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Flaps push-rod attachment bracket, flap 50.0
Landing/taxi light bracket (screws) 10.0
Pitot head base 6.0
Tip light assembly base plate 8.0
RH WING
Aileron push-rod
attachment
bracket, aileron 50.0
Flap asymmetrical tube bonding strap connection 10.0
% Flaps push-rod attachment bracket, flap 50.0
Tip light assembly base plate 8.0
AIRCRAFT
Standard Practices and
Structures
DA 40 Series
AMM
Page 204
20 Sep 2007 51-80-00 Doc # 6.02.01
Rev. 5
B. Low Resistance Measurements in Control System (Lycoming version)
Item Attachment Point
max.
allowable
[mΩ]
measured
[mΩ]
passed
Pilot stick tube 50.0
Co-pilot stick tube 50.0
Trim wheel assembly frame 5.0
Levers frame 10.0
Pilot pedal assembly 150.0
Co-pilot pedal assembly 150.0
C. High Resistance Measurements (Lycoming version)
Use a wet sponge to obtain a constant electrical connection to the static dischargers.
Item Attachment point
max.
allowable
[MΩ]
measured
at 250 V
[MΩ]
passed
STATIC DISCHARGE
WICKS
LH wing, outer 100
LH wing, inner 100
RH wing, outer 100
RH wing, inner 100
Rudder 100
Horizontal stabilizer, LH 100
Horizontal stabilizer, RH 100
TIRES
Nose wheel 100
LH main wheel 100
RH main wheel 100
AIRCRAFT
DA 40 Series
AMM
Standard Practices and
Structures
Doc # 6.02.01
Rev. 5 51-80-00 Page 205
20 Sep 2007
D. Very Low Resistance Measurements (TAE version)
Item Attachment Point
max.
allowable
[mΩ]
measured
[mΩ]
passed
Engine propeller bearing, front 1.0
Heat exchanger case 1.0
Oil Cooler case 2.0
Water Cooler case 2.0
Intercooler case 2.0
External power connector outer large pin 1.5
Nose landing gear tube 10.0
Instrument panel above co-pilot's left knee 2.0
Engine breather tube 6.0
AIRCRAFT
Standard Practices and
Structures
DA 40 Series
AMM
Item Attachment Point
max.
allowable
[mΩ]
measured
[mΩ]
passed
Page 206
20 Sep 2007 51-80-00 Doc # 6.02.01
Rev. 5
FUEL SYSTEM
Fuel gascolator case 15.0
Fuel pump case 15.0
Fuel drain protector sheet metal 15.0
EXTERNAL CONDUCTIVE
PARTS
LH step 5.0
RH step 5.0
OAT sensor 5.0
LH landing gear lower bend, inner side 10.0
RH landing gear lower bend, inner side 10.0
Flap asymmetrical tube LH bond. strap connection 10.0
Flap asymmetrical tube RH bond. strap connection 10.0
ANTENNAS
Top COM antenna mounting screws 6.0
Bottom COM antenna mounting screws 6.0
AIRCRAFT
DA 40 Series
AMM
Standard Practices and
Structures
Item Attachment Point
max.
allowable
[mΩ]
measured
[mΩ]
passed
Doc # 6.02.01
Rev. 5 51-80-00 Page 207
20 Sep 2007
STABILIZER
Vertical lightning protection
tube
upper end 7.0
LH horizontal stabilizer
lightning strap
tip 15.0
RH horizontal stabilizer
lightning strap
tip 15.0
Grindspur aluminum strap 15.0
Rudder hinge rudder side 10.0
Vertical stabilizer fairing FWD LH side screw 12.0
Vertical stabilizer fairing FWD RH side screw 12.0
Horizontal stabilizer front bracket 10.0
Horizontal stabilizer rear bracket 10.0
LH WING
Fuel tank drain drain 5.0
Tank refill ring 5.0
Tank vent plate 10.0
Pitot tube base tube base 6.0
Landing/taxi light bracket (screws) 10.0
Tip light assembly base plate 8.0
Aileron pushrod attachment bracket, aileron 50.0
Flaps pushrod attachment bracket, flap 50.0
RH WING
Fuel tank drain drain 5.0
Tank refill ring 5.0
Tank vent plate 10.0
Tip light assembly base plate 8.0
Aileron push-rod attachment bracket, aileron 50.0
Flaps push-rod attachment bracket, flap 50.0
AIRCRAFT
Standard Practices and
Structures
DA 40 Series
AMM
Page 208
20 Sep 2007 51-80-00 Doc # 6.02.01
Rev. 5
E. Low Resistance Measurements in Control System (TAE version)
Item Attachment Point
max.
allowable
[mΩ]
measured
[mΩ]
passed
Pilot stick tube 50.0
Co-pilot stick tube 50.0
Trim wheel assembly frame 5.0
Levers frame 10.0
Pilot pedal assembly 150
Co-pilot pedal assembly 150
Canopy hinge RH tube tip 100
Canopy hinge RH tube tip 100
　
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本文鏈接地址：鉆石40系列AMM 2(125)