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WorksheetsAES - Pneudraulic System
Total questions: 25
Worksheet time: 24mins
Branch of science and technology concerned with the conveyance of liquids through pipes and channels, expeciall as a source of mechanical force.
(a)
Is the system that uses compressed air to transmit and control energy.
(a)
A device any of various tools and instrument that generate and utilize compressed air.
(a)
Derived from the words Pneumatics and Hydraulics. It is a term used in the discussing system on military aircraft that used either some or combination of Pneumatic and Hydraulic system.
(a)
LANDING GEAR:
The aircraft is equipped with a ___________ landing gear.
non retractable tail dagger
non retractable tricycle landing gear
non retractable conventional gear
retractable conventional gear
LANDING GEAR
Is the statement true or false?
The landing gear of t41 consists of Cessna flat steel sprin or tubular spring steel main gear struts and a steerable nose wheel mounted on an air-oil shock strut comprises the main landing gear.
False, MAIN LANDING GEAR should be NOSE GEAR
False, CESSNA FLAT STEEL SPRING should be CESSNA FLAT ALLOY SPRING
False, STEERABLE NOSE WHEEL should be NOSE GEAR
True
A steerable nose wheel mounted on an air oil shock strut comprises the nose gear.
(a)
NOSE LANDING GEAR:
What minimizes wheel shimmy?
(a)
NOSE LANDING GEAR:
What is attached to the forgings riveted to the firewall and lower fuselage?
(a)
I provide nose gear resistance to shimmy
What am I?
(a)
I am forged alloy that keep the lower strut aligned in the nose gear steering system.
(a)
(a) is accomplished through used of the rudder pedals. Two spring loaded push pull tubes connect to the rudder bars to the nose gear.
(a) is afforded up to approximately 10 degrees either side of neutral, after which brakes maybe used to gain a maximum deflection of 30 degree right or left from the center.
(a) are spring-loaded and should not be disassembled internally. These are connected by clevises to rod ends extending from the steering arm assembly on the nose ear and by a ball joint connection at the rudder pedal crossbars.
What am I?
(a)
(a) is attached to forgings in the landing gear bulkhead structure.
(a) is attached with the wheel thru-bolts or Cap screws and becomes an integral part of the wheel.
Consists of 6.00X6 ply rating tire, 6.00X6 inner tube and 6.00X6 wheel assembly.
Its single brake disc is secured to the wheel inner section.
(a)
How many inches is the minimum allowable thickness of brake disc?
(a)
BRAKE SYSTEM
It is located just forward of the pilot rudder pedal, are actuated by applying toe pressure on the rudder pedal.
(a)
MASTER BRAKE CYLINDER
(a) is incorporated with each master cylinder.
(a) are rigid aluminum tubing, except flexible hosed used at master cylinders and at wheel brake assemblies. A separate line is used to connect each master cylinder to its corresponding wheel brake cylinder.
A handle and ratchet mechanism connected by a cable to linkage at the master cylinder. Pulling out the handle depresses both master cylinder piston rods and the ratchet locks the handle in this position until the handle is turned and released.
(a)
(a) consists of housing, piston, pressure plate, back plate, linings riveted on pressure plate and back plate.
(a) should be replaced when they are worn to a minimum thickness of 3/32 inch.
