# Eurocopter AS365N3

- Type: Aircraft model (FAA registry)
- Registry code: 8680903
- Manufacturer (registry): EUROCOPTER
- Model: AS365N3
- Aircraft type: Rotorcraft
- Category: Rotorcraft
- Engines: 2 · Turbo-shaft
- Seats: 14
- Weight class: 12,500 to 19,999 lb
- Certification: Type certificated
- Data sheet: [TCDS H10EU](https://openairdocs.org/tcds/H10EU) (OpenAirDocs)
- Holder: Airbus Helicopters
- Registered aircraft: 11
- Page: https://openairdocs.org/model/eurocopter-as365n3

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 2026-17-05](https://openairdocs.org/ad/2026-17-05): Cabin Equipment/Furnishings · Airbus Helicopters H160-B, EC225LP, AS 365 N3 and 18 more. Effective Oct 2, 2026
- [AD 2025-14-07](https://openairdocs.org/ad/2025-14-07): Fire Detection System · Airbus Helicopters AS-365N3, EC 155B and EC155B1. Effective Aug 26, 2025
- [AD 2025-13-09](https://openairdocs.org/ad/2025-13-09): Main rotor control · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 3 more. Effective Aug 14, 2025
- [AD 2025-04-09](https://openairdocs.org/ad/2025-04-09): Bulkhead/Firewall · Airbus Helicopters EC 155B, EC155B1, SA-365N and 3 more. Effective Apr 11, 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 2025-03-04](https://openairdocs.org/ad/2025-03-04): Cabin Equipment/Furnishings · Airbus Helicopters AS332L, AS332L1, AS-365N3 and 4 more. Effective Feb 19, 2025
- [AD 2024-10-10](https://openairdocs.org/ad/2024-10-10): Tail Rotor Control System · Airbus Helicopters SA-365N, SA-365N1, AS-365N2 and 1 more. Effective Jul 23, 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 2022-22-02](https://openairdocs.org/ad/2022-22-02): Placards and Markings, Passenger/Crew Doors · Airbus Helicopters SA-365N, SA-365N1, AS-365N2 and 3 more. Effective Dec 21, 2022
- [AD 2022-13-14](https://openairdocs.org/ad/2022-13-14): Tail Rotor Drive System · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 2 more. Effective Aug 15, 2022
- [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 2022-09-04](https://openairdocs.org/ad/2022-09-04): Tail Rotor Drive System · Airbus Helicopters SA-365N1, AS-365N2, AS-365N3 and 3 more. Effective May 31, 2022
- [AD 2022-05-10](https://openairdocs.org/ad/2022-05-10): Cabin Equipment/Furnishings · Airbus Helicopters AS332L, AS332L1, AS332L2 and 57 more. Effective Apr 20, 2022
- [AD 2022-01-03](https://openairdocs.org/ad/2022-01-03): Fire Bottle, Portable · Airbus Helicopters AS332C, AS332C1, AS332L and 35 more. Effective Mar 7, 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 2021-26-18](https://openairdocs.org/ad/2021-26-18): Tail Rotor Drive System · Airbus Helicopters AS-365N2, AS-365N3, SA-365N1 and 5 more. Effective Feb 9, 2022
- [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 2021-22-07](https://openairdocs.org/ad/2021-22-07): Fire Bottle, Portable · Airbus A319-111, A319-112, A319-113 and 127 more. Effective Nov 18, 2021
- [AD 2021-18-06](https://openairdocs.org/ad/2021-18-06): Engine Cowling System · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 3 more. Effective Sep 10, 2021
- [AD 2021-11-10](https://openairdocs.org/ad/2021-11-10): Life Raft · Airbus Helicopters AS-365N2, AS-365N3, SA-365N and 1 more. Effective Aug 27, 2021
- [AD 2021-14-16](https://openairdocs.org/ad/2021-14-16): Fuselage Main, Frame · Airbus Helicopters AS-365N2, AS-365N3, SA-365N and 2 more. Effective Aug 24, 2021
- [AD 2021-13-19](https://openairdocs.org/ad/2021-13-19): Fuselage Structure · Airbus Helicopters AS-365N2, AS-365N3, SA-365N and 1 more. Effective Aug 17, 2021
- [AD 2021-12-06](https://openairdocs.org/ad/2021-12-06): Main Rotor Drive System · Airbus Helicopters AS-365N2, AS-365N3, SA-365N and 1 more. Effective Jul 20, 2021
- [AD 2021-02-08](https://openairdocs.org/ad/2021-02-08): Fuselage Structure · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 4 more. Effective Apr 15, 2021
- [AD 2021-02-01](https://openairdocs.org/ad/2021-02-01): Placards and markings · Airbus Helicopters AS-365N2, AS-365N3, AS332C and 7 more. Effective Apr 6, 2021
- [AD 2021-03-06](https://openairdocs.org/ad/2021-03-06): Main Rotor Gearbox · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 3 more. Effective Apr 1, 2021
- [AD 2020-21-15](https://openairdocs.org/ad/2020-21-15): Tail Rotor Gearbox · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 2 more. Effective Dec 7, 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 2020-10-02](https://openairdocs.org/ad/2020-10-02): Main Rotor System · Airbus Helicopters AS-365N2, AS-365N3, SA-365C and 5 more. Effective Jun 15, 2020
- [AD 2018-18-11](https://openairdocs.org/ad/2018-18-11): Lights · Airbus Helicopters AS-365N2 and AS-365N3. Effective Oct 18, 2018
- [AD 2016-13-07](https://openairdocs.org/ad/2016-13-07): Placards and Markings · Airbus Helicopters AS-365N3. Effective Aug 2, 2016
- [AD 2016-09-09](https://openairdocs.org/ad/2016-09-09): Fuselage Main, Frame · Airbus Helicopters AS-365N2, AS-365N3, SA-365N and 2 more. Effective Jun 10, 2016
- [AD 2016-07-26](https://openairdocs.org/ad/2016-07-26): Horizontal Stabilizer Structure · Airbus Helicopters AS-365N2, AS-365N3, SA-365N and 1 more. Effective May 16, 2016
- [AD 2016-05-10](https://openairdocs.org/ad/2016-05-10): Life Raft · Airbus Helicopters AS-365N3, EC 155B and EC155B1. Effective Mar 28, 2016
- [AD 2015-11-06](https://openairdocs.org/ad/2015-11-06): Main Rotor Control · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 4 more. Effective Jul 13, 2015
- [AD 2015-10-05](https://openairdocs.org/ad/2015-10-05): Equipment/Furnishing · Airbus Helicopters AS-365N3, EC 155B and EC155B1. Effective Jun 5, 2015
- [AD 2014-26-02](https://openairdocs.org/ad/2014-26-02): Autopilot System · Airbus Helicopters AS-365N3 and EC155B1. Effective Jan 30, 2015
- [AD 2013-19-07](https://openairdocs.org/ad/2013-19-07): JASC Code: 2510: Flight Compartment Equipment · Airbus Helicopters AS-365N2, AS-365N3, AS332C and 8 more. Effective Nov 6, 2013
- [AD 2013-12-04](https://openairdocs.org/ad/2013-12-04): Fuel storage · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 4 more. Effective Aug 2, 2013
- [AD 2013-06-51](https://openairdocs.org/ad/2013-06-51): Equipment/Furnishings · Agusta A109, A109A, A109A II and 43 more. Effective Jul 15, 2013
- [AD 2013-06-07](https://openairdocs.org/ad/2013-06-07): Attitude Gyro and Indicator System · Airbus Helicopters AS-365N2, AS-365N3 and SA-365N1. Effective May 9, 2013
- [AD 2013-03-02](https://openairdocs.org/ad/2013-03-02): Tail Rotor Head · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 2 more. Effective Feb 27, 2013
- [AD 2012-26-10](https://openairdocs.org/ad/2012-26-10): Main Rotor Gearbox · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 7 more. Effective Feb 13, 2013
- [AD 2012-17-02](https://openairdocs.org/ad/2012-17-02): Cracked main rotor mast nut · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 4 more. Effective Oct 10, 2012
- [AD 2012-05-01](https://openairdocs.org/ad/2012-05-01): Main Rotor Head · Airbus Helicopters AS-365N2, AS-365N3, SA-365C and 5 more. Effective Apr 24, 2012
- [AD 2011-03-06](https://openairdocs.org/ad/2011-03-06): Tail rotor (T/R) blade pitch control shaft · Airbus Helicopters AS-365N2, AS-365N3 and SA-365N1. Effective Apr 14, 2011
- [AD 2010-20-20](https://openairdocs.org/ad/2010-20-20): MGB planet gear carrier · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 8 more. Effective Nov 12, 2010
- [AD 2010-19-05](https://openairdocs.org/ad/2010-19-05): Tail rotor · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 2 more. Effective Oct 27, 2010
- [AD 2010-06-07](https://openairdocs.org/ad/2010-06-07): Rotorcraft Flight Control · Airbus Helicopters AS-365N2, AS-365N3, AS332C and 14 more. Effective Apr 21, 2010
- [AD 2008-04-03](https://openairdocs.org/ad/2008-04-03): Main rotor hub · Airbus Helicopters AS-365N2, AS-365N3, SA-365C and 4 more. Effective Mar 6, 2008

Historical (superseded or no longer in force):

- [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 2021-11-03](https://openairdocs.org/ad/2021-11-03) (historical): Engine Cowling System · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 3 more. Effective Jul 15, 2021
- [AD 2021-05-05](https://openairdocs.org/ad/2021-05-05) (historical): Tail Rotor · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 3 more. Effective Apr 16, 2021
- [AD 2020-21-01](https://openairdocs.org/ad/2020-21-01) (historical): Tail Rotor Drive System · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 2 more. Effective Nov 12, 2020
- [AD 2018-19-01](https://openairdocs.org/ad/2018-19-01) (historical): Rotorcraft tail boom · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 3 more. Effective Oct 22, 2018
- [AD 2016-23-05](https://openairdocs.org/ad/2016-23-05) (historical): Tail Rotor Gearbox · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 3 more. Effective Dec 12, 2016
- [AD 2015-26-01](https://openairdocs.org/ad/2015-26-01) (historical): Placards and Markings · Airbus Helicopters AS-365N2, AS-365N3, AS332C1 and 5 more. Effective Jan 26, 2016
- [AD 2014-11-02](https://openairdocs.org/ad/2014-11-02) (historical): Fuselage Structure (General) · Airbus Helicopters AS-365N2, AS-365N3, SA-365N and 1 more. Effective Jul 15, 2014
- [AD 2013-18-01](https://openairdocs.org/ad/2013-18-01) (historical): Main Rotor Control · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 4 more. Effective Oct 18, 2013
- [AD 2013-08-17](https://openairdocs.org/ad/2013-08-17) (historical): Fuselage Main, Frame · Airbus Helicopters AS-365N2, AS-365N3, SA-365N and 2 more. Effective Jun 5, 2013
- [AD 2012-19-09](https://openairdocs.org/ad/2012-19-09) (historical): Tail Rotor Head · Eurocopter France AS-365N2, AS-365N3, EC 155B and 2 more. Effective Oct 10, 2012
- [AD 2010-23-02](https://openairdocs.org/ad/2010-23-02) (historical): Horizontal stabilizers · Airbus Helicopters AS-365N2, AS-365N3, SA-365N and 1 more. Effective Nov 22, 2010
- [AD 2007-25-08](https://openairdocs.org/ad/2007-25-08) (historical): T/R gearbox (TGB) · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 3 more. Effective Jan 14, 2008
- [AD 2006-09-10](https://openairdocs.org/ad/2006-09-10) (historical): Pitch control rod assembly double bearing (bearing) · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 3 more. Effective May 18, 2006
- [AD 2005-03-09](https://openairdocs.org/ad/2005-03-09) (historical): Main gearbox (MGB) planet gear · Eurocopter France AS-365N2, AS-365N3, EC 155B and 8 more. Effective Mar 1, 2005
- [AD 2004-16-15](https://openairdocs.org/ad/2004-16-15) (historical): Main gearbox (MGB) · Eurocopter France AS-365N2, AS-365N3, EC 155B and 4 more. Effective Sep 3, 2004
- [AD 2003-18-03](https://openairdocs.org/ad/2003-18-03) (historical): Hydraulic brake hose (hose) · Eurocopter France AS-365N2, AS-365N3, EC 155B and 2 more. Effective Oct 14, 2003

All 86: https://openairdocs.org/model/eurocopter-as365n3/ads.md

## Information bulletins (advisory) (4)

- [SAIB SW-15-07](https://openairdocs.org/saib/SW-15-07): Rotor Drive-Tail Rotor Drive Flange Shur-Lok Nut Inspection. Issued Dec 30, 2014
- [SAIB SW-08-30R2](https://openairdocs.org/saib/SW-08-30R2): Inadvertent Deployment of Crash Position Indicator (CPI) Beacon. Issued Jul 1, 2008
- [SAIB SW-08-30R1](https://openairdocs.org/saib/SW-08-30R1) (historical): Inadvertent Deployment of Crash Position Indicator (CPI) Beacon. Issued Jun 30, 2008
- [SAIB SW-05-01](https://openairdocs.org/saib/SW-05-01): . Issued Oct 7, 2004

## Registered aircraft (11)

- [N176MT](https://openairdocs.org/aircraft/N176MT): [Dr Heli Acquistion LLC](https://openairdocs.org/faa-owner/DR%20HELI%20ACQUISTION%20LLC), [Princeton, NJ](https://openairdocs.org/faa-place/NJ/Princeton), built 2004, S/N 6677
- [N178MT](https://openairdocs.org/aircraft/N178MT): [Tribeca Heli LLC](https://openairdocs.org/faa-owner/TRIBECA%20HELI%20LLC), [Princeton, NJ](https://openairdocs.org/faa-place/NJ/Princeton), built 1998, S/N 6527
- [N234VM](https://openairdocs.org/aircraft/N234VM): [Integrity Aircraft Title Holdings LLC](https://openairdocs.org/faa-owner/INTEGRITY%20AIRCRAFT%20TITLE%20HOLDINGS%20LLC), [Portland, OR](https://openairdocs.org/faa-place/OR/Portland), S/N 6548
- [N365JA](https://openairdocs.org/aircraft/N365JA): [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 2000, S/N 6585
- [N365RT](https://openairdocs.org/aircraft/N365RT): [Integrity Aircraft Title Holdings LLC](https://openairdocs.org/faa-owner/INTEGRITY%20AIRCRAFT%20TITLE%20HOLDINGS%20LLC), [Portland, OR](https://openairdocs.org/faa-place/OR/Portland), built 2002, S/N 6624
- [N38MD](https://openairdocs.org/aircraft/N38MD): [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 1989, S/N 6335
- [N444Y](https://openairdocs.org/aircraft/N444Y): [Union Airspeed LLC](https://openairdocs.org/faa-owner/UNION%20AIRSPEED%20LLC), [Cincinnati, OH](https://openairdocs.org/faa-place/OH/Cincinnati), built 2008, S/N 6827
- [N600LL](https://openairdocs.org/aircraft/N600LL): [Integrity Aircraft Title Holdings LLC](https://openairdocs.org/faa-owner/INTEGRITY%20AIRCRAFT%20TITLE%20HOLDINGS%20LLC), [Portland, OR](https://openairdocs.org/faa-place/OR/Portland), built 1987, S/N 6262
- [N82MD](https://openairdocs.org/aircraft/N82MD): [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 1998, S/N 6550
- [N896LL](https://openairdocs.org/aircraft/N896LL): [Analar Corp](https://openairdocs.org/faa-owner/ANALAR%20CORP), [Princeton, NJ](https://openairdocs.org/faa-place/NJ/Princeton), built 1988, S/N 6294
- [N97MD](https://openairdocs.org/aircraft/N97MD): [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), S/N 6330

## NTSB investigations (2)

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 ERA22LA334](https://openairdocs.org/ntsb/ERA22LA334), Jul 26, 2022: Eurocopter AS365 (N520CF), Hamilton, OH, substantial damage. Probable cause: The pilot’s decision to continue the landing without having visually identified wires that were known to be in the vicinity of the landing zone, which resulted in a collision with the wires while…
- [NTSB CEN10IA372](https://openairdocs.org/ntsb/CEN10IA372), Jul 4, 2010: Eurocopter AS365N3 (N520CF), Dayton, OH, incident, minor damage. Probable cause: The unintentional movement of the jettison handle in-flight due to the pilot’s dropping of a manual that impacted the handle and released the door window, which then impacted the horizontal…

## 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 20220726020089A](https://openairdocs.org/incident/20220726020089A), Jul 26, 2022: Eurocopter AS365N3 (N520CF), Hamilton, OH, Destroyed. On 7/26/2022 at 0435, [privacy data omitted] Eurocopter AS365N3, while responding to an ems/haa call, the pilot struck high tension wires during approach to…
- [Incident 20140709010719I](https://openairdocs.org/incident/20140709010719I), Jul 9, 2014: Eurocopter AS365N3 (N520CF), Moraine, OH, Minor damage. The helicopter was in a hover at night when the pilot noticed the helicopter in a slow rearward drift. When the pilot started to adjust for the drift the tail…
- [Incident 20130925018559I](https://openairdocs.org/incident/20130925018559I), Sep 25, 2013: Eurocopter AS365N3 (N95MD), California, MD, Minor damage. On 25 September, 2013, [privacy data omitted], an instructor pilot for the Maryland state police, was administering an annual check ride for line pilot…
- [Incident 20120220002199I](https://openairdocs.org/incident/20120220002199I), Feb 20, 2012: Eurocopter AS365N3 (N82MD), Belair, MD, Minor damage. Third party reports indicate that the aircraft had flames coming from the right engine during landing at a ground vehicle accident site. The fire was…
- [Incident 20100704038179I](https://openairdocs.org/incident/20100704038179I), Jul 4, 2010: Eurocopter AS365N3 (N520CF), Dayton, OH, Minor damage. During cruise flight at 2000 feet, the upper front corner of the emergency egress door was dislodged, the airstream caught door and bent the top half down to…

## Service difficulty reports (58, newest 50)

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

- [SDR QMLA2023040520025](https://openairdocs.org/sdr/QMLA2023040520025), Apr 5, 2023: UNKNOWN. UNKNOWN. PRIOR TO TAKE OFF, YELLOW GOV LIGHT ILLUMINATED ON THE WARNING/CAUTION PANEL. I FAILED TO CAPTURE THE FAULT CODE PRIOR TO SHUTTING BOTH ENGINES DOWN. MECHANIC A
- [SDR U0GA ASR8774](https://openairdocs.org/sdr/U0GA%20ASR8774), Oct 3, 2022: RADIO. SMOKE. UPON PICK UP INTO A HOVER, PASSENGER SMELLED A FAINT ODOR OF BURNING PLASTIC OR OZONE. THE TECHNASONIC RADIO FLICKERED THEN SHUT OFF AND RELEASED LIGHT WISPS OF
- [SDR QMLA2022090720063](https://openairdocs.org/sdr/QMLA2022090720063), Sep 3, 2022: NONE. NONE. CREW DETECTED A BURNING ODOR IN FLIGHT. FOUND NO TRACE OF ODOR ALL SYSTEM NORMAL. SUSPECTED TO BE AFT A.C. BLOWER MOTOR.
- [SDR QMLA2022090220061](https://openairdocs.org/sdr/QMLA2022090220061), Aug 31, 2022: NONE. NONE. AFTER LANDING, CREW SMELLED AN ELECTRICAL BURNING ODOR IN THE CABIN, WHICH WAS ELIMINATED IMMEDIATELY UPON OPENING THE CABIN DOORS. NORMAL SHUTDOWN WAS COMPLETE
- [SDR 2022FA0000273](https://openairdocs.org/sdr/2022FA0000273), Jun 2, 2022: NONE. NONE. DURING TAKEOFF THE CABIN EXPERIENCED A RUBBER BURNING SMELL, THE AIRCRAFT RETURNED TO BASE, SHUTDOWN WITHOUT FURTHER INCIDENT. TROUBLE SHOOTING INDICATES THAT T
- [SDR U0GA ASR7942](https://openairdocs.org/sdr/U0GA%20ASR7942), May 31, 2022: NONE. BURNED. BURNING SMELL FOLLOWED BY FRONT AIR CONDITIONER FAN STOPPING. SHUT OFF AIR CONDITIONER.
- [SDR 7AJA20220425005](https://openairdocs.org/sdr/7AJA20220425005), Apr 25, 2022: NONE. NONE. MGB CHIP LIGHT ILLUMINATED IN CRUISE FLIGHT. REDUCED POWER. LIGHT EXTINGUISHED. TURNED AROUND AND RETURNED TO KGYR. LIGHT REMAINED EXTINGUISHED EXCEPT FOR ONE O
- [SDR QMLA2022032920021](https://openairdocs.org/sdr/QMLA2022032920021), Mar 28, 2022: SKIN. UNSERVICEABLE. HORZ. STAB IS UNSERVICABLE UPPER SKIN RH SIDE HAS 24 WORKING RIVITS WITH SKIN MOVEMENT (WARRANTY ISSUE)
- [SDR 2022FA0000040](https://openairdocs.org/sdr/2022FA0000040), Jan 21, 2022: FUEL CELL. LEAKING. DURING A ROUTINE VISUAL MAINTENANCE INSPECTION, THE UPPER FUEL BLADDER WAS DISCOVERED TO BE LEAKING. UPON REMOVAL OF THE UPPER BLADDER, THE LOWER, AFT SEEM WAS 
- [SDR QMLA2021121020064](https://openairdocs.org/sdr/QMLA2021121020064), Dec 10, 2021: DOUBLER. CRACKED. DURING A 2060 1000 HOUR/36 MONTH INSPECTION, THE REAR DOUBLER PN: L533M1321262 WAS FOUND TO HAVE ABOUT A 6 INCH CRACK RUNNING FROM LEFT REAR TO RIGHT FORWARD. T
- [SDR 2021F00377](https://openairdocs.org/sdr/2021F00377), Dec 3, 2021: NONE. NONE. SUPPLEMENTAL INFORMATION SUBMISSION. QMLA2021082020042. REPLACED THE #2 ENGINE FUEL CONTROL. REPLACED THE MAIN FUEL SUPPLY LINE FROM ENGINE DECK TO MAIN FUEL FI
- [SDR 2A6D20211027001](https://openairdocs.org/sdr/2A6D20211027001), Oct 27, 2021: SKIN PANEL. CORRODED. THERE IS CORROSION DAMAGE TO THE LEFT HAND CABIN FLOOR EDGING (PN: 350A21-1359-20/21).
- [SDR QMLA202109240047](https://openairdocs.org/sdr/QMLA202109240047), Sep 24, 2021: TRANSCEIVER. FAULTED. PILOT SMELLED UNKNOWN FUMES COMING FROM REAR OF AIRCRAFT. WAS COMING IN TO LAND AT MIAMI VALLEY HOSPITAL AND DIFERTED TO MORAINE AIRPARK (OUR MAINTENANCE HANGAR
- [SDR 2021FA0000305](https://openairdocs.org/sdr/2021FA0000305), Aug 25, 2021: ENGINE. MAKING METAL. AIRCRAFT DIVERTED DUE TO A CHIP LIGHT ON THE NR 1 ENGINE. ALL OPERATIONS WERE NORMAL UPON LANDING, THE ENGINES WERE SHUTDOWN AND THE CHIP PLUGS WERE CHECKED, TH
- [SDR QMLA2021060620027](https://openairdocs.org/sdr/QMLA2021060620027), Jun 6, 2021: MOTOR. BURNED OUT. AFTER FUELING THE AIRCRAFT THE PILOT PULLED INTO A HOVER AND SMELLED AND BURNT RUBBER SMELL. I WAS CALLED TO INVESTIGATE THE SMELL AND FOUND THAT IT WAS COMING 
- [SDR QMLA2019071019060](https://openairdocs.org/sdr/QMLA2019071019060), Jul 10, 2019: FRAME. CRACKED. FOUND CRACK ON FRAME X4630 REAR STRUCTURE TRANSMISSION DECK. WHILE REPAIRING THIS CRACK FOUND ANOTHER UNDER RIGHT UPPER FISH PLATE ON SAME FRAME X4630. THIS AIR
- [SDR QMLA2019010719002](https://openairdocs.org/sdr/QMLA2019010719002), Jan 7, 2019: DOOR FRAME. CRACKED. DURING AN INSPECTION WE FOUND 3 SCREWS ON THE 25 DEGREE FRAME THAT WERE PULLED THROUGH AFTER FURTHER INVESTIGATION WE FOUND THE 25 DEGREE FRAME CRACKED ABOUT AN
- [SDR QMLA2018122878137](https://openairdocs.org/sdr/QMLA2018122878137), Dec 27, 2018: FRAME. CRACKED. CRACK FOUND ON THE 14 DEGREE FRAME POST
- [SDR QMLA2018100418108](https://openairdocs.org/sdr/QMLA2018100418108), Oct 1, 2018: WARNING LIGHT. INTERMITTENT. NR 1 ENGINE FIRE LIGHT INTERMITTENT DURING FLIGHT
- [SDR QMLA201702091705](https://openairdocs.org/sdr/QMLA201702091705), Feb 9, 2017: UNKNOWN. ODOR. CREWMEMBER REPORTED SMELLING FUEL. RETURN TO BASE. NO FURTHER DEFECTS FOUND DURING MAINTENANCE INSPECTIONS.
- [SDR QMLA2015111015106](https://openairdocs.org/sdr/QMLA2015111015106), Nov 10, 2015: CONNECTOR. BURNED. REPOSITIONING FROM A PATIENT OFFLOAD FROM OUR SOUTH PAD TO OUR NORTH PAD, SMELLED ELEC SMOKE. AFTER LANDING, DETECTED SMOKE FROM THE AREA AROUND THE 5A PANEL. F
- [SDR QMLA2015081215070](https://openairdocs.org/sdr/QMLA2015081215070), Aug 12, 2015: STUD. SHEARED. DURING TAKEOFF THE LT VERTICAL STABILIZER SEPARATED FROM THE ACFT, THE PIC WAS UNAWARE OF THE ISSUE UNTIL THE COMMUNICATIONS CENTER NOTIFIED HIM BY RADIO. NO EF
- [SDR CA150629021](https://openairdocs.org/sdr/CA150629021), Jun 25, 2015: FUEL SYS. LEAKING. (CAN) EXCESSIVE FUEL LEAKAGE, > 9 DROPS A MINUTE.
- [SDR QMLA2015011415006](https://openairdocs.org/sdr/QMLA2015011415006), Jan 14, 2015: PUMP. SEIZED. AFTER DEPARTING FROM BASE, ON CLIMB OUT, THE LG HANDLE WAS PLACED IN THE UP POSITION WITH NO CYCLE LIGHT & GEAR LIGHT INDICATED GEAR DOWN. THE LG HANDLE WAS THE
- [SDR QMLA2014112214133](https://openairdocs.org/sdr/QMLA2014112214133), Nov 22, 2014: UNKNOWN. ODOR. MAINTENANCE WAS NOT NOTIFIED UNTIL 11/23/2014 AT 2217. RECEIVED AN EMAIL FROM PILOT STATING THAT WE NEEDED TO DO AN SDR FROM HIS SUPERVISOR. THERE WAS NO LOGBOO
- [SDR QMLA2014110714130](https://openairdocs.org/sdr/QMLA2014110714130), Nov 7, 2014: UNKNOWN. ODOR. PILOT REPORTED SMELLING SOMETHING HOT IN THE COCKPIT, NO SMOKE PRESENT. INSPECTED THE ACFT, THEN THEY FLEW FOR APPROX ONE HOUR. COULD NOT DUPLICATE PROBLEM.
- [SDR QMLA2014110414129](https://openairdocs.org/sdr/QMLA2014110414129), Nov 4, 2014: FIRE DETECTOR. INTERMITTENT. INTERMITTENT FIRE LIGHT ON FINAL APPROACH. PILOT REPORTED THAT AS HE WAS LANDING THE FIRE LIGHT WOULD FLICKER. AT NO TIME DID THE LIGHT COME ON & STAY ON.
- [SDR 7EMA20140930007](https://openairdocs.org/sdr/7EMA20140930007), Sep 28, 2014: FUEL CONTROL. LEAKING. ON DAILY INSPECTION TECHNICIAN NOTICED FUEL PUMP LEAKING AT ENG MATING. UPON PUMP REMOVAL DISCOVERED FUEL CONTROL DRIVE BEARING BLUE GREASE LUBRICATION EXCESSIV
- [SDR 9EKA20140911010](https://openairdocs.org/sdr/9EKA20140911010), Sep 10, 2014: BATTERY. DEFECTIVE. ON A FLIGHT NR 2 GEN FAILED EN ROUTE, IT WAS RESET & THE FLIGHT CONTINUED. IT FAILED A SECOND TIME A FEW MINUTES LATER, TURNED GEN OFF, TURNED & HEADED BACK. SM
- [SDR 9EKA20140806008](https://openairdocs.org/sdr/9EKA20140806008), Aug 6, 2014: COMPRESSOR. STALLED. WHILE FLYING A DISTANCE OF 100NM, FOR THE COMPLETION OF THE CONTRACT FLIGHT I HAD TWO COMPRESSOR STALLS. THE FIRST HAPPENED AT A CONSTANT POWER SETTING OF 80% T
- [SDR QMLA2014060714066](https://openairdocs.org/sdr/QMLA2014060714066), Jun 7, 2014: DRIVE BELT. BROKEN. PRIOR TO TAKE OFF, TURNED ON THE ACFT`S AIR CONDITIONER. DURING CLIMB OUT WE SMELLED AN ELEC BURNING SMELL & ASSOCIATED GREY SMOKE COMING FROM THE NOSE OF THE A
- [SDR QMLA2014060614065](https://openairdocs.org/sdr/QMLA2014060614065), Jun 6, 2014: DRIVE BELT. BROKEN. DURING A PATIENT TRANSFER, THERE WAS A BURNT RUBBER ODOR IN THE CABIN & LOSS OF AIR CONDITIONING. AFTER LANDING AT GOOD SAM & OPENING THE TRANSMISSION COWLING, 
- [SDR QMLA2014042814044](https://openairdocs.org/sdr/QMLA2014042814044), Apr 28, 2014: COMPRESSOR. FAILED. BURNING SMELL & SMOKE IN THE CABIN. AIR CONDITIONING & FAN TURNED OFF & IT SUBSIDED. AIR CONDITIONER COMPRESSOR INTERNAL FAILURE.
- [SDR QMLA2014042314041](https://openairdocs.org/sdr/QMLA2014042314041), Apr 23, 2014: STARTER GEN. FAULTY. GENERATOR CAUTION LIGHT ILLUMINATED APPROXIMATELY 10 MINUTES AFTER DEPARTURE. RESET OF GENERATOR EXTINGUISHED THE CAUTION LIGHT. FLIGHT CONTINUED NORMALLY TO HO
- [SDR QMLA2014042314039](https://openairdocs.org/sdr/QMLA2014042314039), Apr 23, 2014: FRAME. CORRODED. MOUNTING SCREW NUTPLATE & FRAME AT STATION X1790.15 & Y400.0 HAS DAMAGE & HAS SURFACE CORROSION JUST FWD OF RT LANDING LIGHT ASSEMBLY.
- [SDR QMLA2014042114040](https://openairdocs.org/sdr/QMLA2014042114040), Apr 21, 2014: DUCT. CONTAMINATED. AFTER STARTING THE ENG FOR A SCENE FLIGHT, THE NURSE & MEDIC DETECTED AN UNIDENTIFIED ODOR. ATTEMPTS TO LOCALIZE & IDENTIFY THE ODOR WERE UNSUCCESSFUL & WE ELEC
- [SDR 2A6R2014041895301](https://openairdocs.org/sdr/2A6R2014041895301), Apr 18, 2014: FRAME. CRACKED. CRACKS LOCATED AT TAIL BOOM, AIRFRAME JUNCTION, ON THE RT SIDE OF THE AIRFRAME. ON OUTSIDE RADIUS OF THE REAR FACING AIRFRAME SIDE. ON THE UPPER HALF OF THE OUT
- [SDR QMLA2014041614038](https://openairdocs.org/sdr/QMLA2014041614038), Apr 16, 2014: PLANETARY GEAR. UNSERVICEABLE. DURING A6031RT, MAST INSPECTION, UPON SEPARATION OF THE MAST & MGB, SEVERAL METALLIC FERROUS FLAKES WAS LOCATED ON & AROUND THE EPICYCLICAL REDUCTION GEAR. AFTE
- [SDR 39LA2014041570](https://openairdocs.org/sdr/39LA2014041570), Apr 15, 2014: SERVO CONTROL. CORRODED. MAIN ROTOR SERVO CYLINDER, PN 7112-3B, SN 494 HAS SEVERE INTERGRANULAR CORROSION ON THE LOWER ATTACH POINT.
- [SDR 2A6R214041695401](https://openairdocs.org/sdr/2A6R214041695401), Apr 14, 2014: TAIL BOOM. DAMAGED. THE TAIL ROTOR GEAR BOX & THE VERTICAL STABILIZER BOLT MOUNTING POINTS ON TOP OF THE TAIL BOOM ARE DAMAGED & NEED REPAIR. FOUND THAT THE WINDINGS INSIDE THE BOL
- [SDR 2A6R2014041195301](https://openairdocs.org/sdr/2A6R2014041195301), Apr 11, 2014: STRUCTURE. CORRODED. DURING INSPECTION PROCESS, FOUND CORROSION LOCATED INSIDE UPPER RT SIDE BAGGAGE COMPARTMENT, UNDER ENG DECK. AFTER REMOVAL OF CORROSION A FULL PENETRATION AREA 
- [SDR MHIA20140408001](https://openairdocs.org/sdr/MHIA20140408001), Apr 7, 2014: PUMP. SEIZED. ON APPROACH TO 65NJ PILOT NOTED HYD LIGHT ON WARNING CAUTION PANEL INDICATING HYD FAILURE. ABORTED LANDING AT 65NJ TO CHANGE COURSE TO EWR FOR A RUN ON LANDING.
- [SDR QMLA2014031714029](https://openairdocs.org/sdr/QMLA2014031714029), Mar 17, 2014: STRUCTURE. CORRODED. FOUND CORROSION UNDER THE LT CABIN DOOR SEAL WHILE PERFORMING A AAIP. THE FLOOR EDGING DAMAGE IS BEYOND THE LIMITS. THE ENGINEERING DEPARTMENT HAS PROVIDED AN A
- [SDR OLJ2014F00000](https://openairdocs.org/sdr/OLJ2014F00000), Mar 4, 2014: BEARING. MAKING METAL. ENROUTE, NR 2 ENGINE CHIP LIGHT INDICATED ON THE MASTER CAUTION PANEL. ACFT ABORTED FLIGHT. AFTER LANDING, THE ACFT WAS TAKEN OUT OF SERVICE. A CHIP WAS FOUND O
- [SDR QMLA2014022214017](https://openairdocs.org/sdr/QMLA2014022214017), Feb 22, 2014: LIGHT. MALFUNCTIONED. DURING STRAIGHT & LEVEL FLIGHT, THE FLIGHT CREW HAD BOTH THE CABIN REAR NVG LIGHTS ON FOR ABOUT 30 MINUTES OF THE 40 MINUTE FLIGHT. AT 30 MINUTES THEY NOTICED S
- [SDR MHIA20140325001](https://openairdocs.org/sdr/MHIA20140325001), Feb 11, 2014: SEAL. DAMAGED. DURING FLIGHT THE RT PILOT DOOR UPPER WINDOW DEPARTED THE ACFT. THE SEAL WAS DRY ROTTED.
- [SDR QMLA2013091013128](https://openairdocs.org/sdr/QMLA2013091013128), Sep 10, 2013: PLATE. CRACKED. DURING ROUTINE MX, FOUND A CRACK IN THE PRIMARY STUCTURE ON THE RT SIDE OF THE FUSELAGE IDENTIFIED AS FISH-PLATE, LOCATED AT THE TOP OF THE 4630 BULKHEAD, OR TH
- [SDR QMLA2012121512191](https://openairdocs.org/sdr/QMLA2012121512191), Dec 15, 2012: LINK. FAILED. AIRCRAFT BEGAN TO EXPEREINCE A 1 TO 1 VERTICAL VIBRATION AND I FELT FEEDBACK IN THE CYCLIC. DECLARED AN EMERGENCY, AND EXECUTED A ROLL ON LANDING WITHOUT INCIDE
- [SDR QMLA2012](https://openairdocs.org/sdr/QMLA2012), Sep 17, 2012: GEARBOX. MAKING METAL. NR 2 ENGINE CHIP LIGHT ILLUMNIATED ON LANDING. ENGINE WAS SHUTDOWN AND MECHANIC CALLED, MECHANIC FOUND FUZZ ON THE CHIP DETECTOR. MECHANIC CLEANED CHIP DETECTOR
- [SDR QMLA2012042612067](https://openairdocs.org/sdr/QMLA2012042612067), Apr 26, 2012: SKIN. DENTED. DURING MX INSPECTIONS A DENT MEASURING 2" HIGH X 1.5" WIDE X .127 INCHES DEEP WAS DISCOVERED ON THE L/E OF THE VERTICAL STABILIZER. THE ACFT WAS REPOSITIONED FO

All 58: https://openairdocs.org/model/eurocopter-as365n3/reports.md

## STCs that may be installed (OpenAirDocs) (47)

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 SR12205SE](https://openairdocs.org/stc/SR12205SE): Installation of Onboard Systems International Cargo Hook Kit. Onboard Systems International LLC
- [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 SR04606NY](https://openairdocs.org/stc/SR04606NY): Installation of Garmin Helicopter Terrain Awareness Warning System (HTAWS). Maxcraft Avionics Ltd
- [STC SR01949NY-D](https://openairdocs.org/stc/SR01949NY-D): Installation of a Honeywell Chadwick Model 15175 VXP System. Diagnostic Solution International LLC
- [STC SR00925DE](https://openairdocs.org/stc/SR00925DE): Installation of Garmin GTX 335/335R and GTX345/345R transponders to provide ADS-B Out and In functionality. Peregrine
- [STC SR04412NY](https://openairdocs.org/stc/SR04412NY): Installation of the Latitude SkyNode S200 Satellite Communication (SATCOM) and Tracker System. Maxcraft Avionics Ltd
- [STC SR04413NY](https://openairdocs.org/stc/SR04413NY): Installation of the Garmin GTN Navigator System. Maxcraft Avionics Ltd
- [STC SR04414NY](https://openairdocs.org/stc/SR04414NY): Installation of the Garmin GTX Transponder and GTS Traffic System. Maxcraft Avionics Ltd
- [STC SH7024SW-D](https://openairdocs.org/stc/SH7024SW-D): Relocation of the aircraft dataplate. Airbus Helicopters Inc
- [STC SR04147NY](https://openairdocs.org/stc/SR04147NY): Installation of Concorde (p/n RG-365) Lead Acid battery. DECA Aviation Engineering Limited
- [STC SR04056CH](https://openairdocs.org/stc/SR04056CH): Installation of L-3 Communications Avionics Systems Trilogy Electronic Standby Instrument (Model ESI-2000). Mayday Avionics Inc
- [STC SP03675AT](https://openairdocs.org/stc/SP03675AT): Installation of a Honeywell Solid State Cockpit Voice Flight Data Recorder (SSCVFDR). B/E Aerospace Inc
- [STC SR02586NY-D](https://openairdocs.org/stc/SR02586NY-D): Installation of a Lifeport MedDeck System 360-3650 on a Eurocopter AS365N3. Sikorsky Aircraft Corporation
- [STC SR02587NY-D](https://openairdocs.org/stc/SR02587NY-D): Installation of a Medical Interior. Sikorsky Aircraft Corporation
- [STC SH3529SW](https://openairdocs.org/stc/SH3529SW): Installation of medical attendant seats. RSG Products Inc
- [STC SH3530SW](https://openairdocs.org/stc/SH3530SW): Installation of dual patient litter. RSG Products Inc
- [STC SH3531SW](https://openairdocs.org/stc/SH3531SW): Installation of dual oxygen system. RSG Products Inc
- [STC SH3532SW](https://openairdocs.org/stc/SH3532SW): Installation of dual vacuum system. RSG Products Inc
- [STC SH3533SW](https://openairdocs.org/stc/SH3533SW): Installation of dual compressed air system. RSG Products Inc
- [STC SH3534SW](https://openairdocs.org/stc/SH3534SW): Installation of 110V AC Inverter System. RSG Products Inc
- [STC SH3535SW](https://openairdocs.org/stc/SH3535SW): Installation of Balloon Pump Model 700. RSG Products Inc
- [STC SH3536SW](https://openairdocs.org/stc/SH3536SW): Installation of transport incubator Model 1100. RSG Products Inc
- [STC SH5832SW](https://openairdocs.org/stc/SH5832SW): Installation of freon air conditioning system with belt driven compressor. RSG Products Inc
- [STC SR01717SE](https://openairdocs.org/stc/SR01717SE): Manufacture and installation of a Supplemental Lighting System. Aviation Specialties Unlimited Inc
- [STC SR01343LA](https://openairdocs.org/stc/SR01343LA): Installation of MASS Systems fire extinguisher cartridges as replacements for W. Kidde Aerospace/L Hotellier/Dexaero fire extinguisher cartridges in fire extinguisher bottles installed in the rotorcraft models noted on the FAA Approved Model List SR01343LA dated June 28, 2002, or later FAA approved revisions. This cartridge is in accordance with MASS Systems Master Drawing List MDL-861345, Revision N/C, dated May 31, 2002, or later FAA approved revisions. AMETEK AMERON LLC d/b/a MASS Systems
- [STC SR01344LA](https://openairdocs.org/stc/SR01344LA): Installation of MASS Systems fire extinguisher cartridges as replacements for W. Kidde Aerospace/L Hotellier/Dexaero fire extinguisher cartridges in fire extinguisher bottles installed in the rotorcraft models noted on the FAA Approved Model List SR01344LA dated June 28, 2002, or later FAA approved revisions. This cartridge is in accordance with MASS Systems Master Drawing List MDL-861355, Revision N/C, dated May 31, 2002, or later FAA approved revisions. AMETEK AMERON LLC d/b/a MASS Systems
- [STC SR00529NY](https://openairdocs.org/stc/SR00529NY): Installation of a three or four place divan and optional single seats. RSG AeroDesign LLC
- [STC SA00680SE](https://openairdocs.org/stc/SA00680SE): Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer. Electronics International
- [STC SH8801SW-D](https://openairdocs.org/stc/SH8801SW-D): Fabrication and installation of Simplex Model 301 fire attack system. Simplex Manufacturing Company
- [STC SH5867SW](https://openairdocs.org/stc/SH5867SW): Installation of tail floodlights. DeVore Aviation Corporation of America, a New Mexico Corporation
- [STC SH7579SW](https://openairdocs.org/stc/SH7579SW): Installation of a rotor disc light. DeVore Aviation Corporation of America, a New Mexico Corporation
- [STC SR09344RC](https://openairdocs.org/stc/SR09344RC): Installation of an Enhanced Ground Proximity Warning System (EGPWS). American Eurocopter Corporation
- [STC SH4747SW-D](https://openairdocs.org/stc/SH4747SW-D): Installation of exterior markings. American Eurocopter Corporation
- [STC SH5499SW-D](https://openairdocs.org/stc/SH5499SW-D): Installation of supplemental strobe light on belly panel. American Eurocopter Corporation
- [STC SH7014SW-D](https://openairdocs.org/stc/SH7014SW-D): Installation of a vertical fin tip mounted anti collision strobe light. American Eurocopter Corporation
- [STC SH7015SW-D](https://openairdocs.org/stc/SH7015SW-D): Installation of a chip detector system, fuzz burn. American Eurocopter Corporation
- [STC SH7022SW-D](https://openairdocs.org/stc/SH7022SW-D): Installation of radio master switch. American Eurocopter Corporation
- [STC SH7338SW-D](https://openairdocs.org/stc/SH7338SW-D): Installation of an aft mounted retractable Nightsun searchlight on the model SA365N-1 helicopter. American Eurocopter Corporation
- [STC SH7339SW-D](https://openairdocs.org/stc/SH7339SW-D): Installation of an extended radome and FLIR 2000 infrared imaging system. American Eurocopter Corporation
- [STC SH7706SW-D](https://openairdocs.org/stc/SH7706SW-D): Installation of improved autopilot coupler and Category II certification. American Eurocopter Corporation
- [STC SH7713SW-D](https://openairdocs.org/stc/SH7713SW-D): Installation of Ground Illumination Lights. American Eurocopter Corporation
- [STC SH8781SW-D](https://openairdocs.org/stc/SH8781SW-D): Installation of Bendix/King CAS 66A Traffic Collision Avoidance System(TCAS 1). American Eurocopter Corporation
- [STC SH363NE](https://openairdocs.org/stc/SH363NE): Replacement of auxiliary fuel boost pumps. Parker Hannifin Corporation, Airborne Division
- [STC SH5632SW](https://openairdocs.org/stc/SH5632SW): Installation of belt-driven freon air conditioner. Advanced Flight System, Inc
- [STC SH644NE](https://openairdocs.org/stc/SH644NE): Emergency Medical Service (EMS) interior installation. Custom Aircraft Completions, Inc
- [STC SA4302NM](https://openairdocs.org/stc/SA4302NM): Installation of Electronics Int'l digital automatic engine analyzer. Electronics International
- [STC SR0466NY](https://openairdocs.org/stc/SR0466NY) (historical): Installation of Garmin Helicopter Terrain Awareness Warning System (HTAWS). Maxcraft Avionics Ltd

## PMA parts (OpenAirDocs) (436, 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.

- [10-DB8991-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187207000220260407171343.0001): Piston Tube, LH. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces 18991-000-02 · Mar 25, 2026
- [10-DB8990-03](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179839523720260407171342.0001): Piston Tube, RH. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces 18990-000-03 · Mar 25, 2026
- [10-MD9465-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151050394820260407171346.0001): Yoke, Complete. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces 19465 · Mar 25, 2026
- [10-MD9324](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127298099820260407171345.0001): Axle. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces 19324 · Mar 25, 2026
- [10-MD8979](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123156311920260407171345.0001): PinTorque Link UpperMain Landing Gear. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces 18979 · Mar 25, 2026
- [10-MD8986-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID120973785220260407171345.0001): Screw, Axle MLG. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces 18986 · Mar 25, 2026
- [10-MD8980](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID113811276220260407171345.0001): PinTorque Link LowerMain Landing Gear. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces 18980 · Mar 25, 2026
- [5001905AB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166269024820260309213203.0001): Plate, Authorization. Aero Brake & Spares Inc. · PMA PQ0694SW · Replaces 5001905 · Feb 19, 2026
- [M2001-22HL](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193756421120250408205153.0001): Brush, Electrical Contact. Miraj Corporation · PMA PQ0870NE · Replaces 150SG1009-16 150SG1009-20 XL2150SG1009-5 · Mar 27, 2025
- [14316](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193185628620250312124240.0001): Cable Assembly,Pigtail, HighTemp Accelerometer. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [17294](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192743889520250312124305.0001): Bracket,Accelerometer Lemo Connector. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [14965](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180170101320250312124245.0001): Cable Assy PC/TRKRPanel Mount Pigtail Airframe. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [12888](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179103111820250312124233.0001): Bracket, Velo, S-76 T-Boom. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [14481](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168869321220250312124243.0001): Bracket, PhotocellEurocopterSA- 365, 315,318, T/R. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [17222](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167516038320250312124304.0001): Cable Assy Pigtail CCU toVXP. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [17009](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166123373320250312124301.0001): Kit, Accelerometer, ICP. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [14319](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164824297620250312124241.0001): Cable Assy, Pigtail, MagP/U, 200Degree C, Airframe. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [10494](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157922943020250312124232.0001): Accelerometer Hi-Temp. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [5876](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID153111437520250312124225.0001): Magnetic Pickup. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [14320](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152176546320250312124243.0001): Cable Assy, Pigtail, HighTempAccelerometer. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [16239](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149745771820250312124250.0001): Cable Assy, Pigtail Velo Pnl Jack 6SA/F. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [16757](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145014865020250312124259.0001): AccelerometerW/Bracket. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [16274](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142551998020250312124253.0001): CableAssembly, ICPAccelerometer. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [16167](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141724636420250312124248.0001): Cable Assy, PCELL PigtailAirframeB212/412. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [8866](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140063911220250312124230.0001): Velocimeter, EMI. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [15175](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134457768420250312124246.0001): VXP Onboard Monitor. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [10200](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133851913220250312124231.0001): Photocell Assy. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [PL915-17226](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128493745020250312124316.0001): Kit, VXP Hardwire Installation, AS365. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [17009-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126068164720250312124314.0001): Kit, Accelerometer,ICP (90 Deg). Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [17295](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124866632820250312124305.0001): Bracket, AccelerometerShim. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [17224](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124044843120250312124304.0001): VXP Control Panel 28 VDC. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [17293](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124018739220250312124305.0001): Bracket Connector. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [13157](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID114862362020250312124235.0001): Bracket, DummyReceptacle. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [42325-779](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID185509612520250116160347.0001): Support Handle Hoist 28V DC. Hornet Acquisition Co, LLC dba Onboard Systems · PMA PQ00038WB · Replaces 704A41816068 · Dec 13, 2024
- [42325-708](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182514299920250116160347.0001): Hoist Electrical Box. Hornet Acquisition Co, LLC dba Onboard Systems · PMA PQ00038WB · Replaces 704A41816069 · Dec 13, 2024
- [42325-16-6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180053845520250116160346.0001): 28V DC Elec Categorie 1 Hoist. Hornet Acquisition Co, LLC dba Onboard Systems · PMA PQ00038WB · Replaces 704A41815120 · Dec 13, 2024
- [44301-440](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168862056520250116160348.0001): Kit - Cable Hook. Hornet Acquisition Co, LLC dba Onboard Systems · PMA PQ00038WB · Replaces 704A41816071 · Dec 13, 2024
- [42325-1156](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID160042841220250116160347.0001): Power Cable Hoist. Hornet Acquisition Co, LLC dba Onboard Systems · PMA PQ00038WB · Replaces 704A41816070 · Dec 13, 2024
- [42325-16-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133091495720250116160346.0001): 28V DC Elec Class 1 Hoist. Hornet Acquisition Co, LLC dba Onboard Systems · PMA PQ00038WB · Replaces 704A41815112 · Dec 13, 2024
- [42325-803](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125108555220250116160347.0001): Hoist Handle. Hornet Acquisition Co, LLC dba Onboard Systems · PMA PQ00038WB · Replaces 704A41816067 · Dec 13, 2024
- [42315-281](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106731494120250116160345.0001): Pyrotechnic Cartridge. Hornet Acquisition Co, LLC dba Onboard Systems · PMA PQ00038WB · Replaces 704A38710042 · Dec 13, 2024
- [10-MD8980](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197943873020241219224033.0001): PinTorque Link LowerMain Landing Gear. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces 18980 · Nov 19, 2024
- [10-MD9324](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192123755620241219224034.0001): Axle. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces 19324 · Nov 19, 2024
- [10-DB8990-03](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178135542020250219211004.0001): Piston Tube, RH. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces 18990-000-03 · Nov 19, 2024
- [10-MD8980](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172068561220250219211006.0001): PinTorque Link LowerMain Landing Gear. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces 18980 · Nov 19, 2024
- [10-MD8986-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170569036520250219211006.0001): Screw, Axle MLG. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces 18986 · Nov 19, 2024
- [10-MD9465-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167129933120250219211007.0001): Yoke, Complete. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces 19465 · Nov 19, 2024
- [10-MD8979](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163508741420241219224033.0001): PinTorque Link UpperMain Landing Gear. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces 18979 · Nov 19, 2024
- [10-MD9324](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154968549520250219211007.0001): Axle. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces 19324 · Nov 19, 2024
- [10-MD8979](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID150964564020250219211006.0001): PinTorque Link UpperMain Landing Gear. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces 18979 · Nov 19, 2024

All of them: https://openairdocs.org/model/eurocopter-as365n3/pma.md

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