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| T-45C TS & ADV BIFP-04
Basic Flight Maneuvers and Transitions
(2) Altitude
(3) Vertical velocity
c. Exit transition
(1) Pitch
(2) Altitude
(3) Vertical velocity
(4) RPM/fuel flow indicator
II. Constant rate climbs and descents
A. Constant rate climb
1. Procedure
a. Set power to 1,500 pph
b. Adjust nose to about 2-3 degrees noseup to
maintain 200 KIAS
c. Adjust power to maintain 1,000 fpm climb
d. Lead level-off at target altitude minus 10% of vertical
velocity
2. Control
a. Entry transition: establish 1,000 fpm rate of climb by
simultaneously advancing power and raising nose
b. In maneuver
(1) Control airspeed with adjustments to pitch
NOTE: Pitot static instruments contain lag
factors. Don't chase the vertical velocity with
pitch or power adjustments.
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(8-99) Original
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