Aircraft Performance

(Refer to Figure 38.) GIVEN: Empty weight (oil is included) 1,271 lb Empty weight moment (in-lb/1,000) 102.04 Pilot and copilot 260 lb Rear seat passenger 120 lb Cargo 60 lb Fuel 37 gal Under these conditions, the CG is determined to be located. within the CG envelope. N/A. N/A.

(Refer to Figure 13.) GIVEN: Aircraft weight 3,400 lb Aircraft pressure altitude 6,000 ft Temperature at 6,000 feet 10 C Using a maximum rate of climb under the given conditions, how much fuel would be used from engine start to a pressure altitude of 16,000 feet?. 43 pounds. N/A. N/A.

(Refer to Figure 15.) GIVEN: Airport pressure altitude 4,000 ft Airport temperature 12 C Cruise pressure altitude 9,000 ft Cruise temperature -4 C What will be the distance required to climb to cruise altitude under the given conditions?. 8.5 miles. N/A. N/A.

With regard to the technique required for a crosswind correction on takeoff, a pilot should use. rudder as required to maintain directional control, aileron pressure into the wind, and higher than normal lift-off airspeed in both convetional- and nosewheel-type airplanes. N/A. N/A.

(Refer to Figure 14.) GIVEN: Aircraft Weight 3,400 lb Airport pressure altitude 4,000 ft Temperature at 4,000 feet 14 C Using a normal climb under the given conditions, how much time would be required to climb to a pressure altitude of 8,000 feet?. 5.5 minutes. N/A. N/A.

(Refer to Figure 35.) GIVEN: Temperature 50 F Pressure altitude Sea level Weight 3,000 lb Headwind 10 kts Determine the approximate ground roll. 636 feet. N/A. N/A.

GIVEN: Total weight 3,037 lb CG location station 68.8 Fuel consumption 12.7 GPH Fuel CG station 68.0 After 1 hour 45 minutes of flight time, the CG would be located at station. 68.83. N/A. N/A.

(Refer to Figure 3A.) What is the approximate glide distance if you are operating at 8,000 feet?. 12 NM. N/A. N/A.

(Refer to Figure 35.) GIVEN: Temperature 70 F Pressure altitude Sea level Weight 3,400 lb Headwind 16 kts Determine the approximate ground roll. 689 feet. N/A. N/A.

(Refer to Figure 35.) GIVEN: Temperature 85 F Pressure altitude 6,000 ft Weight 2,800 lb Headwind 14 kts Determine the approximate ground roll. 742 feet. N/A. N/A.

(Refer to Figure 8.) With 38 gallons of fuel aboard at cruise power (55 percent), how much flight time is available with night VFR fuel reserve still remaining?. 2 hours 34 minutes. N/A. N/A.

(Refer to Figure 34.) GIVEN: Pressure altitude 6,000 ft Temperature +13 C Power 2,500 RPM - 23´´ MP Usable fuel available 460 lb What is the maximum available flight time under the conditions stated?. 5 hours 12 minutes. N/A. N/A.

(Refer to Figure 15.) GIVEN: Airport pressure altitude 2,000 ft Airport temperature 20 C Cruise pressure altitude 10,000 ft Cruise temperature 0 C What will be the fuel, time, and distance required to climb to cruise altitude under the given conditions?. 5 gallons, 9 minutes, 13 NM. N/A. N/A.

(Refer to Figure 32.) GIVEN: Temperature 30 F Pressure altitude 6,000 ft Weight 3,300 lb Headwind 20 kts What is the total takeoff distance over a 50-foot obstacle?. 1,500 feet. N/A. N/A.

(Refer to Figure 8.) Determine the amount of fuel consumed during takeoff and climb at 70 percent power for 10 minutes. 2.88 gallons. N/A. N/A.

GIVEN: Total weight 4,137 lb CG location station 67.8 Fuel consumption 13.7 GPH Fuel CG station 68.0 After 1 hour 30 minutes of flight time, the CG would be located at station. 67.79. N/A. N/A.

(Refer to Figure 38.) GIVEN: Empty weight (oil is included) 1,271 lb Empty weight moment (in-lb/1,000) 102.04 Pilot and copilot 360 lb Cargo 340 lb Fuel 37 gal Will the CG remain within limits after 30 gallons of fuel has been used in flight?. Yes, the CG will remain within limits. N/A. N/A.

(Refer to Figure 11.) What would be the approximate true airspeed and fuel consumption per hour at an altitude of 7,500 feet, using 52 percent power?. 105 MPH TAS, 6.2 GPH. N/A. N/A.

(Refer to Figure 31.) If the tower-reported surface wind is 010 at 18 knots, what is the crosswinf component for a Rwy 08 landing?. 17 knots. N/A. N/A.

(Refer to Figure 9.) Using a normal climb, how much fuel would be used from engine start to 12,000 feet pressure altitude? Aircraft weight 3,800 lb Airport pressure altitude 4,000 ft Temperature 26 C. 58 pounds. N/A. N/A.

GIVEN: Weight A: 140 pounds at 17 inches aft of datum Weight B: 120 pounds at 110 inches aft of datum Weight C: 85 pounds at 2190 inches aft of datum Based on this information, the CG would be located how far aft of datum?. 96.89 inches. N/A. N/A.

An aircraft is loaded with a ramp weight of 3,650 pounds and having a CG of 94.0, approximately how much baggage would have to be moved from the rear baggage area at station 180 to the forward baggage area at station 40 in order to move the CG to 92.0?. 52.14 pounds. N/A. N/A.

(Refer to Figure 31.) What is the headwind component for a Rwy 13 takeoff if the surface wind is 190 at 15 knots?. 7 knots. N/A. N/A.

(Refer to Figure 8.) GIVEN: Fuel quantity 47 gal Power-cruise (lean) 55 percent Approximately how much flight time would be available with a night VFR fuel reserve remaining?. 3 hours 22 minutes. N/A. N/A.

(Refer to Figure 31.) The surface wind is 180 at 25 knots. What is the crosswind component for a Rwy 13 landing?. 19 knots. N/A. N/A.

GIVEN: Weight A: 135 pounds at 15 inches aft of datum Weight B: 205 pounds at 117 inches aft of datum Weight C: 85 pounds at 195 inches aft of datum Based on this information, the CG would be located how far aft of datum?. 100.2 inches. N/A. N/A.

What is the standard temperature at 20,000 feet?. -25 C. N/A. N/A.

(Refer to Figure 31.) Rwy 30 is beinfg used for landing. Which surface wind would exceed the airplane´s crosswind capability of 0.2 V(SO), if V(SO) is 60 knots?. 260 at 20 knots. N/A. N/A.

(Refer to Figure 35.) GIVEN: Temperature 80 F Pressure altitude 4,000 ft Weight 2,800 lb Headwind 24 kts What is the total landing distance over a 50-foot obstacle?. 1,125 feet. N/A. N/A.

The CG of an aircraft can be determined by which of the following methods?. Dividing total moments by total weight. N/A. N/A.

(Refer to Figure 32.) GIVEN: Temperature 100 F Pressure altitude 4,000 ft Weight 3,200 lb Wind Calm What is the ground roll required for takeoff over a 50-foot obstacle?. 1,350 feet. N/A. N/A.

(Refer to Figure 12.) GIVEN: Pressure altitude 18,000 ft Temperature -1 C Power 2,200 RPM - 20´´ MP Best fuel economy usable fuel 344 lb What is the approximate flight tiem available under the given conditions? (Allow for VFR day fuel reserve). 5 hours 59 minutes. N/A. N/A.

A proper crosswind landing on a runway requires that, at the moment of touchdow, the. direction of motion of the airplane and its longitudinal axis be parallel to the runway. N/A. N/A.

An airplane is loaded to a gross weight of 4,800 pounds, withe three pieces of luggage in the rear baggage compartment. The CG is located 98 inches aft of datum, which is 1 inch aft of limits. I luggage which weighs 90 pounds is moved from the rear baggae compartment (145 inches aft of datum) to the front compartment (45 inches aft of datum), what is the new CG?. 96.13 inches aft of datum. N/A. N/A.

(Refer to Figure 10.) Using a maximum rate of climb, how much fuel would be used from engine start to 10,000 feet pressure altitude? Aircraft weight 3,800 lb Airport pressure altitude 4,000 ft Temperature 30 C. 40 pounds. N/A. N/A.

When turbulence is encountered during the approach to a landing, what action is recommended and for wht primary reason?. Increase the airspeed slightly above normal approach speed to attain more positive control. N/A. N/A.

At higher elevation airports the pilot should know that indicated airspeed. will be unchanged, but groundspeed will be faster. N/A. N/A.

What are the standard temperature and pressure values for sea level?. 15 C and 29.92" Hg. N/A. N/A.

Baggage weighing 90 pounds is placed in a normal category airplane´s baggage compartment which is placarded at 100 pounds. If this airplane is subjected to a positive load factor of 3.5 Gs, the total load of the baggage would be. 315 pounds and would not be excessive. N/A. N/A.

Which type of approach and landing is recommended during gusty wind conditions?. A power-on approach and power-on landing. N/A. N/A.

GIVEN: Weight A: 175 pounds at 135 inches aft of datum Weight B: 135 pounds at 115 inches aft of datum Weight C: 75 pounds at 85 inches of datum The CG for the combined would be located how fat aft of datum?. 118.24 inches. N/A. N/A.

(Refer to Figure 8.) GIVEN: Fuel quantity 65 gal Best power (level flight) 55 percent Approximately how much flight time would be available with a day VFR fuel reserve remaining?. 4 hours 30 minutes. N/A. N/A.

(Refer to Figure 12.) GIVEN: Pressure altitude 18,000 ft Temperature -41 C Power 2,500 RPM - 26´´ MP Recommended lean mixture usable fuel 318 lb What is the approximate flight time available under the given conditions? (Allow for VFR night fuel reserve.). 2 hours 27 minutes. N/A. N/A.

If you experience an engine failure in a single-engine aircraft after takeoff. you should. establish the proper glide attitude. N/A. N/A.

(Refer to Figure 32.) GIVEN: Temperature 75 F Pressure altitude 6,000 ft Weight 2,900 lb Headwind 20 kts To safely take off over a 50-foot obstacle in 1,000 feet, what weight reduction is necessary?. 300 pounds. N/A. N/A.

(Refer to Figure 12.) GIVEN: Pressure altitude 18,000 ft Temperature -21 C Power 2,400 RPM - 28´´ MP Recommended lean mixture usable fuel 425 lb What is the approximate flight time available under the given conditions? (Allow for VFR day fuel reserve). 4 hours 1 minute. N/A. N/A.

(Refer to Figure 13.) GIVEN: Aircraft weight 4,000 lb Airport pressure altitude 2,000 ft Temperature at 2,000 feet 32 C Using a maximum rate of climb under the give conditions, how much time would be required to climb to a pressure altitude of 8,000 feet?. 8.4 minutes. N/A. N/A.

When conducting a go-around, the pilot must be aware that. the airplane is trimmed for a power-off condition, and application of takeoff power will cuse the nose to rise rapidly. N/A. N/A.

When diverting to an alternate airport because of an emergency, pilots should. apply rule-of-thumb computations, estimates, and ohter appropiate shortcuts to divert to the new course as soon as possible. N/A. N/A.

(Refer to Figure 9.) Using a normal climb, how much fuel would be used from engine start to 10,000 feet pressure altitude? Aircraft weight 3,500 lb Airport pressure altitude 4,000 ft Temperature 21 C. 35 pounds. N/A. N/A.

When computing weight and balance, the basic empty weight includes the weight of the airframe, engine(s), and all installed optional equipment. Basic empty weight also includes. the unusable fuel, full operating, fluids, and full oil. N/A. N/A.

(Refer to Figure 11.) What would be the endurance at an altitude of 7,500 feet, using 52 percent power?. 7.7 hours. N/A. N/A.

(Refer to Figure 3A.) What is the approximate glide distance if you are operating at 5,500 feet?. 8 NM. N/A. N/A.

(Refer to Figure 10.) Using a maximum rate of climb, how much fuel would be used from engine start to 6,000 feet pressure altitude? Aircraft weight 3,200 lb Airport pressure altitude 2,000 ft Temperature 27 C. 24 pounds. N/A. N/A.

(Refer to Figure 32.) GIVEN: Temperature 50 F Pressure altitude 2,000 feet Weight 2,700 lb Wind Calm What is the total takeoff distance over a 50-foot obstacle?. 800 feet. N/A. N/A.

(Refer to Figure 8.) Approximately how much fuel would be consumed when climbing at 75% power for 7 minutes?. 2.15 gallons. N/A. N/A.

What is the standard temperature at 10,000 feet?. -5 C. N/A. N/A.

GIVEN: Weight A: 155 pounds at 45 inches aft of datum Weight B: 165 pounds at 145 inches aft datum Weight C: 95 pounds at 185 inches aft of datum Based on this information, where would the CG be located aft of datum?. 116.8 inches. N/A. N/A.

(Refer to Figure 34.) GIVEN: Pressure altitude 6,000 ft Temperature 3 C Power 2,200 RPM - 22´´ MP Usable fuel available 465 lb What is the maximum available flight time under the conditions stated?. 6 hours 39 minutes. N/A. N/A.

The performance tables of an aircraft for takeoff and climb are based on. pressure/density altitude. N/A. N/A.

If all index units are positive when computing weight and balance, the location of the datum would be at the. nose, or out in front of the airplane. N/A. N/A.

(Refer to Figure 33.) GIVEN: Weight 3,700 lb Pressure altitude 22,000 ft Temperature -10 C What is the maximum rate of climb under the given conditions?. 384 ft/min. N/A. N/A.

(Refer to Figure 32.) Determine the approximate runway length necessary for takeoff Given: Temperature = 40 degrees F Pressure altitude = 4,000 ft Weight = 3,200 lbs Headwind = 15 kts. 1,300 feet. N/A. N/A.

(Refer to Figure 33.) GIVEN: Weight 4,000 lb Pressure altitude 5,000 ft Temperature 30 C What is the maximum rate of climb under the given conditions?. 702 ft/min. N/A. N/A.

What effect, if any, would a change in ambient temperature or air density have on gas turbine engine performance?. As temperature increases, thrust decreases. N/A. N/A.

What effect does an uphill runway slope have on takeoff performance?. Increases takeoff distance. N/A. N/A.

(Refer to Figure 11.) If the cruise altitude is 7,5000 feet, using 64 percent power at 2,500 RPM, what would be the range with 48 gallons of usable fuel?. 810 miles. N/A. N/A.

(Refer to Figure 34.) GIVEN: Pressure altitude 6,000 ft Temperature -17 C Power 2,300 RPM - 23´´ MP Power 370 lb What is the maximum available flight time under the conditions stated?. 4 hours 30 minutes. N/A. N/A.

(Refer to Figure 14.) GIVEN: Aircraft weight 3,700 lb Airport pressure altitude 4,000 ft Temperature at 4,000 feet 21 C Using a normal climb under the given conditions, how much fuel would be used from engine start to a pressure altitude of 12,000 feet?. 46 pounds. N/A. N/A.

(Refer to Figure 38.) GIVEN: Empty weight (oil is included) 1,271 lb Empty weight moment (in-lb/1,000) 102.04 Pilot and copilot 400 lb Rear seat passenger 140 lb Cargo 100 lb Fuel 37 gal Is the airplane loaded within limits?. Yes, the weight and CG is within limits. N/A. N/A.