AC 43.13-1B

Historical

Advisory circular · Acceptable Methods, Techniques, and Practices—Aircraft Inspection and Repair

A newer version is currentThis is a historical version. AC 43.13-1B CHG 1 Ed Update is the version in force, approved September 27, 2001.
Approved
September 8, 1998
Last reviewed
June 11, 2024
Cancelled by
AC43.13-1B CHG 1
Family
AC 43.13-1 · 7 versions
Revision
B
14 CFR parts
43, 65, 145, 21, 105, 23, 91, 121, 25
Cited by
95 ADs

Guidance, not mandatory unless a rule or AD requires it. DRS record last changed November 21, 2025.

Show pages 634–645
Page 646Open in PDF

Par 11-248 Page 11-582

SECTION 18. CONDUITS

GENERAL. Conduit is manufactured in metallic and nonmetallic materials and in both rigid and flexible forms. Primarily, its purpose is for mechanical protection of cables or wires. Conduit should be inspected for:

proper end fittings; absence of abrasion at the end fittings; proper clamping; distortion;

adequate drain points which are free of dirt, grease, or other obstructions; and freedom from abrasion or damage due to moving objects, such as aircraft control cables or shifting cargo.

SIZE OF CONDUIT. Conduit size should be selected for a specific wire bundle application to allow for ease in maintenance, and possible future circuit expansion, by specifying the conduit inner diameter (I.D.) about 25 percent larger than the maximum diameter of the wire bundle.

CONDUIT FITTINGS. Wire is vulnerable to abrasion at conduit ends. Suitable fittings should be affixed to conduit ends in such a manner that a smooth surface comes in contact with the wire. When fittings are not used, the end of the conduit should be flared to prevent wire insulation damage. Conduit should be supported by use of clamps along the conduit run.

CONDUIT INSTALLATION.

Conduit problems can be avoided by following these guidelines:

Do not locate conduit where passengers or maintenance personnel might use it as a handhold or footstep.

Provide drainholes at the lowest point in a conduit run. Drilling burrs should be carefully removed.

Support conduit to prevent chafi ng against structure and to avoid stressing its end fittings.

RIGID CONDUIT. Conduit sections that have been damaged should be repaired to preclude injury to the wires or wire bundle which may consume as much as 80 percent of the tube area. Minimum acceptable tube bend radii for rigid conduit are shown in table 11-23. Kinked or wrinkled bends in rigid conduits are not recommended and should be replaced. Tubing bends that have been flattened into an ellipse and the minor diameter is less than 75 percent of the nominal tubing diameter should be replaced because the tube area will have been reduced by at least 10 percent. Tubing that has been formed and cut to final length should be deburred to prevent wire insulation damage. When installing replacement tube sections with fittings at both ends, care should be taken to eliminate mechanical strain.

TABLE 11-23. Bend radii for rigid conduit.

Nominal Tube O.D.

(inches) Minimum Bend Radii (inches) 1/8 3/16 1/4 3/8 1/2 5/8 3/4 1 1 1/4 1 1/2 1 3/4 2 3/8 7/16 9/16 15/16 1 1/4 1 1/2 1 3/4 3 3 3/4 5 7 8

Page 647Open in PDF

Par 11-253 Page 11-583 FLEXIBLE CONDUIT. Flexible aluminum conduit conforming to Specification MIL-C-6136 is available in two types: Type I, Bare Flexible Conduit, and Type II, Rubber Covered Flexible Conduit. Flexible brass conduit conforming to Specification MIL-C-7931 is available and normally used instead of flexible aluminum where necessary to minimize radio interference. Also available is a plastic flexible tubing. (Reference MIL-T-8191A.) Flexible conduit may be used where it is impractical to use rigid conduit, such as areas that have motion between conduit ends or where complex bends are necessary. The use of transparent adhesive tape is recommended when cutting flexible tubing with a hacksaw to minimize fraying of the braid. The tape should be centered over the cutting reference mark with the saw cutting through the tape. After cutting the flexible conduit, the transparent tape should be removed, the frayed braid ends trimmed, burrs removed from inside the conduit, and coupling nut and ferrule installed. Minimum acceptable bending radii for flexible conduit are shown in table 11-24.

TABLE 11-24. Minimum bending radii for flexible aluminum or brass conduit.

Nominal I.D. of conduit (inches) Minimum bending radius inside (inches) 3/16 1/4 3/8 1/2 5/8 3/4 1 1 1/4 1 1/2 1 3/4 2 2 1/2 2 1/4 2 3/4 3 3/4 3 3/4 3 3/4 4 1/4 5 3/4 8 8 1/4 9 9 3/4 10

11-254.11-259. [RESERVED.]

Page 648Open in PDF

Par 11-260 Page 11-584

SECTION 19. PROTECTION OF UNUSED CONNECTORS

GENERAL. Connectors may have one or more contact cavities that are not used. Depending on the connector installation, unused connector contact cavities may need to be properly sealed to avoid damage to the connector, or have string wire installed.

QUICK REFERENCE CHART. A quick reference chart of unused connector contact cavity requirements is given in table 11-25. These requirements apply to harness manufacturing or connector replacement only.

UNPRESSURIZED AREA CONNECTORS.

Connectors may be installed in unpressurized areas of the aircraft. Unused connector contact cavities installed in unpressurized areas should be properly sealed as follows:

Firewall Connectors Installations. Firewall unused connector contact cavities should be filled with spare contacts and stub wires. (See figure 11-39.)

Construct stub wires using high temperature wire (260 ºC). Ensure that stub wires are of the same type of wires in the bundle.

Crimp the proper contact, for the connector and cavity being used, onto the wire. Install the crimped contact into the unused cavity.

Extend stub wires beyond the back of the connector clamp from 1.5 to 6 inches. Feather trim stub wires to taper wire bundle.

Secure wire ends with high temperature (greater than 250 ºC) lacing cord. Nylon cable ties are not allowed for this installation.

NOTE: Both connectors mating through the engine fire-seal are considered firewall connectors. Connectors mounted on or near, but not through, the engine fire-seal are not considered firewall connectors

Non-firewall Connector Installations. In this type of installation all unused connector cavities must also be filled with spare contacts. It is not required, however, to crimp stub wires on filling contacts.

Fill unused contact cavities with spare contacts and Teflon sealing plugs or rods. (See figure 11-40.) Rods shall be cut so that they extend 1/8 to 1/4 inch beyond the surface of the grommet when bottomed against the end of the spare contact. (See table 11-26 for dimensions.)

PRESSURIZED AREAS. Connectors installed in pressurized areas of the aircraft may be divided into two main installation categories, sealed and unsealed.

Sealed connector installations. Sealed connectors installed in pressurized areas must have their unused contact cavities filled with Teflon sealing plugs or rods.

(See figure 11-40.) Installation of spare contacts is optional, except for future wiring addition requirements.

(See paragraph 11-234). No stub wires are required.

Unsealed Connector Installations. It is not required to fill unused contact cavities of unsealed connectors installed in pressurized areas with Teflon sealing plugs or rods. Installation of spare contacts is optional, except for future wiring additi on requirements. (See paragraph 11-234.)

Page 649Open in PDF

Par 11-271 Page 11-585 TABLE 11-25. Contact cavity sealing-quick reference.

Connector Installation Types Unpressurized Area Sealing Means Firewall

Non-Firewall Sealing Plugs or Teflon Sealing Rods

No

Yes Stub Wires (Note 2) Yes No Spare Contacts Yes Yes NOTE 1: Sealing plugs may be included with the spare connector and may be used for sealing unused contacts. Sealing rods are procured from stock by the foot. (See table 11-26 for sealing rod dimensions.)

NOTE 2: Stub wires must be of the same type as the other wires of the bundle.

F IGURE 11-39. Stub wire installation.

TABLE 11-26. Sealing rod dimensions.

CONTACT SIZE DIAMETER ROD LENGTH (INCHES) (AWG) (INCHES) MIN MAX 20 1/16 5/8” 3/4” 16 3/32 7/8” 1” 12 1/8 7/8” 1”

FIGURE 11-40. Sealing unused contact cavities-unpressurized areas-(cut-away view).

11-264.11-270. [RESERVED.]

Page 650Open in PDF

Par 11-271 Page 11-586 SECTION 20. ELECTRICAL AND ELECTRONIC SYMBOLS

GENERAL. The electrical and electronic symbols shown here are those that are likely to be encountered by the aviation maintenance technician. They are in accordance with ANSI-Y32.2-1975.

SYMBOLS. Only those symbols associated with aircraft electrical and electronic wiring have been listed in general. Refer to ANSI- Y32.2-1975 for more specific detail on each symbol.

TABLE 11-27. Electronic/Electrical Symbols.

Symbol Meaning

Adjustability Variability

Radiation Indicators

Physical State Recognition

Test-Point Recognition

Polarity Markings

Direction of Flow of Power, Signal, or Information

Kind of Current

Envelope Enclosure

Shield Shielding

Special Connector or Cable Indicator

Page 651Open in PDF

Par 11-271 Page 11-587 TABLE 11-27. Electronic/Electrical Symbols (continued).

Symbol Meaning

Resistor

Capacitor

Antenna

Battery

Thermal Element Thermomechanical Transducer

Thermocouple

Spark Gap Ignitor Gap

Continuous Loop Fire Detector (Temperature Sensor)

Ignitor Plug

Page 652Open in PDF

Par 11-272 Page 11-588 TABLE 11-27. Electronic/Electrical Symbols (continued).

Symbol Meaning

Transmission Patch Conductor Cable Wiring

Distribution Lines Transmission Lines

Alternative or Conditioned Wiring

Associated or Future

Page 653Open in PDF

Par 11-272 Page 11-589 TABLE 11-27. Electronic/Electrical Symbols (continued).

Symbol Meaning

Intentional Isolation of Direct-Current Path in Coaxial or Waveguide Applications

Waveguide

Strip-Type Transmission Line

Termination

Circuit Return

Pressure-Tight Bulkhead Cable Gland Cable Sealing End

Switching Function

Electrical Contact

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Par 11-272 Page 11-590 TABLE 11-27. Electronic/Electrical Symbols (continued).

Symbol Meaning

Basic Contact Assemblies

Magnetic Blowout Coil

Operating Coil Relay Coil

Switch

Pushbutton, Momentary, or Spring-Return

Page 655Open in PDF

Par 11-272 Page 11-591 TABLE 11-27. Electronic/Electrical Symbols (continued).

Symbol Meaning

Two-Circuit, Maintained, or Not Spring-Return

Nonlocking Switching, Momentary, or Spring- Return

Locking Switch

Combination Locking and Nonlocking Switch

Key-Type Switch Lever Switch

Page 656Open in PDF

Par 11-272 Page 11-592 TABLE 11-27. Electronic/Electrical Symbols (continued).

Symbol Meaning

Selector or Multiposition Switch

Safety Interlock

Limit Switch Sensitive Switch

Switches with Time-Delay Feature

Flow-Actuated Switch

Page 657Open in PDF

Par 11-272 Page 11-593 TABLE 11-27. Electronic/Electrical Symbols (continued).

Symbol Meaning

Liquid-Level Actuated Switch

Pressure- or Vacuum-Actuated Switch

Temperature-Actuated Switch

Thermostat

Flasher Self-Interrupting Switch

Foot-Operated Switch Foot Switch

Switch Operated by Shaft Rotation and Responsive to Speed or Direction

Switches with Specific Features