CPE AMT GENERAL
The elevators of a conventional airplane are used to provide rotation about the :
Vertical axis
Longitudinal axis
Lateral axis
None of the above
An airplane is controlled directionally about its vertical axis by the:
Aileron
Elevator
Rudder
Flaps
The chord of a wing is measured from:
Leading edge to trailing edge
Wingtip to wingtip
Wing root to wing tip
None of the above
The purpose of the vertical fin is to provide
Lateral stablity
Longitudinal stability
Directional stability
Overall stability
The stresses that acts on an aircraft are;
Compression, tension , torsion , bending , shear
Compression , tension torsion combustion, ignition
Intake, compression, combustion, turbine, exhaust
Compressing, bending, shearing, shoring, mooring
If the control stick of an aircraft with properly rigged flight controls is moved rearward and to the left the right aileron will move:
Up and the elevator will move down
down and the elevator will move down
down and the elevator will move up
Up and the elevator will move up
The acute angle formed by the chord line of a wing and the relative wind is known as the:
Angle of incidence
Angle of attack
longitudinal dihedral angle
center of gravity
When the lift of an airfoil increases the drag will:
Decrease
Increase
Neither decrease or increase
Increase while the lift is changing but will return to its original value
The purpose of wing slats is to:
Reduce stalling speed
Reduce stalling speed
Increase speed on takeoff
. Increase lift
What is the smallest size cable that may be used in aircraft primary control system
1/16
3/32
1/8
5/32
The potential difference between two conductors which are insulated from each other is measured
Volt
Amperes
Coulombs
Ohms
What unit is used to express electrical power?
volt
Watt
Ampere
Coulombs
The useful load of an aircraft consist of the
Crew, usable fuel passenger and cargo
Crew, usable fuel, oil and fixed equipment
Crew, passengers, usable fuel, oil cargo and fixed equipment
All of the above
Which of the following can provide the empty weight of an aircraft if the aircraft’s weight and balance records become lost, destroyed or otherwise inaccurate?
Reweighing the aircraft
The applicable aircraft specification or type of certificate data sheet
The applicable flight manual or pilot’s operating handbook
The aircraft specification and manual
What type of measurement is used to designate the arm in weight and balance computation?
Distance
weight x distance
Weight
length and distance
What should be clearly indicates on the aircraft weighing form?
Minimum allowable gross weight
Weight of unusable fuel
Weighing points
Maximum gross weight
When dealing with weight and balance of an aircraft the term “maximum weight” is interpreted to mean the maximum
Weight and empty aircraft
Weight and the useful load
Authorized weight of an aircraft and its contents
Weight of the whole aircraft
When towing a large aircraft
A person should be in the cockpit to water for obstructions
person should be stationed at the nose, each wingtip and the empennage at all times
. A person should be in the cockpit to operate the brakes
A person should be at the side of the fuselage
When taxiing an airplane with a quartering frail wind the elevators and
Upwind aileron should be held in the up position
Upwind aileron should be held in the down position
Both ailerons should be kept in the neutral position
Only left aileron should be in the neutral position
When taxiing an aircraft, a flashing red light from the control tower means
stop and wait for a green light
Move clear of the runway/taxiway immediately
Return to starting point
Standby
When taxiing an aircraft, a flashing white light from the control tower means
Move clear of the runway/taxiway immediately
. Ok to proceed but use extreme cautions
Return to starting point
Stop and wait for the green light
A fuel that vaporizes too readily may cause
Hard starting
. Vapor lock
Engine failure
Detonation
Characteristics of aviation gasoline are
High heat value, high volatility
high heat value, low volatility
Low heat value , low volatility
Low heat value,high volatility
When an anodized surface coating is damaged in service, it can be partially restored by
Applying a thin coat of zinc chromate primer
Chemical surface treatment
Use of a suitable mild cleaner
Use dry chemical
A primary cause of intergranular corrosions is
Improper heat treatment
Improper application of primer
. Dissimilar metal contact
Lack of maintenance
. Corrosion should be removed from magnesium parts with a
. Stiff non metallic brush
Carborandum abrasive
Silicon carbide brush
Steel brush
Which of these materials is the most cathodic
Zinc
Stainless steel
2024 aluminum alloy
Magnesium
Where is the record of compliance with airworthiness directives or manufacturers service bulletins normally indicated ?
FAA from 337
Flight manual
Aircraft maintenance record d
Repair manual
When a 100 hour inspection is completed. If the separate maintenance records for the airframe power plants and propeller are maintained where is the entry for the inspection recorded?
In each record
In any one of the records
In the airframe record only
In the power plant record only
Who is responsible for making the entry in the maintenance record after an annual 100 hour or progressive inspection?
The owner or operation of the aircraft
The person approving or disapproving for return of service
The designee or inspector representing the FAA administrator
The certificated aircraft mechanic
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