Questões ATP_pag203

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702. (Refer to Figures 405 through 416.) (Note: Applicants may request a printed copy of
the chart(s) or graph(s) for use while computing the answer. All printed pages must be
returned to test proctor.) With the load weights shown in figure 414, you fill the fuel
tanks to the maximum fuel to remain under maximum gross weight and compute the
center of gravity. Your computations indicate
 A. at a CG of 200.1, your loading is satisfactory for flight operations.
 B. at a CG of 180.19, you need to redistribute your loads.
 C. at a CG of 190.27, you only need to change the cargo pod loading.
1. On Figure 405, note the maximum gross weight of 8,785 pounds.
2. On Figure 410, note the 200 pound pilot yields a 27.1 moment.
3. Using Figure 411, using maximum fuel at a weight of 2,224 pounds, the moment is
451.7.
4. On Figure 414, using the pilot weight of 200 pounds and 27.1 moment, and the fuel
of 2,224 and moment of 451.7, the calculated ramp weight is 7,429 pounds. Adding all
the moments together yields 1408.2.
5. The CG is calculated by taking the total moment (1408.2 X 1000) and dividing by
aircraft weight. 14,082,000 / 7,429 pounds equals 189.6.
6. On figure 415, note the aircraft is out of CG, but can be brought into CG by
changing the cargo pad loading.
703. (Refer to Figures 53 and 55.) What is the STAB TRIM setting for Operating Conditions
R-3?
 A. 3 ANU.
 B. 4-1/2 ANU.
 C. 5 ANU.
CG (inches aft of LEMAC) = 665.2" - 625.0" = 40.2"
CG (% of MAC) = 40.2" ÷ 134.0" = 30.0%
Stab Trim = 3 ANU
704. What is the maximum allowable weight that may be carried on a pallet which has the
dimensions of 42.6 x 48.7 inches?
Floor load limit - 117 lb/sq ft
Pallet weight - 43 lb
Tiedown devices - 31 lb
 A. 1,611.6 pounds.
 B. 1,654.6 pounds.
 C. 1,601.6 pounds.
1. Determine the area. 42.6 x 48.7 ÷ 144 = 14.41 square feet.
2. Determine the floor load limit. 14.41 x 117 = 1,685.63 pounds.
3. Subtract the weight of the pallet and tiedown devices. 1,685.63 - 74 = 1,611.63
pounds.