Airworthiness Directive 69-12-06
one-timeAD 69-12-06 · 1969-01-01 · airframe
Airworthiness Directives; No. 57-1040, (FAA approved revision to be issued); and (B) the tab control rods are replaced with adjustable tab control rods, Boe
Which aircraft AD 69-12-06 applies to
MakesNo 57-1040 And Tab Control Rods Are Replaced With Adjustable Tab Control Rods Boeing P N 69-60081-1 Installed Per Instructions In Aileron Tab Hinge Fitting Flanges For Cracks If Cracks Are Found Replace Hinge Fitting With A New Boeing P N 6937805-6 Before Further Flight If No Cracks Are Found Repeat 737-200 And 737- 200C
Models200C
Whether AD 69-12-06 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 69-12-06 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.