c7.16
問題一覧
1
will need more runway to takeoff
2
specified by the manufacturer
3
negative if it is measured forward of the datum
4
the aircraft flight manual
5
could be anywhere on the aircraft
6
will have a longer take-off run
7
aircraft over 2730kg (6000 lbs) – a Weight and Centre of Gravity Schedule
8
reweighed as required by the CAA
9
must be reweighed after 2 years from manufacture then at periods not exceeding 5 years
10
the fuel that cannot be pumped by the booster pump due to the low fuel level
11
the basic weight plus unusable fuel plus oil
12
The reaction is the load at each separate weighing point
13
using metallic resistance elements or strain gauges, the resistance of which varies with change in length, due to elastic strain
14
A secondary purpose is to achieve the utmost in efficiency during flight
mod 4 test
mod 4 test
Aljuboory · 81問 · 1年前mod 4 test
mod 4 test
81問 • 1年前mod 2 test
mod 2 test
Aljuboory · 100問 · 1年前mod 2 test
mod 2 test
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mod 2,2
Aljuboory · 94問 · 1年前mod 2,2
mod 2,2
94問 • 1年前mod 6,1
mod 6,1
Aljuboory · 277問 · 1年前mod 6,1
mod 6,1
277問 • 1年前c7.1
c7.1
Aljuboory · 18問 · 1年前c7.1
c7.1
18問 • 1年前c7.2
c7.2
Aljuboory · 11問 · 1年前c7.2
c7.2
11問 • 1年前c7.3
c7.3
Aljuboory · 36問 · 1年前c7.3
c7.3
36問 • 1年前c7,4
c7,4
Aljuboory · 20問 · 1年前c7,4
c7,4
20問 • 1年前c7.5
c7.5
Aljuboory · 11問 · 1年前c7.5
c7.5
11問 • 1年前c7.7
c7.7
Aljuboory · 17問 · 1年前c7.7
c7.7
17問 • 1年前c7.8
c7.8
Aljuboory · 5問 · 1年前c7.8
c7.8
5問 • 1年前c7.9
c7.9
Aljuboory · 8問 · 1年前c7.9
c7.9
8問 • 1年前7.10
7.10
Aljuboory · 12問 · 1年前7.10
7.10
12問 • 1年前c7.11
c7.11
Aljuboory · 6問 · 1年前c7.11
c7.11
6問 • 1年前c7.12
c7.12
Aljuboory · 10問 · 1年前c7.12
c7.12
10問 • 1年前c7.13
c7.13
Aljuboory · 10問 · 1年前c7.13
c7.13
10問 • 1年前c7.14
c7.14
Aljuboory · 17問 · 1年前c7.14
c7.14
17問 • 1年前c7.15
c7.15
Aljuboory · 20問 · 1年前c7.15
c7.15
20問 • 1年前c7.17
c7.17
Aljuboory · 14問 · 1年前c7.17
c7.17
14問 • 1年前c7.18
c7.18
Aljuboory · 36問 · 1年前c7.18
c7.18
36問 • 1年前c7.19
c7.19
Aljuboory · 11問 · 1年前c7.19
c7.19
11問 • 1年前c7.20
c7.20
Aljuboory · 18問 · 1年前c7.20
c7.20
18問 • 1年前問題一覧
1
will need more runway to takeoff
2
specified by the manufacturer
3
negative if it is measured forward of the datum
4
the aircraft flight manual
5
could be anywhere on the aircraft
6
will have a longer take-off run
7
aircraft over 2730kg (6000 lbs) – a Weight and Centre of Gravity Schedule
8
reweighed as required by the CAA
9
must be reweighed after 2 years from manufacture then at periods not exceeding 5 years
10
the fuel that cannot be pumped by the booster pump due to the low fuel level
11
the basic weight plus unusable fuel plus oil
12
The reaction is the load at each separate weighing point
13
using metallic resistance elements or strain gauges, the resistance of which varies with change in length, due to elastic strain
14
A secondary purpose is to achieve the utmost in efficiency during flight