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Worksheets

REVIEWER APH : OTEP

Total questions: 56

Worksheet time: 42mins

Name
Class
Date
1.

The overall purpose of primary and intermediate flight training, as outlined in the Airplane Flying Handbook, is ______ 

a)

the exercise of sound judgement that results in optimal operational safety and efficiency

b)

   the ability to operate an airplane with competence and precision both on the ground and in the air

c)

to have a sound acquaintance with the principles of flight

d)

the acquisition and honing of basic airmanship skills

2.

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

a)

Runway Incursion

b)

  Midair Collision

c)

Stall

d)

Runway incident

3.

All are motor skill development that are more sensitive and necessary for operating an aircraft in a different environment, three dimensional except:

a)

Coordination

b)

airmanship

c)

timing

d)

all of the above

4.

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 

a)

  Flight Manual

b)

flight script

c)

airplane flying handbook

d)

checklist

5.

The direct cause of every stall 

a)

excessive angle of attack

b)

inadequate airspeed

c)

pilot error

d)

high pitch altitude

6.

What is the airspeed during Final Approach(Lipa;T41)?

a)

85mph

b)

90mph

c)

95mph

d)

100mph

7.

What is the airspeed during Base Leg? 

a)

85mph

b)

90mph

c)

95mph

d)

100mph

8.

    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. 

a)

touch down

b)

level off

c)

breaking the glide

d)

round out

9.

It is a condition of improved performance encountered when the airplane is operating very close to the ground

a)

bernoullis effect

b)

magnus effect

c)

ground effect

d)

fujiwara effect

10.

     The wind component, measured in knots, at 90° to the longitudinal axis of the runway 

a)

tailwind

b)

crosswind

c)

downind

d)

upwind

11.

It is when the wings are lifting the weight of the airplane off the surface. *

a)

lift off

b)

takeoff

c)

landing

d)

departure

12.

This is where safe flight begins and ends. *

a)

Ground Operations

b)

careful visual inspection of the airplane

c)

thorough flight briefing

13.

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

a)

cracks

b)

fissures

c)

crazing

d)

crevices

14.

WHICH AVGAS IS DYED BLUE?

a)

 80/87

b)

100LL

c)

100/130

d)

Jet A1

15.

Generally recommended RPM setting immediately following engine start. *

a)

800 RPM

b)

Throttle Idle

c)

1000 RPM

d)

1200 RPM

16.

Engines certificated for AVGAS grades 80/87 or 91/96 will run satisfactorily on 100LL

a)

false

b)

true

c)

false

d)

very true

17.

Avoid continuous starter operation for periods longer than 30 seconds without a cool down period of at least 30 seconds to 1 minute 

a)

true

b)

false

18.

It is the controlled movement of the airplane under its own power while on the ground. 

a)

cruising

b)

taxiing

c)

rolling

d)

diving

19.

There are four fundamental basic flight maneuvers upon which all flying tasks are based: straight-and level flight, turns, take-offs, and landings. 

a)

true

b)

false

c)

true

d)

false

20.

The ability to sense a flight condition, such as straight-and-level flight or a dive, without relying on instrumentation. 

a)

Kinesthesis

b)

Feel of the Airplane

c)

Proprioception

d)

feeling in love

21.

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. 

a)

pitch attitude

b)

bank attitude

c)

mental attitude

d)

angular difference

22.

What is IMC stands for? 

a)

instrument meteological condition

b)

instrument meteorological condilion

c)

instrument meteorological condition

d)

instrumen meterological conditiooms

23.

Airplane attitude control is composed of

a)

Pitch Control and Bank Control

b)

Power Control and Trim Control

c)

Yaw Control and Instrument Control

d)

Pitch Control Bank Control,Power Control and Trim Control,

24.

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. 

a)

true

b)

false

25.

Flight in which heading and altitude are maintained *

a)

balance and steady flight

b)

straight and level flight

c)

steady flight

d)

maintained flight

26.

It is used in airplanes to null the pressure exerted by the pilot on the pitch flight control 

a)

Vertical Stabilizer

b)

Flaps

c)

Horizontal Stabilizer

d)

Elevator Trim

27.

It is initiated by banking the wings in the desired direction of the turn through the pilot’s use of the aileron flight controls 

a)

Turn

b)

Yaw

c)

Pitch

d)

Wigwag

28.

It means best rate of climb

a)

Vy

b)

Vx

c)

Vu

d)

Vw

29.

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____.

a)

Adverse Yaw

b)

Magnus Effect

c)

P" Factor

d)

Slip Stream Effect

30.

Level-off should begin at approximately 10 percent of the rate of climb

a)

false

b)

true

c)

true

d)

true

31.

It is a basic maneuver in which the airplane loses altitude in a controlled descent with little or no engine power.

a)

Glide

b)

Descending turn

c)

Power Letdown

d)

Emergency Descend

32.

In a constant power setting of an aircraft, when altitude increases, airspeed decreases. 

a)

true

b)

false

33.

When energy is exchanged, altitude and airspeed always change in opposite directions. 

a)

true

b)

false

34.

To trade speed for altitude, pitch down 

a)

true

b)

false

35.

To trade altitude for speed, pitch up. 

a)

true

b)

false

36.

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? 

a)

pitch up

b)

power up

c)

pitch up and power up

d)

glide

37.

An event that unintentionally exceeds the parameters normally experienced in flight or training. 

a)

Vertigo

b)

Upset

c)

Loss of Control in Flight

d)

Unusual Attitude

38.

The top four causal and contributing factors that have led to an upset and resulted in LOC-I accidents are the following except: 

a)

Mechanical Factors

b)

organizational factors

c)

Environmental Factors

d)

Stall-related Factors

39.

It is an unexpected event that violates a pilot’s expectations and can affect the mental processes used to respond to the event. *

a)

Startle

b)

Upset

c)

Surprise

d)

Spatial Disorientation

40.

. 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. *

a)

Slips

b)

Coordinated Flight

c)

Upset Recovery

d)

Turns

41.

It is the angle at which the chord of the wing meets the relative wind.

a)

triangle

b)

angle of attack

c)

wing chord angle

d)

corrective angle

42.

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 _____ 

a)

left turning tendency

b)

stall

c)

adverse yaw

d)

low pressure

43.

What is the airspeed during Slow Flight of T-41B/D? *

a)

75 mph

b)

80 mph

c)

65 mph

d)

70 mph

44.

The objective of maneuvering in _____ is to develop the pilot’s ability to fly at low speeds and high AOAs

a)

slow flight

b)

straight and level flight

c)

acrobatic flight

d)

take off

45.

It is when pilot makes an abrupt recovery after one stall and exceeds the critical AOA a second time.

a)

power off stall

b)

spiraling slipsteam

c)

primary stall

d)

secondary stall

46.

It results in the airplane following a downward corkscrew path.

a)

drag

b)

spin

c)

inversion stall

d)

spiral slipstream

47.

what is the stalling speed of t41

a)

64 mph

b)

67 mph

c)

65 mph

d)

66mph

48.

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

a)

power control

b)

pitch control

c)

power control

d)

trim control

49.

what gives the greatest altitude gain in the shortest horizontal distance

a)

best angle of climb

b)

best rate of climb

c)

angle of attack

d)

airspeed

50.

It is commonly referenced as an unintended or unexpected attitude in instrument flight

a)

surprise

b)

abrupt flight

c)

upset

d)

unusual attitude

51.

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.

a)

climb

b)

take off roll

c)

ascend

d)

rotate

52.

What is the Vr (Rotating Speed) of T41 B/D?

a)

65 mph

b)

95 mph

c)

50 mph

d)

45 mph

53.

Ground effect is negligible when height or altitude is equal to aircraft’s______

a)

Height

b)

Wings

c)

Wingspan

d)

AOA

54.

is the future impact of a hazard that is not controlled or eliminated. It can be viewed as future uncertainty created by the hazard.

a)

risk

b)

danger

c)

harm

d)

safety

55.

it determines the degree of risk and whether the degree of risk is worth the outcome of the planned activity.

a)

damage worth calculation

b)

risk assessment

c)

risk degree assessment

d)

damage risk assessment

56.

What is the standard taxiing speed in Lipa?

a)

8000-1200 rpm

b)

1000-1400 rpm

c)

1000 rpm - 1200 rpm