I Have The Power
C-40 engine designation
CFM56-7
Splash: Flush eyes for a minimum of 15min. Seek immediate medical attention. Ingestion: Seek immediate medical attention.
Precautions while dealing with BMS 3-11 Type IV (Skydrol)
Located at the rear of aircraft that provides pitch control.
Horizontal Stabilizer
Left wing, Center, Right Wing
Location of C-40 fuel tanks
A, B, Standby
C-40 hydraulic systems
Located at the rear of aircraft that provides yaw stability.
Vertical Stabilizer
20% increase in inlet hazard area
Wind on ground over 25 knots
Pressure exerted anywhere upon enclosed liquid transmitted undiminished in all directions of container interior
Pascal's Law
Located on trailing edge of vertical stabilizer. Provides commanded aircraft yaw control.
Rudder
Supplies fuel to the APU. Located in left rear wing spar.
APU DC pump
Tank #1: 250 gallons, 1675lbs/760Kg
Minimum fuel quantity and location for 2min EMPD operation
Allows pilot to command aircraft roll about longitudinal axis providing bank angle for turns.
Ailerons
First stage of aircraft engine. Provides combustion and thrust bypass air.
First stage fan.
Engine driven pumps, AC electric motor driven pump
4x output ratio
Type of hydraulic pumps used on C-40. Engine driven output vs electric
Increases wing surface area enabling low speed/high angle of attack flight.
Leading Edge Flaps