897 ADs indexed for Airlift International, Inc. | Curtiss-Wright Corporation | Flying Tiger Line, Inc. | L. B. Smith Aircraft Corporation | Skyways International Trading and Transport Co. | Tempo Design Corporation aircraft.
Airworthiness Directives; Ontic Engineering and Manufacturing, Inc. (Type Certificate Previously Held by Swearingen, Fairchild Aircraft, and M7 Aerospace) Airplanes
Unsafe Condition: unsafe condition on these products.
Why matched: Airworthiness Directives; Ontic Engineering and Manufacturing, Inc. (Type Certificate Previously Held by Swearingen, Fairchild Aircraft, and M7 Aerospace) Airplanes
Airworthiness Directives; General Electric Company Engines
Unsafe Condition: unsafe condition on these products.
Why matched: Airworthiness Directives; General Electric Company Engines
Airworthiness Directives; General Electric Company Engines
Unsafe Condition: Fuel leak caused by a defective fuel tube hose connecting the main fuel-oil heat exchanger.
Why matched: Airworthiness Directives; General Electric Company Engines
Airworthiness Directives; Aerospace & Defense Oxygen Systems SaS (Part of Safran Aerosystems) (Formerly Known as Air Liquide) Portable Breathing Equipment (PBE)
Unsafe Condition: Occurrences of PBE not delivering oxygen once donned, caused by a manufacturing issue.
Why matched: Airworthiness Directives; Aerospace & Defense Oxygen Systems SaS (Part of Safran Aerosystems) (Formerly Known as Air Liquide) Portable Breathing Equipment (PBE)
Airworthiness Directives; General Electric Company Engines
Unsafe Condition: Fracture and subsequent uncontained release of certain HPC stage 5 blisks due to a nonconforming indication in a single forged ingot used to manufacture the affected parts.
Why matched: Airworthiness Directives; General Electric Company Engines
Airworthiness Directives; General Electric Company Engines
Unsafe Condition: High-pressure turbine (HPT) stage 1 and HPT stage 2 disks manufactured from powder metal material suspected to contain iron inclusion, which may cause reduced material properties and a lower fatigu...
Why matched: Airworthiness Directives; General Electric Company Engines
Airworthiness Directives; Aerospace & Defense Oxygen Systems SaS (Part of Safran Aerosystems) (Formerly Known as Air Liquide)
Unsafe Condition: Occurrences of incorrect usage of PBE have been reported, which could lead to flight or cabin crewmember incapacitation, possibly affecting crewmember capability to accomplish tasks during an emerg...
Why matched: Airworthiness Directives; Aerospace & Defense Oxygen Systems SaS (Part of Safran Aerosystems) (Formerly Known as Air Liquide)
Airworthiness Directives; Aerospace & Defense Oxygen Systems SaS (Part of Safran Aerosystems) (Formerly Known as Air Liquide)
Unsafe Condition: occurrences of incorrect usage of certain PBEs have been reported, which could lead to flight or cabin crewmember incapacitation, possibly affecting crewmember capability to accomplish tasks during...
Airworthiness Directives; GE Aviation Czech s.r.o. (Type Certificate Previously Held by WALTER Engines a.s., Walter a.s., and MOTORLET a.s.) Engines
Unsafe Condition: Failure of the centrifugal compressor case.
Why matched: Airworthiness Directives; GE Aviation Czech s.r.o. (Type Certificate Previously Held by WALTER Engines a.s., Walter a.s., and MOTORLET a.s.) Engines
Airworthiness Directives; General Electric Company Engines
Unsafe Condition: Cracks found in the high-pressure turbine (HPT) front rotating air seal, which could result in uncontained release of the HPT front rotating air seal or HPT rotor disk, damage to the engine, and da...
Why matched: Airworthiness Directives; General Electric Company Engines
Airworthiness Directives; General Electric Company Engines
Unsafe Condition: A predicted reduction in the cyclic life of the combustion chamber assembly (CCA) forward flange.
Why matched: Airworthiness Directives; General Electric Company Engines
Airworthiness Directives; General Electric Company Engines
Unsafe Condition: The detection of iron inclusion in turbine disks manufactured from the same powder metal material used to manufacture certain HPT stage 1 and HPT stage 2 disks for the above-referenced engines may ...
Why matched: Airworthiness Directives; General Electric Company Engines
Airworthiness Directives; General Electric Company Engines
Unsafe Condition: The retention features of the inner and outer support air ducts on GE Model CF34-10E series engines were found to have failed, which could result in possible engine separation and loss of the airpl...
Why matched: Airworthiness Directives; General Electric Company Engines
Airworthiness Directives; General Electric Company Engines
Unsafe Condition: certain HPT stage 1 and HPT stage 2 disks were subject to iron inclusion introduced during the manufacturing process
Why matched: Airworthiness Directives; General Electric Company Engines
Airworthiness Directives; General Electric Company Engines
Unsafe Condition: Degradation of the MN4 integrated circuit microprocessor solder balls in the FADEC can result in the engine not following throttle commands.
Why matched: Airworthiness Directives; General Electric Company Engines
Airworthiness Directives; Thommen Aircraft Equipment AG Digital Air Data Computers
Unsafe Condition: Occurrences of AC32 Digital ADCs that stopped functioning due to the power module failing at temperatures below -20 degrees Celsius.
Why matched: Airworthiness Directives; Thommen Aircraft Equipment AG Digital Air Data Computers
Airworthiness Directives; General Electric Company Engines
Unsafe Condition: Failure of the stage 2 aft turbine cooling plate part number 5166T27P01 due to an actual life limit less than the current limit, which could result in uncontained failure, release of high-energy de...
Why matched: Airworthiness Directives; General Electric Company Engines
Airworthiness Directives; General Electric Company Engines
Unsafe Condition: The actual life limit of the CT7-2E1 stage 2 turbine aft cooling plate is less than the current life limit.
Why matched: Airworthiness Directives; General Electric Company Engines
Airworthiness Directives; General Electric Company Engines
Unsafe Condition: The failure of the stage 1 turbine forward cooling plate and stage 2 turbine aft cooling plate, which could result in uncontained engine failure and damage to the airplane.
Why matched: Airworthiness Directives; General Electric Company Engines
Airworthiness Directives; General Electric Company Engines
Unsafe Condition: A lower life limit may be necessary for certain stages 6-10 compressor rotor spools than allowed by the engine shop manual (ESM).
Why matched: Airworthiness Directives; General Electric Company Engines