Flight Control/Main-Rotor System Malfunctions
M b i t v d o f, v, b, r, o s.
N: B c f i t a c w c o t c t t b a b h o t u o l l.
W: D e t t m r s c c o s f t a a l. E w m/r h s.
1. L a s a p
2. E E(?) S a l
May be indicated through varying degrees of feedback, vibrations, binding, restriction, or sloppiness.
Note: Blade cuff failure is typically a cord wise crack of the cuff through the blade attachment bolt holes on the upper or lower ligament.
Warning: Danger exists that the main rotor system could collapse or separate from the aircraft after landing. Exit when m/r has stopped.
- 1. Possible
- 2. Emer Eng(s) Shutdown after landing.