Airworthiness Directive 91-25-03 R1

one-time
AD 91-25-03 R1 · 1991-01-01 · airframe

Airworthiness Directives; 0.3 9560861-3 0.8 (b) Within 270 days after the effective date of this AD, incorporate the maximum brake wear limits specified in

Which aircraft AD 91-25-03 R1 applies to

ModelsDC-9-30, DC-9-40, DC-9-50, DC-9
Part-conditional9560861-3, B9560861, 9560861-1, 9560861-2, 9560788-7.

applicability read from the AD teaser — confirm exact model/serial from the records

Whether AD 91-25-03 R1 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 complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 91-25-03 R1 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.