Issue of Revision 1 of Supplement No. 21, Doc. No.SSM2008AOIUSS21, which includes added compliance with CFR Title 14 Part 91.205 and Part 91.411 requirements for IFR under VMC operation.
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.
Issue of Revision 1 of Supplement No. 21, Doc. No.SSM2008AOIUSS21, which includes added compliance with CFR Title 14 Part 91.205 and Part 91.411 requirements for IFR under VMC operation.
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.
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.
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