Is AD 99-11-10 a recurring Airworthiness Directive?

No — AD 99-11-10 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 99-11-10 apply to?

AD 99-11-10 applies to Eurocopter. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 99-11-10

one-time

Official AD 99-11-10 · FR doc 99-13321 · 1999-05-26 · appliance

Airworthiness Directives; Eurocopter France Model AS 332L2 Helicopters

What this AD requires

This amendment adopts a new airworthiness directive (AD) that is applicable to Eurocopter France Model AS 332L2 helicopters with a certain power-loss printed circuit board (PCB) installed. This action requires replacing that power-loss PCB with an airworthy power-loss PCB. This amendment is prompted by malfunctions discovered during environmental testing of the power-loss PCB conducted by the manufacturer. The actions specified in this AD are intended to prevent incorrect engine status indications, random activation of the maximum rotor revolutions-per-minute (RPM) alarm, and failure to reset the One- Engine Inoperative (OEI) logic after an actual loss of power from one engine.

Which aircraft AD 99-11-10 applies to

MakesEurocopter

Part-conditional — SE01958, 704A47720091, SE01973, 704A47720109.

Power-loss printed circuit board (PCB) replacement AD to prevent incorrect engine-status indications, spurious max-rotor-RPM alarm, and failure to reset One Engine Inoperative (OEI) logic; replace PCB P/N SE01958 (Eurocopter France P/N 704A47720091), Amendment C or D, with airworthy PCB P/N SE01973 (Eurocopter France P/N 704A47720109). Specific helicopter model is not stated in the extracted applicability text; cross-referenced to DGAC (France) AD 98-290-011(A).

Whether AD 99-11-10 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:

Method of compliance — The specific action taken (inspected, replaced, modified) and to what revision.

Date — When the work was done.

Aircraft time — Total time in service / tach at compliance — how recurring next-due is computed.

Signature & certificate — The A&P/IA who returned it to service, with certificate number.

Is AD 99-11-10 complied with on your aircraft?

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.