DOC AIRBUS | AMM A320FTHS POSITION INDICATING - DESCRIPTION AND OPERATION
** ON A/C NOT FOR ALL
1. General
On the center pedestal, adjacent to each pitch-trim control wheel, the Trimmable Horizontal Stabilizer (THS) position is indicated by an index on a scale painted green over the normal takeoff range (2.5 deg. aircraft NOSE DN to 2.5 deg. aircraft NOSE UP).
On the lower Electronic Centralized Aircraft Monitoring (ECAM) display unit, the same THS position (together with the hydraulic systems still available for the actuator) is shown through the Flight Control Data Concentrator (FCDC) (Ref. 27-95).
There is a special reference mark painted on the THS and on the adjacent structure.
On the center pedestal, adjacent to each pitch-trim control wheel, the Trimmable Horizontal Stabilizer (THS) position is indicated by an index on a scale painted green over the normal takeoff range (3.5 deg. aircraft NOSE DN to 4.5 deg. aircraft NOSE UP).
On the lower Electronic Centralized Aircraft Monitoring (ECAM) display unit, the same THS position (together with the hydraulic systems still available for the actuator) is shown through the Flight Control Data Concentrator (FCDC) (Ref. 27-95).
There is a special reference mark painted on the THS and on the adjacent structure.
On the center pedestal, adjacent to each pitch-trim control wheel, the Trimmable Horizontal Stabilizer (THS) position is indicated by an index on a scale painted green over the normal takeoff range (3 deg. aircraft NOSE DN to 3.5 deg. aircraft NOSE UP).
On the lower Electronic Centralized Aircraft Monitoring (ECAM) display unit, the same THS position (together with the hydraulic systems still available for the actuator) is shown through the Flight Control Data Concentrator (FCDC) (Ref. 27-95).
There is a special reference mark painted on the THS and on the adjacent structure.
On the center pedestal, adjacent to each pitch-trim control wheel, the Trimmable Horizontal Stabilizer (THS) position is indicated by an index on a scale painted green over the normal takeoff range (2.5 deg. aircraft NOSE DN to 3.8 deg. aircraft NOSE UP).
On the lower Electronic Centralized Aircraft Monitoring (ECAM) display unit, the same THS position (together with the hydraulic systems still available for the actuator) is shown through the Flight Control Data Concentrator (FCDC) (Ref. 27-95).
There is a special reference mark painted on the THS and the adjacent structure.
On the center pedestal, adjacent to each pitch-trim control wheel, the Trimmable Horizontal Stabilizer (THS) position is indicated by an index on a scale painted green over the normal takeoff range (2.5 deg. aircraft NOSE DN to 2.5 deg. aircraft NOSE UP).
Center Pedestal - THS Position IndicatingOn the lower Electronic Centralized Aircraft Monitoring (ECAM) display unit, the same THS position (together with the hydraulic systems still available for the actuator) is shown through the Flight Control Data Concentrator (FCDC) (Ref. 27-95).
There is a special reference mark painted on the THS and on the adjacent structure.
On the center pedestal, adjacent to each pitch-trim control wheel, the Trimmable Horizontal Stabilizer (THS) position is indicated by an index on a scale painted green over the normal takeoff range (3.5 deg. aircraft NOSE DN to 4.5 deg. aircraft NOSE UP).
On the lower Electronic Centralized Aircraft Monitoring (ECAM) display unit, the same THS position (together with the hydraulic systems still available for the actuator) is shown through the Flight Control Data Concentrator (FCDC) (Ref. 27-95).
There is a special reference mark painted on the THS and on the adjacent structure.
On the center pedestal, adjacent to each pitch-trim control wheel, the Trimmable Horizontal Stabilizer (THS) position is indicated by an index on a scale painted green over the normal takeoff range (3 deg. aircraft NOSE DN to 3.5 deg. aircraft NOSE UP).
On the lower Electronic Centralized Aircraft Monitoring (ECAM) display unit, the same THS position (together with the hydraulic systems still available for the actuator) is shown through the Flight Control Data Concentrator (FCDC) (Ref. 27-95).
There is a special reference mark painted on the THS and on the adjacent structure.
On the center pedestal, adjacent to each pitch-trim control wheel, the Trimmable Horizontal Stabilizer (THS) position is indicated by an index on a scale painted green over the normal takeoff range (2.5 deg. aircraft NOSE DN to 3.8 deg. aircraft NOSE UP).
On the lower Electronic Centralized Aircraft Monitoring (ECAM) display unit, the same THS position (together with the hydraulic systems still available for the actuator) is shown through the Flight Control Data Concentrator (FCDC) (Ref. 27-95).
There is a special reference mark painted on the THS and the adjacent structure.