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Airworthiness Directive 91-18-10

one-time
AD 91-18-10 · 1991-01-01 · airframe

Airworthiness Directives; program. Brake Mfr. Brake P/N Boeing P/N Max. Wear Limit Bendix 2607092-1 S160T200-12 2.15 inches Bendix 2607092-2 S160T200-13 2.1

Which aircraft AD 91-18-10 applies to

MakesBoeingBendix
Part-conditional — 2607092-1, 2607092-2, 2607092-3, S160T200-12, S160T200-13, S160T200-14.

Brake wear limit table cross-referencing Bendix brake P/Ns to Boeing P/Ns for the FAA-approved maintenance inspection program; specific Boeing model not captured in this excerpt (applicability read from the AD teaser — confirm exact model/serial from the records.)

Whether AD 91-18-10 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 91-18-10 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.

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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.