# Aerospatiale AS 355F2

- Type: Aircraft model (FAA registry)
- Registry code: 8680825
- Manufacturer (registry): AEROSPATIALE
- Model: AS 355F2
- Aircraft type: Rotorcraft
- Category: Rotorcraft
- Engines: 2 · Turbo-shaft
- Seats: 7
- Weight class: 12,500 to 19,999 lb
- Certification: Type certificated
- Data sheet: [TCDS H11EU](https://openairdocs.org/tcds/H11EU) (OpenAirDocs)
- Holder: Airbus Helicopters
- Registered aircraft: 6
- Page: https://openairdocs.org/model/aerospatiale-as-355f2

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 2026-20-08](https://openairdocs.org/ad/2026-20-08): Tail rotor drive system · Airbus Helicopters AS355E, AS355F, AS355F1 and 2 more. Effective Nov 5, 2026
- [AD 2026-20-03](https://openairdocs.org/ad/2026-20-03): Placards and Markings · Airbus Helicopters AS350B, AS350BA, AS350B1 and 11 more. Effective Nov 5, 2026
- [AD 2026-16-03](https://openairdocs.org/ad/2026-16-03): Tail Rotor Drive System · Airbus Helicopters AS355E, AS355F, AS355F1 and 2 more. Effective Sep 17, 2026
- [AD 2026-10-16](https://openairdocs.org/ad/2026-10-16): Time Limits/Maintenance Checks · Airbus Helicopters AS355E, AS355F, AS355F1 and 3 more. Effective Jul 21, 2026
- [AD 2026-09-15](https://openairdocs.org/ad/2026-09-15): Tail rotor head · Airbus Helicopters AS350B, AS350BA, AS350B1 and 9 more. Effective Jul 21, 2026
- [AD 2026-12-03](https://openairdocs.org/ad/2026-12-03): Main rotor gearbox · Airbus Helicopters AS350B, AS350B1, AS350B2 and 11 more. Effective Jul 14, 2026
- [AD 2026-05-09](https://openairdocs.org/ad/2026-05-09): Powerplant/Engine Drains · Airbus Helicopters AS355E, AS355F, AS355F1 and 3 more. Effective Mar 25, 2026
- [AD 2025-24-04](https://openairdocs.org/ad/2025-24-04): Vertical Stabilizer, Spar/Rib Structure · Airbus Helicopters AS350B3, AS355E, AS355F and 4 more. Effective Jan 12, 2026
- [AD 2025-09-13](https://openairdocs.org/ad/2025-09-13): Doors · Airbus Helicopters AS350B, AS350BA, AS350B1 and 9 more. Effective Jul 7, 2025
- [AD 2025-03-02](https://openairdocs.org/ad/2025-03-02): Flight compartment equipment · Airbus Helicopters AS332C, AS332C1, AS332L and 15 more. Effective Mar 7, 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 2024-15-08](https://openairdocs.org/ad/2024-15-08): Main Rotor Blades · Airbus Helicopters AS350B, AS350BA, AS350B1 and 7 more. Effective Oct 15, 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 2023-03-13](https://openairdocs.org/ad/2023-03-13): Tail Rotor Drive System · Airbus Helicopters AS355E, AS355F, AS355F1 and 2 more. Effective Mar 31, 2023
- [AD 2022-11-18](https://openairdocs.org/ad/2022-11-18): Engine Cowling System · Airbus Helicopters AS355E, AS355F, AS355F1 and 7 more. Effective Jul 13, 2022
- [AD 2022-10-51](https://openairdocs.org/ad/2022-10-51): Flight Control System · Airbus Helicopters AS350B, AS350B1, AS350B2 and 22 more. Effective Jun 7, 2022
- [AD 2021-03-16 R1](https://openairdocs.org/ad/2021-03-16-R1): Passenger/Crew Doors · Airbus Helicopters AS350B, AS350B1, AS350B2 and 9 more. Effective Mar 24, 2022
- [AD 2022-01-01](https://openairdocs.org/ad/2022-01-01): Main Rotor System · Airbus Helicopters AS350B, AS350BA, AS350B1 and 17 more. Effective Mar 7, 2022
- [AD 2021-20-06](https://openairdocs.org/ad/2021-20-06): Turbine section · Airbus Helicopters AS355E, AS355F, AS355F1 and 1 more. Effective Nov 22, 2021
- [AD 2021-17-17](https://openairdocs.org/ad/2021-17-17): Cabin Equipment/Furnishings · Airbus Helicopters EC135P3, EC135T3, MBB-BK 117 C-2 and 32 more. Effective Nov 22, 2021
- [AD 2021-19-09](https://openairdocs.org/ad/2021-19-09): Cabin Equipment/Furnishings · Airbus Helicopters AS355E, AS355F, AS355F1 and 6 more. Effective Nov 4, 2021
- [AD 2021-16-16](https://openairdocs.org/ad/2021-16-16): Rotorcraft Flight Control · Airbus Helicopters AS355E, AS355F, AS355F1 and 9 more. Effective Oct 13, 2021
- [AD 2021-16-11](https://openairdocs.org/ad/2021-16-11): Tail Rotor Control System · Airbus Helicopters AS355E, AS355F, AS355F1 and 9 more. Effective Oct 6, 2021
- [AD 2021-14-07](https://openairdocs.org/ad/2021-14-07): Cabin Equipment/Furnishings · Airbus Helicopters AS332C, AS332C1, AS332L and 12 more. Effective Aug 19, 2021
- [AD 2021-07-15](https://openairdocs.org/ad/2021-07-15): Tail Rotor Drive Shaft · Airbus Helicopters AS355E, AS355F, AS355F1 and 11 more. Effective May 7, 2021
- [AD 2021-05-09](https://openairdocs.org/ad/2021-05-09): Tail Rotor Control System · Airbus Helicopters AS355E, AS355F, AS355F1 and 8 more. Effective Apr 16, 2021
- [AD 2021-04-13](https://openairdocs.org/ad/2021-04-13): Main Rotor Mast Inner Race Rings · Airbus Helicopters AS355E, AS355F, AS355F1 and 11 more. Effective Apr 14, 2021
- [AD 2021-04-17](https://openairdocs.org/ad/2021-04-17): Tail Rotor Blades · Airbus Helicopters AS355E, AS355F, AS355F1 and 7 more. Effective Mar 23, 2021
- [AD 2020-22-20](https://openairdocs.org/ad/2020-22-20): Main Rotor Gearbox · Airbus Helicopters AS355E, AS355F, AS355F1 and 12 more. Effective Dec 14, 2020
- [AD 2020-20-14](https://openairdocs.org/ad/2020-20-14): Rotorcraft Servo System · Airbus Helicopters AS-365N2, AS-365N3, AS355F and 11 more. Effective Oct 23, 2020
- [AD 2015-17-01 R1](https://openairdocs.org/ad/2015-17-01-R1): Tail Rotor · Airbus Helicopters AS355E, AS355F, AS355F1 and 11 more. Effective Sep 11, 2020
- [AD 2020-09-01](https://openairdocs.org/ad/2020-09-01): Main Rotor Gearbox · Airbus Helicopters AS355E, AS355F, AS355F1 and 2 more. Effective May 28, 2020
- [AD 2020-02-23](https://openairdocs.org/ad/2020-02-23): Landing gear · Emergency Floats (Dart Aerospace ULC STC SR00470LA or SR00645LA). Effective Feb 28, 2020
- [AD 2018-19-10](https://openairdocs.org/ad/2018-19-10): Tail Rotor Driveshaft · Airbus Helicopters AS355E, AS355F, AS355F1 and 2 more. Effective Oct 30, 2018
- [AD 2018-02-02](https://openairdocs.org/ad/2018-02-02): Main Gearbox Mast · Airbus Helicopters AS355E, AS355F, AS355F1 and 11 more. Effective Feb 12, 2018
- [AD 2016-25-20](https://openairdocs.org/ad/2016-25-20): Main Rotor Drive System · Airbus Helicopters AS355E, AS355F, AS355F1 and 13 more. Effective Jan 31, 2017
- [AD 2016-05-06](https://openairdocs.org/ad/2016-05-06): Rotorcraft tailboom · Airbus Helicopters AS355E, AS355F, AS355F1 and 11 more. Effective Apr 8, 2016
- [AD 2015-17-11](https://openairdocs.org/ad/2015-17-11): Main Rotor System · Airbus Helicopters AS355E, AS355F, AS355F1 and 13 more. Effective Sep 29, 2015
- [AD 2015-12-01](https://openairdocs.org/ad/2015-12-01): Fuel Flow Sensor · Airbus Helicopters AS355E, AS355F, AS355F1 and 1 more. Effective Jul 14, 2015
- [AD 2014-05-10](https://openairdocs.org/ad/2014-05-10): Tail Rotor · Airbus Helicopters AS355E, AS355F, AS355F1 and 11 more. Effective May 2, 2014
- [AD 2014-05-07](https://openairdocs.org/ad/2014-05-07): Tail Rotor Control System · Airbus Helicopters AS355E, AS355F, AS355F1 and 9 more. Effective Apr 15, 2014
- [AD 2014-04-11](https://openairdocs.org/ad/2014-04-11): Tail rotor blades · Airbus Helicopters AS355E, AS355F, AS355F1 and 8 more. Effective Apr 9, 2014
- [AD 2013-23-10](https://openairdocs.org/ad/2013-23-10): Fuselage Miscellaneous Structure · Airbus Helicopters AS355E, AS355F, AS355F1 and 8 more. Effective Dec 30, 2013
- [AD 2013-23-09](https://openairdocs.org/ad/2013-23-09): Doors · Airbus Helicopters AS355E, AS355F, AS355F1 and 11 more. Effective Dec 27, 2013
- [AD 2013-16-03](https://openairdocs.org/ad/2013-16-03): Tail Rotor Gearbox · Airbus Helicopters AS355E, AS355F, AS355F1 and 11 more. Effective Oct 22, 2013
- [AD 2013-17-01](https://openairdocs.org/ad/2013-17-01): Tail rotor control system · Airbus Helicopters AS355E, AS355F, AS355F1 and 11 more. Effective Oct 9, 2013
- [AD 2013-10-51](https://openairdocs.org/ad/2013-10-51): Rotorcraft Servo System · Airbus Helicopters AS355E, AS355F, AS355F1 and 11 more. Effective Jul 31, 2013
- [AD 2013-08-19](https://openairdocs.org/ad/2013-08-19): Fuselage Door Hinges · Airbus Helicopters AS355E, AS355F, AS355F1 and 10 more. Effective Jun 5, 2013
- [AD 2012-25-01](https://openairdocs.org/ad/2012-25-01): Emergency Equipment · Airbus Helicopters AS355E, AS355F, AS355F1 and 11 more. Effective Jun 5, 2013
- [AD 2011-18-12](https://openairdocs.org/ad/2011-18-12): Vertical stabilizer spar/rib structure · Airbus Helicopters AS355E, AS355F, AS355F1 and 8 more. Effective Feb 8, 2012

Historical (superseded or no longer in force):

- [AD 2025-06-04](https://openairdocs.org/ad/2025-06-04) (historical): Main Rotor Gearbox · Airbus Helicopters AS350B, AS350B1, AS350B2 and 11 more. Effective May 9, 2025
- [AD 2023-01-04](https://openairdocs.org/ad/2023-01-04) (historical): Tail Rotor Head · Airbus Helicopters AS350B, AS350BA, AS350B1 and 9 more. Effective Mar 8, 2023
- [AD 2022-19-13](https://openairdocs.org/ad/2022-19-13) (historical): Tail Rotor Blades · Airbus Helicopters AS355E, AS355F, AS355F1 and 3 more. Effective Oct 27, 2022
- [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 2021-20-16](https://openairdocs.org/ad/2021-20-16) (historical): Vertical Stabilizer, Spar/Rib · Airbus Helicopters AS355E, AS355F, AS355F1 and 4 more. Effective Nov 22, 2021
- [AD 2021-05-02](https://openairdocs.org/ad/2021-05-02) (historical): Main Rotor System · Airbus Helicopters AS350B, AS350BA, AS350B1 and 12 more. Effective Apr 16, 2021
- [AD 2021-04-15](https://openairdocs.org/ad/2021-04-15) (historical): Vertical Stabilizer, Spar/Rib · Airbus Helicopters AS355F, AS355F1, AS355F2 and 3 more. Effective Mar 23, 2021
- [AD 2021-03-16](https://openairdocs.org/ad/2021-03-16) (historical): Passenger/Crew Doors · Airbus Helicopters AS355E, AS355F, AS355F1 and 9 more. Effective Mar 3, 2021
- [AD 2020-24-03](https://openairdocs.org/ad/2020-24-03) (historical): Rotorcraft Flight Control · Airbus Helicopters AS355E, AS355F, AS355F1 and 6 more. Effective Dec 16, 2020
- [AD 2018-15-02](https://openairdocs.org/ad/2018-15-02) (historical): Tail Rotor Control System · Airbus Helicopters AS-350B, AS-350B1, AS-350B2 and 8 more. Effective Aug 3, 2018
- [AD 2015-17-01](https://openairdocs.org/ad/2015-17-01) (historical): Tail Rotor · Airbus Helicopters AS-350B, AS-350B1, AS-350B2 and 11 more. Effective Sep 24, 2015
- [AD 2014-07-52](https://openairdocs.org/ad/2014-07-52) (historical): Rotorcraft Tailboom · Airbus Helicopters AS-350B, AS-350B1, AS-350B2 and 11 more. Effective Jun 25, 2014
- [AD 2013-21-01](https://openairdocs.org/ad/2013-21-01) (historical): Tail Rotor · Airbus Helicopters AS-350B, AS-350B1, AS-350B2 and 11 more. Effective Oct 25, 2013
- [AD 2011-22-05](https://openairdocs.org/ad/2011-22-05) (historical): Tail rotor control system · Airbus Helicopters AS-350B, AS-350B1, AS-350B2 and 11 more. Effective Nov 25, 2011
- [AD 2010-21-01](https://openairdocs.org/ad/2010-21-01) (historical): Fuselage Misc. Structure · Eurocopter France AS-350B, AS-350B1, AS-350B2 and 8 more. Effective Oct 29, 2010
- [AD 2010-11-51](https://openairdocs.org/ad/2010-11-51) (historical): Tail Rotor Control System · Airbus Helicopters AS-350B, AS-350B1, AS-350B2 and 9 more. Effective Sep 2, 2010
- [AD 2008-24-04](https://openairdocs.org/ad/2008-24-04) (historical): Magnetic chip detector plug (chip detector) · Airbus Helicopters AS355E, AS355F, AS355F1 and 2 more. Effective Dec 30, 2008
- [AD 2003-21-09 R1](https://openairdocs.org/ad/2003-21-09-R1) (historical): Magnetic chip detector plug (chip detector) and the main gearbox (MGB) oil-sight glass · Eurocopter France AS355F, AS355F1, AS355F2 and 1 more. Effective Jul 6, 2006
- [AD 2004-01-51](https://openairdocs.org/ad/2004-01-51) (historical): Main or combiner gearbox · Airbus Helicopters AS355E, AS355F, AS355F1 and 2 more. Effective Mar 15, 2004
- [AD 2003-25-01](https://openairdocs.org/ad/2003-25-01) (historical): Hoist operator control unit · Airbus Helicopters AS-350B, AS-350B1, AS-350B2 and 11 more. Effective Jan 20, 2004
- [AD 2003-22-06](https://openairdocs.org/ad/2003-22-06) (historical): Tail rotor pitch control rod (control Rod) · Eurocopter France AS-350B, AS-350B1, AS-350B2 and 10 more. Effective Dec 3, 2003
- [AD 2003-21-09](https://openairdocs.org/ad/2003-21-09) (historical): Magnetic chip detector · Eurocopter France AS355E, AS355F, AS355F1 and 2 more. Effective Nov 26, 2003
- [AD 2002-21-51](https://openairdocs.org/ad/2002-21-51) (historical): Magnetic chip detector plug · Eurocopter France AS355E, AS355F, AS355F1 and 2 more. Effective Jan 2, 2003
- [AD 2002-02-51](https://openairdocs.org/ad/2002-02-51) (historical): Metal bushing and the STARFLEX star arm end (arm end) · Eurocopter France AS-350B, AS-350B1, AS-350B2 and 11 more
- [AD 2000-10-10](https://openairdocs.org/ad/2000-10-10) (historical): Main Gearbox Suspension Bi-directional Cross-Beam · Eurocopter France AS-350B, AS-350B1, AS-350B2 and 7 more. Effective Jun 26, 2000
- [AD 86-15-10 R2](https://openairdocs.org/ad/86-15-10-R2) (historical): Main Rotor Head Components, the Main Gearbox (MGB) Suspension Bars, and Ground Resonance Prevention System Components · Eurocopter France AS-350B, AS-350B1, AS-350B2 and 8 more. Effective May 23, 2000
- [AD 99-24-18](https://openairdocs.org/ad/99-24-18) (historical): Tail Rotor Spider Plate Bearing · Eurocopter France AS-350B, AS-350B1, AS-350B2 and 8 more. Effective Dec 15, 1999
- [AD 98-24-35](https://openairdocs.org/ad/98-24-35) (historical): Outboard Spherical Bearing Ball · Eurocopter France AS-350B, AS-350B1, AS-350B2 and 9 more. Effective Dec 17, 1998
- [AD 98-14-01](https://openairdocs.org/ad/98-14-01) (historical): Cross-Beam Crack Inspection · Eurocopter France AS-350B, AS-350B1, AS-350B2 and 7 more. Effective Aug 3, 1998
- [AD 89-21-01](https://openairdocs.org/ad/89-21-01) (historical): Main Rotor Swash Plate Bearing · Eurocopter France AS-350B, AS-350B1, AS-350B2 and 10 more. Effective May 3, 1990
- [AD 86-15-10 R1](https://openairdocs.org/ad/86-15-10-R1) (historical): Main Rotor Arms & Gearbox Bars · Eurocopter France AS-350B, AS-350B1, AS-350B2 and 10 more. Effective Mar 22, 1990
- [AD 85-14-06 R1](https://openairdocs.org/ad/85-14-06-R1) (historical): Fuselage Tailboom Interface · Eurocopter France AS-350B, AS-350B1, AS-350B2 and 10 more. Effective Sep 12, 1985

All 110: https://openairdocs.org/model/aerospatiale-as-355f2/ads.md

## Information bulletins (advisory) (3)

- [SAIB SW-15-04](https://openairdocs.org/saib/SW-15-04): Cabin Ventilation Air Scoop Draining. Issued Nov 25, 2014
- [SAIB SW-11-33](https://openairdocs.org/saib/SW-11-33): Eurocopter France Model AS 355 Helicopters; Main Gearbox Cowling Lock Improvement. Issued May 16, 2011
- [SAIB SW-11-07](https://openairdocs.org/saib/SW-11-07): Star Flex Arm Failures on Eurocopter France Model AS350, AS355, and EC130 Helicopters. Issued Dec 20, 2010

## Registered aircraft (6)

- [N355ER](https://openairdocs.org/aircraft/N355ER): [Elite Rotorcraft LLC](https://openairdocs.org/faa-owner/ELITE%20ROTORCRAFT%20LLC), [Mt Juliet, TN](https://openairdocs.org/faa-place/TN/Mt%20Juliet), built 1990, S/N 5436
- [N624TD](https://openairdocs.org/aircraft/N624TD): [Eurotec Vertical Flight Solutions LLC](https://openairdocs.org/faa-owner/EUROTEC%20VERTICAL%20FLIGHT%20SOLUTIONS%20LLC), [Eudora, KS](https://openairdocs.org/faa-place/KS/Eudora), S/N 5459
- [N627TD](https://openairdocs.org/aircraft/N627TD): [Eurotec Vertical Flight Solutions LLC](https://openairdocs.org/faa-owner/EUROTEC%20VERTICAL%20FLIGHT%20SOLUTIONS%20LLC), [Eudora, KS](https://openairdocs.org/faa-place/KS/Eudora), S/N 5460
- [N712CA](https://openairdocs.org/aircraft/N712CA): [Catalyst Aviation LLC](https://openairdocs.org/faa-owner/CATALYST%20AVIATION%20LLC), [Hammonton, NJ](https://openairdocs.org/faa-place/NJ/Hammonton), built 1987, S/N 5362
- [N713CA](https://openairdocs.org/aircraft/N713CA): [Catalyst Aviation LLC](https://openairdocs.org/faa-owner/CATALYST%20AVIATION%20LLC), [Hammonton, NJ](https://openairdocs.org/faa-place/NJ/Hammonton), S/N 5363
- [N808FX](https://openairdocs.org/aircraft/N808FX): [N808fx LLC](https://openairdocs.org/faa-owner/N808FX%20LLC), [Kalispell, MT](https://openairdocs.org/faa-place/MT/Kalispell), S/N 5438

## NTSB investigations (3)

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 ERA21LA043](https://openairdocs.org/ntsb/ERA21LA043), Nov 14, 2020: Aerospatiale AS355 (N712CA), Hammonton, NJ, substantial damage. Probable cause: The pilot's decision to continue the takeoff with a perceived mechanical deficiency.
- [NTSB ERA19FA035](https://openairdocs.org/ntsb/ERA19FA035), Oct 30, 2018: Aerospatiale AS 355F2 (N372CA), Beekmantown, NY, destroyed, 2 fatal. Probable cause: The pilot's failure to keep the helicopter clear of a utility pole while hovering with a tailwind, which resulted in a dynamic rollover into active power lines.
- [NTSB SEA89LA086](https://openairdocs.org/ntsb/SEA89LA086), Apr 14, 1989: Aerospatiale AS-355-F2 (N225CC), Las Vegas, NV, substantial damage. Probable cause: THE PILOT'S POOR INFLIGHT DECISION IN SELECTING AN UNSUITABLE AREA FOR PRACTICE LANDINGS AND THE PILOT'S INADEQUATE VISUAL LOOKOUT RESULTING IN A TAIL ROTOR STRIKE AND LOSS OF ANTITORQUE CONTROL.

## FAA accident and incident reports (5)

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 20201114019419A](https://openairdocs.org/incident/20201114019419A), Nov 14, 2020: Aerospatiale AS 355F2 (N712CA), Hammonton, NJ, Substantial damage. Pilot stated that he performed pre-takeoff flight control checks by memory, and all responses were normal. As the helicopter was lifting off to a hover, the…
- [Accident 20181030021189A](https://openairdocs.org/incident/20181030021189A), Oct 30, 2018: Aerospatiale AS 355F2 (N372CA), Beekmantown, NY, Destroyed, 2 fatal. On 10/30/2018 at approximately 1630 N372CA an Aerospatiale AS355F2 operator while performing powerline inspection/repair operations with four persons on board…
- [Incident 20121002024199I](https://openairdocs.org/incident/20121002024199I), Oct 2, 2012: Aerospatiale AS 355F2 (N808FX), Lumberton, NJ, Substantial damage. Maintenance had been performed prior to the flight on the left engine (remove, inspect, clean & reinstall the magnetic chip detector plugs). The mechanic…
- [Incident 20101209054339I](https://openairdocs.org/incident/20101209054339I), Dec 9, 2010: Aerospatial AS 355F2 (N808FX), East Windsor, NJ, Minor damage. Aircraft suffered bird strike (2 geese) at 1200' feet AGL, heading 060, over East Windsor, new jersey. Damage was found to be isolated to forward nose section…
- [Accident 19890414011619A](https://openairdocs.org/incident/19890414011619A), Apr 14, 1989: Aerosp AS355F2 (N225CC), Las Vegas, NV, Substantial damage. Practice pickup to hover from cement building site pad. Tail rotor hit concrete rebar doing considerable damage.

## Service difficulty reports (69, newest 50)

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

- [SDR CA190528012](https://openairdocs.org/sdr/CA190528012), May 24, 2019: GEARBOX. MAKING METAL. (CAN) MAIN GEARBOX BEVEL REDUCTION (MGB) CHIP LIGHT ON AIRCRAFT STARTUP, AIRCRAFT GROUNDED. DURING STARTUP PILOT NOTICED, MGB CHIP LIGHT ILLUMINATED. PILOT SHUT
- [SDR H0CR2018050101](https://openairdocs.org/sdr/H0CR2018050101), Apr 26, 2018: COMPRESSOR. DELAMINATED. NR 1 AND 2 ENGINE POWER CHECKS WERE TRENDING DOWN. DURING ROUTINE 300HR/12MONTH INSPECTION, FOUND EXCESSIVE DELAMINATION OF THE LINING OF THE COMPRESSOR CASE HA
- [SDR CA150603011](https://openairdocs.org/sdr/CA150603011), Jun 3, 2015: SERVO. FAILED. (CAN) RIGHT MAIN SERVO PN 31026-110 TSO 0.0 RETURNED FROM OVERHAULED. SERVO INSTALLED ON AIRCRAFT & FAILED ELECTRICAL SERVO FUNCTION TEST. SERVO PN 31026-110 RE
- [SDR 2015FA0000049](https://openairdocs.org/sdr/2015FA0000049), Jan 30, 2015: SCISSORS. UNSERVICEABLE. INSTALLED THE O/H SCISSORS LINK AND WAS NOTIFIED BY THE CUSTOMER THAT ON A ROUTINE ALF CHECKS, ON THE ROTATING SCISSORS LINK THAT ABLE ENGINEERING HAD RE-BUSHED
- [SDR CA140627006](https://openairdocs.org/sdr/CA140627006), Jun 19, 2014: STARTER GEN. INOPERATIVE. (CAN) AFTER ATTEMPTING TO START RT ENGINE, A SMALL NOISE OCCURRED BUT THE ENGINE DID NOT ROTATE, MUCH LESS START.
- [SDR CA130603019](https://openairdocs.org/sdr/CA130603019), May 23, 2013: SHAFT. DAMAGED. (CAN) IN FLIGHT SURGE ON NR 1 ENGINE DURING MAINTENANCE OPERATIONS, THE FCU WAS REMOVED AND FOUND INPUT SHAFT DAMAGED.
- [SDR 2011FA0000529](https://openairdocs.org/sdr/2011FA0000529), Aug 4, 2011: SKIN. CRACKED. DURING INSPECTION, A LARGE CRACK WAS FOUND ON UPPER VERTICAL FIN NEAR THE FWD ATTACHMENT POINT. CRACK IS LOCATION ON L/E EXTENDING FROM RT SIDE TO LT SIDE OF AC
- [SDR CA110321007](https://openairdocs.org/sdr/CA110321007), Mar 18, 2011: BEARING. BROKEN. (CAN) ENG CHIP LIGHT EXPERIENCED. SERVICEABILITY CHECK CARRIED OUT. ENG CHIP LIGHT EXPERIENCED. GEARBOX REMOVED, DISCOVERED OUTER RACER OF NR 4 BEARING BROKEN. 
- [SDR 2011F00023](https://openairdocs.org/sdr/2011F00023), Jan 31, 2011: FIRE DETECTOR. FALSE INDICATION. WHILE FLYING TO DESTINATION, THE LT ENGINE FIRE LIGHT ILLUMINATED. 1 PASSENGER WAS ABOARD. PILOTS MADE A PRECAUTIONARY DIVERSION TO OTHER AIRPORT WHICH WAS THE 
- [SDR E30A20090704001](https://openairdocs.org/sdr/E30A20090704001), Jul 4, 2009: ENGINE. MAKING METAL. NR 1 ENGINE CHIP LIGHT ILLUMINATED ON MASTER WARNING PANEL. CHIPS FOUND ON DETECTORS, ENGINE REMOVED FOR REPAIR.
- [SDR CA080723004](https://openairdocs.org/sdr/CA080723004), May 27, 2008: STOP. DAMAGED. (CAN) ACFT WAS CLIMBING AT APPROX 6000` ASL. (OAT 1°C). COLLECTIVE HIT ITS UPPER STOP DURING A POWER INCREASE. AT THIS POINT TORQUE READING WAS APPROX 65 PERCEN
- [SDR 550001062008](https://openairdocs.org/sdr/550001062008), Jan 6, 2008: UNKNOWN. ODOR. AS PILOT STARTED DESCENT, CREW NOTICED STRONG SMOKE ODOR IN COCKPIT; FIRST ODOR WAS "CHEMICAL ODOR" WHICH QUICKLY BECAME "ELECTRICAL" IN NATURE. AS CREW LOOKED 
- [SDR 2007FA0001016](https://openairdocs.org/sdr/2007FA0001016), Nov 6, 2007: SKIN. WORN. RT AND LT FUSELAGE SKIN AT TAILBOOM ATTACH BULKHEAD. FOUND WORKING RIVETS ON BOTH SIDES. (40) FOUND SKIN UNDER WORKING RIVETS WORN .018. ASB 05-00-42 AS FACTOR.
- [SDR CA070912008](https://openairdocs.org/sdr/CA070912008), Sep 10, 2007: PUMP. DEFECTIVE. (CAN) ENGINE AUTO-REIGNITION ACTIVATED IN FLIGHT. REPORTS OF SOFT (BANG) PRECEEDING DECEL. INVESTIGATION REVEALED AIR IN FUEL SYSTEM, SUBSEQUENT TROUBLESHOOTING
- [SDR CA070518001](https://openairdocs.org/sdr/CA070518001), May 14, 2007: LEVER. BROKEN. (CAN) PART BROKE IN (2) PIECES JUST ABOVE ATTACHMENT POINT DURING ENGINE PRE-START CHECK PROCEDURES. (TC NR 20070518001)
- [SDR BAQA20070011](https://openairdocs.org/sdr/BAQA20070011), Apr 15, 2007: WIRE HARNESS. FATIGUED. DURING CRUISE FLIGHT THE RT (NR 2) ENGINE FIRE WARNING LIGHT ILLUMINATED WITH NO SECONDARY INDICATION OBSERVED. AIRCRAFT LANDED SAFELY AT A NEARBY EMS HELIPAD W
- [SDR BAQA20070007](https://openairdocs.org/sdr/BAQA20070007), Mar 8, 2007: LINE. CUT. DURING POST FLIGHT WALK AROUND INSPECTION FOUND MAJORITY OF TAILBOOM OF AIRCRAFT COVERED IN BLACK OIL. REPAIRED CUT OIL LINE.
- [SDR BAQA200700005](https://openairdocs.org/sdr/BAQA200700005), Mar 1, 2007: COMPRESSOR. SEIZED. PILOT WENT TO START NR 1 ENGINE. ENGINE WOULD NOT TURN. FOUND ENGINE SEIZED. REMOVED AND REPLACED ENGINE ASSEMBLY. BROUGHT ENGINE TO ARC, DISASSEMBLED ENGINE AN
- [SDR BAQA200600010](https://openairdocs.org/sdr/BAQA200600010), Nov 29, 2006: GEARBOX. MAKING METAL. MAIN GEARBOX CHIP LIGHT ILLUMINATED ON GROUND RUN UP DRAINED AND FLUSHED GEARBOX PERFORMED REQUIRED PENALTY RUN. CHIP LIGHT ILLUMINATED AGAIN. REMOVED AND REPLA
- [SDR BAQ2005F00004](https://openairdocs.org/sdr/BAQ2005F00004), Dec 13, 2005: PUMP. UNKNOWN. PUMP REMOVED IN COMPLIANCE WITH AD 03-21-09. (K)
- [SDR IJA2005F00003](https://openairdocs.org/sdr/IJA2005F00003), Dec 10, 2004: STARTER GEN. VIBRATION. STARTER GEN VIBRATION WAS CHECKED AFTER A NR 1 ENGINE EXHAUST PIPE WAS FOUND CRACKED. VIBRATION WAS ABOVE LIMITS AND THE STARTER WAS REMOVED AND REPLACED WITH O
- [SDR BAQA094539](https://openairdocs.org/sdr/BAQA094539), May 19, 2004: GYRO. FAILED. GYRO FAILED. REPLACED WITH SERVICABLE UNIT.
- [SDR CA040806005](https://openairdocs.org/sdr/CA040806005), May 17, 2004: BUSHING. LOOSE. (CAN) ALL 3 BUSHINGS FOUND LOOSE ON D.I. STARFLEX WAS REPLACED.
- [SDR CA040723004](https://openairdocs.org/sdr/CA040723004), May 17, 2004: BUSHING. LOOSE. (CAN) ALL 3 BUSHINGS FOUND LOOSE ON D.I. STARFLEX WAS REPLACED.
- [SDR BAQA094679](https://openairdocs.org/sdr/BAQA094679), May 17, 2004: TRANSMITTER. FAILED. TORQUE TRANSMITTER UNIT FAILED OUT OF BOX, WILL NOT ADJUST. RETURNED TO TRADEWIND INTERNATIONAL.
- [SDR BAQA094582](https://openairdocs.org/sdr/BAQA094582), May 13, 2004: INDICATOR. INTERMITTENT. ACTUATION LIGHT ON CAD AMBER RT ON HSI INTERMITTENT. REPLACED WITH SERVICEABLE UNIT.
- [SDR BAQA094252](https://openairdocs.org/sdr/BAQA094252), Apr 22, 2004: SHAFT. SEVERED. SHAFT SEVERED ON UNIT. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 04/28/2004
- [SDR BAQA094193](https://openairdocs.org/sdr/BAQA094193), Apr 22, 2004: PUMP. FAILED. PUMP FAILS TO PROVIDE SUFFICIANT PRESSURE. REPLACED WITH SERVICABLE UNIT. 04/26/2004
- [SDR BAQA094236](https://openairdocs.org/sdr/BAQA094236), Mar 31, 2004: FUEL NOZZLE. DIRTY. REQUIRES CLEANING AND FLOW CHECK. FUEL NOZZLE IS ORIGINAL EQUIPMENT OFF OF ENG. REPLACED WITH SERVICABLE UNIT. 04/22/2004
- [SDR BAQA093729](https://openairdocs.org/sdr/BAQA093729), Mar 10, 2004: FILTER. FAILED. UNIT FAILED FILTER BY-PASS CHECK. THIS UNIT WAS ORIGINALLY ON THE ENGINE WHEN INSTALLED ON A/C S/N 5498. REPLACED WITH SERVICABLE UNIT. 03/11/2004
- [SDR BAQA092464](https://openairdocs.org/sdr/BAQA092464), Feb 23, 2004: SHAFT. WORN. BLEED VALVE SHAFT WORN. BLEED VAVLE IS ORIGINAL EQUIPMENT OFF OF ENGINE. REPLACED WITH SERVICABLE UNIT. 02/25/2004
- [SDR BAQA092608](https://openairdocs.org/sdr/BAQA092608), Feb 9, 2004: CASE HALF. CRACKED. PLASTIC MISSING/CRACKED BEYOND LIMITS. UNIT ORIGINAL EQUIPMENT OFF OF ENG.. REPLACED WITH SERVICABLE UNIT. 02/26/2004
- [SDR BAQA091613](https://openairdocs.org/sdr/BAQA091613), Dec 23, 2003: CASE. DAMAGED. CASE HALVES OF COMPRESSOR, COATING LIFTING. PART REPLACED WITH SERVICABLE UNIT.
- [SDR BAQA091155](https://openairdocs.org/sdr/BAQA091155), Nov 25, 2003: RECEIVER. FAILED. RECEIVER DISPLAY DOES NOT WORK. REPLACED WITH SERVICEABLE UNIT.
- [SDR BAQA089603](https://openairdocs.org/sdr/BAQA089603), Nov 5, 2003: FUEL CONTROL. MALFUNCTIONED. FUEL CONTROL PRODUCING HUNG STARTS, OCCURING BETWEEN 50 PERCENT AND 60 PERCENT. REPLACED WITH SERVICEABLE UNIT. 11/10/03
- [SDR BAQA088838](https://openairdocs.org/sdr/BAQA088838), Aug 25, 2003: TRANSMITTER. INOPERATIVE. TORQUE TRANSMITTER IS INOPERATIVE. REPLACED WITH SERVICEABLE UNIT.
- [SDR BAQA088677](https://openairdocs.org/sdr/BAQA088677), Jul 31, 2003: SERVO. LEAKING. TAIL ROTOR SERVO LEAKING AT SHAFT. REPLACED WITH SERVICEABLE UNIT.
- [SDR BAQA088189](https://openairdocs.org/sdr/BAQA088189), Jul 21, 2003: SERVO. LEAKING. MAIN ROTOR SERVO LEAKING. REPLACED WITH SERVICEABLE UNIT.
- [SDR BAQA087566](https://openairdocs.org/sdr/BAQA087566), Jul 1, 2003: TRANSCEIVER. MALFUNCTIONED. TRANSCEIVER DOES NOT POWER UP. REPLACED WITH SERVICEABLE UNIT.
- [SDR CA030407010](https://openairdocs.org/sdr/CA030407010), Mar 21, 2003: FRAME. CRACKED. (CAN) DURING A 6000 HR. 2T AIRFRAME INSPECTION, TAILBOOM TAILCONE AREA WAS INSPECTED AS AN REQUIREMENT OF EUROCOPTER S/B 55.00.09 'CHECK OF FIN ATTACHMENT FRAME
- [SDR BAQA084698](https://openairdocs.org/sdr/BAQA084698), Feb 24, 2003: CONTROLLER. BROKEN. BACK OF CONNECTOR ON HSI IS BROKEN. BROKEN AT TIME OF RECEIVING.
- [SDR BAQA081640](https://openairdocs.org/sdr/BAQA081640), Dec 12, 2002: ENGINE. MALFUNCTIONED. ENGINE FAILING POWER CHECK. REPLACED WITH SERVICEABLE UNIT.
- [SDR BAQA081639](https://openairdocs.org/sdr/BAQA081639), Dec 12, 2002: ENGINE. MALFUNCTIONED. ENGINE FAILING POWER CHECK. REPLACED WITH SERVICEABLE UNIT.
- [SDR CA020815001](https://openairdocs.org/sdr/CA020815001), Aug 8, 2002: DRIVE SHAFT. SHEARED. (CAN) IN CRUISE FLT, NR 2 ENGINE TORQUE DROPPED BELOW ENGINE TRIM ADJUSTMENT WITH POWER FLUXS. NR 2 ENGINE THROTTLED BACK FROM FLT TO IDLE. RETURNED TO GATE AS 
- [SDR 2002FA0000789](https://openairdocs.org/sdr/2002FA0000789), Apr 5, 2002: SEAL. LEAKING. MECHANIC NOTICED DRIPPING OF FLUID WHILE AIRCRAFT TOOK OFF, RADIOED PILOT AND REQUESTED AIRCRAFT TO RETURN TO BASE. INSPECTION FOUND FUEL COMING FROM (SEAL DRAI
- [SDR 2001FA0000234](https://openairdocs.org/sdr/2001FA0000234), Jul 2, 2001: BLADE. CRACKED. FOUND CRACK ON PREFLIGHT. NO SURE CAUSE FOR CRACK. CRACK BEYOND LIMITS.
- [SDR 20000515SH033](https://openairdocs.org/sdr/20000515SH033), Apr 24, 2000: COWLING. DEPARTED. RIGHT HAND MAIN GEARBOX COWLING CAME OFF OF AIRCRAFT DURING FLIGHT. NO DAMAGE TO AIRCRAFT OTHER THAN MGB COWL ITSELF. NO PERSONAL OR PROPERY DAMAGE OCCURRED. (X
- [SDR 98ZZZX2596](https://openairdocs.org/sdr/98ZZZX2596), Jun 12, 1998: BLADE. DEFECTIVE. PILOT REPORTED T/R GEARBOX CHIP LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. PILOT DIVERTED TO NEAREST AIRPORT AND SECURED HELICOPTER. EXAMINATION OF CHIP DETECTOR 
- [SDR 98ZZZX1683](https://openairdocs.org/sdr/98ZZZX1683), Apr 27, 1998: CONTROL CABLE. FRAYED. CABLE FRAYED AND BEARING WORN OUT CAUSING BINDING OF N2 LINKAGE. SUBMITTER SUGGESTED INSTALLING A BETTER, MORE RELIABLE SYSTEM.
- [SDR HEEA0012199](https://openairdocs.org/sdr/HEEA0012199), Dec 3, 1997: INDICATOR. DEFECTIVE. HIGH RESISTANCE ACROSS RED AND BLUE WIRES.

All 69: https://openairdocs.org/model/aerospatiale-as-355f2/reports.md

## STCs that may be installed (OpenAirDocs) (297, 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 SH4716NM](https://openairdocs.org/stc/SH4716NM): Redesign and relocation of cargo door hinges and relocation of cargo door latch. Turbolyft USA Corporation
- [STC SR00219SE](https://openairdocs.org/stc/SR00219SE): Installation of a color video camera on either the left, right, or both upper outboard surfaces of the horizontal stabilizer. Turbolyft USA Corporation
- [STC SR00242SE](https://openairdocs.org/stc/SR00242SE): Fabrication and Installation of a new instrument panel and pedestal. Turbolyft USA Corporation
- [STC SR00326SE](https://openairdocs.org/stc/SR00326SE): Installation of Geneva Aviation Microwave System. Turbolyft USA Corporation
- [STC SR00361SE](https://openairdocs.org/stc/SR00361SE): Installation of baggage compartment utility rack. Turbolyft USA Corporation
- [STC SR00474SE](https://openairdocs.org/stc/SR00474SE): Installation of a modular equipment rack in the left side only, right side only, or both side cargo compartments. Turbolyft USA Corporation
- [STC SR00643SE](https://openairdocs.org/stc/SR00643SE): Installation of Geneva Aviation Video System. Turbolyft USA Corporation
- [STC SR04464NY](https://openairdocs.org/stc/SR04464NY): Installation of the iPad Mount. Avio Design Group Inc
- [STC SR00521SE](https://openairdocs.org/stc/SR00521SE): Installation of Geneva Aviation Audio System. AEM USA Inc
- [STC SR02301SE](https://openairdocs.org/stc/SR02301SE): Installation of Geneva Aviation 28 - 14 VDC Power Converter. AEM USA Inc
- [STC SR02445SE](https://openairdocs.org/stc/SR02445SE): Installation of P178 Failsafe Audio Mixer. AEM USA Inc
- [STC SR00307DE](https://openairdocs.org/stc/SR00307DE): Installation of Aft Jump Seat. Air Methods LLC
- [STC SR00308DE](https://openairdocs.org/stc/SR00308DE): Installation of Composite Interior. Air Methods LLC
- [STC SR04644CH](https://openairdocs.org/stc/SR04644CH): Replacement of existing main ship battery with Lithium Ion Battery and installation of Battery System Annunciator. Airwolf Aerospace LLC
- [STC SR12092IB](https://openairdocs.org/stc/SR12092IB): Manufacturing and Installation of Cargo Hold Nets. ICARUS AERO INC
- [STC SR00425SE](https://openairdocs.org/stc/SR00425SE): Installation of a satellite phone. Turbolyft USA Corporation
- [STC SR00184IB](https://openairdocs.org/stc/SR00184IB): Installation of External Cargo Basket and Boarding Step. Boost Human External Cargo Systems Inc
- [STC SR00182IB](https://openairdocs.org/stc/SR00182IB): Installation of the Avidyne Integrated Flight Display (IFD) Navigator(s). Horizon Design Services Ltd
- [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 SR00125DE](https://openairdocs.org/stc/SR00125DE): Installation of infrared imaging system. Dart Aerospace Company
- [STC SR00133DE](https://openairdocs.org/stc/SR00133DE): Installation of external pod and camera mount. Dart Aerospace USA Inc
- [STC SR00416DE](https://openairdocs.org/stc/SR00416DE): Installation of laser mapping system. Dart Aerospace USA Inc
- [STC SR00118IB](https://openairdocs.org/stc/SR00118IB): Manufacture of Cargo Hook Mount for Side Pull Operations. Mustang 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 SR00645LA](https://openairdocs.org/stc/SR00645LA): Installation of emergency floats. Dart Aerospace ULC
- [STC SR04557NY](https://openairdocs.org/stc/SR04557NY): Installation of the Fuel Cap Replacement. Avio Design Group Inc
- [STC SR00091IB](https://openairdocs.org/stc/SR00091IB): Installation of the Bear Paw Kit. Alpine Aerotech LP
- [STC SR04669NY](https://openairdocs.org/stc/SR04669NY): Installation of Human External Cargo Y-Rope and Long-Line Kit. Boost Human External Cargo Systems Inc
- [STC SR01424SE](https://openairdocs.org/stc/SR01424SE): Fabrication of Onboard Systems Model 200-292-01 Cargo Hook Kit and Model 200-292-02 Cargo Hook Kit. Onboard Systems International LLC
- [STC SR02035SE](https://openairdocs.org/stc/SR02035SE): Fabrication of Onboard Systems International Model 200-352-00, Cargo Hook Kit. Onboard Systems International LLC
- [STC SH4846SW](https://openairdocs.org/stc/SH4846SW): Installation of formed plexiglass windshield. The NORDAM Group LLC
- [STC SR02704SE](https://openairdocs.org/stc/SR02704SE): Installation and maintenance of the Sunspot 36 and 46 series lights. AeroLED's Holdings LLC
- [STC SR02230AK](https://openairdocs.org/stc/SR02230AK): Installation of Chelton Flight Systems FlightLogic Electronic Flight Instrument System (EFIS). Genesys Aerosystems Inc
- [STC SR02770NY](https://openairdocs.org/stc/SR02770NY): The installation of Quick Release Maintenance Step, Maintenance Peg Step and Fixed Cabin Step. Dart Aerospace Limited
- [STC SR03913NY](https://openairdocs.org/stc/SR03913NY): The installation of Quick Release Bicycle Rack. Dart Aerospace Limited
- [STC SR02680NY](https://openairdocs.org/stc/SR02680NY): The installation of External Attachement Provisions and Cargo Basket to. Dart Aerospace Limited
- [STC SR00457NY](https://openairdocs.org/stc/SR00457NY): Installation of a left-hand or right-hand cargo mirror. Airbus Helicopters Canada Limited
- [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 SR02432NY](https://openairdocs.org/stc/SR02432NY): Installation of Helitowcart Bear Paw Models BP350, BP44 or BP130. Dart Aerospace Ltd
- [STC SR00359BO](https://openairdocs.org/stc/SR00359BO): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies
- [STC SR00699LA](https://openairdocs.org/stc/SR00699LA): Installation of medical system. LifePort LLC
- [STC SR09145RC](https://openairdocs.org/stc/SR09145RC): Installation of an air medical system. LifePort LLC
- [STC SR00600NY](https://openairdocs.org/stc/SR00600NY): Installation of skid mounted cargo baskets. Dart Aerospace Limited
- [STC SR00012SE](https://openairdocs.org/stc/SR00012SE): Installation of LifePort patient loading and support system. LifePort LLC
- [STC SR00821DE](https://openairdocs.org/stc/SR00821DE): Installation of Automatic Dependent Surveillance - Broadcast (ADS-B) Out and in functionality using the BendixKing KT74 Transponder and qualified position sensor and ADS-B In Receiver. Peregrine
- [STC SR00795NY](https://openairdocs.org/stc/SR00795NY): Installation of LH and/or RH "Squirrel Cheeks" Cargo Pods. Airbus Helicopters Canada Limited
- [STC SR00211SE](https://openairdocs.org/stc/SR00211SE): Fabrication and Installation of rear seat shoulder harnesses. Dart Aerospace USA Inc
- [STC SR00646SE](https://openairdocs.org/stc/SR00646SE): Replacement of the original landing gear skid tubes. Dart Aerospace USA Inc
- [STC SR02253SE](https://openairdocs.org/stc/SR02253SE): Fabrication of Geneva Aviation P162 Cross-Tube Antenna Mounts. Dart Aerospace USA Inc
- [STC SR00602NY](https://openairdocs.org/stc/SR00602NY): Operation with the left-hand and/or right-hand aft/side cabin doors removed. Airbus Helicopters Canada Limited

All 297: https://openairdocs.org/model/aerospatiale-as-355f2/stcs.md

## The same model under other registry codes

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

- [Aerospatiale AS355F2 ECUREUIL](https://openairdocs.org/model/aerospatiale-as355f2-ecureuil): 3 registered aircraft, registry code 8680812
- [Airbus Helicopters AS355F2](https://openairdocs.org/model/airbus-helicopters-as355f2): 1 registered aircraft, registry code 8680971
- [Eurocopter France AS355F2](https://openairdocs.org/model/eurocopter-france-as355f2): 1 registered aircraft, registry code 8680976
- [S N I A S AS355 F2](https://openairdocs.org/model/s-n-i-a-s-as355-f2): 0 registered aircraft, registry code 8680613

---
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.