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WorksheetsREVIEWER APH : OTEP
Total questions: 56
Worksheet time: 42mins
The overall purpose of primary and intermediate flight training, as outlined in the Airplane Flying Handbook, is ______
the exercise of sound judgement that results in optimal operational safety and efficiency
the ability to operate an airplane with competence and precision both on the ground and in the air
to have a sound acquaintance with the principles of flight
the acquisition and honing of basic airmanship skills
It is any occurrence at an airport involving an aircraft, vehicle, person, or object, on the ground that creates a collision hazard or results in a loss of separation with an aircraft taking off, landing or intending to land
Runway Incursion
Midair Collision
Stall
Runway incident
All are motor skill development that are more sensitive and necessary for operating an aircraft in a different environment, three dimensional except:
Coordination
airmanship
timing
all of the above
It is an aid to the memory and helps to ensure that critical items necessary for the safe operation of aircraft are not overlooked or forgotten
Flight Manual
flight script
airplane flying handbook
checklist
The direct cause of every stall
excessive angle of attack
inadequate airspeed
pilot error
high pitch altitude
What is the airspeed during Final Approach(Lipa;T41)?
85mph
90mph
95mph
100mph
What is the airspeed during Base Leg?
85mph
90mph
95mph
100mph
During landing, it is a slow, smooth transition from a normal approach attitude to a landing attitude; parallel to and a few inches above the runway.
touch down
level off
breaking the glide
round out
It is a condition of improved performance encountered when the airplane is operating very close to the ground
bernoullis effect
magnus effect
ground effect
fujiwara effect
The wind component, measured in knots, at 90° to the longitudinal axis of the runway
tailwind
crosswind
downind
upwind
It is when the wings are lifting the weight of the airplane off the surface. *
lift off
takeoff
landing
departure
This is where safe flight begins and ends. *
Ground Operations
careful visual inspection of the airplane
thorough flight briefing
It is the first stage of delamination of the plastic of windshields and side windows. Small fractures in aircraft windshields and windows caused from being exposed to the ultraviolet rays of the sun and temperature extremes
cracks
fissures
crazing
crevices
WHICH AVGAS IS DYED BLUE?
80/87
100LL
100/130
Jet A1
Generally recommended RPM setting immediately following engine start. *
800 RPM
Throttle Idle
1000 RPM
1200 RPM
Engines certificated for AVGAS grades 80/87 or 91/96 will run satisfactorily on 100LL
false
true
false
very true
Avoid continuous starter operation for periods longer than 30 seconds without a cool down period of at least 30 seconds to 1 minute
true
false
It is the controlled movement of the airplane under its own power while on the ground.
cruising
taxiing
rolling
diving
There are four fundamental basic flight maneuvers upon which all flying tasks are based: straight-and level flight, turns, take-offs, and landings.
true
false
true
false
The ability to sense a flight condition, such as straight-and-level flight or a dive, without relying on instrumentation.
Kinesthesis
Feel of the Airplane
Proprioception
feeling in love
It is the angle formed between the airplane’s longitudinal axis, which extends from the nose to tail of the airplane, and the natural horizon.
pitch attitude
bank attitude
mental attitude
angular difference
What is IMC stands for?
instrument meteological condition
instrument meteorological condilion
instrument meteorological condition
instrumen meterological conditiooms
Airplane attitude control is composed of
Pitch Control and Bank Control
Power Control and Trim Control
Yaw Control and Instrument Control
Pitch Control Bank Control,Power Control and Trim Control,
50% of time, the pilot's attention should be outside the flight deck. And the other 50% of pilot's attention should be inside the flight deck.
true
false
Flight in which heading and altitude are maintained *
balance and steady flight
straight and level flight
steady flight
maintained flight
It is used in airplanes to null the pressure exerted by the pilot on the pitch flight control
Vertical Stabilizer
Flaps
Horizontal Stabilizer
Elevator Trim
It is initiated by banking the wings in the desired direction of the turn through the pilot’s use of the aileron flight controls
Turn
Yaw
Pitch
Wigwag
It means best rate of climb
Vy
Vx
Vu
Vw
As pitch attitude is increased, the center of thrust from the propeller moves to the right and becomes asymmetrical. This asymmetric condition is often called____.
Adverse Yaw
Magnus Effect
P" Factor
Slip Stream Effect
Level-off should begin at approximately 10 percent of the rate of climb
false
true
true
true
It is a basic maneuver in which the airplane loses altitude in a controlled descent with little or no engine power.
Glide
Descending turn
Power Letdown
Emergency Descend
In a constant power setting of an aircraft, when altitude increases, airspeed decreases.
true
false
When energy is exchanged, altitude and airspeed always change in opposite directions.
true
false
To trade speed for altitude, pitch down
true
false
To trade altitude for speed, pitch up.
true
false
Unintentionally descending below the desired glideslope on final approach to landing and failing to make the proper correction. To bring the airplane back to the desired glideslope, what should the pilot do?
pitch up
power up
pitch up and power up
glide
An event that unintentionally exceeds the parameters normally experienced in flight or training.
Vertigo
Upset
Loss of Control in Flight
Unusual Attitude
The top four causal and contributing factors that have led to an upset and resulted in LOC-I accidents are the following except:
Mechanical Factors
organizational factors
Environmental Factors
Stall-related Factors
It is an unexpected event that violates a pilot’s expectations and can affect the mental processes used to respond to the event. *
Startle
Upset
Surprise
Spatial Disorientation
. It occurs whenever the pilot is proactively correcting for yaw effects associated with power (engine/propeller effects), aileron inputs, how an airplane reacts when turning. *
Slips
Coordinated Flight
Upset Recovery
Turns
It is the angle at which the chord of the wing meets the relative wind.
triangle
angle of attack
wing chord angle
corrective angle
Above a wing’s critical AOA, the flow of air separates from the upper surface and backfills, burbles, and eddies, which reduces lift and increases drag. This condition is called a _____
left turning tendency
stall
adverse yaw
low pressure
What is the airspeed during Slow Flight of T-41B/D? *
75 mph
80 mph
65 mph
70 mph
The objective of maneuvering in _____ is to develop the pilot’s ability to fly at low speeds and high AOAs
slow flight
straight and level flight
acrobatic flight
take off
It is when pilot makes an abrupt recovery after one stall and exceeds the critical AOA a second time.
power off stall
spiraling slipsteam
primary stall
secondary stall
It results in the airplane following a downward corkscrew path.
drag
spin
inversion stall
spiral slipstream
what is the stalling speed of t41
64 mph
67 mph
65 mph
66mph
it controls the airplane’s pitch attitude about the lateral axis by using the elevator to raise and lower the nose in relation to the natural horizon or to the airplane’s flight instrumentation
power control
pitch control
power control
trim control
what gives the greatest altitude gain in the shortest horizontal distance
best angle of climb
best rate of climb
angle of attack
airspeed
It is commonly referenced as an unintended or unexpected attitude in instrument flight
surprise
abrupt flight
upset
unusual attitude
It is the portion of the takeoff procedure during which the airplane is accelerated from a standstill to an airspeed that provides sufficient lift for it to become airborne.
climb
take off roll
ascend
rotate
What is the Vr (Rotating Speed) of T41 B/D?
65 mph
95 mph
50 mph
45 mph
Ground effect is negligible when height or altitude is equal to aircraft’s______
Height
Wings
Wingspan
AOA
is the future impact of a hazard that is not controlled or eliminated. It can be viewed as future uncertainty created by the hazard.
risk
danger
harm
safety
it determines the degree of risk and whether the degree of risk is worth the outcome of the planned activity.
damage worth calculation
risk assessment
risk degree assessment
damage risk assessment
What is the standard taxiing speed in Lipa?
8000-1200 rpm
1000-1400 rpm
1000 rpm - 1200 rpm
