# Aerospatiale SA365N

- Type: Aircraft model (FAA registry)
- Registry code: 8680669
- Manufacturer (registry): AEROSPATIALE
- Model: SA365N
- Aircraft type: Rotorcraft
- Category: Rotorcraft
- Engines: 2 · Turbo-shaft
- Seats: 6
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS H10EU](https://openairdocs.org/tcds/H10EU) (OpenAirDocs)
- Holder: Airbus Helicopters
- Registered aircraft: 0
- Page: https://openairdocs.org/model/aerospatiale-sa365n

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 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 2023-22-14](https://openairdocs.org/ad/2023-22-14): Tail rotor gearbox · Airbus Helicopters SA-365C1, SA-365C2 and SA-365N. Effective Dec 26, 2023
- [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 2022-11-18](https://openairdocs.org/ad/2022-11-18): Engine Cowling System · Airbus Helicopters AS355E, AS355F, AS355F1 and 7 more. Effective Jul 13, 2022
- [AD 2022-01-03](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 2021-03-06](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 2020-20-14](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 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 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 2011-16-05](https://openairdocs.org/ad/2011-16-05): Fuel switches · Airbus Helicopters SA-365N and SA-365N1. Effective Sep 12, 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 2010-06-07](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 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
- [AD 2002-15-08](https://openairdocs.org/ad/2002-15-08): Cargo Hooks · Airbus Helicopters AS-365N2, AS-365N3, AS332C and 21 more. Effective Sep 6, 2002
- [AD 2000-15-19](https://openairdocs.org/ad/2000-15-19): Sand Filter Ejection Nozzle · Airbus Helicopters AS-365N2, AS-365N3, SA-365N and 1 more. Effective Aug 24, 2000
- [AD 2000-11-18](https://openairdocs.org/ad/2000-11-18): Bearing Attachment Joint · Airbus Helicopters AS-365N2, AS-365N3, SA-365C and 5 more. Effective Jul 11, 2000
- [AD 2000-10-13](https://openairdocs.org/ad/2000-10-13): Sliding Door · Airbus Helicopters AS-365N2, AS-365N3, SA-365N and 1 more. Effective Jun 6, 2000
- [AD 99-23-02](https://openairdocs.org/ad/99-23-02): "CONNECTRAL" Green Electrical Module · Airbus Helicopters AS-365N2, SA-365N and SA-365N1. Effective Dec 8, 1999
- [AD 99-21-14](https://openairdocs.org/ad/99-21-14): Electrical Master Box Assembly Inspection · Airbus Helicopters AS-365N2, SA-360C Dauphin, SA-365C and 5 more. Effective Nov 12, 1999
- [AD 85-15-01 R2](https://openairdocs.org/ad/85-15-01-R2): Main Rotor Mask · Airbus Helicopters SA-365C, SA-365C1, SA-365C2 and 1 more. Effective Oct 19, 1999

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 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 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 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 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 98-08-14](https://openairdocs.org/ad/98-08-14) (historical): Diagonal Cross-Member · Eurocopter France AS-365N2, SA-365N and SA-365N1. Effective May 15, 1998
- [AD 97-15-15](https://openairdocs.org/ad/97-15-15) (historical): Main Gear Box Planetary Gear Shaft · Eurocopter France SA-365N, SA-365N1 and SA-366G1. Effective Feb 23, 1998

All 72: https://openairdocs.org/model/aerospatiale-sa365n/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

None registered with this model now.

## NTSB investigations (1)

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 CHI05FA192](https://openairdocs.org/ntsb/CHI05FA192), Jul 14, 2005: Aerospatiale AS365N (N365S), Valparaiso, IN, substantial damage. Probable cause: The loose tail rotor drive shaft coupling due to its improper installation by the operator's maintenance personnel, which resulted in the failure of the tail rotor drive shaft. An additional cause…

## 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 20050714024169A](https://openairdocs.org/incident/20050714024169A), Jul 14, 2005: Aerosp SA365N (N365S), Valparaiso, IN, Substantial damage. (-23) Pilot had aircraft in hover on an approximately 230-240 degree heading, 4-6 foot height. Pilot then began a pedal turn to right, aircraft got to…
- [Incident 19930816033489I](https://openairdocs.org/incident/19930816033489I), Aug 16, 1993: Aerosp SA365N (N24AE), Latrobe, PA, Minor damage. Lost control on a practice slope takeoff and landing. Lower edge of right outboard fin contacted ground.
- [Incident 19930606021019I](https://openairdocs.org/incident/19930606021019I), Jun 6, 1993: Aerosp SA365N (N24AE), St Marys, PA, Minor damage. Uncontrolled turn to left after engine start. Lifted aircraft off platform. Returned to pad. Shut engines down.
- [Incident 19930504016689I](https://openairdocs.org/incident/19930504016689I), May 4, 1993: Aerosp SA365N (N917EG), Utica, NY, Minor damage. Truck struck the tail stinger as pilot was attempting to land. Angles of vision obscuring view of pilot and driver.
- [Incident 19880618059339I](https://openairdocs.org/incident/19880618059339I), Jun 18, 1988: Aerosp SA365N (N365SJ), St Joseph, MI, Minor damage. Hit a light pole during a night landing in a hospital parking lot. Minor damage to the helicopter.

## Service difficulty reports (196, newest 50)

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

- [SDR QMLA2013102513148](https://openairdocs.org/sdr/QMLA2013102513148), Oct 25, 2013: STARFLEX. CRACKED. DURING MAINTENANCE INSPECTION, A CRACK WAS FOUND IN THE ARM OF THE STARFLEX. THE STARFLEX IS CURRENTLY BEING REPLACED AT THE TIME OF THIS SUBMISSION.
- [SDR QMLA2012022412054](https://openairdocs.org/sdr/QMLA2012022412054), Feb 24, 2012: CONNECTOR. LOOSE. AT ABOUT 10-20 FT AFTER TAKEOFF, AIRCRAFT BEGAN A RAPID YAW TO THE LT. DID NOT HAVE FULL AUTHORITY OF THE RT YAW PEDAL. WAS ABLE TO STOP THE YAW RATE AND STABIL
- [SDR QMLA2011072311080](https://openairdocs.org/sdr/QMLA2011072311080), Jul 23, 2011: CONNECTOR. CONTAMINATED. THE NR 1 GAUGE WENT TO ZERO WITH NO ASSOCIATED WARNING LIGHT WHILE IN CRUISE FLIGHT. THE PILOT IMMEDIATELY LANDED AT THE CLOSEST AIRPORT AND CALLED THE MECHANIC
- [SDR QMLA2011061411064](https://openairdocs.org/sdr/QMLA2011061411064), Jun 14, 2011: CABLE. BROKEN. PILOT NOTED ON ENGINE START, THAT THE NR 2 ENGINE NG INDICATION WAS 15 PERCENT LOWER THAN THE NR 1 ENGINE NG INDICATION. PERFORMED A NORMAL ENGINE SHUTDOWN AND 
- [SDR QMLA2011052011058](https://openairdocs.org/sdr/QMLA2011052011058), May 20, 2011: CONNECTOR. LOOSE. AFTER LANDING AT A SCENE TO PICK UP A PATIENT, THE PILOT NOTICED THE NR 1 ENGINE OIL PRESSURE INDICATION DROP TO 0 PSI. THE PILOT IMMEDIATELY SHUTDOWN ACFT, AND
- [SDR EGRR119766](https://openairdocs.org/sdr/EGRR119766), May 22, 2008: WINDOW FRAME. CRACKED. DURING 600 HR INSPECTION TECHNICIAN FOUND LT AND RT UPPER WINDSHEILD FRAMES CRACKED. REPAIRS TO LT AND RT UPPER WINDSHIELD FRAMES WILL BE PERFORMED IN ACCORDANC
- [SDR EGRR119748](https://openairdocs.org/sdr/EGRR119748), May 20, 2008: DOUBLER. CORRODED. DURING 600 HR INSPECTION FOUND CORROSION ON LT AND RT DOUBLERS AT FITTINGS IN TAILBOOM AT AIRCRAFT STATION 7951 MM. REMOVED DOUBLER INSPECTED AND REPAIRED IAW A
- [SDR BAQ2006F00004](https://openairdocs.org/sdr/BAQ2006F00004), Jul 5, 2006: GEARBOX. 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 BAQA106369](https://openairdocs.org/sdr/BAQA106369), Oct 14, 2005: TACHOMETER. FLUCTUATES. NG GAUGE WOULD FLUCTUATE THROUGH ENTIRE ENGINE RANGE.
- [SDR EGRA20041227](https://openairdocs.org/sdr/EGRA20041227), Nov 5, 2004: COWLING. DEPARTED. PILOT NOTICED COWLING WAS MISSING FROM AIRCRAFT AFTER HE LANDED AT HIS HOME BASE. HE REPORTED SEVERE TURBULENCE ENROUTE FROM HIS LAST STOP. HINGE ATTACHED TO CO
- [SDR BAQA094210](https://openairdocs.org/sdr/BAQA094210), Apr 30, 2004: ALTIMETER. INACCURATE. UNIT INACCURATE WHEN IN FLIGHT. REPLACED WITH SERVICABLE UNIT. 04/30/2004
- [SDR BAQA094215](https://openairdocs.org/sdr/BAQA094215), Apr 30, 2004: ALTIMETER. INACCURATE. ALTIMETER UNIT INACCURATE IN FLIGHT. REPLACED WITH SERVICABLE UNIT. 05/01/2004
- [SDR BAQA094105](https://openairdocs.org/sdr/BAQA094105), Apr 27, 2004: ACTUATOR. LEAKING. ACTUATOR IS LEAKING. REPLACED WITH SERVICABLE UNIT. 04/28/2004
- [SDR BAQA093902](https://openairdocs.org/sdr/BAQA093902), Apr 19, 2004: RECEIVER. UNSERVICEABLE. RENTAL - RETURN OF RENTAL UNIT S/N 10327 IN SERVICEABLE CONDITION REPLACED WITH UNIT BACK FROM REPAIR, 04/21/2004
- [SDR BAQA094041](https://openairdocs.org/sdr/BAQA094041), Mar 23, 2004: WIRE HARNESS. DAMAGED. WIRE HARNESS HAS DAMAGED SOLDER JOINTS ON UNIT. REPLACED WITH SERVICABLE UNIT. 04/02/2004
- [SDR BAQA093894](https://openairdocs.org/sdr/BAQA093894), Mar 23, 2004: WIRE HARNESS. DAMAGED. ENGINE, PROBES DAMAGED AT SOLDER JOINT. REPLACED WITH SERVICABLE UNIT.
- [SDR BAQA093337](https://openairdocs.org/sdr/BAQA093337), Mar 1, 2004: FUEL CONTROL. INOPERATIVE. UNIT COULD NOT PASS FUEL CHECK. THIS IS ORIGINAL EQUIPMENT OFF OF THE ENGINE, TIMES DO MATCH UP TO OVERHAULS. REPLACED WITH SERVICABLE UNIT. 03/09/2004
- [SDR BAQA093775](https://openairdocs.org/sdr/BAQA093775), Feb 24, 2004: FREQ ADAPTER. CRACKED. UNITS CRACKED BEYOND LIMITS. REPLACED WITH SERVICABLE ASSET UNIT. 03/17/2004
- [SDR BAQA093101](https://openairdocs.org/sdr/BAQA093101), Feb 18, 2004: ACTUATOR. INOPERATIVE. TRIM ACTUATOR UNIT PITCH AUTO TRIM DECOUPLES. SELF TEST FAULT CODE 1. REPLACED WITH SERVICABLE UNIT. 02/23/2004
- [SDR BAQA092609](https://openairdocs.org/sdr/BAQA092609), Feb 4, 2004: START VALVE. LEAKING. START VALVE UNIT LEAKING FUEL. REPLACED WITH SERVICABLE UNIT. 02/12/2004
- [SDR BAQA092553](https://openairdocs.org/sdr/BAQA092553), Jan 21, 2004: DRAIN VALVE. STICKS. VALVE STICKS IN COLD WEATHER. UNIT WAS REMOVED AS ORIGINAL EQUIPMENT FROM ENGINE S/N 2060, AND THE ENGINE WAS INSTALLED AT ACFTT 4865.2. REPLACED WITH SERVICABL
- [SDR BAQA092251](https://openairdocs.org/sdr/BAQA092251), Jan 21, 2004: BLADE. CRACKED. TAIL ROTOR BLADE SUSPECTED TO BE CRACKED. HARDCARDS ENCLOSED. REPLACED WITH SERVICABLE UNIT. 01/27/2004
- [SDR BAQA092410](https://openairdocs.org/sdr/BAQA092410), Jan 21, 2004: SOLENOID VALVE. INOPERATIVE. UNIT INOPERATIVE. REPLACED WITH SERVICABLE UNIT. 01/27/2004
- [SDR BAQA092392](https://openairdocs.org/sdr/BAQA092392), Jan 21, 2004: START VALVE. LEAKING. START DRAIN VALVE, LEAKING. REPLACED WITH SERVICABLE UNIT. 01/27/2004
- [SDR BAQA092612](https://openairdocs.org/sdr/BAQA092612), Jan 20, 2004: FUEL CONTROL. INOPERATIVE. FUEL CONTROL PRODUCING FUEL VAPOR AFTER ENGINE SHUTS DOWN. HARDCARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 02/10/2004
- [SDR BAQA092556](https://openairdocs.org/sdr/BAQA092556), Jan 19, 2004: GENERATOR. INOPERATIVE. WARRANTY. UNIT INOPERATIVE. UNIT WAS REMOVED AS ORIGINAL EQUIPMENT FROM ENGINE S/N 2060, AND THE ENGINE WAS INSTALLED AT ACFTT 4865.2 REPLACED WITH SERVICABLE U
- [SDR BAQA092555](https://openairdocs.org/sdr/BAQA092555), Jan 19, 2004: EXCITER. INOPERATIVE. WARRANTY. UNIT INOPERATIVE. UNIT WAS REMOVED AS ORIGINAL EQUIPMENT FROM ENG. S/N 2106 AND THE ENGINE WAS INSTALLED AT ACFTT 4578.5. REPLACED WITH SERVICABLE UNI
- [SDR BAQA092554](https://openairdocs.org/sdr/BAQA092554), Jan 19, 2004: VALVE. STICKS. WARRANTY. VALVE STICKS IN COLD WEATHER. UNIT WAS REMOVED AS ORIGINAL EQUIPMENT FROM ENGINE S/N 2060, AND THE ENGINE WAS INSTALLED AT ACFTT 4865.2 REPLACED WITH 
- [SDR BAQA092473](https://openairdocs.org/sdr/BAQA092473), Jan 19, 2004: START VALVE. LEAKING. START VALVE LEAKS FUEL. UNIT WAS REMOVED AS ORIGINAL EQUIPMENT FROM ENG. S/N 2060, AND THE ENGINE WAS INSTALLED AT ACFTT 4865.2 REPLACED WITH SERVICABLE UNIT. 0
- [SDR BAQA093233](https://openairdocs.org/sdr/BAQA093233), Jan 17, 2004: SOLENOID VALVE. INOPERATIVE. NR 1 ENGINE SMOKES ON SHUT DOWN. UNIT IS ORIGINAL EQUIPMENT ON ENGINE. ENG. TSI-898.6 REPLACED WITH SERVICEABLE UNIT. 02/24/2004
- [SDR BAQA093231](https://openairdocs.org/sdr/BAQA093231), Jan 17, 2004: DRAIN VALVE. MALFUNCTIONED. NR 1 ENGINE SMOKES ON SHUT DOWN. REPLACED WITH SERVICABLE UNIT. 02/24/2004
- [SDR BAQA091933](https://openairdocs.org/sdr/BAQA091933), Jan 12, 2004: DRAIN VALVE. LEAKING. DRAIN VALVE LEAKING. REPLACED WITH SERVICABLE UNIT. 01/27/2004
- [SDR BAQA091877](https://openairdocs.org/sdr/BAQA091877), Dec 29, 2003: WIRE. SHORTED. "D" WIRE SHORTED TO "C" CONNECTOR. GENERATOR WILL NOT LOADSHARE. HARD CARD ENCLOSED. PART REPLACED WITH SERVICABLE UNIT. 01/08/2004
- [SDR BAQA091493](https://openairdocs.org/sdr/BAQA091493), Dec 17, 2003: BLADE. DAMAGED. TAIL ROTOR BLADE NEEDS PAINT REPAIR. REPLACED WITH SERVICEABLE UNITS.
- [SDR BAQA091530](https://openairdocs.org/sdr/BAQA091530), Dec 11, 2003: PROBE. BROKEN. PROBE BROKEN FROM HARNESS. RETAINING NUT ON PROBE BROKEN. REPLACED WITH SERVICEABLE UNIT.
- [SDR BAQA091532](https://openairdocs.org/sdr/BAQA091532), Dec 3, 2003: FIRE DETECTOR. FALSE INDICATION. ENGINE UNDER CONTRACT. FALSE FIRE WARNINGS OCCUR WHEN IT IS DAMP. THIS IS BEING SENT BACK UNDER A MFG WARRANTY CLAIM. REPLACED WITH SERVICEABLE UNIT. 12/16/03
- [SDR BAQA090687](https://openairdocs.org/sdr/BAQA090687), Nov 7, 2003: RADIO. INOPERATIVE. VHF RADIO DOES NOT TRANSMIT. PART INSTALLED ON 9/24/03. LASTED ONLY 71.2 HOURS. REPLACED WITH SERVICEABLE UNIT. 11/24/03
- [SDR BAQA091261](https://openairdocs.org/sdr/BAQA091261), Oct 30, 2003: BRUSHES. WORN. STARTER-GEN BRUSHES WORN BEYOND LIMITS. BEARING WORN. OVERHAULED STARTER GENERATOR. REPLACED WITH SERVICEABLE UNIT.
- [SDR BAQA090584](https://openairdocs.org/sdr/BAQA090584), Oct 30, 2003: BRUSHES. WORN. STARTER GENERATOR BRUSHES WORN BEYOND LIMITS. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 11/3/03
- [SDR BAQA089978](https://openairdocs.org/sdr/BAQA089978), Oct 17, 2003: PITCH HORN. CORRODED. PITCH HORN HAS PITS IN BOLT HOLES. REPLACED WITH SERVICEABLE UNIT.
- [SDR BAQA089834](https://openairdocs.org/sdr/BAQA089834), Oct 13, 2003: INDICATOR. CONTAMINATED. CONDENSATION IN GAUGE FACE. THIS IS A NEW AEC PART.
- [SDR BAQA089524](https://openairdocs.org/sdr/BAQA089524), Oct 4, 2003: INDICATOR. DAMAGED. ADI CAGE KNOB SPRING INOPERATIVE. REPLACED WITH SERVICEABLE UNIT.
- [SDR BAQA088356](https://openairdocs.org/sdr/BAQA088356), Oct 2, 2003: PUMP. INOPERATIVE. BOOST PUMP INOPERATIVE. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT.
- [SDR BAQA089381](https://openairdocs.org/sdr/BAQA089381), Sep 27, 2003: RADIO. WEAK. WEAK AUDIO. REPLACED WITH SERVICEABLE UNIT. 9/25/03
- [SDR BAQA089177](https://openairdocs.org/sdr/BAQA089177), Sep 25, 2003: INDICATOR. ERRATIC. TRIPLE TACH INDICATOR ERRATIC AT LOW RANGE. SPLIT AT 360/350. REPLACED WITH SERVICEABLE UNIT.
- [SDR BAQA089269](https://openairdocs.org/sdr/BAQA089269), Sep 22, 2003: WIRE. BROKEN. FIRE FAIL LIGHT WIRE BROKEN/LOCK IN BACK OF CONNECTOR BROKEN. REPLACED WITH SERVICEABLE UNIT. 9/25/03
- [SDR BAQA089304](https://openairdocs.org/sdr/BAQA089304), Sep 18, 2003: CONTROL HEAD. MALFUNCTIONED. WILL NOT HOLD FREQUENCY IN MEMORY. REPLACED WITH SERVICEABLE UNIT. 9/23/03
- [SDR BAQA091533](https://openairdocs.org/sdr/BAQA091533), Sep 16, 2003: FIRE DETECTOR. FALSE INDICATION. FALSE FIRE WARNINGS WHEN DAMP. REMOVED FROM ENGINE 12104. THIS UNIT BEING SENT BACK WITH TURBOMECA WARRANTY CLAIM FORM. REPLACED WITH SERVICEABLE UNIT. 12/16/03
- [SDR BAQA088825](https://openairdocs.org/sdr/BAQA088825), Aug 22, 2003: INVERTER. INOPERATIVE. INVERTER INOPERATIVE. REPLACED WITH SERVICEABLE UNIT.
- [SDR BAQA088676](https://openairdocs.org/sdr/BAQA088676), Aug 13, 2003: INDICATOR. FAILED. UNIT WAS SLOW TO ERECT AND LANE 2 PITCH ROLL WAS INOPERATIVE. WOULD NOT RUN AUTOPILOT LANE 2 PITCH ROLL.

All 196: https://openairdocs.org/model/aerospatiale-sa365n/reports.md

## STCs that may be installed (OpenAirDocs) (79, 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 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 SH2216NM](https://openairdocs.org/stc/SH2216NM): Installation of a Sperry Primus 500 weather radar system. Honeywell International Inc
- [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 SR04147NY](https://openairdocs.org/stc/SR04147NY): Installation of Concorde (p/n RG-365) Lead Acid battery. DECA Aviation Engineering Limited
- [STC SH7572SW](https://openairdocs.org/stc/SH7572SW): Installation of a liquid oxygen, air vacuum, and electrical EMS systems. RSG Products
- [STC SH7573SW](https://openairdocs.org/stc/SH7573SW): Installation of a secondary stretcher and attendant seat combination. 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 SR02587NY-D](https://openairdocs.org/stc/SR02587NY-D): Installation of a Medical Interior. Sikorsky Aircraft Corporation
- [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 SR00529NY](https://openairdocs.org/stc/SR00529NY): Installation of a three or four place divan and optional single seats. RSG AeroDesign LLC
- [STC SA2693NM](https://openairdocs.org/stc/SA2693NM): Installation of Electronics International digital volt/amp gauges and accessories. Electronics International Inc
- [STC SR00530NY](https://openairdocs.org/stc/SR00530NY): Installation of a cocoon wall panel system. Texas Aviation Services
- [STC SA00680SE](https://openairdocs.org/stc/SA00680SE): Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer. Electronics International
- [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 SR00811NY](https://openairdocs.org/stc/SR00811NY): Installation of Technisonic Industries Limited TFM-138 series transceiver models. Technisonic Industries Limited
- [STC SR01834NY](https://openairdocs.org/stc/SR01834NY): Installation of Globalstar Satellite Telephone System. Atlantic Avionics Inc
- [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 SH4746SW-D](https://openairdocs.org/stc/SH4746SW-D): Installation of 13-person high density interior per AHS Drawing List H365-87-2D-102 latest FAA approved revision. American Eurocopter Corporation
- [STC SH4748SW-D](https://openairdocs.org/stc/SH4748SW-D): Installation of specific interior per AHC Drawing List H365-87-2D-101 latest FAA approved revision. American Eurocopter Corporation
- [STC SH4873SW-D](https://openairdocs.org/stc/SH4873SW-D): Installation of Modular Avionics system. American Eurocopter Corporation
- [STC SH4880SW-D](https://openairdocs.org/stc/SH4880SW-D): Installation of Emergency Lighting System. American Eurocopter Corporation
- [STC SH5420SW-D](https://openairdocs.org/stc/SH5420SW-D): Installation of medical attendant seats. American Eurocopter Corporation
- [STC SH5429SW-D](https://openairdocs.org/stc/SH5429SW-D): Installation of dual defibrillator mounts. American Eurocopter Corporation
- [STC SH5486SW-D](https://openairdocs.org/stc/SH5486SW-D): Installation of dual supplemental medical oxygen system. American Eurocopter Corporation
- [STC SH5487SW-D](https://openairdocs.org/stc/SH5487SW-D): Installation of dual pivoting ltters and support cabinets. American Eurocopter Corporation
- [STC SH5488SW-D](https://openairdocs.org/stc/SH5488SW-D): Installation of stowable patient litter. American Eurocopter Corporation
- [STC SH5489SW-D](https://openairdocs.org/stc/SH5489SW-D): Installation of rear cabin medical supply cabinet. American Eurocopter Corporation
- [STC SH5490SW-D](https://openairdocs.org/stc/SH5490SW-D): Installation of side cabin medical equipment cabinets. American Eurocopter Corporation
- [STC SH5499SW-D](https://openairdocs.org/stc/SH5499SW-D): Installation of supplemental strobe light on belly panel. American Eurocopter Corporation
- [STC SH6005SW-D](https://openairdocs.org/stc/SH6005SW-D): Deletion of center cabin doors. American Eurocopter Corporation
- [STC SH6006SW-D](https://openairdocs.org/stc/SH6006SW-D): Installation of a non-heated glass windshield. American Eurocopter Corporation
- [STC SH6019SW-D](https://openairdocs.org/stc/SH6019SW-D): Installation of IFR Bendix(Generation III) avionics. American Eurocopter Corporation
- [STC SH7013SW-D](https://openairdocs.org/stc/SH7013SW-D): Removal of the aft row of fold-up seats (4 places) in the utility interior. American Eurocopter Corporation
- [STC SH7021SW-D](https://openairdocs.org/stc/SH7021SW-D): Installation of SFIM three axis VFR autopilot. American Eurocopter Corporation
- [STC SH7406SW-D](https://openairdocs.org/stc/SH7406SW-D): To move the height-velocity diagram from the limitation section of the RFM to the Performance Section. American Eurocopter Corporation
- [STC SH7709SW-D](https://openairdocs.org/stc/SH7709SW-D): Installation of Bendix/King KLN88 Loran C System for IFR use. American Eurocopter Corporation
- [STC SH7711SW-D](https://openairdocs.org/stc/SH7711SW-D): Installation of Bendix/King KNS 660 flight management system for IFR use. American Eurocopter Corporation
- [STC SH7713SW-D](https://openairdocs.org/stc/SH7713SW-D): Installation of Ground Illumination Lights. American Eurocopter Corporation

All 79: https://openairdocs.org/model/aerospatiale-sa365n/stcs.md

## The same model under other registry codes

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

- [Eurocopter SA365N](https://openairdocs.org/model/eurocopter-sa365n): 0 registered aircraft, registry code 868081A

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