# Dehavilland DHC-6-200

- Type: Aircraft model (FAA registry)
- Registry code: 2802620
- Manufacturer (registry): DEHAVILLAND
- Model: DHC-6-200
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-prop
- Seats: 24
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS A9EA](https://openairdocs.org/tcds/A9EA) (OpenAirDocs)
- Holder: De Havilland Aircraft of Canada Limited
- Registered aircraft: 19
- Page: https://openairdocs.org/model/dehavilland-dhc-6-200

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 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2022-11-12](https://openairdocs.org/ad/2022-11-12): Engine Controls · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 2 more. Effective Jul 13, 2022
- [AD 2022-11-09](https://openairdocs.org/ad/2022-11-09): Wing Structure · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 2 more. Effective Jul 6, 2022
- [AD 2022-10-07](https://openairdocs.org/ad/2022-10-07): Flight Control System · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 2 more. Effective Jun 23, 2022
- [AD 2022-10-03](https://openairdocs.org/ad/2022-10-03): Flight Control System · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 2 more. Effective Jun 23, 2022
- [AD 2022-03-04](https://openairdocs.org/ad/2022-03-04): Time Limits · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 2 more. Effective Mar 17, 2022
- [AD 2019-10-05](https://openairdocs.org/ad/2019-10-05): Flight Controls · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 2 more. Effective Jun 20, 2019
- [AD 2018-04-02](https://openairdocs.org/ad/2018-04-02): Flight Controls · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 2 more. Effective Mar 27, 2018
- [AD 2009-04-09](https://openairdocs.org/ad/2009-04-09): Wing front spar adapter · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Mar 26, 2009
- [AD 2008-24-01](https://openairdocs.org/ad/2008-24-01): Flight control gust locks · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Dec 30, 2008
- [AD 2008-13-11](https://openairdocs.org/ad/2008-13-11): Corrosion · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Aug 5, 2008
- [AD 2006-16-18 R1](https://openairdocs.org/ad/2006-16-18-R1): Installing a warning placard on the TAWS/RMI · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 100 more. Effective Jul 18, 2008
- [AD 2005-25-08](https://openairdocs.org/ad/2005-25-08): Electronic Flight Information System (EFIS) · B-N Group BN-2A, 172, 180 and 22 more. Effective Jan 23, 2006
- [AD 2005-18-20](https://openairdocs.org/ad/2005-18-20): "FASTprop" propeller de-icers · Hartzell PHC-C3YF-1RF/F8468A(B,K)-8R constant speed propeller (STC SA00718LA or 17 others). Effective Oct 14, 2005
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2000-06-03](https://openairdocs.org/ad/2000-06-03): Pneumatic Deicing Boots · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective May 5, 2000
- [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998
- [AD 97-23-09](https://openairdocs.org/ad/97-23-09): Inspect Fuselage Side Frames for Cracks · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Dec 22, 1997
- [AD 97-07-10 R1](https://openairdocs.org/ad/97-07-10-R1): Wing Struts · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective May 23, 1997
- [AD 96-09-11](https://openairdocs.org/ad/96-09-11): Airplane Flight Manual (AFM) - Icing · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Jun 11, 1996
- [AD 95-22-07](https://openairdocs.org/ad/95-22-07): Horizontal Stabilizer Attachment Fittings · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Dec 27, 1995
- [AD 95-21-14](https://openairdocs.org/ad/95-21-14): Tailplane Outboard Hinge Arm Assembly · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Dec 4, 1995
- [AD 95-18-11](https://openairdocs.org/ad/95-18-11): Wing Rear Spar Attachment Caps · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Oct 26, 1995
- [AD 95-18-10](https://openairdocs.org/ad/95-18-10): Elevator Root Rib · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Oct 26, 1995
- [AD 94-14-22](https://openairdocs.org/ad/94-14-22): Elevator Control Support · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Aug 31, 1994
- [AD 94-08-10](https://openairdocs.org/ad/94-08-10): Wing Main Spar · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Jun 13, 1994
- [AD 94-04-01](https://openairdocs.org/ad/94-04-01): Wing Attachment Fittings · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Mar 31, 1994
- [AD 93-10-08](https://openairdocs.org/ad/93-10-08): Controls in Overhead Control Console · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Jul 16, 1993
- [AD 93-02-04](https://openairdocs.org/ad/93-02-04): Elevator Support Assembly · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Mar 19, 1993
- [AD 90-11-01](https://openairdocs.org/ad/90-11-01): Elevator Pushrod Assembly · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Nov 16, 1990
- [AD 87-04-23](https://openairdocs.org/ad/87-04-23): Wing Support Strut · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Mar 16, 1987
- [AD 87-03-12](https://openairdocs.org/ad/87-03-12): Utility Seat - Forward Legs · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Feb 13, 1987
- [AD 80-13-11 R2](https://openairdocs.org/ad/80-13-11-R2): Rod Assemblies · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Aug 10, 1983
- [AD 82-26-06](https://openairdocs.org/ad/82-26-06): Windscreen Washer/Deicing System · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Dec 27, 1982
- [AD 81-22-03](https://openairdocs.org/ad/81-22-03): Elevator Torque Tube · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Nov 2, 1981
- [AD 69-05-01 R2](https://openairdocs.org/ad/69-05-01-R2): Control Column Sub-assembly Cracks · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Jul 7, 1980
- [AD 80-13-13](https://openairdocs.org/ad/80-13-13): Struts · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Jul 1, 1980
- [AD 80-03-08](https://openairdocs.org/ad/80-03-08): Flap Control Rod Tubes · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Feb 7, 1980
- [AD 79-14-01](https://openairdocs.org/ad/79-14-01): Elevator Control System · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Jul 6, 1979
- [AD 78-01-05](https://openairdocs.org/ad/78-01-05): Electrical Failure · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Feb 9, 1978
- [AD 76-13-06](https://openairdocs.org/ad/76-13-06): Lightning Protection · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Jul 6, 1976
- [AD 76-07-08](https://openairdocs.org/ad/76-07-08): Water Leakage-float Models · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Apr 12, 1976
- [AD 75-26-07](https://openairdocs.org/ad/75-26-07): Electrical Fire Hazards · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Dec 17, 1975
- [AD 75-24-15](https://openairdocs.org/ad/75-24-15): AC Power · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Nov 28, 1975
- [AD 75-12-10](https://openairdocs.org/ad/75-12-10): Autopilots · M7 Aerospace 60, 95-C55, 95-C55A and 17 more. Effective Jun 11, 1975
- [AD 75-08-02](https://openairdocs.org/ad/75-08-02): Aileron Control Cable · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Apr 7, 1975
- [AD 74-22-06](https://openairdocs.org/ad/74-22-06): Horizontal Stabilizer · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Oct 23, 1974
- [AD 74-08-11](https://openairdocs.org/ad/74-08-11): Side Seat Rail Attachment · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Apr 18, 1974
- [AD 73-19-01](https://openairdocs.org/ad/73-19-01): Prop Auto-feathering System · Viking Air DHC-6-100, DHC-6-200 and DHC-6-300 with STC SA2608WE. Effective Feb 18, 1974
- [AD 73-20-05](https://openairdocs.org/ad/73-20-05): Float To Fuselage Bolts · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Oct 3, 1973

Historical (superseded or no longer in force):

- [AD 2008-11-10](https://openairdocs.org/ad/2008-11-10) (historical): Wing front spar adapter assemblies · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Aug 5, 2008
- [AD 2008-03-01](https://openairdocs.org/ad/2008-03-01) (historical): Structural components · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Mar 6, 2008
- [AD 99-18-13](https://openairdocs.org/ad/99-18-13) (historical): Airplane Flight Manual (AFM) - Limitation Section - power levers · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Oct 8, 1999
- [AD 97-07-10](https://openairdocs.org/ad/97-07-10) (historical): Wing Struts · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective May 23, 1997
- [AD 89-24-06 R1](https://openairdocs.org/ad/89-24-06-R1) (historical): Elevator Quadrant · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Sep 13, 1990
- [AD 83-02-02](https://openairdocs.org/ad/83-02-02) (historical): Structural Components · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Feb 4, 1983
- [AD 80-13-12 R1](https://openairdocs.org/ad/80-13-12-R1) (historical): Longerons · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Jun 19, 1981
- [AD 80-13-10](https://openairdocs.org/ad/80-13-10) (historical): Y-Joint Main Landing Gear Legs · Viking Air DHC-6-1, DHC-6-100, DHC-6-200 and 1 more. Effective Jul 1, 1980

All 67: https://openairdocs.org/model/dehavilland-dhc-6-200/ads.md

## Registered aircraft (19)

- [N10EA](https://openairdocs.org/aircraft/N10EA): [Eagle Air Transport Inc](https://openairdocs.org/faa-owner/EAGLE%20AIR%20TRANSPORT%20INC), [Ottawa, IL](https://openairdocs.org/faa-place/IL/Ottawa), S/N 199
- [N123FX](https://openairdocs.org/aircraft/N123FX): [Freefall Express](https://openairdocs.org/faa-owner/FREEFALL%20EXPRESS), [Gardiner, NY](https://openairdocs.org/faa-place/NY/Gardiner), built 1969, S/N 200
- [N153KD](https://openairdocs.org/aircraft/N153KD): [Mec International Trading LLC](https://openairdocs.org/faa-owner/MEC%20INTERNATIONAL%20TRADING%20LLC), [Mission, TX](https://openairdocs.org/faa-place/TX/Mission), built 1968, S/N 153
- [N186AL](https://openairdocs.org/aircraft/N186AL): [Alm Holdings Delaware LLC](https://openairdocs.org/faa-owner/ALM%20HOLDINGS%20DELAWARE%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 186
- [N204BD](https://openairdocs.org/aircraft/N204BD): [Kavalair LLC Series G](https://openairdocs.org/faa-owner/KAVALAIR%20LLC%20SERIES%20G), [Marion, MT](https://openairdocs.org/faa-place/MT/Marion), built 1969, S/N 204
- [N223AL](https://openairdocs.org/aircraft/N223AL): [Win Win Aviation Inc](https://openairdocs.org/faa-owner/WIN%20WIN%20AVIATION%20INC), [Wake Forest, NC](https://openairdocs.org/faa-place/NC/Wake%20Forest), built 1969, S/N 223
- [N228YK](https://openairdocs.org/aircraft/N228YK): [Desert Sand Aircraft Leasing Co Inc](https://openairdocs.org/faa-owner/DESERT%20SAND%20AIRCRAFT%20LEASING%20CO%20INC), [Rosharon, TX](https://openairdocs.org/faa-place/TX/Rosharon), built 1969, S/N 228
- [N301CL](https://openairdocs.org/aircraft/N301CL): [Win Win Aviation Inc](https://openairdocs.org/faa-owner/WIN%20WIN%20AVIATION%20INC), [Wake Forest, NC](https://openairdocs.org/faa-place/NC/Wake%20Forest), built 1969, S/N 221
- [N321CY](https://openairdocs.org/aircraft/N321CY): [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), built 1968, S/N 211
- [N40269](https://openairdocs.org/aircraft/N40269): [Freefall Express Inc](https://openairdocs.org/faa-owner/FREEFALL%20EXPRESS%20INC), [Gardiner, NY](https://openairdocs.org/faa-place/NY/Gardiner), built 1968, S/N 152
- [N469TS](https://openairdocs.org/aircraft/N469TS): [Desert Sand Aircraft Leasing Co Inc](https://openairdocs.org/faa-owner/DESERT%20SAND%20AIRCRAFT%20LEASING%20CO%20INC), [Rosharon, TX](https://openairdocs.org/faa-place/TX/Rosharon), built 1968, S/N 149
- [N512AR](https://openairdocs.org/aircraft/N512AR): [Twin Otter International Ltd](https://openairdocs.org/faa-owner/TWIN%20OTTER%20INTERNATIONAL%20LTD), [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas), built 1967, S/N 59
- [N647MC](https://openairdocs.org/aircraft/N647MC): [Collier Mosquito Control District](https://openairdocs.org/faa-owner/COLLIER%20MOSQUITO%20CONTROL%20DISTRICT), [Naples, FL](https://openairdocs.org/faa-place/FL/Naples), built 1967, S/N 087
- [N669JW](https://openairdocs.org/aircraft/N669JW): [Kapowsin Air Sports Ltd](https://openairdocs.org/faa-owner/KAPOWSIN%20AIR%20SPORTS%20LTD), [Shelton, WA](https://openairdocs.org/faa-place/WA/Shelton), built 1968, S/N 088
- [N690MF](https://openairdocs.org/aircraft/N690MF): [Desert Sand Aircraft Leasing Co Inc](https://openairdocs.org/faa-owner/DESERT%20SAND%20AIRCRAFT%20LEASING%20CO%20INC), [Rosharon, TX](https://openairdocs.org/faa-place/TX/Rosharon), built 1968, S/N 121
- [N692DA](https://openairdocs.org/aircraft/N692DA): [Direct Action Aviation LLC](https://openairdocs.org/faa-owner/DIRECT%20ACTION%20AVIATION%20LLC), [Reno, NV](https://openairdocs.org/faa-place/NV/Reno), built 1968, S/N 151
- [N70EA](https://openairdocs.org/aircraft/N70EA): [Eagle Air Transport](https://openairdocs.org/faa-owner/EAGLE%20AIR%20TRANSPORT), [Ottawa, IL](https://openairdocs.org/faa-place/IL/Ottawa), S/N 139
- [N753AF](https://openairdocs.org/aircraft/N753AF): [Twin Otter International Ltd](https://openairdocs.org/faa-owner/TWIN%20OTTER%20INTERNATIONAL%20LTD), [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas), S/N 206
- [N82LH](https://openairdocs.org/aircraft/N82LH): [Airborne Support Group LLC](https://openairdocs.org/faa-owner/AIRBORNE%20SUPPORT%20GROUP%20LLC), [Marion, MT](https://openairdocs.org/faa-place/MT/Marion), built 1969, S/N 208

## NTSB investigations (9)

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 ERA15LA343](https://openairdocs.org/ntsb/ERA15LA343), Sep 6, 2015: Dehavilland DHC-6 (N181CS), Louisburg, NC, substantial damage. Probable cause: The propeller’s movement to the beta position during landing for reasons that could not be determined during postaccident examination and testing, which resulted in an attempted go-around and…
- [NTSB ERA15LA124](https://openairdocs.org/ntsb/ERA15LA124), Feb 9, 2015: Dehavilland DHC 6 200 (N70EA), Sebastian, FL, substantial damage. Probable cause: The pilot's failure to conduct all of the required items on the Before Starting Engines checklist, which resulted in her failure to detect an open hydraulic circuit breaker and led to insufficient…
- [NTSB CEN14LA272](https://openairdocs.org/ntsb/CEN14LA272), Jun 1, 2014: Dehavilland DHC 6 200 (N223AL), Middletown, OH, minor damage, 1 fatal. Probable cause: The skydiving operator employee’s failure to see and avoid the rotating propeller blades when she walked toward the cockpit while the airplane’s engines were running.
- [NTSB MIA00FA229](https://openairdocs.org/ntsb/MIA00FA229), Jul 31, 2000: de Havilland DHC-6-200 (N201RH), Raleigh, NC, destroyed, 1 fatal. Probable cause: the pilot's continued VFR flight into IMC conditions, by failing to maintain altitude, and descending from VFR conditions into IMC, which resulted in him subsequently impacting with trees. Factors in…
- [NTSB MIA96WA150](https://openairdocs.org/ntsb/MIA96WA150), Mar 9, 1996: de Havilland DHC-6-200 (N245GW), Bagua, Peru, destroyed, 3 fatal
- [NTSB LAX95LA137](https://openairdocs.org/ntsb/LAX95LA137), Mar 16, 1995: de Havilland DHC-6-200 (N37ST), Honolulu, HI, destroyed. Probable cause: Intentional ditching due to the flightcrew's failure to properly manage the fuel system, and operation of the airplane in an excessively overweight condition.
- [NTSB LAX93WA028](https://openairdocs.org/ntsb/LAX93WA028), Nov 1, 1992: de Havilland DHC-6-200 (N201RH), Kenya, no damage, 1 fatal
- [NTSB ANC72DAA27](https://openairdocs.org/ntsb/ANC72DAA27), Mar 31, 1972: Dehavilland DHC-6 (N512AR), Prudhoe Bay, AK, substantial damage
- [NTSB ANC71DAA23](https://openairdocs.org/ntsb/ANC71DAA23), Dec 1, 1970: Dehavilland DHC-6 (N512AR), Prudhoe Bay, AK, substantial damage

## FAA accident and incident reports (43)

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 20260321003969I](https://openairdocs.org/incident/20260321003969I), Mar 21, 2026: Dehavilland DHC-6-200 (N204BD), Eloy, AZ, No damage, 1 fatal. On March 21, 2026, between approximately 1255 and 1303 MST (1955Z–2003Z), a parachutist employed by [privacy data omitted] was conducting video recording…
- [Incident 20250502004559I](https://openairdocs.org/incident/20250502004559I), May 2, 2025: Dehavilland DHC-6-200 (N204BD), Eloy, AZ, No damage, 1 fatal. On may 2, 2025, at approximately 11:00 am MST, a parachute jumper at Eloy airport (E60) in Eloy, Arizona, sustained fatal injuries after failing to deploy his…
- [Incident 20230428002639I](https://openairdocs.org/incident/20230428002639I), Apr 28, 2023: Dehavilland DHC-6-200 (N690MF), Fentress, TX, No damage, 1 fatal. On April 28th,2023. At approximately 1225 pm a parachute jumper perished while jumping at Fentress Airpark. Texas. His main parachute opened and failed. He…
- [Incident 20220731022469I](https://openairdocs.org/incident/20220731022469I), Jul 31, 2022: Dehavilland DHC-6-200 (N228YK), Whitewright, TX, No damage, 1 fatal. At about 13:30 parachutist [privacy data omitted]uspa member [privacy data omitted], A-101737 made a 3/4 braked l/h turn at about 100'. He impacted the ground…
- [Incident 20220619023399I](https://openairdocs.org/incident/20220619023399I), Jun 19, 2022: Dehavilland DHC-6-200 (N692DA), Sylvania, WI, No damage. Aircraft [privacy data omitted] not invoved in accident. Parachute operations at the sulvania Wisconsin airport. Tandum jump instructor and student had just…
- [Incident 20200628010739I](https://openairdocs.org/incident/20200628010739I), Jun 28, 2020: Dehavilland DHC-6-200 (N40269), Gardiner, NY, No damage, 1 fatal. 06-28-2020 During skydiving training, the skydiver, left the aircraft wearing a parachute, but didn't have the parachute on his body when he hit the ground.…
- [Incident 20180927014089I](https://openairdocs.org/incident/20180927014089I), Sep 27, 2018: Dehavilland DHC-6-200 (N321CY), Lebanon, ME, No damage, 1 fatal. During a group tandem skydive event, instructor [privacy data omitted] was secured to his student, r[privacy data omitted]. The flight/jump was filmed from…
- [Incident 20160806014899I](https://openairdocs.org/incident/20160806014899I), Aug 6, 2016: Dehavilland DHC-6-200 (N153KD), Acampo, CA, No damage. At Lodi Airport, CA. Parachute center, two skydivers using a u.p.t. tandem parachute rig was fatally injured from impact with the ground. Tandem instructor was…
- [Incident 20160213002679I](https://openairdocs.org/incident/20160213002679I), Feb 13, 2016: Dehavilland DHC-6-200 (N10EA), Arecibo, PR, No damage, 1 fatal. On February 13, 2016 at 14:00 UCT/10:00 local time. Mr. Gary farracane was fatally injured in a voluntary parachute jumping incident. He was participating in…
- [Incident 20151017021779I](https://openairdocs.org/incident/20151017021779I), Oct 17, 2015: Dehavilland DHC-6-200 (N10EA), Sebastian, FL, No damage, 1 fatal. A practice parachute jump was being conducted from 6000 feet for an upcoming demonstration "flag" jump. All skydivers exited normally, but the second skydiver…
- [Accident 20150906023729A](https://openairdocs.org/incident/20150906023729A), Sep 6, 2015: Dehavilland DHC-6-200 (N181CS), Louisberg, NC, Destroyed. During landing, N181CS, a Dehavilland twin otter, DHC-6-200, s/n 181, departed the runway surface at approximately 30 degrees to the right of the runway…
- [Incident 20150523011959I](https://openairdocs.org/incident/20150523011959I), May 23, 2015: Dehavilland DHC-6-200 (N204BD), Eloy, AZ, No damage, 1 fatal. Skydiver was participating in a 16 man formation jump which was practice for a larger 100 way attempt. The exit from the aircraft and formation portion of the…
- [Accident 20150209000881A](https://openairdocs.org/incident/20150209000881A), Feb 9, 2015: Dehavilland DHC-6-200 (N70EA), Sebastian, FL, Substantial damage. On 2/9/2015, at approximately 0630, N30EA (piloted by[privacy data omitted]) and N70EA had a head on collision on the ramp of the Sebastian municipal airport.…
- [Accident 20140601008289A](https://openairdocs.org/incident/20140601008289A), Jun 1, 2014: Dehavilland DHC-6-200 (N223AL), Middletown, OH, Minor damage, 1 fatal. Aircraft was conducting a hot load parachute operation when one of the ground crew walked into the left spinning propeller and was struck in the head, she…
- [Incident 20140412006249I](https://openairdocs.org/incident/20140412006249I), Apr 12, 2014: Dehavilland DHC-6-200 (N321CY), Zephyrhills, FL, No damage, 1 fatal. Per current FAA order 8020.11C: 1. Name of jumper: robert a. waspe. 2. Experience/training of jumper: 1362 jumps since 2008. 3. Club affiliation: uspa member…
- [Incident 20140403006159I](https://openairdocs.org/incident/20140403006159I), Apr 3, 2014: Dehavilland DHC-6-200 (N204BD), Eloy, AZ, No damage, 1 fatal. During a 222 way skydiving formation attempt the jumper flew in the formation and deployed her canopy at approximately 2000 AGL. Witnesses stated they observed…
- [Incident 20130616009999I](https://openairdocs.org/incident/20130616009999I), Jun 16, 2013: Dehavilland DHC-6-200 (N669JW), Laurel, DE, No damage. Two experienced jumpers performing canopy relative work (crw) in stack formation. Lower parachutist (jumper 1) made contact with upper parachutist (jumper 2)…
- [Incident 20120615011839I](https://openairdocs.org/incident/20120615011839I), Jun 15, 2012: Dehavilland DHC-6-200 (N40269), Plattekill, NY, No damage, 2 fatal. Name of jumpers: david winoker, student and aleksandr chulsky, instructorexperience and training: winoker, first jumpchulsky, uspa "d"licensed coach, tandem…
- [Incident 20120330004359I](https://openairdocs.org/incident/20120330004359I), Mar 30, 2012: Dehavilland DHC-6-200 (N10EA), Sebastian, FL, No damage, 1 fatal. Witnesses stated that the skydiver came in to low and fast. They further stated that his feet hit the edge of the ditch and he tumbled to the ground. He had…
- [Incident 20070317004969I](https://openairdocs.org/incident/20070317004969I), Mar 17, 2007: Dhav DHC6200 (N690MF), Dublin, GA, 2 fatal. (-23) 10 Skydivers had exited two aircraft. With chutes open and descending through about 500' two of the skydivers were maneuvering to a traffic pattern for…
- [Incident 20050511009419I](https://openairdocs.org/incident/20050511009419I), May 11, 2005: Dhav DHC6200 (N669JW), Abingdon, VA, Minor damage. (-23) [privacy data omitted] the pilot taxiied between two rows of parked airplanes then initiated a left hand turn to proposed parking for refueling. During…
- [Incident 20050501007969I](https://openairdocs.org/incident/20050501007969I), May 1, 2005: Dhav DHC6200 (N228YK), Trenton, TX, 1 fatal. (-23) Skydiver [privacy data omitted] attempted to release his main parachute after experiencing a malfunction. The left main riser failed to release before…
- [Incident 20050216005289I](https://openairdocs.org/incident/20050216005289I), Feb 16, 2005: Dhav DHC6200 (N204BD), Eloy, AZ, 1 fatal. (-23) Multiple skydivers left aircraft and were farther away from landing area than were able to travel back under canopy to land. One of the other skydivers…
- [Incident 20050115003129I](https://openairdocs.org/incident/20050115003129I), Jan 15, 2005: Dhav DHC6200 (N228YK), Trenton, TX, 1 fatal. (-23) Skydiver [privacy data omitted] on 99th jump experienced malfunction on main canopy pd spectre 210. #6 cell non load bearing rib separated from nose to…
- [Incident 20040619020489I](https://openairdocs.org/incident/20040619020489I), Jun 19, 2004: Dhav DHC6200 (N223AL), Hinckley, IL, 1 fatal. (-23) On June 19, 2004, [privacy data omitted] sustained fatal injuries suffered from a skydiving incident at chicagoland skydive, 12637 rt. 30, Hinckley, IL.…
- [Incident 20021122036119I](https://openairdocs.org/incident/20021122036119I), Nov 22, 2002: Dhav DHC6200 (N226CS), Lake Wales, FL, 2 fatal. (-23) Attachment ot incident number S-234 that occurred on November 22, 2002, at Lake Wales, Florida involving a sky dive from aircraft N226CS, a DHC-6 twin…
- [Incident 20020407005829I](https://openairdocs.org/incident/20020407005829I), Apr 7, 2002: Dhav DHC6 (N690MF), Rosharon, TX. (-23) Skydiver injured during parachute landing after making 360 degree turn too close to ground. Broken leg and internal injuries. No aircraft damage or other…
- [Incident 20011118034949I](https://openairdocs.org/incident/20011118034949I), Nov 18, 2001: Dhav DHC6200 (N10EA), Delavan, WI, Minor damage. (-23) PIC, nelson, stated that he has flown to lade Lawn airport several times and was aware of the FAA NOTAM stating only the west side runway lightswere…
- [Incident 20011014034939I](https://openairdocs.org/incident/20011014034939I), Oct 14, 2001: Dhav DHC6200 (N10EA), Ottawa, IL, 1 fatal. (-23) On October 10, 2001, bruce a. greig [privacy data omitted] sustained fatal injuries from a skydiving incident at Skydive Chicago, Ottawa, IL. A witness…
- [Incident 20011006030179I](https://openairdocs.org/incident/20011006030179I), Oct 6, 2001: Dhav DHC6200 (N10EA), Ottawa, IL, 2 fatal. (-23) On October 6, 2001, steven a. smith, (dob 11/18/1956) and deborah a. luhmann, (dob 03/27/1974) sustained fatal injuries from a skydiving incident at…
- [Incident 20010530030169I](https://openairdocs.org/incident/20010530030169I), May 30, 2001: Dhav DHC6200 (N10EA), Ottawa, IL, Minor damage. (-23) Passenger lost hat through open window in cockpit. He exited aircraft to retrieve hat. Although engines had been shut down, propellers were still…
- [Incident 20010516015439I](https://openairdocs.org/incident/20010516015439I), May 16, 2001: Dhav DHC6200 (N223AL), Sebastian, FL, 1 fatal. (-23) Witnesses say that upon exiting aircraft on the 13th student jump, Mr. Bischofberger began to tumble and could not open the main chute. The reserve chute…
- [Incident 20010415009689I](https://openairdocs.org/incident/20010415009689I), Apr 15, 2001: Dhav DHC6200 (N228YK), Trenton, TX, 1 fatal. (-23)[privacy data omitted] first jump student [privacy data omitted] . Witness states that at approximately 100 ft. jumper pulled toggles down to half brakes…
- [Accident 20000731005409A](https://openairdocs.org/incident/20000731005409A), Jul 31, 2000: Dhav DHC6200 (N201RH), Raleigh-Durham, NC, No damage, 1 fatal. (-23) The aircraft, while on a VFR flight, was attempting to find the Raleigh, NC (rdu) airport at might with a low ceiling. The Raleigh ATC had the aircraft…
- [Incident 20000624032209I](https://openairdocs.org/incident/20000624032209I), Jun 24, 2000: Dhav DHC6200 (N223AL), Chico Hot Sprin, MT, 1 fatal. (-23)Based on the investigation by officer[privacy data omitted] of the park county sheriif's office, livingston, Montana, eye witnesses reported the…
- [Incident 19981218043229I](https://openairdocs.org/incident/19981218043229I), Dec 18, 1998: Dhav DHC6200 (N123FX), Zephyrhills, FL, Minor damage. (-5)After takeoff from runway 18, the pilot turned and banked to the east, made a low pass across sky dive city's jump zone. With the aircraft in a banked…
- [Incident 19970530018809I](https://openairdocs.org/incident/19970530018809I), May 30, 1997: Dhav DHC6200 (N123FX), Cross Keys, NJ, 1 fatal. Main chute tangled in students legs. Main chute failed. Release. Jammed. Reserve alsto tangled.
- [Incident 19960928043049I](https://openairdocs.org/incident/19960928043049I), Sep 28, 1996: Dhav DHC6 (N186AL), Waller, TX. Narrative: this incident involved a Dehavilland DHC-6 that experienced an engine fire. The fire was successfully extinguished and an uneventful landing was…
- [Incident 19960328011029I](https://openairdocs.org/incident/19960328011029I), Mar 28, 1996: Dhav DHC6200 (N123FX), Deland, FL. Narrative: nils hellberg and rob laidlaw were part of a twenty person formation group. When the divers broke their formation and separated, hellberg opened his…
- [Incident 19960305006289I](https://openairdocs.org/incident/19960305006289I), Mar 5, 1996: Dhav DHC6200 (N123FX), Deland, FL. Narrative: while parachuting at Deland, FL, jeff coban impacted the ground at a high rate of descent which resulted in a broken leg and possible back injuries,…
- [Incident 19950715024699I](https://openairdocs.org/incident/19950715024699I), Jul 15, 1995: Dhav DHC6200 (N669JW), Waynesville, OH. Encountered severe downdrafts descending. Opened chutes near ground. Hard landings. Injured three jumpers.
- [Accident 19950316004089A](https://openairdocs.org/incident/19950316004089A), Mar 16, 1995: Dhav DHC6200 (N37ST), Honolulu, HI, Destroyed. Departed overweight on 17HR trip. Ferry tanks transfer failed short of destination. Ditched mismanaged fuel system.
- [Incident 19931230051689I](https://openairdocs.org/incident/19931230051689I), Dec 30, 1993: Dhav DHC6200 (N123FX), Zfphyrills, FL, 1 fatal. Jumper was performing a hook manuver and misjudged the height. Impacted the ground.

## Service difficulty reports (54, newest 50)

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

- [SDR CA190527026](https://openairdocs.org/sdr/CA190527026), Apr 25, 2019: RESISTOR. BURNED. (CAN) A FEW MINUTES AFTER TAKEOFF, THE PILOTS NOTICED AN ELECTRICAL BURNING SMELL. THE PILOTS COMPLETED THE CHECKLIST AND NOTICED THAT THE FUMES SEEMED TO DECRE
- [SDR CA190328016](https://openairdocs.org/sdr/CA190328016), Mar 27, 2019: SKIN. DEBONDED. (CAN) WHEN SB V6/0018 WAS CARRIED OUT, DISBOND WAS FOUND TO THE OUTER LIMITS OF THE INSPECTION CRITERIA (YW 65 TO YW 155) ON THE RH UPPER WING SURFACE TO CORRUG
- [SDR CA190314011](https://openairdocs.org/sdr/CA190314011), Mar 7, 2019: SWITCH. FAILED. (CAN) DURING A TRAINING FLIGHT, THE CO-PILOT LET THE NOSE GET TOO HIGH, IN RESPONSE, THE PILOT PUSHED FORWARD AGGRESSIVELY TO AVOID A POTENTIAL STALL, AT WHICH 
- [SDR CA190315016](https://openairdocs.org/sdr/CA190315016), Mar 2, 2019: SWITCH. FAILED. (CAN) PILOT REPORTED THAT THE PROPELLER DID NOT FEATHER WHILE CONDUCTING GROUND FUNCTION CHECK OF THE AUTO FEATHER SYSTEM. MAINTENANCE CHANGED THE SWITCH AND TH
- [SDR CA160317011](https://openairdocs.org/sdr/CA160317011), Feb 28, 2016: STRUT. DAMAGED. (CAN) DURING AN INSPECTION OF THE WING STRUT LOWER ATTACHMENT BOLTS, CORROSION WAS FOUND AT THE LOWER LUG ATTACHMENT POINT ON BOTH THE LT AND RT STRUTS. CORROSI
- [SDR CA150318016](https://openairdocs.org/sdr/CA150318016), Mar 14, 2015: PRESSURE SWITCH. FAILED. (CAN) AFTER ACFT HAD DOCKED, MAINTENANCE NOTICED AN OIL LEAK FROM THE NR 1 ENGINE COWLING. UPON INVESTIGATION IT WAS FOUND THAT THE SOURCE OF THE OIL LEAK WAS T
- [SDR CA150422003](https://openairdocs.org/sdr/CA150422003), Nov 28, 2014: LEG ASSY. CORRODED. (CAN) MAIN LANDING GEAR NDT`D BY AUTHORIZED FACILITY PER 5 YEAR INSPECTION REQUIREMENT. PITTING, CORROSION & BOLT FLANGE HOLES OUT OF LIMITS FOUND DURING INTERN
- [SDR CA141022009](https://openairdocs.org/sdr/CA141022009), Oct 18, 2014: PRESSURE SWITCH. FAILED. (CAN) AFTER TAKE OFF, THROUGH 400 FT. THE LEFT ENGINE FEATHERED. PILOTS ORIGINALLY THOUGHT THERE WAS AN ENGINE FAILURE AS TORQUE WAS INDICATING ZERO. PIC MADE T
- [SDR CA120606003](https://openairdocs.org/sdr/CA120606003), May 14, 2012: COMPRESSOR. FOD. (CAN) DURING FLIGHT, THE PILOT REPORTED A LOUD NOISE FROM THE LT ENGINE. THE TORQUE PRESSURE DROPPED TO 20 LBS BUT ALL OTHER INDICATIONS WERE NORMAL. THE PILOT 
- [SDR CA120514008](https://openairdocs.org/sdr/CA120514008), May 10, 2012: ENGINE. FAILED. (CAN) PILOT REPORTED A BIG BANG AND POP COMING FROM THE LT ENGINE, TORQUE PRESSURE DROPPED TO 20 LBS BUT ALL OTHER INDICATIONS WERE NORMAL. HE THEN REDUCED POWE
- [SDR CA120323006](https://openairdocs.org/sdr/CA120323006), Mar 23, 2012: BELLCRANK. WARPED. (CAN) DURING REPETITIVE INSPECTION OF ELEVATOR BELLCRANK AND AREA, AN AME NOTICED SLIGHT SIGNS OF CHAFFING AROUND UPPER AND LOWER ELEVATOR CABLE ATTACH POINTS. 
- [SDR CA110922005](https://openairdocs.org/sdr/CA110922005), Sep 21, 2011: HEAD. LOOSE. (CAN) PRESSURE GAUGE ON THE FIRE EXTINGUISHER READ ZERO. HEAD ASSY WAS FOUND TO BE LOOSE ON THE BOTTLE WHICH ALLOWED THE CONTENTS TO ESCAPE. FIRE EXTINGUISHER I
- [SDR CA110120003](https://openairdocs.org/sdr/CA110120003), Jan 19, 2011: O-RING. LEAKING. (CAN) THE AIRCRAFT HAD A FUEL LEAK THAT ONLY STARTED AFTER A HIGH POWER APPLICATION. UPON INSPECTION, IT WAS NOTED THE O-RING HAD PARTIALLY DISPLACED FROM AROUN
- [SDR CA100218011](https://openairdocs.org/sdr/CA100218011), Feb 11, 2010: OIL FILTER. SEPARATED. (CAN) INNER CONE (SCREEN) SEAMS ARE BECOMING UNGLUED. (TC 20100218011)
- [SDR CA080407010](https://openairdocs.org/sdr/CA080407010), Apr 2, 2008: CABLE. BROKEN. STEERING CABLE BROKE ON TAXI WHILE THE AIRCRAFT WAS PREPARING FOR TAKEOFF.
- [SDR CA080401004](https://openairdocs.org/sdr/CA080401004), Mar 26, 2008: ENGINE. POWER LOSS. ON TAKEOFF, THE LEFT ENGINE LAGGED BEHIND NOT PRODUCING MAX. POWER, TROUBLE SHOOTING FOUND THE TEMPERATURE COMPENSATOR UNIT LEAKING P3 AIR. THE PART WAS REPLACE
- [SDR CA070515002](https://openairdocs.org/sdr/CA070515002), May 14, 2007: COLLAR. CRACKED. (CAN) DURING MAINTENACE TO REPAIR THE NOSE GEAR ASSEMBLY IT WAS NOTED THAT THE STEERING COLLAR WAS CRACKED. THE NOSE GEAR WAS THEN FULLY DISASSEMBLED TO REMOVE 
- [SDR CA061219020](https://openairdocs.org/sdr/CA061219020), Nov 15, 2006: ENGINE. FAILED. (CAN) DURING TAXI, THE ENGINE EMITTED A NOISE AND LOST POWER. SUBSEQUENT INSPECTION REVEALED INTERNAL ENGINE DAMAGE. MFG WILL INVESTIGATE AND ADVISE OF ROOT CAU
- [SDR CA060315004](https://openairdocs.org/sdr/CA060315004), Mar 9, 2006: RELAY. FAILED. A/C SHUT DOWN AFTER FLT, CREW REPORTED NR 2 GENERATOR WARNING LIGHT DID NOT ILLUMINATE. A/C WAS RUN FOR TROUBLESHOOTING, DURING WHICH TIME GEN FUNCTIONED INTERM
- [SDR CA060208011](https://openairdocs.org/sdr/CA060208011), Feb 2, 2006: FCU. FLUCTUATES. (CAN) WHEN AC WAS ABOUT 10 MIN FROM LANDING, ON DESCENT, ENG POWER LEVERS WERE RETARDED FROM 38 LBS OF TORQUE. THE RT ENGINE TQ AND T5 STARTED FLUCTUATING. RT P
- [SDR CA061201005](https://openairdocs.org/sdr/CA061201005), Dec 28, 2005: RIB. CRACKED. (CAN) WHILE PERFORMING AD CF-82-21 R1 USING A BORESCOPE, CRACKS WERE FOUND AT THE ATTACHMENT POINT OF THE TORQUE TUBE TO THE ELEVATOR RIB. SEE PHOTOS AND DAMAGE
- [SDR AU510001605](https://openairdocs.org/sdr/AU510001605), Nov 7, 2005: FUEL SYS. FAULTY. FUEL SYSTEM SUSPECT FAULTY. LIMITED INFORMATION PROVIDED.
- [SDR CA051108004](https://openairdocs.org/sdr/CA051108004), Nov 4, 2005: PITOT HEAD. DAMAGED. (CAN) THE CAPTAIN REPORTED A 10 - 15 KTS SPLIT ON AIRSPEED INDICATIONS BETWEEN PILOT-F/O INDICATORS. MAINTENANCE INVESTIGATION REVEALED THAT THE CAPTAINS (LT) P
- [SDR CA050711007](https://openairdocs.org/sdr/CA050711007), Jul 8, 2005: STRUT. DAMAGED. (CAN) DURING WALKAROUND, THE FLIGHT CREW OBSERVED A RIVET HEAD MISSING FROM THE OUTSIDE OF THE LOWER LUG OF THE LT FORWARD FLOAT STRUT. THE AIRCRAFT WAS FERRIED
- [SDR AU510001604](https://openairdocs.org/sdr/AU510001604), Mar 6, 2005: PANEL. MISMARKED. NO LABELS ON DUAL RADIOS/INDICATORS AND ADVISORY LABELS AS REQUIRED BY ANO 108.34 SECTION 6.2.
- [SDR CA050309013](https://openairdocs.org/sdr/CA050309013), Mar 6, 2005: CSU. FAILED. (CAN) ON RUNUP AFTER INSTALLATION, IT WAS FOUND THAT THE OVERHAULED PROPELLER CONTROL UNIT WOULD NOT FUNCTION PROPERLY. THE PROPELLER REMAINED IN THE BETA MODE 
- [SDR CA050128007](https://openairdocs.org/sdr/CA050128007), Nov 20, 2004: HINGE BRACKET. DAMAGED. (CAN) LOOSE RIVETS ATTACHING CENTER FLAP HINGE BRACKET TO IB AND OB PORTIONS OF FORE FLAP ASSY. HIDDEN PROBLEM DOES NOT REALLY SHOW UP UNTILL YOU TAKE THE FLAP 
- [SDR CA040928014](https://openairdocs.org/sdr/CA040928014), Sep 27, 2004: ENGINE. FAILED. (CAN) ON DESCENT TO LAND, THE PILOT HEARD A LOUD BANG AND LOSS OF TQ IN THE LT ENGINE. ALL OTHER INDICATIONS WERE NORMAL. THEY SECURED THE LEFT ENGINE AND MADE 
- [SDR CA040804011](https://openairdocs.org/sdr/CA040804011), Aug 3, 2004: FUEL CONTROL. FAILED. (CAN) WHEN THE FLIGHT CREW REDUCED POWER ON FINAL APPROACH, NR 1 ENGINE FAILED TO RESPOND TO POWER LEVEL INPUT, AND REMAINED AT 15 LBS TORQUE. THE TORQUE THEN S
- [SDR CA030723005](https://openairdocs.org/sdr/CA030723005), Jul 19, 2003: SWITCH. MISINSTALLED. (CAN) NR 1 ENGINE, BETA BACK-UP SYSTEM, STEADY BLUE LIGHT ILLUMINATED IN CRUISE. FAULT FOUND TO BE KLIXON SPRING PN KX5, DRILLED MOUNTING HOLES NOT LINING UP WI
- [SDR AUS20030500](https://openairdocs.org/sdr/AUS20030500), Apr 24, 2003: CONTROL CABLE. FRAYED. (AUS) AILERON CABLES PNO C6CW1031-1 (2OFF) AND PNO C6CW1032-1 CONTAINED BROKEN STRANDS IN AREA OF WING ROOT FAIRLEADS.
- [SDR CA021120007](https://openairdocs.org/sdr/CA021120007), Nov 20, 2002: GEAR. WORN. (CAN) FUEL PUMP WAS REMOVED FROM ENGINE DURING ENGINE CONVERSION FROM PT6A-20 TO PT6A-27. THE PUMP WAS SENT TO PWC FOR BENCH TEST AND INHIBITING. CONTRACTOR ASS
- [SDR CA021011002](https://openairdocs.org/sdr/CA021011002), Sep 26, 2002: ENGINE. OVERTORQUED. (CAN) AIRCRAFT HIT LARGE WAVE SWELL AND CREW INADVERTENTLY ALLOWED POWER LEVER TO ADVANCE FORWARD TO OVER TORQUE ENGINE. POWER SECTION WAS REPLACED.
- [SDR CA020617004](https://openairdocs.org/sdr/CA020617004), May 27, 2002: COVER. FAILED. (CAN) THE PLASTIC COVER UNDER THE PILOT SEAT THAT PROTECTS THE AILERON PULLEY AND CABLE WAS DAMAGED. THE AIRCRAFT HIT SOME TURBULENCE AND A SMALL ROCK CAME OFF 
- [SDR CA020507013](https://openairdocs.org/sdr/CA020507013), Apr 24, 2002: BOLT. SHEARED. (CAN) DURING ENGINE REMOVAL OF A PT6A-20 FROM A DHC-6-200, TWO OF THE TWELVE (12) LEFT HAND ENGINE MOUNT BOLT SHEARED OFF. 1 BOLT TOP MOUNT, 1 BOLT R/H SIDE MOU
- [SDR AUS20011405](https://openairdocs.org/sdr/AUS20011405), Nov 26, 2001: BLADE. FAILED. (AUS) LT ENGINE INTERNAL FAILURE. INITIAL REPORTS INDICATE POWER TURBINE BLADE FAILURE.
- [SDR AU000563](https://openairdocs.org/sdr/AU000563), Jul 3, 2000: FIRE DETECTOR. FAULTY. (AUS) RIGHT ENGINE GEARBOX FIRE DETECTOR FAULTY. LOW RESISTANCE.
- [SDR CA000712019](https://openairdocs.org/sdr/CA000712019), Jul 3, 2000: BELLCRANK. TWISTED. (CAN) WHILE CARRYING OUT AD CF-72-06R4 PART III, THE ELEVATOR QUADRANT WAS FOUND TO BE RUBBING AGAINST THE SIDE OF THE CABLE GUARD AS DESCRIBED IN THE AD. THE Q
- [SDR CA000621009](https://openairdocs.org/sdr/CA000621009), Jun 10, 2000: ATTACH FITTING. CORRODED. (CAN) LEVEL 3 CORROSION FOUND ON PLATE BETWEEN ATTACH POINTS.
- [SDR CA000530012](https://openairdocs.org/sdr/CA000530012), May 15, 2000: BETA SWITCH. FAILED. (CAN) NR 2 ENGINE BETA BACK UNSERVICEABLE, PROPELLER REVERSES WITH NO BLUE LIGHT IN TEST MODE.
- [SDR CA000306008](https://openairdocs.org/sdr/CA000306008), Mar 6, 2000: ARMATURE. MISOVERHAULED. (CAN) PUMP WAS SENT FOR OVERHAUL. INTERNAL INSPECTION REVEALED THAT THE ARMATURE HAD BEEN MODIFIED BY REDUCING THE ARMATURE SHAFT SIZE AND SUBSTITUTING THE ORIG
- [SDR CA991209072](https://openairdocs.org/sdr/CA991209072), Nov 15, 1999: RIVET. LOOSE. (CAN) DURING INSPECTION OF THE ELEVATOR CONTROL SYSTEM, IT WAS NOTICED THAT THE PUSH PULL RIVETS WERE BLACK AND STAINED.THE PUSH PULL ROD WAS REMOVED FROM THE A
- [SDR CA991209002](https://openairdocs.org/sdr/CA991209002), Nov 11, 1999: LINER. WRONG PART. (CAN) UNIT SENT FOR OVERHAUL. DURING INSPECTION IT WAS NOTED THAT THE DRIVE END BALL BEARING LINER HAD BEEN REPAIRED WITH A COPPER LIKE PLATING, IN ORDER TO RES
- [SDR SMPA99002](https://openairdocs.org/sdr/SMPA99002), Aug 6, 1999: SPAR. CORRODED. PPG - DISCOVERED SEVERE CORROSION ON RT WING MAIN SPAR CAPS DURING AD 94-08-10, AND SP NR 57 INSPECTION. CORROSION WAS FOUND ON BOTH LOWER FORWARD AND AFT SPAR 
- [SDR SMPA99001](https://openairdocs.org/sdr/SMPA99001), Aug 6, 1999: SPAR. CORRODED. PPG - RIGHT WING WAS INSPECTED IAW AD 94-08-10 AND EMMA SP NR 57, MAIN SPAR CAP INSP FOR CORROSION. A SPOT OF CORROSION WAS FOUND ON THE LOWER FORWARD SPAR CAP 
- [SDR CA990715015](https://openairdocs.org/sdr/CA990715015), Apr 28, 1999: LINE. LEAKING. (CAN) AIRCRAFT PARKED FOR 5 MONTHS. ON INSPECTION, NOTED THAT FUEL WAS RUNNING DOWN STRUT. FUEL WAS NOTED COMING FROM STEEL BRAIDED LINE. TYPE 601 LINE MFD 2Q90
- [SDR AU981667](https://openairdocs.org/sdr/AU981667), Dec 20, 1998: DOOR. UNLOCKED. (AUS) ON ROTATION, THE DOOR UNSAFE WARNING ANNUNICATOR ILLUMINATED. DURING GROUND INVESTIGATION, THE RT EMERGENCY EXIT DOOR LATCHING MECHANISM WAS REMOVED AND I
- [SDR CA981202002](https://openairdocs.org/sdr/CA981202002), Nov 25, 1998: BRACKET. CORRODED. (CAN) ELEVATOR HINGE BRACKETS FOUND WITH EXFOLIATION CORROSION. LESS THAN HALF OF THE MATERIAL REMAINING.
- [SDR CA981207021](https://openairdocs.org/sdr/CA981207021), Nov 23, 1998: SKIN. CRACKED. (CAN) CRACK FOUND ON SKIN UNDER LOWER VHF BLADE ANTENNA. SERVICE BULLETIN 6/305 IN REGARD TO THIS AREA HAD NOT BEEN CARRIED OUT.
- [SDR CA981125027](https://openairdocs.org/sdr/CA981125027), Sep 16, 1998: ARMATURE. WRONG PART. (CAN) THE WRONG ARMATURE WAS FOUND IN THE STARTER/GENERATOR DURING OVERHAUL. THE ARMATURE SHOULD HAVE BEEN A 23048-1031. THE ARMATURE USED BELONGS TO AN APC 250

All 54: https://openairdocs.org/model/dehavilland-dhc-6-200/reports.md

## STCs that may be installed (OpenAirDocs) (227, 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 SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC
- [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC
- [STC SA1841NM](https://openairdocs.org/stc/SA1841NM): Installation of larger windows and the lowering of the seats. Twin Otter STC Holdings, LLC
- [STC SA12430IB](https://openairdocs.org/stc/SA12430IB): Installation of the Garmin G1000 NXi Integrated Flight Deck System. Aerocorp Avionics Solutions Inc
- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power supplies. Whelen Aerospace Technologies
- [STC SA7738SW](https://openairdocs.org/stc/SA7738SW): Installation of a freon air conditioning system. Twin Otter STC Holdings LLC
- [STC SA943EA](https://openairdocs.org/stc/SA943EA): Replacement of de Havilland wing bleed air ducting with alternate ducting. Texas Air Services Inc
- [STC SA03749NY](https://openairdocs.org/stc/SA03749NY): Installation of Garmin G950 Integrated Flight Deck System. Aerocorp Avionic Solutions Inc
- [STC SA12280IB](https://openairdocs.org/stc/SA12280IB): Installation of Wing and Outboard Fore Flap Trailing Edge Assemblies. Unity Aviation Canada Ltd
- [STC SA00887LA](https://openairdocs.org/stc/SA00887LA): Installation of Pitot Heater Fail Lights. Team J.A.S
- [STC SA02556LA](https://openairdocs.org/stc/SA02556LA): Installation of Passenger Utility Seats. Team J.A.S
- [STC SA02649LA](https://openairdocs.org/stc/SA02649LA): Installation of Max-Viz 2300 Enhanced Vision System. Team J.A.S
- [STC SA02730LA](https://openairdocs.org/stc/SA02730LA): Installation of High-Flow 250 AMP Starter-Generators. Team J.A.S
- [STC SA02806LA](https://openairdocs.org/stc/SA02806LA): Structural Provisions for AFT Camera Hatch. Team J.A.S
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA8709SW](https://openairdocs.org/stc/SA8709SW): Installation of a Traffic Alert and Collision Avoidance System I (TCAS I) model TCAS 791/791A. Acron Aviation Inc
- [STC SA09887AC](https://openairdocs.org/stc/SA09887AC): Installation of an Avionica MK-III mini Quick Access Recorder (QAR) and optional 4G or LTE Avionica Cellular Module (avCM. Aircraft Systems and Manufacturing Inc
- [STC SA39CH](https://openairdocs.org/stc/SA39CH): Installation of an Amphibian Landing Gear Position Advisory System/Laser Gear Advisory System. Wipaire Inc
- [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC
- [STC SA00196IB](https://openairdocs.org/stc/SA00196IB): Installation of the Replacement Aluminum Cargo Floor Panels. Rocky Mountain Aircraft
- [STC SA02380LA](https://openairdocs.org/stc/SA02380LA): Re-Life of the Viking Air Limited Model DHC-6 Series 100, 200 and 300 fuselage, horizontal stabilizer, and vertical stabilizer. IKHANA Group Inc
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA00171IB](https://openairdocs.org/stc/SA00171IB): Installation of the Radar Altimeter Mounts (Structural Provisions Only). Rocky Mountain Aircraft
- [STC SA00152IB](https://openairdocs.org/stc/SA00152IB): Installation of High Back Seat Modification. Kenn Borek Air Ltd
- [STC SA02457LA](https://openairdocs.org/stc/SA02457LA): Re-Life flight controls. IKHANA Group Inc
- [STC SA00129IB](https://openairdocs.org/stc/SA00129IB): Decommission of Standard Operators Options (S.O.O.) 6095 Fuel System. Kenn Borek Air Ltd
- [STC SA00085IB](https://openairdocs.org/stc/SA00085IB): Installation of Elevator Replacement Trailing Edge. Rocky Mountain Aircraft
- [STC SA02010WI](https://openairdocs.org/stc/SA02010WI): Installation of the Mid-Continent Instruments & Avionics MD23 FLEX Custom Function Display (CFD). Mid-Continent Instruments and Avionics
- [STC SA04550AT](https://openairdocs.org/stc/SA04550AT): Main Wheel and Brake Assembly for the Viking Air DHC-6 Series aircraft. PMA Design and Manufacturing
- [STC SA1065GL](https://openairdocs.org/stc/SA1065GL): Install Aircraft Wheel and Brake CONVERSION Kit 199-92, N/C. KAMAN Corporation Aircraft Wheel and Brake LLC
- [STC SA00061IB](https://openairdocs.org/stc/SA00061IB): Activation of the Garmin GTN 750 (Xi) TAWS-A. Rocky Mountain Aircraft
- [STC SA00060IB](https://openairdocs.org/stc/SA00060IB): Installation of LED Replacement Cockpit Panels. Rocky Mountain Aircraft
- [STC SA00054IB](https://openairdocs.org/stc/SA00054IB): Installation of Pitot Heat Indication System. Rocky Mountain Aircraft
- [STC SA00042IB](https://openairdocs.org/stc/SA00042IB): Installation of Engine Chip Detectors. Rocky Mountain Aircraft
- [STC SA02254AK](https://openairdocs.org/stc/SA02254AK): Installation of "Single Screen", "2 or 3 Screen", "Dual Screen", or "4 or 6 screen". Genesys Aerosystems Inc
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA04701NY](https://openairdocs.org/stc/SA04701NY): Replacement of Fixed Wing Control Cables. Thunder Bay Aviation Ltd
- [STC SA04698NY](https://openairdocs.org/stc/SA04698NY): Approval of an Controlled Aircraft Equipment Configuration providing for the authorized use of Transmitting Portable Electronic Devices (TPED). Kilroy Aviation LLC
- [STC SA00282NY](https://openairdocs.org/stc/SA00282NY): Replacement latches on upper and lower cargo door. PMA Design & Manufacturing Inc
- [STC SA00160LA](https://openairdocs.org/stc/SA00160LA): Installation of IKHANA Aircraft Services wing box assembly. IKHANA Group Inc
- [STC SA04587NY](https://openairdocs.org/stc/SA04587NY): Installation of Acorn Welding C6SC1107-NG Exhaust stacks. Acorn Welding Ltd
- [STC SA04672NY](https://openairdocs.org/stc/SA04672NY): Installation of the Emergency Cabin Lighting System. Aerocorp Avionic Solutions Inc
- [STC SA09856AC](https://openairdocs.org/stc/SA09856AC): Installation of BendixKing Aerowave 100 In-flight Data Link System for non-essential, non-required aircraft Cabin Systems & Equipments. Honeywell International Inc (Bendix King)
- [STC SA11174SC PAGE 2](https://openairdocs.org/stc/SA11174SC%20PAGE%202): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC
- [STC SA04623NY](https://openairdocs.org/stc/SA04623NY): Installation of Type 1 (PAA Design group) DHC-6 Twin Otter Seats. Regent Aircraft Services
- [STC SA02075SE](https://openairdocs.org/stc/SA02075SE): Installation of a Mid-Continent MD835( ) Lithium Ion Battery. Mid-Continent Instrument Co. Inc

All 227: https://openairdocs.org/model/dehavilland-dhc-6-200/stcs.md

## PMA parts (OpenAirDocs) (over 1,000, 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.

- [9143FR-0200](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195053467420260909221038.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026
- [9143FR](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173233226220260909221038.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026
- [9143FR-0100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162603096220260909221038.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026
- [9143FR-0315](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154342368020260909221039.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026
- [9143FR-0325](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117837139520260909221039.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026
- [PDMC6FSM3730-29](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151556801720260705233110.0001): Guide Locking Pin Assembly. PMA Design & Manufacturing · PMA PQ1570CE · Replaces C6FSM3730-29 · Jun 1, 2026
- [PDMC6FSM2699-27](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124999350220260705233109.0001): Guide Block Assembly. PMA Design & Manufacturing · PMA PQ1570CE · Replaces C6FSM2699-27 · Jun 1, 2026
- [KAC3FF30-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103142174820260512112234.0001): Clamp – Fwd Pilot’s Seat Support. Kenmore Air Harbor LLC · PMA PQ1939NM · Replaces C3FF30-3 · May 6, 2026
- [TAS1002-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190891927220260522104407.0001): Overboard Vent Assy. Texas Air Services, Inc. · PMA PQ1041SW · Modification part · Apr 28, 2026
- [TAS1001-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184626060420260522104406.0001): Duct Assy & Details. Texas Air Services, Inc. · PMA PQ1041SW · Modification part · Apr 28, 2026
- [TAS1004-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174088256520260522104407.0001): Gasket. Texas Air Services, Inc. · PMA PQ1041SW · Modification part · Apr 28, 2026
- [TAS1005-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171738474320260522104407.0001): Spacer. Texas Air Services, Inc. · PMA PQ1041SW · Modification part · Apr 28, 2026
- [TAS1003-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID153876420020260522104407.0001): Doubler. Texas Air Services, Inc. · PMA PQ1041SW · Modification part · Apr 28, 2026
- [TAS1006-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131262830720260522104408.0001): Bellows Assy. Texas Air Services, Inc. · PMA PQ1041SW · Modification part · Apr 28, 2026
- [TASX229-181](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121369529620260522104408.0001): Clamp Assy. Texas Air Services, Inc. · PMA PQ1041SW · Modification part · Apr 28, 2026
- [APS160-01100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194850003020260313134801.0001): Air Valve Assy. Airforms LLC · PMA PQ2644CE · Replaces 160-01100, TR747-05 · Mar 9, 2026
- [APS162-03400](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186997995320260313134725.0001): Outer Wheel Half. Airforms LLC · PMA PQ2644CE · Replaces 162-03400, 161-03401 · Mar 9, 2026
- [APS161-13301](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186020852720260313134758.0001): Inner Wheel Half. Airforms LLC · PMA PQ2644CE · Replaces 161-13301 · Mar 9, 2026
- [APS153-00900](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID158444971020260313134732.0001): Ring-Grease Seal. Airforms LLC · PMA PQ2644CE · Replaces 153-00900 · Mar 9, 2026
- [APS154-03900](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID158225973920260313134802.0001): Molded Grease Seal. Airforms LLC · PMA PQ2644CE · Replaces 154-03900 · Mar 9, 2026
- [APS040-21101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155282574620260313134757.0001): 11.00-12 Wheel Assy. Airforms LLC · PMA PQ2644CE · Replaces 040-21101 · Mar 9, 2026
- [APS214-01400](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155171304720260313134737.0001): Cone-Bearing. Airforms LLC · PMA PQ2644CE · Replaces 214-01400, LM29749-20629, 214-30795-2 · Mar 9, 2026
- [APS158-01700](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152008728020260313134804.0001): Hub Cap. Airforms LLC · PMA PQ2644CE · Replaces 158-01700 · Mar 9, 2026
- [APS214-09200](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID150826604820260313134802.0001): Cone-Bearing. Airforms LLC · PMA PQ2644CE · Replaces 214-09200, 39250-20629 · Mar 9, 2026
- [APS40-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149502255320260313134721.0001): 7.50-10 Wheel Assy. Airforms LLC · PMA PQ2644CE · Replaces 40-101, 40-101D · Mar 9, 2026
- [APS214-39412](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148872661220260313134759.0001): Cup-Bearing. Airforms LLC · PMA PQ2644CE · Replaces 214-39412, 39412-20629 · Mar 9, 2026
- [APS214-01300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146514109820260313134727.0001): Cup-Bearing. Airforms LLC · PMA PQ2644CE · Replaces 214-01300, LM29710-20629, 214-30795-1 · Mar 9, 2026
- [APS155-08300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142759621320260313134804.0001): Snap Ring. Airforms LLC · PMA PQ2644CE · Replaces 155-08300 · Mar 9, 2026
- [APS155-00100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139559416620260313134735.0001): Snap Ring. Airforms LLC · PMA PQ2644CE · Replaces 155-00100 · Mar 9, 2026
- [APS162-12401](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID138422211520260313134800.0001): Outer Wheel Half. Airforms LLC · PMA PQ2644CE · Replaces 162-12401 · Mar 9, 2026
- [APS067-06300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128321287520260313134729.0001): Spacer. Airforms LLC · PMA PQ2644CE · Replaces 067-06300 · Mar 9, 2026
- [APS161-03600](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125910952420260313134723.0001): Inner Wheel Half. Airforms LLC · PMA PQ2644CE · Replaces 161-03600, 161-03601 · Mar 9, 2026
- [APS158-00300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104911189920260313134740.0001): Hub Cap. Airforms LLC · PMA PQ2644CE · Replaces 158-00300 · Mar 9, 2026
- [650-0100-05](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149139328720250918135512.0001): avCM LTE. Avionica LLC. · PMA PQ1734CE · Modification part · Jun 20, 2025
- [650-0100-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124455338920250918135509.0001): avCM 4G. Avionica LLC. · PMA PQ1734CE · Modification part · Jun 20, 2025
- [804-1201, 804-1205, 804-1205-03, 804-1212, 804-1216](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108510883820250918135507.0001): miniQAR MKIII. Avionica LLC. · PMA PQ1734CE · Modification part · Jun 20, 2025
- [MQAR-Y-XXXXZZZZ#](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102387109620250918135514.0001): miniQAR Installation Kit. Avionica LLC. · PMA PQ1734CE · Modification part · Jun 20, 2025
- [WF19310-30](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190180238420250624152914.0001): Filter Element. Donaldson Company Inc · PMA PQ2432CE · Replaces S4-19310-30 · Jun 2, 2025
- [9520218AB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172114135320250617112735.0001): Bolt, Wheel. Aero Brake & Spares Inc · PMA PQ0694SW · Replaces 9520218 · Jan 23, 2025
- [PM-76](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184469513420251118174441.0001): Radome Mask. PM Research, Inc. · PMA PQ10049NE · Modification part · Dec 16, 2024
- [PDMC6FSM1734-1CR](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139176996820250724165930.0001): Hinge Assembly. PMA Design & Manufacturing · PMA PQ1570CE · Replaces C6FSM1734-1 · Nov 7, 2024
- [M06-201100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183943991720241022163142.0001): Label. Miraj Corporation · PMA PQ0870NE · Replaces Safran 06-201100 · Oct 10, 2024
- [MQAR-Y-XXXXZZZZ#](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164906975020240924135409.0001): miniQAR Installation Kit. Avionica LLC. · PMA PQ1734CE · Modification part · Sep 20, 2024
- [9143FR-0250](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195800852920240826152109.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 22, 2024
- [9143FR-2400](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167804689420240826152110.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 22, 2024
- [9143FR-0375](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143354690920240826152110.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 22, 2024
- [9143FR-0075](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139731902220240826152108.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 22, 2024
- [9143FR-0125](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133796165320240826152109.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 22, 2024
- [9143FR-0300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132573376120240826152109.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 22, 2024
- [9143FR-0225](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110178059620240826152109.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 22, 2024

All of them: https://openairdocs.org/model/dehavilland-dhc-6-200/pma.md

## The same model under other registry codes

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

- [Dehavilland Acft Of Canada DHC-6-200](https://openairdocs.org/model/dehavilland-acft-of-canada-dhc-6-200): 0 registered aircraft, registry code 2805150

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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.