ICON A5 - Page 452

13-32 INSTRUMENTS (AND AVIONICS) / INSTRUMENTS AND AVIONICS GENERAL MAINTENANCE
ICON A5 / MAINTENANCE MANUAL CHANGE C2
CHAPTER 13
None
Aircraft System and Number
10—Instruments (and Avionics)
Consumables
LOCTITE 222 (THREADLOCKER, ACRYLIC, REMOVALBLE LOW STR, PURPLE)
A pitot-static-AOA leak test is required. See “Pitot-Static-AOA Leak Test Procedures” on page 13-70.
TASK INSTRUCTIONS:
1. Install cluster bezel with 10 #6-32 mounting panel attachment screws. Apply a small amount of
LOCTITE 222. Torque to 6-10 in-lb. See Figure 13-4.
2. Position instrument cluster into aircraft crossbeam rib. Reconnect all electrical connections while
holding instrument cluster in place.
NOTE: Do not damage pitot-static tubes.
3. Secure instrument cluster to aircraft crossbeam rib with four #8-32 attachment screws. Apply
small amount of LOCTITE 222. See Figure 13-3.
4. Attach static tube to the altimeter.
5. Attach static and pitot tubes to airspeed indicator.
6. Perform pitot-static-AOA leak test. (See “Pitot-Static-AOA Leak Test Procedures” on page
13-70.)
7. Re-install hood shell. Slide it forward into the clip hole and then press it down on the instrument
cluster.
VERIFICATION METHOD:
Performing the pitot-static-AOA leak test operates as the verification method for this task.
RELATED INFORMATION:
"Remove Instrument Cluster" on page 13-29
"Replace Instrument Panel Gauge" on page 13-26
"Replace Annunciator Panel" on page 13-39
13.3.8 Access Center Stack Instruments and Switches
This section contains instructions to remove and install Center Stack instrument wire connections.
TASK INFORMATION:
Type of Maintenance
Line
Level of Certification