N332X1992 Airbus Helicopters AS332L1
Registration validUnclaimedSource: FAA, updated Oct 20, 2026
Safety record in brief:No NTSB accidents or incidents since 198245 ADs may apply2 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Valiair Ltd Co Trustee
- Owner type
- LLC
- City, state
- Casper, WY
- Certificate issued
- Jun 2, 2023
- Expires
- Jun 30, 2030
- Airworthiness
- Experimental · Research and Development, Operating Kit Built Aircraft
- Airworthiness date
- Oct 23, 2025
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Airbus Helicopters
- Model
- AS332L1
- Year
- 1992
- Serial number
- 2384
- Aircraft type
- Rotorcraft
- Category
- Land
- Certification
- Type Certificated
- Seats
- 26
- Engines
- 2
- Max takeoff weight
- 12,500 - 19,999 lb
- Type certificate data sheet
- H4EU
- Mode S code
- A39F4A
Engine
- Make and model
- Turbomeca Makila 1a1
- Type
- Turbo-shaft
- Power
- 1819 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2023 – nowValiair Ltd Co TrusteeCasper, WY · current
- Date unknownIndividual ownerdifferent airframe: Maule M-5-210c S/N 6139c
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
ADs published since 1998 that may apply (45)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2026-13-01 | Doors | Aug 3, 2026 | Airframe (AS332L1) |
| 2026-05-06 | Tail rotor system | Apr 17, 2026 | Airframe (AS332L1) |
| 2026-05-11 | Helicopter vibration analysis | Apr 17, 2026 | Airframe (AS332L1)Only with: Equipped with a dual hoist installation and de-icing system. |
| 2026-04-08 | Main Rotor Mast/Swashplate | Apr 7, 2026 | Airframe (AS332L1) |
| 2026-05-02 | Horizontal stabilizer structure | Mar 18, 2026 | Airframe (AS332L1) |
Show all 45 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2025-23-01 | Main Rotor Transmission Mount | Jan 12, 2026 | Airframe (AS332L1) |
| 2025-24-05 | Aircraft fuel filter/strainer | Jan 12, 2026 | Airframe (AS332L1)Only with: Fuel filter part number 4020P25-5 or 704A44620049 installed and original airworthiness certificate or original export certificate of airworthiness issued before February 15, 2024. |
| 2025-17-03 | Emergency Equipment | Sep 8, 2025 | Airframe (AS332L1) |
| 2025-12-06 | Time Limits/ Maintenance Checks | Jul 25, 2025 | Airframe (AS332L1) |
| 2025-07-08 | Airbus Helicopters | Apr 25, 2025 | Airframe (AS332L1) |
| 2025-03-04 | Cabin Equipment/Furnishings | Feb 19, 2025 | Airframe (AS332L1) |
| 2025-03-02 | Flight compartment equipment | Mar 7, 2025 | Airframe (AS332L1)Only with: Collective pitch handle installed on a pilot or co-pilot collective stick P/N 704A41-1100-42, -50, -56, -57, -60, -67, -68, -97, -98, -99, 704A41-1101-14, -30, or -32, as applicable to the model. |
| 2024-19-05 | Engine (Turbine/Turboprop) | Nov 26, 2024 | Engine (MAKILA 1A1) |
| 2024-18-05 | Airbus Helicopters | Nov 12, 2024 | Airframe (AS332L1) |
| 2023-20-51 | Airbus Helicopters | Oct 31, 2023 | Airframe (AS332L1) |
| 2023-01-11 | Engine (Turbine/Turboprop) | Feb 6, 2023 | Engine (MAKILA 1A1) |
| 2022-23-05 | Airbus Helicopters | Jan 3, 2023 | Airframe (AS332L1)Only with: With front upper hoist attachment fitting MP/N 332A87-1116-21, rear upper hoist attachment fitting MP/N 332A87-1117-20, or lower hoist attachment fitting MP/N 332A87-1176-20 installed. |
| 2022-18-07 | Airbus Helicopters | Oct 13, 2022 | Airframe (AS332L1) |
| 2022-08-01 | Airbus Helicopters | May 17, 2022 | Airframe (AS332L1) |
| 2021-17-17 | Airworthiness Directives; Airbus Helicopters and Airbus Helicopters Deutschland GmbH… | Nov 22, 2021 | Airframe (AS332L1)Only with: With an affected part as defined in EASA AD 2020-0064, dated March 19, 2020, installed. |
| 2021-14-07 | Cabin Equipment/Furnishings | Aug 19, 2021 | Airframe (AS332L1)Only with: AS332 models: with Breeze 300 lb electric hoist and hoist box P/N 332A67-2875-00 installed, without MOD 332PCS 78 288 (ASB 25.01.18); AS350/AS355 models: with Breeze, TRW, Lucas, or Air Equipement 300 lb hoist and hoist box P/N 350A63-1136-00 or -01 installed, without MOD 07 3190. |
| 2021-13-04 | Tail rotor head | Aug 11, 2021 | Airframe (AS332L1)Only with: Tail rotor hub assembly P/N 332A33-0001-05 or 332A33-0001-06 installed. |
| 2021-06-02 | Main Rotor Gear Box | Apr 30, 2021 | Airframe (AS332L1) |
| 2021-05-06 | Airbus Helicopters | Apr 19, 2021 | Airframe (AS332L1)Only with: With window extraction tape with snap fasteners installed. |
| 2021-03-01 | Airbus Helicopters | Apr 1, 2021 | Airframe (AS332L1) |
| 2020-23-03 | Airbus Helicopters | Jan 4, 2021 | Airframe (AS332L1)Only with: Helicopters with emergency flotation gear installed, except those with Airbus Helicopters MOD 0728456 installed. |
| 2020-23-06 | Airbus Helicopters | Dec 24, 2020 | Airframe (AS332L1)Only with: Main rotor hub assembly P/N 332A31-0001-00, -01, -02, -03, -04, -05, or -06 installed. |
| 2020-20-08 | Airbus Helicopters | Dec 11, 2020 | Airframe (AS332L1)Only with: Excludes AS332C/C1/L/L1 with MOD 07 28630, 332P087142.09 or 332P087142.12; AS332L2 with MOD 07 28630 or 332P087142.00; EC225LP with MOD 07 28370, 332A087149.00, 332A087149.03, 332P087142.00, 332P087142.03 or 332P087142.06 installed. |
| 2020-22-13 | Attitude and direction data system | Dec 8, 2020 | Airframe (AS332L1)Only with: Equipped with an Advanced Helicopter Cockpit & Avionics System (AHCAS), except helicopters with Airbus Helicopters modification 0728576 embodied in production. |
| 2020-11-02 | Airbus Helicopters | Jun 25, 2020 | Airframe (AS332L1)Only with: With a hoist arm and with right-hand side lateral sliding plug door reinforced bracket modification MOD 0726841 (also identified as MOD 07.26841) installed. |
| 2020-05-20 | Airbus Helicopters | Apr 24, 2020 | Airframe (AS332L1)Only with: Except helicopters with modification 0726383 installed. |
| 2020-05-23 | Airbus Helicopters | Apr 24, 2020 | Airframe (AS332L1)Only with: Delivered to the first owner or customer before September 1, 2018, with attachment screws P/N 330A22013520 installed with MGB RH side rear attachment fitting P/N 330A22270207 and LH side rear attachment fitting P/N 330A22270206 of the MGB suspension bars. |
| 2018-05-01 | Airbus Helicopters | Apr 5, 2018 | Airframe (AS332L1)Only with: Date of manufacture on or before July 14, 2014; for AS332 models, only with sliding cabin plug door with Airbus Helicopters modification AL25612 or 0725870 installed. |
| 2017-10-12 | Airbus Helicopters | Aug 15, 2017 | Airframe (AS332L1)Only with: Intermediate gear box (IGB) fairing P/N 332A24-0303-05XX, 332A24-0303-06XX, 332A08-1391-00, or 332A08-1391-01 installed. |
| 2016-07-29 | Airbus Helicopters (Previously Eurocopter France) Helicopters | May 16, 2016 | Airframe (AS332L1)Only with: TECALEMIT main gear box (MGB) hydraulic flexible hose installed. |
| 2015-26-01 | Airbus Helicopters | Jan 26, 2016 | Airframe (AS332L1)Only with: Helicopters with an energy absorbing seat listed in Figure 1 to paragraph (a) installed (Fischer + Entwicklungen H110, H140, H160, 185/410, 236/406; SICMA/Zodiac 192, 159; Socea Sogerma ST102, ST107, ST120). |
| 2015-18-51 | Airbus Helicopters | Oct 20, 2015 | Airframe (AS332L1)Only with: Tail rotor de-icing installation unit P/N 204ZP01Y01 and T/R blade P/N 332A12-0055-XX (any dash number) installed. |
| 2015-02-27 | Airbus Helicopters (Previously Eurocopter France) Helicopters | Feb 17, 2015 | Airframe (AS332L1)Only with: With main gearbox bevel gear vertical shaft P/N 332A32-5101-00, 332A32-5101-05, 332A32-5101-10, or 332A32-5101-15 installed. |
| 2014-10-03 | Airbus Helicopters (Type Certificate Previously Held By Eurocopter France) Helicopters | Jun 11, 2014 | Airframe (AS332L1)Certain serial numbers: AS332L1 2774; EC225LP 2600; EC225LP 2623; EC225LP 2645; EC225LP 2656; EC225LP 2659; … |
| 2014-05-08 | Airbus Helicopters (Type Certificate Previously Held by Eurocopter France) (Airbus… | Apr 15, 2014 | Airframe (AS332L1)Certain serial numbers: AS332L1 2635; AS332L1 2641; AS332L1 2644; AS332L1 9007; AS332L1 9008; AS332L1 9009 |
| 2014-05-11 | Airbus Helicopters (Type Certificate Previously Held by Eurocopter France) (Airbus… | Apr 15, 2014 | Airframe (AS332L1)Only with: Tail rotor control turnbuckle P/N 330A27-5031-20 installed. |
| 2014-05-15 | Airbus Helicopters (Type Certificate Previously Held by Eurocopter France) (Airbus… | Apr 15, 2014 | Airframe (AS332L1)Only with: Hoist beam P/N 330A87-2345-00, -01, -02, -03, -04, -05, or -06 installed with a single or double hoist plate (AS332 models) or a single hoist plate (SA330J). |
| 2008-08-16 | Turbomeca Makila 1A and 1A1 Turboshaft Engines | May 21, 2008 | Engine (MAKILA 1A1) |
| 2007-03-20 | Turbomeca S.A. Makila 1A and 1A1 Turboshaft Engines | Mar 19, 2007 | Engine (MAKILA 1A1) |
| 2000-06-11 | Turbomeca Makila 1 Series Turboshaft Engines | Jun 12, 2000 | Engine (MAKILA 1A1) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (2)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Electrical power · trans rectifier · groundedNov 8, 2024
BOTH TRANSFORMER RECTIFIERS (TRUS) WENT OFFLINE (CIRCUIT BREAKERS POPPED) DURING AN AERIAL FIREFIGHTING MISSION. THIS ACTIVATED EMERGENCY ELECTRICAL SYSTEMS AND THE PILOTS WERE ABLE TO RETURN TO THE POINT OF DEPARTURE WITHOUT FURTHER INCIDENT. UPON INSPECTION ON THE GROUND, IT WAS DETERMINED THAT…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Electrical power · tru · groundedNov 8, 2024
BOTH TRANSFORMER RECTIFIERS (TRUS) WENT OFFLINE (CIRCUIT BREAKERS POPPED) DURING AN AERIAL FIREFIGHTING MISSION. THIS ACTIVATED THE EMERGENCY ELECTRICAL SYSTEM AND THE PILOTS WERE ABLE TO RETURN TO THE POINT OF DEPARTURE WITHOUT FURTHER INCIDENT. UPON INSPECTION ON THE GROUND, IT WAS DETERMINED…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026