Phase III Block I Flashcards
Ensure the ______________ and T/Rs are closed or removed before extension of the _______ and leading _____ and _______.
Ensure the onboard fan duct cowling and T/Rs are closed or removed before extension of the Krueger Flaps and leading flaps and slats.
__________ exit door swings out and up if opening from the outside, hold your _______________ while opening.
Over wing exit door swings out and up if opening from the outside, hold your knee against the door while opening.
Don’t open service doors when __________________ is visible. Warning that __________ is installed and the slide will automatically deploy.
Don’t open service doors when orange warning flag is visible. Warning that Girt Bar is installed and the slide will automatically deploy.
The fuselage is a _____________[__ component which provides _________ and __________________ compartments containing:
____________
_____________
Safety devices for ____________________
The fuselage is a high cylindrical shaped component which provides pressurized and non pressurized compartments containing:
Avionics
Mechanical
Safety devices for Aircrew, Personnel, and Cargo
The __________, ___________, and _____________ is attached to the fuselage
The wings, elevators, and rudder is attached to the fuselage
The internal fuselage can be configured/rigged in three manners depending on mission requirements
Pax: ______________________
Combo: __________________
Cargo: ___________________
The internal fuselage can be configured/rigged in three manners depending on mission requirements
Pax: All passenger mode w/ 121 passengers and 0 pallets
Combo: Combination mode w/ 69 passengers and up to 3 pallets
Cargo: All cargo mode w/ 0 passengers and up to 8 pallets
The tail of the aircraft is made up of a _____________ and ____________ stabilizer.
The tail of the aircraft is made up of a horizontal and vertical stabilizer.
The __________________ affects pitch control and reduces uncontrolled movement along lateral axis.
The Horizontal stabilizer affects pitch control and reduces uncontrolled movement along lateral axis.
The __________________ affects yaw control along the vertical axis.
The vertical stabilizer affects yaw control along the vertical axis.
The wings provide ____________ and _______________ for flight control surfaces and engines.
The wings provide lift and attachment points for flight control surfaces and engines.
The winglets provide the potential benefits of lower operating costs by____________, _____________, and ___________________.
The winglets provide the potential benefits of lower operating costs by reducing fuel burn, improve payload capability, and increase range.
Two ______________, one on each wing, are attached to the wings. They are the attachment structures connecting the engines to the wings and provide _______________ and ___________________________________.
Two engine pylons, one on each wing, are attached to the wings. They are the attachment structures connecting the engines to the wings and provide aerodynamic properties and protection of engine related components.
The ______________ is the aerodynamic cone on the forward fuselage. It covers the _______________ and additional ______________.
The radome is the aerodynamic cone on the forward fuselage. It covers the radar dish and additional avionics.
The Radome provides ________________ and ________________________.
The Radome provides aerodynamic properties and protection of engine related components.
There are ____________ doors/hatches used for normal maintenance and egress ___________________________
There are six door/hatches used for normal maintenance and egress (FWD pass, FWD Galley SVC, overwing(2), AFT Pass, AFT Galley SVC)
There are 5 main access doors/hatches __________________
There are 5 main access doors/hatches (FWD cargo, aft cargo,APU access, FWD access, E/E bay). And main deck cargo for cargo loading
The control column is located in the cockpit. There are two _________ and are used for ___________ to control elevators.
The control column is located in the cockpit. There are two (pilot/1st officer) and are used for (push/pull) to control elevators.
The ailerons are located on the _________________ of the outer wing. With inputs from the _______________, the ailerons induce aerodynamic changes that caused the aircraft ____________ on the longitudinal access
The ailerons are located on the trailing edge of the outer wing. With inputs from the control wheel on the control column, the ailerons induce aerodynamic changes that caused the aircraft to roll on the longitudinal access
The rudderpedals are located _____________. Two pairs of pedals (pilot/first officer) onn the floor, forward of the control column, and are used for steering (up to ________ each side of center) and yaw control
The rudderpedals are located in the cockpit. Two pairs of pedals (pilot/first officer) onn the floor, forward of the control column, and are used for steering (up to 7° each side of center) and yaw control
The rudder Is located on the trailing edge of the _______________. With input from the _________________, the rudder induces Aerodynamic changes that cause the aircraft to _____________ along the vertical axis.
The rudder Is located on the trailing edge of the vertical stabilizer. With input from the rudderpedals, the rudder induces Aerodynamic changes that cause the aircraft to yaw along the vertical axis.
The elevators are located on the ______________ of the ________________. With input from the control column, Elevators Induce aerodynamic changes that cause the aircraft to _________ along the lateral axis.
The elevators are located on the trailing edges of the horizontal stabilizer. With input from the control column, Elevators Induce aerodynamic changes that cause the aircraft to pitch along the lateral axis.
Trim tabs are _______________ located on the trailing edges of the ailerons, elevators, and rudder. With input from ______________ controls in the cockpit, they cause minute changes in the desired direction.
Trim tabs are small airfoils located on the trailing edges of the ailerons, elevators, and rudder. With input from trim tab controls in the cockpit, they cause minute changes in the desired direction.
The leading edge flaps (Krueger flaps) are located ______________ and trailing edge flaps on the trailing edges of the ____________ . They are high lift devices that increase wing lift and decrease stall speed during ___________________
The leading edge flaps (Krueger flaps) are located inboard of the engines and trailing edge flaps on the trailing edges of the mid and inner wings. They are high lift devices that increase wing lift and decrease stall speed during takeoff, low speed maneuvering and landing.
The leading edge slats, located ___________ of the engines, are ___________ devices that _________ and _________________ during takeoff, low-speed maneuvering and landing.
The leading edge slats, located outboard of the engines, or highlift devices that increase wing lift and decreased stall speed during takeoff, low-speed maneuvering and landing.
