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Aviation Maintenance Technician Handbook–Airframe

FAA-H-8083-31B Version 2023

Chapter 9

Aircraft Electrical System

In some instances, the wire may be capable of carrying more

Figure 9-115. American wire gauge for standard annealed solid copper wire.
Figure 9-115. American wire gauge for standard annealed solid copper wire.
Formula: Figure 9-115 formula reference: American Wire Gauge reference for annealed solid copper: AWG 0000 through 40 with conductor diameter, circular-mil area, square-inch area, and resistance in ohms per 1,000 feet at 25 °C and 65 °C. Source text: Cross Section Ohms per 1,000 ft ; Gauge Number Diameter (mils) Circular (mils) Square inches 25 °C (77 °F) 65 °C (149 °F) ; 0000 460.0 212,000.0 0.166 0.0500 0.0577 ; 000 410.0 168,000.0 0.132 0.0630 0.0727 ; 00 365.0 133,000.0 0.105 0.0795 0.0917 ; 0 325.0 106,000.0 0.0829 0.100 0.166 ; 1 289.0 83,700.0 0.0657 0.126 0.146 ; 2 258.0 66,400.0 0.0521 0.159 0.184 ; 3 229.0 52,600.0 0.0413 0.201 0.232 ; 4 204.0 41,700.0 0.0328 0.253 0.292 ; 5 182.0 33,100.0 0.0260 0.319 0.369 ; 6 162.0 26,300.0 0.0206 0.403 0.465 ; 7 144.0 20,800.0 0.0164 0.508 0.586 ; 8 128.0 16,500.0 0.0130 0.641 0.739 ; 9 114.0 13,100.0 0.0103 0.808 0.932 ; 10 102.0 10,400.0 0.00815 1.02 1.18 ; 11 91.0 8,230.0 0.00647 1.28 1.48 ; 12 81.0 6,530.0 0.00513 1.62 1.87 ; 13 72.0 5,180.0 0.00407 2.04 2.36 ; 14 64.0 4,110.0 0.00323 2.58 2.97 ; 15 57.0 3,260.0 0.00256 3.25 3.75 ; 16 51.0 2,580.0 0.00203 4.09 4.73 ; 17 45.0 2,050.0 0.00161 5.16 5.96 ; 18 40.0 1,620.0 0.00128 6.51 7.51 ; 19 36.0 1,290.0 0.00101 8.21 9.48 ; 20 32.0 1,020.0 0.000802 10.40 11.90 ; 21 28.5 810.0 0.000636 13.10 15.10 ; 22 25.3 642.0 0.000505 16.50 19.00 ; 23 22.6 509.0 0.000400 20.80 24.00 ; 24 20.1 404.0 0.000317 26.20 30.20 ; 25 17.9 320.0 0.000252 33.00 38.10 ; 26 15.9 254.0 0.000200 41.60 48.00 ; 27 14.2 202.0 0.000158 52.50 60.60 ; 28 12.6 160.0 0.000126 66.20 76.40 ; 29 11.3 127.0 0.0000995 83.40 96.30 ; 30 10.0 101.0 0.0000789 105.00 121.00 ; 31 8.9 79.7 0.0000626 133.00 153.00 ; 32 8.0 63.2 0.0000496 167.00 193.00 ; 33 7.1 50.1 0.0000394 211.00 243.00 ; 34 6.3 39.8 0.0000312 266.00 307.00 ; 35 5.6 31.5 0.0000248 335.00 387.00 ; 36 5.0 25.0 0.0000196 423.00 488.00 ; 37 4.5 19.8 0.0000156 533.00 616.00 ; 38 4.0 15.7 0.0000123 673.00 776.00 ; 39 3.5 12.5 0.0000098 848.00 979.00 ; 40 3.1 9.9 0.0000078 1,070.00 1,230.00

current than is recommended for the contacts of the related connector. In this instance, it is the contact rating that dictates the maximum current to be carried by a wire. Wires of larger gauge may need to be used to fit within the crimp range of connector contacts that are adequately rated for the current being carried. Figure 9-117 gives a family of curves whereby the bundle derating factor may be obtained.

Maximum Operating Temperature

The current that causes a temperature steady state condition equal to the rated temperature of the wire should not be exceeded. Rated temperature of the wire may be based upon the ability of either the conductor or the insulation to withstand continuous operation without degradation.

Single Wire in Free Air Determining a wiring system’s current-carrying capacity begins with determining the maximum current that a given-sized wire can carry without exceeding the allowable temperature difference (wire rating minus ambient °C). The curves are based upon a single copper wire in free air. [Figure 9-117]

Wires in a Harness When wires are bundled into harnesses, the current derived for a single wire must be reduced, as shown in Figure 9-118. The amount of current derating is a function of the number of wires in the bundle and the percentage of the total wire bundle capacity that is being used.

Harness at Altitude Since heat loss from the bundle is reduced with increased altitude, the amount of current should be derated. Figure 9-119 gives a curve whereby the altitude-derating factor may be obtained.

Aluminum Conductor Wire When aluminum conductor wire is used, sizes should be selected on the basis of current ratings shown in Figure 9-120. The use of sizes smaller than #8 is discouraged. Aluminum wire should not be attached to engine mounted accessories or used in areas having corrosive fumes, severe vibration, mechanical stresses, or where there is a need for frequent disconnection. Use of aluminum wire is also discouraged for runs of less than 3 feet. Termination hardware should be of the type specifically designed for use with aluminum conductor wiring.

Computing Current Carrying Capacity

The following section presents some examples on how to calculate the load carrying capacity of aircraft electrical wire. The calculation is a step by step approach and several graphs are used to obtain information to compute the current carrying capacity of a particular wire.

Example 1 Assume a harness (open or braided) consisting of 10 wires, size 20, 200 °C rated copper, and 25 wires size 22, 200 °C rated copper, is installed in an area where the ambient

Formula: temperature is 60 °C and the aircraft is capable of operating ; at a 35,000 foot altitude. Circuit analysis reveals that 7 of the ; 35 wires in the bundle (7/35 = 20 percent) are carrying power

currents near or up to capacity.

Step 1—Refer to the single wire in free air graph in

to determine free air ratings. Since the wire is in an ambient

Formula: temperature of 60 °C and rated at 200 °C, the change of the ; temperature is 200 °C – 60 °C = 140 °C. Follow the 140 °C

temperature difference horizontally until it intersects with wire size line on Figure 9-117. The free air rating for size 20 is 21.5 amps, and the free air rating for size 22 is 16.2 amps.

Step 2—Refer to the bundle derating curves in Figure 9-118. The 20 percent curve is selected since circuit analysis indicate that 20 percent or less of the wire in the harness would be carrying power currents and less than 20 percent of the bundle capacity would be used. Find 35 (on the horizontal axis), since there are 35 wires in the bundle, and determine a derating factor of 0.52 (on the vertical axis) from the 20 percent curve.