A2. The capability to perform microminiature
REVIEW SUBSET NUMBER 3
A1. In parallel.
The highest range.
REVIEW SUBSET NUMBER 7
A3. Open circuit.
A1. Common and peculiar.
A2. The MA-2 aircraft electrical power test set.
A5. Circuit shorting to ground.
A6. (1) The VOM can load the circuit, and
REVIEW SUBSET NUMBER 8
(2) the meter movement is easy to damage.
A1. A power-off condition.
A2. SND mode.
A3. Open circuit signature.
interferes with normal signal flow.
A4. The test leads are only conductive at the
A5. 270 ohms.
REVIEW SUBSET NUMBER 4
REVIEW SUBSET NUMBER 9
A1. Jet ignition system tester.
A2. Make the ground connection for the power
A3. 15 inches maximum.
A3. 95 to 135 Vac.
REVIEW SUBSET NUMBER 10
REVIEW SUBSET NUMBER 5
A1. Aircraft Structural Hardware for Aircraft
Repair, NAVAIR 01-1A-8.
A2. Corrosion, strength, size, length, magnetic
properties, special features, and lubrication
or coating of the substitution part.
A3. To separate the wire bundle from the
REVIEW SUBSET NUMBER 11
A4. (1) Lock wire, (2) shear wire, (3) seal wire.
A2. Debugging new programs.
A5. To ensure that all metal parts of the aircraft
have the same electrical charge.
REVIEW SUBSET NUMBER 12
REVIEW SUBSET NUMBER 6
A1. 20 volts.
A1. Aircraft Weapons Systems Cleaning and
Corrosion Control, NAVAIR 01-1A-509,
A3. 250,000 ohms.
and Avionic Cleaning and Corrosion
Prevention/Control, NAVAIR 16-1-540.