- Study guides, Class notes & Summaries

The third segment of the NFP is the segment correct answers c) during which the flaps are retracted The maximum bank angle permitted for a class A aertoplane before reaching 400ft gross height is: correct answers 15 degrees The second segment of the NFP commences when. correct answers the undercarriage 1s fully retracted The third segment of the NFP commences when: correct answers (b) acceleration to lap retraction speed commences The requirements for the third segment of the NFP are...

-

5 pages

Written in 2023/2024

Grade A+

SirAnton

Avia 455 Final Exam With Complete Solutions 100% Verified!!...

-

43 pages

Written in 2024/2025

Grade A+

Easton

AVIA 455 Aircraft Performance Exam 1 CH. 4,5,6 Newest 2026 Questions and Correct Detailed Answers Already Graded A+

-

17 pages

Written in 2025/2026

Grade A+

emilywambura

AVIA 455 - Aircraft Performance Final Exam Chapter 1,2,3, 7, 8, 9, 10, 14-19 Newest 2026 Questions and Correct Detailed Answers Already Graded A+

-

180 pages

Written in 2025/2026

Grade A+

emilywambura

Avia 455 Exam 2 Ch 8, Avia 455 Exam 2 Ch 7 Questions And Correct Answers. Verified 2025/2026.

-

14 pages

Written in 2025/2026

Grade A+

sirjoel

AVIA 455 Exam 2 CH 7&8 QUESTIONS ANSWERED CORRECTLY LATEST 2025 (d) may exceed the runway strength by 50% in an emergency only - Answers With reference to the runway strength, the ACN: (a) must not exceed 90% of the runway strength (b) may unconditionally exceed the runway strength by 10% (c) may exceed the runway strength by a factor of 2 (d) may exceed the runway strength by 50% in an emergency only (a) positive touchdown, full reverse thrust and brakes as soon as the wheels have spun up...

-

13 pages

Written in 2025/2026

Grade A+

TutorJosh

Avia 455 Exam 2 Ch 8, Avia 455 Exam 2 Ch 7 (Latest) Questions With Passed Solutions.

-

40 pages

Written in 2025/2026

Grade A+

EvaTee

AVIA 455 Exam 2 CH 9, AVIA 455 Exam 2 CH 8, AVIA 455 Exam 2 CH 7 || The A+ Blueprint: Exam Questions with Verified Answers!! AVIA 455 - Aircraft Performance Final Exam Chapter 1,2,3, 7, 8, 9, 10, 14-19 || Full Exam Pack: A+ Verified Questions & Answers!! AVIA 455 PJ s Ch: 7-10 || Guaranteed Grade Booster: A+ Verified Exam Questions!!

-

15 items

ProPerfomer

The definition of TODA is that it is equal to: (a) TORA plus stopway plus clearway (b) TORA plus clearway (c) TORA plus stopway (d) ASDA minus stopway. correct answers b Given TORA: 3000m Stopway 1000m and Clearway 2000m. What is the length of the TODA to be used in take-off calculations? (a) 3100 m (b) 3200 m (c) 4500 m (d) 5000 m correct answers c A balanced field-length is when (a) the distance taken to accelerate to VI and the distance to stop are identical (b) TODA plu...

-

5 pages

Written in 2025/2026

Grade A+

ProPerfomer

1.1 A jet aeroplane flying for max endurance has a mass decrease, because of fuel used, by 5% from its original mass, the change to the fuel consumption per hour from that at the original mass is: (a) increase by 5% (b) decrease by 5% (c) increase by 10% (d) decrease by 10% correct answers (b) decrease by 5% 1.6 At a constant thrust setting and altitude the fuel flow of a jet engine: (a) decreases with decreasing OAT (b) increases slightly with increasing speed (c) is independent o...

-

69 pages

Written in 2025/2026

Grade A+

ProPerfomer

If the cost index number is increased, it will correct answers decrease the indurance Optimum altitude is correct answers the altitude at which an aeroplane attains the maximum specific air range The long-range cruising speed for a jet aeroplane is correct answers Higher than the maximum range speed From the buffet onset boundary chart the pilot can obtain correct answers The values of the low-speed and high-speed stall for various altitudes and masses At the maximum range speed in a...

-

4 pages

Written in 2025/2026

Grade A+

ProPerfomer

The definition of TODA is that it is equal to: (a) TORA plus stopway plus clearway (b) TORA plus clearway (c) TORA plus stopway (d) ASDA minus stopway correct answers TORA plus clearway Given: TORA 3000 m. Stopwey 1900 m and Cleanway 2000 m. What is the length of the TODA to be used in take-off calculations? (a) 3100 m (b) 3200 m (c) 4500 m (d) 5000 m correct answers 4500 m A balanced field-length is when: (a) the distance taken to accelerate to Vi and the distance to stop are ide...

-

22 pages

Written in 2025/2026

Grade A+

ProPerfomer

The maximum EAS/Drag ratio is approximately correct answers 1.32 V(imd) The speed to attain the minimum power required for a turbo-jet aeroplane is correct answers less than the speed for the minimum drag The region of speed instability is correct answers the same as the region of reversed command With increasing altitude, the power required curve moves correct answers up and to the right The region of 'reversed command' means correct answers a lower airspeed requires more thru...

-

3 pages

Written in 2025/2026

Grade A+

ProPerfomer

A jet aeroplane flying for maximum endurance has a mass decrease, because of the fuel used, by 5% from its original mass, the change to the fuel consumption per hour from that at the original mass is correct answers Decrease by 5% Two identical turbo-jet aeroplanes are flying at the same altitude at V(IMD). Aircraft A weighs 130,000kg and has a fuel flow of 4300 kg/hr. If aircraft B weighs 115000kg its fuel flow will be correct answers 3804 kg/hr At a constant thrust setting and altitude t...

-

1 pages

Written in 2025/2026

Grade A+

ProPerfomer

Turbofan engine correct answers A type of gas turbine engine in which a lengthened compressor or turbine blade accelerates air around the outside of the core engine Which of the following are true when comparing the diesel or CI engine to the gasoline engine? correct answers 1. Air-cooled horizontally opposed will dominate in thej future 2. The CI engine is 10% to 15% more fuel efficient. 3. The diesel engine is considerably heavier. 4. CI is less cost efficient Turbosupercharger correc...

-

12 pages

Written in 2025/2026

Grade A+

ProPerfomer

The effect that runway slope has on V1 is that: (a) it has no effect (b) V1 increases with a downslope (c) V1 decreases with an upslope (d) V1 increases with an upslope correct answers (d) V1 increases with an upslope The maximum safety margin, for a class 'A' aeroplane, provided by Vmc over Vsr is: (a) 13% (b) 23% (c) 30% (d) 40% correct answers (a) 13% If the V1 used for take-off is in excess of the calculated value then: (a) the V1/Vr ratio is unaffected (b) the continue...

-

52 pages

Written in 2025/2026

Grade A+

ProPerfomer

The definition of TODA is that it is equal to correct answers TORA plus clearway Given: TORA 3000m, stopway 1000m, clearway 2000m. What is the length of the TODA to be used in takeoff? correct answers 4500m A balanced field length is when correct answers ASDA and TODA are equal in length The length of the TORA plus stopway defines correct answers ASDA The minimums semi-width of the stopway is correct answers The same as the associated runway The maximum length of the clearway is e...

-

10 pages

Written in 2025/2026

Grade A+

ProPerfomer

A balanced field exists when: A ) The stopway length and the clearway length are equal B ) The takeoff distance and the landing distance are equal C ) The runway length and the takeoff weight are balanced D ) The clearway length is twice the stopway length correct answers A ) The stopway length and the clearway length are equal A balanced field length is when: A ) ASDA and TODA are equal B ) ASDA and LDA are equal C ) TODA and TORA are equal D ) TORA and LDA are equal correct answers ...

-

22 pages

Written in 2025/2026

Grade A+

ProPerfomer

Which of the following sets of conditions would it be preferable to use 10 degrees of flap instead of 20 degrees of flap for takeoff? (a) low ambient temperature, low aerodrome elevation, having a short runway and a close-in obstacle (b) high ambient temperature, low aerodrome elevation, having a short runway and a distant obstacle (c) high ambient temperature, high aerodrome elevation, having a long runway and a close-in obstacle (d) low ambient temperature, low aerodrome elevation, having ...

-

15 pages

Written in 2025/2026

Grade A+

ProPerfomer

With reference to the runway strength, the ACN: (a) must not exceed 90% of the runway strength (b) may unconditionally exceed the runway strength by 10% (c) may exceed the runway strength by a factor of 2 (d) may exceed the runway strength by 50% in an emergency only correct answers (d) may exceed the runway strength by 50% in an emergency only When approaching a wet runway, with a risk of hydroplaning, the technique to be adopted by the pilot is: (a) positive touchdown, full reverse th...

-

8 pages

Written in 2025/2026

Grade A+

ProPerfomer

With reference to the runway strength, the ACN: (a) must not exceed 90% of the runway strength (b) may unconditionally exceed the runway strength by 10% (c) may exceed the runway strength by a factor of 2 (d) may exceed the runway strength by 50% in an emergency only correct answers (d) may exceed the runway strength by 50% in an emergency only When approaching a wet runway, with a risk of hydroplaning, the technique to be adopted by the pilot is: (a) positive touchdown, full reverse th...

-

4 pages

Written in 2025/2026

Grade A+

ProPerfomer

2.1 Which of the following variables will not affect the shape or position of the Total Drag v IAS curve for speeds below the critical Mach no? (a) configuration (b) mass (c) aspect ratio (d) altitude correct answers (d) altitude 2.2 As speed is reduced below Vimd, total drag: (a) increases and speed stability decreases (b) decreases and speed stability increases (c) increases and speed stability increases (d) decreases and speed stability decreases correct answers (a) increases...

-

7 pages

Written in 2025/2026

Grade A+

ProPerfomer