Atpl performance and loading Exam
Questions and Answers with Verified
Solutions | Latest Updated 2026
Most critical segment for Second segment. It extends from
obstacle clearance in the gear retraction to a minimum height
event of engine failure after of 400ft. or such greater height so
take off? as to achieve obstacle clearence. By
the time second stage ends the
obstacles are cleared.
What is the effect on V1 speed V1 may be increased. A stopway
if stopway is included in take increases ASDA. which permits a
off and asd performance higher V1 speed thereby reducing
calculation is? TODA(1 inop). or increasing the
runway limited t/o weight.
The second segment climb The completion of landing gear
refers to the period from? retraction to a minimum of 400ft.
What height should the V@ At or before 35ft.
reached by?
What is the effect on BRW if A clearway increases the TODA and
the clearway is approved for therefore the BRW may be incleased
inclusion in the TODA. if the BRW was limited by runway
length.
When a range of V1 speeds is Decrease the one engine inop TODR
available for a given set of and increase the ASDR. A higher V1
conditions,selection of a high will make it more difficultreject in
, V1 will? the event of an engine failure up to
V1 but easier to go in the event of
an engine failure after V1.
An aircraft approaching to land 1000ft. The usual touchdown point
at a 3 deg approach angle, from an ILS approach on a 3 deg
crosses the landing threshold glideslope is at the glideslope
50ft higher than the normal transmitter which is situated about
approach height. Compared to 1000ft in from the landing threshold
the normal touchdown following an approach to land over
position, the extra distance to the landing threshold at 50 ft.
the touchdown position for this Anextra 50 ft over the threshold
approach is? results in extra 1000ft in along the
runway at touchdown.
The ASDR for a particular there is a 2 to 3 sec reaction time
aircraft as shown in the between V1 and the pilot response.
manufacturers data assumes?
The VREf is? the landing speed in a nominated
configuration.
The reason for specifying a To prevent excessive stress on the
maximum zero fuel weight for wings and fuselage with low fuel
an aircraft is? quantities.
Following an engine failure positive.
recognised by V1 in a twin
engine turbine transport
aircraft, the gross climb
gradient that must be
achieved without landing gear
retraction is?
Questions and Answers with Verified
Solutions | Latest Updated 2026
Most critical segment for Second segment. It extends from
obstacle clearance in the gear retraction to a minimum height
event of engine failure after of 400ft. or such greater height so
take off? as to achieve obstacle clearence. By
the time second stage ends the
obstacles are cleared.
What is the effect on V1 speed V1 may be increased. A stopway
if stopway is included in take increases ASDA. which permits a
off and asd performance higher V1 speed thereby reducing
calculation is? TODA(1 inop). or increasing the
runway limited t/o weight.
The second segment climb The completion of landing gear
refers to the period from? retraction to a minimum of 400ft.
What height should the V@ At or before 35ft.
reached by?
What is the effect on BRW if A clearway increases the TODA and
the clearway is approved for therefore the BRW may be incleased
inclusion in the TODA. if the BRW was limited by runway
length.
When a range of V1 speeds is Decrease the one engine inop TODR
available for a given set of and increase the ASDR. A higher V1
conditions,selection of a high will make it more difficultreject in
, V1 will? the event of an engine failure up to
V1 but easier to go in the event of
an engine failure after V1.
An aircraft approaching to land 1000ft. The usual touchdown point
at a 3 deg approach angle, from an ILS approach on a 3 deg
crosses the landing threshold glideslope is at the glideslope
50ft higher than the normal transmitter which is situated about
approach height. Compared to 1000ft in from the landing threshold
the normal touchdown following an approach to land over
position, the extra distance to the landing threshold at 50 ft.
the touchdown position for this Anextra 50 ft over the threshold
approach is? results in extra 1000ft in along the
runway at touchdown.
The ASDR for a particular there is a 2 to 3 sec reaction time
aircraft as shown in the between V1 and the pilot response.
manufacturers data assumes?
The VREf is? the landing speed in a nominated
configuration.
The reason for specifying a To prevent excessive stress on the
maximum zero fuel weight for wings and fuselage with low fuel
an aircraft is? quantities.
Following an engine failure positive.
recognised by V1 in a twin
engine turbine transport
aircraft, the gross climb
gradient that must be
achieved without landing gear
retraction is?
