Airworthiness Directive 87-25-10

one-time
AD 87-25-10 · 1987-01-01 · airframe

Airworthiness Directives; screws, M 6 x 45 (mm), in accordance with GROB Repair Instruction No. 315-33/2 for SB TM 315-33, dated August 3, 1987. (c) Prior t

Which aircraft AD 87-25-10 applies to

MakesGrob
Part-conditional103B-4430/1.

rudder lever/stop screw replacement gated by GROB Repair Instruction No. 315-33/2 (SB TM 315-33) — confirm exact model/serial from the records

Whether AD 87-25-10 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 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 87-25-10 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.