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15 Cards in this Set
- Front
- Back
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Fuselage |
E6B jet propelled, long range, high speed aircraft with swept wing and tail. Fuselage compartments pressurized in flight: main cabin, flight deck, forward and aft lobes, lower nose section. Pressure is maintained by seals of fuselage, wing to body seal and vapor wing to body deal at wing root. 3 sections: forward, center and aft fuselage |
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Aileron control system |
In conjunction with spoilers provides lateral control about roll axis of aircraft. Two ailerons located in trailing edge of wing. Inboard ailerons are used along spoilers for high and low speed operation. Outboard ailerons used with spoilers and inboard for low speed |
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Spoiler and speed break control system |
-assist ailerons in providing lateral control about roll axis of aircraft -aircraft speed reduction -increase rate of descent -to increase braking effectiveness by transferring weight to wheels more rapidly -aircraft pitch trim correction in event of stabilizer trim malfunction
Regulated operations of 8 spoilers located on upper wing surfaces of each wing |
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Wing flap system |
Provide high lift on takeoff and max left and high drag on approach and landing. 10 leading edge slats and three leading edge flaps on each wing. Inboard and outboard double slotted wing flap and single slotted fillet flap on each wing |
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Stabilizer trim control system |
Provides longitudinal trim about pitch axis. Can be operated manually, manual-electronically, or auto-pilot |
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Directional (yaw) control |
Vertical axis is provided by rudder, rudder control tab and rudder control system. Mechanical system provides directional control is hydraulic system fails |
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Directional (yaw) control |
Vertical axis is provided by rudder, rudder control tab and rudder control system. Mechanical system provides directional control is hydraulic system fails |
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Elevator control system |
Provides primary pitch control about lateral axis of aircraft through series of cables |
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Directional (yaw) control |
Vertical axis is provided by rudder, rudder control tab and rudder control system. Mechanical system provides directional control is hydraulic system fails |
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Elevator control system |
Provides primary pitch control about lateral axis of aircraft through series of cables |
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Landing gear |
Trunion, shock strut, truck, brakes, tires and wheels, drag strut, side strut and actuator walking beam |
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Directional (yaw) control |
Vertical axis is provided by rudder, rudder control tab and rudder control system. Mechanical system provides directional control is hydraulic system fails |
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Elevator control system |
Provides primary pitch control about lateral axis of aircraft through series of cables |
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Landing gear |
Trunion, shock strut, truck, brakes, tires and wheels, drag strut, side strut and actuator walking beam |
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Access points |
Normal access: forward lower lobe and forward access hatch into main deck. Additional access: forward crew entry door, aft crew entry door, aft lower lobe door and electronics/battery access door |
