ATPL - FLIGHT PERFORMANCE &
PLANNING SET B 2/3 Exam Questions
and Answers with Verified Solutions |
Latest Updated 2026
1. A flight is planned from L to d. 1hr 16 min, 616nm
M, distance 850 nm. Wind
component out is 35 kt(TWC),
TAS 450kt. Mean fuel flow out
is 2500kg/hr, mean fuel flow
inbound is 1900kg/hr and the
fuel available is 6000kg. The
time and distance to PSR is: a.
1hr 30 min, 660nm b. 1hr 30
min, 616nm c. 1hr 15 min,
606nm d. 1hr 16 min, 616nm
2. Refer to CAP697 MRJT1 Fig. c. 25,000ft & 435kt
4.2 & 4.5.3.2 Estimated
take-off mass 57,000kg;
ground distance 150nm;
temperature ISA
- 10C; cruise at M0.74. What is
the optimum cruise altitude
and TAS? a. 25,000ft & 445kt
b. 33,000ft & 420kt c. 25,000ft
& 435kt d. 33,000ft & 430kt
3. Given: DOM 33,510kt; b. Estimated landing mass at
Traffic load 7,600kg; Trip fuel destination 43,295kg
PLANNING SET B 2/3 Exam Questions
and Answers with Verified Solutions |
Latest Updated 2026
1. A flight is planned from L to d. 1hr 16 min, 616nm
M, distance 850 nm. Wind
component out is 35 kt(TWC),
TAS 450kt. Mean fuel flow out
is 2500kg/hr, mean fuel flow
inbound is 1900kg/hr and the
fuel available is 6000kg. The
time and distance to PSR is: a.
1hr 30 min, 660nm b. 1hr 30
min, 616nm c. 1hr 15 min,
606nm d. 1hr 16 min, 616nm
2. Refer to CAP697 MRJT1 Fig. c. 25,000ft & 435kt
4.2 & 4.5.3.2 Estimated
take-off mass 57,000kg;
ground distance 150nm;
temperature ISA
- 10C; cruise at M0.74. What is
the optimum cruise altitude
and TAS? a. 25,000ft & 445kt
b. 33,000ft & 420kt c. 25,000ft
& 435kt d. 33,000ft & 430kt
3. Given: DOM 33,510kt; b. Estimated landing mass at
Traffic load 7,600kg; Trip fuel destination 43,295kg