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Airworthiness Directive 88-01-01

one-time
AD 88-01-01 · 1988-01-01 · airframe

Airworthiness Directives; Washington, or at the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. This amendment bec

Which aircraft AD 88-01-01 applies to

MakesTextron Aviation Inc.
ModelsBAe.125 Series 800A, BAe.125 Series 800A (C-29A), BAe.125 Series 800A (U-125), BAe.125 Series 800B, BAe.125

Effective February 2, 1988; document examination location includes the Seattle Aircraft Certification Office. Historic manufacturer designator not present in retrieved excerpt; footer lists current type-certificate holder Textron Aviation Inc. for BAe.125 series 800 models.

Whether AD 88-01-01 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 88-01-01 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.