C-17 2AXXX Production Team Member Exam Review

C-17 2AXXX Production Team Member Exam Review

Professional Development

26 Qs

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C-17 2AXXX Production Team Member Exam Review

C-17 2AXXX Production Team Member Exam Review

Assessment

Quiz

Other

Professional Development

Medium

Created by

Elliot Rivera

Used 6+ times

FREE Resource

26 questions

Show all answers

1.

MULTIPLE CHOICE QUESTION

1 min • 4 pts

How many degrees is the radiation hazard area of the color weather radar system on the C-17A aircraft?

280 degrees

240 Degrees

180 Degrees

360 Degrees

Answer explanation

IAW T.O. 1C-17A-2-34JG-40-1, 34-41-01 Warning

2.

MULTIPLE CHOICE QUESTION

1 min • 4 pts

The _______ helps to make the TOs easier to use.

type of maintenance and system described in the manual

CTRL+F

applicability code

S/S/SN

Answer explanation

IAW T.O. 1C-17A-2-00GV-00-1, PAGE 1-12, PARA. 1-186

3.

MULTIPLE CHOICE QUESTION

1 min • 4 pts

Aircraft jacking, towing, and taxiing is not allowed with a lateral fuel imbalance between wings that exceeds _______of fuel.

16,000 lbs

80,000 lbs

8000 lbs

2 tons

Answer explanation

IAW T.O. 1C-17A-2-12JG-28-1, PAGE 1-6, WARNING

4.

MULTIPLE CHOICE QUESTION

1 min • 4 pts

Operation of the fuel boost pumps from the Ground Refuel Control panel is possible only when the POWER switch is in _______.

Refuel

Defuel

OFF

Neutral

Answer explanation

IAW T.O. 1C-17A-2-12JG-28-1, PAGE 2-80, SPECIAL INSTRUCTION

5.

MULTIPLE CHOICE QUESTION

1 min • 4 pts

How should you approach the wheels during a "hot brake" event?

From any direction

From the side

From above the tire

From the front or aft only

Answer explanation

IAW T.O. 1C-17A-2-00GV-00-1, PAGE 3-9, PARA. 3-70

6.

MULTIPLE CHOICE QUESTION

1 min • 4 pts

Which Job Guide is used to perform C-17A refueling?

12JG-28-01

00GV-00-1

00JG-00-1

29JG-10-01

Answer explanation

IAW 1C17-A-E12-28-0100-00001-999A-A (12-28-01)

7.

MULTIPLE CHOICE QUESTION

1 min • 4 pts

If the primary climb and dive valve has failed, it is permissible to continue refueling as long as the wing pressure does not exceed 1.7 PSIG and the secondary valve is functional.

True

False

Answer explanation

IAW T.O. 1C-17A-2-12JG-28-1, PAGE. 2-72, S/S/SN 12-28-01-5

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