Air Tech - CPL Performance

Air Tech - CPL Performance

University

9 Qs

quiz-placeholder

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Air Tech - CPL Performance

Air Tech - CPL Performance

Assessment

Quiz

Engineering

University

Medium

Created by

NZAAL Theory

Used 4+ times

FREE Resource

9 questions

Show all answers

1.

MULTIPLE SELECT QUESTION

45 sec • 1 pt

The Basic Empty Weight of an aircraft includes...

Select all that apply

unusable

crew

rations

radios

2.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The Basic Operating Weight of an aircraft is also known as the...

Aircraft prepared for service weight

Zero fuel weight

Gross weight

All up weight

3.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The Basic Operating Weight of an aircraft includes...

pilot/s and crew

passengers

fuel for the flight

cargo

4.

MULTIPLE SELECT QUESTION

45 sec • 1 pt

Which of these are limitations?

Select all that apply

Zero fuel weight

Maximum certificated take off weight

Maximum landing weight

Ramp weight

5.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

A lateral fuel imbalance in a light aircraft will cause...

the nose to pitch up

the nose to pitch down

the aircraft to be unable to take off

one wing to be heavier than another

6.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Your AUW = 4800 kg and total moment = 604800. The CG is at STA 126, with CG limits between STA 123 and 128. You need to offload 200 kg from STA 161. What station will the new CG for the aircraft be at?

124

120

130

129

121

7.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

If a Station has a negative value, eg: STA -40, this means that...

the station is in front of the datum

the station is behind the datum

weight must be removed from that station

weight can be added to that datum

8.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Given: Gross weight = 1838 kg with CH at STA 27, MCTOW = 4000 kg. At which station can you load 240 kg of cargo to put the aircraft CG at STA 35?

96

27

86

43

9.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Zero Fuel Weight is equal to...

APSW + payload

APSW + fuel

Ramp weight + fuel

Gross weight + fuel