The maximum allowable takeoff weight to
achieve a 4.1% single engine climb gradient is
12,600 pounds . Enter that weight in the appropriate
block on the TOLD card.
Allowable Takeoff Weight.
Enter the most restrictive weight from each column,
including the Max Wt For Req. SE CLB GRAD block,
in the appropriate space on the TOLD card. For Flaps
UP the weight is 12,600 pounds. Climb, one engine
inop is the most restrictive weight for this departure.
e. Completed TOLD (Back) and Decision
Making. Refer to Figure 7-2. The completed back
side of the TOLD card is now used for determining the
takeoff configuration (Flaps 0% or 40%) and the fuel
load in order to maintain the aircraft at the maximum
allowable weight for all of the conditions.
(1) For this example, the takeoff can be
accomplished at an aircraft weight of 12,600 pounds
with the flaps UP or at APPROACH. This takeoff is
planned with Flaps UP at 12,600 pounds.
For this example, the aircraft Operating Weight is
9,300 pounds and the Load for the mission is
(Operating Weight plus the Load) is 10,625 pounds.
The takeoff weight of 12,600 pounds minus the zero
fuel weight of 10,625 pounds allows for 1,975 pounds
of fuel for the mission.
(2) Transfer the pertinent information to the
front side of the TOLD card and complete it for the
Performance Planning (Front of TOLD
Card). Refer to Figure 7-3. The front side of the
TOLD card is used to record the critical information for
conduct of the takeoff and, in the event of an
emergency during the takeoff, landing data for an
immediate return to the departure airport. The
instructions here are consistent with the ATM.
Complete the front side of the card as follows:
(1) thru (5) were determined on the back
side of the card and transposed to these blocks.
(6) Minimum Takeoff Power. Use Figure
7-17, Minimum Takeoff Power at 2000 RPM with Ice
Vanes Retracted (65 Knots) or Figure 7-18, Minimum
Takeoff Power with Ice Vanes Extended (65 Knots).
Figure 7-2. TOLD Card Back (Example Completed)