20 ADs indexed for Lavia Argentina S.A. (Laviasa) aircraft.
Airworthiness Directives; Various Aircraft Equipped With Wing Lift Struts
Unsafe Condition: Corrosion in wing lift struts and cracks in wing lift strut forks could lead to structural failure of the wing lift system.
Why matched: Airworthiness Directives; Various Aircraft Equipped With Wing Lift Struts
Airworthiness Directives; LATINOAMERICANA DE AVIACIÓN (LAVIA) S.A. (Type Certificate Data Sheets No. 2A8 and No. 2A10 Previously Held by The New Piper Aircraft, Inc.) Models PA-25, PA-25-235, and PA-25-260 Airplanes
Unsafe Condition: Severe corrosion and cracks in both rear and forward supports of the horizontal stabilizer, caused by the accumulation of steam or application products vapors.
Why matched: Airworthiness Directives; LATINOAMERICANA DE AVIACION (LAVIA) S.A. (Type Certificate Data Sheets No. 2A8 and No. 2A10 Previously Held by The New Piper Aircraft, Inc.) Models PA-25, PA-25- 235, and PA-25-260 Airplanes
Airworthiness Directives; Engine Components Inc. (ECi) Reciprocating Engine Cylinder Assemblies
Unsafe Condition: Cracks in the cylinder assemblies and possible engine failure caused by separation of a cylinder head.
Why matched: Airworthiness Directives; Engine Components Inc. (ECi) Reciprocating Engine Cylinder Assemblies
Airworthiness Directives; GARMIN International GNS 430 Units
Unsafe Condition: could result in the pilot making flight decisions that put the aircraft in unsafe flight conditions.
Why matched: Airworthiness Directives; GARMIN International GNS 430 Units
Airworthiness Directives; The New Piper Aircraft, Inc. Models PA-25, PA-25-235, PA-25-260, PA-28S-160, PA-28S-180, PA-32S-300, PA-28-151, and PA-28-161 Airplanes
Unsafe Condition: Pieces of damaged induction air filters could be ingested into the engine, leading to reduced or loss of engine power.
Why matched: Airworthiness Directives; The New Piper Aircraft, Inc. Models PA-25, PA-25-235, PA-25-260, PA-28S-160, PA-28S-180, PA-32S-300, PA-28-151, and PA-28-161 Airplanes
Airworthiness Directives; The New Piper Aircraft, Inc. PA-20, PA-22, PA-23, PA-24, PA-25, PA-30, PA-31P, PA-36, PA-39, and PA-44 Series Airplanes
Unsafe Condition: Improper brake operations during ground operations can cause airplane controllability problems.
Why matched: Airworthiness Directives; The New Piper Aircraft, Inc. PA-20, PA-22, PA-23, PA-24, PA-25, PA-30, PA-31P, PA-36, PA-39, and PA-44 Series Airplanes
Airworthiness Directives; Piper Aircraft Corporation PA-25 Series Airplanes
Unsafe Condition: Cracks or corrosion in the wing forward spar fuselage attachment assembly could lead to in-flight wing separation.
Why matched: Airworthiness Directives; Piper Aircraft Corporation PA-25 Series Airplanes
Airworthiness Directives; PIPER Models PA-25, PA-25-235, and PA-25-260 Airplanes
Unsafe Condition: Cracks or other damage in the forward wing spar cap(s) due to incorporation of the metal wing skin modification by Supplemental Type Certificate (STC) SA501SW.
Why matched: Airworthiness Directives; PIPER Models PA-25, PA-25-235, and PA-25-260 Airplanes
Airworthiness Directives; Piper Model PA-25 Series Airplanes
Unsafe Condition: Cracks or damage in the forward wing spar cap and misdrilled holes in the bulbed spar flange and skin attach angles could result in structural failure of the wing spar.
Why matched: Airworthiness Directives; Piper Model PA-25 Series Airplanes
Airworthiness Directives; ESB WISCO, INCORPORATED: Applies To Those Batteries Manufactured During December 1978, January and February 1979
Unsafe Condition: The Exide AC 78M and Willard W 78M batteries manufactured between December 1978 and February 1979, identified by N-8, A-9, or B-9 stamped on terminal posts, may fail due to internal short circuits ...
Why matched: Airworthiness Directives; ESB WISCO, INCORPORATED: Applies To Those Batteries Manufactured During December 1978, January and February 1979
Airworthiness Directives; Piper Models PA-25, PA-25-235 and PA-25-260 Airplanes
Unsafe Condition: Weakening of the fuselage steel tubing cluster in the area of the rear wing spar attachment due to corrosion of the fuselage tubing.
Why matched: Airworthiness Directives; Piper Models PA-25, PA-25-235 and PA-25-260 Airplanes
Airworthiness Directives; Piper Models PA-25-235 and PA-25-260 Airplanes
Unsafe Condition: Fuel unbalance and fuel line chafing due to improper installation of fuel tank vents and grommets, leading to potential fuel line damage.
Why matched: Airworthiness Directives; Piper Models PA-25-235 and PA-25-260 Airplanes
Airworthiness Directives; Piper Model PA-25, PA-25-235, and PA-25-260 Airplanes
Unsafe Condition: Cracks in the forward wing spar web and doubler in the area of wing spar attach fitting bolt holes and in the forward spar lower cap rear flange around the inboard four skin attachment holes.
Why matched: Airworthiness Directives; Piper Model PA-25, PA-25-235, and PA-25-260 Airplanes
Airworthiness Directives; Piper Model PA-25-235 Airplanes
Unsafe Condition: Cracks in the left and right 7/8 inch x 0.035 inch upper longerons (P/N 61001-5) and 3/4 inch x 0.035 inch upper longerons (P/N 64001-13 and -14) in the hopper and fuel bays, which could lead to st...
Why matched: Airworthiness Directives; Piper Model PA-25-235 Airplanes
Airworthiness Directives; Piper Model PA-28-140, PA-28-150, PA- 28-160, PA-28-S-160, PA-25 (150 HP) Airplanes
Unsafe Condition: Power interruption as a result of abrupt throttle movement
Why matched: Airworthiness Directives; Piper Model PA-28-140, PA-28-150, PA- 28-160, PA-28-S-160, PA-25 (150 HP) Airplanes
Airworthiness Directives; Piper Model PA-25-235 Airplanes
Unsafe Condition: Failure of engine exhaust system components such as cracks, burn-throughs, weld separations, or failed internal baffles.
Why matched: Airworthiness Directives; Piper Model PA-25-235 Airplanes
Airworthiness Directives; Piper Models PA-25 and PA-25-235 Aircraft
Unsafe Condition: Worn clevis bolts, AN-24-14, on the elevator cable link assembly, P/N 81352-15, could result in loss of the elevator control system.
Why matched: Airworthiness Directives; Piper Models PA-25 and PA-25-235 Aircraft
Airworthiness Directives; Piper Model PA-25-235 Aircraft
Unsafe Condition: Air leaks permit entrance of engine fumes into the cockpit in the area of the fuselage right main landing gear fittings.
Why matched: Airworthiness Directives; Piper Model PA-25-235 Aircraft
Airworthiness Directives; Piper Model PA-25-235 Aircraft
Unsafe Condition: Weld separations on the end of the landing gear shock strut assembly, Piper P/N 486604, which attaches to the landing gear vee assembly.
Why matched: Airworthiness Directives; Piper Model PA-25-235 Aircraft
Airworthiness Directives; Piper Model PA-25 Aircraft
Unsafe Condition: Aluminum front spar wing-to-fuselage attachment fittings (Piper P/N's 61111-00 and 61111-01) may fail due to stress corrosion cracking.
Why matched: Airworthiness Directives; Piper Model PA-25 Aircraft