INDUCCIÓN TLA I

Which statement below reflects a typical requirement when towing some aircraft ?. Discharge all hydraulic pressure to prevent accidental operation of the nosewheel steering mechanism. Tailwheel aircraft must be towed backwards. If the aircraft has a steerable nosewheel, the torque-link lock should be set to full swivel.

Which statement(s) is/are true regarding tiedown of small aircraft ? 1. Manila (hemp) rope has a tendency to stretch when it gets wet. 2. Nylon or dacron rope is preferred to manila rope. 3. The aircraft should be headed downwind in order to eliminate or minimize wing lift. 4. Leave the nosewheel or tailwheel unlocked. 1, 2, 3, and 4. 1 and 2. 2.

When approaching the front of an idling jet engine, the hazard area extends forward of the engine approximately. 10 feet. 15 feet. 25 feet.

Which of the following is the most satisfactory extinguishing agent for use on a carburetor or intake fire ?. Dry chemical. A fine, water mist. Carbon dioxide.

(Refer to Figure 50.) Identify the signal to engage rotor on a rotorcraft. 1. 3. 2.

If a radial engine has been shut down for more than 30 minutes, the propeller should be rotated through at least two revolutions to. check for hydraulic lock. check for leaks. prime the engine.

(Refer to Figure 51.) Which marshalling signal should be given if a taxiing aircraft is in imminent danger of striking an object ?. 1 or 3. 2. 3.

What effect, if any, will Aviation Gasoline (AVGAS) mixed with Jet Fuel (JET A1) have on a Turbine Engine?. No appreciable effect. The tetraethyl lead in the gasoline forms deposits on the turbine blades. The tetraethyl lead in the gasoline forms deposits on the compressor blades.

(1) Jet fuel is of higher viscosity than aviation gasoline and therefore holds contaminants better. (2) Viscosity has no relation to contamination of fuel. Regarding the above statements,. only No. 1 is true. both No. 1 and No. 2 are true. neither No. 1 nor No. 2 is true.

When towing a large aircraft. a person should be in the cockpit to watch for obstructions. persons should be stationed at the nose, each wingtip, and the empennage at all times. a person should be in the cockpit to operate the brakes.

Weathervaning tendency is greatest when taxiing. both nosewheel and tailwheel-type airplanes in a quartering tailwind. a tailwheel-type airplane in a direct crosswind. a nosewheel-type airplane in a quartering headwind.

When taxiing an airplane with a quartering tailwind, the elevators and. upwind aileron should be held in the up position. upwind aileron should be held in the down position. both ailerons should be kept in the neutral position.

When taxiing (or towing) an aircraft, a flashing red light from the control tower means. stop and wait for a green light. move clear of the runway/taxiway immediately. return to starting point.

A person should approach or leave a helicopter in the pilot's field of vision whenever the engine is running in order to avoid. the tail rotor. the main rotor. blowing dust or debris caused by rotor downwash.

When taxiing (or towing) an aircraft, a flashing white light from the control tower means. move clear of the runway/taxiway immediately. OK to proceed but use extreme caution. return to starting point.

When taxiing (or towing) an aircraft, an alternating red and green light from the control tower means. move clear of the runway/taxiway immediately. OK to proceed but use extreme caution. return to starting point.

When stopping a nosewheel-type airplane after taxiing (or towing), the nosewheel should be left. unlocked and pointed straight ahead. turned at a small angle towards uphill if the parking area is not perfectly flat. pointed straight ahead.

When first starting to move an aircraft while taxiing, it is important to. test the brakes. closely monitor the instruments. notify the control tower.

The color of 100-LL fuel is. blue. colorless or straw. red.

Why is ethylene dibromide added to aviation gasoline ?. To remove zinc silicate deposits from the spark plugs. To scavenge lead oxide from the cylinder combustion chambers. To increase the antiknock rating of the fuel.

STUDY QUESTIONS: FIRE PROTECTION. Three things that are necessary for a fire are:.

STUDY QUESTIONS: FIRE PROTECTION. A fire involving paper as a fuel is a class ____.

STUDY QUESTIONS: FIRE PROTECTION. A fire involving a flammable liquid as a fuel is a class ______.

STUDY QUESTIONS: FIRE PROTECTION. A fire involving an energized electrical system is a class _____.

STUDY QUESTIONS: FIRE PROTECTION. A fire involving combustible metals is a class.

A fire extinguisher suitable for use on a Class-A fire is identified by a. Red square. Blue circle. Yellow star. Green triangle.

A fire extinguisher suitable for use on a Class-B fire is identified by a. Red square. Blue circle. Green triangle. Yellow star.

A fire extinguisher suitable for use on a Class-C fire is identified by a. Red square. Blue circle. Yellow star. Green triangle.

A fire extinguisher suitable for use on a Class-D fire is identified by a. Yellow star. Green triangle. Red square. Blue circle.

A fire extinguishing agent with a toxicity rating of 2 is ___________ (more or less) toxic than one with a rating of 6. less. more.

STUDY QUESTIONS: AVIATION FUELS. Two reasons the use of aviation gasoline should be limited in turbine engines are.

STUDY QUESTIONS: AVIATION FUELS. The reason jet fuel must not be used in reciprocating engines is that it causes ________.

The Viscosity of Jet Fuel is __________ (Higher or Lower) than that of aviation gasoline (AVGAS). Higher. Lower.

Give the color of each of these Grades of Aviation Gasolines (AVGAS). Grade 80. Grade 100. Grade 100LL.

STUDY QUESTIONS: AVIATION FUELS. Aviation gasoline whose antidetonation characteristics are better than those of the reference fuel (100-octane) are rated in _____________.

The Antiknock characteristic of aviation gasoline is increased by using ______________ as an additive. Tetraethyl Lead. Ethylene Dibromide.

Lead contaminants are purged from the combustion chamber of a reciprocating engine by adding ______________to the gasoline. Ethylene Dibromide. Tetraethyl Lead.

The heat energy content per gallon of jet fuel is _____________ (greater or less) than that of aviation gasoline. Greater. Less.

An uncontrolled burning or explosion of the fuel-air mixture within the cylinder of a reciprocating engine is called ______________. Detonation. Antidetonation.

If its vapor pressure is too high, a fuel will vaporize too __________ (Readily or Slowly). Readily. Slowly.

Vapor Lock can occur when the vapor pressure of the fuel is too ____________ (High or Low). High. Low.

The designations of jet engine fuel ________ (do or do not) relate to the performance of the fuel in the engine. Do. Do Not.

In the Dual-Number Rating System for aviation gasoline, 100/130 aviation gasoline has an octane rating of 100 with a (Lean or Rich mixture). Lean mixture. Rich mixture.

Liquid gasoline ___________ (will or will not) bum. will burn. will not burn.

STUDY QUESTIONS: AVIATION FUELING. Two bits of information must be marked on the FUEL TANK for a reciprocating-engine-powered aircraft are:.

STUDY QUESTIONS: AVIATION FUELING. If the aircraft is equipped for pressure Fueling and Defueling, two bits of information are displayed at the FUELING CONTROL PANEL. These are:.

STUDY QUESTIONS: AVIATION FUELING. Water is removed from the fuel carried in a fuel tank truck by passing the fuel through a __________ before it is pumped into the aircraft.

Before fuel is pumped into an aircraft fuel tank, the fuel nozzle should be electrically connected to the aircraft structure, the fuel truck should be connected to the aircraft, and both the fuel truck and the aircraft should be electrically connected to the ____________. air. ground.

A fire extinguisher must be readily available when fueling an aircraft. The recommended Type of Extinguisher uses __________ as the Extinguishing Agent. CO2. HC2. H2O.

What important precaution should be taken before pumping fuel into a fuel tank by the over-wing method? The fuel nozzle and the aircraft should be __________. Air. Ground.

STUDY QUESTIONS: AVIATION FUELING. It _______________________ (is or is not) normally safe to defuel an aircraft in an air conditioned hangar.

Refer to the figure below. Identify the meaning of each of these signals. Signal A. Signal B. Signal C. Signal D.

Refer to the figure below. Identify the meaning of each of these signals. Signal A. Signal B. Signal C. Signal D.

STUDY QUESTIONS: AVIATION TIEDOWN. The proper knot for securing an aircraft to its tiedown with a rope is a _________ knot.

When a Tail Wheel Airplane is tied Down Facing the Wind, the Elevators should be secured in their full __________ (up or down) position. Up. Down.

When a Tail Wheel Airplane is tied Down Facing Away from the Wind. the elevators should be secured in their full (up or down) position. Up. Down.

One of the drawbacks for the use of manila rope for tying down an aircraft is the fact that manila rope __________ (shrinks or stretches) when it gets wet. shrinks. stretches.

It is necessary when installing Jack Pads on some aircraft that the Stress from the pad be evenly distributed through the structure by the installation of ________________. stress plates. tension plates. compression plates.

A wing jack is prevented from collapsing because of a hydraulic leak by the use of a ______________ screwed on the threaded jack strut. collar. tow bar.

Removal of ice after it has formed on an aircraft structure is called ______________. de-icing. anti-icing.

Preventing the formation of ice on an aircraft structure is called _____________. anti-icing. de-icing.

Deicing is normally accomplished by using _________ (heated or cold) FPD fluid. heated. cold.

The FPD fluid that is best suited for anti-icing is Type ___________ (I or II). I. II.

When starting an aircraft engine equipped with a float-type carburetor, the carburetor heat control should be in the (hot or cold) position. Hot position. Cold position.

The most satisfactory Fire-Extinguishing Agent for putting out an Induction Fire in an aircraft engine is _____________. CO2. H2O. NFPA.

Oil collected in the lower cylinders of a Radial Engine can cause a problem known as. Vapor Lock. Hydraulic Lock.

horizontally opposed engine equipped with a fuel injection system is primed by placing the mixture control in the ______________ position and turning on the boost pump. FULL RICH. IDLE CUTOFF POSITION.

A flooded reciprocating engine using either a float carburetor or a fuel injection system can be cleared of excessive fuel by placing the mixture control in the ___________position. Turn the ignition off, open the throttle. and crank the engine with the starter or by hand until the fuel charge in the cylinders has been cleared. CUTOFF POSITION. FULL RICH POSITION.

As soon as a reciprocating engine is started, you should check for an indication of ____________. Oil pressure. Oil Temperature. Oil Quantity.

The mixture control of a float-type carburetor should be placed in the __________ position for starting the engine. FULL RICH. CUTOFF POSITION.

A Turbine Engine start in which the engine lights off but does not accelerate to a speed that allows it to operate without help from the starter is called a/an __________ start. HUNG START. HOT START. NO OIL PRESSURE.

A turbine engine start in which the engine lights off but its temperature exceeds the allowable limits is called a/an _________ start. HUNG START. HOT START. NO OIL PRESSURE.

The hazard area extends out Ahead of an Idling Turbojet Engine for about __________ feet. 25 feet. 100 feet.

The hazard area extends out Behind an Idling Turbojet Engine for about ___________ feet. 100 feet. 25 feet.

A Hot Start of a Turbojet Engine is often caused by an excessively ____________ (rich or lean) mixture. Rich mixture. Lean mixture.