Airworthiness Directive 04-2782
one-timeAirworthiness Directives; Eurocopter France Model AS332C, L, and L1 Helicopters
What this AD requires
This amendment adopts a new airworthiness directive (AD) for the specified Eurocopter France (Eurocopter) model helicopters that requires inspecting the bevel gear for a crack using a borescope. This amendment is prompted by a crack that was detected on a bevel gear during a main gearbox teardown inspection. The actions specified by this AD are intended to prevent failure of the bevel gear, loss of torque to the main rotor system, and subsequent loss of control of the helicopter.
Which aircraft AD 04-2782 applies to
Applies only if main gearbox bevel gear P/N 332A32-2027-00 or 332A32-2026-00, containing bevel gears P/N 332A32-2181-00, -01, -02, -03, or -04, or 331A32-3110-07, -08, -09, or -19, is installed. Does not apply to main gearboxes overhauled after December 31, 2002; parts inspected per AS332 Letter to Repair Stations No. 183; or parts repaired per Repair Sheet (F.R.) 332A32-2181-ZA or 331A32-3110-ZA.
Whether AD 04-2782 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.
How AD compliance is recorded
A valid compliance record (14 CFR 43.9) states:
Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.
Look up a tail number →Read the full directive (Federal Register)Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.