1Which statement is true regarding bearings used in high-powered reciprocating aircraft engines?
There is less rolling friction when ball bearings are used than when roller bearings are employed
2A condition that can occur in radial engines but is unlikely to occur in horizontally opposed engines is
hydraulic lock
3Which condition would be the least likely to be caused by failed or failing engine bearings?
low oil temperatures
4What is the principal advantage of using propeller reduction gears?
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
5Which of the following will decrease volumetric efficiency in a reciprocating engine?
Improper valve timing, sharp bends in the induction system, and high carburetor air temperatures
6Which of the following is a characteristic of a thrust bearing used in most radial engines?
Deep-groove ball
7Which bearing is least likely to be a roller or ball bearing?
Master rod bearing (radial engine)
8The operating temperature valve clearance of a radial engine as compared to cold valve clearance is
Greater
9A nine-cylinder engine with a bore of 5.5 inches and a stroke of 6 inches will have a total piston displacement of
1,283 cubic inches
10The five events of a four-stroke cycle engine in the order of their occurrence are
intake, compression, ignition, power, and exhaust
11The primary concern in establishing the firing order for an opposed engine is to
Provide for balance and eliminate vibration to the greatest extent possible
12If fuel/air ratio is proper and ignition timing is correct, the combustion process should be completed
Just after top center at the beginning of the power stroke
13Grinding the valves of a reciprocating engine to a feather edge is likely to result in
preignition and burned valves
14Which statement is correct regarding engine crankshafts?
Moveable counterweights serve to reduce the torsional vibrations in an aircraft reciprocating engine
15On which strokes are both valves on a four-stroke cycle reciprocating aircraft engine open?
Exhaust and intake
16Which type of bearings are generally used for connecting rods and cam shafts?
Plain
17The actual power delivered to the propeller of an aircraft engine is called
Brake horsepower
18Cam-ground pistons are installed in some aircraft engines to
provide a better fit at operating temperatures
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.
19Exhaust closes 10°: ATDC.
245 degrees
20Some aircraft engine manufacturers equip their product with choked or taper-ground cylinders in order to
provide a straight cylinder bore at operating temperatures
21An 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?
During normal operation
22What tool is generally used to measure the crankshaft rotation in degrees?
timing disk
23If an engine with a stroke of 6 inches is operated at 2,000 RPM, the piston movement within the cylinder will be
at maximum velocity 90 degrees after TDC
24If the intake valve is opened too early in the cycle of operation of a four-stroke cycle engine, it may result in
backfiring into the induction system
25Some cylinder barrels are hardened by
nitriding
26Which statement is correct regarding a four-stroke cycle aircraft engine?
The intake valve closes on the compression stroke
27On which part of the cylinder walls of a normally operating engine will the greatest amount of wear occur?
Near the top of the cylinder
28During overhaul, reciprocating engine exhaust valves are checked for stretch
With a contour or radius gauge
29When is the fuel/air mixture ignited in a conventional reciprocating engine?
shortly before the piston reaches the top of the compression stroke
30Ignition 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.)
373 degrees
31What is the purpose of the safety circlet installed on some valve stems?
To prevent valves from falling into the combustion chamber
32Valve overlap is defined as the number of degrees of crankshaft travel
During which both valves are off their seats
33The valve clearance of an engine using hydraulic lifters, when the lifters are completely flat, or empty, should not exceed
a specified amount above zero
34If the exhaust valve of a four-stroke cycle engine is closed and the intake valve is just closed, the piston is on the
compression stroke
35How many of the following are factors in establishing the maximum compression ratio limitations of an aircraft engine?
detonation characteristics of the fuel, design limitations of the engine, and the degree of supercharging
36Full-floating piston pins are those which allow motion between the pin and
both the piston and the small end of the connecting rod
37The primary purpose in setting proper valve timing and overlap is to
obtain the best volumetric efficiency and lower cylinder operating temperatures
38If the hot clearance is used to set the valves when the engine is cold, what will occur during operation of the engine?
The valve will open late and close early
39What is the purpose of installing two or more springs on each valve in an aircraft engine?
To eliminate valve spring vibration or surging
40During overhaul, the disassembled parts of an engine are usually degreased with some form of mineral spirits solvent rather than water-mixed degreasers primarily because
water-mixed degreaser residues may cause engine oil contamination in the overhauled engine
41Why does the smoothness of operation of an engine increase with a greater number of cylinders?
The power impulses are spaced closer together
42Compression ratio is the ratio between the
cylinder volume with piston at bottom dead center and at top dead center.
43If the crankshaft runout readings on the dial indicator are plus .002 inch and minus .003 inch, the runout is
.005 inch
(1) Cast iron piston rings may be used in chrome-plated cylinders.
(2) Chrome-plated rings may be used in plain steel cylinders.
44Regarding the above statements,
Both 1 and 2 are true
45How is proper end-gap clearance on new piston rings assured during the overhaul of an engine?
By placing the rings in the cylinder and measuring the end gap with a feeler gauge
46The 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?
7:1
47When cleaning aluminum and magnesium engine parts, it is inadvisable to soak them in solutions containing soap because
Some of the soap will become impregnated in the surface of the material and subsequently cause engine oil contamination and foaming
48What is the purpose of a power check on a reciprocating engine?
To determine satisfactory performance
49What 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 worn or defective ring(s) indication
50Which of the following will be caused by excessive valve clearance of a cylinder on a reciprocating aircraft engine?
Reduced valve overlap period
51The floating control thermostat, used on some reciprocating engine installations, helps regulate oil temperature by
Controlling air flow through the oil cooler
52Which of the following would indicate a general weak-engine condition when operated with a fixed-pitch propeller or test club?
Lower then normal static RPM, full throttle operation
53What is required by 14 CFR Part 43 Appendix D when performing an annual/100-hour inspection on a reciprocating engine aircraft?
Cylinder compression check
54After spark plugs from an opposed engine have been serviced, in what position should they be reinstalled?
Next in firing order to the one from which they were removed and swapped bottom to top
55As 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?
The piston was positioned past top dead center
56Excessive valve clearance results in the valves opening
late and closing early
57During 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
may be a result of abnormal plain type bearing wear and is cause for further investigation
58A characteristic of dyna-focal engine mounts as applied to aircraft reciprocating engines is that the
Shock mounts point toward the engines center of gravity
59If metallic particles are found in the oil filter during an inspection,
The cause should be identified and corrected before the aircraft is released for flight
60If the oil pressure gauge fluctuates over a wide range from zero to normal operating pressure, the most likely cause is
Low oil supply
61What special procedure must be followed when adjusting the valves of an engine equipped with a floating cam ring?
Eliminate cam bearing clearance when making valve adjustments
62Which of the following is most likely to occur if an overhead valve engine is operated with inadequate valve clearances?
The valves will not seat positively during start and engine warm-up
63Excessive valve clearances will cause the duration of valve opening to
decrease for both intake and exhaust valves
64What does valve overlap promote?
Better scavenging and cooling characteristics.
65At what speed must a crankshaft turn if each cylinder of a four-stroke cycle engine is to be fired 200 times a minute?
400 RPM
66Engine crankshaft runout is usually checked
During engine overhaul, and after a "prop strike" or sudden engine stoppage.
67Before attempting to start a radial engine that has been shut down for more than 30 minutes,
Turn the propeller by hand three or four revolutions in the normal direction of rotation to check for liquid lock
68An engine misses in both the right and left positions of the magneto switch. The quickest method for locating the trouble is to
Check for one or more cold cylinders
69A hissing sound from the exhaust stacks when the propeller is being pulled through manually indicates
Exhaust valve blow-by
70If the oil pressure of a cold engine is higher than at normal operating temperatures, the
Engines lubrication system is probably operating normally
71If an engine operates with a low oil pressure and a high oil temperature, the problem may be caused by a
Leaking oil dilution valve
72Which fuel/air mixture will result in the highest engine temperature (all other factors remaining constant)?
A mixture leaner than a manual lean mixture of .060
73If an engine cylinder is to be removed, at what position in the cylinder should the piston be?
Top dead center
74The horsepower developed in the cylinders of a reciprocating engine is known as the
Indicated horsepower
75Engine operating flexibility is the ability of the engine to
run smoothly and give the desired performance at all speeds
76Standard 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
Have relatively thin walls and may be nitrided
77If the ignition switch is moved from BOTH to either LEFT or RIGHT during an engine ground check, normal operation is usually indicated by a slight
drop in torque meter pressure indication
78During 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 dead cylinder
79What is the best indication of worn valve guides?
High oil consumption.
80By use of a differential pressure compression tester, it is determined that cylinder 3 of a nine-cylinder radial engine will not hold pressure after the crankshaft has been rotated 260° from top dead center compression stroke cylinder 1. How can this indication usually be interpreted?
A normal indication
81hen does valve overlap occur in the operation of an aircraft reciprocating engine?
At the end of the exhaust stroke and the beginning of the intake stroke
82What is an advantage of using metallic-sodium filled exhaust valves in aircraft reciprocating engines?
Reduced valve operating temeratures
83Valve clearance changes on opposed-type engines using hydraulic lifters are accomplished by
push rod replacement
84What is likely to occur if a reciprocating engine is operated at high power settings before it is properly warmed up?
Oil starvation of bearings and other parts
85An increase in manifold pressure with a constant RPM will cause the bearing load in an engine to
Increase
86Direct mechanical push-pull carburetor heat control linkages should normally be adjusted so that the stop located on the diverter valve will be contacted
Before the stop at the control lever is reached in both HOT and COLD positions
87Reduced air density at high altitude has a decided effect on carburetion, resulting in a reduction of engine power by
Excessively enriching the fuel/air mixture
88Increased water vapor (higher relative humidity) in the incoming air to a reciprocating engine will normally result in which of the following?
Decreased engine power at a constant RPM and manifold pressure
(1) Preignition is caused by improper ignition timing.
(2) Detonation occurs when an area of the combustion chamber becomes incandescent and ignites the fuel/air mixture in advance of normal timed ignition.
89Regarding the above statements,
Neither 1 nor 2 is true
90Which of the following engine servicing operations generally requires engine pre-oiling prior to starting the engine?
Engine installation
91During the inspection of an engine control system in which push-pull control rods are used, the threaded rod ends should
be checked for the amount of thread engagement by means of the inspection holes
92Which of the following conditions would most likely lead to detonation?
Use of fuel with too low an octane rating
93An unsupercharged aircraft reciprocating engine, operated at full throttle from sea level, to 10,000 feet, provided the RPM is unchanged, will
lose power due to the reduced density of the air drawn into the cylinders
94Which of the following would most likely cause a reciprocating engine to backfire through the induction system at low RPM operation?
Lean mixture
95How may it be determined that a reciprocating engine with a dry sump is pre-oiled sufficiently?
Oil will flow from the engine return line or indicator port
96What is the basic operational sequence for reducing the power output of an engine equipped with a constant-speed propeller?
Reduced the manifold pressure, then the RPM
97Which statement pertaining to fuel/air ratios is true?
The mixture ratio which gives the best power is richer than the mixture ratio which gives maximum economy
98Backfiring through the carburetor generally results from the use of
an excessively lean mixture
99Which of these conditions will cause an engine to have an increased tendency to detonate?
High manifold pressure or high intake air temperature
100When will small induction system air leaks have the most noticeable effect on engine operation?
at low RPM
101To reduce the power output of an engine equipped with a constant-speed propeller and operating near maximum BMEP, the
manifold pressure is reduced with the throttle control before the RPM is reduced with the propeller control
102One of the best indicators of reciprocating engine combustion chamber problems is
spark plug condition
103What could cause excessive pressure buildup in the crankcase of a reciprocating engine?
Plugged crankcase breather
104Excessive valve clearance in a piston engine
decreases valve overlap.
105To what altitude will a turbo charged engine maintain sea level pressure?
Critical altitude
106If air is heard coming from the crankcase breather or oil filler during a differential compression check, what is this an indication of?
Piston ring leakage
107One cause of afterfiring in an aircraft engine is
an excessively rich mixture.