-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 27-26-17-400-001 Installation of the Yaw Damper Position Transducer Unit 2CC AMM 27-26-41-000-001 Removal of the Centering Spring Rod for the Actuator of the Yaw Damper Servo AMM 27-26-41-400-001 Installation of the Centering Spring Rod for the Actuator of the Yaw Damper Servo AMM 27-26-51-000-001 Removal of the Yaw Damper Servo Actuator (3CC1) and (3CC2) AMM 27-26-51-400-001 Installation of the Yaw Damper Servo Actuator (3CC1)
and (3CC2)
R AMM 53-59-00-210-001 Operational Check of Single Drain Pipe Aft of FR70
R from Outside 27-20-00-991-001 Fig. 201 27-20-00-991-002 Fig. 202 27-20-00-991-003 Fig. 203
3. Fault Confirmation
__________________
A. Test
(1) Do the operational test of the rudder artificial-feel loads (Ref. AMM TASK 27-23-00-710-001).
4. Fault Isolation
_______________
WARNING : MAKE SURE THAT THE FAC'S ARE ELECTRICALLY ISOLATED DURING WORK ON
_______
THE MECANICAL CONTROL SYSTEM OF THE RUDDER.
IF NOT, PARTS CAN MOVE AND CAUSE INJURY AND/OR DAMAGE.
A. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AUTO FLT/FAC1/28VDC 5CC1 B04 49VU AUTO FLT/FAC1/26VAC 14CC1 B03 121VU AUTO FLT/FAC2/28VDC 5CC2 M19 121VU AUTO FLT/FAC2/26VAC 14CC2 M18
B. If you find a hard spot:
- make sure that there is no water or ice in the lower area of the tail cone. if you find water or ice, remove it and check that the drain tube is not clogged (Ref. AMM TASK 53-59-00-210-001).
「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 202
Feb 01/05 CES
(1) If you find a hard spot:
- do a check of the pedals and cable linkage.
(Ref. Fig. 201/TASK 27-20-00-991-001) R - disconnect the lower point of the rod (3) between the cable R quadrant and the differential mechanism.
- move the rudder pedals.
(2) If you find a hard spot:
- disconnect the ajustable bellcrank rod (2)
- move the rudder pedals.
(a) If you do not find a hard spot:
- connect the rod (2) and see Para. (c)
(b) If you find a hard spot:
- disconnect the link rod (1) between the CAPT and F/O pedals
1 move the CAPT pedals:
_ a If you do not find a hard spot:
_ . do a check to find the mechanical part failure at the F/O pedals and do the corrective action (Ref. AMM TASK 27-21-42-000-002) and (Ref. AMM TASK 27-21-42-400-002).
b If you find a hard spot:
_ . do a check to find the mechanical part failure at the CAPT pedals and do the corrective action (Ref. AMM TASK 27-21-42-000-001) and (Ref. AMM TASK 27-21-42-400-001).
2 Connect the rod (3).
_
(c) If the fault continues:
- do a visual inspection of the tension regulator, rudder control cables and pulleys (5)
- make sure for each equipment that the cables are correctly installed in the pulley grooves and on the tension regulator. 中國(guó)航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 飛行操縱 1(29)
