钻石40飞机维护手册 DA 40 SERIES AMM 3(60)

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%) 31-50 The central warning system for the DA 40 with the Lycoming engine installed.
%) 31-51 The central warning system for the DA 40 with the TAE 125 Diesel engine installed.
The DA 40 has these indicating systems:
) An instrument panel. The instrument panel is made in one piece with a shelf. The shelf goes between the panel and the firewall.
) A control panel in the center console. This panel has the engine controls, fuel controls, cabin heat control levers, parking brake and trim. It has a forward part and an aft part.
) Independent instruments. The airplane has an integrated electronic indicating system which covers the engine instruments and fuel quantities. The airplane also has a digital chronometer (optional), an optional engine operated hours meter and an outside air temperature (OAT) indicator.
%) Warning lights (red), caution lights (amber), and status lights (white).
This Section does not tell you about the indicators that belong to systems. See the related system for data. For example, see Section 27-31 for data about the trim indicator.
Note:  Equipment which is certified for installation in the DA 40 is listed in Section 6.5 of the Airplane Flight Manual. Such equipment may be installed in accordance with the Airplane Maintenance Manual.
Any equipment which is not listed in Section 6.5 of the Airplane Flight Manual is called "Additional Equipment". The installation of Additional Equipment is a modification which must be handled in accordance with national regulations or a Service Bulletin.
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Section 31-10
Instrument and Control Panels - Lycoming Engine

1. General
% The DA 40 with the Lycoming engine installed has these instrument and control panels: ) An instrument panel. The instrument panel is made in one piece with a shelf. The shelf goes between the panel and the firewall. ) A control panel in the center console. This panel has a forward cover and an aft cover. The forward cover has the cabin heat control levers and parking brake lever. The aft cover has the engine controls and fuel shut-off valve. See the related Chapter or Section for data about the controls. For example, see Section 76-00 for data on the engine controls.
% The instrument and avionic equipment installed in the airplane can be chosen by the customer. The
% following instrument panel assemblies are available:
%) DA4-3110-00-00 (Basic certification, Figure 1)

%) DA4-3120-00-00 (O.M 40-067, Figure 2) %) DA4-3111-00-00 (O.M 40-064, Figure 3) %) DA4-3112-00-00 (O.M 40-065a, Figure 4) %) DA4-3117-00-00 (O.M 40-089, Figure 5) %) DA4-3120-00-00/1 (O.M 40-071, Figure 6) %) DA4-3121-00-00 (O.M 40-054, Figure 7) %) DA4-3122-00-00 (O.M 40-091, Figure 8) %) DA4-3123-00-00 (O.M 40-097, Figure 9) %) DA4-3123-00-00/1 (O.M 40-071, Figure 10) %) DA4-3124-00-00 (O.M 40-098, Figure 11) %) DA4-3126-00-00 (O.M 40-103, Figure 12) %) DA4-3129-00-00 (O.M 40-104, Figure 13)
%

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%) DA4-3130-00-00 (O.M 40-114, Figure 14) %) DA4-3131-00-00 (O.M 40-115, Figure 15) %) DA4-3132-00-00 (O.M 40-117, Figure 16) %) DA4-3133-00-00 (O.M 40-120, Figure 17) %) DA4-3134-00-00 (O.M 40-119, Figure 18) %) DA4-3135-00-00 (O.M 40-121, Figure 19) %) DA4-3137-00-00 (O.M 40-117a, Figure 20) %) DA4-3138-00-00 (O.M 40-122, Figure 21) %) DA4-3139-00-00 (O.M 40-127, Figure 22) %) DA4-3140-00-00 (O.M 40-128, Figure 23) %) DA4-3141-00-00 (O.M 40-138, Figure 24)
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% Figure 2: DA4-3120-00-00
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% Figure 4: DA4-3112-00-00 % % % % % % % % % % % % % %

%

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