DOC AIRBUS | FIN A320FFIN: (92CV) RELAY-SLAT 2 FAULT
AMM TASK
- FLAPS ELECTRICAL CONTROL AND MONITORING
-
27-51-00-040-001-A
Deactivation of the Slat and Flap Control Computer (SFCC) No. 2 Flap Channel -
27-51-00-440-001-A
Reactivation of the Slat and Flap Control Computer (SFCC) No. 2 Flap Channel -
27-51-00-040-005-A
Deactivation of the Slat and Flap Control Computer (SFCC) No. 2 Slat Channel -
27-51-00-440-005-A
Reactivation of the Slat and Flap Control Computer (SFCC) No. 2 Slat Channel -
27-51-00-040-004-A
Flap WTB Solenoid - WTB Test Procedure -
27-51-00-710-001-A
Operational Test of the Wing Tip Brake and the Pressure Off Brake -
27-51-00-740-001-A
Read-out of Class 3 Faults in the Flap System -
27-51-00-740-002-A
BITE Test of the Slat and Flap Control Computers (Flap System) -
27-51-00-820-001-A
Manual Adjustment of the Position Pick-Off Units -
27-51-00-710-002-A
Operational Test of the Flap Interconnecting Strut and the Flap-Attachment Failure-Detection Sensors -
27-51-00-750-001-A
Automatic Integrity Test of the Slat and Flap Control Computers -
27-51-00-820-003-A
To do a Check of the Flap Rigged Position (with the Sharks Fin) -
27-51-00-820-004-A
Adjustment of the Forward Eccentrics (Tracks 3 and 4) -
27-51-00-820-008-A
Adjustment (Rigging) of the Flaps with the Sharks Fin Tool (A318/319/320) -
27-51-00-820-009-A
Adjustment (Rigging) of the Flaps with the Sharks Fin Tool (A321) -
27-51-00-820-010-A
Adjustment of the Flap Rollers
-
27-51-00-040-001-A