Airworthiness Directive 2005-15-10

one-time
Official AD 2005-15-10 · FR doc 05-14389 · 2005-07-26 · airframe

Airworthiness Directives; The New Piper Aircraft, Inc. Models PA-34-200T, PA-34-220T, PA-44-180, and PA-44-180T Airplanes

What this AD requires

The FAA adopts an airworthiness directive (AD) to supersede AD 2003-11-14, which applies to certain The New Piper Aircraft, Inc. (Piper) Models PA-34-200T, PA-34-220T, PA-44-180, and PA-44-180T airplanes that have a model 91E92-1 or model 91E93-1 combustion heater fuel pump installed. AD 2003-11-14 currently requires you to do a one- time inspection of the combustion heater fuel pumps for fuel leakage. If leakage is found, repair or replace the fuel pump. This AD retains all the actions of AD 2003-11-14 and includes additional serial numbers for the Models PA-34-220T and PA-44-180 airplanes in the applicability section. This AD results from an investigation that concluded that after the issuance of AD 2003-11-14, additional fuel pumps that did not meet the quality control (inspection or design) requirements of the AD had been installed in Models PA-34-220T and PA-44-180 airplanes. We are issuing this AD to correct quality control problems with the heater fuel pump, which could result in failure of the heater fuel pump. Such failure could lead to fire or explosion in the cockpit.

Which aircraft AD 2005-15-10 applies to

MakesPiper
ModelsPA-34-200T, PA-34-220T, PA-44-180, PA-44-180T, PA-34, PA-44
Serial-conditional — narrows to serials 34-7570002–34-8170092, 34-8133002–3449278, 44-7995001–4496168, 44-8107001–44-8207020, 3449279–3449309, 4496169–4496190.
Part-conditional91E92-1, 91E93-1.

Applies to New Piper Aircraft, Inc. airplanes certificated in any category and equipped with a model 91E92-1 or model 91E93-1 aircraft heater fuel pump. Group 1 (PA-34-200T, PA-34-220T, PA-44-180, PA-44-180T) retained from AD 2003-11-14; Group 2 (PA-34-220T, PA-44-180) newly added serial ranges not covered by AD 2003-11-14.

Whether AD 2005-15-10 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 2005-15-10 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.