Quantcast Takeoff Checklist - P-5530189

 

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JOINT ADVANCED MULTI-ENGINE T-44A
6.
PRIMARY GOVERNORS
"CHECKED" (P)
With N2 still set at 1900 RPM, P performs the following checks:
a.  Prop levers Move both aft. Stop when prop levers reach the detent. This will be felt as
increased resistance. Be careful not to allow prop levers to enter into the FEATHER position. If
FEATHER is inadvertently selected, bring the props forward immediately.
b.
N2 Stabilized between 1600-1800 RPM
c.
Prop levers Slowly full forward
d.
N2 Returns to approximately 1900 RPM
7.
AUTOFEATHER
"CHECKED" (P)
With power at 500 ft-lbs torque minimum, P performs the following checks:
a.
AUTOFEATHER switch TEST (down position)
Check both LH and RH AUTO FEATHER ARMED annunciator lights (green) on. If lights do not
come on, advance the power levers slightly.
b.  Left power lever Retard slowly. As torque reaches 410 + 50 ft-lbs, check RH AUTO
FEATHER ARMED annunciator light out. Continue retarding power lever toward idle. At 210-310
ft-lbs torque (260 + 50), check LH AUTO FEATHER ARMED annunciator light flashing. This
indicates the prop is feathering. After N2 decreases to 800 RPM, advance left power lever to 500 ft-
lbs torque and note both AUTO FEATHER ARMED annunciator lights on.
c.  Right power lever Retard slowly. As torque reaches 410 + 50 ft-lbs, check LH AUTO
FEATHER ARMED annunciator light out. Continue retarding power lever toward idle. At 210-310
ft-lbs torque (260 + 50), check RH AUTO FEATHER ARMED annunciator light flashing. This
indicates the prop is feathering. After N2 decreases to 800 RPM, retard both power levers to idle.
d.  AUTOFEATHER TEST switch Release after noting right prop feathering cycle terminated
and N2 increasing toward 900-1100 RPM.
9.
MANUAL FEATHER
"CHECKED" (P)
P performs the following checks:
a.
Power levers IDLE, N2 stabilized. (Power must be at idle).
b.  Prop levers FEATHER. Simultaneously pull both prop levers firmly aft, past the detent, to the
stops.
c.
N2 Note N2 decrease as props feather.
d.
Prop levers full forward after N2 decreases to 800 RPM.
e.
N2 Note N2 returns to 900-1100 RPM.
CP reports "Engine Runup Checklist complete."
TAKEOFF CHECKLIST
The Takeoff Checklist is designed to check the remaining systems and configure the aircraft for
takeoff.
1.
AUTOPILOT
"CHECKED, DISENGAGED" (P, CP)
P and CP perform the following checks:
a.
Annunciator lights Check
P rotates dim control fully counterclockwise (P's AP mode selector panel on pedestal) and ensures
lights illuminate on mode selector panel and flight director annunciator (above P's attitude gyro). P
directs CP to "check your lights" (by performing the same action on CP autopilot mode selector
E-10
COCKPIT PROCEDURES


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