# Hughes Helicopters 369E

- Type: Aircraft model (FAA registry)
- Registry code: 4470707
- Manufacturer (registry): HUGHES HELICOPTERS INC
- Model: 369E
- Aircraft type: Rotorcraft
- Category: Rotorcraft
- Engines: 1 · Turbo-shaft
- Seats: 4
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS H3WE](https://openairdocs.org/tcds/H3WE) (OpenAirDocs)
- Holder: MD Helicopters LLC
- Registered aircraft: 29
- Page: https://openairdocs.org/model/hughes-helicopters-369e

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 2026-21-05](https://openairdocs.org/ad/2026-21-05): Engine/transmission coupling · MD Helicopters 369D, 369E, 369F and 3 more. Effective Nov 27, 2026
- [AD 2026-19-01](https://openairdocs.org/ad/2026-19-01): Rotorcraft flight control · MD Helicopters 369, 369 (Army YOH-6A), 369A and 11 more. Effective Oct 20, 2026
- [AD 2025-17-11](https://openairdocs.org/ad/2025-17-11): tail rotor control system · MD Helicopters 369 (Army YOH-6A), 369A (Army OH-6A), 369D and 9 more. Effective Oct 10, 2025
- [AD 2024-20-07](https://openairdocs.org/ad/2024-20-07): Emergency Equipment; Emergency Flotation Section · Apical Emergency Float Kit, P/N 20498 (STC SR00780LA or 12 others). Effective Dec 5, 2024
- [AD 2023-11-07](https://openairdocs.org/ad/2023-11-07): Ground Proximity System · Airbus Helicopters 47, 206, 210 and 237 more. Effective Jun 22, 2023
- [AD 2021-22-11](https://openairdocs.org/ad/2021-22-11): Tail Rotor Control System · MD Helicopters 369D, 369E, 369F and 7 more. Effective Jan 10, 2022
- [AD 2020-18-20](https://openairdocs.org/ad/2020-18-20): Main Rotor Blade · MD Helicopters 369A, 369D, 369E and 7 more. Effective Oct 28, 2020
- [AD 2020-11-07](https://openairdocs.org/ad/2020-11-07): Main Rotor System · MD Helicopters 369D, 369E, 369FF and 6 more. Effective Jun 30, 2020
- [AD 2019-05-04](https://openairdocs.org/ad/2019-05-04): Main Rotor Blade · MD Helicopters 369A, 369D, 369E and 7 more. Effective Apr 17, 2019
- [AD 2016-05-09](https://openairdocs.org/ad/2016-05-09): Fuel Quantity Indicating System · MD Helicopters 369A, 369D, 369E and 7 more. Effective Apr 15, 2016
- [AD 2016-04-15](https://openairdocs.org/ad/2016-04-15): Main Rotor Blades · MD Helicopters 369A, 369D, 369E and 6 more. Effective Mar 31, 2016
- [AD 2013-19-24](https://openairdocs.org/ad/2013-19-24): Tail Rotor Blades · MD Helicopters 369A, 369D, 369E and 6 more. Effective Dec 5, 2013
- [AD 2013-05-16](https://openairdocs.org/ad/2013-05-16): Tailboom assembly · MD Helicopters 369D, 369E, 369F and 1 more. Effective Apr 30, 2013
- [AD 2008-15-03](https://openairdocs.org/ad/2008-15-03): Tail rotor (T/R) blade abrasion strip · MD Helicopters 369A, 369D, 369E and 6 more. Effective Sep 3, 2008
- [AD 2007-12-23](https://openairdocs.org/ad/2007-12-23): Landing gear fairing support assembly · MD Helicopters 369A, 369D, 369E and 7 more. Effective Jul 19, 2007
- [AD 2007-09-51](https://openairdocs.org/ad/2007-09-51): Tail rotor blade · MD Helicopters 369, 369A, 369D and 7 more. Effective Jul 5, 2007
- [AD 2005-21-02](https://openairdocs.org/ad/2005-21-02): Main rotor blade (blade) · Main rotor blades P/N 500P2300-501/503/505 (Helicopter Technology STC SR01050LA or 2 others). Effective Nov 1, 2005
- [AD 2002-13-05 R1](https://openairdocs.org/ad/2002-13-05-R1): Tail rotor gearbox · Aerometals tailboom, P/N 369X23500-505, 507 (STC SH5055NM or SH4801NM). Effective Feb 25, 2003
- [AD 2000-25-52](https://openairdocs.org/ad/2000-25-52): Main rotor blade · MD Helicopters 369A, 369D, 369E and 6 more. Effective Feb 6, 2001
- [AD 2000-08-22](https://openairdocs.org/ad/2000-08-22): Turbine Outlet Temperature (TOT) Indicating System · MD Helicopters 369D, 369E, 500N and 1 more. Effective May 22, 2000
- [AD 99-20-12](https://openairdocs.org/ad/99-20-12): Bracket P/N 369F5190-1 · MD Helicopters 369D, 369E, 369FF and 2 more. Effective Nov 4, 1999
- [AD 99-13-09](https://openairdocs.org/ad/99-13-09): Fork Assembly Inspection · MD Helicopters 369D and 369E. Effective Aug 4, 1999
- [AD 99-08-07](https://openairdocs.org/ad/99-08-07): Engine Control And Warning System · MD Helicopters 369E, 369FF, 500N and 1 more. Effective Apr 21, 1999
- [AD 99-04-12](https://openairdocs.org/ad/99-04-12): Input Shaft Coupling Assembly · MD Helicopters 369D, 369E, 369FF and 3 more. Effective Mar 23, 1999
- [AD 98-21-12](https://openairdocs.org/ad/98-21-12): Overrunning Clutch Retainer Inspection · MD Helicopters 369D, 369E, 369FF and 1 more. Effective Oct 22, 1998
- [AD 98-15-26](https://openairdocs.org/ad/98-15-26): Main Rotor Blade Cracking Inspection · MD Helicopters 369A, 369D, 369E and 8 more. Effective Aug 3, 1998
- [AD 98-09-02](https://openairdocs.org/ad/98-09-02): Overrunning Clutch Assembly Outer Race · MD Helicopters 369, 369A, 369D and 8 more. Effective May 6, 1998
- [AD 97-15-08](https://openairdocs.org/ad/97-15-08): Transmission Output Drive Gear · MD Helicopters 369D, 369E, 369F and 2 more. Effective Aug 4, 1997
- [AD 96-10-09](https://openairdocs.org/ad/96-10-09): Blade Root End Crack Inspection · MD Helicopters 369, 369A, 369D and 8 more. Effective May 29, 1996
- [AD 96-08-03](https://openairdocs.org/ad/96-08-03): Hardpoint Assemblies · Hardpoints (Flight Trails Helicopters STC SH6080NM). Effective May 20, 1996
- [AD 95-03-13](https://openairdocs.org/ad/95-03-13): Main Rotor Blade Attach Lugs · MD Helicopters 369, 369A, 369D and 7 more. Effective Mar 21, 1995
- [AD 95-03-11](https://openairdocs.org/ad/95-03-11): Tail Rotor Bade Inspection · MD Helicopters 369, 369A, 369D and 7 more. Effective Mar 1, 1995
- [AD 94-24-04](https://openairdocs.org/ad/94-24-04): Pitch Control Assembly · MD Helicopters 369D, 369E, 369F and 1 more. Effective Dec 13, 1994
- [AD 93-18-05](https://openairdocs.org/ad/93-18-05): Fuel Vent Line · MD Helicopters 369D, 369E, 369F and 2 more. Effective Dec 21, 1993
- [AD 93-07-10](https://openairdocs.org/ad/93-07-10): Airspeed Limitations · External cargo container (Gajon Associates STC SH1134EA). Effective Jul 6, 1993
- [AD 94-18-08](https://openairdocs.org/ad/94-18-08): Tail Rotor Blade Inspection · MD Helicopters 369, 369A, 369D and 7 more. Effective Jan 13, 1992
- [AD 91-08-02](https://openairdocs.org/ad/91-08-02): Tail Rotor Blades · MD Helicopters 369, 369A, 369D and 7 more. Effective May 3, 1991
- [AD 90-24-07](https://openairdocs.org/ad/90-24-07): Main Rotor Transmission Bolts · MD Helicopters 369D, 369E, 369F and 1 more. Effective Dec 10, 1990
- [AD 81-26-01 R1](https://openairdocs.org/ad/81-26-01-R1): Main Rotor Drive Shaft · MD Helicopters 369, 369A, 369D and 7 more. Effective Oct 31, 1990
- [AD 90-19-02](https://openairdocs.org/ad/90-19-02): Clutch Assembly · MD Helicopters 369, 369A, 369D and 7 more. Effective Oct 5, 1990
- [AD 89-02-01 R1](https://openairdocs.org/ad/89-02-01-R1): Main Rotor Blade Strap Assemblies · MD Helicopters 369D, 369E, 369F and 1 more. Effective Jul 19, 1990
- [AD 90-12-03](https://openairdocs.org/ad/90-12-03): Tail Rotor Bearing Assembly · MD Helicopters 369D, 369E, 369F and 1 more. Effective Jun 22, 1990
- [AD 90-01-08](https://openairdocs.org/ad/90-01-08): Driveshaft Coupling · MD Helicopters 369, 369A, 369D and 7 more. Effective Feb 5, 1990
- [AD 88-17-09 R1](https://openairdocs.org/ad/88-17-09-R1): Tail Rotor Transmission · MD Helicopters 369D, 369E, 369F and 1 more. Effective Dec 26, 1989
- [AD 89-23-14](https://openairdocs.org/ad/89-23-14): Main Rotor Collective Tubes · MD Helicopters 369, 369A, 369D and 7 more. Effective Dec 4, 1989
- [AD 89-20-02](https://openairdocs.org/ad/89-20-02): Tail Rotor Hubs · MD Helicopters 369D and 369E. Effective Oct 16, 1989
- [AD 87-18-12 R1](https://openairdocs.org/ad/87-18-12-R1): Main Rotor Transmission · MD Helicopters 369D, 369E, 369F and 1 more. Effective Jan 15, 1988
- [AD 87-18-11](https://openairdocs.org/ad/87-18-11): Main Rotor Transmission And Drive Shaft · MD Helicopters 369D, 369E, 369F and 1 more. Effective Sep 1, 1987
- [AD 86-20-07](https://openairdocs.org/ad/86-20-07): Tail Rotor Drive Shaft · MD Helicopters 369, 369A, 369D and 5 more. Effective Oct 24, 1986
- [AD 86-01-04](https://openairdocs.org/ad/86-01-04): Tail Rotor Blades · MD Helicopters 369, 369A, 369D and 7 more. Effective Feb 14, 1986

Historical (superseded or no longer in force):

- [AD 2024-23-06](https://openairdocs.org/ad/2024-23-06) (historical): Rotorcraft Flight Control · MD Helicopters 369, 369A, 369D and 11 more. Effective Dec 24, 2024
- [AD 2021-23-13](https://openairdocs.org/ad/2021-23-13) (historical): Ground Proximity System · Airbus Helicopters K-225, K-190A, K-240 and 237 more. Effective Dec 9, 2021
- [AD 2003-24-01](https://openairdocs.org/ad/2003-24-01) (historical): Main rotor blade (blade) · Replacement main rotor blade (Helicopter Technology STC SR09074RC or 2 others). Effective Dec 10, 2003
- [AD 2003-08-51](https://openairdocs.org/ad/2003-08-51) (historical): Tail rotor blade pitch horn (pitch horn) · MD Helicopter 369A, 369D, 369E and 6 more. Effective Jul 17, 2003
- [AD 2002-13-05](https://openairdocs.org/ad/2002-13-05) (historical): Tail rotor gearbox · Modification of tailboom attaching hardware (Aerometals STC SH4801NM or SH5055NM). Effective Aug 1, 2002
- [AD 2000-24-51](https://openairdocs.org/ad/2000-24-51) (historical): Blade Spar · MD Helicopter 369A, 369D, 369E and 6 more

All 62: https://openairdocs.org/model/hughes-helicopters-369e/ads.md

## Information bulletins (advisory) (3)

- [SAIB AIR-21-19R1](https://openairdocs.org/saib/AIR-21-19R1): AERIAL TOW EQUIPMENT, Side Pull Hook. Issued Nov 29, 2021
- [SAIB AIR-21-19](https://openairdocs.org/saib/AIR-21-19) (historical): AERIAL TOW EQUIPMENT, Side Pull Hook. Issued Nov 29, 2021
- [SAIB SW-12-45](https://openairdocs.org/saib/SW-12-45): Garmin Model 400W/500W Series GPS-WAAS Navigation System. Issued Oct 3, 2012

## Registered aircraft (29)

- [N165H](https://openairdocs.org/aircraft/N165H): [Midvale Air Research LLC](https://openairdocs.org/faa-owner/MIDVALE%20AIR%20RESEARCH%20LLC), [Lewes, DE](https://openairdocs.org/faa-place/DE/Lewes), built 1985, S/N 0150E
- [N297E](https://openairdocs.org/aircraft/N297E): [County Of Kern](https://openairdocs.org/faa-owner/COUNTY%20OF%20KERN), [Bakersfield, CA](https://openairdocs.org/faa-place/CA/Bakersfield), S/N 197E
- [N298PP](https://openairdocs.org/aircraft/N298PP): [Gillespie Flying Services LLC](https://openairdocs.org/faa-owner/GILLESPIE%20FLYING%20SERVICES%20LLC), [Trenton, SC](https://openairdocs.org/faa-place/SC/Trenton), built 1982, S/N 0006E
- [N299DR](https://openairdocs.org/aircraft/N299DR): [Kings County Sheriffs Office](https://openairdocs.org/faa-owner/KINGS%20COUNTY%20SHERIFFS%20OFFICE), [Hanford, CA](https://openairdocs.org/faa-place/CA/Hanford), built 1986, S/N 196E
- [N369JH](https://openairdocs.org/aircraft/N369JH): [Jack Harter Helicopters Inc](https://openairdocs.org/faa-owner/JACK%20HARTER%20HELICOPTERS%20INC), [Lihue, HI](https://openairdocs.org/faa-place/HI/Lihue), built 1985, S/N 0145E
- [N369KD](https://openairdocs.org/aircraft/N369KD): [Dairy Air LLC](https://openairdocs.org/faa-owner/DAIRY%20AIR%20LLC), [Scottsdale, AZ](https://openairdocs.org/faa-place/AZ/Scottsdale), built 1983, S/N 0037E
- [N415WC](https://openairdocs.org/aircraft/N415WC): [Wilson Construction Co](https://openairdocs.org/faa-owner/WILSON%20CONSTRUCTION%20CO), [Canby, OR](https://openairdocs.org/faa-place/OR/Canby), built 1981, S/N 0005E
- [N42FF](https://openairdocs.org/aircraft/N42FF): [Beef Aviation LLC](https://openairdocs.org/faa-owner/BEEF%20AVIATION%20LLC), [Bradenton, FL](https://openairdocs.org/faa-place/FL/Bradenton), built 1984, S/N 0141E
- [N458PB](https://openairdocs.org/aircraft/N458PB): [Barbaro Paul G](https://openairdocs.org/faa-owner/BARBARO%20PAUL%20G), [Argyle, TX](https://openairdocs.org/faa-place/TX/Argyle), built 1985, S/N 0123E
- [N500AR](https://openairdocs.org/aircraft/N500AR): [Helicopter Roundup Service LLC](https://openairdocs.org/faa-owner/HELICOPTER%20ROUNDUP%20SERVICE%20LLC), [Nephi, UT](https://openairdocs.org/faa-place/UT/Nephi), S/N 0149E
- [N500LK](https://openairdocs.org/aircraft/N500LK): [Winco Inc](https://openairdocs.org/faa-owner/WINCO%20INC), [Aurora, OR](https://openairdocs.org/faa-place/OR/Aurora), built 1983, S/N 0009E
- [N500TY](https://openairdocs.org/aircraft/N500TY): [Southern Aircraft Consultancy Inc Trustee](https://openairdocs.org/faa-owner/SOUTHERN%20AIRCRAFT%20CONSULTANCY%20INC%20TRUSTEE), [Casper, WY](https://openairdocs.org/faa-place/WY/Casper), built 1984, S/N 0086E
- [N5200W](https://openairdocs.org/aircraft/N5200W): [Emerald City Aircraft Leasing Inc](https://openairdocs.org/faa-owner/EMERALD%20CITY%20AIRCRAFT%20LEASING%20INC), [Port Orchard, WA](https://openairdocs.org/faa-place/WA/Port%20Orchard), S/N 0025E
- [N5238C](https://openairdocs.org/aircraft/N5238C): [Aviation Advantage Inc](https://openairdocs.org/faa-owner/AVIATION%20ADVANTAGE%20INC), [Tabor City, NC](https://openairdocs.org/faa-place/NC/Tabor%20City), S/N 0151E
- [N5245P](https://openairdocs.org/aircraft/N5245P): [Flight Level Zero LLC](https://openairdocs.org/faa-owner/FLIGHT%20LEVEL%20ZERO%20LLC), [Othello, WA](https://openairdocs.org/faa-place/WA/Othello), S/N 0140E
- [N538ST](https://openairdocs.org/aircraft/N538ST): [J&J Holdings And Investments LLC](https://openairdocs.org/faa-owner/J%26J%20HOLDINGS%20AND%20INVESTMENTS%20LLC), [Phoenix, AZ](https://openairdocs.org/faa-place/AZ/Phoenix), S/N 0192E
- [N54PD](https://openairdocs.org/aircraft/N54PD): [Cameron Kenneth D](https://openairdocs.org/faa-owner/CAMERON%20KENNETH%20D), [Montgomery, TX](https://openairdocs.org/faa-place/TX/Montgomery), S/N 0180E
- [N550JM](https://openairdocs.org/aircraft/N550JM): [National Aggregates Inc](https://openairdocs.org/faa-owner/NATIONAL%20AGGREGATES%20INC), [Malvern, OH](https://openairdocs.org/faa-place/OH/Malvern), built 1982, S/N 0013E
- [N59SD](https://openairdocs.org/aircraft/N59SD): [International Air Services Inc Trustee](https://openairdocs.org/faa-owner/INTERNATIONAL%20AIR%20SERVICES%20INC%20TRUSTEE), [Carson City, NV](https://openairdocs.org/faa-place/NV/Carson%20City), built 1983, S/N 0019E
- [N66SD](https://openairdocs.org/aircraft/N66SD): [Enforcement Aviation Services Inc](https://openairdocs.org/faa-owner/ENFORCEMENT%20AVIATION%20SERVICES%20INC), [Midway City, CA](https://openairdocs.org/faa-place/CA/Midway%20City), built 1985, S/N 0147E
- [N757TB](https://openairdocs.org/aircraft/N757TB): [White Bird LLC](https://openairdocs.org/faa-owner/WHITE%20BIRD%20LLC), [Campobello, SC](https://openairdocs.org/faa-place/SC/Campobello), S/N 0166E
- [N765KV](https://openairdocs.org/aircraft/N765KV): [Winco Inc](https://openairdocs.org/faa-owner/WINCO%20INC), [Aurora, OR](https://openairdocs.org/faa-place/OR/Aurora), built 1984, S/N 0082E
- [N774CB](https://openairdocs.org/aircraft/N774CB): [Cbhelos LLC](https://openairdocs.org/faa-owner/CBHELOS%20LLC), [Chesapeake, VA](https://openairdocs.org/faa-place/VA/Chesapeake), built 1983, S/N 0016E
- [N805MD](https://openairdocs.org/aircraft/N805MD): [Integrity Aircaft Title Holdings LLC](https://openairdocs.org/faa-owner/INTEGRITY%20AIRCAFT%20TITLE%20HOLDINGS%20LLC), [Portland, OR](https://openairdocs.org/faa-place/OR/Portland), built 1986, S/N 0168E
- [N842JH](https://openairdocs.org/aircraft/N842JH): [Jack Harter Helicopters Inc](https://openairdocs.org/faa-owner/JACK%20HARTER%20HELICOPTERS%20INC), [Lihue, HI](https://openairdocs.org/faa-place/HI/Lihue), built 1983, S/N 0020E
- [N888EV](https://openairdocs.org/aircraft/N888EV): [Top Flight Aviation Of Mississippi LLC](https://openairdocs.org/faa-owner/TOP%20FLIGHT%20AVIATION%20OF%20MISSISSIPPI%20LLC), [Picayune, MS](https://openairdocs.org/faa-place/MS/Picayune), built 1985, S/N 0152E
- [N911CP](https://openairdocs.org/aircraft/N911CP): [St Louis County Police Department](https://openairdocs.org/faa-owner/ST%20LOUIS%20COUNTY%20POLICE%20DEPARTMENT), [Clayton, MO](https://openairdocs.org/faa-place/MO/Clayton), built 1984, S/N 0105E
- [N9460T](https://openairdocs.org/aircraft/N9460T): [Evermore Aviation LLC](https://openairdocs.org/faa-owner/EVERMORE%20AVIATION%20LLC), [Wasilla, AK](https://openairdocs.org/faa-place/AK/Wasilla), built 1988, S/N 0238E
- [N98CP](https://openairdocs.org/aircraft/N98CP): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 1985, S/N 0155E

## NTSB investigations (25)

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 ERA24FA075](https://openairdocs.org/ntsb/ERA24FA075), Dec 27, 2023: Hughes Helicopters 369E (N757TB), Miami, FL, substantial damage, 1 fatal. Probable cause: Main rotor contact with the tail boom for unknown reasons, resulting in the separation of the tail boom.
- [NTSB WPR22LA305](https://openairdocs.org/ntsb/WPR22LA305), Aug 15, 2022: Hughes Helicopters 369E (N500AR), Ely, NV, substantial damage. Probable cause: The pilot’s failure to maintain clearance from terrain while maneuvering at a low altitude.
- [NTSB GAA18CA117](https://openairdocs.org/ntsb/GAA18CA117), Feb 1, 2018: Hughes Helicopters 369 (N618SG), Wrightwood, CA, substantial damage. Probable cause: The pilot’s high altitude, high gross weight landing with insufficient tail rotor thrust resulting in a loss of tail rotor effectiveness.
- [NTSB ERA17LA209](https://openairdocs.org/ntsb/ERA17LA209), Jun 23, 2017: Hughes 369 (N765KV), Dennis, WV, substantial damage. Probable cause: The unporting of fuel due to the helicopter's nose-up attitude during long line operations, which resulted in fuel starvation and a total loss of engine power.
- [NTSB WPR12LA328](https://openairdocs.org/ntsb/WPR12LA328), Jul 26, 2012: Hughes Helicopters 369E (N427WC), The Dalles, OR, substantial damage. Probable cause: The loss of engine power due to fuel starvation, which resulted from the fuel tank supply pickup becoming unported while the helicopter was pulling power lines.
- [NTSB SEA07LA021](https://openairdocs.org/ntsb/SEA07LA021), Nov 21, 2006: Hughes 369E (N500FU), Jensen, UT, substantial damage, 1 fatal. Probable cause: The pilot's failure to maintain clearance with the transmission wires due to an inadquate visual lookout while maneuvering during a search and rescue flight.
- [NTSB SEA05CA200](https://openairdocs.org/ntsb/SEA05CA200), Sep 24, 2005: McDonnell Douglas 369E (N5207C), Medford, OR, substantial damage. Probable cause: In-flight collision with terrain during a precautionary landing. Factors include instrument meteorological conditions and pilot disorientation.
- [NTSB SEA05CA173](https://openairdocs.org/ntsb/SEA05CA173), Aug 16, 2005: Hughes 369E (N500FU), Donnelly, ID, substantial damage. Probable cause: The pilot's failure to maintain clearance of a tree during a landing attempt due to loss of visibility from a self induced brown-out condition. Contributing factors were the pilot's failure to…
- [NTSB SEA03TA116](https://openairdocs.org/ntsb/SEA03TA116), Jun 25, 2003: McDonnell Douglas 369E (N1502), Big Timber, MT, substantial damage. Probable cause: Fretting on the outside diameter of the compressor coupling adapter which resulted in fatigue and subsequent fracture of the adapter, and ultimately the disconnection of the compressor from the…
- [NTSB ANC03LA026](https://openairdocs.org/ntsb/ANC03LA026), Feb 10, 2003: Hughes 369E (N500DX), Paxson, AK, substantial damage. Probable cause: The pilot's failure to maintain altitude/clearance from terrain. A factor contributing to the accident was the pilot's attention being diverted inside the cockpit to look at the global positioning…
- [NTSB FTW03LA066](https://openairdocs.org/ntsb/FTW03LA066), Dec 22, 2002: Hughes 369E (N5234Y), Fritch, TX, substantial damage. Probable cause: The loss of engine power due to the failure of the generator input drive-end bearing, which resulted in excessive vibrations that induced a fatigue fracture of the Pc line leading to the engine fuel…
- [NTSB DEN02GA016](https://openairdocs.org/ntsb/DEN02GA016), Dec 27, 2001: Hughes 369E (N280SP), Park City, UT, destroyed, 3 fatal. Probable cause: the pilot's inadequate visual lookout, resulting in an inflight collision with powerlines. Contributing factors were the fog and the powerlines.
- [NTSB LAX01FA006](https://openairdocs.org/ntsb/LAX01FA006), Oct 8, 2000: McDonnell Douglas 369E (N819CE), Kernville, CA, substantial damage. Probable cause: The pilot's improper storage of personal items and his inadequate preflight inspection, which resulted in the unlatching of the left rear cabin door during flight and allowing a plastic garment bag…
- [NTSB LAX00LA047](https://openairdocs.org/ntsb/LAX00LA047), Nov 30, 1999: Boeing 369E (N5238C), Taft, CA, substantial damage. Probable cause: The fatigue failure of a second stage compressor vane due to erosion, which resulted in a catastrophic engine failure. An inadequate inspection of the compressor section by company maintenance…
- [NTSB MIA99FA158](https://openairdocs.org/ntsb/MIA99FA158), May 20, 1999: Hughes 369E (N144CM), Intercession, FL, substantial damage, 1 fatal. Probable cause: The pilot's improper fuel management that resulted in fuel exhaustion and a total loss of engine power.
- [NTSB SEA98LA050](https://openairdocs.org/ntsb/SEA98LA050), Mar 22, 1998: Hughes 369E (N5245P), Seattle, WA, substantial damage. Probable cause: Loss of engine power due to a restricted fuel system filter.
- [NTSB ATL97LA086](https://openairdocs.org/ntsb/ATL97LA086), Jun 13, 1997: McDonnell Douglas MDHC-369E (N765KV), Okahumpka, FL, no damage. Probable cause: The failure of the crewmember to use the necessary safety equipment, and his subsequent fall from an elevated platform. A factor was the crewmember's distraction with an animal.
- [NTSB CHI97LA008](https://openairdocs.org/ntsb/CHI97LA008), Oct 15, 1996: Hughes 369E (N504AP), Hesston, KS, substantial damage. Probable cause: the pilot selected unsuitable terrain for landing. The factors involved were: an inoperative landing light, dusk light conditions, and the terrain condition.
- [NTSB MIA95GA062](https://openairdocs.org/ntsb/MIA95GA062), Jan 19, 1995: Hughes 369E (N4TP), Tampa, FL, destroyed, 1 fatal. Probable cause: THE PILOT'S FAILURE TO MAINTAIN AIRCRAFT CONTROL AS A RESULT OF BECOMING SPATIALLY DISORIENTED WHILE MANEUVERING. CONTRIBUTING TO THE ACCIDENT WAS THE DARK NIGHT WITH NO VISIBLE HORIZON.
- [NTSB LAX94LA352](https://openairdocs.org/ntsb/LAX94LA352), Sep 4, 1994: Hughes 369E (N279F), Volcano, HI, substantial damage. Probable cause: the pilot's failure to maintain adequate main rotor rpm and the resultant inadvertent skid contact with the ground.
- [NTSB SEA92LA088](https://openairdocs.org/ntsb/SEA92LA088), May 1, 1992: Hughes 369E (N5211Y), Hillsboro, OR, substantial damage. Probable cause: THE PILOT IN COMMAND'S EXCESSIVE APPLICATION OF COLLECTIVE.
- [NTSB BFO90LA075](https://openairdocs.org/ntsb/BFO90LA075), Sep 14, 1990: Hughes 369E (N50075), Prestonburg, KY, destroyed. Probable cause: THE LOST OF ENGINE POWER FOR UNDETERMINED REASONS.
- [NTSB FTW90TL#01](https://openairdocs.org/ntsb/FTW90TL%2301), Dec 14, 1989: Hughes 369E (N600TP), Stroud, OK, substantial damage
- [NTSB LAX87FA173](https://openairdocs.org/ntsb/LAX87FA173), Apr 11, 1987: Hughes 369E (N5200W), Palm Desert, CA, substantial damage
- [NTSB CHI85FA213](https://openairdocs.org/ntsb/CHI85FA213), May 25, 1985: Hughes 369E (N5219A), Indianapolis, IN, destroyed

## FAA accident and incident reports (26)

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

- [Accident 20231227021549A](https://openairdocs.org/incident/20231227021549A), Dec 27, 2023: Hughes Helicopters Inc 369E (N757TB), Miami, FL, Substantial damage, 1 fatal. Rotorcraft was substantially damaged in an accident west in a rural area of west Miami-dade county. The aircraft was located in a canal in approximately 20' of…
- [Accident 20220815008049A](https://openairdocs.org/incident/20220815008049A), Aug 15, 2022: Hughes Helicopters Inc 369E (N500AR), Ely, NV, Substantial damage. During a low level maneuver while rounding up a herd of horses tail rotor struck the ground.
- [Accident 20180201001939A](https://openairdocs.org/incident/20180201001939A), Feb 1, 2018: Hughes Helicopters Inc HU-369-E (N618SG), Wrightwood, CA, Substantial damage. N618SG, a HU369E on a part 135 revenue flight, lost control during its landing approach just prior to touchdown at a 8300 ft MSL mountain landing zone (lz)…
- [Accident 20170623006959A](https://openairdocs.org/incident/20170623006959A), Jun 23, 2017: Hughes Helicopters Inc 369E (N765KV), Quinwood, WV, Substantial damage. N756KV, a Hughes 369E, made an autorotation, landing in a field after losing power during a long line operation. The main rotor struck the tail boom on…
- [Accident 20120726015289A](https://openairdocs.org/incident/20120726015289A), Jul 26, 2012: Hughes Helicopters Inc 369E (N427WC), The Dalles, OR, Substantial damage. Several witness stated the helicopter had just picked up the 3 power lines and started to pull the lines when they heard a loud "pop" and a very noticeable…
- [Accident 20061121025419A](https://openairdocs.org/incident/20061121025419A), Nov 21, 2006: Hughes 369E (N500FU), Jensen, UT, Destroyed, 1 fatal. (-23) On nov. 21, 2006, at 1250 MST, a Hughes 369E, N500FU, crashed and was destroyed after striking high tension wires, approx 2 miles n.e. of Jensen, UT. The…
- [Accident 20050924021289A](https://openairdocs.org/incident/20050924021289A), Sep 24, 2005: Hughes 369E (N5207C), Medford, OR, Substantial damage. (-23) Prior to departing on a FAR part 91 flight, the pilot obtained a "special VFR clearance" and reported clear of kmfr class "d" airspace to the west…
- [Accident 20050817018229A](https://openairdocs.org/incident/20050817018229A), Aug 17, 2005: Hughes 369E (N500FU), Donnelly, ID, Substantial damage. (-23) On landing at cabin in the woods located in the mountains, the pilot experienced a brown out caused by the dust and dirt from the landing pad. The pilot…
- [Accident 20030625013709A](https://openairdocs.org/incident/20030625013709A), Jun 25, 2003: Hughes 369E (N1502), Big Timber, MT, Substantial damage. (-23) While performing predator control, a usda helicopter engine sustained complete failure while aircraft was at approximately 40' AGL with an airspeed of…
- [Accident 20030210001889A](https://openairdocs.org/incident/20030210001889A), Feb 10, 2003: Hughes 369E (N500DX), Paxon, AK, Substantial damage. (-23) The pilot indicated that he was distracted by one of his passengers while encountering flat light conditions and flew the helicopter into terrain.…
- [Accident 20021222033859A](https://openairdocs.org/incident/20021222033859A), Dec 22, 2002: Hughes 369E (N5234Y), Amarillo, TX, Substantial damage. (-23) On December 22, 2002, at approximately 14:45 CST, local time, a Hughes MD369E helicopter aircraft, N5234Y, experienced loss of power, subsequently making…
- [Accident 20011227035379A](https://openairdocs.org/incident/20011227035379A), Dec 27, 2001: Hughes 369E (N280SP), Saltlakecity, UT, No damage, 3 fatal. (-23) This is an interim report. The final report will be forwarded when all applicable information is known and investigated. (.19) on December 27, 2001, at…
- [Accident 20001007015019A](https://openairdocs.org/incident/20001007015019A), Oct 7, 2000: Hughes 369E (N819CE), Kernville, CA, No damage. (-23)On October 7, 2000, N819CE, an MD-369E helicopter was on a ferry flight from big creek, east of fresno, CA to ontario airport,ontario, CA where the…
- [Incident 20000811025559I](https://openairdocs.org/incident/20000811025559I), Aug 11, 2000: Hughes 369E (N504AP), Westcliffe, CO, Minor damage. (-23)Upon landing approach to private property, encountered a strong crosswind. Could not maneuver helicopter to selected landing site. Pulled up to avoid…
- [Accident 19991130042909A](https://openairdocs.org/incident/19991130042909A), Nov 30, 1999: Hughes 369E (N5238C), Taft, CA, Substantial damage. (-23) The MD-500E helicopter was hovering at approx. 100' AGL with an external load of 800 pounds. Upon lifting this load an audible "pop" was heard from the…
- [Accident 19990520005519A](https://openairdocs.org/incident/19990520005519A), May 20, 1999: Hughes 369E (N144CM), Intercession, FL, Substantial damage, 1 fatal. 1986 Hughes 369-E helicopter was laying fiber optic cables when it lost power, the acft auto-rotated to a landing, the pilot sustained minor injuries, and a…
- [Accident 19980321021639A](https://openairdocs.org/incident/19980321021639A), Mar 21, 1998: Hughes 369E (N5245P), Seattle, WA, Substantial damage. (-23)Made hard landing. (.4)the pilot stated that he was making a normal approach until about 30 feet in the air on short final, when he experienced a loss of…
- [Accident 19970613014189A](https://openairdocs.org/incident/19970613014189A), Jun 13, 1997: Hughes 369E (N765KV), Okahumka, FL. While repairing highline tower began chasing a pig. Crewman fell of helicopter platform. (-23) helicopter is utilized for power line repairs and is certified…
- [Accident 19961014032109A](https://openairdocs.org/incident/19961014032109A), Oct 14, 1996: Hughes 369E (N504AP), Hesston, KS, Substantial damage. Running late elected land at his farm. Landing light inop. Aborted. Unknown noise. Rolled landing on golf course.
- [Accident 19950118017069A](https://openairdocs.org/incident/19950118017069A), Jan 18, 1995: Hughes 369E (N4TP), Tampa, FL, Destroyed. While flying low over bay searching for drowning victim. Collided with the water. Spatial disorientation factor.
- [Accident 19940903032269A](https://openairdocs.org/incident/19940903032269A), Sep 3, 1994: Hughes 369E (N279F), Volcano, HI, Substantial damage. Skid struck down slopingland on takeoff. Helicopter rolled over. Density altitude factor. Winds light.
- [Accident 19920501013149A](https://openairdocs.org/incident/19920501013149A), May 1, 1992: Hughes 369E (N5211Y), Portland, OR, Substantial damage. During evaluation check ride pulled collective too soon on autorotation landing. Impact flexed rotors. Chopped tail
- [Incident 19901201058529I](https://openairdocs.org/incident/19901201058529I), Dec 1, 1990: Hughes 369E (N279F), Hilo, HI, Minor damage. On a 180 degree autorotation turn aircraft sink was faster than normal. Tail skid, then tail rotor hit ground.
- [Accident 19900914039799A](https://openairdocs.org/incident/19900914039799A), Sep 14, 1990: Hughes 369E (N50075), Prestonburg, KY, Substantial damage. Lost power struck trees short of open field. Main tank empty. Aux tank full. Fuel transfer control system closed.
- [Accident 19870411009089A](https://openairdocs.org/incident/19870411009089A), Apr 11, 1987: Hughes 369E (N5200W), Paln Desert, CA, Substantial damage. Loud bang,began spin to right and crashed into city street. Tail rotor gear box separated after attach bolts failed
- [Accident 19850525020859A](https://openairdocs.org/incident/19850525020859A), May 25, 1985: Hughes 369E (N5219A), Indianapolis, IN, Destroyed. Surged and yawed on approach and lost power. Stalled avoiding high line. Improper fuel line installation.

## Service difficulty reports (230, newest 50)

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

- [SDR 2026FA0000472](https://openairdocs.org/sdr/2026FA0000472), May 28, 2026: LOCK NUT. FAILED. MS20143 NUTS ARE UTILIZED TO SECURE WITHIN THE ENGINE ASSEMBLY THE FOLLOWING ARTICLES COMPRESSOR, TURBINE, FUEL CONTROL, GOVERNOR, FUEL PUMP, TACH GENERATORS, G
- [SDR 2026FA0000467](https://openairdocs.org/sdr/2026FA0000467), May 28, 2026: WINDOW. CRACKED. PILOT REPORTED BIRD STRIKE TO LOWER LEFT-HAND WINDOW. MAINTENANCE FOUND CRACK DAMAGE REQUIRING REPLACEMENT OF WINDOW.
- [SDR 2026FA0000248](https://openairdocs.org/sdr/2026FA0000248), Mar 31, 2026: BLADE. DENTED. AT LANDING PILOT REPORTED MAIN BLADE CONTACT WITH TREE BRANCHES WITH NO CHANGE IN RPM. MECHANIC DETERMINED PER MDHI CSP HMI-2 THAT THERE WAS NO SUDDEN STOPAGE D
- [SDR 2026FA0000161](https://openairdocs.org/sdr/2026FA0000161), Mar 5, 2026: TRANSMISSION. MAKING METAL. PILOT REPORTED INTERMITTENT MAIN GEARBOX CHIP LIGHT DURING APPROACH TO LANDING. MAGNETIC PLUG INSPECTION REVEALED METAL CONTAMINATION BEYOND ACCEPTABLE LIMITS A
- [SDR DCGA202509100629](https://openairdocs.org/sdr/DCGA202509100629), Sep 8, 2025: BLADE. DENTED. DURING A POST FLIGHT MAINTENANCE INSPECTION A SMALL DENT WAS DISCOVERED ON THE OUTBOARD FACE OF ONE OF THE AIRCRAFT TAIL ROTOR BLADES. PILOT REPORTED THERE WAS 
- [SDR 2024FA0000959](https://openairdocs.org/sdr/2024FA0000959), Dec 12, 2024: ENGINE. MAKING METAL. PILOT EXPERIENCED AN ENGINE CHIP LIGHT DURING LANDING. ENGINE REMOVED FROM AIRCRAFT FOR FURTHER INVESTIGATION.
- [SDR 2024FA0000958](https://openairdocs.org/sdr/2024FA0000958), Dec 11, 2024: ENGINE. MAKING METAL. PILOT EXPERIENCED AN ENGINE CHIP INDICATION DURING APPROACH. MAINTENANCE PERFORMED CLEANING AND GROUND RUNS AND RETURNED TO SERVICE.
- [SDR 2024FA0000554](https://openairdocs.org/sdr/2024FA0000554), Jul 28, 2024: CLUTCH. MAKING METAL. DURING A SCHEDULED 100 HOUR MAINTENANCE INSPECTION ON THE AIRCRAFT. THE MECHANIC QUESTIONED THE DARK BURNT APPEARANCE OF THE GREASE IN THE • BEARING, OVERRUNNIN
- [SDR 2024FA0000495](https://openairdocs.org/sdr/2024FA0000495), Jul 9, 2024: CLUTCH. MAKING METAL. DURING AIRCRAFT INSPECTION AN AIRCRAFT MECHANIC QUESTIONED DISCOLORING OF THE OVERRUNNING CLUTCH OUTPUT BEARING GREASE. THE BEARING DID NOT DEMONSTRATE ANY ABNO
- [SDR 2024FA0000203](https://openairdocs.org/sdr/2024FA0000203), Mar 6, 2024: ENGINE. MAKING METAL. PILOT REPORTED AN ENGINE CHIP LIGHT ILLUMINATION AND PERFORMED AN UNSCEDULED LANDING. A MECHANIC WAS SENT TO THE AIRCRAFT AND DISCOVERED METAL ON THE UPPER ENGI
- [SDR 2023FA122200001](https://openairdocs.org/sdr/2023FA122200001), Dec 19, 2023: TRANSMISSION. INSTALLED. DURING A 135 TOUR OPERATION EXPERIENCED A MAIN ROTOR TRANSMISSION CHIP LIGHT RESULTING IN A PRECAUTIONARY LANDING. ANOTHER HELICOPTER WAS BROUGHT IN WITH MAINTE
- [SDR 2023FA0000497](https://openairdocs.org/sdr/2023FA0000497), Aug 28, 2023: ENGINE. ABNORMAL. UDRING STRAIGHT AND LEVEL FLIGHT THE PILOT REPORTED LOW ENGINE TORQUE. THE PILOT SELECTED A LANDING SPOT AND PERFORMED AN UNEVENTFUL PRECAUTIONARY LANDING. THE 
- [SDR 2023FA0000430](https://openairdocs.org/sdr/2023FA0000430), Aug 16, 2023: DOUBLER. CRACKED. DURING A POST FLIGHT INSPECTION, THE MECHANIC FOUND A CRACK ON THE AFT END OF THE RIGHT-HAND STATION 174 DOUBLER CONNECTING THE BOOM FAIRING AND TURTLE BACK OF 
- [SDR 2023FA0000285](https://openairdocs.org/sdr/2023FA0000285), May 30, 2023: CONNECTOR. LOOSE. DURING FLIGHT THE PILOT NOTICED THE FUEL QUANTITY GAUGE DROPPED TO ZERO THEN THE ENGINE OIL TEMP WENT TO ZERO. THE INSTRUMENT CIRCUIT BREAKER THEN POPPED. THE P
- [SDR 2022FA0000760](https://openairdocs.org/sdr/2022FA0000760), Dec 14, 2022: ENGINE. MAKING METAL. ENGINE GEARBOX CHIP LIGHT ILLUMINATED DURING APPROACH FOR LANDING. UPON INSPECTION IT WAS DETERMINED THAT THE UPPER GEARBOX MAGNETIC CHIP DETECTOR HAD ILLUMINAT
- [SDR 2022FA0000677](https://openairdocs.org/sdr/2022FA0000677), Nov 8, 2022: ENGINE. MAKING METAL. PILOT GOT AN ENGINE CHIP LIGHT DURING FLIGHT AND PERFORMED A PRECAUTIONARY LANDING. MAINTENANCE FOUND EVIDENCE OF CHIPS ON THE LOWER AND UPPER ENGINE GEARBOX CH
- [SDR 2022FA0000568](https://openairdocs.org/sdr/2022FA0000568), Oct 3, 2022: SPRAG CLUTCH. BROKEN. INITIAL CLUTCH WAS REMOVED FOR A DIFFERENT DISCREPANCY AND WAS FOUND TO HAVE A BAD SPRAG CLUTCH 300 HOURS AFTER OVERHAUL. NEXT CLUTCH WAS FOUND TO HAVE A BAD SP
- [SDR 2021FA0000272](https://openairdocs.org/sdr/2021FA0000272), Sep 29, 2021: HUB. WORN. DURING A PREFLIGHT INSPECTION ONE OF THE MAIN ROTOR HUB DROOP STOP FOLLOWER ROLLER SHAFTS WAS FOUND PROTRUDING DOWNWARD FROM THE PLUNGER ASSEMBLY. FURTHER INSPE
- [SDR 2021FA0000137](https://openairdocs.org/sdr/2021FA0000137), May 13, 2021: TURBINE WHEEL. BINDING. DURING MAINTENANCE THE MECHANICS DETERMINED THE FIRST STAGE TURBINE BLADES WERE RUBBING ON THE NOZZLE.ASSEMBLY REMOVED FROM ENGINE
- [SDR 2019FA0000423](https://openairdocs.org/sdr/2019FA0000423), Dec 27, 2019: BLADE. DENTED. DURING A POST FLIGHT INSPECTION A MECHCANIC FOUND A 1/4 X 1/4 INCH DENT IN THE LEADING EDGE OF A MAIN ROTOR BLADE 42 INCHES IBOARD FROM THE TIP OF THE BLADE.
- [SDR 2019FA0000338](https://openairdocs.org/sdr/2019FA0000338), Oct 14, 2019: FUEL CONTROL. LEAKING. DURING MAINTENANCE GROUND RUN CHECK OPERATIONS ENGINE FUEL WAS NOTICED COMING OUT OF THE FUEL CONTROL CASE AND LEAKING TO THE GROUND. FUEL CONTROL WAS REMOVED F
- [SDR 2019FA0000291](https://openairdocs.org/sdr/2019FA0000291), Aug 29, 2019: BLADDER. LEAKING. FUEL LEAKING FROM LEFT HAND FUEL BLADDER. REPLACED BOTH LEFT AND RIGHT HAND BLADDERS.
- [SDR 2019FA0000194](https://openairdocs.org/sdr/2019FA0000194), Jun 25, 2019: ENGINE. MAKING METAL. ENGINE CHIP LIGHT ILLUMINATED WHEN ENGINE WAS BROUGHT TO FLIGHT IDLE AFTER ENGINE START UP. MAINTENANCE FOUND 2 FLAKES WITHIN LIMITS ON THE UPPER CHIP PLUG.A 30
- [SDR DCGA2019FA0000153](https://openairdocs.org/sdr/DCGA2019FA0000153), May 15, 2019: ENGINE. MAKING METAL. ENGINE CHIP LIGHT DURING FLIGHT. MAINTENANCE FOUND 4 FLAKES ON UPPER AND LOWER PLUGS WITHIN PARAMETERS. PERFORMED AN OIL SYSTEM DRAIN, FLUSH AND FILTER CLEAN AN
- [SDR K2DA2019052800003](https://openairdocs.org/sdr/K2DA2019052800003), Mar 19, 2019: BLEED VALVE. STICKS. DURING AN ROUTINE INSPECTION IT WAS DISCOVERED THAT THE ENGINE BLEED VALVE WAS STICKING. BLEED VALVE HAD 317.2 TSO.
- [SDR 2019FA0000075](https://openairdocs.org/sdr/2019FA0000075), Mar 18, 2019: BLADE. CRACKED. THE BOTTOM SKIN OF THE MAIN ROTOR BLADE HAS A 4 1/2 INCH CRACK STATING AT THE TRAILING EDGE AND PERPENDICULAR TO SPAN 57 1/4 INCHES IN FOR BLADE TIP.
- [SDR K2DA2019052800002](https://openairdocs.org/sdr/K2DA2019052800002), Feb 17, 2019: BLEED VALVE. STUCK. PILOT WAS RUNNING ENGINE ON THE GROUND AND THE COMPRESSOR STARTED STALLING. MAINTENANCE PERSONNEL DISCOVERED THE ENGINE BLEED VALVE WAS STUCK IN THE CLOSED POSI
- [SDR J5XA2019FA0000031](https://openairdocs.org/sdr/J5XA2019FA0000031), Feb 5, 2019: CHIP DETECTOR. CONTAMINATED. PILOT REPORTED AN ENGINE CHIP LIGHT DURING APPROACH TO LANDING. MAINTENANCE FOUND ACCEPTABLE CHIPS ON UPPER AND LOWER PLUGS. THE PLUGS WERE CLEANED AND REINSTAL
- [SDR DCGA201811200487](https://openairdocs.org/sdr/DCGA201811200487), Nov 20, 2018: CHIP DETECTOR. SHORTED. DURING A PREFLIGHT INSPECTION THE PILOT NOTICE A MAIN ROTOR GEARBOX DIMMLY ILLUMINATED CHIP LIGHT. MAINTENANNCE DISCOVERED AND INTERNAL SHORT IN THE CHIP DETECT
- [SDR DCGA2018FA0000398](https://openairdocs.org/sdr/DCGA2018FA0000398), Oct 1, 2018: GEARBOX. MAKING METAL. DURING A POST MAINTENANCE OPERATIONAL CHECK FLIGHT THE MAIN ROTOR GEARBOX CHIP LIGHT ILLUMINATED. A PIECE OF METAL WAS FOUND ON THE CHIP PLUG. THE TRANSMISSION 
- [SDR DCGA2018071200221](https://openairdocs.org/sdr/DCGA2018071200221), Jul 12, 2018: CHIP DETECTOR. CONTAMINATED. PILOT REPORTED AND ENGINE CHIP LIGHT AND PERFORMED AN UNSCHEDULED LANDING. MAINTENANCE FOUND 1 SLIVER ON THE UPPER GEARBOX CHIP PLUG. THE PLUG WAS CLEANED AND A
- [SDR 2018FA0000126](https://openairdocs.org/sdr/2018FA0000126), Apr 3, 2018: BLADDER. LEAKING. DURING 100 HOUR MAINTENANCE INSPECTION, A SMALL FUEL LEAK WAS DISCOVERED ON THE BOTTOM OF THE RIGHT FUEL BLADDER. BLADDER WAS REMOVED AND REPLACED
- [SDR DCGA201801230044](https://openairdocs.org/sdr/DCGA201801230044), Jan 23, 2018: ENGINE. MAKING METAL. DURING CRUISE FLIGHT AND ENGINE CHIP LIGHT INDICATION OCCURRED. THE PILOT PERFORMED A PRECAUTIONARY LANDING. MAINTENANCE DISCOVERED METAL FLAKES ON UPPER AND LO
- [SDR 2017FA0000485](https://openairdocs.org/sdr/2017FA0000485), Sep 12, 2017: BLADE. DELAMINATED. DURING A POST FLIGHT INSPECTION BY AN AIRCRAFT MECHANIC TAIL ROTOR LEADING EDGE DELAMINATION WAS FOUND. BOTH TAIL BLADES WERE REMOVED FROM THE AIRCRAFT AND REPL
- [SDR 2017FA0000142](https://openairdocs.org/sdr/2017FA0000142), Mar 22, 2017: HOUSING. WORN. EXTREME PLAY FOUND BETWEEN MAIN ROTOR PITCH HOUSING AND PITCH BEARING HOUSING. THE UPPER BOLT STILL HAD TORQUE STRIP APPLIED BETWEEN NUT WASHER AND BOLT BUT WAS
- [SDR 2017FA0000408](https://openairdocs.org/sdr/2017FA0000408), Jan 5, 2017: BLADE. DELAMINATED. TAIL ROTOR BLADE WAS FOUND IN A DELAMINATED STATE DURING A PREFLIGHT INSPECTION. THE ABRASION STRIP HAD DELAMINATED FROM THE LEADING EDGE OF THE BLADE. PROBABLE
- [SDR 2017FA0000005](https://openairdocs.org/sdr/2017FA0000005), Jan 5, 2017: GEARBOX. EXCESS PLAY. DURING MAINTENANCE A MECHANIC DISCOVERED EXCESSIVE GEARPLAY IN THE MAIN ROTOR TRANSMISSION. THE UNIT WAS REMOVED FOR REPAIR
- [SDR 2017FA0000004](https://openairdocs.org/sdr/2017FA0000004), Jan 5, 2017: BLADE. DELAMINATED. DURING PRE-FLIGHT INSPECTION FOUND TAIL ROTOR BLADE PN. 500P3100-105 SN. C774 LEADING EDGE ABRASION STRIP DELAMINATED.
- [SDR 2017FA0000000](https://openairdocs.org/sdr/2017FA0000000), Jan 3, 2017: COMPRESSOR. DAMAGED. PILOT REPORTED TURBINE OUTLET TEMPERATURE INCREASE AT END OF FLIGHT. MAINTENANCE DISCOVERED COMPRESSOR BLADES DAMAGED BY UNKNOWN FOD.
- [SDR 2017FA0000409](https://openairdocs.org/sdr/2017FA0000409), Dec 23, 2016: BLADE. DELAMINATED. TAIL ROTOR BLADEWAS FOUND IN A DELAMINATED STATE DURING A POST FLIGHT INSPECTION. THE ABRASION STRIP HAD DELAMINATED FROM THE LEADING EDGE OF THE BLADE. THIS BL
- [SDR 2017F00012](https://openairdocs.org/sdr/2017F00012), Dec 23, 2016: ABRASION STRIP. DELAMINATED. DURING POST FLIGHT INSPECTION FOUND TAIL ROTOR BLADE LEADING EDGE ABRASION STRIP DELAMINATED.
- [SDR 2016FA0000537](https://openairdocs.org/sdr/2016FA0000537), Oct 24, 2016: FUEL CONTROL. LEAKING. DURING A POST FLIGHT INSPECTION MAINTENANCE FOUND A SMALL FUEL LEAK AT THE OUT FITTING LOCATION ON THE ENGINE FUEL CONTROL UNIT. THE UNIT WAS REPLACED WITH A SE
- [SDR DCGA2016071800332](https://openairdocs.org/sdr/DCGA2016071800332), Jul 16, 2016: BLADE. DELAMINATED. FOUND DELAMINATION ON MAIN ROTOR BLADE STAINLESS STEEL LEADING EDGE.
- [SDR DCGA2016FA0000261](https://openairdocs.org/sdr/DCGA2016FA0000261), May 27, 2016: BLADE. DENTED. DAMAGE WAS FOUND IN AREAS A AND H ON 4 OF THE 5 MAIN ROTOR BLADE BOTTOM SKINS APPROXIMATELY 6" FROM THE BLADE TIPS. MAINTENANCE DETERMINED IAW CSP HMI-2 MM THAT
- [SDR 2016FA0000182](https://openairdocs.org/sdr/2016FA0000182), Apr 18, 2016: BLADE. DELAMINATED. DURING ROUTINE MAINTENANCE APROXIMATELY 1" INBD FROM THE TIP ON THE TOP OF THE MAIN ROTOR BLADE, PN 500P2100-105, SN 907B A .5" X .5" DELAMINATION WAS FOUND ON 
- [SDR K2DA20160308001](https://openairdocs.org/sdr/K2DA20160308001), Mar 5, 2016: BLADE. DELAMINATED. UPON THE DAILY INSPECTION, A COIN TAP TEST WAS PERFORMED ON THE TAIL ROTOR BLADES. TAIL ROTOR BLADE, PN 500P3100-105, SN C519 WAS DISCOVERED TO BE DELAMINATED. 
- [SDR CA160302016](https://openairdocs.org/sdr/CA160302016), Mar 2, 2016: PRESSURE SWITCH. FAILED. (CAN) FUEL PRESSURE SWITCH, FOUND TO LEAK DURING A 300HR CAUTION LIGHT FUEL PRESSURE SWITCH TEST. UNIT WAS THEN DISASSEMBLED AND FOUND THE BLUE SILICONE COATING
- [SDR 2016FA0000076](https://openairdocs.org/sdr/2016FA0000076), Feb 9, 2016: BLADE. DELAMINATED. UPON THE DAILY INSPECTION, A COIN TAP TEST WAS PERFORMED ON THE TAIL ROTOR BLADES AND BLADE WAS DISCOVERED TO BE DELAMINATED. THE DELAMINATION CONSISTS OF A 2" 
- [SDR K2D2016011200001](https://openairdocs.org/sdr/K2D2016011200001), Dec 31, 2015: BLADE. DELAMINATED. AFTER THE DAY`S FLIGHTS AND DURING THE DAILY INSPECTION WE FOUND, BY TAP TEST, THE L/E OF 1 OF THE TAIL ROTOR BLADES WAS DELAMINATED IN VARIOUS PLACES, VARYING 
- [SDR DCGA2015FA0000622](https://openairdocs.org/sdr/DCGA2015FA0000622), Dec 3, 2015: ENGINE. MAKING METAL. PILOT GOT AN INTERMITTENT ENGINE CHIP LIGHT INDICATION AFTER TAKEOFF AND RETURNED FOR LANDING. MAINTENANCE FOUND LIGHT EXTINGUISHED BUT FOUND METAL ON UPPER AND

All 230: https://openairdocs.org/model/hughes-helicopters-369e/reports.md

## STCs that may be installed (OpenAirDocs) (246, 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 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 SR01059LA](https://openairdocs.org/stc/SR01059LA): Installation of right side dual utility mount. Airfilm Camera Systems LLC
- [STC SH133WE](https://openairdocs.org/stc/SH133WE): Installation of C-75 cargo rack set. Isolair Inc
- [STC SH3686NM](https://openairdocs.org/stc/SH3686NM): Installation of an Isolair Model3700-110 spray tank system. (500N restricted category). Isolair Inc
- [STC SR00181IB](https://openairdocs.org/stc/SR00181IB): Installation of alternate Cabin Door Latches to replace OEM door locks. Aerologic LLC
- [STC SR00709AT](https://openairdocs.org/stc/SR00709AT): Installation of Starter-Generator Cooling Kit. Precision Heli-Support LLC. Lists 369 Series
- [STC SR00771LA](https://openairdocs.org/stc/SR00771LA): Installation of right-side utility mount. Airfilm Camera Systems LLC
- [STC SR00772LA](https://openairdocs.org/stc/SR00772LA): Installation of left-side utility mount. Airfilm Camera Systems LLC
- [STC SR00862LA](https://openairdocs.org/stc/SR00862LA): Installation of aft belly utility mount. Airfilm Camera Systems LLC
- [STC SR04637CH](https://openairdocs.org/stc/SR04637CH): Replacement of existing main ship battery with Lithium Ion Battery and installation of Annunciator Control Panel. Airwolf Aerospace LLC
- [STC SR00068DE](https://openairdocs.org/stc/SR00068DE): Installation of infrared imaging system. Dart Aerospace Company
- [STC SH5247NM](https://openairdocs.org/stc/SH5247NM): Installation of external pod, camera mount, and 12 volt power provision. Dart Aerospace USA Inc
- [STC SR00146IB](https://openairdocs.org/stc/SR00146IB): nstallation of the Integrated Health and Usage Monitoring System (HUMS). RMCI Canada Inc
- [STC SR02120SE](https://openairdocs.org/stc/SR02120SE): Installation of Garmin GTN 6XX/7XX Navigation System. Garmin International Inc
- [STC SH2735NM](https://openairdocs.org/stc/SH2735NM): Installation of pneumatic door actuators. Dart Aerospace USA Inc
- [STC SR02808LA](https://openairdocs.org/stc/SR02808LA): Installation of MD500 Side Pull Kit. Aerocraft Incorporated
- [STC SH5206NM](https://openairdocs.org/stc/SH5206NM): Installation of two underfuselage jacking hard points. Dart Aerospace USA Inc
- [STC SR00376DE](https://openairdocs.org/stc/SR00376DE): Installation of laser mapping system. Dart Aerospace USA Inc
- [STC SR04160CH](https://openairdocs.org/stc/SR04160CH): Installation of Heli-Preheat Kit, p/n TA3089-1 for 115 volt application. HARTZELL PROPELLER INC
- [STC SR00043LA](https://openairdocs.org/stc/SR00043LA): Installation of clip on Main Rotor Swashplate. Pac West Helicopters Inc
- [STC SH3319NM](https://openairdocs.org/stc/SH3319NM): Installation of Precise Flight Pulselite Control Unit in the Landing /Taxi Recognition Visual Control Light system,. Precise Flight Inc
- [STC SR01778SE](https://openairdocs.org/stc/SR01778SE): Installation of Onboard Systems International Cargo Hook Kits and Load Weigh Kit. Onboard Systems International LLC
- [STC SH2263NM](https://openairdocs.org/stc/SH2263NM): Installation of a fore-and-aft medical evacuation litter(s) kit. MD Helicopters LLC
- [STC SR00902DE](https://openairdocs.org/stc/SR00902DE): Installation of External Equipment Mounts for provisions. MD Helicopters Inc
- [STC SR04680NY](https://openairdocs.org/stc/SR04680NY): Installation of Human External Cargo (HEC) Long-Line Kit. Boost Human External Cargo Systems Inc
- [STC SR00314AT](https://openairdocs.org/stc/SR00314AT): Installation of engine firewall in Hughes 369 model helicopter. Thoroughbred Aviation Maintenance Inc
- [STC SR00450AT](https://openairdocs.org/stc/SR00450AT): Installation of a seat pan inspection panel. Thoroughbred Aviation Maintenance Inc. Lists 369 Series
- [STC SR00829AT](https://openairdocs.org/stc/SR00829AT): Installation of front extended cabin step. Thoroughbred Aviation Maintenance Inc. Lists 369 Series
- [STC SR01839AT](https://openairdocs.org/stc/SR01839AT): Installation of cyclic friction levers. Thoroughbred Aviation Maintenance Inc
- [STC SR02859AT](https://openairdocs.org/stc/SR02859AT): Installation of Part Number 369HT21004 main rotor hub fairing as a direct replacement for OEM Part Number 369D21004-11 (BSC). Thoroughbred Aviation Maintenance Inc
- [STC SR03265AT](https://openairdocs.org/stc/SR03265AT): Modification of engine gearbox breather system by the installation of Heli-Tech "HT800-Engine Gearbox Breather Kit", P/N HT800. Thoroughbred Aviation Maintenance Inc
- [STC SR04175AT](https://openairdocs.org/stc/SR04175AT): Installation of the HT400 Inspection Panel Kit. Thoroughbred Aviation Maintenance Inc
- [STC SR02693LA](https://openairdocs.org/stc/SR02693LA): Installation of a redundant system for the primary Cargo Hook system when conducting Human External Cargo (HEC) external loads operations. Onboard Systems International LLC
- [STC SH4908NM](https://openairdocs.org/stc/SH4908NM): Fabrication of Onboard Systems Model 200-034-00, 200-034-01, and 200-034-02 Load Weigh Kits. Onboard Systems International
- [STC SR00407SE](https://openairdocs.org/stc/SR00407SE): Fabrication of Onboard Systems Model 200-187-00 cargo hook kit. Onboard Systems International LLC
- [STC SR00525SE](https://openairdocs.org/stc/SR00525SE): Fabrication of Onboard Systems Model 200-231-00 and 200-231-01 Cargo Hook Attach Point Kit and installation of these Cargo Hook Attach Point Kits. Onboard Systems International
- [STC SR00892SE](https://openairdocs.org/stc/SR00892SE): Fabrication of Onboard Systems International Model 200-264-00, 200-264-01, and 200-264-02 Cargo Hook Kits. Onboard Systems International
- [STC SR02001SE](https://openairdocs.org/stc/SR02001SE): Fabrication and installation of Model 72448 locking fuel cover assembly. Timberline Aerospace LLC
- [STC SR02713SE](https://openairdocs.org/stc/SR02713SE): Manufacture and Installation of Human External Cargo (HEC) Hook System. Mechanical Specialties Inc
- [STC SR02704SE](https://openairdocs.org/stc/SR02704SE): Installation and maintenance of the Sunspot 36 and 46 series lights. AeroLED's Holdings LLC
- [STC SR01343NY](https://openairdocs.org/stc/SR01343NY): Installation of main rotor blade tie down tips. VIH Aerospace Inc
- [STC SR04539NY](https://openairdocs.org/stc/SR04539NY): Installation of the Human External Cargo (HEC) System. Boost Human External Cargo Systems Inc
- [STC SR02622SE](https://openairdocs.org/stc/SR02622SE): Installation of Garmin G500H TXi Display System (Primary Flight Display (PDF), Multi-Function Display (MFD)). Garmin International Inc
- [STC SH4655NM](https://openairdocs.org/stc/SH4655NM): Installation of Soloy 375-1000 series auxiliary fuel system. Fifty-Ten-Yankee LLC
- [STC SR02712LA](https://openairdocs.org/stc/SR02712LA): Installation of Torque Indicating Systems. Precision Heli-Support LLC
- [STC SR02124SE](https://openairdocs.org/stc/SR02124SE): Installation functionality. of Data Garmin Required: transponders: (1) Garmin GTX Master 345/345R Drawing with List ADS-B (MDL), Out and In 005-00734-A4, functionality;. Garmin International Inc
- [STC SH656GL](https://openairdocs.org/stc/SH656GL): Installation of auxiliary fuel system. Fargo Manufacturing Co
- [STC SH698GL](https://openairdocs.org/stc/SH698GL): Installation of belly-mounted cargo carrier. Fargo Manufacturing Co
- [STC SH907GL](https://openairdocs.org/stc/SH907GL): Installation of a starter generator cooling system. Fargo Manufacturing Co
- [STC SH908GL](https://openairdocs.org/stc/SH908GL): Installation of air conditioning system. Fargo Manufacturing Co

All 246: https://openairdocs.org/model/hughes-helicopters-369e/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.

- [PTA369D27502-6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172189254920261008195107.0001): Foot Pedal. PT Aerospace LLC · PMA PQ05337NM · Replaces 369D27502-6 · Sep 28, 2026
- [PTA369D27502-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID112106115420261008195107.0001): Foot Pedal. PT Aerospace LLC · PMA PQ05337NM · Replaces 369D27502-5 · Sep 28, 2026
- [369D28631-APX](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137017068520261008195357.0001): Gasket,Exhaust Duct. APEX HELI-SUPPORT LLC · PMA PQ00075WB · Replaces 369D28631 · Sep 11, 2026
- [369A5528-APX](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189070476720260923123829.0001): Bolt. APEX HELI-SUPPORT · PMA PQ00075WB · Replaces 369A5528 · Sep 4, 2026
- [369D25157-APX](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187302131420260923123829.0001): Shim,Tail Rotor Output. APEX HELI-SUPPORT · PMA PQ00075WB · Replaces 369D25157 · Sep 4, 2026
- [369D25436-APX](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162408468820261008195342.0001): Input Bearing Shim. APEX HELI-SUPPORT LLC · PMA PQ00075WB · Replaces 369D25436 · Sep 4, 2026
- [369D25155-APX](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137547262920260923123829.0001): Shim, Output Bearing. APEX HELI-SUPPORT · PMA PQ00075WB · Replaces 369D25155 · Sep 4, 2026
- [369D25155](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194847140320260923124247.0001): Output Bearing Shim. APEX Heli-Support · PMA PQ00075WB · Replaces 369D25155-APX · Jul 30, 2026
- [PTAMHS1551S238](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155861036820260618160551.0001): Special Washer. PT Aerospace LLC · PMA PQ05337NM · Replaces MHS1551S238 · Jun 22, 2026
- [PTA369H7032](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID198880634220260618165644.0001): Cap Ring. PT Aerospace LLC · PMA PQ05337NM · Replaces 369H7032 · May 29, 2026
- [PTA369H7031](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128542753020260618165643.0001): Cap Ring. PT Aerospace LLC · PMA PQ05337NM · Replaces 369H7031 · May 29, 2026
- [E369D2122 7-11](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121756856420260527183114.0001): Ring, Droop Stop. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 369D21227-11 · May 13, 2026
- [AP600UM02-11](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180254682420260508190532.0001): Aft Plate. AirFilm Camera Systems · PMA PQ2334NM · Replaces AP600UM02-11 · Apr 28, 2026
- [AP600UM02-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179700397020260508190531.0001): Adaptor. AirFilm Camera Systems · PMA PQ2334NM · Replaces AP600UM02-04 · Apr 28, 2026
- [AP600UM02-09](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177351588220260508190531.0001): Aft Bracket. AirFilm Camera Systems · PMA PQ2334NM · Replaces AP600UM02-09 · Apr 28, 2026
- [AP600UM02-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID158186472320260508190530.0001): Mount Bracket, Left. AirFilm Camera Systems · PMA PQ2334NM · Replaces AP600UM02-02 · Apr 28, 2026
- [AP600UM02-08](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140873988320260508190531.0001): Channel. AirFilm Camera Systems · PMA PQ2334NM · Replaces AP600UM02-08 · Apr 28, 2026
- [AP600UM02-03](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139188686020260508190530.0001): Doubler. AirFilm Camera Systems · PMA PQ2334NM · Replaces AP600UM02-03 · Apr 28, 2026
- [AP600UM02-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126961058820260508190530.0001): Mount Bracket, Right. AirFilm Camera Systems · PMA PQ2334NM · Replaces AP600UM02-01 · Apr 28, 2026
- [AP600UM02-05](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID114745498620260508190531.0001): Lateral Brace. AirFilm Camera Systems · PMA PQ2334NM · Replaces AP600UM02-05 · Apr 28, 2026
- [PTA369D25184-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118581873720260304181416.0001): O-Ring. PT Aerospace LLC · PMA PQ05337NM · Replaces 369D25184-3 · Jan 22, 2026
- [KD651510](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136641814820250624152916.0001): Filter Replacement Kit. Donaldson Company Inc · PMA PQ2432CE · Replaces KD651510 · Jun 2, 2025
- [WF336342](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183441687520250602133029.0001): Filter Element, Lube. Donaldson Company Inc · PMA PQ2432CE · Replaces 038088-08, P-1050 · May 23, 2025
- [AP500UM03-RV2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142150914820250508133400.0001): Mount Assembly. AirFilm Camera Systems · PMA PQ2334NM · Modification part · Apr 17, 2025
- [PG369-25123](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190381256620250313100630.0001): Input Gear. PACIFIC GEAR SYSTEMS, INC · PMA PQ5267NM · Replaces 369D25123-11 · Dec 31, 2024
- [PG369-25125](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180496981320250313100630.0001): OutputPinion. PACIFIC GEAR SYSTEMS, INC · PMA PQ5267NM · Replaces 369D25125-11 · Dec 31, 2024
- [PG369-25127](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169644165720250313100630.0001): Output Gear. PACIFIC GEAR SYSTEMS, INC · PMA PQ5267NM · Replaces 369D25127-11 · Dec 31, 2024
- [PG369-25121](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165738612020250313100629.0001): Input Pinion. PACIFIC GEAR SYSTEMS, INC · PMA PQ5267NM · Replaces 369D25121-11 · Dec 31, 2024
- [M2001-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID112754735620240802183931.0001): Brush, Electrical Contact. Miraj Corporation · PMA PQ0870NE · Replaces 150SG1009-5 · Jun 20, 2024
- [AAI- 150SG1070](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184047911720240320173349.0001): Friction Disc. Augusta Aero Innovations LLC · PMA PQ04441CE · Replaces 150SG1070 · Jan 31, 2024
- [N1830-1*](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170386827320240123183029.0001): NAASCO Carbon Brush. NAASCO Northeast Corp · PMA PQ0961NE · Replaces Lucas (LSI) Carbon Brushes 30300-1380… · Dec 20, 2023
- [N1830-2*](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145296719720240123183031.0001): NAASCO Carbon Brush. NAASCO Northeast Corp · PMA PQ0961NE · Replaces Lucas (LSI) Carbon Brushes 23081-1802… · Dec 20, 2023
- [TAU03323](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164396667520240221143036.0001): AV/Cabin Heat Kit. Hartzell Propeller LLC · PMA PQ2040CE · Modification part · Dec 14, 2023
- [N1834-1N1834-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193409817420230816180106.0001): Carbon BrushCarbon Brush. NAASCO Northeast Corp · PMA PQ0961NE · Replaces Lucas (LSI)2Carbon Brush… · Aug 15, 2023
- [N1834-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161576449820230816180101.0001): Carbon Brush. NAASCO Northeast Corp · PMA PQ0961NE · Replaces SkurkaAerospaceInc.(Aircraft… · Aug 15, 2023
- [MDL 375-100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103155313420230713163906.0001): Auxiliary Fuel Tank for MD500. Fifty-Ten-Yankee LLC · PMA PQ05439NM · Replaces ModificationPart · Jun 14, 2023
- [375-1000-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159016181820230630134926.0001): Auxiliary Fuel Tank RH Kit. DV Aviation, Inc. · PMA PQ00016CB · Modification part · Jun 8, 2023
- [375-1000-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID150523330120230630134925.0001): Auxiliary Fuel Tank LH & RH Kit. DV Aviation, Inc. · PMA PQ00016CB · Modification part · Jun 8, 2023
- [375-1000-7](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128125086420230630134928.0001): Auxiliary Fuel Tank. DV Aviation, Inc. · PMA PQ00016CB · Modification part · Jun 8, 2023
- [375-1000-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121658942520230630134927.0001): Auxiliary Fuel Dual Tank Additions Kit. DV Aviation, Inc. · PMA PQ00016CB · Modification part · Jun 8, 2023
- [HT369-0994](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194988218320230127192326.0001): Rear Extended Cabin Step. Thoroughbred Aviation Maintenance, Inc. · PMA PQ00013CB · Modification part · Jan 25, 2023
- [369HT21004](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164533126820230127192329.0001): Main Rotor Hub Fairing. Thoroughbred Aviation Maintenance, Inc. · PMA PQ00013CB · Modification part · Jan 25, 2023
- [HT400](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155644213920230127192330.0001): Inspection Panel Kit. Thoroughbred Aviation Maintenance, Inc. · PMA PQ00013CB · Modification part · Jan 25, 2023
- [HT500-369A3018](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID153474967620230127192324.0001): Engine Firewall. Thoroughbred Aviation Maintenance, Inc. · PMA PQ00013CB · Modification part · Jan 25, 2023
- [HT800](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID138835222420230127192329.0001): Engine Gearbox Breather Kit. Thoroughbred Aviation Maintenance, Inc. · PMA PQ00013CB · Modification part · Jan 25, 2023
- [HT369-0794](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121256731720230127192327.0001): Front Extended Cabin Step. Thoroughbred Aviation Maintenance, Inc. · PMA PQ00013CB · Modification part · Jan 25, 2023
- [HT301](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID120973253620230127192328.0001): Cyclic Friction Release Levers. Thoroughbred Aviation Maintenance, Inc. · PMA PQ00013CB · Modification part · Jan 25, 2023
- [HT100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116660875820230127192326.0001): Seat Pan Inspection Panel. Thoroughbred Aviation Maintenance, Inc. · PMA PQ00013CB · Modification part · Jan 25, 2023
- [E-9208-211](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199507372620221219222203.0001): Crew Seats Upholstered. CUSTOM AIRCRAFT INTERIORS · PMA PQ1890NM · Replaces 369D26554-511 · Dec 8, 2022
- [H5-5000-152](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199269702020221219222527.0001): Conv. Panel L/H Rotor Brake. CUSTOM AIRCRAFT INTERIORS · PMA PQ1890NM · Replaces 369D26570-17 · Dec 8, 2022

All of them: https://openairdocs.org/model/hughes-helicopters-369e/pma.md

## The same model under other registry codes

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

- [Mcdonnell Douglas Helicopter 369E](https://openairdocs.org/model/mcdonnell-douglas-helicopter-369e): 83 registered aircraft, registry code 3027369
- [MD Helicopters 369E](https://openairdocs.org/model/md-helicopters-369e): 40 registered aircraft, registry code 3030008
- [MD Helicopters 369E](https://openairdocs.org/model/md-helicopters-369e): 2 registered aircraft, registry code 3030014
- [Mcdonnell Douglas Mdhs 369E](https://openairdocs.org/model/mcdonnell-douglas-mdhs-369e): 1 registered aircraft, registry code 3030019

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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.