Airworthiness Directive 52-07-03

one-time
AD 52-07-03 · 1952-01-01 · airframe

Airworthiness Directives; around the slots and lower strut end. (i) Refinish strut. (j) Install new forked fitting, P/N 13710 and AN 315-7R locknut. (k) Due

Which aircraft AD 52-07-03 applies to

MakesPiper Aircraft, Inc.
ModelsJ-3, J3C-40, J3C-50, J3C-50S, J3C-65S, J3F-50, J3F-50S, J3F-60, J3F-60S, J3F-65 (Army L-4D), J3F-65S, J3L, J3L-65 (Army L-4C), J3L-65S, J3L-S, J3P, PA-11, J3C-65 (Army L-4; L-4A; L-4B (Navy NE-1); L-4H; L-4J (Navy NE-2)), J3C, J3F
Part-conditional13710, AN 315-7R.

applicability read from the AD teaser — confirm exact model/serial from the records

Whether AD 52-07-03 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 52-07-03 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.