12 results found (1600ms)
Airworthiness Directives; GULFSTREAM AMERICAN CORPORATION Models G-1159 and G-1159B Series Airplanes
Unsafe Condition: Possible severe flutter of the elevator and/or elevator trim tab due to cracks in the outboard elevator trim tab hinge fittings and elevator rear spar.
Why matched: Airworthiness Directives; GULFSTREAM AMERICAN CORPORATION Models G-1159 and G-1159B Series Airplanes
Airworthiness Directives; GULFSTREAM AMERICAN CORPORATION Model G-1159 and G-1159A
Unsafe Condition: Loss of fluid flow in the auxiliary hydraulic system following a complete loss of fluid in the combined hydraulic system.
Why matched: Airworthiness Directives; GULFSTREAM AMERICAN CORPORATION Model G-1159 and G-1159A
Airworthiness Directives; GULFSTREAM AMERICAN CORPORATION Model AA5, AA5A and A5B Series Airplanes
Unsafe Condition: Broken wires in carburetor airbox screens can cause filter material to enter the induction system and carburetor throat, leading to engine power loss.
Why matched: Airworthiness Directives; GULFSTREAM AMERICAN CORPORATION Model AA5, AA5A and A5B Series Airplanes
Airworthiness Directives; GULFSTREAM AMERICAN CORPORATION Model G-1159 Airplanes
Unsafe Condition: Improper functioning of the landing gear system due to installation of landing gear selector valve part numbers 1159SCH216-3, which may interrupt retraction or extension.
Why matched: Airworthiness Directives; GULFSTREAM AMERICAN CORPORATION Model G-1159 Airplanes
Airworthiness Directives; GULFSTREAM AMERICAN CORPORATION Model G-159 Airplanes
Unsafe Condition: Possible operation at degraded performance levels due to inaccurate performance data presented in the AFM.
Why matched: Airworthiness Directives; GULFSTREAM AMERICAN CORPORATION Model G-159 Airplanes
Airworthiness Directives; Gulfstream American Corporation (GAC) Model AA-5, AA-5A, AA-5B, Airplanes
Unsafe Condition: Possible aileron oscillation due to loose rivets, damage, delamination, wear, damage, insecure mounting of aileron bearings and stops, improper rigging and cable tension, or worn and loose joints i...
Why matched: Airworthiness Directives; Gulfstream American Corporation (GAC) Model AA-5, AA-5A, AA-5B, 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; Gulfstream American Corporation (GAC) Model GA-7 Airplanes
Unsafe Condition: Failure of the elevator trim control master chain and loss of elevator trim control
Why matched: Airworthiness Directives; Gulfstream American Corporation (GAC) Model GA-7 Airplanes
Airworthiness Directives; GULFSTREAM AMERICAN CORPORATION (GAC) (FORMERLY GRUMMAN AMERICAN AVIATION CORPORATION Model G-1159 Airplanes
Unsafe Condition: Cabin window pane failure and possible engine damage.
Why matched: Airworthiness Directives; GULFSTREAM AMERICAN CORPORATION (GAC) (FORMERLY GRUMMAN AMERICAN AVIATION CORPORATION Model G-1159 Airplanes
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 Models G-44 and G-44A Aircraft
Unsafe Condition: Landing gear locking mechanism failures due to hydraulic system leaks or mechanical lock failures in both up and down positions.
Why matched: Airworthiness Directives; Grumman Models G-44 and G-44A Aircraft
Airworthiness Directives; Grumman Model G-44 and G-44A Aircraft
Unsafe Condition: Cracks extending radially from the outside edge of the ears to the inside of the hole in the stabilizer strut upper terminal (P/N 17257-1).
Why matched: Airworthiness Directives; Grumman Model G-44 and G-44A Aircraft