曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專營(yíng)店坑蒙拐騙欺詐消費(fèi)者

-5.0 to 0.0 kg.cm 1.0 to 1.5 kg.cm -5.1 to -2.0 kg.cm 25.5 to 33.1 kg.cm
center line horizontal center line horizontal center line horizontal upper surface horizontal upper surface horizontal
r P r P rP r P r
M = P * r
P ...[kg] or [lb]
r ...[cm] or [in]
Calculation. M = P * r Where M is the residual moment, r (cm or inches) is the distance between the hinge line
and the point where the force P (kg or lb) acts.
Notes. Positive moments are tail heavy, negative moments are nose heavy.
Rudder - weight and residual moment include lower hinge and trim plate.
Elevator - weight and residual moment include trim tab, horn, and trim tab control rods.
Aileron - weight and residual moment include horn, trim plate and hinges.
Wing flaps - Weight and residual moment include horn and hinges.
P
(12.57 to 15.21 lb) (0.617 to 0.860 lb) (5.73 to 6.94 lb) (9.26 to 11.35 lb)
(-4.34 to 0.00 in.lb) (0.868 to 1.302 in.lb) (-4.43 to -1.74 in.lb) (22.13 to 28.73 in.lb)
3.5 to 4.4 kg
(7.72 to 9.7 lb)
35.6 to 45.8 kg.cm
(30.9 to 39.75 in.lb)
AIRCRAFT
DA 40 Series
AMM
Standard Practices and
Structures
Doc # 6.02.01
Rev. 5 51-60-00 Page 7
20 Sep 2007
Figure 3a: Weights and Residual Moments Report %%
% (valid for TAE version with 'LRT', OÄM 40-130, installed)
AIRCRAFT
Standard Practices and
Structures
DA 40 Series
AMM
Page 8
20 Sep 2007 51-60-00 Doc # 6.02.01
Rev. 5
Rudder Elevator Trim Tab
Aileron Wing Flap
LH RH LH RH
weight
incl. BW
nominal
nominal
actual
actual
3.5 to 4.9 kg 5.7 to 6.9 kg 0.28 to 0.39 kg 2.6 to 3.15 kg 4.0 to 4.8 kg
balancing
weight
[kg] or [lb]
Center:
LH: RH:
P
r
residual
moment
35.6 to 44.8 kg.cm -5.0 to 0.0 kg.cm 1.0 to 1.5 kg.cm -5.1 to -2.0 kg.cm 23.4 to 31.1 kg.cm
center line horizontal center line horizontal center line horizontal upper surface horizontal upper surface horizontal
r P r P rP r P r
M = P * r
P ...[kg] or [lb]
r ...[cm] or [in]
Calculation. M = P * r Where M is the residual moment, r (cm or inches) is the distance between the hinge line
and the point where the force P (kg or lb) acts.
Notes. Positive moments are tail heavy, negative moments are nose heavy.
Rudder - weight and residual moment include lower hinge and trim plate.
Elevator - weight and residual moment include trim tab, horn, and trim tab control rods.
Aileron - weight and residual moment include horn, trim plate and hinges.
Wing flaps - Weight and residual moment include horn and hinges.
P
(7.72 to 10.8 lb) (12.57 to 15.21 lb) (0.617 to 0.860 lb) (5.73 to 6.94 lb) (8.82 to 10.58 lb)
(30.90 to 38.89 in.lb) (-4.34 to 0.00 in.lb) (0.868 to 1.302 in.lb) (-4.43 to -1.74 in.lb) (20.31 to 26.99 in.lb)
Figure 3b: Weights and Residual Moments Report %%
% (valid for TAE version with 'LRT-Rudder', MÄM 40-113, installed)
AIRCRAFT
DA 40 Series
AMM
Standard Practices and
Structures
Doc # 6.02.01
Rev. 5 51-60-00 Page 9
20 Sep 2007
Mass Balance
Weights
Pivot Axis
Pivot Axis
Moment Arm
Tape
Spring
Balance
Horizontal
Lower Mounting Bracket
Lower Mounting Bracket
Without Stop Bolts.
Moment
Arm
Top Pivot
Refer to Figure 1 (Standard Tanks) or Figure 2 (Long Range Tanks) for the weight and residual
% moment for the DA 40. Refer to Figure 3 for the weight and residual moment for the DA 40 D.
Use any suitable method to support the rudder horizontally at the pivot axis.
The rudder must be able to rotate freely around the pivot axis.
Remove the stop bolts from the lower mounting bracket before weighing and balancing.
The residual moment is tail heavy.
% Figure 4: Rudder Static Balance. Refer to Figure 1 (Standard Tanks) or Figure 2 (Long Range
% Tanks) for the weight and residual moment for the DA 40. Refer to Figure 3 for the weight and
% residual moment for the DA 40 D.
AIRCRAFT
Standard Practices and
Structures
DA 40 Series
AMM
Page 10
20 Sep 2007 51-60-00 Doc # 6.02.01
Rev. 5
Moment Arm
Horizontal
Pivot Axis
Pivot Axis
Balance Weight Balance Weight
Balance Weight
Tape
Spring Balance
Use any suitable method to support the elevator horizontally at the pivot axis.
The elevator must be able to rotate freely around the pivot axis.
The balance includes the trim tab, trim tab control rod and horn.
% Figure 5: Elevator Static Balance
AIRCRAFT
DA 40 Series
AMM
Standard Practices and
　
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