AIRCRAFT
DA 42 NG AMM
Standard
Practices/Structures
Doc # 7.02.15
Rev. 4
51-60-00
Page 5
15 Mar 2018
SN:
W
e
ig
h
t in
cl.
ma
s
s
b
a
la
nc
e
DA 42 NG
Mass Balance [lb]
P [lbf]
r [in]
Upper Rudder Horn
Lower Rudder Horn
Rudder
Elevator
Elevator Trim
Tab
Rudder Trim
Limits [lbf]
Limits [lbf in]
20.0 to 28.7
1.13 to 1.87
0.87 to 6.60
0.87 to 1.30
14.6 to 18.2
0.62 to 0.86
11.7 to 14.0
0.62 to 0.86
Actual [lbf]
Actual [lbf in]
Centre:
Push Rod:
L:
R:
S
tat
ic
Mo
me
n
t
Center-line horizontal
Rudder trim tab and push rod
Elevator trim tab and push rod
Center-line horizontal
M = P*r
P [lbf]
r [in]
P
P
P
P
r
r
r
r
Typ: 20.63 in
Typ: 5.1 in
Typ: 12.2 in
Typ: 3.94 in
Figure 4: Typical Weights and Residual Moments Report DA 42 NG Airplane
(if MÄM 42-600 is NOT installed) - Sheet 1 (Imperial Dimensions)
Summary of Contents for DA 42 NG
Page 933: ...AIRCRAFT DA 42 NG AMM Fuel Doc 7 02 15 Rev 4 28 TITLE Page 1 15 Mar 2018 CHAPTER 28 FUEL ...
Page 1459: ...AIRCRAFT DA 42 NG AMM Lights Doc 7 02 15 Rev 4 33 TITLE Page 1 15 Mar 2018 CHAPTER 33 LIGHTS ...
Page 1711: ...AIRCRAFT DA 42 NG AMM Doors Doc 7 02 15 Rev 4 52 TITLE Page 1 15 Mar 2018 CHAPTER 52 DOORS ...
Page 1853: ...AIRCRAFT DA 42 NG AMM Wings Doc 7 02 15 Rev 4 57 TITLE Page 1 15 Mar 2018 CHAPTER 57 WINGS ...
Page 2071: ...AIRCRAFT DA 42 NG AMM Engine Doc 7 02 15 Rev 4 72 TITLE Page 1 15 Mar 2018 CHAPTER 72 ENGINE ...
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