Please follow in manual AC CHAPTER 7

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Presentation transcript:

Please follow in manual ---------- AC 43.13 CHAPTER 7

HARDWARE

NAME THE HARDWARE

SCREWS are not as strong as a bolt and have a looser thread fit and are divided into 3 main groups 1-structural for structural applications (obviously) , 2 -machine screws used for general use eg screwing inside panels of a/c together , 3 - self tapping will tap their own hole are used in minor non-structural areas and blind applications

additional types of screws could be set screw usually have a allen screw head and can be used to lock something in place different head types include torque, Philips , flat head and many others

DO NOT USE CORDLESS DRILLS ON SCREWS ON FUEL PANELS (748 WING) AS STATIC ELECTRICITY CAN CAUSE A SPARK. All other panels on an a/c are ok but set the clutch on low as to not strip heads on installation. most heads have drilled heads to allow for lockwiring or saftying of the bolts . This is essential in aviation for safety reasons CLICK

All hardware must be traceable back to an approved source (vender) All hardware must be traceable back to an approved source (vender) . Bolts are widely used through out aerospace because of their wide applications and their shear or tensile(pulling apart) strength.

Why take the time to build a perfect wing only to attach it to the fuselage with used hardware. The strength of any chain is it’s weakest link

use nothing but aircraft grade hardware use nothing but aircraft grade hardware. Commercial grade hardware found in hardware or automotive stores is legal to use on an experimental airplane but should not be considered for even a moment. Common steel bolts purchased from a hardware store are made of low carbon steel that has a low tensile strength of 50,000 to 60,000 psi. They also bend easily and have little corrosion protection. In contrast, aircraft bolts are made from corrosion resistant steel and are heat treated to a strength in excess of 125,000 psi.

All fasteners are identified with a specification number and a series of letters and dashes identifying their size, type of material, If you see no markings at all on the head of a bolt, do not use it. It is probably a commercial grade bolt

parts of a bolt are as follows . *The shank is threaded on the end and the unthreaded portion of the bolt is termed the grip. The diameter of a bolt is the width of the grip. *The shank of a bolt will be either drilled to accept a cotter pin or undrilled. Another option is to purchase a bolt that has the head drilled for the purpose of accepting safety wire. Clevis bolts are manufactured with a slotted head and are used for control cable applications.

close tolerance bolts are used on some flight control installations and use heating and cooling for installation. They have high very strength

typical measurement of a bolt ------------ AN4H-8A AN means the bolt is manufactured according to Air Force- Navy specs. * The 4 is the width of the shank in 16ths *8 identifies the length of the shank in 1/8" increments *“A” means the shank of the bolt is undrilled (no letter here means a drilled shank) *“H” means drlled head

NUTS Aircraft nuts usually have no identification on them but they are made from the same material as bolts. Due to the vibration of aircraft, nuts must have some form of a locking device to keep them in place. The most common ways of locking are cotter pins used in castle nuts, fiber inserts, lockwashers, and safety wire.

The aircraft nuts you will most likely encounter are castle nuts, self-locking nuts, and plain nuts. Wing nuts and anchor nuts are also used. Never re-use lockwire or tab washers, except in the case of a 4 tab washer and only 2 tabs were used

Castle nuts are used with drilled shank bolts, clevis bolts and eye bolts. The slots in the nut accommodate a cotter pin for safetying purposes

Self-locking nuts, as the name implies, do not need a locking device Self-locking nuts, as the name implies, do not need a locking device. The most common method of locking is derived from a fiber insert. This fiber insert is temperature limited to 250-deg. F

An all metal locking nut is used forward of the firewall and in other high temperature areas. In place of a fiber insert, the threads of a metal locking nut narrow slightly at one end to provide more friction. An AN363 is an example of this type of nut. It is capable of withstanding temperatures to 550-deg.f

Plain nuts require a locking device such as a check nut or lockwasher Plain nuts require a locking device such as a check nut or lockwasher. These are sometimes used on turnbarrels for flight control cable runs

Wing nuts (AN350) are commonly used on battery connections or hose clamps where proper tightness can be obtained by hand. Anchor nuts are widely used in areas where it is difficult to access a nut. Tinnerman nuts, instrument mounting nuts, pal nuts, cap nuts, etc. are all examples of other types that are used.

Basics of Aircraft Nut Installation 1. When using a castle nut, the cotter pin hole may not line up with the slots on the nut. The Mechanics General Handbook states "except in cases of highly stressed engine parts, the nut may be over tightened to permit lining up the next slot with the cotter pin hole." Common sense should prevail. Do not over tighten to an extreme, instead, remove the nut and use a different washer and then try to line the holes again. 2. A fiber nut may be reused if you are unable to tighten by hand. 3. At least one thread should be projecting past the fiber on a fiber nut installation. 4. No self-locking nuts on moving part installations. 5. Do not use AN364 or AN365 fiber nuts in areas of high temperature - above 250' F. 6. Shear nuts are to be used only in shear loads (not tension). 7. Plain nuts require a locking device such as a lockwasher or a check nut. 8. When using a lockwasher, place a plain washer between the surface of the airplane part and the lockwasher. 9. Shear nuts and standard nuts have different torque values. 10. Use wing nuts only where hand tightness is adequate. 11. Always turn the nut not the bolt

Washers: The main purposes of a washer in aircraft installation are to : 1)provide a shim when needed, 2)act as a smooth load bearing surface, 3)and to adjust the position of castle nuts in relation to the drilled hole in a bolt. 4) Also, remember that plain washers are used under a lockwasher to prevent damage to a surface.

There are other types of washers There are other types of washers. I mentioned lockwashers that are made several different ways. They are often split ring, they are sometimes internal tooth and even external tooth (see Figure 5)

COTTER PINS AND SAFETY WIRE The cotter pins mostly used on custom aircraft are AN380 and AN381. -You will normally use them with castle nuts. The dash numbers indicate diameter (in 32nds) and length (in quarters) of the pin. As an example, AN380-2-2 would be a cadmium plated pin 1/16" in diameter and 1/2" long.

-Safety wire is also widely used. -The most used sizes in diameter are .020, .032 and .041 or small variations thereof. -The material is usually stainless steel or brass. The easiest method of installation is acquired by using safety wire pliers. -The wire is installed so that if the nut or bolt begins to loosen it will increase the tension on the wire. -Be sure you do not overtwist the wire -doing so will weaken the safety wire. Leave about 3 to 6 twists and then cut off the excess wire and bend its end so you do not snag it with your hand at a later time

The End