FIA Aircraft Performance Practice Test

These questions are part of the practice quiz. Start practicing

• If 50 pounds of weight is located at point X and 100 pounds at point Z, how much weight must be located at point Y to balance the plank?
• What is the required ground run for takeoff under the given conditions?
• What is maneuvering speed (Va) and when is it relevant?
• Which statement correctly defines endurance in aviation performance terms?
• Which factor is critical for determining the rate of climb in a single-engine operation of a twin-engine airplane?
• What effect does an uphill runway slope have on takeoff performance?
• What happens if the center of gravity is too far aft on a fixed-wing aircraft?
• In flight planning, what is the primary purpose of listing an alternate airport?
• When the CG is moved aft, what is the general effect on stability?
• Based on the given weights, how does the airplane's condition relate to acceptable limits?
• Why is it essential to verify chart revision date against the aircraft model/configuration?
• In CG calculations, what quantities are used to determine the center of gravity?
• What can a pilot expect when landing at an airport located in mountainous terrain?
• How does increased weight affect the takeoff distance of an airplane?
• What are the consequences of a forward CG on stall speed, elevator effectiveness, and takeoff performance?
• If the CG needs to be shifted to 80 inches by moving weight B, how many inches must weight B be moved?
• At what weight does the stall speed of an aircraft typically increase?
• What occurs if the maximum demonstrated crosswind component exceeds a certain limit?
• What indicated airspeed provides the greatest gain in altitude at 3,200 feet?
• What indicated airspeed at 3,000 feet would result in the greatest increase in altitude for a given distance?
• Why must CG be verified within limits after fuel changes?
• At what altitude is the aircraft’s performance most affected by temperature and pressure altitude?
• How does a tailwind component influence landing distance and approach planning?
• How much weight must be shifted from Station 150.0 to Station 30.0 to move the CG to exactly the aft CG limit when the total weight is 7,500 lbs?
• Density altitude effect on takeoff performance: which statement is true?
• What condition is indicated if the total weight of pilot, copilot, passengers, baggage, and fuel results in being 185 pounds under allowable gross weight?
• What is the approximate total distance required to clear a 50-foot obstacle with a temperature of 35°C and a pressure altitude of 3,000 ft?
• What is the maximum weight that can be added at Station 150.0 without exceeding the aft CG limit if the aircraft weight is 5,000 lb?
• How do Mach number limitations influence high-altitude performance charts and decision-making?
• What happens to landing distance as the weight of an aircraft increases?
• How do configuration choices (flaps, gear) influence landing distance and approach speed?
• Define V1, Vr, and V2. What do these speeds represent and when are they critical?
• What should be done when density altitude exceeds capability as indicated on the performance chart?
• How does aircraft weight impact climb rate and climb gradient?
• What is the relationship between aircraft weight and distance to clear obstacles during takeoff?
• What should be monitored to maintain proper weight and balance during flight?
• To balance the board about its center with A = 300, B = 375, C = 600, how many inches should weight B be moved left?
• What is the required takeoff distance to clear a 50-foot obstacle at a temperature of 23°C and a pressure altitude of 3,000 feet?
• What must happen to maintain level flight with a CG at the forward limit?
• How does deploying flaps influence takeoff distance and initial climb performance in light aircraft?
• If 50 pounds of weight is located at point X and 100 pounds at point Y, how much weight is needed at point Z to balance the plank?
• What would be the indicated stall speed during a 40° banked turn with the gear down and flaps set at 45°?
• Why are fuel reserves and contingencies required in IFR flight planning?
• How do you perform a weight-and-balance calculation to verify that the aircraft CG lies within limits?
• What happens to the service ceiling of an aircraft as weight is reduced?
• Which factor, when increased, will increase landing distance?
• What happens to the weight of an aircraft if fuel is burned from the main tanks?
• In a twin-engine airplane, the single-engine service ceiling indicates what rate of climb?
• What effects can wind shear or microbursts have on takeoff and initial climb performance?
• How does increasing humidity typically affect aircraft performance?
• How does an increase in outside air temperature generally affect the density altitude?
• For maximum altitude gain with one engine inoperative, when should the blue radial line be used?
• If the given weights are A = 100, B = 200, and C = 200, how far must weight B be shifted to obtain a new CG of 50?
• If 50-pound weights are located at points X, Y, and Z, how would point Z need to be adjusted to balance the plank?
• How does the recovery from a stall change as the center of gravity (CG) location is moved rearward?
• Which statement is true regarding the operation of a multiengine airplane with one engine inoperative?
• What is the approximate crosswind component when landing on Rwy 22 with winds from 260° at 23 kts?
• What is a key consideration when distributing fuel among tanks during preflight to maintain CG within limits?
• What is the pressure altitude at an airport that is 3,563 feet MSL with an altimeter setting of 29.96?
• What is the approximate glide distance at a height above terrain of 10,500 feet with a tailwind of 20 knots?
• What is ISA deviation and how should it be treated when applying performance charts?
• What is the effect of a higher stalling speed on aircraft handling characteristics?
• Which inputs influence takeoff distance to clear an obstacle?
• What is the center of gravity (CG) and why must flights stay within the CG envelope?
• What contributes to an increase in density altitude?
• What is the maximum weight that could be added at Station 130.0 without exceeding the aft CG limit if the total weight is 2,900 lb and the CG is at Station 115.0?
• What is the primary purpose of determining density altitude?
• What tends to increase landing distance during approach and landing?
• What is the effect of high density altitude on propeller efficiency?
• What risks are associated with an aft center of gravity and how do performance characteristics change?
• Along which axis is the center of gravity of an aircraft computed?
• How does wind affect takeoff and landing performance, and which wind component has the greatest impact on ground roll?
• Why might a pilot use different flap settings for takeoff and landing?
• What happens to engine power, propeller efficiency, and climb performance as density altitude increases?
• Define zero fuel weight (ZFW) and explain its role in payload and structural load planning.
• What is the definition of pressure altitude?
• How does indicated airspeed relate to true airspeed as altitude increases?
• What is the relationship between wing loading and stall speed, and how does it affect approach and landing?
• Differentiate absolute ceiling from service ceiling and explain how climb performance is assessed near these ceilings.
• What effect does exceeding an aircraft's forward CG limit have on its flight characteristics?
• What happens to the controllability of an aircraft loaded with the CG aft of the aft limit?
• What defines the required climb rate in order to reach a specified obstacle clearance height?
• At V(MC), what can a pilot expect regarding performance in a light multiengine airplane?
• What condition leads to the highest value of V(MC)?
• If the center of gravity (CG) of an aircraft is moved from the aft limit to beyond the forward limit, how are cruising and stalling speeds affected?
• What is the condition of the airplane when the total weight is 197 pounds under the allowable gross weight?
• Why must planned flights include fuel reserves and an alternate airport, and how is endurance calculated?
• What condition will lead to the highest stalling speed of an aircraft?
• What effect does having the center of gravity (CG) at the aft limit have on performance characteristics?
• How does climb performance relate to obstacle clearance height and required gradient?
• What is the significance of the CG location in flight?
• How should performance charts be adjusted when the runway is sloped or contaminated?
• During a descent, a plane's altitude and headwind can affect what crucial performance metric?
• What effect does a 35-gallon fuel burn have on the weight and balance of an aircraft weighing 2,890 pounds with a MOM/100 of 2,452 at takeoff?
• What is the purpose of interpolation when reading performance charts, and how is it performed?
• What would lead to an increase in density altitude at a given airport?
• What is accelerates-stop distance and when must it be used in planning?
• How is the center of gravity of an aircraft determined?
• In cruise planning, which airspeed is typically used and why?
• Which statement about V2 is true?
• What is an effect of having the center of gravity excessively forward on a fixed-wing airplane?
• What handling issues might suggest an aft CG, and what corrective actions should a pilot take?
• How much additional weight can be added at Station 160 without exceeding the aft CG limit of Station 90.5?
• What happens to the stall speed as wing loading increases?
• What happens to the allowable useful load if additional items are installed in an aircraft?
• If weight increases, what happens to V2?
• Why is it important to compare calculated TAS with chart data when planning cruise at altitude?
• In a propeller-driven airplane, when does maximum range occur?
• When one engine fails in a twin-engine airplane, what is the expected performance loss?
• What are the typical advantages of short-field and soft-field takeoff and landing techniques?
• When a crosswind component is present on landing, how should you adjust?
• What impact does an increase in aircraft weight have on takeoff performance?
• Which factor most directly increases takeoff distance?
• What aspect of aircraft performance does the indicated stall speed influence directly?
• What is an obstacle clearance requirement and how is it verified in takeoff performance planning?
• What would typically happen to the takeoff roll on a hot day?
• What would be the indicated stall speed in a 30° banked turn with the gear down and flaps set at 15°?
• What is the approximate ground roll for an airplane at a pressure altitude of 6,000 ft and weight of 2,800 lb with a 14 kts headwind?
• What is the density altitude if the airport elevation is 3,795 ft, OAT 24°C, and altimeter setting 29.70" Hg?
• When an aircraft is loaded with the CG forward of the forward limit, what issue may arise?
• What is the effect of flaps on takeoff distance?
• How does increasing gross weight affect takeoff distance and V speeds V1, Vr, and V2?
• What must be managed to ensure safe flight during adverse weather conditions?
• Which statement best describes IAS, CAS, TAS and their use in performance planning?
• How does the aft movement of the nosewheel during gear retraction affect the CG location?
• What is the consequence of exceeding the aft CG limit during flight operations?
• How would you calculate the required runway length using takeoff and landing distance charts in a mixed weight and wind scenario?
• What is the effect on distances when slope or contamination corrections are applied?
• How does wind direction affect landing distance?
• How does an increase in humidity affect takeoff performance while other conditions remain the same?
• If weight A = 40, what weight must be placed at point B to balance the lever?
• How does weight distribution affect an aircraft's stability?
• Which statement about planning around ceilings is true?
• What would be the new CG location if 135 pounds of weight were added at Station 109.0, with a total weight of 2,340 lb and CG location at Station 103.0?
• What is the relationship between density altitude, pressure altitude, and temperature on TAS and fuel burn?
• What would be a critical consideration for flight planning concerning weight distribution?
• What is the approximate total distance required to clear a 50-foot obstacle at a temperature of 25°C and pressure altitude of 2,500 ft?
• What would happen to the CG location if 50 pounds of weight were added at Station 90.0?
• What is the crosswind component for a landing on Runway 18 if the wind is reported as 220° at 30 knots?
• What is the location of the center of gravity (CG) if 146 pounds are removed from Station 150?
• What happens to the takeoff distance with increased headwind during takeoff?
• Which statement about wind effects on landing distance is correct?
• Under which condition is a forward center of gravity (CG) most critical?
• What is the approximate crosswind component when landing on Rwy 03 with a wind from 060° at 35 knots?
• What conclusion can be drawn if the maximum demonstrated crosswind component is exceeded during landing?
• Which parameter is commonly adjusted via flap setting to influence landing distance?
• What is the purpose of crosswind correction factors in landing distance estimates?
• What is the effect of increased forward CG on stall speed?
• Which aspect of an aircraft's performance is most affected by an aft CG position?
• What is the required takeoff distance to clear a 50-foot obstacle at a temperature of 3°C and a pressure altitude of 6,000 feet with a weight of 3,000 pounds?
• What occurs to indicated airspeed if the CG is at the most forward allowable position while maintaining constant power and altitude?
• Describe short-field takeoff techniques and the configuration settings that minimize takeoff distance.
• What happens to the center of gravity location when weight is removed from Station 150?
• What is the effect of temperature on aircraft performance during takeoff?
• What parameter must be considered for engine-out climb performance during takeoff?
• What is the approximate glide distance at a height above terrain of 5,500 feet with a tailwind of 10 knots?
• In a twin-engine aircraft, what is the significance of engine-out climb gradient and how is it calculated?
• What is the total landing distance over a 50-foot obstacle at a temperature of 15°C and pressure altitude of 4,000 ft with weight of 3,000 lb and a 22 kts headwind?
• What weight must be placed at point A to balance the lever if B weighs 150 pounds?
• As altitude increases, what generally happens to air density?
• What is the approximate total distance required to clear a 50-foot obstacle with a temperature of 20°C and a pressure altitude of 1,000 ft?
• Why is it important to correct CG when loading an aircraft?
• How does a decrease in air density at higher elevations affect engine power output?
• Performance charts typically use which airspeed reference for lift and drag calculations?
• How can fuel distribution in a multi-tank wing affect CG during flight, and how is it mitigated?
• How much additional weight can be added at Station 120 without exceeding the aft CG limit for an aircraft weighing 9,500 lb with a CG location at Station 90.0 and an aft CG limit at Station 90.5?
• How is performance data validated before use, and what checks should be performed on charts and limits?
• If 60 pounds are removed from Station 70, where is the new Center of Gravity (CG) location?
• Can 100 pounds of weight be shifted from Station 30.0 to Station 120.0 without exceeding the aft CG limit?
• How is the density altitude determined if the airport elevation is 3,450 ft, OAT is 35°C, and the altimeter setting is 30.40" Hg?
• How does wing loading affect stall speed and overall handling characteristics?
• How is alternate fuel planning incorporated into total fuel calculations for a trip?
• What is indicated by an aft center of gravity in terms of aircraft stability?
• Which statement about climb performance and weight?
• As the center of gravity (CG) moves aft, how does the stability and controllability of an aircraft change?
• How far aft of datum is the CG located in the provided weight scenario?
• Given a height above terrain of 7,500 ft and a headwind of 30 kts, what is the approximate glide distance?
• In terms of allowable weight, how does the addition of equipment affect an aircraft?
• In which situation would a heavier rearward CG place an airplane at greater risk?
• Differentiate best angle of climb (Vx) from best rate of climb (Vy) and describe typical use cases.
• What control measures should be applied for managing density altitude conditions during flight operations?
• What are Vle and Vlo and why are they important in performance planning for gear-equipped aircraft?
• How does the maximum lift-to-drag ratio affect flight distance in an airplane?
• Which performance characteristic is negatively impacted by an aft CG in aircraft?
• For an airplane with reciprocating, non-turbocharged engines, how does V(MC) change with altitude?
• What is the effect of tailwind on ground roll distance?
• What occurs to density altitude with a temperature increase from 30 to 50 degrees F, given a constant pressure altitude of 3,000 feet MSL?
• Which input is explicitly included when calculating the takeoff distance to clear an obstacle?
• Using a maximum demonstrated crosswind component equal to 0.2 V(SO), what conclusion can a pilot make with V(SO) at 60 knots and wind from 150° at 20 knots?
• If 90 pounds are removed from Station 140, what is the new location of the CG for an aircraft weighing 6,230 lb with the CG located initially at Station 79?
• What is the ground roll required for takeoff at a temperature of 25°C and a pressure altitude of 2,000 ft with a weight of 2,200 lb and a headwind of 15 kts?
• What happens to propeller force at high density altitudes compared to low density altitudes?
• What is the recommended reduction in indicated speed to maintain the best rate of climb?
• If weight B needs to be moved 50 inches right to balance the board, what are the weights given A = 500, B = 200, C = 400?
• How do you determine if there is enough fuel to reach an alternate plus holding IFR?
• How does altitude generally affect an aircraft's takeoff distance?
• If an aft CG is suspected in flight, which action is recommended?
• What is the effect of high density altitude on aircraft performance?
• Density altitude is defined as which of the following?
• With a total weight of 2,800 lb and CG at Station 120.0, can 100 pounds be shifted from Station 130.0 to Station 30.0 without exceeding the forward CG limit of Station 117.0?
• How does high density altitude affect takeoff performance?
• What is the significance of the altimeter setting of 29.70" Hg in density altitude calculations?
• How far aft of datum would the CG be located with the given weights at specific stations?
• Why is interpolation between chart points needed when calculating takeoff distance with variable weight and wind?
• How do you compute endurance and range from usable fuel and throttle settings?
• Based on the given weights, how far aft of datum is the CG located?
• What should a pilot consider when determining the takeoff weight concerning the aircraft balance?
• What is the total landing distance over a 50-foot obstacle at a temperature of 35°C, pressure altitude of 2,000 ft, and weight of 3,400 lb?
• Determine the density altitude given an airport elevation of 5,515 ft, OAT of 30°C, and an altimeter setting of 29.40" Hg.
• What inputs are typically used on takeoff performance charts, and how is interpolation performed between values?
• Which sequence correctly describes how to compute CG and total weight from a weight-and-balance sheet?
• What is the approximate crosswind component for landing on Rwy 30 with a wind from 020° at 15 kts?
• What is the effect of a tailwind on glide distance?
• What is a critical factor in takeoff performance in regards to temperature and pressure altitude?
• What would the indicated stall speed be in a 60° banked turn with the gear and flaps up?
• What does the blue radial line on the airspeed indicator indicate in a light multiengine airplane?
• If the landing gear on an airplane moves forward during retraction, what happens to the total moment?
• Which statement about wind direction and takeoff distance is correct?