Use LEFT and RIGHT arrow keys to navigate between flashcards;
Use UP and DOWN arrow keys to flip the card;
H to show hint;
A reads text to speech;
41 Cards in this Set
- Front
- Back
|
C-130 engines? |
Four Allison T56-A-16, turboprop, constant speed engines. |
|
|
Reduction Gear Assembly (RGB) reduces what? |
The RPM of the prop to the engi |
|
|
RGB is located where? |
Between the torque meter and the prop |
|
|
Torque Meter assembly transmits ________? |
Torque from the engine to Reduction gearbox |
|
|
The torque meter is located where? |
Between the engine and reduction gearbox |
|
|
The torque meter assembly is located? |
Between the engine and the reduction gearbox |
|
|
Compressor assembly compresses what? |
Air for the engine to run |
|
|
Compressor assembly is located where? |
On the forward section of the engine |
|
|
The Diffuser channels what? |
The air from the compressor to the combustion section. |
|
|
The diffuser provides what? |
Mounting for engine bleed air ducts used for engine starting and pressurization |
|
|
The diffuser is located where? |
Between the compressor and combustion section |
|
|
Combustion section is where what? |
Fuel is injected into compressed air and ignited through six connected combustion chambers |
|
|
Combustion section is located where? |
Between the diffuser and turbine |
|
|
The turbine unit converts what? |
Heat energy into mechanical energy to drive the compressor and necessary accessories |
|
|
The Turbine is located where? |
Aft of the combustion section |
|
|
The accessory drive housing provides what? |
Mounting pads for numerous engine driven accessories |
|
|
The accessory drive is located on what? |
The lower section if the compressor |
|
|
What kind of propellors do we have? (C-130) |
Hamilton Standard 54-H60-111 hydromatic, four blade, constant-speed props with full feathering and reversible pitch |
|
|
What does the Propeller Control Assembly control? |
Prop blade pitch at all power settings, and is compromised of the valve housing and pump housing |
|
|
Where is the prop control located? |
Between the propeller and reduction gearbox |
|
|
Dome assembly contains what? |
The piston that changes the propellor blade angle with hydraulic power from the pump housing |
|
|
Dome assembly is located where? |
Forward of the blade hub assembly |
|
|
Dome assembly is located where? |
Forward of the blade hub assembly |
|
|
Propeller anti-ice/de-ice provides |
Electrical anti-ice and de-icing of the propeller |
|
|
Dome assembly is located where? |
Forward of the blade hub assembly |
|
|
Propeller anti-ice/de-ice provides |
Electrical anti-ice and de-icing of the propeller |
|
|
Prop anti-ice is located where |
On each blade, spinner and after-body assembly |
|
|
What are the two methods of refueling the c-130? |
Single point refueling and gravity refueling |
|
|
What are the two methods of refueling the c-130? |
Single point refueling and gravity refueling |
|
|
Single point refueling (SPR) panel is located where? |
Aft of the right hand main wheel well |
|
|
Gravity refueling is accomplished where? |
Over the wing, through a cap at the top of the tank |
|
|
Gravity refueling is accomplished where? |
Over the wing, through a cap at the top of the tank |
|
|
Low point drains are located where? What is there purpose? |
On each tanks underside. To draw fuel from the tanks and inspect for the presence of contamination |
|
|
Fuel dump system is designed to what? |
Pump fuel out of the aircraft during an in-flight emergency by using dump pumps, dump valves and dump manifold plumbing |
|
|
What is the purpose of the fuel cross feed system? |
To enable the crew to use fuel from any tank to feed any engine in-flight or on the ground. |
|
|
What is the purpose of the fuel cross feed system? |
To enable the crew to use fuel from any tank to feed any engine in-flight or on the ground. |
|
|
What does the fuel vent system provide? |
A means to equalize tank pressure and prevent purge tanks from overfilling |
|
|
Explain the Bleed Air System |
Consists of high-pressure ducts and valves which direct compressed air to the pneumatically operated systems of the aircraft |
|
|
Auxiliary power unit (apu) supplies what? |
Supplies air for ground operation of the air-conditioning systems, for engine starting, and provides shaft power to drive a 40-kva ac generator. |
|
|
Auxiliary power unit (apu) supplies what? |
Supplies air for ground operation of the air-conditioning systems, for engine starting, and provides shaft power to drive a 40-kva ac generator. |
|
|
APU is located where? |
Forward of the port wheel well |
