# Bombardier DHC-8-103 - Type: Aircraft model (FAA registry) - Registry code: 1390003 - Manufacturer (registry): BOMBARDIER INC - Model: DHC-8-103 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-prop - Seats: 40 - Weight class: 12,500 to 19,999 lb - Certification: Type certificated - Data sheet: [TCDS A13NM](https://openairdocs.org/tcds/A13NM) (OpenAirDocs) - Holder: De Havilland Aircraft of Canada Limited - Registered aircraft: 0 - Page: https://openairdocs.org/model/bombardier-dhc-8-103 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 160: https://openairdocs.org/model/bombardier-dhc-8-103/ads.md ## Registered aircraft None registered with this model now. ## 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 NYC03LA004](https://openairdocs.org/ntsb/NYC03LA004), Oct 15, 2002: de Havilland DHC-8-102 (N847EX), Albany, NY, substantial damage. Probable cause: An in-flight collision with birds. A factor was the night conditions. ## 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. - [Accident 20021014026679A](https://openairdocs.org/incident/20021014026679A), Oct 14, 2002: Dhav DHC8102 (N847EX), Albany, NY, Substantial damage. (-23) A DHC-8 aircraft was enroute from dca to alb. 10 miles west of alb at 0015Z descending through 4,000FT MSL a flock of 10-15 geese were encountered. The… ## Service difficulty reports (844, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 2023FA0000593](https://openairdocs.org/sdr/2023FA0000593), Aug 29, 2023: INVERTER. FAILED. INVERTER PRODUCED BURNING SMELL AND FAILED. CREW DECLARED IFE AND EXECUTED PRECAUTIONARY LANDING. - [SDR 2023F00008](https://openairdocs.org/sdr/2023F00008), Dec 29, 2022: PUMP. FAULTED. #1 STBY HYD PUMP HOT LIGHT ILLUMINATED IN FLIGHT. REPLACED LH STBY JPUMP WITH REPAIRED UNIT. - [SDR 7C7A2022122980050](https://openairdocs.org/sdr/7C7A2022122980050), Dec 28, 2022: PUMP. OVERTEMP. #1 STBY HYD PUMP HOT LIGHT ILLUMINATED IN FLIGHT - [SDR 7C7A2022122000041](https://openairdocs.org/sdr/7C7A2022122000041), Dec 20, 2022: ANNUNCIATOR. INOPERATIVE. CHECK FIRE DET WARNING LIGHT WONT STAY LATCHED. R&R WARNING ANNUNCIATOR PANEL - [SDR 7C7A2022122000040](https://openairdocs.org/sdr/7C7A2022122000040), Dec 20, 2022: WARNING MESSAGE. ILLUMINATED. DURING CLIMB OUT OF ANC THE CHECK FIRE DTC LIGHT ON THE MASTER WARNING PANEL BECAME INOPERATIVE. THE CREW ATTEMPTED TO FIX THE PROBLEM WITH PROCEDURES ADVISED D - [SDR 7C7A2022120500032](https://openairdocs.org/sdr/7C7A2022120500032), Dec 1, 2022: FLIGHT RECORDER. FAULTED. FLT DATA RECORDER CAUTION LIGHT ILLUMINATED PRIOR TO TAKE OFF. - [SDR 7C7A2021100800019](https://openairdocs.org/sdr/7C7A2021100800019), Oct 8, 2021: NONE. NONE. FOUND LOOSE CANNON PLUG ON POWER SUPPLY 3352-PS1, 3351-PS3 AND 3351-PS4 TIGHTENED AS REQUIRED POWER DHC-8-100 AMM 33-51-00 OPS CHECK GOOD. NRW-23529 - [SDR 7C7A2020040100023](https://openairdocs.org/sdr/7C7A2020040100023), Mar 31, 2020: SKIN. DENTED. RIGHT WING, INBOARD FLIGHT SPOILER, UPPER SURFACE HAS 5 DENTS. - [SDR 7C7A2020032700021](https://openairdocs.org/sdr/7C7A2020032700021), Mar 27, 2020: SKIN. DEBONDED. LEFT INBOARD GROUND SPOILER ASSEMBLY (P/N 85770001-007) HAS DENT (7 ON UPPER SURFACE) AND DIS-BOND DAMAGE. - [SDR 7C7A2020032700020](https://openairdocs.org/sdr/7C7A2020032700020), Mar 26, 2020: SKIN. DEBONDED. LEFT INBOARD FLIGHT SPOILER ASSEMBLY (P/N 85770012-001) HAS DENT (4 ON LOWER SURFACE AND 11 ON UPPER SURFACE) AND DIS-BOND DAMAGE. - [SDR 7C7A2020032700019](https://openairdocs.org/sdr/7C7A2020032700019), Mar 26, 2020: FITTING. WORN. LEFT ELEVATOR TRIM TAB, INBOARD SIDE, DRIVE FITTING (P/N: 85520205) IS WORN. - [SDR 7C7A2020032700018](https://openairdocs.org/sdr/7C7A2020032700018), Mar 26, 2020: SKIN. DENTED. THREE DENTS WERE FOUND ON THE LEFT ELEVATOR SPRING TAB, UPPER SURFACE. - [SDR 7C7A2020032400011](https://openairdocs.org/sdr/7C7A2020032400011), Mar 24, 2020: SKIN. DEBONDED. MULTIPLE DENTS (23) AND DIS-BOND DAMAGE NOTED ON RIGHT WING INBOARD GROUND SPOILER UPPER SURFACE SKIN. - [SDR 7C7A2020032400015](https://openairdocs.org/sdr/7C7A2020032400015), Mar 23, 2020: SKIN. DEBONDED. MULTIPLE DENTS (1 ON UPPER SURFACE AND 2 ON LOWER SURFACE) AND DIS-BOND DAMAGE NOTED ON RIGHT WING, OUTBOARD FLIGHT SPOILER, SKIN. - [SDR 7C7A2020032400013](https://openairdocs.org/sdr/7C7A2020032400013), Mar 23, 2020: SKIN. DEBONDED. MULTIPLE DENTS (8) AND DIS-BOND DAMAGE NOTED ON LEFT WING, OUTBOARD GROUND SPOILER, SKIN UPPER SURFACE. - [SDR 7C7A2020032400012](https://openairdocs.org/sdr/7C7A2020032400012), Mar 23, 2020: SKIN. DEBONDED. MULTIPLE DENTS (8 UPPER SURFACE AND 1 LOWER SURFACE) AND DIS-BOND DAMAGE NOTED ON LEFT WING, OUTBOARD FLIGHT SPOILER, SKIN. - [SDR 7C7A2020032500016](https://openairdocs.org/sdr/7C7A2020032500016), Mar 19, 2020: SKIN. CRACKED. A SMALL (0.22 IN LONG) CRACK WAS FOUND ON THE LEFT ELEVATOR, UPPER SURFACE, INBOARD CORNER, ALONG TRAILING EDGE (P/N: 85520057) - [SDR 7C7A2020032400014](https://openairdocs.org/sdr/7C7A2020032400014), Mar 16, 2020: SHROUD. CHAFED. LEFT NACELLE, CENTER EXHAUST SHROUD, LOWER HALF HAS 2 CHAFED HOLES. - [SDR 7C7A2020032300003](https://openairdocs.org/sdr/7C7A2020032300003), Mar 13, 2020: SKIN. SCRATCHED. BAGGAGE DOOR, EXTERNAL SKIN, HAS 5 SCRATCHES ON IT. - [SDR 7C7A2020032700022](https://openairdocs.org/sdr/7C7A2020032700022), Mar 11, 2020: TAIL CONE. DAMAGED. FORWARD TAILCONE ASSEMBLY (P/N 85560061) HAS MULTIPLE AREAS OF BUBBLED PAINT AND SOFT COMPOSITE ALONG RIGHT SIDE OF FUSELAGE. - [SDR 7C7A2020032400010](https://openairdocs.org/sdr/7C7A2020032400010), Mar 11, 2020: FITTING. WORN. LEFT WING, INBOARD FLAP ASSEMBLY (P/N: 85750002-005), #2 TRACK FITTING HAS RUBBING-WEAR DAMAGE (P/N: 85750302). - [SDR 7C7A2020032600017](https://openairdocs.org/sdr/7C7A2020032600017), Mar 10, 2020: FIREWALL. CRACKED. LEFT NACELLE, INBOARD SIDE, LOWER SHEAR WEB (FIREWALL, P/N: 85410594-111) HAS A CRACK (0.550 INCHES LONG). - [SDR 7C7A2020032400008](https://openairdocs.org/sdr/7C7A2020032400008), Mar 10, 2020: SEAT TRACK. CORRODED. RIGHT OUTBOARD SEAT TRACK BETWEEN X445.50 AND X467.00 HAS CORROSION DAMAGE (P/N: 85330507). - [SDR 7C7A2020032300005](https://openairdocs.org/sdr/7C7A2020032300005), Mar 10, 2020: SKIN PANEL. GOUGED. SKIN PANEL ON LEFT SIDE OF FUSELAGE HAS A DENT WITH A GOUGE. X387.35-X405.737 AND STR. 30P-31P - [SDR 7C7A2020032300004](https://openairdocs.org/sdr/7C7A2020032300004), Mar 10, 2020: SKIN. GOUGED. FUSELAGE SKIN PANEL ON RIGHT SIDE HAS GOUGE DAMAGE. - [SDR 7C7A2020032400007](https://openairdocs.org/sdr/7C7A2020032400007), Mar 9, 2020: SEAT TRACK. DAMAGED. RIGHT OUTBOARD SEAT TRACK BETWEEN X270.50 AND X370.80 HAS PITTING AND GOUGE DAMAGE (P/N: 85320701). - [SDR 7C7A2020032300006](https://openairdocs.org/sdr/7C7A2020032300006), Mar 9, 2020: SHEAR WEB. CORRODED. CORROSION DAMAGE WAS NOTED ON AFT CENTER FUSELAGE LEFT SIDE SHEAR WEB (CARGO FLOOR). - [SDR 7C7A201906050507](https://openairdocs.org/sdr/7C7A201906050507), Jun 4, 2019: HANDLE. LOOSE. TESTING FUEL PULL OFF HANDLE, INTERMITTENTLY VALVE DOES NOT CLOSE AND/OR AFT EXTINGUISHER BOTTLE DOES NOT ARM. SECURED LOOSE T-HANDLE SWITCH PACK MOUNTING HARDW - [SDR 7C7A2019031300491](https://openairdocs.org/sdr/7C7A2019031300491), Mar 13, 2019: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHT INOPERABLE. BATTERY POWER SUPPLY REMOVED AND REPLACED REFERENCING 7H-NRW-6949 - [SDR 7C7A2018052400444](https://openairdocs.org/sdr/7C7A2018052400444), May 24, 2018: RELAY. HOT. ELECTRICAL SMELL COMING FROM CLOSET IN CABIN. - [SDR 7C7A2018040900392](https://openairdocs.org/sdr/7C7A2018040900392), Apr 11, 2018: SKIN. DENTED. PERMANENT REPAIR FOR 2 DENTS RT FUSELAGE SKIN PANEL BTW X240.5-X253.4 AND STR 31S-32S. COMPLETED WITH ECO 008.53-18.13 AND RD 8-53-15612. - [SDR 7C7A2018040900340](https://openairdocs.org/sdr/7C7A2018040900340), Apr 6, 2018: DOOR TRACK. CHAFED. CHAFE DAMAGE TO FWD CARGO DOOR TRACK PN:85230460, PERMANENT ALLOWANCE FOR CHAFE DAMAGE PROVIDED BY ECO 008.52-18.07 AND RD 8-52-1439. - [SDR 7C7A2018041900399](https://openairdocs.org/sdr/7C7A2018041900399), Apr 4, 2018: WINDOW FRAME. CORRODED. LEFT PASSENGER CABIN WINDOW FRAME AT BS 436.5 CORRODED BEYOND LIMITS. THE WINDOW FRAME WAS REPLACED IAW 51-42-05. - [SDR 7C7A2018041900398](https://openairdocs.org/sdr/7C7A2018041900398), Apr 4, 2018: WINDOW FRAME. CORRODED. LEFT PASSENGER CABIN WINDOW FRAME AT BS 396.74 FOUND CORRODED BEYOND LIMITS. REPLACED WINDOW FRAME IAW SRM 51-42-05. - [SDR 7C7A2018041900397](https://openairdocs.org/sdr/7C7A2018041900397), Apr 4, 2018: WINDOW FRAME. CORRODED. LEFT PASSENGER CABIN WINDOW FRAME AT BS 282.40 IS CORRODED BEYOND LIMITS. THE WINDOW FRAME REPLACED IAW SRM 51-42-05. - [SDR 7C7A2018040900388](https://openairdocs.org/sdr/7C7A2018040900388), Apr 2, 2018: SKIN. DENTED. 3 DENTS TO FORWARD LT FUSELAGE SKIN OF AIRCRAFT. STA X167-X182 BETWEEN STR 26P-27P. COMPLETED PERMANENT REPAIR WITH ECO 008.53-17.27 AND RD 8-53-15288. - [SDR 7C7A2018040900389](https://openairdocs.org/sdr/7C7A2018040900389), Mar 29, 2018: SKIN. DEBONDED. DISBOND DAMAGE TO CENTER FUSELAGE LOWER SKIN PN:85330022 BETWEEN X445.5-X488.5 AND STR. 31S-33. COMPLETED REPAIR WITH ECO 008.53-18.12 AND RD 8-53-15613. - [SDR 7C7A2018030700369](https://openairdocs.org/sdr/7C7A2018030700369), Mar 6, 2018: WARNING LIGHT. FALSE ACTIVATION. AFTER TAKEOFF, AND GEAR UP SELECTED, GEAR & GEAR DOOR LIGHTS WENT OUT THEN THE LT DOOR LIGHT ILLUMINATED. CYCLED THE GEAR DOWN THEN UP AND NO FURTHER LIGHT. - [SDR 7C7A2018013000358](https://openairdocs.org/sdr/7C7A2018013000358), Jan 27, 2018: BULB. INOPERATIVE. EMERGENCY LIGHT INOPERATIVE. REPLACED THE BULB. - [SDR 7C7A2017111300339](https://openairdocs.org/sdr/7C7A2017111300339), Nov 12, 2017: LIGHT. INOPERATIVE. FWD CENTER AISLE CABIN EMERGENCY LIGHT INOPERATIVE. - [SDR 7C7A201709020206](https://openairdocs.org/sdr/7C7A201709020206), Sep 1, 2017: BATTERY. DISCHARGED. MID CABIN EXIT AND EMERGENCY LIGHTS INOPERATIVE. FOUND THE BATTERY DISCHARGED. - [SDR HNAA2017030800081](https://openairdocs.org/sdr/HNAA2017030800081), Mar 8, 2017: BULB. INOPERATIVE. EMERGENCY EXIT LIGHT IS INOPERATIVE AT FORWARD RIGHT SIDE DOOR. REMOVED AND REPLACED THE BULBS. OPS CHECKED GOOD. - [SDR 7C7A2016062900248](https://openairdocs.org/sdr/7C7A2016062900248), Jun 29, 2016: PROXIMITY SENSOR. MALFUNCTIONED. NOSE LANDING GEAR NORMAL INDICATOR RED WITH GEAR EXTENDED AND HANDLE LIGHT ILLUMINATED. ALT GEAR INDICATOR LIGHTS ALL GREEN. PSEU MEMORY RECALL REVEALED NLG DOW - [SDR 7C7A201602140](https://openairdocs.org/sdr/7C7A201602140), Apr 2, 2016: BATTERY PACK. DISCHARGED. SOME EMERGENCY LIGHTING INOPERATIVE. - [SDR CA160107004](https://openairdocs.org/sdr/CA160107004), Jan 1, 2016: O-RING. CUT. (CAN) UPON MORNING REFUELING, ACFT LEAKING FUEL FROM REFUEL/DEFUEL SHROUD DRAIN ON AFT RT NACELLE. FUEL FOUND LEAKING ON EXHAUST PIPE IN WHEEL WELL AFTER REFUEL - [SDR CA160107003](https://openairdocs.org/sdr/CA160107003), Jan 1, 2016: FMU. FAILED. (CAN) NR 2 ENGINE FAILED TO START. EXTENSIVE TROUBLESHOOTING WAS CARRIED OUT BY MAINTENANCE. THE INITIAL FMU REPLACEMENT FAILED TO RECTIFY THE DEFECT. ULTIMATEL - [SDR CA160106015](https://openairdocs.org/sdr/CA160106015), Dec 30, 2015: BEARING. WORN. (CAN) NR 2 AC GENERATOR CHIP DETECTOR CODE 937 WAS RECEIVED. MAINTENANCE TROUBLESHOOTING WAS CARRIED OUT AND THE MATERIAL DISCOVERED INDICATED THAT THE AC GENER - [SDR 7C7A2015123028](https://openairdocs.org/sdr/7C7A2015123028), Dec 30, 2015: RUDDER. DENTED. REPAIR FOR DENT DAMAGE TO LOWER TRAILING RUDDER, PN 85540002 AN CAP0086. REPAIRED IAW ECO 008 55-15 06. - [SDR 7C7A2015123101](https://openairdocs.org/sdr/7C7A2015123101), Dec 30, 2015: RUDDER. DENTED. REPAIR FOR DENT DAMAGE TO LOWER TRAILING RUDDER, PN 85540002 AN CAP0086. REPAIRED IAW ECO 008 55 15 06. - [SDR CA151119003](https://openairdocs.org/sdr/CA151119003), Nov 17, 2015: ACTUATOR. FAULTED. (CAN) CREW REPORT THAT THEY HAD TO DO AN ALTERNATE GEAR EXTENTION AS THE NOSE DOORS DID NOT OPEN AND THE NOSE GEAR DID NOT EXTEND WHEN GEAR WAS SELECTED DOWN. T All 844: https://openairdocs.org/model/bombardier-dhc-8-103/reports.md ## STCs that may be installed (OpenAirDocs) (137, 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 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 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 All 137: https://openairdocs.org/model/bombardier-dhc-8-103/stcs.md ## PMA parts (OpenAirDocs) (517, 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/bombardier-dhc-8-103/pma.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Dehavilland DHC-8-103](https://openairdocs.org/model/dehavilland-dhc-8-103): 2 registered aircraft, registry code 2809006 - [Boeing / Dehavilland DHC-8-103](https://openairdocs.org/model/boeing-dehavilland-dhc-8-103): 0 registered aircraft, registry code 1386005 --- 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.