.org/faa-place/DC/Washington), S/N 374
- [N807MR](https://openairdocs.org/aircraft/N807MR): [US Department Of Homeland Security](https://openairdocs.org/faa-owner/US%20DEPARTMENT%20OF%20HOMELAND%20SECURITY), [Washington, DC](https://openairdocs.org/faa-place/DC/Washington), built 2009, S/N 663
- [N808MR](https://openairdocs.org/aircraft/N808MR): [US Department Of Homeland Security](https://openairdocs.org/faa-owner/US%20DEPARTMENT%20OF%20HOMELAND%20SECURITY), [Washington, DC](https://openairdocs.org/faa-place/DC/Washington), built 2009, S/N 667
- [N810MR](https://openairdocs.org/aircraft/N810MR): [US Department Of Homeland Security](https://openairdocs.org/faa-owner/US%20DEPARTMENT%20OF%20HOMELAND%20SECURITY), [Washington, DC](https://openairdocs.org/faa-place/DC/Washington), S/N 590

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA13CA008](https://openairdocs.org/ntsb/DCA13CA008), Oct 17, 2012: Bombardier DHC-8-315 (N800AW), Kabul, Afghanistan, substantial damage. Probable cause: the captains ineffective management of the airplanes energy state during final approach and flare that resulted in a hard landing and tail strike at touchdown.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20170224001749I](https://openairdocs.org/incident/20170224001749I), Feb 24, 2017: Bombardier Inc DHC-8-315 (N807MR), Fort Myers, FL, No damage. On February 24, 2017, at 11:10 EDT, a Bombardier, inc. DHC-8-315, N807MR, registered to "us department of homeland security" conducted an emergency evacuation…

## Service difficulty reports (124, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR 2023FA0000406](https://openairdocs.org/sdr/2023FA0000406), Aug 9, 2023: VALVE. UNRELIABLE. WITH #2 ENGINE RUNNING, PARKING BRAKE SET, WHILE STARING #1 ENGINE AIRCRAFT STARTED TO MOVE FORWARD MAKING CONTACT WITH GSE (TUG) ATTACHED TO STARTING POWER UNI
- [SDR 3SDR20210216006](https://openairdocs.org/sdr/3SDR20210216006), Jan 15, 2021: STICK SHAKER. FAULTED. DURING FLIGHT, STICK PUSHER DID NOT ACTIVATE AND DID NOT GIVE ANY INDICATION OF A SYSTEM FAILURE.
- [SDR K08R202010290001](https://openairdocs.org/sdr/K08R202010290001), Oct 29, 2020: TSCU. MALFUNCTIONED. A SCHEDULED FLIGHT, THE FLIGHT CREW HAD ENGINES OPERATING AND GOING THROUGH THEIR GROUND CHECKS WHEN THEY HAD THE NR 1 ENGINE FEATHERING DURING AUTO-FEATHER CHE
- [SDR CA190806001](https://openairdocs.org/sdr/CA190806001), Aug 5, 2019: WIRE. SHORTED. (CAN) #1 AC GENERATOR FAILED IN FLIGHT. RESET CONDUCTED AND DID NOT WORK. GCU CHANGED. GENERATOR ALSO CHANGED.TEST OK THEN FAILED ON SUBSEQUENT START. FURTHER T
- [SDR CA191115005](https://openairdocs.org/sdr/CA191115005), Aug 4, 2019: WIRE. DAMAGED. (CAN) FROM PILOT REPORT - DURING FLARE ON LANDING, ELEVATORS JAMMED AND THE AIRCRAFT WAS NOT ABLE TO BE PITCHED UPWARDS OF 2-3 DEGREES. AIRCRAFT TOUCHED DOWN AT
- [SDR CA190725002](https://openairdocs.org/sdr/CA190725002), Jul 18, 2019: BLADE. DAMAGED. (CAN) AIRCRAFT CLIMBED TO INITIAL CRUISE AT FL190 BUT ENCOUNTERED ICING. ICING WAS BEING SHED NORMALLY BUT CREW ELECTED TO CLIMB TO AVOID IT. AS THEY CLIMBED TH
- [SDR V0XR20190723001](https://openairdocs.org/sdr/V0XR20190723001), May 22, 2019: CHANNEL. CORRODED. PAX DOOR SILL BELOW FLOOR HAVE SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED THRESHOLD CHANNEL IAW SRM 51-42-05, 51-42-45, 51-40-07, AMM 20-30-06 
- [SDR CA190628009](https://openairdocs.org/sdr/CA190628009), Apr 30, 2019: ENGINE. DETERIORATED. (CAN) AIRCRAFT REPORTED STALL/SURGE AROUND 60-70% DURING ACCELERATION AND DECELERATION. PILOTS REPORTED THE DEFECT ON THE#1 ENGINE, HOWEVER UPON INVESTIGATION T
- [SDR CA190409001](https://openairdocs.org/sdr/CA190409001), Mar 10, 2019: TIRE. FAILED. (CAN) REPETITIVE DOUBLE TIRE FAILURES WITH DR26222T TIRE INSTALLED. WHILE TAXING TO THE RUNWAY FOR TAKEOFF, BOTH LEFT MAIN WHEELS FAILED(NO 1 TIRE DEFLATED AND 
- [SDR CA190226003](https://openairdocs.org/sdr/CA190226003), Feb 26, 2019: LINE. LEAKING. (CAN) TOTAL LOSS OF FLUID FROM #1 HYDRAULIC SYSTEM DURING CRUISE. AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE. (SEE ALSO CASA SDR #2019611953376/611953376) (T
- [SDR CA190226011](https://openairdocs.org/sdr/CA190226011), Feb 22, 2019: INVERTER. FAILED. (CAN) PILOT REPORTED : SMOKE SMELL IN THE COCKPIT, AND WE FOUND THAT THE SOURCE OF THE SMELL WAS THE PRIMARY INVERTER. WE CURRENTLY DO NOT HAVE ACCESS TO A SERV
- [SDR CA181119017](https://openairdocs.org/sdr/CA181119017), Nov 15, 2018: STRUT. DISCHARGED. (CAN) ON APPROACH, THE AIRCRAFT NOSE LANDING GEAR FAILED TO EXTEND UNDER NORMAL OR ALTERNATE EXTENSION. DUE TO WEATHER AND RUNWAY CONDITIONS THE AIRCRAFT THEN P
- [SDR CA180208004](https://openairdocs.org/sdr/CA180208004), Feb 1, 2018: TRANSDUCER. FAULTY. (CAN) PILOT CARRIED OUT NR 2 ENG SHUTDOWN DUE TO LOW OIL PRESSURE INDICATION DEFECT, WAS FIXED BY REPLACING THE TRANSDUCER. THE PINS APPEARED TO BE STAINED/CONT
- [SDR CA160203011](https://openairdocs.org/sdr/CA160203011), Jan 25, 2016: ENGINE. MALFUNCTIONED. (CAN) WHILE STARTING THE ENGINES WITH INTENT TO PERFORM A TEST FLIGHT, FOLLOWING THE 500 HRS INSPECTION REQUIREMENTS, ON SELECTION OF BLEEDS TO MAX., A STRONG O
- [SDR CA151216002](https://openairdocs.org/sdr/CA151216002), Dec 2, 2015: WARNING LIGHT. ILLUMINATED. (CAN) CUSTOMER REPORTED A FUEL BY-PASS INDICATION IN COCKPIT AND POWER FLUCTUATIONS. THE CREW ELECTED TO PERFORM A COMMANDED IFSD.
- [SDR CA151130020](https://openairdocs.org/sdr/CA151130020), Nov 19, 2015: UNKNOWN. ODOR. (CAN) DURING CLIMB PASSING 2,800, AS THE BLEEDS WERE TURNED ON, AN OIL ODOR IN THE COCKPIT. THE CREW CONTINUED THE CLIMB TO 8,000, BLEEDS WERE TURNED OFF AND TH
- [SDR CA151030004](https://openairdocs.org/sdr/CA151030004), Oct 19, 2015: COMPRESSOR. CONTAMINATED. (CAN) THIS ENGINE HAS HAD REPEAT EVENTS OF OIL ODOR IN CABIN, THE 1ST EVENT TROUBLESHOOTING IDENTIFIED OIL AROUND THE HIGH PRESSURE COMPRESSOR. MAINTENANCE ACTI
- [SDR CA151006003](https://openairdocs.org/sdr/CA151006003), Sep 21, 2015: UNKNOWN. ODOR. (CAN) OIL ODOR IN THE CABIN OCCURRED ON CLIMBOUT FROM TRANSIENT ALTITUDE. ALL CREW MEMBERS WENT ON OXYGEN TO THE DESTINATION. ACFT LANDED UNEVENTFULLY. TROUBLES
- [SDR CA150828004](https://openairdocs.org/sdr/CA150828004), Jul 7, 2015: BLADES. MISSING. (CAN) CUSTOMER JUST REPORTED THAT THEY HAD IFSD EVENT ON NR 2 ENGINE DURING CRUISE. ENGINE WAS SENT FOR HSI & INVESTIGATION. HEAVY DAMAGES WERE FOUND IN HOT SEC
- [SDR CA150629006](https://openairdocs.org/sdr/CA150629006), Jun 19, 2015: ENGINE. ODOR. (CAN) WHILE ON A SURVEILLANCE MISSION, SURVEILLANCE CREW REPORTED INTERMITTENT OIL SMELL IN THE CABIN WITH CRUISE POWER AT 60% TORQUE. PILOTS WERE NOTIFIED & PO
- [SDR CA150519008](https://openairdocs.org/sdr/CA150519008), Apr 30, 2015: OIL SYSTEM. ODOR. (CAN) THE CREW EXPERIENCED AN OIL SMELL IN CABIN EVENT. THE EVENT OCCURRED PRIOR TO TAKEOFF, WHEN THE ENG POWER LEVER WAS MOVED FROM BELOW FLIGHT IDLE INTO DISK
- [SDR 2015FA0000147](https://openairdocs.org/sdr/2015FA0000147), Apr 17, 2015: COLLAR. CRACKED. DURING VISUAL INSPECTION OF LT NACELLE HORSE COLLAR ASSY FOUND A 1.1250 CRACK DAMAGE ON FORWARD OUTER ANGLE, DAMAGE CRACK WAS REPORTED TO MFG HELP DESK. MFG PRO
- [SDR 2015FA0000153](https://openairdocs.org/sdr/2015FA0000153), Mar 12, 2015: ANGLE. CRACKED. DURING ENGINE REMOVAL FOR HSI AN INSPECTION OF THE NACELLE AREA WAS CONDUCTED PER THE OEM, WE NOTICED BOTH LEFT AND RIGHT ENGINE FRONT NACELLE HORSE COLLAR LOWE
- [SDR 2015FA0000152](https://openairdocs.org/sdr/2015FA0000152), Feb 28, 2015: ANGLE. CRACKED. DURING ENGINE CHANGE AND INSPECTION OF THE NACELLE AREA NOTICED A ONE INCH CRACK ON THE HORSE COLLAR BOTTOM LEFT SIDE AT THE OUTER ANGEL OF THE ENGINE NACELLE H
- [SDR CA150217008](https://openairdocs.org/sdr/CA150217008), Feb 14, 2015: WARNING LIGHT. ILLUMINATED. (CAN) DIVERSION DUE TO NR 2 HYD PUMP CAUTION LIGHT ILLUMINATED.
- [SDR CA150109005](https://openairdocs.org/sdr/CA150109005), Jan 8, 2015: OUTFLOW VALVE. FAILED. (CAN) INITIAL REPORT INDICATED PRESSURIZATION SYSTEM WAS NOT WORKING AND CABIN WAS TOO COLD. NO CONTROL WITH AUTO OR MAN. NO FAULT INDICATION. TEMPORARY CONTROL
- [SDR CA141229011](https://openairdocs.org/sdr/CA141229011), Dec 28, 2014: PITOT TUBE. CRACKED. (CAN) FLIGHT DIVERTED DUE TO ROLL OB SPOILER CAUTION LIGHT. MAINTENANCE FOUND THAT BOTH PITOT ACCUMULATORS WERE FULL TO THE TOP WITH WATER. CARRIED OUT A LEAK C
- [SDR CA141229009](https://openairdocs.org/sdr/CA141229009), Dec 28, 2014: ENGINE. MAKING METAL. (CAN) CAPTAIN REPORTED SMOKE IN THE FLIGHT DECK AND DIVERTED, NO INCIDENTS UPON LANDING. MAINTENANCE PERSONNEL AFTER INVESTIGATION FOUND CODE 939 RGB CHIP DETEC
- [SDR CA141229007](https://openairdocs.org/sdr/CA141229007), Dec 24, 2014: PUSHROD. DISCONNECTED. (CAN) FOLLOWING TAKEOFF, THE LH FWD MLG DOOR DID NOT CLOSE. THERE WAS NO FLIGHT DECK INDICATION BUT THE DOOR WAS VISUALLY CONFIRMED TO BE OPEN. THE AIRCRAFT RET
- [SDR CA141223003](https://openairdocs.org/sdr/CA141223003), Dec 22, 2014: PUMP. LEAKING. (CAN) FLIGHT CREW CARRIED OUT AN INFLIGHT TURN AROUND DUE TO NR 1 HYDRAULIC ISOLATION CAUTION LIGHT ILLUMINATED AFTER DEPARTURE, NR 1 HYDRAULIC QUANTITY INDICAT
- [SDR CA141211001](https://openairdocs.org/sdr/CA141211001), Dec 10, 2014: COFFEEMAKER. OVERHEATED. (CAN) IN CRUISE FLIGHT THE FA REPORTED A SMOKE SMELL FROM THE GALLEY AREA. THE GALLEY CB WERE PULLED & THE SMELL DISSIPATED. THE AIRCRAFT CONTINUED TO DESTINATI
- [SDR CA141211003](https://openairdocs.org/sdr/CA141211003), Dec 9, 2014: UNION. LEAKING. (CAN) HYDRAULIC FLUID WAS NOTED ON THE AIRCRAFT IN THE VICINITY OF THE NOSE LANDING GEAR. MAINTENANCE INSPECTION CONFIRMED THAT THE LEAK WAS COMING FROM THE NLG
- [SDR CA150113011](https://openairdocs.org/sdr/CA150113011), Dec 5, 2014: ENGINE. POWER LOSS. (CAN) THE NR 2 ENGINE WAS NOT ABLE TO DEVELOP POWER ON TAKEOFF ROLL. MAXIMUM OF 45 PERCENT TORQUE ACHIEVEABLE. TAKEOFF ABORTED AND ACFT RETURNED TO RAMP. MFC AN
- [SDR CA141210003](https://openairdocs.org/sdr/CA141210003), Dec 4, 2014: PIN. GROUNDED. (CAN) WHILE CLIMBING FLIGHT CREW RECEIVED A NR 2 AC BUSS CAUTION LIGHT THROUGH ABOUT FL 240, AND THEN THE RH AC BUS CAUTION LIGHT ALSO CAME ON. FLIGHT CREW COMP
- [SDR CA141125002](https://openairdocs.org/sdr/CA141125002), Nov 24, 2014: SHUTOFF VALVE. UNKNOWN. (CAN) DURING CLIMB THROUGH FL 130 CREW ENCOUNTERED PRESSURIZATION PROBLEM. AT ONE POINT PRESSURIZATION SEEMED STABILIZED BUT CABIN STARTED TO RISE AGAIN. AIRCRA
- [SDR CA141008015](https://openairdocs.org/sdr/CA141008015), Sep 30, 2014: ENGINE. ODOR. (CAN) WHILE ON A NON-REVENUE FLIGHT (NO PASSENGERS)Ï¿½THE LAV SMOKE DETECTOR SOUNDED WITH NO SMOKE OR ODOR APPARENT TO THE FLIGHT CREW. MAINTENANCE INVESTIGATED
- [SDR CA141010002](https://openairdocs.org/sdr/CA141010002), Sep 20, 2014: ENGINE. LEAKING. THE ACFT DEPARTED, JUST AFTER ROTATION THE COCKPIT AND CABIN WERE FILLED WITH SMOKE, AN EMERGENCY WAS DECLARED AND THE ACFT EVACUATED ON THE RAMP. THE ACFT WAS 
- [SDR CA140922010](https://openairdocs.org/sdr/CA140922010), Sep 20, 2014: ACM. FAILED. (CAN) AIRCRAFT EXPERIENCED SMOKE IN THE CABIN AND COCKPIT IMMEDIATELY UPON TAKEOFF FROM THE AIRPORT. AN INSPECTION OF THE AIRCRAFT AND SYSTEMS DETERMINED THAT T
- [SDR CA141212008](https://openairdocs.org/sdr/CA141212008), Jun 25, 2014: BRACKET. CRACKED. (CAN) BRACKET FOUND CRACKED.
- [SDR CA140630004](https://openairdocs.org/sdr/CA140630004), Jun 15, 2014: AUTOFEATHER SYS. MALFUNCTIONED. (CAN) DURING TAKEOFF ROLL, THE AUTOFEATHER SYS DID NOT ARM UPON SETTING TAKEOFF POWER. THE TAKEOFF WAS ABORTED AND THE ACFT RETURNED TO THE GATE. TROUBLESHOOTIN
- [SDR 2014FA0000318](https://openairdocs.org/sdr/2014FA0000318), May 14, 2014: STRINGER. CRACKED. INSPECTED ACFT AND FOUND NO CRACKS IN THE FS 222.0 AND 252.30 OUTSIDE SKIN, FOUND THE FORWARD AND AFT STRINGERS IN THE INTERNAL STRUCTURE THAT SUPPORTS THE ANTE
- [SDR 2014FA0000317](https://openairdocs.org/sdr/2014FA0000317), May 14, 2014: STRINGER. CRACKED. A POSSIBLE PRESSURIZATION ISSUE, INSPECTED THE VHF ANTENNA FOR POSSIBLE EXTERNAL SKIN CRACKS IN THE PRESSURE VESSEL AND FOUND NO CRACKS IN THE BS 222 - 252.3 OU
- [SDR 2014FA0000316](https://openairdocs.org/sdr/2014FA0000316), May 14, 2014: SKIN. CRACKED. ACFT EXPERIENCED PRESSURIZATION PROBLEM, MECHANIC CHECKED FUSELAGE DRAIN SEAL UNDER THE BELLY, DISCOVERED A LARGE CRACK IN THE SKIN BETWEEN BS 222 - 252.3. ALSO
- [SDR 2014FA0000315](https://openairdocs.org/sdr/2014FA0000315), May 14, 2014: STRINGER. CRACKED. POSSIBLE PRESSURIZATION ISSUE ON ACFT, INSPECTED THE VHF ANTENNA FOR POSSIBLE EXTERNAL SKIN CRACKS IN THE PRESSURE VESSEL, FOUND NO CRACKS IN THE OUTSIDE SKIN B
- [SDR CA140211007](https://openairdocs.org/sdr/CA140211007), Feb 1, 2014: STARTER GEN. SHORTED. (CAN) DURING MAINTENANCE TROUBLESHOOTING OF APU GENERATOR DEFECT THE STARTER/GENERATOR DEVELOPED AN INTERNAL SHORT OVERHEATED AND CAUGHT FIRE. THE FIRE WAS EXTI
- [SDR CA140109005](https://openairdocs.org/sdr/CA140109005), Jan 3, 2014: CHECK VALVE. LEAKING. (CAN) WHILE ON THE GROUND AT THE AIRPORT TERMINAL THE FLIGHT CREW STARTED THE ENGINES AND NOTICED THAT THE NR 2 HYDRAULIC SYS FLUID HAD DEPLETED. THE RELATED HY
- [SDR CA130909010](https://openairdocs.org/sdr/CA130909010), Sep 5, 2013: PROPELLER. LEAKING. (CAN) DURING ACFT TURN-AROUND FLIGHT CREW NOTICED LARGE AMOUNT OF ENGINE OIL AROUND THE LT PROPELLER & FWD ENGINE COWLS. SUBSEQUENT INVESTIGATION BY MAINTENANCE
- [SDR CA130705002](https://openairdocs.org/sdr/CA130705002), Jul 4, 2013: ROTOR. BROKEN. (CAN) DURING A WHEEL ASSEMBLY REPLACEMENT THE AME FOUND NR 3 & NR 4 BRAKE ASSY ROTATIONAL DISKS, ROTOR, BROKEN, NR 3 HAD 2 AND NR 4 HAD 1 BROKEN DISK. BRAKE ASS
- [SDR CA130416010](https://openairdocs.org/sdr/CA130416010), Apr 3, 2013: OIL SYSTEM. LOW PRESSURE. (CAN) DURING REVENUE FLIGHT, THE ACFT WAS IN CLIMB WHEN PILOTS GOT A LOW OIL PRESSURE WARNING FOLLOWED BY A DROP IN OIL PRESSURE ON THE INDICATOR. WHEN THE PRES
- [SDR CA130404006](https://openairdocs.org/sdr/CA130404006), Apr 2, 2013: OIL SYSTEM. LEAKING. (CAN) IN CLIMB, THROUGH 15,000 FT CREW GOT NR 2 ENG OIL PRESSURE MASTER CAUTION ANNUNCIATOR. THEY OPERATED AT FLIGHT IDLE IAW QRH UNTIL OIL PRESSURE STARTED TO 

All 124: https://openairdocs.org/model/bombardier-dhc-8-315/reports.md

## STCs that may be installed (OpenAirDocs) (130, 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 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 ST03224NY](https://openairdocs.org/stc/ST03224NY): Replacement of existing flight data recording systems with new Mini Flight Data Acquisition Unit (MFDAU) and Flight Data Recorder, sensors and wiring capable of recording 57 parameters. KGB Aviation Solutions LLC
- [STC ST02050NY](https://openairdocs.org/stc/ST02050NY): Installation of U.S. Customs Special Mission Modifications. Field Aviation East Limited
- [STC ST03795NY](https://openairdocs.org/stc/ST03795NY): Installation of the TB44 Lithium-Ion Battery System. Avmax Aviation Services Inc
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST01909NY](https://openairdocs.org/stc/ST01909NY): Installation of Hawker 9750W0370-6 (24V 43Ah) sealed lead-acid batteries. Securaplane Technologies Inc
- [STC 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 ST00388BO](https://openairdocs.org/stc/ST00388BO): Installation of a Night Vision Imaging System (NVIS). ATI Engineering Services LLC
- [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 ST03354NY](https://openairdocs.org/stc/ST03354NY): Installation of the Dual Auxiliary Air Condintioning system. Field Aviation Company Inc
- [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 SA1000NE](https://openairdocs.org/stc/SA1000NE): Installation of a Sundstrand Turbomach T-62T-40C7B gas turbine auxiliary power unit with a Lear Siegler Model 23088-002 DC starter-generator. Avmax Aviation Services Inc
- [STC ST01689WI](https://openairdocs.org/stc/ST01689WI): Installation of Crane Aerospace & Electronics SmartStem Wireless Tire Pressure Sensing System. ELDEC Corporation
- [STC SA1220NW](https://openairdocs.org/stc/SA1220NW): Installation of Universal flight data recorder. Honeywell International Inc
- [STC ST04667NY](https://openairdocs.org/stc/ST04667NY): Installation of the Honeywell MK VIII Enhanced Ground Proximity Warning System (EGPWS) Override Control. Field Aviation East Limited
- [STC 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 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 ST04372NY](https://openairdocs.org/stc/ST04372NY): Installation of saf-Tglo® SSUL23 Photoluminescent Aisle Path Marking System. STG Aerospace Ltd
- [STC ST01900WI](https://openairdocs.org/stc/ST01900WI): Heated (LH) Side Canopy Window Assembly replacement installation. Lee Aerospace Inc
- [STC ST04344NY](https://openairdocs.org/stc/ST04344NY): Installation of the Universal Avionics EFI-890R MFD. Avmax Aviation Services Inc
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST09015SC](https://openairdocs.org/stc/ST09015SC): Installation of a C & X band fuselage nose radome shell. The NORDAM Group LLC
- [STC ST04324NY](https://openairdocs.org/stc/ST04324NY): Installation of the Honeywell Solid State Cockpit Voice Recorder (SSVR) system. Avmax Aviation Services Inc
- [STC ST09858AC](https://openairdocs.org/stc/ST09858AC): Replacement of certain OEM pneumatic deicer boots. SMR Technologies Inc

All 130: https://openairdocs.org/model/bombardier-dhc-8-315/stcs.md

## PMA parts (OpenAirDocs) (450, 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
- [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
- [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
- [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
- [AG627000-12](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID175486155620220408140223.0001): Gasket – Marker Beacon Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 17, 2021
- [AG358000-08](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID114261030820220408135752.0001): Gasket – ELT Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 17, 2021
- [RS24-350](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192110452120260311205438.0001): Remote Switch. Chelton Avionics Inc. dba Canyon Aeroconnect · PMA PQ2204NM · Replaces RS24-350 · Nov 1, 2021
- [10-900-59/1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID987843753220211209184153.0001): Static Discharger. Specmat Technologies, Inc · PMA PQ1365CE · Replaces TCO ManufacturingDD2 · Sep 15, 2021
- [10-900-60/1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID198566103520211209184154.0001): Static Discharger. Specmat Technologies, Inc · PMA PQ1365CE · Replaces TCO ManufacturingTIDI · Sep 15, 2021
- [1104-4000-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID863506262720210713125924.0001): Interface Unit, GDC64, Tablet to Aircraft Interface Unit (TAIU). DAC International · PMA PQ05446NM · Modification part · Feb 3, 2021
- [AG846000-31](https://drs.faa.gov/browse/excelExternalWindow/92A601E0B1E952A3862585BB0036FCDE.0001): Gasket - VHF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Aug 2, 2020
- [032220-01-A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166122143020260608173221.0001): Hot Jug. Aereos Interior Solutions LLC · PMA PQ03905SW · Replaces 180-140 · Jun 15, 2020
- [032220-01-2-A](https://drs.faa.gov/browse/excelExternalWindow/E02B454D1EE554878625859F00383E74.0001): Hot Jug. Aeros Interior Solutions · PMA PQ3892SW · Replaces 180-140 · Jun 14, 2020
- [SP3558-51-1450](https://drs.faa.gov/browse/excelExternalWindow/2303B92B6268F03A86258570004EAB4A.0001): Gasket, Dilution. Soundair Aviation Services · PMA PQ2540NM · Replaces 553008 · Oct 16, 2019

All of them: https://openairdocs.org/model/bombardier-dhc-8-315/pma.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Dehavilland DHC-8-315](https://openairdocs.org/model/dehavilland-dhc-8-315): 2 registered aircraft, registry code 2809010
- [Boeing Of Canada/Dehav Div DHC-8-315](https://openairdocs.org/model/boeing-of-canada-dehav-div-dhc-8-315): 0 registered aircraft, registry code 1386107

---
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.