These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
The New Piper Aircraft, Inc. Models PA-34-200T, PA-34-220T, PA-44-180, and PA-44-180T…
Aug 26, 2005
Airframe (PA-34-200T)Certain serial numbers: PA-34-200T 34-7570002–34-8170092; PA-34-220T 34-8133002–3449278; PA-44-180 44-7995001–4496168; PA-44-180T 44-8107001–44-8207020; PA-34-220T 3449279–3449309; PA-44-180 4496169–4496190. Only with: Equipped with a model 91E92-1 or 91E93-1 aircraft heater fuel pump.
The New Piper Aircraft, Inc. PA-24, PA- 28R, PA-30, PA-32R, PA-34, and PA-39 Series…
Dec 8, 1998
Airframe (PA-34-200T)Certain serial numbers: PA-28R-180 28R-30002–28R-31135; PA-28R-180 28R-7130001–28R-7130013; PA-28R-200 28R-35001–28R-35820; PA-28R-200 28R-7135001–28R-7635539; PA-28R-201 28R-7737002–28R-7737096; PA-28R-201T 28R-7703001–28R-7703239; …. Only with: All serials of PA-24, PA-24-250, PA-24-260, PA-24-400, PA-30, PA-39; PA-28R, PA-32R, PA-34 models (all serials of PA-34-200) only if not equipped with Piper P/N 78717-02 (or FAA-approved equivalent) main gear sidebrace stud in both main gear sidebrace bracket assemblies.
The New Piper Aircraft Corporation Models PA-23, PA-23-160, PA-23-235, PA-23-250…
Mar 13, 1998
Airframe (PA-34-200T)
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (2)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
Engine oil · probe · malfunctionedMay 20, 2007
ERRATIC OIL TEMP GAGE MOVEMENT. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Landing gear · spring · weakApr 2, 1997
LANDING GEAR DOWN LIGHT SLOW COMING ON. LEFT GEAR FELT LOOSE ON LANDING. WEAK SPRINGS ON BOTH GEAR. SUBMITTER STATED DOWNLOCK SPRINGS SHOULD BE REPLACED EVERY 2,000 HOURS OR 2,000 CYCLES.
From FAA Service Difficulty Reports; matched by N-number and serial number.