Airworthiness Directive 87-05-51

one-time
AD 87-05-51 · 1987-01-01 · appliance

Airworthiness Directives; BOEING, MCDONNELL DOUGLAS, LOCKHEED, DEHAVILLAND, FAIRCHILD, NIHON, AND GRUMMAN Specified Models

Which aircraft AD 87-05-51 applies to

ModelsBoeing 727-100, DC-9-15, Boeing 727-200, Nihon YS-11A, Lockheed L-1011, DC-8-62, DC-8-63, Dehavilland DHC-7, DC-9-50, DC-9-80
Part-conditionalSA3688SW, SA3689SW, SA3691SW, SA3694SW, SA3695SW, SA3696SW, SA3697SW, SA3698SW.

Applies to specific serial-numbered airplanes modified under the listed STCs (SA3688SW Boeing 727-100, SA3689SW DC-9-15, SA3691SW Boeing 727-200, SA3694SW Nihon YS-11A, SA3695SW Lockheed L-1011, SA3696SW DC-8-62/-63, SA3697SW DHC-7, SA3698SW DC-9-15/-50/-80). Fairchild and Grumman models referenced in the heading are not resolved in the truncated source text. Effective May 18, 1987.

Whether AD 87-05-51 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 87-05-51 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.