Due to repeated non-compliance with service instructions of the emergency system manufacturer and in order to increase the emergency system safety the aircraft manufacturer points out on the compliance with service instructions of the emergency system manufacturer.
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.
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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