F/CTRL FLAPS 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: 27-54-00-710-001-A — Operational Test of the Flap System A320
TSM: 27-51-00-810-814-A — FLAP SYSTEM 1 (2) FAULT A320
MEL STATUS: 27-51-01








