Airworthiness Directive 99-11-02
recurringAirworthiness Directives; Pratt & Whitney R-1340 Series Reciprocating Engines
What this AD requires
This amendment adopts a new airworthiness directive (AD), applicable to Pratt & Whitney R-1340 series reciprocating engines, that requires initial and repetitive visual and fluorescent penetrant inspections of cylinders for head cracking. This amendment is prompted by reports of cylinder head cracking. The actions specified by this AD are intended to prevent cylinder head cracking, which can result in engine power loss, forced landing, and damage to the aircraft.
Which aircraft AD 99-11-02 applies to
Includes Wasp S1H1, S1H1-G, S1H2, S1H4, S1H5-G, S3H2, R-1340-61 under Type Certificate E-129; Wasp S3H1-G, R-1340-59 under Type Certificate E-142; and Wasp S3H1 under Type Certificate E-143. Installed on but not limited to de Havilland DHC-3, Air Tractor AT-301, and Ag Cat Corporation G-164A aircraft.
Whether AD 99-11-02 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.