SEPERATE ( FALSE )345–346. An external tank may be formed by spaces between frames or other cavities within theengine.A store of fluid may also be held in a gearbox.INTERNAL ( FALSE )
347–348. A separate, external tank is usually constructed of sheet steel or stainless steel.ALLUMINIUM( FALSE )349–350. The tank is designed to furnish a constant supply of oil for all approved flight manoeuvres.(TRUE )351–352. Most oil reservoirs are unpressurised to suppress foaming and supply a head of pressure,forcing the oil to the pump inlet.PRESSURISED ( FALSE )353–354. An oil tank needs expansion space of at least 40% of the tank capacity.10% ( FALSE )355–356. Filling and replenishing the oil is done remotely or at the oil tank.DRAINING ( FALSE )357–358. A filler cap is usually corporated for manual filling with oil cans.INCORPORATED ( FALSE )359–360. Pressure and overflow ports may be included for filling from a pressure rig.( TRUE )361–362. The tank may have a low point of usable oil.This area collects any sediment and is the pointfor draining the tank.UNUSABLE ( FALSE )363–364. Vane pump - most common type consists of two meshed gears that rotate inside a housingwith minimum clearance between gear & housing.GEAR ( FALSE )365–366. Gear pump - consists of a housing that contains a steel sleeve with off centre bore. 4 vanes,hollow steel rotor and a coupling that turns the rotor.VANE ( FALSE )367–368. Gerotor pump - consists of a an engine driven spur gear that rotates within a free spinningrotor housing, the housing has two oblong openings (oil inlet & oil outlet).( TRUE )369–370. The oil scavenge pump may also be a gear, vane or gerotor type pump that is driven by thegenerator.ENGINE ( FALSE )371–372. In many reciprocating engine oil pumps, the pressure pump and scavenge pumps are oftenenclosed in the one housing.TURBINE ( FALSE )373–374. Pressure oil filters are positioned upstream from the oil pump.DOWNSTREAM ( FALSE )375–376 - Spacer thickness determines particle width filtration.SIZE ( FALSE )INNUMERATION :377–379. Types Of Air Inlets•SUBSONIC INLETS•SUPERSONIC INLETS•TURBOPROP INLETS380–382. The typical turbosupercharger is composed of three main parts:•COMPRESSOR ASSEMBLY•TURBINE WHEEL ASSEMBLY•A FULL FLOATING SHAFT BEARING ASSEMBLY383–385.A sea level booster turbo supercharger system used widely is automatically regulated bythree components:•EXHAUST BYPASS VALVE ASSEMBLY•DENSITY CONTROLLER•DIFFERENTIAL PRESSURE CONTROLLER
386–388. Types of bearings•PLAIN BEARING•ROLLER BEARING•BALL BEARING389–391. Types of Friction•ROLLING FRICTION•SLIDING FRICTION•WIPING FRICTION392–397. The principal units in a typical reciprocating engine dry sump oil system includes:•AN OIL SUPPLY TANK•AN ENGINE-DRIVEN PRESSURE OIL PUMP•A SCAVENGE PUMP•AN OIL COOLER WITH AN OIL COOLER CONTROL VALVE•OIL TANK VENT, - NECESSARY TUBING•PRESSURE AND TEMPERATURE INDICATORS.
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Gas turbine, engine inlet