W & B - Partial answers only

Given the following conditions, what is the maximum payload the aircraft can carry without exceeding a weight limitation? / Basic Operating Weight: 120,100 pounds / Maximum Zero Fuel Weight: 164,400 pounds / Maximum Takeoff Weight: 185,600 pounds / Fuel load: 40,800 pounds

24,700 pounds.

(Refer to figure 432.) With an actual runway length of 7,000 feet, and 5 knots of headwind, the Reference A is

2.2

(Refer to figures 297 and 450.) With a reported temperature of 0°C, Flaps 8, 0.5% upslope, calm winds at takeoff, and a weight of 82,300 pounds, the V1mbe is

166 knots.

(Refer to figures 321 and 458.) With a reported temperature of 10°C, a 1.2% downslope, and 5 knots of headwind, the maximum permissible quick turn-around landing weight is

81,000 pounds.

Dispatch has provided you with performance data based on actual aircraft takeoff weight and current weather conditions. You notice that the Vmcg speed is less than the V1 speed. You should

continue since the relationship between Vmcg speed and V1 speed is safe and normal.

(Refer to figures 273 and 474.) At 45°C and a weight of 52,000 pounds, the first segment takeoff gross climb gradient is

0.043%.

Given the following conditions, calculate the maximum payload: / Maximum Takeoff Weight: 184,200 pounds / Maximum Landing Weight: 142,000 pounds / Maximum Zero Fuel Weight: 138,000 pounds / Basic Operating Weight: 100,500 pounds / Fuel (onboard): 50,000 pounds / Fuel Capacity: 54,000 pounds

33,700 pounds.

(Refer to appendix 2, figure 44.) Where is the new CG if the weight is shifted from the forward to the aft compartment under Loading Conditions WS-5?

+19.15 index arm.

(Refer to appendix 2, figure 44.) Where is the new CG if the weight is removed from the aft compartment under Loading Conditions WS-4?

+8.50 index arm.

(Refer to figure 459.) With a payload of 14,200 pounds, maximum still air range is

1,840 NM.

(Refer to figure 432.) With an actual runway length of 8,000 feet, and 5 knots of tailwind, the Reference A is

2.26

(Refer to figure 469.) With an OAT of -15°C, altitude 15,000 MSL, and IAS of 170 kts, the maximum continuous power torque setting is

81%.

Given the following conditions, what is the maximum payload the aircraft can carry without exceeding a weight limitation? / Basic Operating Weight: 174,700 pounds / Maximum Zero Fuel Weight: 240,600 pounds / Maximum Takeoff Weight: 263,900 pounds / Fuel load: 58,000 pounds

31,200 pounds.

(Refer to appendix 2, 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.

(Refer to appendix 2, figure 44.) What is the new CG if the weight is shifted from the aft to the forward compartment under Loading Conditions WS-4?

23.5 percent MAC.

Departure procedures are based on what aircraft operating conditions?

All engines operating.

(Refer to figure 440.) With a reference A of 2.2 and a reference B of 33.9, takeoff weight is limited to

78,500 pounds.

(Refer to figures 297 and 485.) At a weight of 57,500 pounds, flaps 10° degrees, an 8 knot headwind, and a 0.5% downslope, the landing distance is

3,150 feet.

(Refer to figure 460.) At a weight of 73,500 pounds and a landing elevation below 5,000 MSL, Vref is

139 knots.

(Refer to figures 373 and 473.) With a reported temperature of 30°C, the maximum permissible takeoff weight is

65,100 pounds.

(Refer to appendix 2, 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.

(Refer to figure 398.) With a field OAT of 20°C, inertial separator in normal, and gross weight 8,750 pounds, you calculate the climb gradient at 8,000 feet to be

330 feet/NM.

(Refer to appendix 2, figures 4, 7, 9, 10, and 11.) What is the CG in inches from datum under Loading Conditions AC-6?

Station 300.5.

(Refer to figures 340 and 457.) With a weight of 67,500 pounds, flaps 45, and calm winds, the Vref is

133 knots.

(Refer to figures 349 and 474.) At 40°C and a weight of 54,000 pounds, the first segment takeoff gross climb gradient is

0.040%.

(Refer to figure 457.) You are flying an approach at a landing gross weight of 74,000 pounds when ATC notifies you that the runway has just become wet due to a rain shower. What is the effect on Vref speed and landing distance?

Vref does not change and landing distance will increase.

Which condition has the effect of greatly reducing critical engine failure speed (V1) on transport category airplane?

Runway length.

(Refer to figure 428.) Given an outside air temperature of 0°C, an altimeter setting of 29.92, and an airport at sea level, what would the %N1 takeoff setting be?

87.4%.

Why is it so important to keep in mind zero fuel weight (ZFW)?

To limit load forces on the wing spars.

Given the following conditions, what is the maximum payload the aircraft can carry without exceeding a weight limitation? / Basic Operating Weight: 98,300 pounds / Maximum Zero Fuel Weight: 135,600 pounds / Maximum Takeoff Weight: 156,300 pounds / Fuel load: 28,900 pounds

29,100 pounds.

(Refer to appendix 2, figure 44.) What is the new CG if the weight is shifted from the forward to the aft compartment under Loading Conditions WS-1?

33.8 percent MAC.

(Refer to figures 310 and 439.) At 0°C, with packs on, and wing and cowl anti-ice on, reference B is

36.4

(Refer to figure 459.) With a payload of 21,200 pounds, maximum still air range is

1,290 NM.

(Refer to figure 440.) With a reference A of 2.5 and a reference B of 30.5, takeoff weight is limited to

75,000 pounds.

(Refer to figure 457.) You are flying an approach at a landing gross weight of 74,000 pounds when ATC notifies you of a 10 knot increase in headwind. What is the effect on Vref speed?

Vref does not change.