ATPL (Philippines) - Flight Performance
& Planning 2 Exam Questions and
Answers with Verified Solutions | Latest
Updated 2026
1. V2 MIN is determined by a. 1.08VSR for 4 engine turboprops
(excluding Vmca): a. 1.08VSR with 1.13VSR for 2 and 3 engined
for 4 engine turboprops with turboprops
1.13VSR for 2 and 3 engined
turboprops b. 1.2VS for all
turbojets c. 1.2VSR for all
turboprops and 1.15VSR for all
turbojets d. 1.15Vs for all
aeroplanes
2. for a turbojet aeroplane, the b. Landing gear is fully retracted
second segment of the climb
begins when: a. Accelerating
from V2 to flap retraction
speed begins b. Landing gear
is fully retracted c. Flap
retraction begins d. flaps are
fully retracted
3. For a turbojet aeroplane the a. Acceleration to flap retraction
third segment of the climb speed begins (min 400ft)
begins when: a. Acceleration
to flap retraction speed begins
(min 400ft) b. Landing ear is
fully retracted c. Acceleration
from Vlof to V2 begins d. Flaps
, are fully retracted
4. The speed for minimum a. Slower than the speed for
power required in a turbojet minimum drag
will be: a. Slower than the
speed for minimum drag b.
Faster than the speed for
minimum drag c. Slower in a
climb and faster in the descent
d. Same as speed for
minimum drag
5. In wet conditions, what b. 92%
extra percentage over the dry
gross landing distance must
be available for a turbojet?: a.
43% b. 92% c. 67% d. 15%
6. Vref for a Class B aircraft is a. 1.3Vs
defined by: a. 1.3Vs b. 1.2Vs c.
1.3Vmcl d. 1.2Vmcl
7. VR for a jet aircraft must be a. 1.05 Vmca and V1
faster than, the greater of: a.
1.05 Vmca and V1 b. Vmca
and 1.1V1 c. VMBE and V1 d.
V1 and 1.1 Vmca
8. A balanced field length is d. ASDA equals TODA
when: a. Distance taken to
accelerate to V1 and distance
to stop are identical b. TORA x
1.5 c. V1=Vr d. ASDA equals
TODA
& Planning 2 Exam Questions and
Answers with Verified Solutions | Latest
Updated 2026
1. V2 MIN is determined by a. 1.08VSR for 4 engine turboprops
(excluding Vmca): a. 1.08VSR with 1.13VSR for 2 and 3 engined
for 4 engine turboprops with turboprops
1.13VSR for 2 and 3 engined
turboprops b. 1.2VS for all
turbojets c. 1.2VSR for all
turboprops and 1.15VSR for all
turbojets d. 1.15Vs for all
aeroplanes
2. for a turbojet aeroplane, the b. Landing gear is fully retracted
second segment of the climb
begins when: a. Accelerating
from V2 to flap retraction
speed begins b. Landing gear
is fully retracted c. Flap
retraction begins d. flaps are
fully retracted
3. For a turbojet aeroplane the a. Acceleration to flap retraction
third segment of the climb speed begins (min 400ft)
begins when: a. Acceleration
to flap retraction speed begins
(min 400ft) b. Landing ear is
fully retracted c. Acceleration
from Vlof to V2 begins d. Flaps
, are fully retracted
4. The speed for minimum a. Slower than the speed for
power required in a turbojet minimum drag
will be: a. Slower than the
speed for minimum drag b.
Faster than the speed for
minimum drag c. Slower in a
climb and faster in the descent
d. Same as speed for
minimum drag
5. In wet conditions, what b. 92%
extra percentage over the dry
gross landing distance must
be available for a turbojet?: a.
43% b. 92% c. 67% d. 15%
6. Vref for a Class B aircraft is a. 1.3Vs
defined by: a. 1.3Vs b. 1.2Vs c.
1.3Vmcl d. 1.2Vmcl
7. VR for a jet aircraft must be a. 1.05 Vmca and V1
faster than, the greater of: a.
1.05 Vmca and V1 b. Vmca
and 1.1V1 c. VMBE and V1 d.
V1 and 1.1 Vmca
8. A balanced field length is d. ASDA equals TODA
when: a. Distance taken to
accelerate to V1 and distance
to stop are identical b. TORA x
1.5 c. V1=Vr d. ASDA equals
TODA
