Airworthiness Directives
Displaying 61 - 80 of 80
To prevent failure of the forward engine mounts
Type: Text
Year: 1986
Member of: Airworthiness Directives
To prevent failure of the main engine mount beam
Type: Text
Year: 1980
Member of: Airworthiness Directives
Recurring - LANDING GEAR - INSPECTION OF RH AND LH M.L.G. SIDESTAY JACK PIVOT FOR POSSIBLE CRACKING
Type: Text
Year: 1995
Member of: Airworthiness Directives
Recurring - LANDING GEAR - INSPECTION OF RH AND LH M.L.G. SIDESTAY JACK PIVOT FOR POSSIBLE CRACKING (Inspection)
Type: Text
Year: 1994
Member of: Airworthiness Directives
[Recurring] TO DETECT AND CORRECT CRACKS IN THE BRIDGE CAST
Type: Text
Year: 1983
Member of: Airworthiness Directives
[Recurring] To detect cracking and possible failure of the attaching lugs of the tee pieces, P/N 25-7PA41 Amendment: 39-3168
Type: Text
Year: 1978
Member of: Airworthiness Directives
[Recurring] To ensure proper operation of the main landing gear (MLG) door
Type: Text
Year: 1991
Member of: Airworthiness Directives
[Recurring] To prevent a circuit from overheating and a resultant fire. Amendment: 39-8493
Type: Text
Year: 1993
Member of: Airworthiness Directives
[Recurring] To prevent displacement of the aileron mass balance side plate, and possible control surface interference. Amendment: 39-5877
Type: Text
Year: 1988
Member of: Airworthiness Directives
[Recurring] To prevent erroneous altimeter and airspeed indications due to plugged or taped pitot/static and stall vent drain valves. Amendment: 39-11949
Type: Text
Year: 2000
Member of: Airworthiness Directives
[Recurring] To prevent failure of the restraint provisions for the weather radar receiver/transmitter. Amendment: 39-3245
Type: Text
Year: 1978
Member of: Airworthiness Directives
[Recurring] To prevent structural failure of the flap. Amendment: 39-4392 as amended by Amendment 39-5058
Type: Text
Year: 1985
Member of: Airworthiness Directives
[Recurring] To prevent the inability of the MLG to deploy and a consequent wheels-up landing. Amendment: 39-9913
Type: Text
Year: 1997
Member of: Airworthiness Directives
[Recurring] To prevent the possible loss of flaps. Amendment: 39-3797 as amended by Amendment 39-4524
Type: Text
Year: 1983
Member of: Airworthiness Directives
AIRBORNE AUXILIARY POWER - To introduce heavy duty bonding between A.P.U. and engine mounting beam
Type: Text
Year: 1986
Member of: Airworthiness Directives
Electrical Power - Electrical Interference Suppression. Revision 3
Type: Text
Year: 1982
Member of: Airworthiness Directives
ELECTRICAL POWER - BATTERY AND EMERGENCY CONTACTORS - INTRODUCTION OF REVISED MOUNTING ARRANGEMENTS FOR THE BATTERY AND EMERGENCY CONTACTORS
Type: Text
Year: 1993
Member of: Airworthiness Directives
ELECTRICAL POWER - CABLE INSTALLATION - CHAFING - OF WIRE AT PANEL ZL
Type: Text
Year: 1987
Member of: Airworthiness Directives