# Aerospatiale SA365N1

- Type: Aircraft model (FAA registry)
- Registry code: 8680603
- Manufacturer (registry): AEROSPATIALE
- Model: SA365N1
- Aircraft type: Rotorcraft
- Category: Rotorcraft
- Engines: 2 · Turbo-shaft
- Seats: 14
- 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: 1
- Page: https://openairdocs.org/model/aerospatiale-sa365n1

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 2023-11-07](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 2021-03-06](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 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 2011-16-05](https://openairdocs.org/ad/2011-16-05): Fuel switches · Airbus Helicopters SA-365N and SA-365N1. Effective Sep 12, 2011
- [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 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
- [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 88: https://openairdocs.org/model/aerospatiale-sa365n1/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)

- [N365MY](https://openairdocs.org/aircraft/N365MY): [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 6325

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (45)

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

- [SDR QMLA2015081715073](https://openairdocs.org/sdr/QMLA2015081715073), Aug 17, 2015: GEARBOX. UNSERVICEABLE. MGB WAS REPLACED DUE TO SCHEDULED OVERHAUL PERIOD COMING DUE. DURING POST MX CHECKS, HOVER & FLIGHT, OF REPLACEMENT MGB A LOW PITCH GROWLING WAS HEARD. AFTER LA
- [SDR QMLA2013070813096](https://openairdocs.org/sdr/QMLA2013070813096), Jul 8, 2013: DOOR FRAME. CRACKED. DURING SCHEDULED MX, FOUND CRACK EMERGING FROM UNDER PILOT'S DOOR UPPER STRIKER PLATE ON 14 DEGREE FRAME. REMOVED STRIKER PLATE AND FOUND 2 MORE CRACKS FROM SCR
- [SDR CA120612015](https://openairdocs.org/sdr/CA120612015), Jun 11, 2012: BEARING. FAILED. (CAN) CHECKED CHIP PLUG AFTER 1.5 HRS OPERATING TIME, DUE TO METAL FOUND ON PLUG DURING 100 HR INSPECTION, REMOVED T/R GEARBOX AND INSTALLED SPARE. CHECKED TGB 
- [SDR QMLA2011012411014](https://openairdocs.org/sdr/QMLA2011012411014), Jan 24, 2011: BLADE. CRACKED. DURING A SCHEDULED MX INSP, THE MECHANIC FOUND A CRACK IN THE UPPER SKIN OF THE MAIN ROTOR BLADE. THE BLADE IS CURRENTLY BEING SENT FOR REPAIR. A RENTAL BLADE H
- [SDR 2008FA0000314](https://openairdocs.org/sdr/2008FA0000314), May 2, 2008: LINE. BACKED OUT. ENGINE NR2 P2 LINE TO THE M5 MODULE WORKED LOOSE INFLIGHT RESULTING IN A LOSS OF OIL PRESSURE WITH THE ASSOCIATED WARNING LIGHT LOGIC. ENGINE NR2 WAS SHUTDOWN B
- [SDR 2008FA0000313](https://openairdocs.org/sdr/2008FA0000313), May 2, 2008: LINE. BACKED OUT. ENGINE NR2 P2 LINE TO THE M5 MODULE WORKED LOOSE INFLIGHT RESULTING IN A LOSS OF OIL PRESSURE WITH THE ASSOCIATED WARNING LIGHT LOGIC. ENGINE NR2 WAS SHUTDOWN B
- [SDR 2008FA0000312](https://openairdocs.org/sdr/2008FA0000312), May 2, 2008: LINE. LOOSE. ENGINE NR2 P2 LINE TO THE M5 MODULE WORKED LOOSE INFLIGHT RESULTING IN A LOSS OF OIL PRESSURE WITH THE ASSOCIATED WARNING LIGHT LOGIC. ENGINE NR2 WAS SHUTDOWN B
- [SDR 2008FA0000311](https://openairdocs.org/sdr/2008FA0000311), May 2, 2008: LINE. LOOSE. ENGINE NR2 P2 LINE TO THE M5 MODULE WORKED LOOSE INFLIGHT RESULTING IN A LOSS OF OIL PRESSURE WITH THE ASSOCIATED WARNING LIGHT LOGIC. ENGINE NR2 WAS SHUTDOWN B
- [SDR BAQA200700015](https://openairdocs.org/sdr/BAQA200700015), Jun 1, 2007: DIMMER. BURNED OUT. IN CRUISE FLIGHT MEDICAL CREW REPORTED A DIMMING OF THE CABIN FLOOD LIGHTING FOLLOWED BY AN "ELECTRICAL BURNING SMELL".
- [SDR 2005FA0001515](https://openairdocs.org/sdr/2005FA0001515), Oct 18, 2005: FLOOR PANEL. CORRODED. DURING A PRE-BUY INSPECTION, THE LONCOIN RUBBER MATS WERE PULLED UP FROM THE COCKPIT FLOORS. UNDER THE PILOTS SIDE OF THE MATS, MAJOR CORROSION ACCUMULATION WAS
- [SDR OU1R01003](https://openairdocs.org/sdr/OU1R01003), Aug 13, 2001: PRESSURE SWITCH. FAILED. AUX HYDRAULIC LIGHT ILLUMINATED INFLIGHT. AIRCRAFT MADE PRECAUTIONARY UNSCHEDULED LANDING TO VACANT PARKING LOT. CAUSED BY UNIT FAILURE.
- [SDR OLJ2001F00001](https://openairdocs.org/sdr/OLJ2001F00001), Aug 12, 2001: PRESSURE SWITCH. INOPERATIVE. AUX HYDRAULIC ILLUMINATED DURING CRUISE FLIGHT. PILOT PERFORMED A PRECAUTIONARY LANDING. MAINTENANCE WAS DISPATCHED TO THE SITE. MAINTENANCE FOUND PRESSURE SWIT
- [SDR OLJ2001F00000](https://openairdocs.org/sdr/OLJ2001F00000), Jun 14, 2001: STUD. DEPARTED. RIGHT HAND VERTICAL FIN DEPARTED AIRCRAFT DURING FLIGHT. CAUSE: FATIGUE ON ONE STUD LEADING TO FAILURE OF OTHER STUDS.
- [SDR 20010124CW008](https://openairdocs.org/sdr/20010124CW008), Jan 9, 2001: BEARING. FAILED. MANUFACTURER TEARDOWN OF GEARBOX, FOUND PITCH CHANGE SHAFT DUPLEX BEARING FAILURE AND SHAFT SHEAR T/R BLADES IN-NEG-PITCH WITH NO CONTROL OF TAIL ROTOR.NOTE: NO
- [SDR 20010130CW009](https://openairdocs.org/sdr/20010130CW009), Jan 5, 2001: GEARBOX. FAILED. INITIAL GRND RUN-UP, AFTER MJR INSP, A T/R GBX FAILURE WAS EXPERIENCED AFTER APPROX 15-20 MINUTES. AC JERKED SEVERAL TIMES ALONG THE YAW AXIS, WITH NR1 ENG RUNN
- [SDR OLJA574U001](https://openairdocs.org/sdr/OLJA574U001), Dec 19, 2000: HOSE. LEAKING. FOUND ON DAILY INSPECTION, HYDRAULIC FLUID LEAKING FROM PRESSURE LINE TO NOSE LANDING GEAR ACTUATOR. PRESSURE LINE HOSE REPLACED IN NOSE LANDING GEAR ACTUATOR.
- [SDR 20000406SH006](https://openairdocs.org/sdr/20000406SH006), Jan 28, 2000: DRAIN VALVE. LEAKING. VALVE LEAKING AROUND SPLIT LINE OF CASING. (X)
- [SDR 97ZZZX4831](https://openairdocs.org/sdr/97ZZZX4831), Oct 19, 1997: VALVE. LEAKS. DRAIN VALVE LEAKS AT SEAMS.
- [SDR 97ZZZX4809](https://openairdocs.org/sdr/97ZZZX4809), Oct 14, 1997: VALVE. LEAKS. START DRAIN VALVE UNIT LEAKS. REPAIR AS NECESSARY.
- [SDR 97ZZZX4591](https://openairdocs.org/sdr/97ZZZX4591), Oct 6, 1997: DOOR. DEPARTED. THE AIRCRAFT RETURNED WITHIN A FEW MINUTES OF ITS DEPARTURE, THE LEFT FORWARD PASSENGER DOOR HAD DEPARTED THE AIRCRAFT, IN-FLIGHT. INSPECTION REVEALED NO DEFECT
- [SDR 97ZZZX3461](https://openairdocs.org/sdr/97ZZZX3461), Jun 23, 1997: INDICATOR. MALFUNCTION. 'ERR' DISPLAYED AT ALL TIMES.
- [SDR 97ZZZX3460](https://openairdocs.org/sdr/97ZZZX3460), Jun 23, 1997: INDICATOR. FLAG STUCK. RADAR ALTIMETER FLAG 'STUCK' (WILL NOT MOVE). DOES NOT TEST.
- [SDR 97ZZZX3462](https://openairdocs.org/sdr/97ZZZX3462), Jun 20, 1997: REGULATOR. FAILED. VOLTAGE REGULATOR FAILED DUE TO CROSSED WIRING AND TERMINALS.
- [SDR 96ZZZX5164](https://openairdocs.org/sdr/96ZZZX5164), Sep 1, 1996: DECK. CRACKED. 250 MM CRACK FOUND LT SIDE TRANSMISSION DECK AT STA 3826.7. REPAIR MADE PER EUROCOPTER REPAIR DATA SHEET. MANUFACTURER ISSUED AIRFRAME SB 05.00.36. OPERATOR REC
- [SDR 96ZZZX3613](https://openairdocs.org/sdr/96ZZZX3613), May 7, 1996: INDICATOR. FAILED. ORDERED EXCHANGE UNIT, BUT UNIT DOES NOT WORK PROPERLY (LIGHT WORKS, BUT DOES NOT ILLUMINATE GAUGE FACE).
- [SDR 96ZZZX3250](https://openairdocs.org/sdr/96ZZZX3250), Apr 19, 1996: TRANSMITTER. DEFECTIVE. OUT OF CALIBRATION. AT FLIGHT IDLE (70 PERCENT NG), OIL PRESSURE INDICATING AT BOTTOM RED LINE. SWAPPED ENGINES, SAME RESULTS.
- [SDR 96ZZZX2800](https://openairdocs.org/sdr/96ZZZX2800), Mar 2, 1996: DUPLEX ACTUATOR. FAULTY. PITCH CHANNEL DISENGAGEMENT AND PITCH C5 FAULT.
- [SDR 96ZZZX2799](https://openairdocs.org/sdr/96ZZZX2799), Mar 1, 1996: ELECTROVALVE. FAILED. NR 2 ENGINE WOULD NOT HAVE T4 CLIMB UNTIL NG SHOWED 30 PERCENT, THEN RAPID RISE ONCE IGNITION OCCURRED. REPLACED START FUEL ELECTROVALVE.
- [SDR 96ZZZX2801](https://openairdocs.org/sdr/96ZZZX2801), Feb 29, 1996: DUPLEX ACTUATOR. FAILED. FAILED INSULATION TEST LOW MEG CHECK.
- [SDR 96ZZZX1018](https://openairdocs.org/sdr/96ZZZX1018), Dec 28, 1995: INDICATOR. FLUCTUATE. NR 2 ENGINE N.G. FLUCTUATING. REPLACED NG INDICATOR, SYSTEM CHECKED OK.
- [SDR 96ZZZX208](https://openairdocs.org/sdr/96ZZZX208), Dec 15, 1995: TRANSMITTER. FLUCTUATING. TRANSMITTER HAS FLUCTUATING PRESSURE.
- [SDR 96ZZZX207](https://openairdocs.org/sdr/96ZZZX207), Dec 15, 1995: TRANSMITTER. DEFECTIVE. OIL PRESSURE TRANSMITTER FLUCTUATING AND PEGGING AT 5 BARS.
- [SDR 96ZZZX206](https://openairdocs.org/sdr/96ZZZX206), Dec 13, 1995: COUPLING. CRACKED. FLEX COUPLING HAS CRACKED LAYER.
- [SDR 96ZZZX205](https://openairdocs.org/sdr/96ZZZX205), Dec 11, 1995: ENCODER. DEFECTIVE. LOOSE ITEM WITHIN, ENCODING DIGITIZER.
- [SDR 95ZZZX6968](https://openairdocs.org/sdr/95ZZZX6968), Oct 31, 1995: TRANSMITTER. FAULTY. WHEN TRANSMITTING, GOES TO TRANSMIT FOR ABOUT 2 SECONDS, THEN, SWITCHES BACK TO NO TRANSMIT.
- [SDR 95ZZZX6499](https://openairdocs.org/sdr/95ZZZX6499), Oct 6, 1995: H. E. GENERATOR. DEFECTIVE. INTERMITTENT OPERATION OF H.E. GENERATOR.
- [SDR 95ZZZX6591](https://openairdocs.org/sdr/95ZZZX6591), Jul 25, 1995: SEAL SEAT. EXCESS WEAR. SEAL SEAT HAS EXCESSIVE WEAR. RMA NR R003777. REMOVED AND REPLACED.
- [SDR 95ZZZX5734](https://openairdocs.org/sdr/95ZZZX5734), Jun 23, 1995: BEARING. BLISTERED. BLUE SPHERICAL THRUST BEARING BLISTERED. INSTALLED 2 EACH SERVICEABLE SPHERICAL THRUST BEARINGS.
- [SDR 95ZZZX5733](https://openairdocs.org/sdr/95ZZZX5733), Jun 23, 1995: BEARING. BLISTERED. BLUE SPHERICAL THRUST BEARING BLISTERED. INSTALLED 2 EACH SERVICEABLE SPHERICAL THRUST BEARINGS.
- [SDR 95ZZZX5085](https://openairdocs.org/sdr/95ZZZX5085), Jun 10, 1995: RECEIVER DRIER. FAILED. AIR CONDITIONER COMPRESSOR LOCKED UP POLLUTING SYSTEM WITH BURNED OIL. REMOVED AND REPLACED.
- [SDR 95ZZZX2079](https://openairdocs.org/sdr/95ZZZX2079), Mar 29, 1995: DETECTOR. MALFUNCTION. NR 2 ENGINE FIRE LIGHT ILLUMINATED. WHILE ENGINE WAS COLD. LIGHT WENT OUT AFTER START. TESTED DETECTOR, INITIAL READING ON TEST BENCH WAS 500 MV.
- [SDR RMXA9520576](https://openairdocs.org/sdr/RMXA9520576), Mar 26, 1995: FITTING FWD. CRACKED. CRACKED FITTING. REMOVED AND REPLACED.
- [SDR 95ZZZX2080](https://openairdocs.org/sdr/95ZZZX2080), Mar 22, 1995: ACTUATOR. DEFECTIVE. ACTUATOR CAUSES ROLL CHANNEL FAILURE. ON IN-FLIGHT TEST, BOX COMPARITOR NR 5 IN AAU LIGHT IS LIT. ACTUATOR HAS ONLY 1.1 MIL OHM RESISTANCE ON PINS 'C' AND 'D', 
- [SDR 95ZZZX2082](https://openairdocs.org/sdr/95ZZZX2082), Mar 16, 1995: BLADE. CRACKED. NR 3 LEADING EDGE EROSION GUARD CRACKED.
- [SDR 95ZZZX2081](https://openairdocs.org/sdr/95ZZZX2081), Mar 16, 1995: BLADE. CRACKED. NR 3 LEADING EDGE STRIP CRACKED.

## STCs that may be installed (OpenAirDocs) (91, 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 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 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 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 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 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 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 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 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 SH7017SW-D](https://openairdocs.org/stc/SH7017SW-D): Installation of an emergency exit window in the left side of the passenger cabin. American Eurocopter Corporation

All 91: https://openairdocs.org/model/aerospatiale-sa365n1/stcs.md

## The same model under other registry codes

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

- [Aerospatiale SA365N-1 DAUPHIN](https://openairdocs.org/model/aerospatiale-sa365n-1-dauphin): 1 registered aircraft, registry code 8680668
- [Aerospatiale SA365N-1 ECUREIL](https://openairdocs.org/model/aerospatiale-sa365n-1-ecureil): 0 registered aircraft, registry code 8680818
- [Eurocopter France SA-365N1](https://openairdocs.org/model/eurocopter-france-sa-365n1): 0 registered aircraft, registry code 8680984

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