Wayground logo

Free Printable Worksheets

Font size

S
M
L
XL
Worksheets

Stan/Eval Rehack

Total questions: 35

Worksheet time: 26mins

Name
Class
Date
1.

As soon as an anomaly occurs in flight, these are the four steps that you should verbalize verbatim to handle the situation (MATL)

(a)  

2.

What is the normal operating range of the T-41 cylinder head temperature?

(a)  

3.

105. During taxi, maintain at least ____ feet behind light single-engine aircraft and ____ feet behind

multi-engine or jet aircraft.

a)

A. 30; 60

b)

B. 100; 200

c)

C. 100; 500

d)

D. 50; 100

4.

106. (T-41) Do not exceed _____ degrees of bank in the pattern.

a)

20

b)

30

c)

45

d)

35

5.

If denied closed, offset go-around aircraft shall turn ____________ the departure end of the

runway away from the upwind leg to __________ .

a)

At 3/4 mile past; NAIL/SAW

b)

No later than; the 45 to initial point (for the opposite runway)

c)

At 1/2 mile past; NAIL/SAW

d)

At 1/2 mile past; intercept crosswind prior to NAIL/SAW

6.

Plan all T-41D missions to land with a minimum of __________ usable fuel remaining.

a)

20 minutes

b)

9 gallons

c)

2.5 gallons

d)

4 gallons

7.

(T-41) With a total loss of oil pressure, the propeller will go to _____ and will not be controllable

by the propeller control knob.

a)

A. Low pitch (high RPM)

b)

B. High pitch (low RPM)

c)

C. Flat pitch (zero thrust)

d)

D. Feather (minimum drag configuration)

8.

State each part of the check to ensure you are landing in a suitable field during a forced landing (SLOWW)

(a)  

9.

(T-41) If the suction gauge reads less than 1 inch Hg, the mission __________.

a)

Should be terminated

b)

May be continued if instrument conditions are not expected

c)

May be continued only if the attitude gyroscope is caged

d)

May be continued only if the attitude gyroscope continues to properly indicate pitch and

bank

10.

93. (T-41) Failure of the engine-driven vacuum pump will affect which flight instruments?

a)

Vertical velocity indicator, turn and bank, attitude indicator

b)

Attitude indicator, turn and bank, heading

c)

Attitude, heading, and vertical velocity indicator

d)

Attitude and heading indicators

11.

(T-41) Any time the engine is started, it should be run for at least ____ minutes prior to shutdown

to reduce condensation in the crankcase.

a)

5

b)

10

c)

3

d)

1

12.

(T-41) If a pilot chooses to perform a spark plug cleanout during the engine run-up, the procedure

may be performed _________.

a)

Once

b)

No more than twice

c)

Three times

d)

As many times as required

13.

Minimum horizontal spacing between aircraft in the KAFF pattern is ___________.

a)

500 feet or well clear

b)

1000 feet

c)

1500 feet

d)

1 statute mile

14.

State each part of the check to determine whether there is an engine fire (FEVER)

(a)  

15.

The minimum runway condition reading (RCR) for takeoff or landing is _______. Pilots will not

takeoff or land if the existing crosswind component exceeds the RCR.

a)

6

b)

10

c)

12

d)

15

16.

(T-41) Electrical energy is supplied by a ____ volt ____ current system powered by a 60 ampere

engine driven alternator.

a)

22; alternating

b)

14; pulse

c)

22; direct

d)

14; direct

17.

State each part of the check that you do prior to entry into USAFA training areas (FENCE)

(a)  

18.

(T-41) Normal operating range of the oil pressure is (a)   psi.

19.

(T-41) After an engine failure, if oil pressure is available and the propeller pitch is still controllable,

__________ will provide the optimum glide distance.

a)

Turning the battery half of the master switch OFF

b)

A flap setting of 20 degrees

c)

Setting the throttle to IDLE

d)

Pulling the propeller control knob to FULL DECREASE

20.

What are the five Fs to determine whether you should attempt to restart your engine?

(a)  

21.

(T-41) In the LOW position, the auxiliary fuel pump will switch to the alternate flow rate at a

throttle setting of approximately ____ RPM.

a)

1900

b)

2000

c)

2100

d)

2200

22.

The heading indicator is ___________.

a)

Electrically powered

b)

Mechanically driven by a flexible shaft connected to the oil pump

c)

Vacuum powered

d)

None of the above

23.

(T-41) The maximum gross weight (normal category) is _______lbs.

a)

2150 (2100 for 57L)

b)

2800 (2700 for 57L)

c)

2650 (2600 for 57L)

d)

2550 (2500 for 57L)

24.

The maximum density altitude for T-41D takeoffs above 2,350 pounds gross weight is _____.

a)

14,500

b)

12,500

c)

No limit

d)

9,500

25.

(T-51)!!!!!!!! What is the cylinder heads continuous operation temperature and maximum temperature?

(Format: continuous, maximum)

(a)  

26.

(T-51)!!!!!!!

What is minimum and emergency (usable) fuel in the T-51?

(Format: min fuel, emergency fuel)

(a)  

27.

(T-51)!!!!!!

What is the maximum gross weight in the T-51 (lbs)

(a)  

28.

(T-51!!!!!!!!!)

What is the normal operating range of the tachometer in the T-51?

(a)  

29.

(T-51!!!!!!!!)

What is the minimum idling oil pressure on the ground (PSI)?

(a)  

30.

What is the maximum airspeed in the T-41 (KIAS)?

(a)  

31.

State each part of the check that you do prior to maneuvers (CLEEF)

(a)  

32.

What is the normal operating range of the tachometer for the T-41 (RPM)?

(a)  

33.

If lightning or thunderstorms are reported within ___ nautical miles of the area of operation, pilots

will ensure the aircraft is not exposed to hail, lightning, windshear, or microbursts. (T-2). Units will

terminate operations when lightning is within ____ nautical miles. (AFMAN 11-2T-41-51-52-53v3 3.6.2)

a)

15,5

b)

5, 1

c)

10, 5

d)

20, 10

34.

What is the check that you should complete to maintain aircraft control in most emergencies? (TCCC)

(a)  

35.

You must complete at least one SFL every (a)   days to remain current