Airframe

Question 1

Purpose of Hydraulic Fluid Contamination Analysis

Answer 1

Determining fluid containment level

Question 2

Purpose of tactical paint scheme

Answer 2

Lessen visual and photographic detection

Question 3

Purpose of NAVAIR 509

Answer 3

Prevent, control, repair corrosion

Question 4

Purpose of NAVAIR IETM

Answer 4

Support diagnostics, maintenance, repair of aircraft

Question 5

Three modes of wheel brake operation

Answer 5

Normal, emergency, parking

Question 6

Purpose of composite airframes material

Answer 6

Limit weight, increase strength, decrease effect of corrosion attack

Question 7

Temporary repair

Answer 7

Repair to allow aircraft to fly until a permanent repair is made

Question 8

One time flight repair

Answer 8

Repair made to fly aircraft to repair station (one time)

Question 9

Permanent repair

Answer 9

Made to meet or exceed strength of structure or component

Question 10

Radome

Answer 10

Covers radar and window for transmission and reception of radar signals

Question 11

Forward Fuselage

Answer 11

Front of aircraft (radome-canopy)

Question 12

Center fuselage

Answer 12

Main landing gear-AMAD and Intake ducts

Question 13

Aft fuselage

Answer 13

exhaust-engine-stabilators

Question 14

Wings

Answer 14

Provides lift

Question 15

Leading edge extension

Answer 15

added lift for high angles of attack

Question 16

Ailerons

Answer 16

Produces roll

Question 17

Leading Edge Flaps

Answer 17

Changes lift and produces roll

Question 18

Trailing Edge Flaps

Answer 18

Changes lift and aids in roll

Question 19

Stabilators

Answer 19

Produces Pitch and roll on tail end

Question 20

Rudders

Answer 20

Increase lift and stability and produce yaw

Question 21

LEX spoiler

Answer 21

Speed brake

Question 22

Hydraulic Systems

Answer 22

HS1- Provides hydraulic fluid pressure to flight controls

HS2-Primary or secondary source also supplies pressure to non flight control system

APU accumulator-Gas charge cylinder provides fluid pressure to APU
Switching valves- Backup hydraulic pressure to replace primary hydraulic pressure

Question 23

Landing gear

Answer 23

nose, main, wheel brakes, launch bar, arresting hook

Question 24

Electronic flight control system

Answer 24

two flight control computers, surface servo actuators, air data and inertial sensors and control sensors

Question 25

Emergency extension of landing gear

Answer 25

Supplied by APU and emergency brake to unlock landing gear