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Seitenansicht 96
G1000 System Maintenance Manual – Diamond DA40/40F Page 4-5
190-00545-01 Revision G
Table 4-1. Maintenance Intervals, Cont.
G1000 Accessories
Item Description/Procedure
Manual
Section No.
Interval
Configuration Module
Replacement (Qty 4)
Removal & Replacement. 6.12
On Condition
GEA 71 Backshell
Thermocouple
Removal & Replacement. 6.13
OAT Probe Removal & Replacement. 6.6
PFD, MFD, & GIA
Cooling Fans (Qty 3)
Removal & Replacement; Refer to
G1000/DA40 Installation Drawing,
005-00304-00.
N/A
Cooling Fan Function and Fan Failure
Annunciation Test.
4.13
250 Hours or
Aircraft Annual
GFC 700 AFCS
GFC 700 AFCS
System
Complete Visual Inspection 4.4 Aircraft Annual
GSA 81 Servos (all)
Removal & Replacement. Refer to the
servo install drawings listed in Table 1-3.
6.10 On Condition
Clean and Apply Grease to Output Gears. 4.8
1000 Hours or 36
Months
GSM 85 Servo
Mounts (all)
Removal & Replacement. Refer to the
servo install drawings listed in Table 1-3.
6.11 On Condition
Check Slip Clutch Torque 4.10.1
500 Hours or 12
Months
GSM 86 Servo
Mounts (all)
Removal & Replacement. Refer to the
servo install drawings listed in Table 1-2
6.11 On Condition
GSM 86 Servo Gear
Box Slip Clutch
Torque Check
Conduct an manual overpower of the servo
to ensure it is not mechanically jammed
4.10.4 Aircraft Annual
For installations with the GSM 86 servo
gearbox, verify that the pitch, roll and
pitch trim GSM 86 slip clutch torque
values are within acceptable limits.
4.10.2
1200 Hours or 36
Months
GFC 700 AFCS
System
Perform a check to verify that flap-in-
motion discrete inputs function correctly.
4.9
100 Hours or
Aircraft Annual
Pitch Trim Control
Chain
Removal & Replacement; Refer to the pitch
trim installation drawing listed in Table 1-2
and or Table 1-3.
N/A On Condition
Pitch & Roll Control
Cable/Phenolic
Isolator Assemblies
and Clamps
Removal & Replacement; Refer to the pitch
and roll servo installation drawings listed in
Table 1-2 or Table 1-3.
N/A On Condition
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