Aircraft performance

When computing weight and balance, the basic empty weight includes the weight of the airframe, engines, and all isntalled optional equipment. Basic empty weight also includes. the unusable fuel, full operating fluids, and full oil. N/A.

Given total weight: 4137 lb CG location 67.8 Fuel consumption 13.7 GPH Fuel CG station 68.0 After 1 hour 30 minutes of flight time, the CG woud be located at station. 67.79. N/A.

GIVEN: Temperature 75F Pressure altitude 6000ft Weight 2900 lb Headwind 20 Knts To safely take off over a 50ft obstacle in 1000 feet, what weight reduction is necesary?. 300 pounds. N/A.

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.

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

GIVEN: Temperature 100F Pressure altitude 4000ft Weight 3200 lb Wind Calm What is the ground roll required for takeoff over a 50 foot obtacle?. 1.350 feet. N/A.

When conduction a go around, the pilot must be aware that. the irplane is trimmed for a power off condition, ans application of takeoff power will cause the nose to rise rapidly. N/A.

GIVEN: Temperature 30F Pressure altitude 6000 ft Weight 3300 lb Headwind 20 kts What is the total takeoff distance over a 50 foot obstacle?. 1500 feet. N/A.

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

GIVEN: Pressure altitude 18000 Temperature -21c Power 2400 RPM - 28" MP Recommended lean mixture usable fuel 425 lb What is the approximate flight time available under the given condition? (Allow for CFR day fuel reserve). 4 hours 1 minute. N/A.

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

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

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

GIVEN: Aircraft weight 3700lb Airport pressure altitude 4000ft Temperature at 4000 ft 21C Using normal climb under the given conditions, how much fuel would be used from engine start to a pressure altitude af 12.000 feet?. 46 pounds. N/A.

Determine the approximate runway lenght necessary for takeoff GIVEN: Temperature 40F Pressure altitude 4000 ft Weight 3200 lbs Headwind 15 ktos. 1300 feet. N/A.

GIVEN: Temperature 70F Presuure altitude Sea level Weight 3400lb Headwind 16kts Determine the approximate ground roll. 689 feet. N/A.

Rwy 30 is being used for landing. Which surface wind would exceed the airplanes crosswind capability of 0.2 V(SO), if V(SO) is 60 knots?. 260 at 20 knots. N/A.

GIVEN: Pressure altitude 6000ft Temperature 3C Power 2200 RPM - 22 "MP Usable fuel available 465Lb What is the maximum available flight time under the conditions stated?. 6 hours 39 minutes. N/A.

An airplane is loaded to a gross weight od 4800 pounds, with three pieces of laggage in the rear baggage compartment. The CG is located 98 inches aft of datum, which is 1 inch aft of limits. If luggage which wighs 90 pounds is moved fro the rear baggage 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.

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 conventional and nosewheel type airplane. N/A.

Determine the amount of fuel consumed during takeoff and climb at 70 percent power for 10 minutes. 2.88 gallons. N/A.

GIVEN: Pressure altitude 18.000ftg Temperature -41C Power 2.500 RPM - 26 "MP Recommended lean mixture usable fuel 318lb What is the approximate flight time available under the given conditions?. 2 hours 27 minutes. N/A.

GIVEN: Pressure altitude 6000ft Temperature 13C Power 2500 RPM - 23 "MP Usable fuel available 460lb What is the maximum available flight time under the conditions stated?. 5 hours 12 minutes. 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.

GIVEN: Aircraft weight 3400 lb Airport pressure altitude 4000ft Temperature at 4000ft 14C Using a normal climb under the given conditions, how much time would be required to climb to a pressure altitude of 8000 ft?. 5.5 minutes. N/A.

GIVEN: Temperature 50F Pressure altitude 2000 FT Weight 2700 lb Wind Calm What is the total takeoff distance over a 50 foot obstacle?. 800 feet. N/A.

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

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

Using normal climb, how much fuel would be used from engine start to 10000 feet pressure altitude ? Aircraft weight 3500lb Airport pressure altitude 4000ft temperature 21C. 35 pounds. N/A.

GIVEN: Aircraft weight 4000lb Airport pressure altitude 2000ft Temperature at 2000 feet 32C Using a maximum rate of climb under the given conditions, how much time would be required to climb to a pressure altitude of 8000 feet?. 8.4 minutes. N/A.

The surface wind is 180 at 25 kts. What is the crosswind component for a Rwy 13 landing ?. 19 kts. N/A.

GIVEN: Pressure altitude 6000ft Temperature -17C Power 2300 RPM - 23" MP Usable fuel available 370 lb What is the maximum available flight time under the conditions stated?. 4 hours 30 minutes. N/A.

What is the standard temperature at 10.000 feet?. -5C. N/A.

GIVEN: Temperature 50F Pressure altitude Sea level Weight 3000lb Headwind 10kts Determine the approximate ground roll. 636 feet. N/A.

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.

GIVEN: Pressure altitude 18.000ft Temperature -1C Power 2.200 RPM - 20"MP Best fuel economy usable fuel 344lb What is the approximate flight time available under the given condition?. 5 hours 59 minutes. N/A.

GIVEN: Aircraft weight 3400lb Airport pressure altitude 6000 ft Temperature at 6000 feet 10C Using the 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.

What is the standard temperature at 20.000 feet?. -25C. N/A.

GIVEN: Total weight 3027lb 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.

What would be the approximate true airspeed and fuel consuption per hour at an altitude of 7500 feet, using 52 percent power ?. 105 MPH TAS, 6.2 GPH. N/A.

Using a normal climb, how much fuel would be used from engine start to 12.000 feet pressure altitude? Aircraft weight 3800lb Airport pressure altitude 4000ft Temperature 26C. 58 pounds. N/A.

What is the headwind component for a Rwy 13 takeoff if the surface wind is 190 at 15 kts?. 7 knots. N/A.

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

GIVEN: Empty weight 1271lb Emprty weight moment 102.04 Pilot and copilot 400lb Rear seat passenger 140lb Cargo 100lb Fuel 37gal Is the airplane loaded within limits?. Yes, the weight and CG is within limits. N/A.

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

GIVEN: Weight 4000lb Pressure altitude 5000ft Temperture 30C What is the maximum rate of climb under the given condition?. 702 ft/min. N/A.

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

GIVEN: Weight 3700lb Pressure altitude 22000ft Temperature -10C What is the maximum rate of climb under the given conditions?. 384 ft/min. N/A.

What is the approcimate glide distance if you are operating at 8000 feet?. 12 NM. N/A.

What are the standard temperature and pressure values for sea level?. 15C and 29.98 "HG. N/A.

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

GIVEN: Empty weight 1271lb Empty weight moment 102.04 Pilot and copilot 260lb Rear and passenger 120lb Cargo 60lb Fuel 37Gal Under these conditions, the CG is determined to be located. within the CG envelope. N/A.

Approximately how much fuel would be consumed when climbing at 75% power for 7 minutes. 2.15 gallons. N/A.

Using a maximum rate of climb, how much fuel would be used from engine start to 6000 feet pressure altitude? Aircraft weight 3200lb Airport pressure altitude 2000ft Temperature 27C. 24 pounds. N/A.

If the tower-reported surface wind is 010 at 18 knots, what is the crosswind component for a rwy 08 landing ?. 17 knots. N/A.

GIVEN: Airport pressure altitude 2000ft Aiport temperature 20C Cruise pressure altitude 10000ft Cruise temperature 0C What will be the fuel, time, and distance required to climb to cruise altitude under the givn condition?. 5 gallons, 9 minutes, 13NM. N/A.

If the cruise altitude is 7500 feet, using 64 percent power at 2.500 RPM, what would be the range with 48 gallons of usable fuel?. 810 miles. N/A.

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

GIVEN: Empty weight 1271lb Empty weight moment 102.04 Pilot and copilot 360lb Cargo 340lb Fuel 37gal Will the CG remains within limits after 30 gallons of fuel has been used in flight?. Yes, the CG will remains within limits. N/A.

GIVEN: Temperature 85F Pressure altitude 6000ft Weight 2800lb Headwind 14kts Determine the approximate ground roll. 742 feet. N/A.

What is the approximate glide distance if you are operating at 5500 feet?. 8 NM. N/A.

An aircraft is loaded with a ramp weight of 3650 ponds 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. N/A.

What would be the endurance at an altitude of 7500 feet, using 52 percent power? NOTE: (With 48 gallons fuel no reserve). 7.7 hours. N/A.

Using maximum rate of climb, how much fue would be used from engine start to 10000 feet pressure altitude ? Aircraft weight 3800lb Airport pressure altitude 4000ft Temperature 30C. 40 pounds. N/A.

GIVEN: Temperature 80F Pressure altitude 4000ft Weight 2800lb Headwind 24 kts What is the total landing ditance over a 50 foot obstacle?. 1125 feet. N/A.