SYSTEM LIMITATIONS

Question 1

SYSTEM LIMITATIONS

1. Operation of pitot-static and AOA heat on
   the ground is limited to ___ minutes.

Answer 1

SYSTEM LIMITATIONS

1. Operation of pitot-static and AOA heat on
   the ground is limited to two minutes.

Question 2

SYSTEM LIMITATIONS

2. The maximum demonstrated fuel imbalance
   for emergency return following a fuel system
   malfunction is ___ pounds.

Answer 2

SYSTEM LIMITATIONS

2. The maximum demonstrated fuel imbalance
   for emergency return following a fuel system
   malfunction is 600 pounds.

Question 3

SYSTEM LIMITATIONS

3. The maximum field elevation for engine
   starting (any source of electrical power) is
   ________ feet.

Answer 3

SYSTEM LIMITATIONS

3. The maximum field elevation for engine
   starting (any source of electrical power) is
   14,000 feet.

Question 4

SYSTEM LIMITATIONS

4. The maximum permitted altitude for
   extension of flaps and/or landing gear is
   _____.

Answer 4

SYSTEM LIMITATIONS

4. The maximum permitted altitude for
   extension of flaps and/or landing gear is
   FL180.

Question 5

SYSTEM LIMITATIONS

5. The maximum permitted fuel imbalance for
   normal operations is:

___ pounds.

Answer 5

SYSTEM LIMITATIONS

5. The maximum permitted fuel imbalance for
   normal operations is:

200 pounds.

Question 6

SYSTEM LIMITATIONS

6. The maximum permitted landing gear
   operating speed is:

_____ KIAS.

Answer 6

SYSTEM LIMITATIONS

6. The maximum permitted landing gear
   operating speed is:

200 KIAS.

Question 7

SYSTEM LIMITATIONS

7. The minimum allowable battery voltage for
   battery start of an engine is:

___ volts.

Answer 7

SYSTEM LIMITATIONS

7. The minimum allowable battery voltage for
   battery start of an engine is:

24 volts.

Question 8

SYSTEM LIMITATIONS

8. The minimum allowable height for use of the
   autopilot during a non-precision approach is:
   ____ feet AGL.

Answer 8

SYSTEM LIMITATIONS

8. The minimum allowable height for use of the
   autopilot during a non-precision approach is:
   350 feet AGL.

Question 9

SYSTEM LIMITATIONS

9. The minimum allowable speed for sustained
   flight in icing (except approach and landing) is:

____ KIAS.

Answer 9

SYSTEM LIMITATIONS

9. The minimum allowable speed for sustained
   flight in icing (except approach and landing) is:

180 KIAS.

Question 10

SYSTEM LIMITATIONS

10. The minimum allowable temperature for tail
    deice boot operation is:

____°C RAT.

Answer 10

SYSTEM LIMITATIONS

10. The minimum allowable temperature for tail
    deice boot operation is:

-35°C RAT.