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 636–647
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

Page 654Open in PDF

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

Page 658Open in PDF

Par 11-272 Page 11-594 TABLE 11-27. Electronic/Electrical Symbols (continued).

Symbol Meaning

Governor Speed Regulator

Relay

Inertia Switch

Mercur Switch

Terminals

Page 659Open in PDF

Par 11-272 Page 11-595 TABLE 11-27. Electronic/Electrical Symbols (continued).

Symbol Meaning

Cable Termination

Connector Disconnecting Device

Connectors of the Type Commonly Used for Power-Supply Purposes

Test Blocks

Coaxial Connector

Waveguide Flanges Waveguide Junction