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DA 40 F
CHAPTER 28
FUEL SYSTEM
Section 28-00
Fuel System - Lycoming Engine
1. General
The 4th paragraph is amended to read:
All individual chambers are interconnected. The total usable fuel capacity of the fuel system is 152 % liters (40 US gal) with the Standard Tank and 189 liters (50 US gal) with the optional Long Range Tank installed. Two pumps supply fuel to the engine and a filter gives protection to sensitive components.
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The caption of figure 1 is amended to read:
% Figure 1: Fuel System Schematic Diagram Lycoming IO-360-M1A engine, Standard Tanks Installed
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The following figure is added behind figure 1:
% %
%
% Figure 1a: Fuel System Schematic Diagram Lycoming O-360-A4M engine, % Standard Tanks Installed
DA 40 F
1. Description
A. Standard Tanks
The third paragraph is amended to read:
There are two versions of the inboard fuel chamber. They look similar from outside, but can be identified by the version of the fuel quantity indicating system. Version A of the inboard fuel chamber is compatible with Version A of the fuel quantity indicating system (factory standard up to serial number 40.054). Version B of the inboard fuel chamber is compatible with Version B of the % fuel quantity indicating system (factory standard from serial number 40.055 on and all DA 40 F
% airplanes with the Lycoming O-360-A4M engine installed). Refer to Section 28-40 for more data on the fuel quantity indication system.
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DA 40 F
(2) Version B (M.M 40-047)
The last sentence is amended to read:
% Version B is factory standard from serial number 40.055 on (M.M 40-047 installed) and all % DA 40 F airplanes with the Lycoming O-360-A4M engine installed.
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Section 31-10 Instrument and Control Panels - Lycoming Engine
1. General
Add the following line to the list of instrument panel assemblies available:
) D4F-3142-00-00 (V.M-40-002, DA 40 F variant, Figure 24a)
Add the following figure:
Figure 24a: D4F-3142-00-00
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Legend
1 Electrical switches, ignition switch 18 Attitude gyro (artificial horizon)
2 Circuit breakers* 19 Vertical speed indicator (VSI)
3 Flap selector switch 20 Altimeter
4 Rotary buttons for instrument lighting and flood light 21 Course deviation indicator (CDI)
5 Test button for CO-detector 22 Intercom
6 Chronometer with OAT indicator 23 COM / NAV / GPS
7 Annunciator panel 24 ELT control unit
8 Engine instruments 25 Transponder
9 Fuel quantity indicator 26 Fuel prime button
10 Carbon-Monoxide detector 27 Stall warning horn
11 Accessory power socket 28 GPS Annunciation Unit
12 Microphone socket 29
13 Alternate static valve 30
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