Fluid Lines and Fittings Flashcards
- Which coupling nut should be selected for use with 1/2-inch aluminum oil lines which are to be assembled using flared tube ends and standard AN nuts, sleeves, and fittings?
A— AN-818-5.
B— AN-818-16.
C— AN-818-8.
C— AN-818-8.
An AN-818-5 nut will fit a 5/16-inch tube. (The last dash number is the tube diameter in 1/16-inch increments.) An AN-818-16 nut will fit a 1-inch tube. An AN-818-8 nut will fit a 1/2-inch tube.
- Metal tubing fluid lines are sized by wall thickness and
A— outside diameter in 1/16 inch increments.
B— inside diameter in 1/16 inch increments.
C— outside diameter in 1/32 inch increments.
A— outside diameter in 1/16 inch increments.
Metal tubing used in aircraft fluid power installations is sized by its outside diameter, which is measured fractionally in sixteenths of an inch.
8193-1.
Rolling-type flaring tools are used to flare __________, __________, and ___________ tubing.
A— Stainless steel, hard copper, mild steel.
B— Titanium, soft copper, corrosion resistant steel.
C—Soft copper, aluminum, brass.
C—Soft copper, aluminum, brass.
Use rolling-type flaring tools only to flare soft copper, aluminum, and brass tubing. Do not use with corrosion resistant steel or titanium.
- From the following sequences of steps, indicate the proper order you would use to make a single flare on a piece of tubing:
1) Place the tube in the proper size hole in the flaring block.
2) Project the end of the tube slightly from the top of the flaring tool, about the thickness of a dime.
3) Slip the fitting nut and sleeve on the tube.
4) Strike the plunger several light blows with a lightweight hammer or mallet and turn the plunger one-half turn after each blow.
5) Tighten the clamp bar securely to prevent slippage.
6) Center the plunger or flaring pin over the tube.
A— 1, 3, 5, 2, 4, and 6.
B— 3, 1, 6, 2, 5, and 4.
C— 3, 1, 2, 6, 5, and 4.
B— 3, 1, 6, 2, 5, and 4.
The correct sequence for making a single flare on a piece of tubing is:
(3) Slip the fitting nut and sleeve on the tube.
(1) Place the tube in the proper size hole in the flaring block.
(6) Center the plunger or flaring pin over the tube.
(2) Project the end of the tube slightly from the tip of the f laring tool, about the thickness of a dime.
(5) Tighten the clamp bar securely to prevent slippage. (4) Strike the plunger several light blows with a lightweight hammer or mallet. Turn the plunger one-half turn after each blow.
- Hydraulic tubing, which is damaged in a localized area to such an extent that repair is necessary, may be repaired
A— by cutting out the damaged area and utilizing a swaged tube fitting to join the tube ends.
B— only by replacing the tubing section run (connection to connection) using the same size and material as the original.
C— by cutting out the damaged section and soldering in a replacement section of tubing.
A— by cutting out the damaged area and utilizing a swaged tube fitting to join the tube ends.
If a piece of high-pressure hydraulic tubing is damaged in a localized area, the damage can be cut out and a new piece of tubing cut to replace the damaged section. Swage-type splice fittings are slipped over each end of the tubing, and the fittings are swaged to the tube ends.
- What is an advantage of a double flare on aluminum tubing?
A— Ease of construction.
B— More resistant to damage when the joint is tightened.
C— Can be applied to any size and wall-thickness of tubing.
B— More resistant to damage when the joint is tightened.
Tubing made of 5052-O and 6061-T aluminum alloy in sizes from 1/8- to 3/8-inch OD should be flared with a double flare. Double flares are smoother than single flares and are more concentric. Also, the extra metal makes the flare more resistant to the shearing effect when the f ittings are torqued.
- A certain amount of slack must be left in a flexible hose during installation because, when under pressure, it
A— expands in length and diameter.
B— expands in length and contracts in diameter.
C— contracts in length and expands in diameter.
C— contracts in length and expands in diameter.
When flexible hose is installed in an aircraft, it must be given a certain amount of slack because when pressure is applied to the hose, it contracts in length and expands in diameter.
- The term “cold flow” is generally associated with
A— the effects of low temperature gasses or liquids f lowing in hose or tubing.
B— impressions left in natural or synthetic rubber hose material.
C— flexibility characteristics of various hose materials at low ambient temperatures.
B— impressions left in natural or synthetic rubber hose material.
Cold flow describes the deep, permanent impression left in a natural or synthetic rubber hose by the pressure of hose clamps or supports.
- What is the color of an AN steel flared-tube fitting?
A— Black.
B— Blue.
C— Red.
A— Black.
Steel AN flared tube fittings are colored black. Aluminum alloy AN fittings are colored blue.
- Which of the following statements is/are correct in reference to flare fittings?
1) AN fittings have an identifying shoulder between the end of the threads and the flare cone.
2) AC and AN fittings are considered identical except for material composition and identifying colors.
3) AN fittings are generally interchangeable with AC fittings of compatible material composition
A— 1.
B— 1 and 3.
C— 1, 2, and 3.
A— 1.
AN flare fittings have a shoulder between the end of the threads and the flare cone. In AC fittings the threads go all the way to the cone. AN fittings are dyed blue or black and AC fittings are gray or yellow. The threads on an AN fitting are coarser than those on an AC fitting. AN and AC fittings are not interchangeable.
- Flexible lines must be installed with
A— a slack of 5 to 8 percent of the length.
B— a slack of at least 10 to 12 percent of the length.
C— enough slack to allow maximum flexing during operation.
A— a slack of 5 to 8 percent of the length.
When flexible lines are installed in a fluid power system, they should be between 5 percent and 8 percent longer than the space between the fittings.
This extra length (this slack) makes allowance for expansion in the system due to heat and for the fact that a hose contracts in its length when it is pressurized.
- The maximum distance between end fittings to which a straight hose assembly is to be connected is 50 inches. The minimum hose length to make such a connection should be
A— 54-1/2 inches.
B— 51-1/2 inches.
C— 52-1/2 inches.
C— 52-1/2 inches.
When a flexible line is installed in a fluid power system, it should be between 5 percent and 8 percent longer than the space between the fittings.
If the distance between the fittings is 50 inches, the hose should be at least 5 percent longer than this, or 52- 1/2 inches long.
- Excessive stress on fluid or pneumatic metal tubing caused by expansion and contraction due to temperature changes can best be avoided by
A— using short, straight sections of tubing between fixed parts of the aircraft.
B— using tubing of the same material as the majority of the adjoining structure.
C— providing bends in the tubing.
C— providing bends in the tubing.
Never select a path for a rigid fluid line that does not require bends in the tubing. Bends are necessary to permit the tubing to expand and contract under temperature changes and to absorb vibration.
- The material specifications for a certain aircraft require that a replacement oil line be fabricated from 3/4- inch 0.072 5052-0 aluminum alloy tubing. What is the inside dimension of this tubing?
A— 0.606 inch.
B— 0.688 inch.
C— 0.750 inch.
A— 0.606 inch.
Find the inside diameter of a tube by subtracting two times the wall thickness from its outside diameter.
0.750 – 2(0.072) = 0.606 inch
The inside diameter is 0.606 inch.
- In most aircraft hydraulic systems, two-piece tube connectors consisting of a sleeve and a nut are used when a tubing flare is required. The use of this type connector eliminates
A— the flaring operation prior to assembly.
B— the possibility of reducing the flare thickness by wiping or ironing during the tightening process.
C— wrench damage to the tubing during the tightening process.
B— the possibility of reducing the flare thickness by wiping or ironing during the tightening process.
There are two types of flare fittings that can be used in aircraft hydraulic systems. One type is the single-piece AN817 nut, and the other is the two-piece MS20819 sleeve and an AN818 nut.
The AN818 nut and sleeve are preferred over the single-piece fitting because it eliminates the possibility of reducing the thickness of the flare by the wiping or ironing action when the nut is tightened.
With the two-piece fitting, there is no relative motion between the fitting and the flare when the nut is being tightened.