Stepper Motors & Rotor Control Quiz
- 1.The type of rotor control that is phased out during conversion from heli mode to acft mode is the?
- A.
Flaperons
- B.
Elevators
- C.
Rudders
- D.
Cyclic
- 2.How many pounds per square foot is the cabin floor limit load?
- A.
300
- B.
400
- C.
500
- D.
600
- 3.What windows are configured with explosive (fast burn) escape separators to provide emergency egress for the pilots?
- A.
Left/right windshields
- B.
Left/right side windows
- C.
Left/right cockpit windwos
- D.
Left/right look-down windows
- 4.The pilot and copilot seats adjust through a range of?
- A.
Five inches vertically and five inches longitudinally
- B.
Five inches vertically and three inches longitudinally
- C.
Seven inches vertically and five inches longitudinally
- D.
Seven inches vertically and three inches longitudinally
- 5.What configuration is flight ready with the nacelles rotated to the vertical position, and the wing rotated perpendicular to the fuselage?
- A.
FULL STOW
- B.
AIRPLANE
- C.
HELICOPTER
- D.
EMERGENCY WING STOW
- 6.Which digit of the four-digit numbering system identifies zones and areas with access provisions on the Osprey is a numerical identification of the panel/door within a zone?
- A.
First
- B.
Second
- C.
Third
- D.
Fourth
- 7.While both cabin doors have normal opening/closing mechanisms, what is the only door that is given emergency opening provisions?
- A.
Side
- B.
Upper
- C.
Lower
- D.
Escape
- 8.How many feet above the ground or deck are the rudders that are located on the rear of the edge of the vertical stabilizers?
- A.
7 to 10
- B.
10 to 15
- C.
11 to 17
- D.
11 to 20
- 9.All aircraft fuel servicing/defueling operations will be performed in accordance with local activities supplemental instructions and?
- A.
Naval Air Systems Command (NAVAIR) 00-80T-109
- B.
Technical Order (TO) 1V-22(C)B-1
- C.
NAVAIR A1-V22AC-MRC-000
- D.
TO 1V-22(C)B-6
- 10.What mode of operation does the ground refuel/defuel panel (GRDP) operate in?
- A.
NORMAL
- B.
REFUEL
- C.
OFF
- D.
ON
- 11.What system on the nose landing gear (NLG) provides the means to raise the nose of the nose of the aircraft during ground maintenance and towing of the aircraft?
- A.
Hike
- B.
Chamber
- C.
Elevation
- D.
Extension
- 12.What provides control and indication of the primary landing gear extension/retraction system and control of the emergency extension system in the event the primary system fails?
- A.
Drag strut/actuator
- B.
Gas control manifold (GCM)
- C.
Landing gear control unit (LGCU)
- D.
Emergency gear extension unit (EGEU)
- 13.How many degrees of steering authority left or right of center is provided by the nose wheel steering system while on the ground?
- A.
45
- B.
60
- C.
75
- D.
90
- 14.What parking brake component applies hydraulic pressure seperately to the main landing gear left and right wheels and brakes and retains hydraulic pressure for parking brake engagement?
- A.
Transfer module
- B.
1st stage relief valve
- C.
Master brake cylinders
- D.
Pressure reducer valve module
- 15.What independent hydraulic system(s) provide hydro power to the Osprey?
- A.
Auxiliary hydraulic power system
- B.
Hydraulic system 1 and 2 only
- C.
Main hydraulic power system
- D.
Hydraulic system 1, 2, and 3
- 16.What monitors the fluid level in the reservoirs for hydraulic systems 1, 2, and 3?
- A.
Hydraulic reservoir quantity multi-function display control layer
- B.
Hydraulic fluid level monitor (HFLM)
- C.
Fluid compensation valves
- D.
Remote switching valves
- 17.Hydraulic pump 1 delivers how many gallons per minute (GPM) of hydraulic fluid?
- A.
30 Helicopter and 30 airplane
- B.
34 Helicopter and 30 airplane
- C.
38 Helicopter and 32 airplane
- D.
44 Helicopter and 36 airplane
- 18.What components provide artificial feel forces and magnetic brake functions for the mehcanical flight controls?
- A.
Cockpit control thrust dirve actuators and cockpit control feel drive actuators
- B.
CCTDAs and cockpit control position transducers (CCPT)
- C.
CCPTs and thrust control levers (TCL)
- D.
CCFDAs and CCPTS
- 19.Which panel has the capability to activate and/or reset the automated flight control system (AFCS), adjust individual engine torque values, and engage backup hydraulic power drive units (HPDU) on the conversion actuators?
- A.
Flight control
- B.
Engine control
- C.
Backup flight control
- D.
Primary flight control
- 20.What component prevents inadvertent engine shutdown when the condition lever is moved from FLY to START position?
- A.
Nacelle waste gate
- B.
CRANK/START gate
- C.
CRANK/START lever
- D.
Rotor brake control lever
- 21.In what mode do the rotor hub flapping sensors correct excessive flapping?
- A.
AIRPLANE MODE
- B.
TRANSITION MODE
- C.
HELICOPTER MODE
- D.
Vertical short take-off and landing (VSTOL) MODE
- 22.What percentage of the max hinge movement required of the surface are the left, right, and center elevator servo actuators capable of supplying?
- A.
40
- B.
50
- C.
60
- D.
70
- 23.What hydraulic system powers each section of the swashplate actuators?
- A.
Sections A and B are powered by hydraulic system 1, while section C is powered by system 2
- B.
Sections A and B are powered by hydraulic system 2, while section C is powered by system 2
- C.
Sections A and B are powered by hydraulic system 1, while section C is powered by system 3
- D.
Sections A and B are powered by hydraulic system 2, while section C is powered by system 3
- 24.With the doors open, the cargo hook external doors must be latched open prior to flight when the speed will be above how many knots?
- A.
65
- B.
70
- C.
75
- D.
80
- 25.In knots, what is the max speed for flight with a latched open cargo door?
- A.
250
- B.
200
- C.
180
- D.
150
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