____
the rudder trim index.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-20-00∞∞∞∞∞∞∞∞∞∞Page 213
May 01/05R
CES Rudder Trim out of the Limits
1. Possible Causes_______________
- FAC-1 (1CC1)
- adjustment of the ailerons
- aileron servo controls and hinge bearings
- adjustment of the rudder neutral position
- rudder servo controls and hinge bearings
- adjustment of the spoilers
- spoilers servo controls and hinge bearings
- flap rigged position
2. Job Set-up Information______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 22-66-34-000-002 Removal of the FAC (1CC1,1CC2)
AMM 22-66-34-400-002 Installation of the FAC (1CC1,1CC2)
AMM 27-14-00-220-001 Check of the Aileron Servo Controls and Hinge Bearings for too much Play and Condition
AMM 27-14-00-820-001 Adjustment of the Aileron
AMM 27-24-00-200-001 Check of the Rudder Servo Controls and Hinge Bearings for too much Play and Condition
AMM 27-24-00-820-001 Adjustment of the Rudder Neutral Position
AMM 27-51-00-820-003 To Do a Check of the Flap Rigged Position (With the Sharks Fin)
AMM 27-51-00-820-006 Adjustment of the Flap Rigged Position (With the Rigging Boards)
AMM 27-64-00-200-001 Check of the Spoilers Servo Controls and Hinge Bearings for Excessive Play and Condition
AMM 27-64-00-820-001 Adjustment of the Spoilers
3. Fault Confirmation__________________
A. Test
Not applicable, you cannot confirm this fault on ground.
NOTE : The maximum admissible rudder trim limits indicated on the control
____ panel 110VU when the aircraft is stabilized in heading with the AP engaged are 1 deg RH and 2.3 deg LH.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-20-00∞∞∞∞∞∞∞∞∞∞Page 214
May 01/05R
CES
4. Fault Isolation
_______________
A. With the QAR or DMU or DAR or DFDR, record the rudder position when the aircraft is in the conditions below:
- normal cruise range,
- straight flight,
- AP engaged more than 10 mn in the HEADING mode,
- symmetrical, fuel in the wing tanks
- symmetrical, engine thrust.
NOTE : The recorded rudder position (PARAM ALPHA code: RUDD) must be the
____ average value of the rudder position during the above conditions.
(1) If the rudder position value is in the + or - 1.5. range in the L and R directions:
- do a check of the adjustment of the ailerons (Ref. AMM TASK 27-14-00-820-001).
(2) If the rudder position value is out of the + or - 1.5. range in the L and R directions:
- Do a check of the adjustment of the ailerons (Ref. AMM TASK 27-14-00-820-001).
- Do a check of the aileron servo controls and hinge bearings for too much play and condition (Ref. AMM TASK 27-14-00-220-001).
- Do a check of the adjustment of the rudder neutral position (Ref. AMM TASK 27-24-00-820-001).
- Do a check of the rudder servo controls and hinge bearings for too much play and condition (Ref. AMM TASK 27-24-00-200-001).
- Do a check of the adjustment of the spoilers (Ref. AMM TASK 27-64-00-820-001).
- Do a check of the spoilers servo controls and hinge bearings for too much play and condition (Ref. AMM TASK 27-64-00-200-001).
- Do a check of the flap rigged position (with the sharks fin (Ref. AMM TASK 27-51-00-820-003), or with the rigging boards (Ref. AMM TASK 27-51-00-820-006)).
- Replace the FAC-1 (1CC1) (Ref. AMM TASK 22-66-34-000-002) (Ref. AMM TASK 22-66-34-400-002)
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-20-00∞∞∞∞∞∞∞∞∞∞Page 215
May 01/05R
CES Results of the Operational Test of the Rudder Artificial - Feel Loads not
Satisfactory
1. Possible Causes
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本文链接地址：A320 Trouble Shooting Manual 排故手册 飞行操纵 1(33)
