73 ADs indexed for de Havilland Aircraft Co., Ltd., The aircraft.
Airworthiness Directives; British Aerospace Model DH-114 Heron series 2A, 2DA, and 2X Series Airplanes
Unsafe Condition: Fatigue failure of the tailplane upper pick-up eyebolts.
Why matched: Airworthiness Directives; British Aerospace Model DH-114 Heron series 2A, 2DA, and 2X Series Airplanes
Airworthiness Directives; British Aerospace Model DH-114 Heron Series 1B and All Series 2 Airplanes
Unsafe Condition: Wing leading edge access doors may not remain properly secured, which could result in door failure during flight.
Why matched: Airworthiness Directives; British Aerospace Model DH-114 Heron Series 1B and All Series 2 Airplanes
Airworthiness Directives; Hawker Siddeley Aviation, Limited (British Aerospace) Model DH-104 "Dove" Series Airplanes
Unsafe Condition: Failure of the wing to fuselage attachment and loss of wing in flight due to cracks in the upper three lugs at each end of the center section main spar top boom, P/N 4FS.135 A/1.
Why matched: Airworthiness Directives; Hawker Siddeley Aviation, Limited (British Aerospace) Model DH-104 "Dove" Series Airplanes
Airworthiness Directives; Hawker Siddeley Aviation Limited Model DH-114 Heron Airplanes
Unsafe Condition: Failure of the wing to fuselage attachment and loss of the wing in flight due to cracks in the upper lugs of the left and right hand side of the upper carry through boom, P/N 14FS345.
Why matched: Airworthiness Directives; Hawker Siddeley Aviation Limited Model DH-114 Heron Airplanes
Airworthiness Directives; Hawker Siddeley Aviation Limited Model DH-104 "Dove" Series Airplanes
Unsafe Condition: Cracking and possible failure of the lugs of the lower center section main spar wing to fuselage attachment.
Why matched: Airworthiness Directives; Hawker Siddeley Aviation Limited Model DH-104 "Dove" Series Airplanes
Airworthiness Directives; Hawker Siddeley Aviation, Ltd de Havilland Model DH-104 "Dove" Series Airplanes
Unsafe Condition: Fatigue failure of the wing structure due to insufficient fatigue life of the wing lower spar boom and fuselage center section lower spar boom.
Why matched: Airworthiness Directives; Hawker Siddeley Aviation, Ltd de Havilland Model DH-104 "Dove" Series Airplanes
Airworthiness Directives; Hawker Siddeley Aviation, Limited Model DH-114 Airplanes
Unsafe Condition: Possible seizure of the main landing gear damper ram, P/N AC11164, leading to consequent damage to the aircraft upon landing.
Why matched: Airworthiness Directives; Hawker Siddeley Aviation, Limited Model DH-114 Airplanes
Airworthiness Directives; Hawker Siddeley Aviation, Ltd Model DH-104 Series Airplanes
Unsafe Condition: Corrosion of engine mount stay struts, part numbers 4 EM.357A and 4 EM.359A, could result in structural failure.
Why matched: Airworthiness Directives; Hawker Siddeley Aviation, Ltd Model DH-104 Series Airplanes
Airworthiness Directives; Hawker Siddeley Aviation, Ltd Models DH-104 "Dove" and DH-114 "Heron" Airplanes
Unsafe Condition: The possibility that a loss of generated electrical power would be undetected by the flight crew.
Why matched: Airworthiness Directives; Hawker Siddeley Aviation, Ltd Models DH-104 "Dove" and DH-114 "Heron" Airplanes
Airworthiness Directives; Hawker Siddeley Aviation, Ltd Model DH-114 Airplanes
Unsafe Condition: Internal corrosion of the engine mount stay strut, part number 14 EM.337A, could lead to structural failure of the strut.
Why matched: Airworthiness Directives; Hawker Siddeley Aviation, Ltd Model DH-114 Airplanes
Airworthiness Directives; Hawker Siddeley Aviation, Limited Model DH-114 Airplanes
Unsafe Condition: Corrosion and cracking of the drag brace fittings at the center section spar lower cap could lead to structural failure of the wing.
Why matched: Airworthiness Directives; Hawker Siddeley Aviation, Limited Model DH-114 Airplanes
Airworthiness Directives; Hawker Siddeley Aviation Limited Model DH-104 Airplanes
Unsafe Condition: Corrosion and cracking of the drag brace fittings at the center section spar lower cap could lead to structural failure of the wing.
Why matched: Airworthiness Directives; Hawker Siddeley Aviation Limited Model DH-104 Airplanes
Airworthiness Directives; Hawker Siddeley Aviation Ltd Model DH-114 Heron Airplanes
Unsafe Condition: Cracks in the nose landing gear inner casing could lead to possible collapse of the nose landing gear upon landing.
Why matched: Airworthiness Directives; Hawker Siddeley Aviation Ltd Model DH-114 Heron Airplanes
Airworthiness Directives; Hawker Siddeley Aviation, Ltd Model DH-104 "Dove" Airplanes
Unsafe Condition: Cracks in the nose landing gear inner casting could result in failure of the casing and collapse of the nose gear.
Why matched: Airworthiness Directives; Hawker Siddeley Aviation, Ltd Model DH-104 "Dove" Airplanes
Airworthiness Directives; Hawker Siddeley Aviation, Ltd Model DH-104 "Dove" Series Airplanes
Unsafe Condition: Failure of engine mounting pick-up brackets due to cracks, cut-outs, nicks, rough edges, or similar defects in the flange edges.
Why matched: Airworthiness Directives; Hawker Siddeley Aviation, Ltd Model DH-104 "Dove" Series Airplanes
Airworthiness Directives; Hawker Siddeley Aviation Limited Model DH-104 "Dove" Airplanes
Unsafe Condition: Failure of the lefthand engine mounting frame top tube, P/N 4EM.201A, and consequent tearing away of the engine.
Why matched: Airworthiness Directives; Hawker Siddeley Aviation Limited Model DH-104 "Dove" Airplanes
Airworthiness Directives; Hawker Siddeley Aviation DH-114 Series Airplanes
Unsafe Condition: Cracking of the nose gear adjusting screw (P/N 4U.493).
Why matched: Airworthiness Directives; Hawker Siddeley Aviation DH-114 Series Airplanes
Airworthiness Directives; Hawker Siddeley Aviation Ltd Model DH-104 Series Airplanes
Unsafe Condition: Cracking of the nose gear and main gear adjusting screws, P/N 4U.493.
Why matched: Airworthiness Directives; Hawker Siddeley Aviation Ltd Model DH-104 Series Airplanes
Airworthiness Directives; Hawker Siddeley Aviation Limited DH-114 Heron Airplanes
Unsafe Condition: Failure of the wing structure due to cracks in the inboard sections of the left and right wing main spar upper and lower flanges.
Why matched: Airworthiness Directives; Hawker Siddeley Aviation Limited DH-114 Heron Airplanes
Airworthiness Directives; Hawker Siddeley Aviation Limited Hawker Siddeley DH-104 "Dove" Airplanes
Unsafe Condition: Spanwise cracks in the upper and lower wing main spar joint could result in failure of the joint.
Why matched: Airworthiness Directives; Hawker Siddeley Aviation Limited Hawker Siddeley DH-104 "Dove" Airplanes