13-82 INSTRUMENTS (AND AVIONICS) / PITOT-STATIC-ANGLE OF ATTACK (AOA) SYSTEM
ICON A5 / MAINTENANCE MANUAL CHANGE C2
Parts Required
None
Aircraft System and Number
10—Instruments (and Avionics)
Consumables
None
1. Connect syringe to pitot port using flexible tubing pushed over the tip of the pitot tube.
2. Slowly apply pressure with the syringe until the airspeed indicator reads 100 knots. With 100
knots set, start timing while tapping glass of instrument.
3. Record the new airspeed reading result after one minute.
4. Remove test setup.
5. Adjust the altimeter baro setting until an even altitude is displayed.
6. Seal one instrument static port with tape.
7. Secure syringe to open static port with ITW Tacky Tape. Slowly apply suction (this will add
suction to both the static and pitot sides at the same time) until a 1,000 ft increase in indicated
altitude is displayed.
8. With the new altitude set, begin timing while tapping glass of instrument. After one minute, note
the displayed altitude and record the results.
RESULT:
Date of Test:
Initials of Technician:
Airspeed Reading at Time 0 sec:
Airspeed Reading at Time 60 sec:
Altitude Reading at Time 0 sec:
To Next Page
Loading...
