# Aerospatiale AS332L

- Type: Aircraft model (FAA registry)
- Registry code: 8680809
- Manufacturer (registry): AEROSPATIALE
- Model: AS332L
- Aircraft type: Rotorcraft
- Category: Rotorcraft
- Engines: 2 · Turbo-shaft
- Seats: 25
- Weight class: 12,500 to 19,999 lb
- Certification: Type certificated
- Data sheet: [TCDS H4EU](https://openairdocs.org/tcds/H4EU) (OpenAirDocs)
- Holder: Airbus Helicopters
- Registered aircraft: 0
- Page: https://openairdocs.org/model/aerospatiale-as332l

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2026-13-01](https://openairdocs.org/ad/2026-13-01): Doors · Airbus Helicopters AS332C, AS332C1, AS332L and 1 more. Effective Aug 3, 2026
- [AD 2026-05-11](https://openairdocs.org/ad/2026-05-11): Helicopter vibration analysis · Airbus Helicopters AS332C, AS332C1, AS332L and 1 more. Effective Apr 17, 2026
- [AD 2026-05-06](https://openairdocs.org/ad/2026-05-06): Tail rotor system · Airbus Helicopters AS332C, AS332C1, AS332L and 2 more. Effective Apr 17, 2026
- [AD 2026-04-08](https://openairdocs.org/ad/2026-04-08): Main Rotor Mast/Swashplate · Airbus Helicopters AS332C, AS332C1, AS332L and 2 more. Effective Apr 7, 2026
- [AD 2026-05-02](https://openairdocs.org/ad/2026-05-02): Horizontal stabilizer structure · Airbus Helicopters AS332C, AS332C1, AS332L and 3 more. Effective Mar 18, 2026
- [AD 2025-24-05](https://openairdocs.org/ad/2025-24-05): Aircraft fuel filter/strainer · Airbus Helicopters AS332C, AS332C1, AS332L and 3 more. Effective Jan 12, 2026
- [AD 2025-23-01](https://openairdocs.org/ad/2025-23-01): Main Rotor Transmission Mount · Airbus Helicopters AS332C, AS332C1, AS332L and 1 more. Effective Jan 12, 2026
- [AD 2025-17-03](https://openairdocs.org/ad/2025-17-03): Emergency Equipment · Airbus Helicopters AS332L, AS332L1, AS332L2 and 1 more. Effective Sep 8, 2025
- [AD 2025-07-01](https://openairdocs.org/ad/2025-07-01): Air Data Computer · Synthetic Vision Electronic Flight Information System (Arrow STC SR09595RC or ST01523WI). Effective May 15, 2025
- [AD 2025-08-04](https://openairdocs.org/ad/2025-08-04): Time Limits/Maintenance Checks · Airbus Helicopters AS332L. Effective May 2, 2025
- [AD 2025-07-08](https://openairdocs.org/ad/2025-07-08): Tail Rotor Head · Airbus Helicopters AS332C, AS332C1, AS332L and 1 more. Effective Apr 25, 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 2024-18-05](https://openairdocs.org/ad/2024-18-05): Fuselage Main, Frame · Airbus Helicopters AS332C, AS332C1, AS332L and 2 more. Effective Nov 12, 2024
- [AD 2023-20-51](https://openairdocs.org/ad/2023-20-51): Main Rotor Mast/Swashplate · Airbus Helicopters AS332C, AS332C1, AS332L and 3 more. Effective Oct 31, 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 2023-08-06](https://openairdocs.org/ad/2023-08-06): Emergency Exits · Airbus Helicopters AS332C, AS332C1, AS332L and 3 more. Effective Jun 22, 2023
- [AD 2022-23-05](https://openairdocs.org/ad/2022-23-05): Cabin Equipment/Furnishings · Airbus Helicopters AS332C, AS332C1, AS332L and 2 more. Effective Jan 3, 2023
- [AD 2022-18-07](https://openairdocs.org/ad/2022-18-07): Miscellaneous Hardware · Airbus Helicopters AS332C, AS332C1, AS332L and 1 more. Effective Oct 13, 2022
- [AD 2022-08-01](https://openairdocs.org/ad/2022-08-01): Fuselage main, attach fittings · Airbus Helicopters AS332C, AS332C1, AS332L and 1 more. Effective May 17, 2022
- [AD 2022-05-10](https://openairdocs.org/ad/2022-05-10): Cabin Equipment/Furnishings · Airbus Helicopters AS332L, AS332L1, AS332L2 and 57 more. Effective Apr 20, 2022
- [AD 2022-01-03](https://openairdocs.org/ad/2022-01-03): Fire Bottle, Portable · Airbus Helicopters AS332C, AS332C1, AS332L and 35 more. Effective Mar 7, 2022
- [AD 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 2021-19-16](https://openairdocs.org/ad/2021-19-16): Passenger/Crew Doors · Airbus Helicopters AS332C, AS332L, AS332L1 and 3 more. Effective Oct 12, 2021
- [AD 2021-14-07](https://openairdocs.org/ad/2021-14-07): Cabin Equipment/Furnishings · Airbus Helicopters AS332C, AS332C1, AS332L and 12 more. Effective Aug 19, 2021
- [AD 2021-13-04](https://openairdocs.org/ad/2021-13-04): Tail rotor head · Airbus Helicopters AS332C, AS332C1, AS332L and 1 more. Effective Aug 11, 2021
- [AD 2021-06-02](https://openairdocs.org/ad/2021-06-02): Main Rotor Gear Box · Airbus Helicopters AS332C, AS332C1, AS332L and 1 more. Effective Apr 30, 2021
- [AD 2021-05-06](https://openairdocs.org/ad/2021-05-06): Window/Windshield System · Airbus Helicopters AS332C, AS332C1, AS332L and 6 more. Effective Apr 19, 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 2021-03-01](https://openairdocs.org/ad/2021-03-01): Tail Rotor Head, Tail Rotor Control System · Airbus Helicopters AS332C, AS332C1, AS332L and 2 more. Effective Apr 1, 2021
- [AD 2020-23-03](https://openairdocs.org/ad/2020-23-03): Emergency Flotation Section · Airbus Helicopters AS332C, AS332C1, AS332L and 3 more. Effective Jan 4, 2021
- [AD 2020-23-06](https://openairdocs.org/ad/2020-23-06): Main Rotor Mast/Swashplate · Airbus Helicopters AS332C, AS332C1, AS332L and 1 more. Effective Dec 24, 2020
- [AD 2020-20-08](https://openairdocs.org/ad/2020-20-08): Main Rotor Gearbox · Airbus Helicopters AS332C, AS332C1, AS332L and 3 more. Effective Dec 11, 2020
- [AD 2020-11-02](https://openairdocs.org/ad/2020-11-02): Doors · Airbus Helicopters AS332C, AS332C1, AS332L and 3 more. Effective Jun 25, 2020
- [AD 2020-05-23](https://openairdocs.org/ad/2020-05-23): Main Rotor Gearbox · Airbus Helicopters AS332C, AS332C1, AS332L and 1 more. Effective Apr 24, 2020
- [AD 2020-05-20](https://openairdocs.org/ad/2020-05-20): Fuel Storage · Airbus Helicopters AS332C, AS332C1, AS332L and 2 more. Effective Apr 24, 2020
- [AD 2018-05-01](https://openairdocs.org/ad/2018-05-01): Emergency Exits · Airbus Helicopters AS332C, AS332C1, AS332L and 3 more. Effective Apr 5, 2018
- [AD 2017-10-12](https://openairdocs.org/ad/2017-10-12): Aerodynamic Fairings · Airbus Helicopters AS332C, AS332C1, AS332L and 3 more. Effective Aug 15, 2017
- [AD 2016-07-29](https://openairdocs.org/ad/2016-07-29): Main Hydraulic System · Airbus Helicopters AS332C, AS332L, AS332L1 and 2 more. Effective May 16, 2016
- [AD 2015-18-51](https://openairdocs.org/ad/2015-18-51): Rotor De-Ice System · Airbus Helicopters AS332C, AS332C1, AS332L and 1 more. Effective Oct 20, 2015
- [AD 2015-02-27](https://openairdocs.org/ad/2015-02-27): Main rotor gearbox · Airbus Helicopters AS332C, AS332L, AS332L1 and 2 more. Effective Feb 17, 2015
- [AD 2014-05-15](https://openairdocs.org/ad/2014-05-15): Cabin Equipment/Furnishings · Airbus Helicopters AS332C, AS332L, AS332L1 and 2 more. Effective Apr 15, 2014
- [AD 2014-05-11](https://openairdocs.org/ad/2014-05-11): Rotorcraft Flight Control · Airbus Helicopters AS332C, AS332L, AS332L1 and 3 more. Effective Apr 15, 2014
- [AD 2014-03-02](https://openairdocs.org/ad/2014-03-02): Rotor Flight Control--Rotorcraft Servo System · Airbus Helicopters AS332C, AS332L, AS332L1 and 2 more. Effective Mar 26, 2014
- [AD 2013-24-19](https://openairdocs.org/ad/2013-24-19): Emergency Exits · Airbus Helicopters AS332C, AS332L, AS332L1 and 2 more. Effective Jan 24, 2014
- [AD 2013-22-17](https://openairdocs.org/ad/2013-22-17): Aerodynamic Fairings · Airbus Helicopters AS332C, AS332L, AS332L1 and 2 more. Effective Dec 9, 2013
- [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 2013-16-07](https://openairdocs.org/ad/2013-16-07): Tail Rotor Gearbox · Airbus Helicopters AS332C, AS332L, AS332L1 and 2 more. Effective Sep 24, 2013
- [AD 2013-08-07](https://openairdocs.org/ad/2013-08-07): Inspections of the outer skin, butt strap, and fuselage frame · Airbus Helicopters AS332C, AS332L and AS332L1. Effective May 23, 2013

Historical (superseded or no longer in force):

- [AD 2024-10-13](https://openairdocs.org/ad/2024-10-13) (historical): Aircraft fuel filter/strainer · Airbus Helicopters AS332C, AS332C1, AS332L and 3 more. Effective Aug 13, 2024
- [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 2021-16-02](https://openairdocs.org/ad/2021-16-02) (historical): Passenger/Crew Doors · Airbus Helicopters AS332C, AS332L, AS332L1 and 3 more. Effective Sep 24, 2021
- [AD 2021-05-15](https://openairdocs.org/ad/2021-05-15) (historical): Doors · Airbus Helicopters AS332C, AS332C1, AS332L and 1 more. Effective May 7, 2021
- [AD 2020-22-01](https://openairdocs.org/ad/2020-22-01) (historical): Fuselage main, attach fittings · Airbus Helicopters AS332C, AS332C1, AS332L and 1 more. Effective Dec 7, 2020
- [AD 2020-09-15](https://openairdocs.org/ad/2020-09-15) (historical): Cabin Equipment/Furnishings; Ice/Rain Protection System; Fuselage Structure (General) · Airbus Helicopters AS332C, AS332C1, AS332L and 1 more. Effective May 20, 2020
- [AD 2020-06-13](https://openairdocs.org/ad/2020-06-13) (historical): Main Rotor Gearbox · Airbus Helicopters AS332C, AS332C1, AS332L and 1 more. Effective May 11, 2020
- [AD 2019-09-03](https://openairdocs.org/ad/2019-09-03) (historical): Doors · Airbus Helicopters AS332C, AS332C1, AS332L and 1 more. Effective Jun 24, 2019
- [AD 2018-05-09](https://openairdocs.org/ad/2018-05-09) (historical): Tail Rotor Head · Airbus Helicopters AS332C, AS332C1, AS332L and 1 more. Effective Mar 26, 2018
- [AD 2017-09-05](https://openairdocs.org/ad/2017-09-05) (historical): Emergency Flotation Section · Airbus Helicopters AS332C, AS332C1, AS332L and 3 more. Effective May 26, 2017
- [AD 2013-19-19](https://openairdocs.org/ad/2013-19-19) (historical): JASC Code: 6320 Main rotor gearbox · Airbus Helicopters AS332C, AS332L, AS332L1 and 2 more. Effective Oct 16, 2013
- [AD 2003-25-01](https://openairdocs.org/ad/2003-25-01) (historical): Hoist operator control unit · Airbus Helicopters AS-350B, AS-350B1, AS-350B2 and 11 more. Effective Jan 20, 2004
- [AD 99-23-07](https://openairdocs.org/ad/99-23-07) (historical): Rotorcraft Flight Manual Atmospheric Conditions · Eurocopter France AS332C, AS332L, AS332L1 and 3 more. Effective Nov 22, 1999
- [AD 99-13-02](https://openairdocs.org/ad/99-13-02) (historical): Fuel Filter By-Pass Valve · Eurocopter France AS332C, AS332L, AS332L1 and 1 more. Effective Jul 2, 1999
- [AD 98-06-04](https://openairdocs.org/ad/98-06-04) (historical): Tail Rotor Gearboxes · Eurocopter France AS332C, AS332L, AS332L1 and 3 more. Effective Jul 13, 1998

All 114: https://openairdocs.org/model/aerospatiale-as332l/ads.md

## 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 NYC96LA143](https://openairdocs.org/ntsb/NYC96LA143), Jul 5, 1996: Aerospatiale AS-332L (N25AN), Lakewood, NJ, substantial damage. Probable cause: a number two system module hydraulic oil leak, which was ignited by an undetermined source and resulted in a hydraulic fluid fire.

## FAA accident and incident reports (1)

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 19960705016349A](https://openairdocs.org/incident/19960705016349A), Jul 5, 1996: Snias AS332L (N25AN), Lakewood, NJ, Substantial damage. Aircraft taxiing when smelled smoke, pilot pulled bottles, did not extinguish fire, rescue responded, put out fire.

## Service difficulty reports (62, newest 50)

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

- [SDR 9EKA2015060322](https://openairdocs.org/sdr/9EKA2015060322), May 29, 2015: STRUCTURE. CRACKED. FOUND CRACKED STABILIZER AT INBD LOCATION. CRACK IS 2 INCHES IN LENGTH, CRACKED THROUGH MATERIAL.
- [SDR 9EKA2015050416](https://openairdocs.org/sdr/9EKA2015050416), May 1, 2015: PIPE. LOOSE. LEFT HYD LOW LEVEL LIGHTS CAME ON IN FLIGHT. LT SERVO TOP PIPE LEAKING. LT SERVO TOP PIPE WAS TIGHTENED & NO FURTHER LEAKS DETECTED. NO LIGHTS AFTER RESERVOIR W
- [SDR 9EKA2015042915](https://openairdocs.org/sdr/9EKA2015042915), Apr 17, 2015: FCU. FAULTY. UPON LANDING DIFF NG LIGHT ILLUMINATED ALONG WITH A NG T4 DROP ON ENG 2 FOLLOWED BY AN NR OVER SPEED ALARM & HIGH NG ON ENG 1 & HIGH NR RPM. PILOT REDUCED THROT
- [SDR 9EKA20150303010](https://openairdocs.org/sdr/9EKA20150303010), Mar 3, 2015: FCU. FAILED. DURING FLIGHT, NG SPLIT OF 2000 BETWEEN ENGS.
- [SDR 9EKA20150218009](https://openairdocs.org/sdr/9EKA20150218009), Feb 18, 2015: FIREWALL. CRACKED. ON A SCHEDULED INSPECTION, NR 2 ENG TO MGB FIREWALL FEED THROUGH FOUND CRACKED.
- [SDR 9EKA02022015008](https://openairdocs.org/sdr/9EKA02022015008), Feb 2, 2015: FIREWALL. CRACKED. ON A SCHEDULED INSPECTION, NR 1 ENG TO MGB FIREWALL FEED THROUGH FOUND CRACKED.
- [SDR 9EKA20140525006](https://openairdocs.org/sdr/9EKA20140525006), May 24, 2014: LOGIC CARD. DIRTY. LANDING GEAR SELECTED TO RETRACT. RETRACTED TO THE KNEELING POSITION ONLY. RECYCLE LG SWITCH WHICH DID A PROPER RETRACT & THEN DOWN & LOCKED POSITION. MISSION W
- [SDR CA110112007](https://openairdocs.org/sdr/CA110112007), Jan 9, 2011: WINDSCREEN. CRACKED. INFLIGHT CRACKING OF OUTER LAYER. RETURN TO BASE.
- [SDR CA110105006](https://openairdocs.org/sdr/CA110105006), Dec 9, 2010: LOGIC CARD. FAILED. (CAN) GEAR WAS SELECTED FOR RETRACTION AFTER T/O. AMBER GEAR TRANSIT LIGHT REMAINED ON. EMERGENCY CHECK LIST CONSULTED. GEAR SELECTED DOWN W/NO CHANGE, TRANSIT 
- [SDR CA110105008](https://openairdocs.org/sdr/CA110105008), Dec 7, 2010: PHASE RELAY. FAILED. (CAN) BEFORE TAXIING, THE INLET ANTI ICE WAS TURNED ON, BUT SHOWED THE DEICE LIGHT ON THE 32 ALPHA PANEL AND COULD NOT BE RESET WITH MULTIPLE TRIES AND ENGINE S
- [SDR CA090522005](https://openairdocs.org/sdr/CA090522005), May 19, 2009: SPACER. FAILED. (CAN) DURING ROUTINE 500 HR INSP AND AFTER THE REMOVAL OF THE FREQUENCY ADAPTORS, THE FLAPPING HINGE PIN SPACER THAT MATES AGAINST THE FREQUENCY ADAPTER SPHERIC
- [SDR CA080513007](https://openairdocs.org/sdr/CA080513007), May 6, 2008: TRANSMISSION. MAKING METAL. (CAN) TRANSMISSION CHIP LIGHT ILLUMINATION. FERROUS METAL CHIPS, WHISKERS AND FLAKES FOUND IN FILTER AND SUMP AND ON CHIP DETECTOR.
- [SDR CA070427001](https://openairdocs.org/sdr/CA070427001), Apr 16, 2007: DOOR. SEPARATED. (CAN) AFTER TAKING OFF FROM AN OFFSHORE RIG AT 300 FT, 70 KNOTS, CREW HEARD A STRONG NOISE AND ONE OF THE PASSENGERS ADVISED THAT DOOR WAS MISSING. P/C NOTICED 
- [SDR CA060419006](https://openairdocs.org/sdr/CA060419006), Apr 18, 2006: TIE BOLT. SHEARED. (CAN) A/C RETURNED FROM AN OFFSHORE TRIP, MAINTENANCE PERSONNEL WERE CARRYING OUT THE TURN AROUND CHECKS AND FOUND THAT ONE OF THE 3 ENGINE TIE BOLTS WAS ONLY H
- [SDR CA060315001](https://openairdocs.org/sdr/CA060315001), Mar 14, 2006: BRACKET. CRACKED. DURING A ROUTINE DAILY INSPECTION, TWO MAIN ROTOR DEICE BRACKET WERE FOUND TO HAVE CRACKS IN THE SAME AREA. THESE BRACKETS WERE REPLACED AND THE A/C RETURNED TO
- [SDR CA060127007](https://openairdocs.org/sdr/CA060127007), Jan 27, 2006: WIRE HARNESS. WORN. (CAN) A/C RETURNED FROM AN OFFSHORE TRIP, THE MAINTENANCE STAFF WERE CARRING OUT A ROUTINE TURN AROUND CHECK AND FOUND THE M/R DEICE HARNESS BROKEN AT THE CONNE
- [SDR CA051123003](https://openairdocs.org/sdr/CA051123003), Nov 22, 2005: BUSHING. CRACKED. DURING THE DAILY INSPECTION, IT WAS NOTICED BLACK T/R BLADE FLAPPING HINGE HADE A LITTLE MORE RESISTANCE, (SIDE TO SIDE MOTION) THAN THE OTHER BLADES. AFTER FUR
- [SDR CA051017013](https://openairdocs.org/sdr/CA051017013), Oct 16, 2005: COUPLING. DAMAGED. AFTER LAST FLIGHT OF THE DAY, ENGINEERING REVIEWED THE HUMS DATA AND NOTICED A SPIKE IN THE SHAFT INFORMATION. THE A/C ENGINE WAS REMOVED THE SHAFT REMOVED FROM
- [SDR CA050719003](https://openairdocs.org/sdr/CA050719003), Jul 2, 2005: BRACKET. CRACKED. (CAN) THE DEICE EQUIPMENT WAS BEING REMOVED FOR THE SUMMER SEASON,WHEN THIS CRACK WAS DISCOVERED. NO PREVIOUS EVIDENCE WAS DISCOVERED CONCERNING THIS PART.THIS 
- [SDR ERAA098198](https://openairdocs.org/sdr/ERAA098198), Sep 14, 2004: BATTERY. LEAKING. THIS INFO FOR FAA SDR. BATTERY LEAKED, MOISTURE DAMAGE, G SWITCH STICKS. ACTION TAKEN: PERFORMED PRELIMINARY INSPECTION AT ARTEX 9/27/2004 AND REPAIRES.
- [SDR ERAA097502](https://openairdocs.org/sdr/ERAA097502), Sep 13, 2004: G SWITCH. INOPERATIVE. THIS INFO FOR FAA SDR. FOUND G SWITCH TO BE NOPERABLE. CORROSION ON FRONT SIDE OF UNIT. ACTION TAKEN: SENT UNIT TO MANUFACTURER FOR REPAIR.
- [SDR ERAA097539](https://openairdocs.org/sdr/ERAA097539), Aug 10, 2004: G SWITCH. DEFECTIVE. THIS INFO FOR FAA SDR. ELT SENT TO ARTEX FOR INSPECTION BATTERY HAS LOW VOLTAGE G SWITCH IS STUCK ACTION TAKEN: REPLACED G SWITCH, SUB ASSY INCORRECT PART INSTA
- [SDR ERAA097091](https://openairdocs.org/sdr/ERAA097091), Jul 19, 2004: CIRCUIT BOARD. MALFUNCTIONED. LANDING GEAR CONTROL HAS NO CONTROL POWER, SHOWING MANUAL EXTENSION LIGHT ACTION TAKEN: UNIT INSPECTED, CAPACITOR C68 UNSERVICEABLE, HEAT DAMAGE EVIDENT ON PCB.
- [SDR CA040603002](https://openairdocs.org/sdr/CA040603002), Jun 2, 2004: BOLT. FRACTURED. (CAN) AFTER LAST FLIGHT, DAILY INSPECTION WAS BEING CARRIED OUT ON THE AIRCRAFT, WHEN THE NR 1 ENG LT UPPER TIE BOLT WAS FOUND TO BE FRACTURED. THE OTHER TWO TI
- [SDR CA040504001](https://openairdocs.org/sdr/CA040504001), Apr 30, 2004: ADJUSTER. CRACKED. (CAN) AIRCRAFT REPORTED PEDAL ADJUSTER JAMMED, AFTER INSPECTION THE SUPPORT WAS FOUND TO BE CRACKED. AIRCRAFT IS IN NORWAY FOR A G-CHECK INSPECTION AND WAS ALSO
- [SDR AUS20040315](https://openairdocs.org/sdr/AUS20040315), Apr 29, 2004: NUT. MISMANUFACTURED. (AUS) NR 1 ENGINE OUTPUT DRIVESHAFT TO OUTPUT FLANGE ATTACHMENT NUTS FAULTY. MATING SURFACE OF NUTS MISALIGNED. NUTS ARE PART OF BOLT SET PN 332BF6. SUSPECT MAN
- [SDR CA040202015](https://openairdocs.org/sdr/CA040202015), Jan 30, 2004: TIE ROD. SHEARED. (CAN) ONE OF THE THREE BOLTS ATTACHING THE ENGINE TO THE MAIN GEARBOX WAS DISCOVERED SHEARED DURING A TURN AROUND CHECK. THE BOLT WAS SHEARED ABOUT MIDWAY IN TH
- [SDR AUS20030952](https://openairdocs.org/sdr/AUS20030952), Sep 12, 2003: ENGINE. MAKING METAL. (AUS) NR 1 ENGINE REAR BEARING CHIP DETECTOR CONTAMINATED WITH METAL.
- [SDR AUS20030871](https://openairdocs.org/sdr/AUS20030871), Aug 29, 2003: BEARING. BROKEN. (AUS) TAIL ROTOR GEARBOX PITCH CHANGE BEARING FAILED. PITCH CHANGESHAFT SERVO END NUT AND LOCKWASHER MISSING. SUSPECT FAILURE OF BEARING DUE TO CONTAMINATION BY
- [SDR AUS20030357](https://openairdocs.org/sdr/AUS20030357), Mar 20, 2003: WIRE HARNESS. FAULTY. (AUS) NR 1 ENGINE NH HARNESS INTERNAL FAULT (OPEN CIRCUIT).
- [SDR AUS20020711](https://openairdocs.org/sdr/AUS20020711), Jul 10, 2002: CONTROL CABLE. FRAYED. (AUS) LT REAR TAIL ROTOR CONTROL CABLE CONTAINED BROKEN STRANDS IN AN AREA WHERE THE CABLE PASSES THROUGH FAIRLEAD. FAIRLEAD INSPECTED AND FOUND SERVICEABLE.
- [SDR CA020125007](https://openairdocs.org/sdr/CA020125007), Jan 25, 2002: ADJUSTER. CRACKED. (CAN) PEDAL ADJUSTER LOCATION PIN SUPPORT CRACKED CAUSING THE PEDAL ADJUSTER LEVER TO BE UNMOVEABLE AND THE PEDALS UNADJUSTABLE.
- [SDR AUS20020004](https://openairdocs.org/sdr/AUS20020004), Jan 2, 2002: RIB. CRACKED. (AUS) HORIZONTAL STABILISER ROOT RIB ASSEMBLY CRACKED BEYOND LIMITS.
- [SDR AUS20011292](https://openairdocs.org/sdr/AUS20011292), Nov 30, 2001: BLADE. CRACKED. (AUS) BLUE MAIN ROTOR BLADE CRACKED AT THE ROOT END TRAILING EDGE.
- [SDR CA011210001](https://openairdocs.org/sdr/CA011210001), Nov 27, 2001: PANEL. INOPERATIVE. (CAN) PRESSURE REFUELING CONTROL PANEL WILL NOT PERMIT SINGLE POINT REFUELING TO BE CARRIED OUT.
- [SDR AUS20011267](https://openairdocs.org/sdr/AUS20011267), Nov 23, 2001: ACTUATOR. LEAKING. (AUS) RT MAIN LANDING GEAR ACTUATOR HYDRAULIC UNIT FAULTY.
- [SDR AUS20011001](https://openairdocs.org/sdr/AUS20011001), Sep 7, 2001: ENGINE. MALFUNCTIONED. (AUS) NR 1 ENGINE AUTOMATICALLY REDUCED POWER TO IDLE. INVESTIGATION COULD FIND NO FAULTS. ENGINE WAS GROUND RUN AND TEST FLOWN WITH ALL SYSTEMS OPERATING CORRE
- [SDR AU010124](https://openairdocs.org/sdr/AU010124), Feb 6, 2001: FUEL CONTROL. FAULTY. (AUS) NR 2 ENGINE FUEL CONTROL UNIT FAULTY.
- [SDR AU010140](https://openairdocs.org/sdr/AU010140), Jan 19, 2001: STRUCTURE. CRACKED. (AUS) TAIL BOOM CRACKED IN AREA OF PYLON DECK.
- [SDR AU010226](https://openairdocs.org/sdr/AU010226), Jan 13, 2001: STATOR. CRACKED. (AUS) ENGINE FIRST STAGE TURBINE NOZZLE GUIDE VANE INNER RING CRACKED.CRACK RAN FOR APPROXIMATELY 270 DEGREES OF CIRCUMFERENCE.
- [SDR AU010009](https://openairdocs.org/sdr/AU010009), Jan 4, 2001: FUEL CONTROL. MALFUNCTIONED. (AUS) NR 1 ENGINE FUEL CONTROL UNIT FAULTY. INVESTIGATION FOUND THE PPNG OF THE FCU INTERNAL CIRCUIT TO BE OPEN CIRCUITED.
- [SDR AU001245](https://openairdocs.org/sdr/AU001245), Dec 28, 2000: SMOKE DETECTOR. FAULTY. (AUS) BAGGAGE BAY SMOKE DETECTOR FAULTY. HEATER HOT AIR VALVE STUCK INOPEN'' POSITION.
- [SDR AU001182](https://openairdocs.org/sdr/AU001182), Dec 9, 2000: LANDING GEAR. FAILED. (AUS) LANDING GEAR WOULD NOT EXTEND. THE GEAR WAS EXTENDED USING THEEMERGENCY SYSTEM. INVESTIGATION COULD FIND NO FAULTS BUT THELANDING GEAR CONTROL PRINTED CIR
- [SDR AU001181](https://openairdocs.org/sdr/AU001181), Dec 9, 2000: WARNING SYSTEM. FAULTY. (AUS) LANDING GEAR WARNING LIGHTS ILLUMINATED DURING DESCENT. THE LANDING GEAR WAS CONFIRMED DOWN. INVESTIGATION OF THE WARNING SYSTEM COULD FIND NO FAULTS. AIR
- [SDR AU001180](https://openairdocs.org/sdr/AU001180), Dec 8, 2000: TRANSMISSION. MAKING METAL. (AUS) MAIN TRANSMISSION MAGNETIC PLUG AND OIL FILTER CONTAMINATED WITHMETAL.
- [SDR AU000302](https://openairdocs.org/sdr/AU000302), Apr 16, 2000: CONNECTOR. SHORTED. (AUS) MAIN TRANSMISSION CHIP DETECTOR CONNECTOR SHORT CIRCUITED ON THE CHIP DETECTOR ACCESS COVER GIVING FALSE INDICATIONS.
- [SDR AU000303](https://openairdocs.org/sdr/AU000303), Apr 14, 2000: HARNESS. FAULTY. (AUS) NR 1 ENGINE N1 HARNESS FAULTY.
- [SDR AU000114](https://openairdocs.org/sdr/AU000114), Apr 13, 2000: TRANSMISSION. CONTAMINATED. (AUS) MAIN TRANSMISSION MAGNETIC PLUG AND OIL FILTER CONTAMINATED WITH METAL.
- [SDR AU000138](https://openairdocs.org/sdr/AU000138), Feb 27, 2000: TRANSMISSION. CONTAMINATED. (AUS) MAIN ROTOR GEARBOX CHIP DETECTOR METAL CONTAMINATION. THERE WAS NO METAL IN THE OIL FILTER. INVESTIGATION FOUND THE CONTAMINATION TO BE WITHIN LIMITS AND 
- [SDR AU000100](https://openairdocs.org/sdr/AU000100), Feb 10, 2000: WINDSHIELD. CRACKED. (AUS) RIGHT HEATED WINDSHIELD CRACKED WITH A BURNING SMELL COMING FROM THE BASE OF THE WINDSHIELD. INVESTIGATION FOUND THAT THE RESISTORS IN THE WINDSHIELD WERE

All 62: https://openairdocs.org/model/aerospatiale-as332l/reports.md

## STCs that may be installed (OpenAirDocs) (64, 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 SR02592AK](https://openairdocs.org/stc/SR02592AK): Installation of Precision Support System PSS-AS332SP Sling Pole. Precision Support Services, LLC
- [STC SR12023AK](https://openairdocs.org/stc/SR12023AK): Installation of Precision Support System PC-A-2550-0001 Cargo Net. Precision Support Services LLC
- [STC SR01099DE](https://openairdocs.org/stc/SR01099DE): Installation of the GPMS Foresight MX Condition Monitoring System. GPMS International Inc
- [STC SR12402IB](https://openairdocs.org/stc/SR12402IB): Manufacture and installation of Heli-One Heated / Motorized Mirror. Heli-One
- [STC SR04509CH](https://openairdocs.org/stc/SR04509CH): Installation of a Helitak FT4250 Super Puma Fire Tank Liquid Dispensing System. Helitak USA, LLC
- [STC SR12132DE](https://openairdocs.org/stc/SR12132DE): Installation of Pilot and Co-Pilot Bubble Doors. Precision Support Services, LLC
- [STC SR02512SE](https://openairdocs.org/stc/SR02512SE): Installation of a Supplemental Lighting System; manufactured and installed. Aviation Specialties Unlimited Inc
- [STC SR03395CH](https://openairdocs.org/stc/SR03395CH): Installation of Mechanical Specialties Model 6111 Cargo Hook. Precision Support Services LLC
- [STC SR12072IB](https://openairdocs.org/stc/SR12072IB): Manufacturing and Installation of Cargo Hold Nets; Maintenance must be in accordance with ICARUS Aero Inc. Instructions for Continued Airworthiness as shown on the attached FAA AML No. SR12072IB. Icarus Aero Inc
- [STC SR02584AK](https://openairdocs.org/stc/SR02584AK): Installation of Recoil Aerospace, Inc. T1000-E or T650-E Fire Suppression Tank. Recoil Aerospace Inc
- [STC SR11833IB](https://openairdocs.org/stc/SR11833IB): Installation of Garmin GTX Transponder System. Heli Austria GmbH
- [STC SR11806IB](https://openairdocs.org/stc/SR11806IB): Modified Upper Boom and Gimbal Joint Assemblies. Coldstream Helicopters Ltd
- [STC SR02828LA](https://openairdocs.org/stc/SR02828LA): Installation of Precision Support Services' Dual Mission System (DMS). Precision Support Services LLC
- [STC SR04502CH](https://openairdocs.org/stc/SR04502CH): Installation of Heli-Preheat Kit, p/n TA3306-1 for 115 volt application in accordance with Heli-Preheat Kit drawing TA3306-1 Revision C, dated December 11, 2023 or later FAA approved revisions and Installation Instruction document # TNH3306 Revision C, dated September 30, 2021 or later FAA approved revisions. HARTZELL PROPELLER LLC
- [STC SR02473AK](https://openairdocs.org/stc/SR02473AK): Installation of the L-3 Communications NGT-9000R/RD and NGT-9000/D ADS-B IN/OUT system. StandardAero Atlantic USA Inc
- [STC SH3319NM](https://openairdocs.org/stc/SH3319NM): Installation of Precise Flight Pulselite Control Unit in the Landing /Taxi Recognition Visual Control Light system,. Precise Flight Inc
- [STC SR02089SE](https://openairdocs.org/stc/SR02089SE): Installation of the Nine Passenger configuration. Precision Support Services LLC
- [STC SR09930AC](https://openairdocs.org/stc/SR09930AC): Installation Rear-View Mirror. Aero-Seats and Systems Inc
- [STC SR04436NY](https://openairdocs.org/stc/SR04436NY): Installation of VIH Aerospace (VIHA) Cockpit Door Bubble Window. VIH Aerospace Inc
- [STC SR04674NY](https://openairdocs.org/stc/SR04674NY): Installation of Coldstream Helicopters LH and RH Vertical Reference Windows. Coldstream Helicopters Ltd
- [STC SH4904NM](https://openairdocs.org/stc/SH4904NM): Fabrication, installation, and inspection of onboard systems model E-53 cargo hook load cell system. Onboard Systems
- [STC SR02588LA](https://openairdocs.org/stc/SR02588LA): Replacement of existing SAFT main Battery models 40208-1, 40208-5, 4308-1 or 4308-1 with Concorde Battery Corporation Valve Regulated Lead Acid (VRLA) Battery models RG-332-1 or RG-332-2. Concorde Battery Corporation
- [STC SR09911AC](https://openairdocs.org/stc/SR09911AC): Installation of alternate hoist cable. Breeze Eastern 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 SR04435NY](https://openairdocs.org/stc/SR04435NY): Installation of the Soft Shell Interior Kit. Heli-One
- [STC SR04428NY](https://openairdocs.org/stc/SR04428NY): Installation of new sponson on main landing gear. TPS AEROSPACE ENGINEERING S.r.l
- [STC SR269CH](https://openairdocs.org/stc/SR269CH): Install air ambulance unit. Spectrum Aeromed LLC dba Spectrum Aeromed
- [STC SH933NE](https://openairdocs.org/stc/SH933NE): Installation of vertical reference doors. Heli-One
- [STC SR00826DE](https://openairdocs.org/stc/SR00826DE): Installation of Honeywell Sky Connect Tracker III system. Cert Works LLC
- [STC SR03838NY](https://openairdocs.org/stc/SR03838NY): Installation of the Soft Shell Interior Kit in accordance with CHT Aerospace Inc. CHT Aerospace Inc
- [STC SR03786NY](https://openairdocs.org/stc/SR03786NY): Installation of Heli-One (Norway) AS's Cockpit Voice Flight Data Recorder Installation. Heli-One (Norway) AS
- [STC SR02399AK](https://openairdocs.org/stc/SR02399AK): Installation of dual Garmin GNS530W/430W system, including Helicopter Terrain Awareness and Warning System (HTAWS) functionality. Vector Aerospace Helicopter Services USA Inc
- [STC SR02159AK](https://openairdocs.org/stc/SR02159AK): Installation of AlliedSignal, Inc., GNS-XLS Flight Management system as a primary means of navigation for oceanic/remote operations. Apical Industries, Inc. dba Dart Aerospace
- [STC SR02415AK](https://openairdocs.org/stc/SR02415AK): Installation of cockpit voice and data recorder system. Vector Aerospace Helicopter Services USA Inc
- [STC SR00631DE-D](https://openairdocs.org/stc/SR00631DE-D): Installation of an AKV, Inc. Dual Engine Cycle Counter. AKV Inc
- [STC SR02405AK](https://openairdocs.org/stc/SR02405AK): Installation of Night Vision Goggle (NVG) Compatible Lighting System. Vector Aerospace Helicopter Services USA Inc
- [STC SR03146NY](https://openairdocs.org/stc/SR03146NY): Installation of Technisonic TDFM-7300 Transceiver with RC-7300 Remote Control. Heli-One
- [STC SR03137NY](https://openairdocs.org/stc/SR03137NY): Installation of a Universal Avionics UNS-1Fw Flight Management Systems. Heli-One
- [STC SR03155NY](https://openairdocs.org/stc/SR03155NY): Installation of an Artex C406-N HM ELT System. Heli-One
- [STC SR03142NY](https://openairdocs.org/stc/SR03142NY): Installation of an Enhanced Ground Proximity Warning System. Heli-One
- [STC SR03144NY](https://openairdocs.org/stc/SR03144NY): Installation of an AXSYS V9 Camera and Moving Map System. Heli-One
- [STC SR03145NY](https://openairdocs.org/stc/SR03145NY): Installation of a Tactical Direction Finder. Heli-One
- [STC SR03139NY](https://openairdocs.org/stc/SR03139NY): Installation of a Technisonic Inter Communication System (ICS). Heli-One
- [STC SR03140NY](https://openairdocs.org/stc/SR03140NY): Installation of a Goodrich Electric Hoist P/N 44311-10-7. Heli-One
- [STC SR03110NY](https://openairdocs.org/stc/SR03110NY): Installation of Sky Trac ISAT-200 Flight Following System. Heli-One
- [STC SR00244BO](https://openairdocs.org/stc/SR00244BO): Installation of BAE Systems AN/ALQ-144B(V)2 IRCM System. BAE SYSTEMS Information and Electronic Systems Integration Inc
- [STC SR02393AK](https://openairdocs.org/stc/SR02393AK): Installation of a SkyTrac ISAT Model 100 or Model 200, Flight Following Satellite Communication System. Vector Aerospace Helicopter Services USA Inc
- [STC SR01343LA](https://openairdocs.org/stc/SR01343LA): Installation of MASS Systems fire extinguisher cartridges as replacements for W. Kidde Aerospace/L Hotellier/Dexaero fire extinguisher cartridges in fire extinguisher bottles installed in the rotorcraft models noted on the FAA Approved Model List SR01343LA dated June 28, 2002, or later FAA approved revisions. This cartridge is in accordance with MASS Systems Master Drawing List MDL-861345, Revision N/C, dated May 31, 2002, or later FAA approved revisions. AMETEK AMERON LLC d/b/a MASS Systems
- [STC SR01344LA](https://openairdocs.org/stc/SR01344LA): Installation of MASS Systems fire extinguisher cartridges as replacements for W. Kidde Aerospace/L Hotellier/Dexaero fire extinguisher cartridges in fire extinguisher bottles installed in the rotorcraft models noted on the FAA Approved Model List SR01344LA dated June 28, 2002, or later FAA approved revisions. This cartridge is in accordance with MASS Systems Master Drawing List MDL-861355, Revision N/C, dated May 31, 2002, or later FAA approved revisions. AMETEK AMERON LLC d/b/a MASS Systems
- [STC SR01074SE](https://openairdocs.org/stc/SR01074SE): Fabrication of Simplex Model 316 Fire Attack System per Simplex Master Drawing List No. MDL 316, Revision D, dated December 14, 2001, or later FAA approved revision; and installation of this system in accordance with Simplex Installation Instructions, Document No. 316-102 002-001, Revision B, dated January 8, 2002, or later FAA approved revision. Simplex Manufacturing Company

All 64: https://openairdocs.org/model/aerospatiale-as332l/stcs.md

## The same model under other registry codes

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

- [Eurocopter AS332L](https://openairdocs.org/model/eurocopter-as332l): 0 registered aircraft, registry code 868098A

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