Airworthiness Directive 77-13-20

one-time
AD 77-13-20 · 1977-01-01 · turbine engine

Airworthiness Directives; for installation, on Hawker Siddeley Model DH/BH-125 series airplanes, certificated in all categories. Compliance is required as i

Which aircraft AD 77-13-20 applies to

MakesBristol
ModelsMK.522, MK.601-22, Viper

Applies to Bristol Viper MK.522 and MK.601-22 engines installed, or being held for installation, on Hawker Siddeley Model DH/BH-125 series airplanes, certificated in all categories; requires realigning the fuel tube for adequate clearance; effective per Amendment 39-2945.

Whether AD 77-13-20 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 77-13-20 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.