INSTRUMENTS (AND AVIONICS) / INSTRUMENTS AND AVIONICS GENERAL MAINTENANCE 13-27
CHANGE C2 ICON A5 / MAINTENANCE MANUAL
Aircraft System and Number
10—Instruments (and Avionics)
Consumables
LOCTITE 222 (THREADLOCKER, ACRYLIC, REMOVABLE LOW STR, PURPLE)
NOTE: Retain removed hardware for re-installation.
This procedure requires a pitot-static-AOA leak test. (See “Pitot-Static-AOA Leak Test Procedures”
on page 13-70.)
1. Remove instrument cluster bezel. (See “Remove Instrument Cluster” on page 13-29.)
2. Remove a set of four #6-32 screws securing each gauge to mount.
NOTE: INDICATOR, ALTIMETER only has three screws.
3. Replace gauge and install four attachment screws. Apply a small amount of LOCTITE 222.
Torque to 6-10 in-lb.
4. Re-install instrument cluster into the aircraft. (See “Install Instrument Cluster” on page 13-31.)
VERIFICATION METHOD:
Task is complete when cluster hood shell is re-installed and the gauge has been replaced.
RELATED INFORMATION:
"Left Instrument Panel Top Panel Removal" on page 8-19
"Install Instrument Cluster" on page 13-31
"Remove Instrument Cluster" on page 13-29
"Pitot-Static-AOA Leak Test Procedures" on page 13-70
"Verify Altimeter Calibration" on page 13-83
13.3.5 Multiple Systems Controller (MSC) Replacement
Use the following procedure to replace the multiple systems controller (MSC).
TASK INFORMATION:
Type of Maintenance
Line
Level of Certification
LSA-RM
Task Specific Training Required
No
Special Tools Required