# Dehavilland DHC-8-101

- Type: Aircraft model (FAA registry)
- Registry code: 2809002
- Manufacturer (registry): DEHAVILLAND
- Model: DHC-8-101
- 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/dehavilland-dhc-8-101

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 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 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 2011-09-12](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 2010-04-12](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 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 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 2007-01-11](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 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 2004-24-03](https://openairdocs.org/ad/2004-24-03): Internal o-ring seal · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 23 more. Effective Jan 3, 2005
- [AD 2004-20-03](https://openairdocs.org/ad/2004-20-03): Wing leading edge de-icer boots · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Nov 3, 2004
- [AD 2004-15-09](https://openairdocs.org/ad/2004-15-09): Auxiliary power unit (APU) · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Aug 31, 2004
- [AD 2004-09-31](https://openairdocs.org/ad/2004-09-31): Engine Oil Coolers · Replace core assembly of Janitrol Engine Oil Cooler, part… (Honeywell International STC SA8937SW). Effective Jun 15, 2004
- [AD 2002-16-10](https://openairdocs.org/ad/2002-16-10): Airstair (main passenger) door · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Sep 26, 2002
- [AD 2002-12-11](https://openairdocs.org/ad/2002-12-11): Hook Roller Shafts · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Jul 31, 2002
- [AD 2002-06-06](https://openairdocs.org/ad/2002-06-06): Rockwell Collins TDR-94 and TDR-94D Mode S transponders · Bombardier ATR42-200, ATR42-300, ATR42-320 and 20 more. Effective May 3, 2002
- [AD 2002-01-25](https://openairdocs.org/ad/2002-01-25): Rudder Pedal Adjustment Fittings · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Mar 6, 2002
- [AD 2001-24-06](https://openairdocs.org/ad/2001-24-06): Oil Pump Pressure Regulating Valve · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Jan 4, 2002
- [AD 2001-17-23](https://openairdocs.org/ad/2001-17-23): Upper Wing Ladder Plates · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Oct 3, 2001
- [AD 2001-15-17](https://openairdocs.org/ad/2001-15-17): Transponder Control Panels · Bombardier ATR42-200, ATR42-300, ATR42-320 and 30 more. Effective Aug 20, 2001
- [AD 2001-10-05](https://openairdocs.org/ad/2001-10-05): Foam Filters · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Jun 22, 2001
- [AD 2001-06-13](https://openairdocs.org/ad/2001-06-13): Main Landing Gear Selector Valve · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective May 7, 2001
- [AD 2001-04-02](https://openairdocs.org/ad/2001-04-02): Wiggins Fuel Couplers · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Mar 28, 2001
- [AD 2000-16-03](https://openairdocs.org/ad/2000-16-03): Weight and Balance Check · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 10 more. Effective Sep 21, 2000
- [AD 2000-11-20](https://openairdocs.org/ad/2000-11-20): Bonded Skin Panels · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 4 more. Effective Jul 18, 2000
- [AD 2000-07-23](https://openairdocs.org/ad/2000-07-23): Power Supply for the Thunderstorm Lights · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 1 more. Effective May 19, 2000
- [AD 2000-02-06](https://openairdocs.org/ad/2000-02-06): Beta Back-Up Test Switches of the Propeller Control System · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Feb 16, 2000
- [AD 2000-01-07](https://openairdocs.org/ad/2000-01-07): Horizontal Stabilizer · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Jan 27, 2000
- [AD 99-19-18](https://openairdocs.org/ad/99-19-18): AFM - Limitations Section - Ice Protection Sys. · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 14 more. Effective Dec 27, 1999
- [AD 99-23-05](https://openairdocs.org/ad/99-23-05): Inspect Wing Ladder Plates for Cracks · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Dec 17, 1999
- [AD 99-19-37](https://openairdocs.org/ad/99-19-37): Uplock Actuator · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 4 more. Effective Oct 27, 1999
- [AD 99-19-34](https://openairdocs.org/ad/99-19-34): Hydraulic System Components · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 4 more. Effective Oct 27, 1999
- [AD 99-17-14](https://openairdocs.org/ad/99-17-14): Rudder Control Feel Unit · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 9 more. Effective Sep 24, 1999
- [AD 98-25-09](https://openairdocs.org/ad/98-25-09): MLG Brake Shuttle Valves · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 11 more. Effective Jan 14, 1999
- [AD 98-24-18](https://openairdocs.org/ad/98-24-18): Inspect Skin Panels of Horizontal Stabilizer · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 4 more. Effective Dec 8, 1998
- [AD 98-20-19](https://openairdocs.org/ad/98-20-19): Inspect Fuselage Structure for Corrosion · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 4 more. Effective Oct 28, 1998
- [AD 98-20-23](https://openairdocs.org/ad/98-20-23): Inspect Electrical Wiring Behind Lavatory · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Oct 27, 1998
- [AD 97-20-10 R1](https://openairdocs.org/ad/97-20-10-R1): Modification of the attitude and heading reference systems (AHRS) · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Sep 11, 1998
- [AD 98-14-04](https://openairdocs.org/ad/98-14-04): Lever Assembly of Roll Disconnect System · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Aug 5, 1998
- [AD 98-06-11](https://openairdocs.org/ad/98-06-11): Cabin/Baggage Compartment Bulkheads Block Seals · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 1 more. Effective Apr 17, 1998
- [AD 97-25-14](https://openairdocs.org/ad/97-25-14): Refuel/Defuel Tube Assemblies · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 6 more. Effective Jan 14, 1998
- [AD 97-13-08](https://openairdocs.org/ad/97-13-08): Low Fuel Pressure Switch · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 4 more. Effective Jul 30, 1997
- [AD 97-04-15](https://openairdocs.org/ad/97-04-15): Fire Extinguisher Bottle Cartridges · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 24 more. Effective Mar 7, 1997
- [AD 96-25-12](https://openairdocs.org/ad/96-25-12): Auxiliary Power Units · BAE Systems HS 748 Series 2A, HS 748 Series 2B, 707-100 Long Body and 74 more. Effective Jan 13, 1997
- [AD 95-26-15 R1](https://openairdocs.org/ad/95-26-15-R1): Traffic Alert and Collision Avoidance Systems · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 159 more. Effective Dec 26, 1996
- [AD 96-20-03](https://openairdocs.org/ad/96-20-03): Main Landing Gear Bolts · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 4 more. Effective Nov 4, 1996

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 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 101: https://openairdocs.org/model/dehavilland-dhc-8-101/ads.md

## Registered aircraft

None registered with this model now.

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (137, newest 50)

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

- [SDR 7C7A201805140414](https://openairdocs.org/sdr/7C7A201805140414), May 8, 2018: PLATE. CORRODED. PAX DOOR STRAIRCASE FWD AND AFT BACKING PLATED CORRODED. REPLACED THE PLATE.
- [SDR HNAA2017042100132](https://openairdocs.org/sdr/HNAA2017042100132), Apr 17, 2017: CONNECTOR. INOPERATIVE. RH THRESHOLD AND EXIT EMERGENCY LIGHT FOR RT FWD EXIT INOPERATIVE ALSO FWD CEILING OUT.
- [SDR HNAA2017042100133](https://openairdocs.org/sdr/HNAA2017042100133), Apr 17, 2017: LIGHT. INOPERATIVE. RIGHT OTBD AFT EMERGENCY LIGHT INOPERATIVE,
- [SDR HNAA2016012500021](https://openairdocs.org/sdr/HNAA2016012500021), Jan 25, 2016: OIL SYSTEM. OVERSERVICED. BURNING ODOR COMING FROM APU BLEEDS. INSPECTED APU COMPARTMENT WITH NO DEFECTS OR SIGNS OF ANYTHING BURNED. FOUND APU OIL SLIGHTLY OVER SERVICED. DRAINED OIL TO
- [SDR CA140630021](https://openairdocs.org/sdr/CA140630021), Jun 19, 2014: ENGINE. OVERTORQUED. (CAN) THE RT ENGINE TORQUE WENT TO 113 PERCENT FOR 3 SECONDS AND BACK TO NORMAL DURING TAXI. ACFT TAXI BACK TO GATE UNEVENTFULLY. TROUBLESHOOTING ONGOING.
- [SDR CA140620008](https://openairdocs.org/sdr/CA140620008), Jun 11, 2014: ENGINE. WARNING LIGHT. (CAN) DURING CRUISE AT FL170 THE MANUAL CAUTION LIGHT ILLUMINATED AND COULD NOT BE RESET. THE PILOT DECIDED TO RETURN TO THE DEPARTURE AIRPORT WHERE IT LANDED S
- [SDR CA140604001](https://openairdocs.org/sdr/CA140604001), May 11, 2014: LINE. RUPTURED. (CAN) DURING CRUISE THE NR 1 MAIN HYDRAULIC SYS LOST ALL FLUID. ACFT DIVERTED TO BASE. AFTER LANDING, SMOKE WAS NOTICED COMING FROM THE LT ENGINE AND AIRFIELD S
- [SDR CA130905001](https://openairdocs.org/sdr/CA130905001), Aug 20, 2013: OIL COOLER. LEAKING. (CAN) THE PILOT SHUTDOWN THE ENGINE DUE TO MAIN OIL PRESSURE FLUCTUATION FOLLOWED BY LOSS OF OIL PRESSURE. AN AIRFRAME COOLER OIL LEAKAGE WAS DETERMINED AS THE 
- [SDR CA130620005](https://openairdocs.org/sdr/CA130620005), Jun 20, 2013: LINK. BROKEN. (CAN) DURING C-CHECK, TECHS HAD PROBLEM WITH MLG ALTERNATE RELEASE SYS, RT MAIN GEAR REFUSED TO EXTEND. AFTER INVESTIGATION TECH FOUND A BROKEN D-LINK, PN 83231
- [SDR CA130521001](https://openairdocs.org/sdr/CA130521001), May 18, 2013: LANDING GEAR. MALFUNCTIONED. (CAN) DURING APPROACH, LT MLG WOULD NOT FULLY EXTEND, ALTERNATE EXTENSION WAS ATTEMPTED TO NO AVAIL. CREW RETRACTED ALL GEAR AND LANDED ON THE BELLY. CREW AND P
- [SDR CA130410015](https://openairdocs.org/sdr/CA130410015), Mar 28, 2013: PROXIMITY SENSOR. MALFUNCTIONED. (CAN) DURING CRUISE, AFTER TAKEOFF AND CLIMBOUT, THE WEIGHT ON WHEELS, CAUTION LIGHT ILLUMINATED. AFTER CONSULTING THE QRH, THE CAPTAIN DECIDED TO RETURN TO BAS
- [SDR CA130212011](https://openairdocs.org/sdr/CA130212011), Jan 7, 2013: SHAFT. CRACKED. (CAN) PROPELLER SHAFT FOUND WITH A CRACK INDICATION AT THE INNER BORE AT THE NR 19 BEARING LOCATION DURING THE NORMAL MAGNETIC PARTICLES INSPECTION WHILE THE RG
- [SDR CA121121005](https://openairdocs.org/sdr/CA121121005), Nov 7, 2012: OIL COOLER. SPLIT. (CAN) ACFT REPORTED TO HAVE DIMINISHING OIL PRESSURE DURING FLIGHT ON THE RT ENGINE. ENGINE SHUTDOWN AND ACFT RETURNED TO BASE SAFELY. PILOTS DEBRIEFED AND ESTA
- [SDR HNAA2012081300915](https://openairdocs.org/sdr/HNAA2012081300915), Aug 10, 2012: DOOR. OPEN. GEAR FAILED TO RETRACT AFTER TAKEOFF. MAINT INSPECTED AND FOUND OVERHEAD BYPASS DOOR OPEN. MAINT CLOSED DOOR AS REQUIRED.
- [SDR CA120314001](https://openairdocs.org/sdr/CA120314001), Mar 14, 2012: ACTUATOR. FAILED. (CAN) A/C LOST HYDRAULIC PRESSURE DUE TO FAILURE OF THE L/H OB SPOILER ACTUATOR. ON DESCENT TO POM, THE CREW COMPLETED A MANUAL ALTERNATE GEAR EXTENSION, WITH A
- [SDR KPVA2012030802](https://openairdocs.org/sdr/KPVA2012030802), Mar 3, 2012: CONNECTOR. BURNED. FLIGHT ATTENDANT NOTICED STRONG "BURN" SMELL IN THE MIDDLE OF THE CABIN SHORTLY AFTER SHUTTING DOWN. FOUND OVERHEAD LIGHT AT FLIGHT ATTENDANT STATION BURNED OUT
- [SDR CA111114001](https://openairdocs.org/sdr/CA111114001), Nov 3, 2011: OIL SYSTEM. LOW PRESSURE. (CAN) DURING CRUISE, THE CREW RECEIVED A LOW OIL PRESSURE WARNING. THE PROPELLER WAS FEATHERED AND THE POWER BROUGHT BACK TO IDLE. THE OIL PRESSURE CONTINUED TO
- [SDR CA110307003](https://openairdocs.org/sdr/CA110307003), Mar 4, 2011: LANDING GEAR. COLLAPSED. (CAN) AN ACFT HAD AN INCIDENT UPON LANDING WHEN THE RT MAIN GEAR COLLAPSED DUE TO A HEAVY LANDING. THE ACFT SKIDDED OF THE SIDE OF THE RUNWAY BEFORE COMING TO R
- [SDR CA110221003](https://openairdocs.org/sdr/CA110221003), Feb 16, 2011: ACTUATOR. CRACKED. DURING A WALK AROUND, A HYD LEAK WAS NOTICED FROM THE LT WING. ENGINEERING FOUND THE LT OTBD SPOILER ACTUATOR LEAKING FROM THE ACTUATOR HSG, HSG THREADS HAD FRA
- [SDR CA110110010](https://openairdocs.org/sdr/CA110110010), Jan 8, 2011: SOCKET. BURNED. A CABIN SIDEWALL LIGHT WAS REPORTED AS BEING UNSERVICEABLE. THE FLUORESCENT TUBE LAMP HOLDER WAS FOUND BURNT AND PARTIALLY MELTED AT ONE OF THE RECEPTACLES ENDS
- [SDR CA101019004](https://openairdocs.org/sdr/CA101019004), Oct 6, 2010: FUEL CONTROL. FAILED. VIBRATIONS/IFSD, DURING CLIMB AFTER T/O, THE PILOT HAD ENGINE VIBRATIONS AND HE ELECTED TO SHUT THE ENGINE DOWN BEFORE RETURNING TO THE DEPARTURE AIRPORT FOR AN
- [SDR P4YA201061100002](https://openairdocs.org/sdr/P4YA201061100002), Jun 10, 2010: AUTOFEATHER SYS. NO TEST. AUTOFEATHER TEST FAILED NR 1 ENGINE. OPERATIONS CONTINUED IAW MEL NR 61-2 ITEM A, CAT B, DUE 13 JUN 2010.
- [SDR P4YA201061100001](https://openairdocs.org/sdr/P4YA201061100001), Jun 7, 2010: CABLE. BROKEN. MLG RELEASE CABLE BROKEN. REPLACED MLG ALTERNATE RELEASE FIXED LENGTH NON-ADJUSTABLE CABLE WITH NEW CABLE PN: 83200506-003 IAW AMM 32-15-00.
- [SDR CA100610001](https://openairdocs.org/sdr/CA100610001), Apr 30, 2010: ACTUATOR. LEAKING. FLT CREW REPORTED LOSS OF NR 1 HYD SYS PRESSURE AT TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE WITHOUT FURTHER INCIDENT. MX FOUND THE RT INBD SPOILER ACTUATOR
- [SDR CA090909001](https://openairdocs.org/sdr/CA090909001), Aug 29, 2009: BEARING. DAMAGED. FLT CREW REPORTED ABNORMAL VIBRATION THROUGHOUT ACFT IN ALL PHASES OF FLIGHT. VIBRATION BECAME WORSE WITH PROPS AT MAX AND HIGHER TORQUE SETTINGS. ACFT LANDED W
- [SDR CA081128001](https://openairdocs.org/sdr/CA081128001), Nov 25, 2008: TURBINE. FAILED. (CAN) PRIOR TO TAKEOFF, THE CREW FELT A THUD AND GRINDING NOISE FROM THE NR 2 ENGINE AT 70 PERCENT TORQUE. THE ENGINE WAS IMMEDIATELY SHUTDOWN, BUT BY THE TIME 
- [SDR FDKA200708388](https://openairdocs.org/sdr/FDKA200708388), Aug 15, 2007: WIRE. DAMAGED. FDM 6014 JFK-SYR (0951 PHX LCL) - OVERHEAD CEILING ENERGENCY LIGHT INOP. MX REPAIRED WIRING TO LIGHT ASSY.
- [SDR FDKA200708378](https://openairdocs.org/sdr/FDKA200708378), Aug 9, 2007: LIGHT. INOPERATIVE. FDM 6175 ALB-JFK (0459 PHX LCL) - 2 FLOOR EMERGENCY STRIP LIGHTS INOP. MX RELAMPED LIGHT STRIPS.
- [SDR FDKA200708358](https://openairdocs.org/sdr/FDKA200708358), Aug 2, 2007: INDICATOR. MALFUNCTIONED. FDM 6205 JFK-PVD (0555 PHX LCL) - PILOT REPORTED THAT THE FLAPS ONLY GO TO 4 DEGREES ON INDICATOR. MX REPLACED THE FLAP INDICATOR.
- [SDR FDKA200708357](https://openairdocs.org/sdr/FDKA200708357), Aug 2, 2007: FLAP SYSTEM. MALFUNCTIONED. FDM 6204 PVD-JFK (0555 PHX LCL) - PILOT ABORTED TAKEOFF DUE TO TAKEOFF CONFIG WANRING HORN ON ROLLOUT. MX RESET SYSTEM AND PERFORMED OPS CK OF FLAPS AND INDICAT
- [SDR FDKA200707339](https://openairdocs.org/sdr/FDKA200707339), Jul 17, 2007: BALLAST. MALFUNCTIONED. FDM 6023 JFK-BWI (1544 PHX LCL) - CAPTAIN REPORTED BURNING SMELL IN REAR CABIN. REMOVED AND REPLACED ROW 7DF SIDEWALL BALLAST AND OPS CHECKED GOOD.
- [SDR HNAA0700144](https://openairdocs.org/sdr/HNAA0700144), Jul 12, 2007: MOUNT. BROKEN. ENGINE REMOVED FROM A/C 942 HA IN MDT ON 7-3-07 RECEIVED AT SBY MAINTANCE SHOP. FOUND TORQUE MOUNT END BROKEN OFF. ENG S/N 12-42.
- [SDR FDKA200707333](https://openairdocs.org/sdr/FDKA200707333), Jul 9, 2007: BULB. BURNED OUT. FDM 6180 ALB-JFK. DURING GEAR EXTENSION INTO JFK, NLG DOWN AND LOCKED INDICATOR DID NOT ILLUMINATE. MX FOUND INDICATOR BULB BURNED OUT AND REPLACED.
- [SDR CA070718001](https://openairdocs.org/sdr/CA070718001), Jul 8, 2007: REGULATOR. FLUCTUATES. (CAN) DURING FLIGHT, THE OIL PRESS INDICATOR NR 1 ENGINE, DROPPED TO 50 PSI. QRH DRILL COMPLETED, UNSCHEDULED LANDING COMPLETED. OIL PRESSURE REGULATOR ASSEMBLY
- [SDR FDKA200707323](https://openairdocs.org/sdr/FDKA200707323), Jul 4, 2007: ARM. BROKEN. FDM 6023 JFK (1746 PHX LCL) - PASSENGER DOOR LT ARM BROKEN. MX RESECURED.
- [SDR FDKA200706299](https://openairdocs.org/sdr/FDKA200706299), Jun 23, 2007: PLUNGER. LACK OF LUBE. FDM 6285 JFK (1100 PHX LCL) CREW REPORTED A GUST LOCK INOP. MX LUBED GUSTLOCK PLUNGER OPS GOOD.
- [SDR FDKA200706260](https://openairdocs.org/sdr/FDKA200706260), Jun 4, 2007: LIGHT. INOPERATIVE. FDM 6182 PVD (1732 PHX LCL) - REAR EMERGENCY ESCAPE PATH LIGHT OUT. MX RELAMPED.
- [SDR FDKA200705255](https://openairdocs.org/sdr/FDKA200705255), May 30, 2007: SWITCH. DIRTY. FDM 6184 BWI-JFK (0428 PHX LCL). TAKEOFF CONFIG WARNING HORN ON TAKEOFF ROLL. MX CLEANED FLAP SWITCHES, OPS CHECKED GOOD.
- [SDR FDKA200705221](https://openairdocs.org/sdr/FDKA200705221), May 22, 2007: LIGHT. INOPERATIVE. FDM 6182 JFK (1309 PHX LCL) - CREW REPORTED THE FLOOR AFT FLOOD LIGHT INOP. MX RELAMPED.
- [SDR FDKA200705216](https://openairdocs.org/sdr/FDKA200705216), May 20, 2007: CONNECTOR. DIRTY. FDM 6178 JFK (1415 PHX LCL) RETURNED TO GATE DUE TO RUDDER PRESS LIGHT FAILED TO ILLUMINATE. MX CLEANED CONNECTOR.
- [SDR FDKA200705215](https://openairdocs.org/sdr/FDKA200705215), May 20, 2007: RELAY. FAILED. FDM 6205 RUDDER PRESS LIGHT FAILED TO ILLUMINATE. ACFT FERRIED TO JFK WHERE MX REPLACED RELAY, OPS CHECK WAS GOOD.
- [SDR FDKA200705212](https://openairdocs.org/sdr/FDKA200705212), May 18, 2007: SWITCH. DIRTY. FDM 6189 BDL. ABORTED T/O DUE TO T/O WARNING HORN GOES OFF ON T/O ROLL. MX CLEANED THROTTLE AND FLAP MICRO SWITCHES, OP CHECKS GOOD.
- [SDR FDKA200705209](https://openairdocs.org/sdr/FDKA200705209), May 17, 2007: SWITCH. FAULTY. FDM 6159 ALB-JFK (0500 PHX LCL). FLIGHT CREW REPORTED RUDDER FULL PRESS, RUDDER PRESS, & NR 2 RUDDER HYD CAUTION LIGHTS ILLUMINATED IN FLT. MX REMOVED AND REPLA
- [SDR FDKA200705198](https://openairdocs.org/sdr/FDKA200705198), May 11, 2007: HYDRAULIC SYSTEM. CONTAMINATED. UPON FLAP EXTENSION RUD PRESS, RUD FULL PRESS, FLAP DRIVE & NR 1 ENG HYD PUMP CAUTION LIGHTS & FLAPS ARE SLOW TO EXTEND. MX BLED AIR FROM SYSTEM AND OPS CHECKED
- [SDR FDKA200705196](https://openairdocs.org/sdr/FDKA200705196), May 9, 2007: LIGHT. BROKEN. FDM RON JFK (1330 PHX LCL) - ROW 4 C/D EMERGENCY EXIT LIGHT BROKEN. MX REMOVED AND REPLACED EMERGENCY LIGHT ASSY.
- [SDR FDKA200705190](https://openairdocs.org/sdr/FDKA200705190), May 7, 2007: UNKNOWN. UNKNOWN. ABORTED TAKEOFF DUE TO CONFIG WARN. CREW CYCLED ALL PARAMETERS, FAULT CLEARED.
- [SDR FDKA200705189](https://openairdocs.org/sdr/FDKA200705189), May 6, 2007: RELAY. INOPERATIVE. PITOT HEAT NR 1 LIGHT ILLUM AND BURNING ODOR IN THE FLIGHT DECK. MX REMOVED AND REPLACED RELAY CURRENT SENSOR.
- [SDR FDKA200705182](https://openairdocs.org/sdr/FDKA200705182), May 4, 2007: ELECTRONIC UNIT. MALFUNCTIONED. FDM 6144 BWI-JFK (1103 PHX LCL) - CREW REPORTED THE NOSE POS IND LIGHT ILLUMINATED GEAR DIS LIGHT CAME ON DURING FLIGHT AND THE WOW FAIL LIGHT ILLUMINATED. MAIN
- [SDR FDKA200705183](https://openairdocs.org/sdr/FDKA200705183), May 4, 2007: GROUND WIRE. BROKEN. FDM 6198 JFK-BTV (1247 PHX LCL). ROW 2 OVERHEAD EMERGENCY LIGHT INOP. MX REPAIRED BROKEN GROUND WIRE.
- [SDR FDKA200704159](https://openairdocs.org/sdr/FDKA200704159), Apr 17, 2007: INDICATOR. FAILED. FDM 6208 PHL-JFK (1732 PHX LCL). AIRCRAFT RETURNED TO THE GATE DUE TO RIGHT STALL WARNING LIGHT. MX REMOVED AND REPLACED FLAP POSITION INDICATOR.

All 137: https://openairdocs.org/model/dehavilland-dhc-8-101/reports.md

## STCs that may be installed (OpenAirDocs) (124, 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 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 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 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 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 ST04445NY](https://openairdocs.org/stc/ST04445NY): Installation of the Collins TDR-94D Transponder / Traffic Collision Avoidance System (TCAS) 4100 Upgrade. Mid Canada Mod Center
- [STC ST02635LA](https://openairdocs.org/stc/ST02635LA): Modification to replace the existing Mode S Transponder system with the ACSS NXT-600 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit. Med-Pac Inc
- [STC ST04372NY](https://openairdocs.org/stc/ST04372NY): Installation of saf-Tglo® SSUL23 Photoluminescent Aisle Path Marking System. STG Aerospace Ltd
- [STC ST01900WI](https://openairdocs.org/stc/ST01900WI): Heated (LH) Side Canopy Window Assembly replacement installation. Lee Aerospace Inc
- [STC ST04344NY](https://openairdocs.org/stc/ST04344NY): Installation of the Universal Avionics EFI-890R MFD. Avmax Aviation Services Inc
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [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
- [STC ST00790DE](https://openairdocs.org/stc/ST00790DE): Installation of BendixKing CAS 67B Traffic Alert and Collision Avoidance System (TCAS) II Version 7.1. Peregrine

All 124: https://openairdocs.org/model/dehavilland-dhc-8-101/stcs.md

## PMA parts (OpenAirDocs) (518, 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
- [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
- [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
- [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
- [LAH8SC0701-009](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152830737620230825141736.0001): DHC-8 Side Canopy Heated Window Assy (LH). Lee Aerospace, Inc. · PMA PQ3766CE · Replaces 8SC0701-009 · Sep 24, 2019
- [SJ8665 FP-048](https://drs.faa.gov/browse/excelExternalWindow/E49BFE6E6A9A514A86258560005D18FF.0001): Radome Boot. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 21, 2019
- [SJ8663 FP-048](https://drs.faa.gov/browse/excelExternalWindow/84ABD7C4B63FE02986258560005D18D0.0001): Radome Boot. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 21, 2019
- [IFE360-LED-02](https://drs.faa.gov/browse/excelExternalWindow/A161743B54B13FD286258463005A6683.0001): IFE360-LED PAR36 Lamp. InFlight Entertainment Products · PMA PQ3968CE · Replaces General Electric 4587, Q5587, Grimes… · Jun 21, 2018
- [Q4559-LED](https://drs.faa.gov/browse/excelExternalWindow/99ADCD404AB1025B86258463005A676D.0001): Q4559-LED PAR64 Lamp. InFlight Entertainment Products · PMA PQ3968CE · Replaces General Electric Q4559, Q4559X… · Jun 21, 2018
- [IFE460-LED-01](https://drs.faa.gov/browse/excelExternalWindow/581FA7A53559274686258463005A66FE.0001): IFE460-LED PAR46 Lamp (FLOOD). InFlight Entertainment Products · PMA PQ3968CE · Replaces Q4554 · Jun 21, 2018
- [SG-1002-SS-300](https://drs.faa.gov/browse/excelExternalWindow/EEB7733C58C57E968625848D005DD0F7.0001): Photo-luminescent Aisle Path Marking System. STG Aerospace Inc · PMA PQ1522CE · Modification part · Jun 3, 2018
- [SG-1002-SSL-300](https://drs.faa.gov/browse/excelExternalWindow/AB7B2BED145F0A42862582F900728379.0001): Photo-luminescent Aisle Path Marking System. STG Aerospace Inc · PMA PQ1522CE · Modification part · Jun 3, 2018
- [SG-1002-SSL-300](https://drs.faa.gov/browse/excelExternalWindow/A1A0EEEBE15B08A48625848D005DD161.0001): Photo-luminescent Aisle Path Marking System. STG Aerospace Inc · PMA PQ1522CE · Modification part · Jun 3, 2018
- [SG-1002-SS-300](https://drs.faa.gov/browse/excelExternalWindow/9433A75AD53EC2CF862582F90072836E.0001): Photo-luminescent Aisle Path Marking System. STG Aerospace Inc · PMA PQ1522CE · Modification part · Jun 3, 2018
- [SG-1002-SSUL-300](https://drs.faa.gov/browse/excelExternalWindow/8607021DC77634508625848D005DD204.0001): Photo-luminescent Aisle Path Marking System. STG Aerospace Inc · PMA PQ1522CE · Modification part · Jun 3, 2018
- [SG-1002-SSUL-300](https://drs.faa.gov/browse/excelExternalWindow/532FEC9E7B30641B862582F900728380.0001): Photo-luminescent Aisle Path Marking System. STG Aerospace Inc · PMA PQ1522CE · Modification part · Jun 3, 2018
- [36903-2](https://drs.faa.gov/browse/excelExternalWindow/AD5FC2B3A1A6C299862582580071B8BB.0001): Front Panel-Black. RANTEC Power Systems Inc · PMA PQ5244NM · Replaces Honeywell 7005413-2 · Feb 4, 2018
- [36902-1](https://drs.faa.gov/browse/excelExternalWindow/7926BC585A2594F9862582580071B8BC.0001): Overlay- Gray. RANTEC Power Systems Inc · PMA PQ5244NM · Replaces Honeywell 7005394-1 · Feb 4, 2018
- [36902-6](https://drs.faa.gov/browse/excelExternalWindow/5924D0EC6FBC19C3862582580071B8BE.0001): Overlay- Black. RANTEC Power Systems Inc · PMA PQ5244NM · Replaces Honeywell 7005394-6 · Feb 4, 2018
- [36903-1](https://drs.faa.gov/browse/excelExternalWindow/2CF02F665CDD0B74862582580071B8B9.0001): Front Panel-Gray. RANTEC Power Systems Inc · PMA PQ5244NM · Replaces Honeywell 7005413-1 · Feb 4, 2018
- [LA8SC0701-011](https://drs.faa.gov/browse/excelExternalWindow/9EF62EA49F0A76658625825100704135.0001): Window Assy Side Canopy (RH). Lee Aerospace, Inc. · PMA PQ3766CE · Replaces 8SC0701-011 · Jan 30, 2018
- [SG-1002-SSL-300](https://drs.faa.gov/browse/excelExternalWindow/ED1DAE5BF7E5C2E68625818E00768A91.0001): Photo-luminescent Aisle Path Marking System. STG Aerospace Inc · PMA PQ1522CE · Modification part · Aug 24, 2017
- [SG-1002-SSUL-300](https://drs.faa.gov/browse/excelExternalWindow/83E53E15DC56E8488625818E00768BA3.0001): Photo-luminescent Aisle Path Marking System. STG Aerospace Inc · PMA PQ1522CE · Modification part · Aug 24, 2017
- [SG-1002-SS-300](https://drs.faa.gov/browse/excelExternalWindow/80247556F3E925198625818E00768956.0001): Photo-luminescent Aisle Path Marking System. STG Aerospace Inc · PMA PQ1522CE · Modification part · Aug 24, 2017
- [EAI-1000](https://drs.faa.gov/browse/excelExternalWindow/98AF9AEDFE1A6E2C862581130069B10F.0001): 28V LED Reading Light. Erie Aviation Inc. · PMA PQ10010NE · Replaces 8GH007429-28 · Apr 19, 2017
- [EAI-LED-001](https://drs.faa.gov/browse/excelExternalWindow/336CD5A18914076B862581130069B29C.0001): LED Light Bulb. Erie Aviation Inc. · PMA PQ10010NE · Replaces 1308 · Apr 19, 2017
- [EAI-LED-001](https://drs.faa.gov/browse/excelExternalWindow/2E78F76A01FEB76886257FE80073FDA1.0001): LED Light Bulb. Erie Aviation Inc. · PMA PQ10010NE · Replaces 1308 · Jun 27, 2016
- [EAI-1000](https://drs.faa.gov/browse/excelExternalWindow/2D37BF31C816FDDE86257FE80073FC42.0001): 28V LED Reading Light. Erie Aviation Inc. · PMA PQ10010NE · Replaces 8GH007429-28 · Jun 27, 2016

All of them: https://openairdocs.org/model/dehavilland-dhc-8-101/pma.md

## The same model under other registry codes

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

- [Bombardier DHC-8-101](https://openairdocs.org/model/bombardier-dhc-8-101): 0 registered aircraft, registry code 1390001

---
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