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Wiring Diagram for Beechcraft 56TC Baron

Beechcraft 56TC Baron · Wiring Diagram

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Overview

This document serves as a wiring diagram for the Beechcraft 56TC Baron, providing essential information for maintenance and troubleshooting electrical systems. It is intended for use by certified technicians and pilots who require detailed electrical schematics for the aircraft. The wiring diagram illustrates the layout and connections of various electrical components, aiding in the understanding of the aircraft's electrical system and facilitating repairs or modifications as necessary.

  • The Beechcraft 56TC Baron operates on a 28-volt DC electrical system.
  • Two 12-volt batteries are used to power the electrical system.
  • Wiring diagrams include detailed connections for components like the alternator and starter.

Document

Source

Originally published by www.csobeech.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Wiring Diagram
Pages
7
File size
396 KB
Publisher
www.csobeech.com
How rare is it?
41Beechcraft 56TC Baron registered worldwide · 38 active

Common. Rarer than 2% of the aircraft models we track.

Documentation completeness
4/7

Most owners only have the POH. Here's the essential set for the Beechcraft 56TC Baron.

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In this document

Electrical System Overview

The electrical system of the Beechcraft 56TC Baron includes a 28-volt DC system powered by two 12-volt batteries. The wiring diagram outlines the main components, including the alternator, starter, and various circuit breakers.

Wiring Connections

Detailed wiring connections are provided for each component, including the location of terminals and connectors. This section is crucial for technicians performing maintenance or troubleshooting electrical issues.

Component Specifications

Specifications for key electrical components such as the alternator output, battery capacity, and circuit breaker ratings are included. This information is vital for ensuring compatibility and safety during repairs.

Safety notes

  • Ensure all electrical connections are secure to prevent system failures.
  • Follow proper safety protocols when working with the aircraft's electrical system.

Full document text

MAINTENANANCE INFORMATION AND ILLUSTRATED PARTS BREAKDOWN for LANDING GEAR MOTOR Part Number 96-380022 (Lamb Electric Co. P/N 14818) used on BEECHCRAFT BARON 55, 56TC, 58 and 58P DUKE 60 TRAVEL AIR 95 PUBLISHED BY COMMERCIAL PUBLICATIONS BEECH AIRCRAFT CORPORATION WICHITA, KANSAS 67201 P/N 98-35798B Reissued: November 15, 1985 PUBLISHED BY COMMERCIAL PUBLICATIONS BEECH AIRCRAFT CORPORATION WICHITA, KANSAS 67201 U. S. A. Beechcraft A Raytheon Company Member of GAMA General Aviation Manufacturers Association MAINTENANCE INFORMATION AND ILLUSTRATED PARTS BREAKDOWN for LANDING GEAR MOTOR P/N 96-380022 Disassembly (See illustration for index numbers) 1. Remove the 2 nuts (2) which are located on the end bracket (12). This will permit removal of the two end brackets and the armature assembly (16) from the field assembly (15). Do not disconnect wiring between commutator end bracket (13) and field assembly (15) unless necessary for future checking and/or repairs. 2. Loosen the 2 set screws (5) in the commutator end bracket (13) and remove brush and spring assembly (17). 3. Remove bearings (3) and (4) from armature shaft. Cleaning 1. Clean all parts, except sealed bearings, with PD680 solvent or equivalent. 2. Do not leave armature or coil of motor in solvent (permissible to immerse and remove immediately). 3. Dry all parts prior to reassembly. Inspection Inspect all parts and scrap those that are nonrepairable. Rejection The specific conditions listed below are cause for rejection. 1. Wear which is greater than the allowable wear tolerances given. 2. Damage which cannot be corrected by one or more of the authorized repairs listed in this manual. 3. Armature assemblies that have shafts that are heavily scored, or that are worn to the extent that bearings are loose on the shaft, or that have loose commutator segments. 4. Armature assemblies and field coils which have cracked, burned, or excessively worn insulation. 5. All screw that are severely damaged or have stripped, excessively worn or scored threads. 6. All gears on which teeth are severely worn. 7. Parts that are cracked, chipped, or broken. 8. Parts that have corrosion or other defects that cannot be repaired within the requirements of this manual. Repair and Reconditioning Recondition and make necessary repairs as follows: Retape or replace wiring that extends outside of the motor case if dirty or discolored. Do not disassemble more than necessary for complete check and reconditioning as follows: - 1 1. 13981 A Armature 2A 2B 3. 4. 30-7623 and 20-7609 Open Bearings (may be relubricated) 30-7625 and 20-7639 Sealed Bear- ings 14818F Field Coil Assembly 33107-A Brush Holder Assembly 5. 0-6864 End Bracket *0-6865 Visually inspect for excessive wear or damage. If noticeable step is worn on involute surface of gear end of shaft, replace armature. Check armature with "growler" for short circuit. If there is a short or open circuit, replace with new or rebuilt armature. If armature tests satisfactorily, recut surface of commutator (if burned, pitted, or uneven) until it is smooth, then regroove. Minimum acceptable diameter of commutator shall be .968 (31/32). The teeth of the armature gear shall not show severe wear or damage. With bearing clean and dry, rotate race by hand and feel for roughness, side-play and end-play; if noticeably greater than that of a new bearing, scrap and replace. Perform a magnetic particle inspection per MIL-I-6868. Install new bearings because the condition of sealed bearings cannot be determined. Visually inspect coils, poles, and housing for severe wear or damage. Replace any part as necessary. Using a "Hi-Pot” tester, check for high potential shorts by applying 500 volts of single phase, 60 cycle alternating current between the field coil wiring and housing for 5 to 15 seconds duration. No breakdown is permissible. Perform tests for continuity. Do not disassemble further unless damaged, or a short or open circuit is indicated, then disassemble only as necessary to repair. Visually inspect brush plugs, insulator and brush holder for severe wear or damage. Visually inspect end bracket for severe wear or damage. *NOTE: Do not disassemble from field coil assembly (4) unless necessary for further testing, rework, or replacement. 6. Visually inspect the following parts. Reuse all that show no severe wear or damage. 2 7978 10-7822 Set Screw 10-7888 Stud 7469 Nut 0-3518 8058 0-3883 0-3896 Load Spring Drive Pin Cord Bushing 39109-A Lead and Clip Assembly P-O-750 Таре YX10-1 Connector 106242-3-00014 Insulator MS20659-5 Terminal 0-2497 Washer 10-4431 Disc 5705 Screw 8047 Name Plate New Parts Required Parts Not To Be Reused - To Be Supplied New (2) 35175-A (2) MS24665-138 Brush Assem. Cotter Pin Authorized Repairs. These are in addition to the specific repairs noted in Repair and Reconditiong. 1. Slight scoring of shafts may be corrected by lapping carefully with a flat oil stone. 2. Smooth minor nicks, burrs and scratches. 3. Strip and replate, with same type plating as removed, those parts that are scratched or worn through the plating. 4. Chase the threads to clean or smooth minor thread damage. 5. Remove all corrosion. 6. Replace severely damaged or unserviceable parts with new or serviceable parts. 7. Revarnish all wiring as needed. 8. Bushings that check within dimensional range of a new part may be reused. Reassembly (See illustration for index numbers) Replace all scrapped parts with new or serviceable parts. 1. Repack all bearings* with MIL-G-23827 grease. Install needle bearings (7) in end bracket (13). Place bearings on armature shaft. NOTE: The bearing opposite the gear end shall be placed on the shaft in such a way that the shield faces inside of the motor. The needle bearing is to be installed with open end facing the outside of the motor. 2. Place new brush assembly and brush holder in the commutator end bracket. Paint around the brush

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holders and adjacent parts of the casting with P-2163 a corrosion preventive (product of General Electric). Before installing the 2 set screws on the outer side of commutator end bracket, place 2 or 3 drops of red Glyptal P-2081 in each set screw hole to cement them in place. 3. Place commutator end bracket, field coil assembly, armature, and end bracket in place and secure with 2 nuts. 4. Stake all flat-head screws at slots. Install cotter pin at brush caps." Functional Test 1. Connect the motor to 24 volts. Run-in to assure full seating of brushes. *30-7625 and 20-7639 are sealed bearings that cannot be lubricated. 3 2. Using a "Hi-Pot" tester, check for high potential shorts by applying 500 volts of single phase, 60 cycle alternating current between motor wiring and motor frame for a maximum duration of 15 seconds. No breakdown is permissible. 3. Check motor operation at no-load, with both clockwise and counterclockwise rotation. Noise and vibration shall not greatly exceed that of the average motor. 4. With motor running at no-load, current drain shall not exceed 6 1/2 amperes. MOTOR DATA Rated voltage - 24 volts DC Horsepower 1/4 to 1/5 Weight 2 lbs. 12 oz. Duty Cycle Intermittent Type - Series - Brush Replacement - New brush length is 17/32 inch. Commutator Minimum brush length is 7/32 inch. Clean commutator every second brush change with a light cut. Replace armature when the commutator reaches a minimum diameter of (.986) 31/32 inch. WHITE BLACK RED 00000 еееее Electrical Wiring Schematic The split field in the series-wound motor allows the motor to drive in either direction. The electric connections for shaft rotation (facing the pinion gear) are: for counterclockwise rotation connect the black and red leads to the line, to reverse connect black and white leads to the line. 4 5 8 17 18 13 3 14 16 15 12 11 19 10 LANDING GEAR MOTOR 123456789 Load Spring 7469 Nut 30-7623 Ball Bearing Ball Bearing Index Part Number IS14818 0-3518 Description Landing Gear Retract Motor Quantity Required 0-3896 10 10-4431 11 5705 12 0-6864 13 0-6865 20-7609 7978 MS24665-138 20-7642 0-3883 Set Screw Cotter Pin Bearing (Needle) Cord Bushing Cord Bushing Fibre Disc Brush Holder Screw End Bracket Comm. End Bracket 14 10-7888 Stud 15 14818-F Field 16 13981-A Armature 17 35107-A Brush & Spring Assem. 18 39109-A Lead and Clip Assem. 19 33107A Brush Holder Assem. 8047 Name Plate 0-2497 Fibre Washer 20-3841 Sleeve 0-5113 Clip 0-5114 Clasp 10-7822 8058 Set Screw Drive Pin 1221122122-1211 ama-20-22N 3 1 1 1 ........ 5

Type certificate, explained

What's in the Beechcraft 56TC Baron TCDS

A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.

TCDS 3A16Rev 90· Issued 2015
Read the full TCDS