AeroElectric-List Digest Archive
Wed 04/21/21 |
Total Messages Posted: 1 |
Today's Message Index:
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1. 04:43 AM - Re: Next Generation Z-Figures (pilot_pat)
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Time: 04:43:24 AM PST US
Subject: Re: Next Generation Z-Figures
From: "pilot_pat" <ocainp@gmail.com>
Planning on Battery, Main, Engine and Aux Buses, connected as shown in Z101B.
There will be a second alternator using a B&C regulator rather than the Ford; no
second battery aside from IBBS.
TCW 6 Ah IBBS would be charged from main bus and power via "aircraft power 2" inputs
the PFD, the engine monitor GEA24, the ADHRS GSU25 and the GPS20A.
Main battery (16 Ah): plan on load testing at annual and operational testing on
first daily engine start.
Engine fuel injection will be Airflow Performance FM-150 and ignition will be dual
pmag 114s fed from the engine bus for starting. Fuel pump is an Airflow Performance
Auxiliary pump assembly.
Pat
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=501460#501460
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