Par 11-146 Page 11-537 Service Loop Routing. The service loop harness should be routed directly from the breakout point to the component.
The harness should not contact moving mechanical components or linkage, and should not be wrapped or tangled with other service loop harnesses.
Service Loop Harness Termination. Strain relief should be provided at the se rvice loop harness termination, and is normally provided by the connector manufacturer’s backshell, heat-shrinkable boot, or tubing.
11-140.11-145. [RESERVED.]
Par 11-146 Page 11-538 SECTION 11. CLAMPING
GENERAL. Wires and wire bundles must be supported by using clamps meeting Specification MS-21919, or plastic cable straps in accessible areas if correctly applied within the restrictions of paragraph 11-158. Clamps and other primary support devices must be constructed of materials that are compatible with their installation and environment, in terms of temperature, fluid resistance, exposure to ultraviolet (UV) light, and wire bundle mechanical loads. They should be spaced at intervals not exceeding 24 inches.
Clamps on wire bundles should be selected so that they have a snug fit without pinching wires, as shown in figure 11-11 through figure 11-13.
CAUTION: The use of metal clamps on coaxial RF cables may cause problems if clamp fit is such that RF cable’s original cross-section is distorted.
Clamps on wire bundles should not allow the bundle to move through the clamp when a slight axial pull is applied. Clamps on RF cables must fit without crushing and must be snug enough to prevent the cable from moving freely through the clamp, but may allow the cable to slide through the clamp when a light axial pull is applied. The cable or wire bundle may be wrapped with one or more turns of electrical tape when required to achieve this fit. Plastic clamps or cable ties must not be used where their failure could result in interference with movable controls, wire bundle contact with movable equipment, or chafing damage to essential or unprotected wiring. They must not be used on vertical runs where inadvertent slack migration could result in chafing or other damage. Clamps must be installed with their attachment hardware positioned above them, wherever practicable, so that they are unlikely to rotate as the result of wire bundle weight or wire bundle chafing. (See figure 11-11.)
Clamps lined with nonmetallic material should be used to support the wire bundle along the run. Tying may be used between clamps, but should not be considered as a substitute for adequate clamping. Adhesive tapes are subject to age deterioration and, therefore, are not acceptable as a clamping means.
The back of the clamp, whenever practical, should be rested against a structural member. Clamps must be installed in such a manner that the electrical wires do not come in contact with other parts of the aircraft when subjected to vibration. Sufficient slack should be left between the last clamp and the electrical equipment to prevent strain at the terminal and to minimize adverse effects on shock-mounted equipment. Where wires or wire bundles pass through bulkheads or other structural members, a grommet or suitable clamp should be provided to prevent abrasion.
When wire bundle is clamped into position, if there is less than 3/8-inch clear ance between the bulkhead cutout and the wire bundle, a suitable grommet should be installed as indicated in figure 11-14. The grommet may be cut at a 45 degree angle to facilitate installation, provided it is cemented in place and the slot is located at the top of the cutout.
WIRE AND CABLE CLAMPS INSPECTION.
Inspect wire and cable clamps for proper tightness. Where cables pass through structure or bulkheads, inspect for proper clamping and grommets. Inspect for sufficient slack between the last clamp and the electronic equipment to prevent strain at the cable terminals and to minimize adverse effects on shock-mounted equipment.
DANGEROUS ANGLES
SAFE ANGLES FIGURE 11-11. Safe angle for cable clamps.
MS5-21919
CABLE CLAMP OR
EQUIVALENT MS-27039/NAS 603 SCREW AN 960 - WASHER, AN 960 PLAIN WASHER, PLAIN AN 9368
LOCKWASHER, MS 35338 LOCKWASHER, AN 340 NUT EXTERNAL TEETH SELF-LOCKING MS 21044 NUT, SPLIT FIGURE 11-12. Typical mounting hardware for MS-21919 cable clamps.
Par 11-146 Page 11-539
Par 11-147 Page 11-540
FIGURE 11-13. Installing cable clamp to structure.
A. CUSHION CLAMP AT MS21919 BULKHEAD HOLE.
CABLE CLAMP
CLEARANCE 3/8" MINIMUM WIRES LESS THAN 3/8 INCH
FROM HOLE EDGE
GROMMET
ANGLE BRACKET WITH
TWO POINT FASTENING MS21919
CABLE CLAMP B. CUSHION CLAMP AT
BULKHEAD HOLE WITH MS35489 GROMMET.
C. CUSHION CLAMP AT
BULKHEAD HOLE WITH MS21266 GROMMET.
ANGLE BRACKET WITH
TWO POINT FASTENING FIGURE 11-14. Clamping at a bulkhead hole.
11-148.11-154. [RESERVED.] Par 11-155 Page 11-541
Par 11-155 Page 11-542 SECTION 12. WIRE INSULATION AND LACING STRING TIE
GENERAL. Insulation of wires should be appropriately chosen in accordance with the environmental characteristics of wire routing areas. Routing of wires with dissimilar insulation, within the same bundle, is not recommended, particularly when relative motion and abrasion between wires having dissimilar insulation can occur. Soft insulating tubing (spaghetti) cannot be considered as mechanical protection against external abrasion of wire; since at best, it provides only a delaying action. Conduit or ducting should be used when mechanical protection is needed.
INSULATION MATERIALS. Insulating materials should be selected for the best combination of characteristics in the following categories:
Abrasion resistance.
Arc resistance (noncarbon tracking).
Corrosion resistance.
Cut-through strength.
Dielectric strength.
Flame resistance.
Heat distortion temperature.
Impact strength.
Mechanical strength.
Resistance to fluids.
Resistance to notch propagation.
Smoke emission.
Special properties unique to the aircraft.
For a more complete selection of insulated wires refer to SAE AS 4372 Aerospace Wire Performance Requirement and SAE AS 4373 Test Methods for Aerospace Wire.
STRIPPING INSULATION.
Attachment of wire, to connectors or terminals, requires the removal of insulation to expose the conductors.
This practice is commonly known as stripping.
Stripping may be accomplished in many ways; however, the following basic principles should be practiced.
Make sure all cutting tools used for stripping are sharp.
When using special wire stripping tools, adjust the tool to avoid nicking, cutting, or otherwise damaging the strands.
Damage to wires should not exceed the limits specified in table 11-13.
When performing the stripping operation, remove no more insulation than is necessary.
LACING AND TIES. Ties, lacing, and straps are used to secure wire groups or bundles to provide ease of maintenance, inspection, and installation. Braided lacing tape per MIL-T-43435 is suitable for lacing and tying wires. In lieu of applying ties, straps meeting Specification MS17821 or MS17822 may be used in areas where the temperature does not exceed 120 ºC. Straps may not be used in areas of SWAMP such as wheel wells, near wing flaps or wing folds. They may not be used in high vibration areas, where failure
Par 11-155 Page 11-543 TABLE 11-13. Allowable nicked or broken strands.
Maximum allowable nicked and broken strands Wire Size Conductor material Number of strands per conductor Total allowable nicked and broken strands 24-14 12-10 8-4 2-1 0-00 000 0000
8-000 Copper or Copper Alloy
Aluminum 19 37 133 665-817 1,045-1,330 1,665- 2,109-
All numbers of strands
2 nicked, none broken 4 nicked, none broken 6 nicked, 6 broken 6 nicked, 6 broken 6 nicked, 6 broken 6 nicked, 6 broken 6 nicked, 6 broken
None, None
of the strap would permit wiring to move against parts which could damage the insulation and foul mechanical linkages or other moving mechanical parts. They also may not be used where they could be exposed to UV light, unless the straps are resistant to such exposure.
Lacing. Lace wire groups or bundles inside junction boxes or other enclosures. Single cord-lacing method, shown in figure 11-15, and tying tape, meeting specification MIL-T-43435, may be used for wire groups of bundles 1-inch in diameter or less. The recommended knot for starting the single cord-lacing method is a clove hitch secured by a double-looped overhand knot as shown in figure 11-15, step a. Use the double cord-lacing method on wire bundles 1-inch in diameter or larger as shown in figure 11-16. When using the double cord-lacing method, employ a bowline on a bight as the starting knot.
Tying. Use wire group or bundle ties where the supports for the wire are more than 12 inches apart. A tie consists of a clove hitch, around the wire group or bundle, secured by a square knot as shown in figure 11-17.
Plastic Ties. Refer to Paragraph 11-220 and table 11-
21.
INSULATION TAPE. Insulation tape should be of a type suitable for the application, or as specified for that particular use. Insulation tape should be used primarily as a filler under clamps and as secondary support.
Nonadhesive tape may be used to wrap around wiring for additional protection, such as in wheel wells. All tape should have the ends tied or otherwise suitably secured to prevent unwinding. Tape used for protection should be applied so that overlapping layers shed liquids.
Drainage holes should be provided at all trap points and at each low point between clamps.
Plastic tapes, that absorb moisture or have volatile plasticizers that produce chemical reactions with other wiring, should not be used. (Reference MIL-W-5088.)
PULL HERE UNTIL TIGHT
BEFORE FINISHING KNOT
CORD CROSSES
UNDER LOOP STEP a - STARTING KNOT
STARTING FINAL KNOT KNOT _
TIGHTENED STEP b - INTERMEDIATE HALF HITCHES FIRST PART OF FINAL STEP c - (PART I) KNOT TIGHTENED TRIM TO 3/8" MIN. STEP c - (PART II) FINAL KNOT FIGURE 11-15. Single cord lacing.
STEP a STARTING KNOT -
BOWLINE ON A BIGHT
STARTING KNOT TIGHTENED STEP b INTERMEDIATE HALF HITCHES STEP c FINAL KNOT FIGURE 11-16. Double cord lacing.
Par 11-167 Page 11-544 (and 11-66)
Par 11-167 Page 11-545 (and 11-66)
FIGURE 11-17. Making ties.
11-160.11-166. [RESERVED.]
Par 11-167 Page 11-546 (and 11-66) SECTION 13. SPLICING.
GENERAL. Splicing is permitted on wiring as long as it does not affect the reliability and the electromechanical characteristics of the wiring.
Splicing of power wires, coaxial cables, multiplex bus, and large gauge wire must have approved data.
Splicing of electrical wire should be kept to a minimum and avoided entirely in locations subject to extreme vibrations. Splicing of individual wires in a group or bundle should have engineering approval and the splice(s) should be located to allow periodic inspection.
Many types of aircraft splice connectors are available for use when splicing individual wires. Use of a selfinsulated splice connector is preferred; however, a noninsulated splice connector may be used provided the splice is covered with plastic sleeving that is secured at both ends. Environmentally sealed splices, that conform to MIL-T-7928, provide a reliable means of splicing in SWAMP areas. However, a noninsulated splice connector may be used, provided the splice is covered with dual wall shrink sleeving of a suitable material.
There should not be more than one splice in any one wire segment between any two connectors or other disconnect points, except; when attaching to the spare pigtail lead of a potted connector, to splice multiple wires to a single wire, to adjust wire size to fit connector contact crimp barrel size, and to make an approved repair. (Reference MIL-W-5088 and NAVAIR 01-1A-505.)
Splices in bundles must be staggered so as to minimize any increase in the size of the bundle, preventing the bundle from fitting into its designated space, or cause congestion that will adversely affect maintenance. (See figure 11-18.)
Splices should not be used within 12 inches of a termination device, except for paragraph f below.
Splices may be used within 12 inches of a termination device when attaching to th e pigtail spare lead of a potted termination device, or to splice multiple wires to a single wire, or to adjust the wire sizes so that they are compatible with the contact crimp barrel sizes.
Selection of proper crimping tool, refer to paragraph
11-178.
FIGURE 11-18. Staggered splices in wire bundle.
11-168.11-173. [RESERVED.]
Par 11-174 Page 11-547
SECTION 14. TERMINAL REPAIRS
GENERAL. Terminals are attached to the ends of electrical wires to facilitate connection of the wires to terminal strips or items of equipment.
The tensile strength of the wire-to-terminal joint should be at least equivalent to the tensile strength of the wire itself, and its resistance negligible relative to the normal resistance of the wire.
Selection of Wire Terminals. The following should be considered in the selection of wire terminals.
Current rating.
Wire size (gauge) and insulation diameter.
Conductor material compatibility.
Stud size.
Insulation material compatibility.
Application environment.
Solder/solderless.
Pre-insulated crimp-type ring-tongue terminals are preferred. The strength, size, and supporting means of studs and binding posts, as well as the wire size, should be considered when determining the number of terminals to be attached to any one post. In hightemperature applications, the terminal temperature rating must be greater than the ambient temperature plus current related temperature ri se. Use of nickel-plated terminals and of uninsulated terminals with hightemperature insulating sleeves should be considered.
Terminal blocks should be provided with adequate electrical clearance or in sulation strips between mounting hardware and conductive parts.
Terminal Strips. Wires are usually joined at terminal strips. A terminal strip fitted with barriers should be used to prevent the term inals on adjacent studs from contacting each other. St uds should be anchored against rotation. When more than four terminals are to be connected together, a small metal bus should be mounted across two or more adjacent studs. In all cases, the current should be carried by the terminal contact surfaces and not by the stud itself. Defective studs should be replaced with studs of the same size and material since terminal stri p studs of the smaller sizes may shear due to overtightening the nut. The replacement stud should be securely mounted in the terminal strip and the terminal securing nut should be tight. Terminal strips should be mounted in such a manner that loose metallic objects cannot fall across the terminals or studs. It is good practice to provide at least one spare stud for future circuit expansion or in case a stud is broken. Terminal strips that provide connection of radio and electronic system s to the aircraft electrical system should be inspected for loose connections, metallic objects that may have fallen across the terminal strip, dirt and grease accumu lation, etc. These type conditions can cause arcing which may result in a fire, or system failures.
Terminal Lugs. Wire terminal lugs should be used to connect wiring to terminal block studs or equipment terminal studs. No more than four terminal lugs or three terminal lugs and a bus should be connected to any one stud. (Total number of terminal lugs per stud includes a common bus bar joining adjacent studs. Four terminal lugs plus a common bus bar thus are not permitted on one stud.) Te rminal lugs should be selected with a stud hole diameter that matches the diameter of the stud. However, when the terminal lugs attached to a
Par 11-176 Page 11-548 stud vary in diameter, the greatest diameter should be placed on the bottom and the smallest diameter on top.
Tightening terminal connections should not deform the terminal lugs or the studs. Terminal lugs should be so positioned that bending of the terminal lug is not required to remove the fastening screw or nut, and movement of the terminal lugs will tend to tighten the connection.
Copper Terminal Lugs. Solderless crimp style, copper wire, terminal lugs should be used and conform to MIL-T-7928. Spacers or washers should not be used between the tongues of terminal lugs.
Aluminum Terminal Lugs. The aluminum terminal lugs conforming to MIL-T-7099 (MS-25435, MS-25436, MS-25437, and MS-25438) should be crimped to aluminum wire only. The tongue of the aluminum terminal lugs or the total number of tongues of aluminum terminal lugs when stacked, should be sandwiched between two MS-25440 flat washers when terminated on terminal studs. Spacers or washers should not be used between the tongues of terminal lugs.
Special attention should be given to aluminum wire and cable installations to guard against conditions that would result in excessive voltage drop and high resistance at junctions that may ultimately lead to failure of the junction. Examples of such conditions are improper installation of terminals and washers, improper torsion (“torquing” of nuts), and inadequate terminal contact areas.
Class 2 Terminal Lugs. The Class 2 terminal lugs conforming to MIL-T-7928 may be used for installation, provided that in such installations, Class 1 terminal lugs are adequate for replacement without rework of installation or terminal lugs. Class 2 terminal lugs should be the insulated type, unless the conductor temperature exceeds 105 °C. In that case uninsulated terminal lugs should be used.
Parts’ lists should indicate the appropriate Class 1 terminal lugs to be used for service replacement of any Class 2 terminal lugs installed.
Termination of Shielded Wire. For termination of shielded wire refer to MIL-DTL-27500.
ATTACHMENT OF TERMINALS TO STUDS.
Connectors and terminals in aircraft require special attention to ensure a safe and satisfactory installation. Every possibility of short circuits, due to misinstallation, poor maintenance, and service life, should be addressed in the design. Electrical equipment malfunction has frequently been traced to poor terminal connections at terminal boards.
Loose, dirty, or corroded contact surfaces can produce localized heating that may ignite nearby combustible materials or overheat adjacent wire insulation.
STUDS AND INSULATORS. The following recommendations concerning studs also apply to other feed-through conductors.
Current Carrying Stud Resistance. Due to heat loss arising from wire-to-lug and lug-to-stud voltage drop, the resistance per unit length of a current carrying stud should not be greater than that of the wire.
Size of Studs. In designing the stud for a feed-through connection, attention should be given to the higher resistance of brass, as compared to copper. A suggested method of determining the size is to use a current density in the stud equivalent to that of the wire, compensating for the differe nce of resistance of the metals. Consideration should also be given to mechanical strength.
Support for Studs. The main stud support in the feedthrough insulation should be independent of the attachment of the lugs to