Garmin G1000 System Maintenance Manual page 121

Item
ITT Thermocouple
Cable (Qty 2)
Oil Pressure Sensor
(Qty 2)
Oil Temperature
Sensor (Qty 2)
Torque Transmitter
(Qty 2)
Fuel Flow Transmitter
(Qty 2)
Prop Tachometer
(Qty 2)
Engine Speed
Tachometer (Qty 2)
Signal Conditioners
(Qty 2)
Annunciator/Switch –
Prop Sync
Standby Airspeed
Indicator
Standby Altimeter
Standby Attitude
Indicator
Standby Battery
Standby Battery
Charge Check*
Standby Instrument
Electrical Power
Checks*
Annunciator/Switch –
Standby Battery
* Denotes Airworthiness Limitation Maintenance Requirement (See Section 4.1)
G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air
190-00716-01
Description/Procedure
Engine/Airframe Sensors
Removal & Replacement:
Refer to Super King Air 300 or B300
Maintenance Manual listed in Table 1-2.
Removal & Replacement
Other Equipment
Removal & Replacement
Static pressure system test according to
14 CFR 91.411 and Part 43 Appendix E.
Removal & Replacement
Test according to 14 CFR 91.411 and
Part 43 Appendix E.
Removal & Replacement
Removal & Replacement
Capacity test of standby battery.
Verify the standby battery is being
charged.
Verify STBY ATT & STBY ALT vibrator
operate and STBY ATT, STBY ALT &
STBY A/S illumination function on
aircraft power and standby battery power
(standby compass checked during
existing maintenance)
Removal & Replacement
Manual
Interval
Section No.
N/A On Condition
6.22
On Condition
6.23
6.26 On Condition
N/A 24 Calendar Months
6.27 On Condition
N/A 24 Calendar Months
6.28 On Condition
6.25 On Condition
4.16.2 12 Calendar Months
220 hours max or
4.16.1
6 Calendar Months,
whichever occurs first
8.1.5 220 hours max
6.23 On Condition
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Revision 4