Airworthiness Directive E9-16383

one-time
AD E9-16383 · 2009-07-15 · airframe

Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft Company) Model G36 Airplanes

What this AD requires

We are adopting a new airworthiness directive (AD) for certain Hawker Beechcraft Corporation (Type Certificate previously held by Raytheon Aircraft Company) Model G36 airplanes. This AD requires you to inspect for any improper installation and/or chafing of the P60/J60 electrical connector, associated wiring, and fuel line and, if found, correct the installation and replace damaged parts. This AD results from reports of chafing between the wire harness/connector(s) and fuel line. We are issuing this AD to detect and correct chafing between the wire harness/connector(s) and fuel line. This chafing could lead to fuel leaking into the cockpit and fire in the cockpit if wiring arcs through the fuel line.

Which aircraft AD E9-16383 applies to

MakesHawker Beechcraft Corporation
ModelsG36
Serial-conditional — narrows to serials E-3630–E-3630, E-3636–E-3817, E-3819–E-3834, E-3836–E-3887, E-3889–E-3896, E-3898–E-3898, E-3899–E-3899.

Addresses chafing between the wire harness/connector(s) and the fuel line, which could lead to fuel leaking into the cockpit and a cockpit fire.

Whether AD E9-16383 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 E9-16383 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.