Phase III Block I

Question 1

Ensure the ______________ and T/Rs are closed or removed before extension of the _______ and leading _____ and _______.

Answer 1

Ensure the onboard fan duct cowling and T/Rs are closed or removed before extension of the Krueger Flaps and leading flaps and slats.

Question 2

__________ exit door swings out and up if opening from the outside, hold your _______________ while opening.

Answer 2

Over wing exit door swings out and up if opening from the outside, hold your knee against the door while opening.

Question 3

Don’t open service doors when __________________ is visible. Warning that __________ is installed and the slide will automatically deploy.

Answer 3

Don’t open service doors when orange warning flag is visible. Warning that Girt Bar is installed and the slide will automatically deploy.

Question 4

The fuselage is a _____________[__ component which provides _________ and __________________ compartments containing:

____________
_____________
Safety devices for ____________________

Answer 4

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

Question 5

The __________, ___________, and _____________ is attached to the fuselage

Answer 5

The wings, elevators, and rudder is attached to the fuselage

Question 6

The internal fuselage can be configured/rigged in three manners depending on mission requirements

Pax: ______________________
Combo: __________________
Cargo: ___________________

Answer 6

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

Question 7

The tail of the aircraft is made up of a _____________ and ____________ stabilizer.

Answer 7

The tail of the aircraft is made up of a horizontal and vertical stabilizer.

Question 8

The __________________ affects pitch control and reduces uncontrolled movement along lateral axis.

Answer 8

The Horizontal stabilizer affects pitch control and reduces uncontrolled movement along lateral axis.

Question 9

The __________________ affects yaw control along the vertical axis.

Answer 9

The vertical stabilizer affects yaw control along the vertical axis.

Question 10

The wings provide ____________ and _______________ for flight control surfaces and engines.

Answer 10

The wings provide lift and attachment points for flight control surfaces and engines.

Question 11

The winglets provide the potential benefits of lower operating costs by____________, _____________, and ___________________.

Answer 11

The winglets provide the potential benefits of lower operating costs by reducing fuel burn, improve payload capability, and increase range.

Question 12

Two ______________, one on each wing, are attached to the wings. They are the attachment structures connecting the engines to the wings and provide _______________ and ___________________________________.

Answer 12

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.

Question 13

The ______________ is the aerodynamic cone on the forward fuselage. It covers the _______________ and additional ______________.

Answer 13

The radome is the aerodynamic cone on the forward fuselage. It covers the radar dish and additional avionics.

Question 14

The Radome provides ________________ and ________________________.

Answer 14

The Radome provides aerodynamic properties and protection of engine related components.

Question 15

There are ____________ doors/hatches used for normal maintenance and egress ___________________________

Answer 15

There are six door/hatches used for normal maintenance and egress (FWD pass, FWD Galley SVC, overwing(2), AFT Pass, AFT Galley SVC)

Question 16

There are 5 main access doors/hatches __________________

Answer 16

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

Question 17

The control column is located in the cockpit. There are two _________ and are used for ___________ to control elevators.

Answer 17

The control column is located in the cockpit. There are two (pilot/1st officer) and are used for (push/pull) to control elevators.

Question 18

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

Answer 18

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

Question 19

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

Answer 19

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

Question 20

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.

Answer 20

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.

Question 21

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.

Answer 21

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.

Question 22

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.

Answer 22

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.

Question 23

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 ___________________

Answer 23

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.

Question 24

The leading edge slats, located ___________ of the engines, are ___________ devices that _________ and _________________ during takeoff, low-speed maneuvering and landing.

Answer 24

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.

Question 25

Four flights spoilers are located on the _____________ of each wing. These are used as _______________ to increase drag and reduce lift, both in flight and on the ground. The flight spoilers also supplement _____________ in response to control wheel commands.

Answer 25

Four flights spoilers are located on the upper surface of each wing. These are used as speedbrakes to increase drag and reduce lift, both in flight and on the ground. The flight spoilers also supplement roll control in response to control wheel commands.

Question 26

Two ground spoilers are located ______________ of the flight spoilers on the upper surface of each wing. The ground spoilers work with the flight spoilers as________________ when the aircraft is ____________ to increase drag and decrease speed.

Answer 26

Two ground spoilers are located outside of the flight spoilers on the upper surface of each wing. The ground spoilers work with the flight spoilers as speedbrakes when the aircraft is on the ground to increase drag and decrease speed.

Question 27

The two main landing gear struts _______________ and hold the airplane weight when the airplane is on the ground. The main landing gear also transmits the _________________ to the airplane structure.

Answer 27

The two main landing gear struts absorb landing forces and hold the airplane weight when the airplane is on the ground. The main landing gear also transmits the braking forces to the airplane structure.

Question 28

The airplane has _________ main landing gear and __________ nose gear.

Answer 28

The airplane has two main landing gear and a single nose gear.

Question 29

Each main gear is a conventional ________________ landing gear unit. The nose gear is a conventional ______________ wheel unit.

Answer 29

Each main gear is a conventional two wheel landing gear unit. The nose gear is a conventional steerable two wheel unit.

Question 30

Hydraulic power for retraction, extension, and nose wheel steering is normally supplied by hydraulic system ______________

Answer 30

Hydraulic power for retraction, extension, and nose wheel steering is normally supplied by hydraulic system A.

Question 31

Each main gear wheel has a _____________ hydraulic powered brake. The brake pedals provide ___________ of the left and right brakes.

Answer 31

Each main gear wheel has a multi-disk hydraulic powered brake. The brake pedals provide independent control of the left and right brakes.

Question 32

The main landing gear wheels are made of inner and outer _______________. _____________ hold the two halves together.

Answer 32

The main landing gear wheels are made of inner and outer wheel halves. Tie bolts hold the two halves together.

Question 33

The nose landing gear doors open to _________________ operation. They close to _________________ the nose landing gear well to ________________. They are attached to the _____________________ of the nose landing gear wheel well with hinges.

Answer 33

The nose landing gear doors open to permit gear operation. They close to aerodynamically seal the nose landing gear well to decrease drag. They are attached to the outboard edges of the nose landing gear wheel well with hinges.

Question 34

The nose wheel steering system supplies __________________ of the airplane. Steering inputs come from the ____________ or the ____________.

Answer 34

The nose wheel steering system supplies the ground directional control of the airplane. Steering inputs come from the steering wheel or the rudder pedals.

Question 35

The antiskid system controls the brake system to prevent _____________ during brake application. The auto brake system supplies _________________ to stop the airplane after the airplane lands or if a ____________occurs.

Answer 35

The antiskid system controls the brake system to prevent wheel skids during brake application. The auto brake system supplies metered brake pressure to stop the airplane after the airplane lands or if a rejected takeoff (RTO) occurs.

Question 36

The main deck cargo door is located ____________ of the _______________. It can be opened _______________________ to expedite loading and unloading of cargo.

Answer 36

The main deck cargo door is located aft of the foward passenger entry door. It can be opened hydraulically or manually to expedite loading and unloading of cargo.

Question 37

Four entry/service doors are located _________________.They are used for normal entrance and egress purposes.

Answer 37

Four entry/service doors are located forward and aft. They are used for normal entrance and egress purposes.