Operating Limitations

Question 1

Normal thrust is the thrust obtained at _____ % RPM or _____oC EGT, whicheve occurs first.

Answer 1

98%, 630oC EGT. (TO 1T-38C-1TO: 5-2)

Question 2

Afterburner range (MIN AB – MAX AB) provides approx. ____ to ____ % thrust augmentation.

Answer 2

5-40% (TO 1T-38C-1TO: 5-2)

??????

Question 3

The maximum allowable airspeed is ____ knots equivalent airspeed. (TO 1T-38C-1TO: 5-2)

Answer 3

710 knots

Question 4

The maximum fuel imbalance display is +_____ pounds. (TO 1T-38C-1TO: 5-6)

Answer 4

+910 pounds

Question 5

Due to engine oil supply and pressure requirements, zero-g flight is restricted to ____ seconds and negative-g flight is restricted to ____ seconds. (TO 1T-38C-1TO: 5-8)

Answer 5

10 seconds, 30 seconds

Question 6

The landing rate of descent should not exceed ____ fpm (not in a crab) with less than 1700 pounds of fuel.

Answer 6

590 fpm. (TO 1T-38C-1TO: 5-11)

Question 7

The landing rate of descent should not exceed ____ fpm (not in a crab) with full fuel. (TO 1T-38C-1TO: 5-11)

Answer 7

340 fpm