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Bulletins
February 14, 2024
EV97-028a_R1_SR
Mandatory
Insufficient insertion of the wing flap drive pins into the guides in flaps can cause wear of the guides and subsequent problems in operation. In the extreme case the loss of flaps controllability can occur.
The ROTAX engine manufacturer has issued Service Bulletins SB-SB-912-078UL / SB-914-059UL / SB-912 i-014iS ordering the replacement of the propeller shaft and its accessories.
Unification of the strength class of the fastening bolts in the joint of the engine and the engine mount hinges and the resulting minimization of the possibility that these bolts will be accidentally interchanged.
Increasing the safety of the oil system of THE ROTAX 912 ULS2 / S2 series engines by installing the PYROJACKET PJA 14 protective sleeves on the oil system hoses.
Unification of the strength class of the fastening bolts in the joint of the engine and the engine mount hinges and the resulting minimization of the possibility that these bolts will be accidentally interchanged.
Unification of the strength class of the fastening bolts in the joint of the engine and the engine mount hinges and the resulting minimization of the possibility that these bolts will be accidentally interchanged.
Increasing the safety of the oil system of THE ROTAX 912 ULS2 / S2 series engines by installing the PYROJACKET PJA 14 protective sleeves on the oil system hoses.
Unification of the strength class of the fastening bolts in the joint of the engine and the engine mount hinges and the resulting minimization of the possibility that these bolts will be accidentally interchanged.
Due to a deviation in the manufacturing process some tailpipe of muffler may have anomalies in the welded joint. In some cases, there is possibility that cracks may occur on a limited number of muffler tailpipe. Undetected cracks during pre-flight check may result in a loss of tailpipe.
Based on an agreement between the French Microlight Association (FFPLUM) and the French Civil Aviation Authority (DGAC), a 2019 New French Microlight Regulation has been issued, where two-seater multiaxis with an MTOM of 500 / 525 kg (without / with parachute system) are considered as a microlight aircraft.
Inspection of the Magnum emergency system due to the repeated non-compliance with service instructions of the emergency system manufacturer on aircraft in the operation.
Due to repeated non-compliance with service instructions of the emergency system manufacturer and in order to increase the emergency system safety the airplane manufacturer points out on the compliance with service instructions of the emergency system manufacturer.
The manufacturer of Rotax 914 F a Rotax 914 UL engines informs about a possibility of clutch slipping during the engine operation, which can lead to an undesirable increase of engine speed above the set limit.
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