# Aerospatiale AS 365 N2

- Type: Aircraft model (FAA registry)
- Registry code: 8680798
- Manufacturer (registry): AEROSPATIALE
- Model: AS 365 N2
- 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: 1
- Page: https://openairdocs.org/model/aerospatiale-as-365-n2

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 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 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 2022-01-03](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 2016-09-09](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 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 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 2013-06-07](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
- [AD 2004-16-15 R1](https://openairdocs.org/ad/2004-16-15-R1): Main gearbox (MGB) base plate · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 4 more. Effective Aug 30, 2006
- [AD 2006-06-02](https://openairdocs.org/ad/2006-06-02): Main gearbox (MGB) · Airbus Helicopters AS-365N2, SA-365N, SA-365N1 and 1 more. Effective Apr 17, 2006
- [AD 2005-13-23](https://openairdocs.org/ad/2005-13-23): Hydraulic brake hose (hose) · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 3 more. Effective Jul 29, 2005
- [AD 2003-22-15](https://openairdocs.org/ad/2003-22-15): Fuel air vent hoses · Airbus Helicopters AS-365N2, AS-365N3, SA-365N and 1 more. Effective Jan 5, 2004
- [AD 2003-20-12](https://openairdocs.org/ad/2003-20-12): Siren Cargo Hook Locking Catch · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 3 more. Effective Nov 18, 2003
- [AD 2003-14-12](https://openairdocs.org/ad/2003-14-12): Equipment Log Card (FME) · Airbus Helicopters AS-365N2, AS-365N3, AS332C and 23 more. Effective Aug 25, 2003
- [AD 2003-14-19](https://openairdocs.org/ad/2003-14-19): Main servocontrols · Airbus Helicopters AS-365N2, AS-365N3, AS355F and 7 more. Effective Aug 21, 2003
- [AD 2003-08-53](https://openairdocs.org/ad/2003-08-53): Tail rotor blade (blade) · Airbus Helicopters AS-365N2, AS-365N3, SA-365N1 and 1 more. Effective Jun 20, 2003
- [AD 2002-23-04](https://openairdocs.org/ad/2002-23-04): 9-degree frame · Airbus Helicopters AS-365N2, AS-365N3, SA-365N and 1 more. Effective Jan 3, 2003

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
- [AD 2000-10-08 R1](https://openairdocs.org/ad/2000-10-08-R1) (historical): Tail Rotor Blade · Eurocopter France AS-365N2, SA-365N1 and SA-366G1. Effective Nov 7, 2001
- [AD 2000-10-08](https://openairdocs.org/ad/2000-10-08) (historical): Tail Rotor Blades · Eurocopter France AS-365N2, SA-365N1 and SA-366G1. Effective Jun 21, 2000
- [AD 99-21-24](https://openairdocs.org/ad/99-21-24) (historical): Tightening Torque Of Bolts Inspection · Eurocopter France AS-365N2, SA-365C, SA-365C1 and 4 more. Effective Nov 18, 1999
- [AD 98-10-04](https://openairdocs.org/ad/98-10-04) (historical): Kevlar Tie-Bar Inspection · Eurocopter France AS-365N2, SA-365N1 and SA-366G1. Effective Jun 11, 1998
- [AD 98-08-14](https://openairdocs.org/ad/98-08-14) (historical): Diagonal Cross-Member · Eurocopter France AS-365N2, SA-365N and SA-365N1. Effective May 15, 1998

All 88: https://openairdocs.org/model/aerospatiale-as-365-n2/ads.md

## Information bulletins (advisory) (1)

- [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

## Registered aircraft (1)

- [N403HH](https://openairdocs.org/aircraft/N403HH): [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 1999, S/N 6570

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (170, newest 50)

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

- [SDR 2026F00067](https://openairdocs.org/sdr/2026F00067), Apr 9, 2026: PIN. SHEARED. PER PILOT'S SAFETY REPORT: "SCENE FLIGHT FROM WABASH COUNTY TO PRMC- SAM 1 RESPONDED. UPON ARRIVING THE PATIENT WAS HOT LOADED. INTITALLY MEDIC HAD TROUBLE CLOS
- [SDR QMLA2024101520133](https://openairdocs.org/sdr/QMLA2024101520133), Oct 14, 2024: UNKNOWN. SMOKE. SMOKE COMING OUT OF BACK OF INSTRUMENT PANEL, COULDN'T DUPLICATE. THIS AIRCRAFT HAS BEEN RETURNED TO REVENUE SERVICE, REF #MEC-000964.
- [SDR 2024FA0000291](https://openairdocs.org/sdr/2024FA0000291), Apr 4, 2024: SEARCH LIGHT. MALFUNCTIONED. ON DEPARTURE FROM (KGWB), HOSPITAL THE PILOT SIDE SEARCH LIGHT BEGAN PANNING TO THE RIGHT IN A 360-DEGREE ROTATION THAT COULD NOT BE STOPPED O, CONTROL BY THE P
- [SDR 2024FA0000256](https://openairdocs.org/sdr/2024FA0000256), Mar 25, 2024: MODULE. FAULTED. CHIPS 2 ILLUMINATED AFTER GEAR EXTENSION AND LANDING CHALLENGE AND RESPONSE CALL OUTS. JUST PASSING THROUGH 2000' MSL AFTER CALL OUTS WERE COMPLETE THE CHIPS 2 
- [SDR OLJA2023060500301](https://openairdocs.org/sdr/OLJA2023060500301), Sep 8, 2022: BEARING. FAILED. #1 ENGINE LOSS OF OIL PRESSURE FOLLOWED BY THE #1 ENGINE FAILURE. AT APPROXIMATELY 2050L, COMPLETED AN UNEVENTFUL TAKEOFF UNDER NVGS FROM A NIGHT SCENE AT THREE
- [SDR QMLA201911229086](https://openairdocs.org/sdr/QMLA201911229086), Nov 20, 2019: DUCT. LOOSE. BURNING SMELL REPORTED BY THE MEDICAL CREW SITTING ON THE PATIENT COMPARTMENT (BACK COMPARTMENT) JUST BEFORE LANDING AT THE BASE, I74. THE MECHANIC WAS CALLED T
- [SDR QMLA2018080118091](https://openairdocs.org/sdr/QMLA2018080118091), Jul 30, 2018: STRUCTURE. CORRODED. CORROSION FOUND UNDER THE LT AND RT FWD CREW DOOR (MIDDLE) UPPER HINGE. THIS DAMAGE IS CURRENTLY BEING REVIEWED BY THE MANUFACTURER FOR AN APPROVED REPAIR PROCE
- [SDR QMLA2018020618015](https://openairdocs.org/sdr/QMLA2018020618015), Feb 6, 2018: FRAME. CRACKED. MULTIPLE CRACKS FOUND ON THE REAR FRAME, STATION 5915 UNDER CARGO DOOR LATCH STOP.
- [SDR QMLA2013120113170](https://openairdocs.org/sdr/QMLA2013120113170), Dec 1, 2013: SWITCH. INTERMITTENT. THE PILOT WAS INBOUND TO A NEARBY AIRPORT. ON APPROACH, IT WAS NOTED THAT THERE WERE THREE GREEN DOWN & LOCKED GEAR INDICATIONS. AS THE PILOT INITIATED THE LAND
- [SDR QMLA2013020413022](https://openairdocs.org/sdr/QMLA2013020413022), Feb 4, 2013: FLEX COUPLING. BROKEN. DURING INSPECTION OF ACFT AFTER REMOVAL OF TAILROTOR AFT DRIVE SHAFT FOUND FLEX COUPLING BROKEN STRAPS AND GROOVE MARKS IN TAILROTOR GEARBOX HSG. NO DAMAGE ALLO
- [SDR MHI2012F00000](https://openairdocs.org/sdr/MHI2012F00000), Jun 5, 2012: TURBINE BLADES. DESTROYED. DURING TAXI BOTH PILOTS HEARD AN ABNORMAL WHINNING NOISE COMING FROM THE NR 1 ENGINE, IMMEDIATELY FOLLOWED BY A NR 1 ENGINE CHIP LIGHT. THEY SHUT THE ENGINES DO
- [SDR MHIA20120605001](https://openairdocs.org/sdr/MHIA20120605001), Jun 3, 2012: ENGINE. MALFUNCTIONED. THE AIRCRAFT WAS SCHEDULED FOR A CHARTER. WHILE TAXIING TO THE TAKEOFF SPOT BOTH PILOTS HEARD A LOUD NOISE COMING FROM THE NR 1 ENGINE FOLLOWED BY A CHIP LIGHT.
- [SDR QMLA2011121011116](https://openairdocs.org/sdr/QMLA2011121011116), Dec 10, 2011: FILTER. DIRTY. ON FINAL APPROACH, PILOT NOTICED THE COLLECTIVE BECAME STIFF AND THE PEDALS HAD A RATCHET FEEL TO THEM. THE PILOT DECIDED TO ABORT THE APPROACH AND DIVERTED FOR
- [SDR QMLA2011012611015](https://openairdocs.org/sdr/QMLA2011012611015), Jan 26, 2011: BLADE. CRACKED. MECHANIC WAS PERFORMING A VISUAL INSP OF THE MAIN ROTOR BLADES WHEN HE DETECTED A CRACK AT STA 2900 ON THE TOP OF THE BLADE. THE CRACK IS 45MM LONG WITH THE OTB
- [SDR QMLA2010081910053](https://openairdocs.org/sdr/QMLA2010081910053), Aug 19, 2010: DOUBLER. DAMAGED. UPON INSP REQUIRED FOR AAIP FLIP, A CRACK WAS DISCOVERED ON THE CO-PILOTS 25 DEGREE FRAME DOUBLER THAT WAS INSTALLED IAW SB 53.00.41. DOUBLER WAS RE-RIVETED IN 
- [SDR KY1R2011072510012](https://openairdocs.org/sdr/KY1R2011072510012), Jul 25, 2010: CHIP DETECTOR. BROKEN. ON PREFLIGHT INSPECTION, PILOT FOUND M04 MAGNETIC DETECTOR TIP BROKEN FROM BASE. TIP OF THE DETECTOR WAS RETAINED BY THE MAGNETIC BASE, AND SUBSEQUENTLY REMOVED
- [SDR 2009FA0000070](https://openairdocs.org/sdr/2009FA0000070), Feb 7, 2009: LANDING GEAR. MALFUNCTIONED. RT LANDING GEAR WOULD NOT LOCK DOWN. PILOT RETURNED TO DEPARTURE WHILE TROUBLESHOOTING ISSUE AND EXECUTING EMERGENCY CHECKLIST. ADDITIONAL TROUBLESHOOTING OVER 
- [SDR BAQA200700036](https://openairdocs.org/sdr/BAQA200700036), Oct 4, 2007: LINE. BURNED. UPON SHUTDOWN, PILOT SMELLED SMOKE, SAW SMOKE COMING FROM NR1 ENGINE, OPENED COWLING SAW SMALL FIRE ON STARTER GENERATOR, RAN BACK TO COCKPIT ACQUIRED THE HANDH
- [SDR BAQA200700023](https://openairdocs.org/sdr/BAQA200700023), Jun 29, 2007: WIRE HARNESS. DEFECTIVE. DURING LEVEL FLIGHT NR 1 ENGINE FIRE LIGHT ILLUMINATED. AIRCRAFT WAS LANDED WITHOUT FURTHER INCIDENT. AFTER MECHANIC INVESTIGATED FOR CAUSE FOUND ENGINE WIRING 
- [SDR BAQA200700002](https://openairdocs.org/sdr/BAQA200700002), Jan 11, 2007: TURBINE WHEEL. DAMAGED. DURING MAINTENANCE GROUND RUNS, STARTED NR 1 ENGINE AND NR 2 ENGINES TO PERFORM REQUIRED MAINTENANCE CHECKS AFTER INSPECTION OF AIRCRAFT AND ENGINES. SHUTDOWN E
- [SDR BAQA200700003](https://openairdocs.org/sdr/BAQA200700003), Jan 11, 2007: TURBINE WHEEL. DAMAGED. DURING MAINTENANCE GROUND RUNS, STARTED NR 1 ENGINE AND NR 2 ENGINES TO PERFORM REQUIRED MAINTENANCE CHECKS AFTER INSPECTION OF AIRCRAFT AND ENGINES. SHUTDOWN E
- [SDR BAQA2006008](https://openairdocs.org/sdr/BAQA2006008), Dec 4, 2006: SERVO. BYPASSING. DURING START UP, AS HYDRAULIC PRESSURE INCREASED THE TAIL ROTOR SERVO WENT HARD OVER TO THE LEFT.
- [SDR BAQA200600002](https://openairdocs.org/sdr/BAQA200600002), Oct 10, 2006: FRAME. BROKEN. DURING A 600 HOUR AIRFRAME INSPECTION, FOUND THE PILOT'S 25 DEGREE FRAME BROKEN. THIS FRAME WAS REPAIRED ABOVE THE AREA WHERE IT IS BROKEN NOW DURING THE LAST 5
- [SDR BAQA200600003](https://openairdocs.org/sdr/BAQA200600003), Oct 10, 2006: FRAME. BROKEN. DURING A 600 HOUR AIRFRAME INSPECTION, FOUND THE PILOT'S 25 DEGREE FRAME BROKEN. THIS FRAME WAS REPAIRED ABOVE THE AREA WHERE IT IS BROKEN NOW DURING THE LAST 5
- [SDR BAQA200600001](https://openairdocs.org/sdr/BAQA200600001), Oct 9, 2006: NUT. BROKEN. DURING PRE-FLIGHT INSPECTION FOR A MAINTENANCE INDUCTION CHECK FLIGHT, FOUND PLAY IN THE TAIL ROTOR OUTPUT FLANGE. GROUNDED AIRCRAFT. REMOVED TAIL ROTOR OUTPUT 
- [SDR BAQ2006F00003](https://openairdocs.org/sdr/BAQ2006F00003), Jul 5, 2006: ENGINE. MAKING METAL. ENGINE CHIP DETECTOR ILLUMINATED ON GROUND. REAR BEARING ELECTRICAL DETECTOR AND ACCESSORY GEARBOX AND REDUCTION GEARBOX WERE INSPECTED WITH METAL FOUND ON REAR
- [SDR AU510001643](https://openairdocs.org/sdr/AU510001643), Dec 12, 2005: COUPLING. CRACKED. (AUS) TAIL ROTOR DRIVESHAFT FORWARD FLEXIBLE COUPLING CRACKED. INVESTIGATION FOUND MECHANICAL DAMAGE ON THE EDGE OF THE COUPLING AT ONE END OF THE CRACK. (OTHER
- [SDR 2005FA0000115](https://openairdocs.org/sdr/2005FA0000115), Nov 19, 2004: COUPLING. CRACKED. DURING INSPECTION FOUND RT FORWARD ENGINE/ MGB DRIVE FLEX COUPLING CRACKED. REPLACED WITH NEW. (RECORD NR 98086) (K)
- [SDR MHIA098086](https://openairdocs.org/sdr/MHIA098086), Nov 19, 2004: COUPLING. CRACKED. DURING INSPECTION, FOUND RT FORWARD ENGINE/MGB DRIVE FLEX COUPLING CRACKED. REPLACED WITH NEW.
- [SDR BAQA094395](https://openairdocs.org/sdr/BAQA094395), Apr 30, 2004: INDICATOR. INOPERATIVE. WILL NOT READ FUEL PRESSURE, NEEDLE AT ZERO. REPLACED WITH SERVICABLE UNIT. 05/10/2004
- [SDR BAQA093954](https://openairdocs.org/sdr/BAQA093954), Mar 10, 2004: TRANSMITTER. INTERMITTENT. PRESSURE TRANSMITTER IS CAUSING GUAGE FLUCTUATIONS (TOP-BOTTOM). REPLACED WITH SERVICABLE UNIT FORM ASSET.
- [SDR BAQA092802](https://openairdocs.org/sdr/BAQA092802), Feb 17, 2004: TACH GENERATOR. FAILED. TACH GENERATOR SCRAPPED, VELOCITY GENERATOR WAS SCRAPPED ON SITE IAW AEC, UNIT WAS REMOVED FOR NO NR INDICATION. REPLACED WITH UNIT FROM ASSET, ORDER TO REPLACE
- [SDR BAQA092534](https://openairdocs.org/sdr/BAQA092534), Feb 5, 2004: TRANSMITTER. READS HIGH. OIL PRESS READ HIGH, INTERMITTENT. REPLACED WITH SERVICEABLE ASSET UNIT. 02/26/2004
- [SDR BAQA092533](https://openairdocs.org/sdr/BAQA092533), Feb 5, 2004: ACTUATOR. INTERMITTENT. PITCH ACTUATOR INTERMITTENT KICK OFF. OFF PITCH LANES. REPLACED WITH SERVICEABLE ASSET UNIT. 02/26/2004
- [SDR BAQA092798](https://openairdocs.org/sdr/BAQA092798), Feb 4, 2004: TRANSMITTER. FLUCTUATES. FUEL PRESSURE GAUGE TRANSMITTER FLUCTUATING. REPLACED WITH SERVICEABLE ASSET UNIT.
- [SDR MHIA092672](https://openairdocs.org/sdr/MHIA092672), Feb 3, 2004: INDICATOR. INOPERATIVE. RT LANDING GEAR LIGHT INOPERATIVE, REPLACED INDICATOR.
- [SDR BAQA092507](https://openairdocs.org/sdr/BAQA092507), Jan 27, 2004: ACTUATOR. FAILED. FAILED MEGGER TEST. REPLACED WITH SERVICABLE UNIT. 02/04/2004
- [SDR BAQA092505](https://openairdocs.org/sdr/BAQA092505), Jan 26, 2004: ACTUATOR. STICKING. YAW ACTUATOR STICKING, TAP UNIT IT MOVES. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/04/2004
- [SDR BAQA092793](https://openairdocs.org/sdr/BAQA092793), Jan 21, 2004: COMPUTER. INOPERATIVE. UNIT IS BEING SENT TO AEC FOR WARRANTY REPAIR. REASON FOR REMOVAL, BOTH ROLL ACTUATORS WERE INOPERATIVE. REPLACED WITH SERVICEABLE UNIT FROM ASSET (S/N 545)
- [SDR BAQA092792](https://openairdocs.org/sdr/BAQA092792), Jan 21, 2004: ACTUATOR. INOPERATIVE. UNIT IS BEING SENT TO AEC FOR WARRANTY REPAIR. REASON FOR REMOVAL, BOTH ROLL ACTUATORS WERE INOPERATIVE. REPLACED WITH SERVICEABLE UNIT FROM ASSET (S/N 634)
- [SDR BAQA091939](https://openairdocs.org/sdr/BAQA091939), Jan 12, 2004: SIGHT GAUGE. DIRTY. SIGHT IS UNREADABLE, NEEDS CLEANING. REPLACED WITH SERVICABLE UNIT.
- [SDR BAQA092080](https://openairdocs.org/sdr/BAQA092080), Jan 10, 2004: INVERTER. FAILED. INVERTER INOPERATIVE. FAILED OUT OF THE BOX. REPLACED WITH SERVICEABLE UNIT. 01/19/2004
- [SDR BAQA091971](https://openairdocs.org/sdr/BAQA091971), Dec 26, 2003: VOLT REGULATOR. FAILED. VOLTAGE REGULATOR WILL NOT CONTROL VOLTAGE OF GENERATOR. REPLACED WITH SERVICEABLE UNIT. 01/14/2004
- [SDR BAQA091617](https://openairdocs.org/sdr/BAQA091617), Dec 24, 2003: INVERTER. INOPERATIVE. INVERTER INOPERATIVE. REPLACED WITH SERVICABLE UNIT. 01/06/2004
- [SDR BAQA091615](https://openairdocs.org/sdr/BAQA091615), Dec 11, 2003: PUMP. INOPERATIVE. FUEL BOOST PUMP INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 01/08/2004
- [SDR AUS20031132](https://openairdocs.org/sdr/AUS20031132), Nov 5, 2003: PIN. FAILED. (AUS) ENGINE TORQUEMETER PIN FAILED. PIN COULD NOT BE FOUND AND IT WAS SUSPECTED THAT THE PIN WAS SOMEWHERE IN THE ENGINE. ENGINE WAS REMOVED FOR REPAIR.
- [SDR BAQA090123](https://openairdocs.org/sdr/BAQA090123), Oct 22, 2003: DRAIN VALVE. LEAKING. FAILED ENGINE CHECK. LEAKS . PART ONLY LASTED 9 MONTHS. REPLACED WITH SERVICEABLE UNIT.
- [SDR BAQA089940](https://openairdocs.org/sdr/BAQA089940), Oct 14, 2003: HOUSING. CRACKED. FUEL FILTER HOUSING IS STRIPPED AND CRACKED. FAXED SCRAP CERTIFICATION WITH MMIR. REPLACED WITH SERVICEABLE UNIT. 10/15/03
- [SDR BAQA090072](https://openairdocs.org/sdr/BAQA090072), Oct 9, 2003: SERVO. LEAKING. SERVO IS LEAKING. PART ON AIRCRAFT FOR ONLY 1.1 HOURS. REPLACED WITH SERVICEABLE UNIT.
- [SDR BAQA089616](https://openairdocs.org/sdr/BAQA089616), Oct 8, 2003: PUMP. MAKING METAL. HYDRAULIC PUMP MAKING METAL. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT.

All 170: https://openairdocs.org/model/aerospatiale-as-365-n2/reports.md

## STCs that may be installed (OpenAirDocs) (89, 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 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 SH1539NM](https://openairdocs.org/stc/SH1539NM): Installation of an air-conditioning system. Air Comm Corporation
- [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 SH8626SW](https://openairdocs.org/stc/SH8626SW): Installation of a Lucas electric hoist. RSG Products
- [STC SH921NE](https://openairdocs.org/stc/SH921NE): Installation of an Emergency Medical Services Interior. RSG Products
- [STC SH7574SW](https://openairdocs.org/stc/SH7574SW): Installation of a dual pivoting litter carriage. RSG Products
- [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 SH922NE](https://openairdocs.org/stc/SH922NE): Installation of an emergency medical services Interior. Sikorsky Aircraft Corporation
- [STC SH924NE](https://openairdocs.org/stc/SH924NE): Installation of a Bendix/King EFS 50 Electronic Flight Instrumentation System and a Bendix/King KNS 660 Flight Management System. Sikorsky Aircraft Corporation
- [STC SR00022NY](https://openairdocs.org/stc/SR00022NY): Installation of Medevac (EMS) interior. Sikorsky Aircraft Corporation
- [STC SR00288NY](https://openairdocs.org/stc/SR00288NY): Remove the right hand floor mounted litter, and install a new right hand floor mounted litter support and a 2 person seat. Sikorsky Aircraft Corporation
- [STC SR00580NY](https://openairdocs.org/stc/SR00580NY): Installation of Medical Interior. 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 SH2989SO](https://openairdocs.org/stc/SH2989SO): Installation of a shock isolation mount kit for the FLIR imager. Bell Helicopter Textron 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 SR09351RC](https://openairdocs.org/stc/SR09351RC): Installation of Bendix/King EFS 50 Electronic Flight Instrumentation System (EPIS). Texas Aviation Services
- [STC SR00529NY](https://openairdocs.org/stc/SR00529NY): Installation of a three or four place divan and optional single seats. RSG AeroDesign LLC
- [STC SR00530NY](https://openairdocs.org/stc/SR00530NY): Installation of a cocoon wall panel system. Texas Aviation Services
- [STC SH699NE](https://openairdocs.org/stc/SH699NE): Installation of a Avionics Specialties power analyzer and recorder Nos. SL17036 & SL17070 . Aerosonic Corporation
- [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 SH5866SW](https://openairdocs.org/stc/SH5866SW): Installation of forward facing recognition lights. DeVore Aviation Corporation of America, a New Mexico Corporation
- [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 SH8804SW-D](https://openairdocs.org/stc/SH8804SW-D): Installation of a Universal Navigation UNS-1C Flight Management System for IFR enroute and non-precision approaches. American Eurocopter Corporation
- [STC SH4747SW-D](https://openairdocs.org/stc/SH4747SW-D): Installation of exterior markings. American Eurocopter Corporation
- [STC SR00523DE](https://openairdocs.org/stc/SR00523DE): Installation of Emergency Medical Services (EMS) interior. Air Methods Corporation
- [STC SR00524DE](https://openairdocs.org/stc/SR00524DE): Installation of an Articulating Patient Loading System (APLS). Air Methods Corporation
- [STC SR00525DE](https://openairdocs.org/stc/SR00525DE): Installation of two Aft Jump Seats. Air Methods Corporation
- [STC SH2215NM-D](https://openairdocs.org/stc/SH2215NM-D): Installation of a Sperry Digital Automatic Flight Control System, Single and Two Pilot IFR. American Eurocopter Corporation
- [STC SH5420SW-D](https://openairdocs.org/stc/SH5420SW-D): Installation of medical attendant seats. American Eurocopter Corporation

All 89: https://openairdocs.org/model/aerospatiale-as-365-n2/stcs.md

## The same model under other registry codes

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

- [Eurocopter France AS-365N2](https://openairdocs.org/model/eurocopter-france-as-365n2): 3 registered aircraft, registry code 8680983
- [Eurocopter AS365N2](https://openairdocs.org/model/eurocopter-as365n2): 1 registered aircraft, registry code 868095C

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