Airworthiness Directive 96-22247

recurring
AD 96-22247 · 1996-09-04 · airframe

Airworthiness Directives; Bellanca, Incorporated Models 17-30, 17-30A, 17-31, 17-31A, 17-31TC, and 17-31ATC Airplanes

What this AD requires

This amendment adopts a new airworthiness directive (AD) that applies to Bellanca, Incorporated (Bellanca) Models 17-30, 17-30A, 17- 31, 17-31A, 17-31TC, and 17-31ATC airplanes. This action requires repetitively inspecting, testing, and possibly replacing the nose landing gear (NLG) strut and brackets. A collapse of a Bellanca airplane's NLG during a landing prompted this action. The actions specified by this AD are intended to prevent possible failure of the nose landing gear, which, if not detected and corrected, could result in loss of control of the airplane during landing operations.

Repetitive inspection. Re-inspect every 50 hours. The next-due date/hours depend on this aircraft’s time in service — a records report computes it from the logbooks.

Which aircraft AD 96-22247 applies to

Part-conditional194650-0, 194383-0.

Extracted text begins at the standard 'preceding applicability provision' boilerplate; the AD's actual airplane model/serial list precedes this excerpt and was not captured by extraction. Requires nose landing gear drag strut bracket inspection/replacement (right P/N 194650-0, left P/N 194383-0) and drag strut rigging checks per Bellanca Service Letter B-107 dated September 20, 1995.

Whether AD 96-22247 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 96-22247 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 →Read the full directive (Federal Register)

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.