NOTE: This procedure is for reference only. The complete rigging procedure is written in AMM TASK 27-51-05-820-801.

1. Make sure Time and date is set correctly on the cockpit clocks.
2. Set the SLAT FLAP Control Lever to SLATS IN and FLAPS 0°.
3. Make sure the SLATS are IN and FLAPS at 0°.
4. Using the PMAT, access CAIMS and make the following selections:

   • Select SYSTEM DIAG
   • Select ATA 27
   • Select SLAT/FLAP CONTROL UNIT #1 (#2)
   • Select LRU TEST
   • Select SLATS RIGGING
   • Select CONFIRM
   • Highlight SLAT RIG ENABLE COMMAND and push SELECT
   • Highlight SLAT RIG COMMAND and push SELECT
   • Select TEST CMPLT
   • When SLATS rigging is complete select "FLAPS RIGGING"
   • Select CONFIRM
   • Highlight FLAP RIG ENABLE COMMAND and push SELECT
   • Highlight FLAP RIG COMMAND and push SELECT
   • Select TEST CMPLT

5. Disregard any CAS or CAIMS fault messages.
6. Once SLAT and FLAP rigging is performed, repeat step 4 to do a second SLATS and FLAPS rigging.
7. Disregard any CAS or CAIMS fault messages.
8. Remove complete power from the aircraft.
9. Apply power to the aircraft and perform a Slat Flap System operational test.
10. The SFCU should now be clear of latched faults and NVM memory should have recorded the new rigging data.