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![]() Builders guide to safe aircraft materials |
Fastener safetyingRev. 1 — published January 15, 2006 |
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Content |
All of the following material is extracted from the FAA advisory circular AC 43.13-1B Chapter 7. The complete hard-copy volume 'Acceptable methods, techniques, and practices — aircraft inspection and repair' (~ 650 pages and incorporating the 2001 changes) is available from the RA-Aus online shop for a reasonable price. It is bound together with the FAA advisory circular AC 43.13-2A 'Acceptable methods, techniques, and practices — aircraft alterations' (~ 100 pages). A PDF version of the book is included in the RA-Aus members' CD.
13.1 [7-122 in advisory circular AC 43.13-1B] GeneralThe word safetying is a term universally used in the aircraft industry. Briefly, safetying is defined as: "Securing by various means any nut, bolt, turnbuckle etc., on the aircraft so that vibration will not cause it to loosen during operation." These practices are not a means of obtaining or maintaining torque, rather a safety device to prevent the disengagement of screws, nuts, bolts, snap rings, oil caps, drain cocks, valves, and parts.Three basic methods are used in safetying; safety-wire, cotter pins, and self-locking nuts. Retainer washers and pal nuts are also sometimes used.
13.2 [7-123] Safety wireDo not use stainless steel, monel, carbon steel, or aluminum alloy safety wire to secure emergency mechanisms such as switch handles, guards covering handles used on exits, fire extinguishers, emergency gear releases, or other emergency equipment. Some existing structural equipment or safety-of-flight emergency devices require copper or brass safety wire (.020 inch diameter only). Where successful emergency operation of this equipment is dependent on shearing or breaking of the safety wire, particular care should be used to ensure that safetying does not prevent emergency operation.
13.3 [7-124] Safety-wiring proceduresThere are many combinations of safety wiring with certain basic rules common to all applications. These rules are as follows.
13.4 [7-125] Twisting with special toolsTwist the wire with a wire twister as follows. (See figure 7-4 above.)CAUTION: When using wire twisters, and the wire extends 3 inches beyond the jaws of the twisters, loosely wrap the wire around the pliers to prevent whipping and possible personal injury. Excessive twisting of the wire will weaken the wire. a. Grip the wire in the jaws of the wire twister and slide the outer sleeve down with your thumb to lock the handles or lock the spring-loaded pin. b. Pull the knob, and the spiral rod spins and twists the wire. c. Squeeze handles together to release wire. 13.5 [7-126] Securing oil caps, drain cocks and valvesWhen securing oil caps and drain cocks, the safety wire should be anchored to an adjacent fillister-head screw (see figure 7-4a below). This method of safety wiring is applied to wingnuts, filler plugs, single-drilled head bolts, fillister-head screws, etc.; which are safety wired individually. When securing valve handles in the vertical position, the wire is looped around the threads of the pipe leading into one side of the valve, double-twisted around the valve handle, and anchored around the threads of the pipe leading into the opposite side of the valve. When castellated nuts are to be secured with safety wire, tighten the nut to the low side of the selected torque range, unless otherwise specified; and, if necessary, continue tightening until a slot lines with the hole. In blind tapped hole applications of bolts or castellated nuts on studs, the safety wiring should be in accordance with the general instructions of this chapter. Hollow-head bolts are safetied in the manner prescribed for regular bolts.
NOTE: Do not loosen or tighten properly tightened nuts to align safety-wire holes. 13.6 Examples of hardware wiringAlthough there are numerous safety wiring techniques used to secure aircraft hardware, practically all are derived from the basic examples shown in the following figures.
Examples 1, 2, 3, and 4 apply to all types of bolts, fillister-head screws, square-head plugs, and other similar parts which are wired so that the loosening tendency of either part is counteracted by tightening of the other part. The direction of twist from the second to the third unit is counterclockwise in examples 1, 3, and 4 to keep the loop in position against the head of the bolt. The direction of twist from the second to the third unit in example 2 is clockwise to keep the wire in position around the second unit. The wire entering the hole in the third unit will be the lower wire, except example 2, and by making a counterclockwise twist after it leaves the hole, the loop will be secured in place around the head of that bolt.
Examples 5, 6, 7, and 8 show methods for wiring various standard items. NOTE: Wire may be wrapped over the unit rather than around it when wiring castellated nuts or on other items when there is a clearance problem.
Example 9 shows the method for wiring bolts in different planes. Note that wire should always be applied so that tension is in the tightening direction. Example 10. Hollow-head plugs shall be wired as shown with the tab bent inside the hole to avoid snags and possible injury to personnel working on the engine. Example 11. Correct application of single wire to closely spaced multiple group.
Examples 12 and 13 show methods for attaching lead seal to protect critical adjustments.
Example 14 shows bolt wired to a right-angle bracket with the wire wrapped around the bracket. Example 15 shows correct method for wiring adjustable connecting rod. Example 16 shows correct method for wiring the coupling nut on flexible line to the straight connector brazed on rigid tube.
Fittings incorporating wire lugs shall be wired as shown in examples 17 and 18. Where no lock-wire lug is provided, wire should be applied as shown in examples 19 and 20 with caution being exerted to ensure that wire is wrapped tightly around the fitting. Small size coupling nuts shall be wired by wrapping the wire around the nut and inserting it through the holes as shown in example 21.
13.7 [7-127] Securing with cotter pins
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The next module is 'Aircraft fabric covering systems' in the
'Airframe materials — fabrics, composites and coatings' group.
Builders guide to aircraft materials — metals and hardware modules
| Guide contents | Properties of metals | Metal corrosion | Hardware fittings in aircraft structures |
| AN, MS hardware — rivets, bolts and locking devices | [Safetying] |