Page 4-8
G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air
Revision 1
190-00716-01
Item Description/Procedure
Manual
Section No.
Interval
Engine/Airframe Sensors
ITT Thermocouple
Cable (Qty 2)
Removal & Replacement:
Refer to Super King Air 300 or B300
Maintenance Manual listed in Table 1-2.
N/A On
Condition
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)
Removal & Replacement
6.22
On Condition
Annunciator/Switch –
Prop Sync
6.23
Other Equipment
Standby Airspeed
Indicator
Removal & Replacement
6.26
On Condition
Static pressure system test according to
14 CFR 91.411 and Part 43 Appendix E.
N/A
24 Calendar Months
Standby Altimeter
Removal & Replacement
6.27
On Condition
Test according to 14 CFR 91.411 and
Part 43 Appendix E.
N/A
24 Calendar Months
Standby Attitude
Indicator
Removal & Replacement
6.28
On Condition
Standby Battery
Removal & Replacement
6.25
On Condition
Capacity test of standby battery.
4.16.2
12 Calendar Months
Standby Battery
Charge Check*
Verify the standby battery is being
charged.
4.16.1
Phase 1, 2, 3 & 4 or
6 Calendar Months
Standby Instrument
Electrical Power
Checks*
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)
8.1.5
Phase 1, 2, 3 & 4
Annunciator/Switch –
Standby Battery
Removal & Replacement
6.23
On Condition
*
Denotes Airworthiness Limitation Maintenance Requirement (See Section 4.1)
Summary of Contents for Cessna Caravan G1000
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