F T ra n sf o F T ra n sf o
PD rm PD rm
Y Y
Y
Y
er
er
ABB
ABB
y
y
bu
bu
2.0
2.0
Participant: WILSON, WILSON
to
to
re
re
he
he
Licence: CPLA
k
k
lic
lic
Examination: 030 Flight Performance & Planning
C
C
w m w om
w
w
w.
Date
A .c o
B B Y Y3 2/11/2013 w.
A B B Y Y.c
1 An aeroplane is loaded with its centre of gravity towards the rear limit. This will result in:
an increase in longitudinal stability.
an increased risk of stalling due to a decrease in tailplane moment
a reduction in power required for a given speed.
a reduced fuel consumption as a result of reduced drag.
Origin ID: 110 Maximum attainable 1.00
Theme 31.1.1.2 Importance in regard to aircraft stability Reached points 1.00
, F T ra n sf o F T ra n sf o
PD rm PD rm
Y Y
Y
Y
er
er
ABB
ABB
y
y
bu
bu
2.0
2.0
Participant: WILSON, WILSON
to
to
re
re
he
he
Licence: CPLA
k
k
lic
lic
Examination: 030 Flight Performance & Planning
C
C
w m w om
w
w
w.
Date
A .c o
B B Y Y3 2/11/2013 w.
A B B Y Y.c
2 At a given mass the CG position is at 15% MAC. If the leading edge of MAC is at a position
625.6 inches aft of the datum and the MAC is given as 134.5 inches determine the position
of the CG in relation to the datum.
645.78 inches aft of datum
20.18 inches aft of datum
605.43 inches aft of datum
228.34 inches aft of datum
Origin ID: 86 Maximum attainable 1.00
Theme 31.1.2.1 Consult aeroplane flight manual for Reached points 0.00
, F T ra n sf o F T ra n sf o
PD rm PD rm
Y Y
Y
Y
er
er
ABB
ABB
y
y
bu
bu
2.0
2.0
Participant: WILSON, WILSON
to
to
re
re
he
he
Licence: CPLA
k
k
lic
lic
Examination: 030 Flight Performance & Planning
C
C
w m w om
w
w
w.
Date
A .c o
B B Y Y3 2/11/2013 w.
A B B Y Y.c
3 033-060.htm
From the loading manual for the transport aeroplane, the aft cargo compartment has a
maximum total load of:
3062 kg
9232 kg
4187 kg
1568 kg
Origin ID: 114 Maximum attainable 1.00
Theme 31.1.2.2 Maximum floor load Reached points 0.00
, F T ra n sf o F T ra n sf o
PD rm PD rm
Y Y
Y
Y
er
er
ABB
ABB
y
y
bu
bu
2.0
2.0
Participant: WILSON, WILSON
to
to
re
re
he
he
Licence: CPLA
k
k
lic
lic
Examination: 030 Flight Performance & Planning
C
C
w m w om
w
w
w.
Date
A .c o
B B Y Y3 2/11/2013 w.
A B B Y Y.c
4 The maximum certificated taxi (or ramp) mass is that mass to which an aeroplane may be
loaded prior to engine start. It is:
a value which is only affected by the outside air temperature. Corrections are
calculated from data given in the Flight Manual.
a value which varies with airfield temperature and altitude. Corrections are listed in
the Flight Manual.
a fixed value which is listed in the Flight Manual.
a value which varies only with airfield altitude. Standard corrections are listed in
the Flight Manual.
Origin ID: 117 Maximum attainable 1.00
Theme 31.1.2.3 Maximum ramp and taxi mass Reached points 0.00
PD rm PD rm
Y Y
Y
Y
er
er
ABB
ABB
y
y
bu
bu
2.0
2.0
Participant: WILSON, WILSON
to
to
re
re
he
he
Licence: CPLA
k
k
lic
lic
Examination: 030 Flight Performance & Planning
C
C
w m w om
w
w
w.
Date
A .c o
B B Y Y3 2/11/2013 w.
A B B Y Y.c
1 An aeroplane is loaded with its centre of gravity towards the rear limit. This will result in:
an increase in longitudinal stability.
an increased risk of stalling due to a decrease in tailplane moment
a reduction in power required for a given speed.
a reduced fuel consumption as a result of reduced drag.
Origin ID: 110 Maximum attainable 1.00
Theme 31.1.1.2 Importance in regard to aircraft stability Reached points 1.00
, F T ra n sf o F T ra n sf o
PD rm PD rm
Y Y
Y
Y
er
er
ABB
ABB
y
y
bu
bu
2.0
2.0
Participant: WILSON, WILSON
to
to
re
re
he
he
Licence: CPLA
k
k
lic
lic
Examination: 030 Flight Performance & Planning
C
C
w m w om
w
w
w.
Date
A .c o
B B Y Y3 2/11/2013 w.
A B B Y Y.c
2 At a given mass the CG position is at 15% MAC. If the leading edge of MAC is at a position
625.6 inches aft of the datum and the MAC is given as 134.5 inches determine the position
of the CG in relation to the datum.
645.78 inches aft of datum
20.18 inches aft of datum
605.43 inches aft of datum
228.34 inches aft of datum
Origin ID: 86 Maximum attainable 1.00
Theme 31.1.2.1 Consult aeroplane flight manual for Reached points 0.00
, F T ra n sf o F T ra n sf o
PD rm PD rm
Y Y
Y
Y
er
er
ABB
ABB
y
y
bu
bu
2.0
2.0
Participant: WILSON, WILSON
to
to
re
re
he
he
Licence: CPLA
k
k
lic
lic
Examination: 030 Flight Performance & Planning
C
C
w m w om
w
w
w.
Date
A .c o
B B Y Y3 2/11/2013 w.
A B B Y Y.c
3 033-060.htm
From the loading manual for the transport aeroplane, the aft cargo compartment has a
maximum total load of:
3062 kg
9232 kg
4187 kg
1568 kg
Origin ID: 114 Maximum attainable 1.00
Theme 31.1.2.2 Maximum floor load Reached points 0.00
, F T ra n sf o F T ra n sf o
PD rm PD rm
Y Y
Y
Y
er
er
ABB
ABB
y
y
bu
bu
2.0
2.0
Participant: WILSON, WILSON
to
to
re
re
he
he
Licence: CPLA
k
k
lic
lic
Examination: 030 Flight Performance & Planning
C
C
w m w om
w
w
w.
Date
A .c o
B B Y Y3 2/11/2013 w.
A B B Y Y.c
4 The maximum certificated taxi (or ramp) mass is that mass to which an aeroplane may be
loaded prior to engine start. It is:
a value which is only affected by the outside air temperature. Corrections are
calculated from data given in the Flight Manual.
a value which varies with airfield temperature and altitude. Corrections are listed in
the Flight Manual.
a fixed value which is listed in the Flight Manual.
a value which varies only with airfield altitude. Standard corrections are listed in
the Flight Manual.
Origin ID: 117 Maximum attainable 1.00
Theme 31.1.2.3 Maximum ramp and taxi mass Reached points 0.00
