Is AD 88-16-02 R1 a recurring Airworthiness Directive?

No — AD 88-16-02 R1 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 88-16-02 R1 apply to?

AD 88-16-02 R1 applies to Goodyear/Loral Systems. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 88-16-02 R1

one-time

AD 88-16-02 R1 · 1988-01-01 · appliance

Airworthiness Directives; are accomplished: 1. For Goodyear/Loral Systems part number 5000758-2, -3, and -5, the maximum brake wear limit is 1.50 inches. 2.

Which aircraft AD 88-16-02 R1 applies to

MakesGoodyear/Loral Systems

Part-conditional — 5000758-2, 5000758-3, 5000758-4, 5000758-5, 5000758-6, 5000758-10, 5003366.

Brake assembly wear limits (1.50 in for P/N 5000758-2,-3,-5) and replacement of unmodified brakes with part number 5000758-4,-6,-10 or modified units with long piston sleeves, part number 5003366.

Whether AD 88-16-02 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 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 88-16-02 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.

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.