F/CTRL SLATS FAULT A320
SLAT/FLAP CONTROL COMPUTER 1/2 (SFCC)
— RESET PROCEDURE—
Pull & reset
SFCC 1: SLATS B06 FLAPS B07
SFCC 2: SLATS R21 FLAPS Q21
Pull CBs for: 1 sec
POST: 65 sec
AMM TEST: 27-84-00-710-001-A — Operational Test of the Slat System A320
TSM: 27-81-00-810-811-A — SLAT SYSTEM 1 (2) FAULT A320
MEL STATUS: 27-81-01








