Chapter 24 Electrical Power - Extra Aircraft

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EXTRA - FLUGZEUGBAU GmbHSERVICE MANUAL EXTRA 30024-60-00 DC ELECTRICAL LOAD DISTRIBUTION(Refer to Figure 0 of Chapter 91) From the main bus whichphysically corresponds to the bus bar the electrical load isdistributed through circuit breakers and switches.The bus bar is located at the back side of the circuitbreakers, the circuit breakers themselves are located at thelower rear instrument panel so as the lever switches.Subminiature pushbotton switches for the radio resp. intercomare mounted on the control sticks and the throttlecontrols.More information concerning the wiring shows Figure 0 ofChapter 91.PAGE DATE: 31. January 1995CHAPTER 24PAGE 8
EXTRA - FLUGZEUGBAU GmbHSERVICE MANUAL EXTRA 30024-61-00 MAINTENANCE PRACTICESI M P O R T A N TIf replacement of wiring passing the firewall is necessary,renew the sealing of the bushing grooves and gapsat the engine side of the firewall. Use PRC-812 (ProductsResearch & Chemical Corporation, USA) firewallsealant.24-61-01 Circuit BreakerRemoval/InstallationC A U T I O NEnsure the master switch is in Off-position.1 Remove the lower panel attachment screws.2 Turn down the panel.3 Loosen the bus bar attachment screws and remove busbar if necessary.4 Disconnect wiring.5 Remove the attachment nut at the front side of the instrumentpanel.6 Remove the circuit breaker.7 Install in reverse sequence of removal.24-61-02 Lever SwitchRemoval/InstallationC A U T I O NDisconnect battery1 Remove the lower panel attachment screws.2 Turn down the panel.PAGE DATE: 31. January 1995CHAPTER 24PAGE 9
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Chapter 24 Electrical Power - Extra Aircraft

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