100 LL gasoline is:

When applying carburetor heat on an aircraft fitted with a fixed pitch propeller there will be a drop in rpm because:

If the correct grade of aviation gasoline is unavailable in an emergency situation then it is probably acceptable to use:

A piston engine aircraft cruises more economically at high altitude than at low altitude at the same power setting because:

During a level balanced turn, increasing the airspeed will ____ the turn radius and _____ the rate of turn.

If the stalling speed in level flight is 50 knots then the stalling speed in a level turn with a 30° angle of bank will increase to:

The 4 strokes of a piston engine typically found in light aircraft are (in sequence)

The tower at Buttonville airport reports that the wind is $$090/20$$ and runway 03 is in use. The magnetic variation is $$22∘W$$. The headwind component is

Which of the following effects are a consequence of airframe icing

How is the propeller pitch controlled on an aeroplane fitted with a constant speed propeller

Fuel injection systems

The tower at Buttonville airport reports that the wind is 090/20 and runway 03 is in use. The magnetic variation is 22°W. The crosswind component is:

Prior to a flight, you receive the following CRFI report: CYVR CRFI 08/26 5 .3 9902231300 At 1400, the ATIS information reports that the wind at Vancouver international is 020/15, that runway 08 is in use and that heavy rain is falling. Under these conditions, the maximum crosswind component in which a landing would be recommended is:(Crosswind limit charts are provided in Appendix A9) (Ref: 5.1.15)

Based on the following information, is it advisable to operate an aircraft on the runway at Kitchener airport?CYKF CRFI RWY 07 /25 - 1 .28 9702210600 The control tower reports the wind as being 130/20.

The maximum crosswind component which the aircraft, as a general rule would be able to handle is __ knots and it is therefore __ to conduct take-off and landings in this aircraft under the described conditions.

In a piston engined aircraft, maximum range will be achieved by flying at:

When would you expect an aircraft to generate the most severe wing tip vortices?

When trimming an aircraft "nose down", the trim tab moves ___ and the elevator moves ___

Whether or not a wing is stalled depends on:

In zero wind conditions, a lightly loaded aircraft is:

Using fuel with an octane rating of 87 in an aircraft which is designed to operate on fuel with an octane rating of 100 will result in:

Service ceiling is:

Maximum endurance in a piston engine aircraft will be achieved:

It is more desirable for the wing __ to stall before the wing ___ and ___ is used to help accomplish this (Ref: 5.1.9)

100LL aviation gasoline weighs approximately: (Ref: 4.1.1)

Valve overlap means:

An increase in weight causes an increase in ___ drag which will mainly affect __ speed performance (Ref: 5.1.3)

Which of the following devices is used to reduce adverse aileron yaw? (Ref: 5.1.12)

Touching down on the nose wheel first is usually as a result of: (Ref: 5.1.15)

An aircraft with a forward cg location will cruise ___ an identical aircraft which weighs the same but has a more rearward cg location (Ref: 5.1.4)

Which of the following has an effect on the lateral stability of an aircraft? (Ref: 5.1.11)

When gliding into a headwind at the "Best Glide" speed given in the POH, the glide range will be __ and the glide endurance will be ___ as compared to the zero wind situation (Ref: 5.1.8)

Differential ailerons are (Ref: 5.1.12)

The mixture must be leaned as altitude increases so as to: (Ref: 5.1.13)

Ground effect is most noticeable on ___ wing aircraft with ___ aspect ratio (Ref: 5.1.3)

Which of the following best describes ground effect? (Ref: 5.1.3)

Static stability refers to

Dynamic stability refers to

An anti-servo tab

Weight affects which component of drag

The function of control surface mass balances is to

The purpose of stall strips on the leading edge of a wing is to

Which grade of oil is appropriate for winter operations?

A windsock hanging about 30° below the horizontal indicates a wind strength of about:

Given that the stall speed of an aircraft is 50 knots, what is the approximate maximum crosswind capability of the aircraft?

Which of the following design features may be used to control wing tip stalling?

With a strong quartering tailwind from the left, the controls should be in the following position:

Raising the tail during the take-off run on a conventional gear aircraft will cause the nose to yaw to the ___ while pitching the nose up to lift off will cause the nose to yaw to the ____ if not corrected with the application of rudder

Wheelbarrowing during the takeoff can be caused by

In order to achieve maximum endurance in a piston engine aircraft with a fixed pitch propeller, the aircraft should be flown

In order to achieve maximum range in still air conditions, the aircraft should be flown

You are in a left turn bank and the ball is to the left of centre. This situation is known as a ____ and appropriate corrective action is to ____

As the angle of attack of a wing is increased towards the stall, the __ moves __

In comparison with an identical but lighter weight aircraft, a heavy aircraft will glide ___ distance and have ___ glide endurance

Application of carburetor heat will cause ____ if carburetor icing has been encountered

A laminar flow wing will have its point of maximum thickness located at around __ chord from the leading edge whereas a conventional wing will have its point of maximum thickness at around ____ chord from the leading edge

Failing to lean the mixture on a normally aspirated engine at altitude will cause:

Wing tip vortices are strongest from aircraft flying ___ in the __ configuration

An aeroplane fitted with a fine pitch propeller will exhibit better ___ performance while an aeroplane fitted with a coarse pitch propeller will exhibit better __ performance

Identify the CORRECT statement

A thin layer of frost on aeroplane wings will have the following effect on an aeroplane

The stall speed for an aircraft in straight and level flight is 58 knots. In a 60° bank, the stall speed will be

Pitch or _____ stability refers to stability about the ___ axis

A forward CG location (within limits) will cause the aircraft to ____ as compared to one with a rearward CG location (within limits)

The longitudinal, lateral and vertical axes all pass through

Carburetor icing can occur

An aircraft which is loaded such that the CG is behind the aft limit will be unstable about the ___ axis

Winglets reduce drag significantly in the following phases of flight

While flying in icing conditions, ice will probably first accumulate on

Why is a propeller twisted to have a coarse pitch at the root and a fine pitch at the propeller tips