12. PESO Y BALANCE SOLO CÁLCULOS

8697. (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. at a CG of 200.1, your loading is satisfactory for flight operations. at a CG of 180.19, you need to redistribute your loads. at a CG of 190.27, you only need to change the cargo pod loading.

8697-1. Given the following, what would be the maximum payload? Basic operating weight (BOW): 100,500 lbs. Maximum zero fuel weight: 138,000 lbs. Maximum landing weight: 142,000 lbs. Maximum takeoff weight: 184,200 lbs. Fuel load: 40,000 lbs. 43,700 lbs. 37,500 lbs. 29,700 lbs.

8697-2. What is the purpose of a zero fuel weight limitation?. To limit load forces on the wing spars with heavy fuselage loads. To limit load forces on the fuselage with a heavy wing fuel load. To prevent overstressing the landing gear during a hard landing.

8697-3. What adverse flight characteristics could result from operating an aircraft with the center of gravity (CG) beyond the published forward limitations?. The flight control forces may become very light. It could be difficult or impossible to flare for landing. It could be difficult or impossible to recover from a stall.

8697-4. What adverse flight characteristics could result from operating an aircraft with the center of gravity (CG) beyond the published aft limitations?. The flight control forces may become very heavy. It could be difficult to flare for landing. It could be impossible to recover from a stall.

8698. (Refer to Figures 405 through 416.) What is the CG in inches from datum under the following loading conditions? Basic empty weight ............................................ 5,005 Pilot................................................................... 185 Cargo Zone 1 .............................................................. 200 Zone 2 .............................................................. 240 Zone 3 .............................................................. 500 Zone 4 .............................................................. 400 Zone 5 .............................................................. 200 Zone 6 ................................................................ 50 Cargo Pod Zone A .................................................................. 0 Zone B .................................................................. 0 Zone C.................................................................. 0 Zone D.................................................................. 0 Fuel............................................................275 gallons. Station 202.6. Station 198.5. Station 205.6.

8699. (Refer to Figures 405 through 416.) What is the CG in inches from datum under the following loading conditions? Basic empty weight ............................................ 5,005 Pilot................................................................... 190 Front seat passenger........................................ 200 Cargo Zone 1 .............................................................. 180 Zone 2 .............................................................. 505 Zone 3 .............................................................. 198 Zone 4 .............................................................. 600 Zone 5 .................................................................. 0 Zone 6 ................................................................ 60 Cargo Pod Zone A .............................................................. 100 Zone B ................................................................ 80 Zone C.............................................................. 200 Zone D.............................................................. 180 Fuel............................................................180 gallons. 196.4 inches aft of datum. 200.4 inches aft of datum. 204.1 inches aft of.

8699-1. (Refer to Figure 419.) With the following condi- tions, would the airplane be in the approved weight and CG envelope for landing? CG location: 25% MAC Aircraft Weight: 74,000 lbs. No, the airplane is over the maximum approved landing weight. Yes, the airplane is within the approved weight and CG envelope. No, the airplane is below the maximum landing weight, but the CG is aft of limits.

8699-2. (Refer to Figure 419.) You are preparing for a flight, with the following planned loading at takeoff. Would the aircraft be within the approved weight limitations? Basic operating weight (including crew): 49,500 lbs. Passengers, baggage, and cargo: 20,850 lbs. Fuel weight: 9,500 lbs. Yes, the weight would be within limits. No, max zero fuel weight would be exceeded. No, the max takeoff weight would be exceeded.

8623. (Refer to Figures 53 and 55.) What is the STAB TRIM setting for Operating Conditions R-1?. 8 ANU. 7-5/8 ANU. 7-3/4 ANU.

8625. (Refer to Figures 53 and 55.) What is the STAB TRIM setting for Operating Conditions R-3?. 3 ANU. 4-1/2 ANU. 5 ANU.

8624. (Refer to Figures 53 and 55.) What is the STAB TRIM setting for Operating Conditions R-2?. 5-3/4 ANU. 7 ANU. 6-3/4 ANU.

8626. (Refer to Figures 53 and 55.) What is the STAB TRIM setting for Operating Conditions R-4?. 4-1/4 ANU. 4-1/2 ANU. 5 ANU.

8627. (Refer to Figures 53 and 55.) What is the STAB TRIM setting for Operating Conditions R-5?. 6-3/4 ANU. 8 ANU. 7-1/2 ANU.

8700. (Refer to Figures 405 through 416.) What is the old and new CG if 300 pounds of cargo is moved from Zone 2 to Zone 3 given the following conditions? Weight (lbs.) Basic empty weight ............................................ 5,005 Pilot................................................................... 190 Front seat passenger........................................ 200 Cargo Zone 1 .............................................................. 180 Zone 2 .............................................................. 505 Zone 3 .............................................................. 198 Zone 4 .............................................................. 600 Zone 5 .................................................................. 0 Zone 6 ................................................................ 60 Cargo Pod Zone A .............................................................. 100 Zone B ................................................................ 80 Zone C.............................................................. 200 Zone D.............................................................. 180 Fuel............................................................180 gallons. 200.2 and 198.6. 196.4 and 199.2. 200.4 and 202.

8578. (Refer to Figure 44.) What is the new CG if the weight is removed from the forward compartment under Loading Conditions WS 1?. 27.1 percent MAC. 26.8 percent MAC. 30.0 percent MAC.

8579. (Refer to Figure 44.) Where is the new CG if the weight is added to the aft compartment under Loading Conditions WS 2?. +17.06 index arm. +14.82 index arm. +12.13 index arm.

8580. (Refer to Figure 44.) What is the new CG if the weight is added to the forward compartment under Loading Conditions WS 3?. 11.4 percent MAC. 14.3 percent MAC. 14.5 percent MAC.

8581. (Refer to Figure 44.) Where is the new CG if the weight is removed from the aft compartment under Loading Conditions WS 4?. +15.53 index arm. +8.50 index arm. -93.51 index arm.

8582. (Refer to Figure 44.) What is the new CG if the weight is removed from the forward compartment under Loading Conditions WS 5?. 31.9 percent MAC. 19.1 percent MAC. 35.2 percent MAC.

8573. (Refer to Figure 44.) What is the new CG if the weight is shifted from the forward to the aft compartment under Loading Conditions WS. 15.2 percent MAC. 29.8 percent MAC. 30.0 percent MAC.

8574. (Refer to Figure 44.) What is the new CG if the weight is shifted from the aft to the forward compartment under Loading Conditions WS 2?. 26.1 percent MAC. 20.5 percent MAC. 22.8 percent MAC.

8575. (Refer to Figure 44.) What is the new CG if the weight is shifted from the forward to the aft compartment under Loading Conditions WS 3?. 29.2 percent MAC. 33.0 percent MAC. 28.6 percent MAC.

8576. (Refer to Figure 44.) What is the new CG if the weight is shifted from the aft to the forward compartment under Loading Conditions WS 4?. 37.0 percent MAC. 23.5 percent MAC. 24.1 percent MAC.

8577. (Refer to Figure 44.) Where is the new CG if the listed weight is shifted from the forward to the aft compartment under Loading Conditions WS 5?. +19.15 index arm. +13.93 index arm. -97.92 index arm.