TM 1-1510-218-10
7A-4
Now, enter the graph at the OUTSIDE AIR
TEMPERATURE ~ C scale at +30 C. Trace up until
intersecting the 4000 feet PA line, trace horizontally to
the right until intersecting the REFERENCE LINE.
Because the intersecting point on the reference line is
below the 4.1% baseline, maintain the same relative
distance between the guidelines and trace up until
intersecting the 4.1% baseline. From that point, trace
down to read the maximum allowable takeoff weight in
order to achieve a single engine climb gradient of
4.1%.
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.
(10) Maximum 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 7A-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 1,325
pounds therefore, the Zero Fuel Weight (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.
Figure 7A-2. TOLD Card Back (Example
Completed)
(2) Transpose the pertinent information to
the front side of the TOLD card and complete it for the
departure.
f.
Performance Planning (Front of TOLD
Card). Refer to Figure 7A-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:
