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时间:2011-03-28 13:42来源:蓝天飞行翻译 作者:航空
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AMM 27-21-00-210-002 Detailed Visual Inspection of the Rudder Mechanical Control Cables AMM 27-21-00-210-003 Detailed Visual Inspection of the Rudder Mechanical
 Control-Linkage in the Vertical Stabilizer AMM 27-21-00-710-001 Operational Test of the Centering Spring Rod AMM 27-21-00-820-002 Adjustment of the Rudder Control-Cables Length AMM 27-21-42-000-001 Removal of the CAPT Pedals AMM 27-21-42-000-002 Removal of the F/O Pedals AMM 27-21-42-400-001 Installation of the CAPT Pedals AMM 27-21-42-400-002 Installation of the F/O Pedals AMM 27-21-48-000-001 Removal of the Centering Rod of the Rudder Control AMM 27-21-48-400-001 Installation of the Centering Rod of the Rudder
 Control AMM 27-23-00-710-001 Operational Test of the Rudder Artificial-Feel Loads AMM 27-23-41-000-001 Removal of the Artificial Feel and Trim Unit AMM 27-23-41-400-001 Installation of the Artificial Feel and Trim Unit AMM 27-23-51-000-001 Removal of the Rudder Travel Limitation Unit 4CC
R AMM 27-23-51-400-001 Installation of the Rudder Travel-Limitation Unit 4CC AMM 27-26-17-000-001 Removal of the Yaw Damper Position Transducer Unit 2CC
 「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 201
 Aug 01/05 CES

 

 -------------------------------------------------------------------------------
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.
 
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