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 · engine · destroyedApr 2, 2005
AFTER TAKE-OFF THE LT ENGINE SUFFERED A CATASTROPHIC FAILURE. TWO CONNECTING RODS (NR 5, 6) FAILED AND KNOCKED A HOLE IN THE CRANKCASE. THE RESULTING HOLE IN THE CRANKCASE WAS THE LOCATION OF A FIRE WHICH BURNED THROUGH THE COWLING AND CONTINUED BURNING. THE AIRCRAFT WAS LANDED SAFELY. AFTER…
From FAA Service Difficulty Reports; matched by N-number and serial number.
CYLINDER HEAD SEPARATED COMPLETELY FROM BARREL IN-FLIGHT. FAILURE POSSIBLE DUE TO FATIGUE. TOTAL CYLINDER TIME IS UNKNOWN. TOTAL TIME SINCE CERMICHROME: 259.0 HOURS. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number.