32 results found (1058ms)
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; Goodrich De-icing and Specialty Systems “FASTprop” Propeller De-icers
Unsafe Condition: Goodrich De-icing and Specialty Systems 'FASTprop' propeller de-icers becoming loose or debonded, and detaching from propeller blades during operation.
Why matched: Airworthiness Directives; Goodrich De-icing and Specialty Systems "FASTprop" Propeller De-icers
Airworthiness Directives; Gulfstream American (Formerly Grumman American Aviation Corporation) Model GA-7 Airplanes
Unsafe Condition: Chafing and possible leakage of the main fuel feed line by the propeller control cable behind the firewall in the left hand engine nacelle.
Why matched: Airworthiness Directives; Gulfstream American (Formerly Grumman American Aviation Corporation) Model GA-7 Airplanes
Airworthiness Directives; Gulfstream American (Formerly Grumman American Aviation Corporation) Model GA-7 Airplanes
Unsafe Condition: Fuel leakage from cracks in the inboard fuel tank ribs at Wing Station (W.S.) 109, at the forward fuel tank outlet fittings in the left and right wings.
Why matched: Airworthiness Directives; Gulfstream American (Formerly Grumman American Aviation Corporation) Model GA-7 Airplanes
Airworthiness Directives; Gulfstream American Corporation (GAC) (Formerly Grumman American Aviation Corporation) Model GA-7 Airplanes
Unsafe Condition: Partial loss of rudder control due to excessive freeplay in the rudder assembly exceeding maximum allowed limits (.040 inches or 1 degree).
Why matched: Airworthiness Directives; Gulfstream American Corporation (GAC) (Formerly Grumman American Aviation Corporation) Model GA-7 Airplanes
Airworthiness Directives; Grumman Model G-21A Aircraft
Unsafe Condition: The inability to restart an engine and the simultaneous loss of the remaining engine due to modifications incorporating Hartzell propellers and governor crossfeed systems under STC SA1-52.
Why matched: Airworthiness Directives; Grumman Model G-21A Aircraft
Airworthiness Directives; Gulfstream American Corporation (GAC) (Formerly Grumman American Aviation Corporation (GAAC) Model GA-7 Airplanes
Unsafe Condition: Excessive force required to move the fuel selector valve from one position to another position creates a hazard to the airplane.
Why matched: Airworthiness Directives; Gulfstream American Corporation (GAC) (Formerly Grumman American Aviation Corporation (GAAC) Model GA-7 Airplanes
Airworthiness Directives; Grumman American Aviation Corporation Model AA-1, AA-1A, AA-1B Airplanes
Unsafe Condition: Failure of the fuel measurement gauge float and associated components could lead to inaccurate fuel quantity indication, increasing the risk of unintentional fuel exhaustion in flight.
Why matched: Airworthiness Directives; Grumman American Aviation Corporation Model AA-1, AA-1A, AA-1B Airplanes
Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION (GAAC) Model G-159 and G-1159 Airplanes
Unsafe Condition: Failure to prevent injury to an occupant of any jumpseat located between fuselage stations 119 and 169 on GAAC Models G-159 and G-1159 airplanes.
Why matched: Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION (GAAC) Model G-159 and G-1159 Airplanes
Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION Model G-1159 Airplanes
Unsafe Condition: Main landing gear failures due to the installation of part number 1159SC-L202-11 or 1159SC-L202-13 side brace/actuating cylinders.
Why matched: Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION Model G-1159 Airplanes
Airworthiness Directives; Grumman American Aviation Corporation Model AA- 5A, and Model AA-5B, Airplanes
Unsafe Condition: Faulty altitude, airspeed, and vertical speed indications from the alternate static source valve Gerdes part number A-1390 due to contamination or lack of lubrication.
Why matched: Airworthiness Directives; Grumman American Aviation Corporation Model AA- 5A, and Model AA-5B, Airplanes
Airworthiness Directives; Grumman American Aviation Corporation Model AA-5 and AA-5A Airplanes
Unsafe Condition: Failure of the carburetor heat valve assembly due to cracks in the bend radius of Configuration A.
Why matched: Airworthiness Directives; Grumman American Aviation Corporation Model AA-5 and AA-5A Airplanes
Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION Model G-1159 Airplanes
Unsafe Condition: Loose terminal connections at the generator terminal boards and associated wiring connections could lead to arcing and failure of the generator system.
Why matched: Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION Model G-1159 Airplanes
Airworthiness Directives; Grumman American Aviation Corporation Model AA1, AA1A, AA1B, AA5, AA-5A, AA-5B Airplanes
Unsafe Condition: Delaminations in bonded skins
Why matched: Airworthiness Directives; Grumman American Aviation Corporation Model AA1, AA1A, AA1B, AA5, AA-5A, AA-5B Airplanes
Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION Model G-1159 Airplanes
Unsafe Condition: unnecessarily high longitudinal stick forces due to an inadvertent excessive increase of nose down electric trim
Why matched: Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION Model G-1159 Airplanes
Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION Model G-1159 Airplanes
Unsafe Condition: Failure of the ground spoilers to deactivate could result in unintended operation during flight, leading to potential loss of control.
Why matched: Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION Model G-1159 Airplanes
Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION Model G-1159 Airplanes
Unsafe Condition: The stall barrier hydraulic in-line filters may become lodged in the stall barrier valves, causing the stick pusher to remain energized after actuation. Portions of the filters could also damage th...
Why matched: Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION Model G-1159 Airplanes
Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION Model G-1159 Airplanes
Unsafe Condition: Possible loss of all DC and AC power due to battery switch ground leads not connected to separate studs at the center overhead panel.
Why matched: Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION Model G-1159 Airplanes
Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION (GAAC) Models G-159 and G-1159 Airplanes
Unsafe Condition: Cracks in the fuselage aft section pressure dome assembly (Part No. 1159B21372 for G-1159, Part No. 159B10252 for G-159) could lead to structural failure.
Why matched: Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION (GAAC) Models G-159 and G-1159 Airplanes
Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION Model G-1159 Airplanes
Unsafe Condition: Operation of the pitch trim at a greater rate when an additional signal in the opposite direction is selected.
Why matched: Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION Model G-1159 Airplanes
Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION Model G-1159
Unsafe Condition: The fire extinguisher circuits may fail due to insufficient redundancy in the electrical squib circuits, which could prevent activation of the fire extinguishing system during an emergency.
Why matched: Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION Model G-1159
Airworthiness Directives; Grumman American Aviation Corporation Model AA-1, Model AA-1A, and Model AA-1B Airplanes
Unsafe Condition: The absence of placards indicating prohibited spins and information to prevent accidental spin entry could lead to unintended spin conditions and loss of control.
Why matched: Airworthiness Directives; Grumman American Aviation Corporation Model AA-1, Model AA-1A, and Model AA-1B Airplanes
Airworthiness Directives; Grumman Model G-21 and G-21A Type Airplanes
Unsafe Condition: Failure of the elevator torque tube assembly P/N 12755, rudder torque tube assembly P/N 12756, L.H. and R.H. rudder pedal torque tube assemblies P/Ns 12757, 12758, and hinge support assembly P/N 12...
Why matched: Airworthiness Directives; Grumman Model G-21 and G-21A Type Airplanes
Airworthiness Directives; Grumman Aircraft Model G-21 and G-21A Airplanes
Unsafe Condition: Engine fuel starvation due to fuel vaporization within fuel feed lines to the engines.
Why matched: Airworthiness Directives; Grumman Aircraft Model G-21 and G-21A Airplanes
Airworthiness Directives; Grumman Aircraft Model G-21A (Converted OA-9, JRF-1 through JRF-5 Under TC 654) Aircraft.
Unsafe Condition: Cracks extending radially from the outside edge of the ears to the inside of the hole into which the shoulder bushings are pressed in the stabilizer forward attachment fittings (P/N 12548 and P/N 1...
Why matched: Airworthiness Directives; Grumman Aircraft Model G-21A (Converted OA-9, JRF-1 through JRF-5 Under TC 654) Aircraft.