24-30-00 Alternator E4A-91-000-000
1. General
This section contains the procedures how to remove/install and examine Alternator E4A-91-000-000.
Fig. 24 - 3 Alternator E4A-91-000-000
2. Maintenance Procedures
A. Remove the Alternator
Refer to the applicable Aircraft
Maintenance Manual.
Disconnect the power line from the B+ terminal.
Disconnect the excitation line marked with
“GEN/G2”.
Remove the V-Ribbed belt.
Refer to Section 85-40-00 Paragraph
1.A.
Remove the screws that attach the alternator
bracket to the engine.
Remove the alternator from the alternator
bracket.