Performance

Question 1

VMCG

Answer 1

1. Minimum takeoff weight.
2. Flaps set at 50 percent.
3. Maximum takeoff power set.
4. No. 1 engine failed with the propeller auto-feathered.
5. ATCS operating.
6. Maximum rudder deflection limited by 150 pounds of rudder pedal force or maximum rudder control surface
   deflection.
7. No nosewheel steering required.
8. Maximum lateral deviation from initial runway track of 30 feet.

Question 2

VMCA

Answer 2

1. Minimum flying weight.
2. Maximum takeoff power set.
3. No. 1 engine failed with the propeller auto-feathered.
4. ATCS operational.
5. Maximum rudder deflection limited by 150 pounds of rudder pedal force or maximum rudder control surface
   deflection.
6. Zero rudder trim.
7. A bank angle ≤5 degrees away from the failed engine. (As required to maintain heading).

Question 4

V1

Answer 4

• the maximum speed to which the aircraft can accelerate with engines at takeoff power and then stop within the remainder of the runway available.
• Two symmetrical engines in reverse
• One engine in ground idle
• One propeller feathered
• Maximum anti-skid braking.

Question 5

Increase in VMCA with wings level

Answer 5

• Flaps up - 23 kts
• Flaps 50 - 43 kts

Question 6

Increase in VMCA if a hyd system is lost

Answer 6

• De-Boosted - 36 kts
• Boosted - 20 kts

Question 7

Critical Field Length

Answer 7

The total runway distance required to accelerate on all engines to crit eng failure speed, experience a failure, then continue the takeoff or stop within the same distance.