Powerplant
Test Question Bank
Please
Note:
Subject
matter codes appear above each item.
A.8.0.0.1.A.1 A01
Which
statement is true regarding bearings used in high powered reciprocating aircraft
engines?
A. Crankshaft bearings are generally of the ball-type
due to their ability to withstand extreme loads without overheating.
B. There is less rolling friction when ball bearings
are used than when roller bearings are employed.
C. The outer race of a single row, self aligning
ball bearing will always have a radius equal to the radius of the balls.
A.8.0.0.2.B.1 A01
A condition
that can occur in radial engines but is unlikely to occur in horizontally
opposed engines is
A. valve overlap.
B. zero valve clearance.
C. hydraulic lock.
A.8.0.0.3.A.1 A01
Which
condition would be the least likely to be caused by failed or failing engine
bearings?
A. High oil temperatures.
B. Low oil temperatures.
C. Excessive oil consumption.
A.8.0.0.4.A.1 A01
What
is the principal advantage of using propeller reduction gears?
A. To enable the engine RPM to be increased with
an accompanying increase in power and allow the propeller to remain at a lower,
more efficient RPM.
B. To enable the engine RPM to be increased with
an accompanying increase in propeller RPM.
C. To enable the propeller RPM to be increased
without an accompanying increase in engine RPM.
A.8.0.0.5.A.1 A01
Which
of the following will decrease volumetric efficiency in a reciprocating engine?
1. Full throttle operation.
2. Low cylinder head temperatures.
3. Improper valve timing.
4. Sharp bends in the induction system.
5. High carburetor air temperatures.
A. 1, 2, 3, and 4.
B. 3, 4, and 5.
C. 2, 4, and 5.
A.8.0.0.6.A.1 A01
Which
of the following is a characteristic of a thrust bearing used in most radial
engines?
A. Tapered roller.
B. Double row ball.
C. Deep groove ball.
A.8.0.0.7.A.1 A01
Which
bearing is least likely to be a roller or ball bearing?
A. Master rod bearing (radial engine).
B. Rocker arm bearing (overhead valve engine).
C. Crankshaft main bearing (radial engine).
A.8.0.0.8.A.1 A01
The
operating temperature valve clearance of a radial engine as compared to cold
valve clearance is
A. less.
B. greater.
C. the same.
A.8.0.0.9.A.1 A01
A nine
cylinder engine with a bore of 5.5 inches and a stroke of 6 inches will have
a total piston displacement of
A. 1,425 cubic inches.
B. 1,283 cubic inches.
C. 740 cubic inches.
A.8.0.1.0.A.1 A01
The
five events of a four stroke cycle engine in the order of their occurrence
are
A. intake, power, compression, ignition, exhaust.
B. intake, ignition, compression, power, exhaust.
C. intake, compression, ignition, power, exhaust.
A.8.0.1.1.A.1 A02
The
primary concern in establishing the firing order for an opposed engine is
to
A. keep power impulses on adjacent cylinders
as far apart as possible in order to obtain the greatest mechanical efficiency.
B. keep the power impulses on adjacent cylinders
as close as possible in order to obtain the greatest mechanical efficiency.
C. provide for balance and eliminate vibration
to the greatest extent possible.
A.8.0.1.2.A.1 A02
If fuel/air
ratio is proper and ignition timing is correct, the combustion process should
be completed
A. when the exhaust valve opens at the end of
the power stroke.
B. 20 to 30° before top center at the end of
the compression stroke.
C. just after top center at the beginning of
the power stroke.
A.8.0.1.3.A.1 A02
Grinding
the valves of a reciprocating engine to a feather edge is likely to result
in
A. normal operation and long life.
B. excessive valve clearance.
C. preignition and burned valves.
A.8.0.1.4.B.1 A02
Which
statement is correct regarding engine crankshafts?
A. Moveable counterweights serve to reduce the
dynamic vibrations in an aircraft reciprocating engine.
B. Moveable counterweights serve to reduce the
torsional vibrations in an aircraft reciprocating engine.
C. Moveable counterweights are designed to resonate
at the natural frequency of the crankshaft.
A.8.0.1.5.B.1 A02
On which
strokes are both valves on a four-stroke cycle reciprocating aircraft engine
open?
A. Intake and compression.
B. Power and exhaust.
C. Exhaust and intake.
A.8.0.1.6.A.1 A02
Master
rod bearings are generally what type?
A. Ball.
B. Roller.
C. Plain.
A.8.0.1.7.A.1 A02
The
actual power delivered to the propeller of an aircraft engine is called
A. brake horsepower.
B. indicated horsepower.
C. friction horsepower.
A.8.0.1.8.A.1 A02
Cam
ground pistons are installed in some aircraft engines to
A. act as a compensating feature so that a compensated
magneto is not required.
B. provide a better fit at operating temperatures.
C. equalize the wear on all pistons.
A.8.0.1.9.A.1 A02
Using
the following information, determine how many degrees the crankshaft will
rotate with both the intake and exhaust valves seated.
Intake
opens 15° BTDC.
Exhaust
opens 70° BBDC.
Intake
closes 45° ABDC.
Exhaust
closes 10° ATDC.
A. 25°.
B. 290°.
C. 245°.
A.8.0.2.0.A.1 A02
Some
aircraft engine manufacturers equip their product with choked or taper-ground
cylinders in order to
A. increase the compression pressure for starting
purposes.
B. flex the rings slightly during operation and
reduce the possibility of the rings sticking in the grooves.
C. provide a straight cylinder bore at operating
temperatures.
A.8.0.2.1.A.1 A02
An aircraft
reciprocating engine using hydraulic valve lifters is observed to have no
clearance in its valve-operating mechanism after the minimum inlet oil and
cylinder head temperatures for takeoff have been reached. When can this condition
be expected?
A. As a result of carbon and sludge becoming
trapped in the lifter and restricting its motion.
B. When the lifters become deflated.
C. During normal operation.
A.8.0.2.2.A.1 A02
What
tool is generally used to measure the crankshaft rotation in degrees?
A. Timing disk.
B. Prop Protractor.
C. Dial indicator.
A.8.0.2.3.A.1 A02
If an
engine with a stroke of 6 inches is operated at 2,000 RPM, the piston movement
within the cylinder will be
A. at maximum velocity around TDC.
B. constant during the entire 360° of crankshaft
travel.
C. at maximum velocity 90° after TDC.
A.8.0.2.4.A.1 A02
If the
intake valve is opened too early in the cycle of operation of a four-stroke
cycle engine, it may result in
A. engine kickback.
B. improper scavenging of exhaust gases.
C. backfiring into the induction system.
A.8.0.2.5.A.1 A02
Some
cylinder barrels are hardened by
A. tempering.
B. shot peening.
C. nitriding.
A.8.0.2.6.A.1 A02
Which
statement is correct regarding a four stroke cycle aircraft engine?
A. The exhaust valve opens on the exhaust stroke.
B. The intake valve closes on the intake stroke.
C. The intake valve closes on the compression
stroke.
A.8.0.2.7.A.1 A02
On which
part of the cylinder walls of a normally operating engine will the greatest
amount of wear occur?
A. Near the center of the cylinder where piston
velocity is greatest.
B. Wear is normally evenly distributed.
C. Near the top of the cylinder.
A.8.0.2.8.B.1 A02
During
overhaul, reciprocating engine exhaust valves are checked for stretch
A. with a contour or radius gauge.
B. by placing the valve on a surface plate and
measuring its length with a vernier height gauge.
C. with a suitable inside spring caliper.
A.8.0.2.9.A.1 A02
When
is the fuel/air mixture ignited in a conventional reciprocating engine?
A. When the piston has reached top dead center
of the intake stroke.
B. When the piston reaches top dead center on
the compression stroke.
C. Shortly before the piston reaches the top
of the compression stroke.
A.8.0.3.0.A.1 A02
Ignition
occurs at 28° BTDC on a certain four-stroke cycle engine, and the intake valve
opens at 15° BTDC. How many degrees of crankshaft travel after ignition does
the intake valve open? (Consider one cylinder only.)
A. 347°.
B. 707°.
C. 373°.
A.8.0.3.1.A.1 A02
What
is the purpose of the safety circlet installed on some valve stems?
A. To prevent valves from falling into the combustion
chamber.
B. To hold the valve spring retaining washer
in position.
C. To hold the valve guide in position.
A.8.0.3.2.A.1 A02
Valve
overlap is defined as the number of degrees of crankshaft travel
A. during which both valves are off their seats.
B. between the closing of the intake valve and
the opening of the exhaust valve.
C. during which both valves are on their seats.
A.8.0.3.3.B.1 A02
The
valve clearance of an engine using hydraulic lifters, when the lifters are
completely flat, or empty, should not exceed
A. 0.00 inch.
B. a specified amount below zero.
C. a specified amount above zero.
A.8.0.3.4.A.1 A02
If the
exhaust valve of a four stroke cycle engine is closed and the intake valve
is just closed, the piston is on the
A. power stroke.
B. intake stroke.
C. compression stroke.
A.8.0.3.5.A.1 A02
How
many of the following are factors in establishing the maximum compression
ratio limitations of an aircraft engine?
1. Detonation characteristics of the fuel used.
2. Design limitations of the engine.
3. Degree of supercharging.
4. Spark plug reach.
A. Two.
B. Three.
C. Four.
A.8.0.3.6.A.1 A02
Full
floating piston pins are those which allow motion between the pin and
A. the piston.
B. both the piston and the large end of the connecting
rod.
C. both the piston and the small end of the connecting
rod.
A.8.0.3.7.A.1 A02
The
primary purpose in setting proper valve timing and overlap is to
A. permit the best possible charge of fuel/air
mixture into the cylinders.
B. gain more thorough exhaust gas scavenging.
C. obtain the best volumetric efficiency and
lower cylinder operating temperatures.
A.8.0.3.8.A.1 A02
If the
hot clearance is used to set the valves when the engine is cold, what will
occur during operation of the engine?
A. The valves will open late and close early.
B. The valves will open early and close early.
C. The valves will open early and close late.
A.8.0.3.9.A.1 A02
The
purpose of two or more valve springs in aircraft engines is to
A. eliminate valve spring surge.
B. equalize side pressure on the valve stems.
C. equalize valve face loading.
A.8.0.4.0.A.1 A02
During
overhaul, the disassembled parts of an engine are usually degreased with some
form of mineral spirits solvent rather than water mixed degreasers primarily
because
A. solvent degreasers are much more effective.
B. water mixed degreaser residues may cause engine
oil contamination in the overhauled engine.
C. water-mixed degreasers cause corrosion.
A.8.0.4.1.A.1 A02
Why
does the smoothness of operation of an engine increase with a greater number
of cylinders?
A. The engine has larger counterbalance weights.
B. The power impulses are spaced closer together.
C. The power impulses are spaced farther apart.
A.8.0.4.2.A.1 A02
Compression
ratio is the ratio between the
A. piston travel on the compression stroke and
on the intake stroke.
B. combustion chamber pressure on the combustion
stroke and on the exhaust stroke.
C. cylinder volume with piston at bottom dead
center and at top dead center.
A.8.0.4.3.A.1 A02
If the
crankshaft runout readings on the dial indicator are plus .002 inch and minus
.003 inch, the runout is
A. plus .001 inch.
B. .005 inch.
C. minus .001 inch.
A.8.0.4.4.A.1 A02
(1)
Cast iron piston rings may be used in chrome plated cylinders.
(2)
Chrome plated rings may be used in plain steel cylinders.
Regarding
the above statements,
A. both No. 1 and No. 2 are true.
B. neither No. 1 nor No. 2 is true.
C. only No. 1 is true.
A.8.0.4.5.A.1 A02
How
is proper end-gap clearance on new piston rings assured during the overhaul
of an engine?
A. By using rings specified by the engine manufacturer.
B. By accurately measuring and matching the outside
diameter of the rings with the inside diameter of the cylinders.
C. By placing the rings in the cylinder and measuring
the end-gap with a feeler gauge.
A.8.0.4.6.A.1 A02
The
volume of a cylinder equals 70 cubic inches when the piston is at bottom center.
When the piston is at the top of the cylinder, the volume equals 10 cubic
inches. What is the compression ratio?
A. 7:10.
B. 7:1.
C. 1:7.
A.8.0.4.7.A.1 A02
When
cleaning aluminum and magnesium engine parts, it is inadvisable to soak them
in solutions containing soap because
A. some of the soap will become impregnated in
the surface of the material and subsequently cause engine oil contamination
and foaming.
B. the soap can chemically alter the metals causing
them to become more susceptible to corrosion.
C. the parts can be destroyed by dissimilar metal
electrolytic action if they are placed together in the solution for more than
a few minutes.
A.8.0.4.8.A.1 A03
What
is the purpose of a power check on a reciprocating engine?
A. To determine if the fuel/air mixture is adequate.
B. To check magneto drop.
C. To determine satisfactory performance.
A.8.0.4.9.A.1 A03
What
will be the likely result if the piston ring gaps happen to be aligned when
performing a differential pressure compression check on a cylinder?
A. A worn or defective ring(s) indication.
B. The rings will not be seated.
C. Little or no effect.
A.8.0.5.0.A.1 A03
Which
of the following will be caused by excessive valve clearance of a cylinder
on a reciprocating aircraft engine?
A. A power increase by shortening the exhaust
event.
B. Intake and exhaust valves will open early
and close late.
C. Reduced valve overlap period.
A.8.0.5.1.A.1 A03
The
floating control thermostat, used on some reciprocating engine installations,
helps regulate oil temperature by
A. controlling oil flow through the oil cooler.
B. controlling air flow through the oil cooler.
C. recirculating hot oil back through the sump.
A.8.0.5.2.A.1 A03
Which
of the following would indicate a general weak engine condition when operated
with a fixed pitch propeller or test club?
A. Manifold pressure lower at idle RPM than at
static RPM.
B. Lower than normal static RPM, full throttle
operation.
C. Lower than normal manifold pressure for any
given RPM.
A.8.0.5.3.A.1 A03
What
is required by 14 CFR Part 43 Appendix D when performing an annual/ 100-hour
inspection on a reciprocating engine aircraft?
A. Magneto timing check.
B. Valve clearance check.
C. Cylinder compression check.
A.8.0.5.4.A.1 A03
After
spark plugs from an opposed engine have been serviced, in what position should
they be reinstalled?
A. Swapped bottom to top.
B. Next in firing order to the one from which
they were removed.
C. Next in firing order to the one from which
they were removed and swapped bottom to top.
A.8.0.5.5.A.1 A03
As the
pressure is applied during a reciprocating engine compression check using
a differential pressure tester, what would a movement of the propeller in
the direction of engine rotation indicate?
A. The piston was on exhaust stroke.
B. The piston was positioned past top dead center.
C. The piston was on compression stroke.
A.8.0.5.6.A.1 A03
Excessive
valve clearance results in the valves opening
A. late and closing late.
B. early and closing late.
C. late and closing early.
A.8.0.5.7.A.1 A03
During
routine inspection of a reciprocating engine, a deposit of small, bright,
metallic particles which do not cling to the magnetic drain plug is discovered
in the oil sump and on the surface of the oil filter. This condition
A. is probably a result of ring and cylinder
wall wear and is cause for engine removal and/or overhaul.
B. may be a result of abnormal plain type bearing
wear and is cause for further investigation.
C. is normal in engines utilizing plain type
bearings and aluminum pistons and is not cause for alarm.
A.8.0.5.8.A.1 A03
A characteristic
of dyna focal engine mounts as applied to aircraft reciprocating engines is
that the
A. engine attaches to the shock mounts at the
engine's center of gravity.
B. shock mounts eliminate the torsional flexing
of the powerplant.
C. shock mounts point toward the engine's center
of gravity.
A.8.0.5.9.A.1 A03
If metallic
particles are found in the oil filter during an inspection,
A. the cause should be identified and corrected
before the aircraft is released for flight.
B. it is an indication of normal engine wear
unless the particles are nonferrous.
C. it is an indication of normal engine wear
unless the deposit exceeds a specified amount.
A.8.0.6.0.A.1 A03
If the
oil pressure gauge fluctuates over a wide range from zero to normal operating
pressure, the most likely cause is
A. low oil supply.
B. air lock in the scavenge pump intake.
C. broken or weak pressure relief valve spring.
A.8.0.6.1.A.1 A03
What
special procedure must be followed when adjusting the valves of an engine
equipped with a floating cam ring?
A. Eliminate cam bearing clearance when making
valve adjustment.
B. Adjust valves when the engine is hot.
C. Adjust all exhaust valves before intake valves.
A.8.0.6.2.B.1 A03
Which
of the following is most likely to occur if an overhead valve engine is operated
with inadequate valve clearances?
A. The valves will remain closed for longer periods
than specified by the engine manufacturer.
B. The further decrease in valve clearance that
occurs as engine temperatures increase will cause damage to the valve-operating
mechanism.
C. The valves will not seat positively during
start and engine warmup.
A.8.0.6.3.A.1 A03
Excessive
valve clearances will cause the duration of valve opening to
A. decrease for intake valves and increase for
exhaust valves.
B. increase for both intake and exhaust valves.
C. decrease for both intake and exhaust valves.
A.8.0.6.4.A.1 A03
What
does valve overlap promote?
A. Better scavenging and cooling characteristics.
B. A backflow of gases across the cylinder.
C. Lower intake manifold pressure and temperatures.
A.8.0.6.5.A.1 A03
At what
speed must a crankshaft turn if each cylinder of a four stroke cycle engine
is to be fired 200 times a minute?
A. 1,600 RPM.
B. 400 RPM.
C. 800 RPM.
A.8.0.6.6.A.1 A03
Engine
crankshaft runout is usually checked
1. during engine overhaul.
2. during annual inspection.
3. after a "prop strike" or sudden
engine stoppage.
4. during 100-hour inspection.
A. 1 and 3.
B. 1, 3, and 4.
C. 1, 2 and 3.
A.8.0.6.7.B.1 A03
Before
attempting to start a radial engine that has been shut down for more than
30 minutes,
A. turn the ignition switch on before energizing
the starter.
B. turn the propeller by hand three or four revolutions
in the opposite direction of normal rotation to check for liquid lock.
C. turn the propeller by hand three to four revolutions
in the normal direction of rotation to check for liquid lock.
A.8.0.6.8.A.1 A03
An engine
misses in both the right and left positions of the magneto switch. The quickest
method for locating the trouble is to
A. check for one or more cold cylinders.
B. perform a compression check.
C. check each spark plug.
A.8.0.6.9.A.1 A03
A hissing
sound from the exhaust stacks when the propeller is being pulled through manually
indicates
A. exhaust valve blow by.
B. a cracked exhaust stack.
C. worn piston rings.
A.8.0.7.0.A.1 A03
If the
oil pressure of a cold engine is higher than at normal operating temperatures,
the
A. oil system relief valve should be readjusted.
B. oil dilution system should be turned on immediately.
C. engine's lubrication system is probably operating
normally.
A.8.0.7.1.A.1 A03
If an
engine operates with a low oil pressure and a high oil temperature, the problem
may be caused by a
A. clogged oil cooler annular jacket.
B. sheared oil pump shaft.
C. leaking oil dilution valve.
A.8.0.7.2.A.1 A03
Which
fuel/air mixture will result in the highest engine temperature (all other
factors remaining constant)?
A. A mixture richer than a full rich mixture
of .087.
B. A mixture leaner than a manual lean mixture
of .060.
C. A mixture leaner than a rich best power mixture
of .085.
A.8.0.7.3.A.1 A03
If an
engine cylinder is to be removed, at what position in the cylinder should
the piston be?
A. Bottom dead center.
B. Top dead center.
C. Halfway between top and bottom dead center.
A.8.0.7.4.A.1 A03
The
horsepower developed in the cylinders of a reciprocating engine is known as
the
A. shaft horsepower.
B. brake horsepower.
C. indicated horsepower.
A.8.0.7.5.A.1 A03
Engine
operating flexibility is the ability of the engine to
A. deliver maximum horsepower at a specific altitude.
B. run smoothly and give the desired performance
at all speeds.
C. meet exacting requirements of efficiency and
low weight per horsepower ratio.
A.8.0.7.6.A.1 A03
Standard
aircraft cylinder oversizes usually range from 0.010 inch to 0.030 inch. Oversize
on automobile engine cylinders may range up to 0.100 inch. This is because
aircraft engine cylinders
A. have more limited cooling capacity.
B. operate at high temperatures.
C. have relatively thin walls and may be nitrided.
A.8.0.7.7.A.1 A03
If the
ignition switch is moved from BOTH to either LEFT or RIGHT during an engine
ground check, normal operation is usually indicated by a
A. slight drop in RPM.
B. momentary interruption of both ignition systems.
C. large drop in RPM.
A.8.0.7.8.A.1 A03
During
ground check an engine is found to be rough running, the magneto drop is normal,
and the manifold pressure is higher than normal for any given RPM. The trouble
may be caused by
A. several spark plugs fouled on different cylinders.
B. a dead cylinder.
C. a leak in the intake manifold.
A.8.0.7.9.A.1 A03
What
is the best indication of worn valve guides?
A. Low oil pressure.
B. Low compression.
C. High oil consumption.
A.8.0.8.0.A.1 A03