Is AD 2009-25-01 a recurring Airworthiness Directive?

No — AD 2009-25-01 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2009-25-01 apply to?

AD 2009-25-01 applies to Beechcraft — models 58, 58A, 58P, 58PA, 58TC, 58TCA, 95-B55, 95-B55A. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2009-25-01

one-time

Official AD 2009-25-01 · FR doc E9-28565 · 2009-12-04 · airframe

Airworthiness Directives; Hawker Beechcraft Corporation Models 58, 58A, 58P, 58PA, 58TC, 58TCA, 95-B55, 95-B55A, A36, A36TC, B36TC, E55, E55A, F33A, and V35B Airplanes

What this AD requires

We are adopting a new airworthiness directive (AD) to supersede AD 91-18-19, which applies to certain Hawker Beechcraft Corporation (Hawker) (Type Certificate Numbers 3A15, 3A16, and A23CE formerly held by Raytheon Aircraft Company; formerly held by Beech Aircraft Corporation) Models 58, 58A, 58P, 58PA, 58TC, 58TCA, 95-B55, 95-B55A, A36, A36TC, B36TC, E55, E55A, F33A, and V35B airplanes. AD 91- 18-19 currently requires you to do a one-time inspection of the pilot and copilot shoulder harnesses for an incorrect washer and replace any incorrect washer with the correct washer. Since we issued AD 91-18-19, we have found that the applicability of AD 91-18-19 was incorrectly stated when the Model A36TC airplane was omitted from the Applicability section. Consequently, this AD would retain the actions and the serial number (SN) applicability of AD 91-18-19 and realign the SN applicability for Models A36TC and B36TC airplanes. We are issuing this AD to detect and correct an incorrect washer installed in the pilot and copilot shoulder harnesses. This incorrect part could result in a malfunctioning shoulder harness. Such a malfunction could lead to occupant injury.

Which aircraft AD 2009-25-01 applies to

MakesBeechcraft

Models58, 58A, 58P, 58PA, 58TC, 58TCA, 95-B55, 95-B55A, A36, B36TC, E55, E55A, F33A, V35B, A36TC, 33, 35, 36, 55

Serial-conditional — narrows to serials TH-733–TH-1609, TJ-3–TJ-497, TK-1–TK-151, TC-1947–TC-2456, E-825–E-2578, EA-242–EA-242, EA-273–EA-509, TE-1078–TE-1201, CE-634–CE-1536, D-9862–D-10403, EA-1–EA-241, EA-243–EA-272.

Serial ranges are per model (Group 1, retaining applicability from AD 91-18-19): 58, 58A TH-733 through TH-1609; 58P, 58PA TJ-3 through TJ-497; 58TC, 58TCA TK-1 through TK-151; 95-B55, 95-B55A TC-1947 through TC-2456; A36 E-825 through E-2578; B36TC EA-242 and EA-273 through EA-509; E55, E55A TE-1078 through TE-1201; F33A CE-634 through CE-1536; V35B D-9862 through D-10403. Group 2 (aligns certain serial numbers to Model A36TC): A36TC EA-1 through EA-241 and EA-243 through EA-272.

Whether AD 2009-25-01 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 2009-25-01 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.

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.