Airworthiness Directive 83-09-03
one-timeAD 83-09-03 · 1983-01-01 · airframe
Airworthiness Directives; with trunnion, P/N 222-010- 154-101. (c) For main rotor trunnions, P/N 222-010-154-101, with less than 2400 hours time in service
Which aircraft AD 83-09-03 applies to
MakesWith Trunnion P N 222-010- 154-101 For Main Rotor Trunnions P N 222-010-154-101 With Less Than 2400 Hours Time In Service On Effective Date Of This Ad Retire Main Rotor Retire Mast Assembly Torquemeter Within Next 100 Hours Time In Service If It Is Utilized Exclusively With Trunnion P N 222-010- 154-101 For Main Rotor Trunnions P N 222 Supplementary Information Regulatory Text 83-09-03 Bell
Models222
Serial-conditional — narrows to serials 47006–47089.
Whether AD 83-09-03 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 83-09-03 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 →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.