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
06-00-00
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 中國航空網 m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：鉆石40飛機維護手冊 DA 40 SERIES AMM 1(62)
