P-3 Eaws (Power Plants) Mprf-001

Front 1

P-3 EAWS (Power Plants)

What are the hazards and areas around the P-3 engine

Back 1

Propeller Area
Propeller Jet Blast Area

Front 2

P-3 EAWS (Power Plants)

The ______-______ ______ should be on when aircraft engines are running on deck.

Back 2

Anti-collision light

Front 3

P-3 EAWS (Power Plants)

The P-3 series aircraft is equipped with how many and what type of aircraft engine.

Back 3

Four
T56-A-14 Turboprop

Front 4

P-3 EAWS (Power Plants)

The Engine Power Lever System includes how many sub-systems?

Back 4

Four Independent Subsystems

Front 5

P-3 EAWS (Power Plants)

What are the basic elements of each power lever subsystem.

Back 5

A pair of engine power levers, one each for the pilot and copilot

Front 6

P-3 EAWS (Power Plants)

Where are the Engine Power Levers located.

Back 6

The four pilot levers are installed as a group on top of the center console at the left end at the flight station and the copilot levers are similarly grouped at the right end.

Front 7

P-3 EAWS (Power Plants)

What does the term "feathered" mean in reguards to Props?

Back 7

The blades are laid flat with the airstream to minimize drag in event the engine is shutdown inflight.

Front 8

P-3 EAWS (Power Plants)

How many fuel tanks are on the P-3 and where are they located?

Back 8

left to right (facing forward) No. 1, No. 2, No. 3 and No. 4 fuel tanks. The auxiliary fuel tank system is No. 5 fuel tank

Front 9

P-3 EAWS (Power Plants)

Each tank can supply fuel to its respective engine or fuel can be supplied from any wing tank to any engine through a _____ ____ ______.

Back 9

Cross Feed System

Front 10

P-3 EAWS (Power Plants)

Where is fuel tank number 5 and how many partsdoes it have?

Back 10

2 ,The integral wing center section fuel tank and the other a bladder cell fuel tank in the fuselage?

Front 11

P-3 EAWS (Power Plants)

Normally, aircraft fueling is accomplished by _____ ____ _____ fueling.

Back 11

Center Point Pressure

Front 12

P-3 EAWS (Power Plants)

What is the total fuel capacity of the P-3C.

Back 12

9200 gallons

Front 13

P-3 EAWS (Power Plants)

The engine bleed air system that provides heated and pressurized air for what systems?

Back 13

Compressor for bomb bay heating, engine anti-ice, wing de-ice, oil cooler augmentation and cross-bleed engine starting

Front 14

P-3 EAWS (Power Plants)

What are the part to the auxiliary power unit (APU)?

Back 14

a compressor, gas turbine engine, and an engine-driven electrical generator

Front 15

P-3 EAWS (Power Plants)

The APU compressor bleed air provides the _____ _____ required for engine starting and a source of air for operation of the aircraft _______ _______ ______

Back 15

Pneumatic Power
Environmental Control System

Front 16

P-3 EAWS (Power Plants)

APU provides aircraft electrical power for both ___-__-___ and _________ __-_____ _______.

Back 16

On-the-ground
Emergency in-flight operations