Rotor Flashcards
Number of lube tanks on the rotor system?
7
How long is the blade cord and how much of it is spar?
Blade cord 32” firt 8” is spar
Which component in the rotor system uses commands from the FCCs of the DAFCS to provide inputs to the rotor system?
LCT’s
What is the purpose of the Centrifugal Droop Stop Assembly?
Provide an additional limit to the drooping of the aft rotor blades during low rotor RPM
What component of the Centrifugal Droop assembly pulls the balancing arm outward as the NR increases from GROUND to FLIGHT?
Weight
What does a rotor blade drooping significantly lower than the other blades possibly indicate?
Could indicate a missing droop stop
What flight condition must be avoided if lightning
cables and straps are damaged or missing from the
rotor blade?
If any lightening cables or straps are missing or broken, avoid flight in or near thunderstorms, especially in areas of observed or anticipated lightning discharges
Which component controls the rate and limits the amount of lead and lag for the blade assemblies?
Blade shock absorbers
Name the three types oil hubs on the rotor head and describe what they lubricate.
Central Oil Tank: Lubricates the six horizontal hinge pin bearings (ensure blade is at 90deg)
Three Pitch Varying Housing Tanks: Lubricate the pitch varying housing bearings on the shaft (blade level)
Three vertical hinge pin tanks (6 tanks): Lubricate vertical hinge pin bearings (check oil when level)
Which component is mounted inside the Pitch Shaft,
passes through the Horizontal Hinge Pin, and connects
to the outboard end of the Pitch Varying Housing?
Tie Bar (Allows for feathering)
What is the maximum transient (power on) rotor RPM
(NR) with the engines driving the rotors?
106%
Name the 6 major components of the rotor head and their purpose.
(1) Rotor hub: Provides the mounting base for the components of the rotor head.
(2) Horizontal hinge pin (HHP): attaches the Pitch Varying Shaft to the Rotor Hub and allows for flapping
(3) Tie bar: (a) Connects the pitch varying housing to the pitch varying shaft. (b) Allows the pitch varying housing to rotate around the pitch varying shaft, changing the pitch in the rotor blades. (Feathering)
(4) Pitch varying shaft: Provides the mount for the pitch varying housing.
(5) Pitch Varying Housing (PVH): Provides the mounting points for: (a) Pitch change links (b) Damper (c) Rotor blade (d) Lighting protection cables (bonding jumpers). The pitch varying housing is the final point of flight control input allowing pitch inputs
(6) Vertical hinge pin (VHP): The pin allows the blade to lead and lag.
Describe the rotor system limitations (NR) IAW TM 1-1520-271-10-1
he digital readout is green if NR is between 97% and 101%, yellow if NR is between 91% and 97% or between 101% and 106%, and red if NR is < 91% or > 106%. The digital readout and tape display appears green when in normal range, changes to yellow, then to red when maximum or minimum NR limit is exceeded.
Where is the rotor blade positioned when checking for the proper oil level of the VHP oil tank?
Blade is level (oil tank level)
During preflight you discover that a rotor blade shock absorber appears to be low on hydraulic fluid. Where is that rotor blade positioned to check for proper
fluid level?
90 degrees from the fuselage