Page 4 Doc # 6.02.01 09 Jan 2003 Rev. 4
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Dimensions and Areas
AMM
Elevator
Up
Down
22° to 24°
14° to 16°
Cruise
Cruise
Take Off
Take Off
+1° to -1°
+1° to -1°
Right Aileron
Left Aileron
18° to 22°
18° to 22°
Up Down
Up Down
18° to 22°
13° to 15°
18° to 22°
13° to 15°
Figure 3: Control Surface Deflections % (valid for Lycoming version with 'Standard' tanks and for TAE version)
Doc # 6.02.01 Page 5
Rev. 4 09 Jan 2003
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AIRCRAFT AMM
Figure 4: Control Surfaces Adjustment Report % (valid for Lycoming version with 'Standard' tanks and for TAE version)
Page 6 Doc # 6.02.01 09 Jan 2003 Rev. 4
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Dimensions and Areas
AMM
%
Elevator
%
%
%
%
%
%
%
% Figure 5: Control Surface Deflections
% (valid for Lycoming version with 'Long Range' tanks installed, O.M 40-071)
%
%
06-00-00
AMM
% % % % % % % % % % % % % % % % % % % % % % % % % % % % % % % % % % % % % % % Figure 6: Control Surfaces Adjustment Report % (valid for Lycoming version with 'Long Range' tanks installed, O.M 40-071)
DA 40 Series
Flap Position Flap Left Flap Right
Radius(mm) 233 233 200 200 200 200 200 200 375 375 240 240
Cruise(UP) Nominal(mm) 0±4 0±4
Actual(mm)
Nominal(°) 0° ±1° 0° ±1°
Actual(°)
Take-Off(T/O) Nominal(mm) 81±8 81±8
Actual(mm)
Nominal(°) +20°±2° +20° ±2°
73.5±6.0 44±3.5 5±6.5
63.5±3.5 33±3.5 20±3.5
52±6.5 21.5±3.5 37.5±6.5
Actual(°)
Landing(LDG) Nominal(mm) 167±4 167±4
Actual(mm)
-46°±4° -27°±2° +3°±4°
-39°±2° -20°±2° +12°±2°
-32°±4° -13°±2° +23°±4°
Nominal(°) +42° ±1° +42° ±1°
Actual(°)
Pre-Load Nominal 3 -5 -11 kp6.6 lbf 3 -5 kp6.6 -11 lbf
Actual
Page 8 Doc # 6.02.01 09 Jan 2003 Rev. 4
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Dimensions and Areas
AMM
Adjustment Report Registration
Date
Wings Horizontal Stabilizer Main Landing Gear (at Empty Weight, on Glide Sheets) Rudder Controls 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址:钻石40飞机维护手册 DA 40 SERIES AMM 1(62)