18 results found (2006ms)
Airworthiness Directives; Various Airplanes
Unsafe Condition: The displayed fuel quantity can have an error as much as four gallons/fuel tank with the display indicating four gallons with an empty tank. In the context of this event, the end level effect is th...
Why matched: Airworthiness Directives; Various Airplanes
Airworthiness Directives; Aviat Aircraft Inc.
Unsafe Condition: Failure of either the forward or rear support transfers loads to the other support, increasing the likelihood that both could fail, which has occurred in one known incident. A combined failure of b...
Why matched: Airworthiness Directives; Aviat Aircraft Inc.
Airworthiness Directives; Aviat Aircraft Inc. Airplanes
Unsafe Condition: The fuel tank vent check valves are sticking in the closed position causing fuel starvation to the engine.
Why matched: Airworthiness Directives; Aviat Aircraft Inc. 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; Aviat Aircraft Inc. Models S-2A, S-2B, and S-2S Airplanes (formerly Pitts Models S-2A, S-2B, and S-2S airplanes)
Unsafe Condition: Cracking in the upper longerons caused by operating the airplane outside of the certificated design limits, leading to subsequent failure of the longerons and consequent loss of control of the airp...
Why matched: Airworthiness Directives; Aviat Aircraft Inc. Models S-2A, S-2B, and S-2S Airplanes (formerly Pitts Models S-2A, S-2B, and S-2S airplanes)
Airworthiness Directives; Aviat Aircraft Inc. Models S-2A, S-2B, and S-2S Airplanes (formerly Pitts Models S-2A, S-2B, and S-2S airplanes)
Unsafe Condition: Cracking in the upper longerons caused by operating the airplane outside of the certificated design limits, leading to subsequent failure of the longerons and consequent loss of control of the airp...
Why matched: Airworthiness Directives; Aviat Aircraft Inc. Models S-2A, S-2B, and S-2S Airplanes (formerly Pitts Models S-2A, S-2B, and S-2S airplanes)
Airworthiness Directives; Aviat Aircraft Inc. Models S-2A, S-2B, and S-2S Airplanes (formerly Pitts Models S-2A, S-2B, and S-2S airplanes)
Unsafe Condition: Cracking and subsequent failure of the longerons aft of the rear cabane struts.
Why matched: Airworthiness Directives; Aviat Aircraft Inc. Models S-2A, S-2B, and S-2S Airplanes (formerly Pitts Models S-2A, S-2B, and S-2S airplanes)
Airworthiness Directives; Aviat Aircraft, Inc. Models S-1S, S-1T, S-2, S-2A, S-2S, and S-2B Airplanes (formerly known as Pitts Models S-1S, S-1T, S-2, S-2A, S-2S, and S-2B Airplanes)
Unsafe Condition: Fatigue cracking at the upper weld above the pivot bearing of the flight control stick with a wall thickness of .035 inch could result in inability to maneuver the airplane and subsequent loss of c...
Why matched: Airworthiness Directives; Aviat Aircraft, Inc. Models S-1S, S-1T, S-2, S-2A, S-2S, and S-2B Airplanes (formerly known as Pitts Models S-1S, S-1T, S-2, S-2A, S-2S, and S-2B Airplanes)
Airworthiness Directives; Aviat Aircraft Inc. Models S-2A, S-2B, and S-2S Airplanes (Formerly Pitts Models S-2A, S-2B, and S-2S Airplanes)
Unsafe Condition: Cracks in the longerons aft of the rear cabane struts due to fatigue.
Why matched: Airworthiness Directives; Aviat Aircraft Inc. Models S-2A, S-2B, and S-2S Airplanes (Formerly Pitts Models S-2A, S-2B, and S-2S Airplanes)
Airworthiness Directives; Aviat Aircraft, Inc. Models S-1S, S-1T, S-2, S-2A, S-2S, and S-2B Airplanes
Unsafe Condition: Possible in-flight separation of the wing from the airplane caused by a cracked aft lower fuselage wing attach fitting.
Why matched: Airworthiness Directives; Aviat Aircraft, Inc. Models S-1S, S-1T, S-2, S-2A, S-2S, and S-2B Airplanes
Airworthiness Directives; AVIAT (formerly Christen Industries) Model A-1 Husky Series Airplanes
Unsafe Condition: Loss of airflow to the carburetor and possible loss of engine power, which could result in loss of control of the airplane.
Why matched: Airworthiness Directives; AVIAT (formerly Christen Industries) Model A-1 Husky Series Airplanes
Airworthiness Directives; CHRISTEN INDUSTRIES, INC. Model A-1 (Husky) Series Airplanes
Unsafe Condition: Failure of the forward seat back, which could result in loss of control of the airplane.
Why matched: Airworthiness Directives; CHRISTEN INDUSTRIES, INC. Model A-1 (Husky) Series Airplanes
Airworthiness Directives; Pitts Model S-2A Series Airplanes
Unsafe Condition: Cracks in the welds attaching P/N 2-5100-12 stick housings to P/N 2-5100-11 tube in the cockpit control tube assembly could cause loss of normal aileron and elevator control.
Why matched: Airworthiness Directives; Pitts Model S-2A Series Airplanes
Airworthiness Directives; Pitts Model S-1S and S-2A Airplanes
Unsafe Condition: Partial loss of rudder control due to control cable slippage resulting from improper swaging of the Nicopress sleeves.
Why matched: Airworthiness Directives; Pitts Model S-1S and S-2A Airplanes
Airworthiness Directives; Pitts S-2A Airplanes
Unsafe Condition: Failure of the induction air box flapper door due to cracks in the welded areas could cause power loss.
Why matched: Airworthiness Directives; Pitts S-2A Airplanes
Airworthiness Directives; Pitts Model S-2A Series Airplanes
Unsafe Condition: Cracks in the horizontal stabilizer support tubes (P/N 2-2123 and 2-2100-109) and front/rear tubes (P/N 2-3100) near AN3 bolt holes could lead to structural failure.
Why matched: Airworthiness Directives; Pitts Model S-2A Series Airplanes
Airworthiness Directives; Pitts Model S-2A Series Airplanes
Unsafe Condition: Failure of the horizontal stabilizer leading edge support tube due to cracks in the vicinity of the AN3 bolt holes.
Why matched: Airworthiness Directives; Pitts Model S-2A Series Airplanes
Airworthiness Directives; Pitts Model S-2A Series Airplanes
Unsafe Condition: Excessive in-flight vibration of the aileron interconnect tubes, part number 2-5216-1, can cause structural damage.
Why matched: Airworthiness Directives; Pitts Model S-2A Series Airplanes