INSTRUMENTS (AND AVIONICS) / PITOT-STATIC-ANGLE OF ATTACK (AOA) SYSTEM 13-83
CHANGE C2 ICON A5 / MAINTENANCE MANUAL
Altitude Reading at Time 60 sec:
FAR Part 23.1325 states that the static system may not leak more than 100 ft in one minute after
starting at 1,000 ft above ambient pressure. The ICON flight test standard is 50 ft for the altimeter test
and 5 knots for the airspeed test as conducted above.
VERIFICATION METHOD:
If the system is outside of ICON limits, then there is a leak in the pitot-static system and the full system
must be inspected and all leaks repaired.
RELATED INFORMATION:
"Multiple Systems Controller (MSC) Replacement" on page 13-27
"Pitot-Static-AOA Leak Test Procedures" on page 13-70
13.8.2 Maintenance Instructions
13.8.2.1 Verify Altimeter Calibration
This section contains instructions to calibrate the altimeter for regular inspections.
TASK INFORMATION:
Type of Maintenance
Line
Level of Certification
LSA-RM
Task Specific Training Required
No
Special Tools Required
None
Parts Required
None
Aircraft System and Number
10—Instruments (and Avionics)
Consumables
None
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