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G1000/GFC 700 Post Installation Checkout Procedure - Hawker / Beechcraft King Air C90
Revision 5
190-00682-00
3.12
Pitot Static System Leak Checks
With a pitot-static test set connected to the aircraft perform a leak test of the aircraft static plumbing at an
altitude of 30,000 ft and airspeed of 120 knots. When static pressure has stabilized, verify and record the
cumulative leak rate is 200ft/minute or less.
ALTITUDE ft/min:
With a pitot-static test set connected to the aircraft perform a leak test of the aircraft pitot plumbing at an
altitude of 30,000 ft and airspeed of 226
knots. When pitot pressure has stabilized, verify and record the
cumulative leak rate is 1 knot/minute or less.
AIRSPEED kts/min:
