Displaying 1 - 60 of 80
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 ensure proper operation of the main landing gear (MLG) door
Type: Text
Year: 1991
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 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 structural failure of the flap. Amendment: 39-4392 as amended by Amendment 39-5058
Type: Text
Year: 1985
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 prevent failure of the restraint provisions for the weather radar receiver/transmitter. Amendment: 39-3245
Type: Text
Year: 1978
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 - CIRCUIT PROTECTION FOR COCKPIT FAN BLOWERS
Type: Text
Year: 2008
Member of: Airworthiness Directives
Electrical Power - Electrical Interference Suppression. Revision 3
Type: Text
Year: 1982
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 - Distribution - Panel `ZL' addition of Protective covers
Type: Text
Year: 1983
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
ELECTRICAL POWER - CONSTANT FREQUENCY SYSTEM - INTRODUCTION OF A COVER FOR THE STANDBY INVERTER
Type: Text
Year: 1990
Member of: Airworthiness Directives
ELECTRICAL POWER - CABLE INSTALLATION - CHAFING - OF WIRE AT PANEL ZL
Type: Text
Year: 1987
Member of: Airworthiness Directives
ELECTRICAL POWER - GENERATOR POWER - TO INTRODUCE ADDITIONAL GENERATOR CONTROL ARRANGEMENTS AND RELOCATE G.C.U. EARTH WIRES
Type: Text
Year: 1992
Member of: Airworthiness Directives
ELECTRICAL POWER - INSPECTION AND REPLACEMENT OF UAM100 LIMITERS
Type: Text
Year: 2006
Member of: Airworthiness Directives
ELECTRICAL POWER - INSPECTION / RELOCATION OF POWER SOURCE FOR INSTRUMENT PANELAND LH AND RH COCKPIT BLOWERS
Type: Text
Year: 2000
Member of: Airworthiness Directives
ELECTRICAL POWER - LIGHTING - TO INTRODUCE A CIRCUIT BREAKER AT THE TRANSFORMER OUTPUT FOR THE 6V LIGHTING CIRCUITS
Type: Text
Year: 1994
Member of: Airworthiness Directives
ELECTRICAL POWER - WIRING INSTALLATION - REROUTING OF WIRING INSTALLATION AT PANEL ZL
Type: Text
Year: 1987
Member of: Airworthiness Directives
Electrical Power - Fuel Computers DC power supply transferred to `PE' busbar from `PE2' busbar
Type: Text
Year: 1980
Member of: Airworthiness Directives
ELECTRICAL POWER - Load Distribution - To introduce uprated feeder fuses in the PE busbar circuits on panel ZL. REVISION NO. 1 Dated February 27th 1984
Type: Text
Year: 1984
Member of: Airworthiness Directives
ELECTRICAL POWER SMOKE DRILLADDITIONAL CIRCUIT BREAKER IDENTIFICATION LABELS
Type: Text
Year: 1988
Member of: Airworthiness Directives
FIRE PROTECTION - INTRODUCTION OF ELECTRICAL WIRE PROTECTION KIT
Type: Text
Year: 2003
Member of: Airworthiness Directives
Mandatory: FUSELAGE - FAIRINGS - INTRODUCTION OF DRAIN MASTS AT REAR EQUIPMENT BAY VENT OUTLETS
Type: Text
Year: 1992
Member of: Airworthiness Directives
ELECTRICAL POWER - STANDBY INVERTER - TO INTRODUCE IMPROVED SEALING OF THE PRINTED CIRCUIT BOARD ASSEMBLY IN THE STATIC INVERTER (TYPE PC 250)
Type: Text
Year: 1994
Member of: Airworthiness Directives
Mandatory: FUEL: INSPECTION OF FUEL FEED PIPE JOINTS FOR MISALIGNMENT AT PIPE ENTRY INTO COUPLING
Type: Text
Year: 1984
Member of: Airworthiness Directives
FLYING CONTROLS-ELEVATOR MASS BALANCE-POSSIBLE CORROSION OF BALANCE WEIGHT SIDEPLATE ASSY AND SPIGOT
Type: Text
Year: 1989
Member of: Airworthiness Directives
FIRE PROTECTION - INSPECTION OF BLOCKING DIODES ASSOCIATED WITH `EXT FIRED' (BOTTLE GONE) INDICATORS, FOR FAILURE
Type: Text
Year: 1992
Member of: Airworthiness Directives
EQUIPMENT/FURNISHINGS - WARMING OVEN - INTRODUCE WARMING OVEN PART Nos. 255D-LH-28/115, 255D-RH-28/115 AND 255-362A WITH OVERHEAT PROTECTION
Type: Text
Year: 1989
Member of: Airworthiness Directives
FUEL - PRESSURE REFUEL/DEFUEL SYSTEM - FAILURE OF HTE 'V' CLAMPS
Type: Text
Year: 1978
Member of: Airworthiness Directives
Mandatory: AIR CONDITIONING - FAN VENTURI MOTOR REPLACEMENT
Type: Text
Year: 2004
Member of: Airworthiness Directives
LANDING GEAR - MAIN GEAR FAIRINGS AND DOORS - TO INTRODUCE STEEL WING ATTACHMENT CASTING FOR MAIN GEAR DOOR JACK
Type: Text
Year: 1988
Member of: Airworthiness Directives
Mandatory: LANDING GEAR - MAIN LANDING GEAR - TO INTRODUCE A REPLACEMENT SIDESTAY JACK PIVOT ASSEMBLY
Type: Text
Year: 1995
Member of: Airworthiness Directives
Mandatory: LANDING GEAR - MAIN LANDING GEAR (MLG) ACTUATOR CYLINDER HEAD INSPECTION
Type: Text
Year: 2000
Member of: Airworthiness Directives
Mandatory: FUSELAGE - INSPECTION OF NOSE LANDING GEAR BAY SIDEWALL FOR CRACKS
Type: Text
Year: 1991
Member of: Airworthiness Directives
Mandatory: LANDING GEAR - INSPECTION OF RH AND LH M.L.G. SIDESTAY JACK PIVOT FOR POSSIBLE CRACKING
Type: Text
Year: 1994
Member of: Airworthiness Directives
Mandatory: LANDING GEAR - CRACKING OF MAIN GEAR DOOR FORWARD HINGE FITTING
Type: Text
Year: 1988
Member of: Airworthiness Directives
Mandatory: HYDRAULIC POWER - REAR FUSELAGE - INTRODUCTION OF A CHARGING INSTRUCTION LABEL FOR HYDRAULIC SYSTEM ACCUMULATORS
Type: Text
Year: 1992
Member of: Airworthiness Directives
Mandatory: OXYGEN - TO INTRODUCE REPLACEMENT OXYGEN FITTINGS IN LIEU OF FITTINGS INCOMPATIBLE WITH THE OXYGEN SYSTEM
Type: Text
Year: 1998
Member of: Airworthiness Directives
Mandatory: OXYGEN SYSTEM - INSPECTION OF OXYGEN SYSTEM FOR POSSIBLE INSTALLATION OF UNQUALIFIED FLEXIBLE HOSES
Type: Text
Year: 1996
Member of: Airworthiness Directives
Recommended: NAVIGATION - MODIFICATION OF PITOT/STATIC AND STALL VENT DRAIN VALVES
Type: Text
Year: 1999
Member of: Airworthiness Directives
Mandatory: NAVIGATION - INSPECTION OF PITOT/STATIC AND STALL VENT DRAIN VALVES
Type: Text
Year: 1999
Member of: Airworthiness Directives
Optional: NAVIGATION - TEMPORARY SEALING PITOT/STATIC AND STALL VENT DRAIN VALVES WITH RTV SEALANT
Type: Text
Year: 1999
Member of: Airworthiness Directives
Mandatory: POWER PLANT - ENGINE MOUNTINGS - COWLING CHAFE DAMAGE
Type: Text
Year: 1985
Member of: Airworthiness Directives
LANDING GEAR - MAIN GEAR - POSSIBLE FAILURE TO LOWER
Type: Text
Year: 1981
Member of: Airworthiness Directives
Mandatory: LANDING GEAR - MAIN LANDING GEAR SIDESTAY UPPER ARM - INTRODUCTION OF AN ULTIMATE LIFE
Type: Text
Year: 1988
Member of: Airworthiness Directives
The FAA is Issuing this AD to Inspect for Cracks and Thickness
Type: Text
Year: 2025
Member of: Airworthiness Directives
Mandatory: NAVIGATION - RCAAVQ21 AND PRIMUS 40 WEATHER RADAR SYSTEMS - DEFECTIVE MOUNTING TRAY FOR RECEIVER/TRANSMITTER
Type: Text
Year: 1978
Member of: Airworthiness Directives
Mandatory: FUEL PRESSURE REFUEL/DEFUEL SYSTEM - FAILURE OF HTE 'V' CLAMPS
Type: Text
Year: 1978
Member of: Airworthiness Directives
Mandatory: TITLE: T-39 APU - FUEL ENCLOSURE BOX TEMPERATURE SENSOR - SEALANT REPLACEMENT REV. l
Type: Text
Year: 1993
Member of: Airworthiness Directives