問題一覧
1
Aircraft flight control trim systems must be designed and installed so that the
Pilot can determine the relative position of the trim tab from the cockpit
2
Why is it generally necessary to jack an aircraft indoors for weighing?
So that air currents do not destabilize the scales
3
Which statement is correct concerning torque effect on helicopters?
Torque direction is the opposite of rotor blade rotation
4
The angle of incidence is that acute angle formed by
A line parallel to the wing chord and a line parallel to the longitudinal axis of the aircraft
5
In a hovering helicopter equipped with a tail rotor, directional control is maintained by
Varying the pitch of the tail rotor blades
6
If a pilot reports that an airplane flies left wing heavy, this condition may be corrected by
Increasing the angle of incidence of the left wing, or decreasing the angle of incidence of the right wing, or both
7
An airplane which has good longitudinal stability should have a minimum tendency to
Pitch
8
The purpose of spring tabs or servo tabs is to
Assist the pilot in moving the control surfaces
9
A reduction in anti-torque thrust will cause the
Tail to pivot in the direction of torque rotation around the main rotor axis
10
Stability about the axis which runs parallel to the line of flight is referred to as
Lateral stability
11
Where is the buttock line or buttline of an aircraft
A width measurement left or right of, and parallel to, the vertical centerline
12
If the vertical fin of a single-engine, propeller- driven airplane is rigged properly, it will generally be parallel to
The vertical axis but not the longitudinal axis
13
How are changes in direction of a control cable accomplished?
Pulleys
14
What is the smallest size cable that may be used in aircraft primary control systems?
1/8 inch
15
Which statement concerning the 100-hour inspection of an airplane equipped with a push-pull tube-type control system is true?
The threaded rod ends should be checked for the amount of thread engagement by means of the inspection hole provided
16
When the lift of an airfoil increases, the drag will
Also increase
17
If all instructions issued by the swaging tool manufacturer are followed when swaging a cable terminal, the resultant swaged terminal strength should be
The full rated strength of the cable
18
Where does the breakage of control cable wires occur most frequently?
Breakage usually occurs where cables pass over pulleys and through fairleads
19
If control cables are adjusted properly and the control surfaces tend to vibrate, the probable cause is
Worn attachment fittings
20
Other than the manufacturer maintenance manual what other document could be used to determine the primary flight control surface deflection for an imported aircraft that is reassembled after shipment?
Aircraft type certificate data sheet
21
The angle of incidence of an airplane at rest
Does not change when in flight
22
What nondestructive checking method is normally used to ensure that the correct amount of swaging has taken place when installing swaged-type terminals on aircraft control cable?
Use a terminal gauge to check the diameter of the swaged portion of the terminal
23
What is the purpose of the free-wheeling unit in a helicopter drive system?
It disconnects the rotor whenever the engine stops or slows below the equivalent of rotor RPM
24
Placing a piece of cloth around a stainless steel control cable and running it back and forth over the length of the cable is generally a satisfactory method of
Inspecting for broken strands
25
When inspecting a control cable turnbuckle for proper installation, determine that
The safety wire ends are wrapped a minimum of four turns around the terminal end shanks
26
The vertical flight of a helicopter is controlled by
Collective pitch changes
27
Movement of the cockpit control toward the nosedown position during a ground operational check of the elevator trim tab system will cause the trailing edge of the trim tab to move in which direction?
Upward regardless of elevator position
28
As the angle of attack of an airfoil increases, the center of pressure will
Move toward the leading edge
29
Main rotor blades that do not cone by the same amount during rotation are said to be out of
Track
30
Which should be accomplished before jacking an aircraft?
Install critical stress panels or plates
31
The acute angle formed by the chord line of a wing and the relative wind is known as the
Angle of attack
32
The auxiliary (tail) rotor of a helicopter permits the pilot to compensate for and/or accomplish which of the following?
Torque and directional control
33
When a fiber or nylon insert-type, self-locking nut can be threaded on a bolt or stud through the insert with only the fingers, it should be
Rejected
34
The universal propeller protractor can be used to measure
Degrees of flap travel
35
If the right wing of a monoplane is improperly rigged to a greater angle of incidence than designated in the manufacturer’s specifications, it will cause the
Airplane to be off balance both laterally and directionally
36
One purpose of the freewheeling unit required between the engine and the helicopter transmission is to
Automatically disengage the rotor from the engine in case of an engine failure
37
The cable-operated control system of an all-metal aircraft, not incorporating a temperature compensating device, has been rigged to the correct tension in a heated hangar. If the aircraft is operated in very cold weather, the cable tension will
Decrease when the aircraft structure and cables become cold
38
A universal propeller protractor used to measure the degrees of aileron travel should be zeroed
With the aileron in the NEUTRAL position
39
Excessive wear on both of the sides of a control cable pulley groove is evidence of
Pulley misalignment
40
The correct dihedral angle can be determined by
Using a dihedral board and bubble level along the front spar of each wing
41
An airplane is controlled directionally about its vertical axis by the
Rudder
42
Rigging and alignment checks should not be undertaken in the open; however, if this cannot be avoided, the aircraft should be positioned
With the nose into the wind
43
The vast majority of aircraft control cables are terminated with swaged terminals, that must be
Checked with a go-no-go gauge before and after, to show compliance with manufacturer’s requirements after the swaging operation
44
What physical factors are involved in the aspect ratio of airplane wings?
Span and chord
45
What type of flap system increase the wing area and changes the wing camber?
Fowler flaps
46
Very often, repairs to a control surface require static rebalancing of the control surface. Generally, flight control balance condition may be determined by
The behavior of the trailing edge when the surface is suspended from its hinge points
47
Fairleads should never deflect the alignment of a cable more than
3°
48
Proper wing twist in a sheet metal constructed wing can usually be checked by utilizing
Bubble level and special fixtures described by the manufacturer
49
The elevators of a conventional airplane are used to provide rotation about the
Lateral axis
50
When used in close proximity to magnetic compasses, cotter pins are made of what material?
Corrosion resisting steel
51
An airplane’s center of lift is usually located aft of its center of gravity
So that the airplane will have a nose-heavy tendency
52
The purpose of wing slats is to
Reduce stalling speed
53
Movement about the longitudinal axis (roll) in a helicopter is affected by movement of the
Cyclic pitch control
54
A tension regulator in the flight control cable system of a large all-metal aircraft is used primarily to
Retain a set tension
55
The purpose of the vertical fin is to provide
Directional stability
56
The primary purpose of stall strips is to
Stall the inboard portion of the wings first
57
If the travel of an airplane’s controls is correct but the cables are rigged exceptionally tight, what probable effect will this have when flying the airplane?
The airplane will be heavy on the controls
58
Where would you find precise information to perform a symmetry alignment check for a particular aircraft?
Aircraft service or maintenance manual
59
Wing dihedral, a rigging consideration on most airplanes of conventional design, contributes most to stability of the airplane about its
Longitudinal axis
60
A helicopter in forward flight, cruise configuration, changes direction by
Tilting the main rotor disk in the desired direction
61
With which system is differential control associated?
Aileron
62
Movement about the lateral axis (pitch) in a helicopter is effected by movement of the
Cyclic pitch control
63
Which is an acceptable safety device for a castle nut when installed on secondary structures?
Cotter pin
64
The purpose in checking main rotor blade tracking is to determine the
Relative position of the blades during rotation
65
An airplane that has a tendency to gradually increase a pitching moment that has been set into motion has
Poor longitudinal stability
66
Improper rigging of the elevator trim tab system will affect the balance of the airplane about its
Lateral axis
67
If a single-rotor helicopter is in forward horizontal flight, the angle of attack of the advancing blade is
Less than the retreating blade
68
Buffeting is the intermittent application of forces to a part of an airplane. It is caused by
An unsteady flow from turbulence
69
The dihedral angle of a wing may be measured by placing a straightedge and level protractor on the
Front spar
70
Where is fuselage station No. 137 located?
137 inches aft of the zero or fixed reference line
71
Washing-in the left wing of a monoplane, for purposes of rigging corrections after flight test, will have what effect on the lift and drag of that wing?
Both drag and lift will increase due to increased angle of attack
72
During inspection of the flight control system of an airplane equipped with differential-type aileron control, side-to-side movement of the control stick will cause
Each aileron to have a greater up travel (from the streamlined position) than down travel
73
In rotorcraft external-loading, the ideal location of the cargo release is where the line of action passes
Through the center of gravity at all times
74
If the control stick of an aircraft with properly rigged flight controls is moved rearward and to the left, the right aileron will move
Down and the elevator will move up
75
Movement of an airplane along its lateral axis (roll) is also movement
Around or about the longitudinal axis controlled by the ailerons
76
Differential control on an aileron system means that
The up travel is more than the down travel
77
After repairing or re-covering a rudder, the surface should be rebalanced
To manufacturer’s specifications
78
The chord of a wing is measured from
Leading edge to trailing edge