# Boeing / Dehavilland DHC-8-103

- Type: Aircraft model (FAA registry)
- Registry code: 1386005
- Manufacturer (registry): BOEING / DEHAVILLAND
- Model: DHC-8-103
- 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: 0
- Page: https://openairdocs.org/model/boeing-dehavilland-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/boeing-dehavilland-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 DCA12IA141](https://openairdocs.org/ntsb/DCA12IA141), Sep 5, 2012: De Havilland DHC8 (N886EA), Soldotna, AK, incident, no damage. Probable cause: an in-flight loss of control due to the flight crew's inattention to airspeed, pitch attitude, and engine power during the climb leading to an aerodynamic stall. Contributing to the incident was the…

## FAA accident and incident reports (3)

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 20120905023859I](https://openairdocs.org/incident/20120905023859I), Sep 5, 2012: Boeing / Dehavilland DHC-8-103 (N886EA), Anchorage, AK, Minor damage. Era 874, dash 8, departed ted stevens international airport, Anchorage, AK on a scheduled flight to homer, AK with 12 passengers and three crewmembers. The…
- [Incident 20111219028149I](https://openairdocs.org/incident/20111219028149I), Dec 19, 2011: Boeing / Dehavilland DHC-8-103 (N882EA), Fairbanks, AK, Minor damage. Ptrs number: AL07201201274DURING the deicing process the hageland (epua) contract deice truck operator was having issues with the trucks intercom system, got…
- [Incident 20030719016329I](https://openairdocs.org/incident/20030719016329I), Jul 19, 2003: Dhav DHC8103 (N882EA), Fairbanks, AK. (-23) 70 Knmi south of fai, aircraft began experiencing uncommanded radio transmissions causing interference with communications between ATC and all aircraft…

## 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/boeing-dehavilland-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/boeing-dehavilland-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/boeing-dehavilland-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
- [Bombardier DHC-8-103](https://openairdocs.org/model/bombardier-dhc-8-103): 0 registered aircraft, registry code 1390003

---
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