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时间:2011-03-28 09:19来源:蓝天飞行翻译 作者:航空
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 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ Loss of the Reception of the FADEC 218 ALL 1 Bus by One FMGC Loss of the Reception of the FADEC 220 ALL 2 Bus by One FMGC Loss of the A/THR Pushbutton 222 ALL Switch Function on the FMGC 1 Loss of the A/THR Pushbutton 223 ALL Switch Function on the FMGC 2 Unwanted A/THR 1 and 2 Inoperative 224 ALL Warning Disagree between the A/THR ENGD 225 ALL Discretes (FMGC1 and FMGC2) Disagree between the A/THR ENGD 228 ALL Discretes (FMGC1 and FMGC2) FMGC Malfunction 230 005-049, 051-052
 054-061, 102-104
 ARTIFICIAL FEEL AND RUDDER TRAVEL 22-61-00 LIMITING COMPUTATION
 FAULT ISOLATION PROCEDURES 201 ALL
 Loss of the Reception of the RTL 201 ALL
 ENGD Discrete Feedback by the FAC
 1
 Loss of the Reception of the RTL 203 ALL
 ENGD Discrete Feedback by the FAC
 2
 Loss of the Rudder Travel Limiting 205 ALL
 Function on the FAC 1
 Loss of the Rudder Travel Limiting 209 ALL
 Function on the FAC 2
 Loss of the Power Supply 26VAC of 213 ALL
 the Rudder Travel Limiting Side 1
 Loss of the Power Supply 26VAC of 215 ALL
 the Rudder Travel Limiting Side 2
 Loss of Power Supply 26VAC of the 217 ALL
 Position Feedback Transducers Side
 1
 Loss of Power Supply 26VAC of the 220 ALL
 Position Feedback Transducers Side
 2

 RUDDER TRIM COMPUTATION 22-62-00
 FAULT ISOLATION PROCEDURES 201 ALL
 Failure of the Circuit of the 201 ALL
 Rudder Trim-Control Switch of the
 FAC 1

 22-CONTENTS Page 3 May 01/05 R CES


 AUTO FLIGHT
 TABLE OF CONTENTS
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 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ Failure of the Circuit of the 203 ALL Rudder Trim-Control Switch of the FAC 2 Rudder Trim-Control Switch 205 ALL Inoperative in One Direction with the FAC 1 Rudder Trim-Control Switch 206 ALL Inoperative in the Two Directions with the FAC 1 Rudder Trim-Control Switch 207 ALL Inoperative in One Direction with the FAC 2 Rudder Trim-Control Switch 208 ALL Inoperative in the Two Directions with the FAC 2 Loss of the Reception of the RT 209 ALL ENGD Feedback Discrete by the FAC 1 Loss of the Reception of the RT 211 ALL ENGD Feedback Discrete by the FAC 2 Loss of the Rudder Trim Function 213 ALL on the FAC 1 Loss of the Rudder Trim Function 217 ALL on the FAC 2 Loss of the Power Supply 26VAC of 221 ALL the Rudder Trim Side 1 Loss of the Power Supply 26VAC of 223 ALL the Rudder Trim Side 2 Failure of the Rudder Trim/Reset 225 ALL Circuit of the FAC 1 Failure of the Rudder Trim/Reset 227 ALL Circuit of the FAC 2 RUD TRIM/RESET Pushbutton Switch 229 ALL Inoperative on the FAC 1 RUD TRIM/RESET Pushbutton Switch 230 ALL Inoperative on the FAC 2 Failure of the Rudder Trim 231 ALL Indicator Rudder Trim Indicator Inoperative 233 ALL Reset of the Rudder Trim 234 ALL Inoperative FAC 1 RT Function Inoperative 236 ALL FAC 2 RT Function Inoperative 237 ALL
 YAW DAMPER COMPUTATION 22-63-00
 22-CONTENTS Page 4 May 01/05 R CES


 AUTO FLIGHT
 TABLE OF CONTENTS
_________________
 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________
 FAULT ISOLATION PROCEDURES 201 ALL Loss of the Yaw Damper Function on 201 ALL the FAC 1 Loss of the Yaw Damper Function on 205 ALL the FAC 2 Loss of the Reception of the YD 209 ALL ENGD Feedback Discrete by the FAC 1 Loss of the Reception of the YD 211 ALL ENGD Feedback Discrete by the FAC 2 Loss of the Signal from the 213 ALL Yaw-Damper Position Transducer-Unit (2CC) to the FAC 1 Loss of the Signal from the 216 ALL Yaw-Damper Position Transducer-Unit (2CC) to the FAC 2 Loss of the Power Supply 26VAC of 219 ALL the Yaw Damper Side 1 Loss of the Power Supply 26VAC of 220 ALL the Yaw Damper Side 2 FAC 1 YD Function Inoperative 221 ALL FAC 2 YD Function Inoperative 222 ALL Loss of the Reception of the HYD 223 ALL CIRC PRESS SW Discrete by the FAC 1 Loss of the Reception of the HYD 225 ALL CIRC PRESS SW Discrete by the FAC 2 Loss of the Yaw Damper Function 227 ALL
 FLIGHT AUGMENTATION COMPUTER (FAC) 22-66-00
 FAULT ISOLATION PROCEDURES 201 ALL Failure of the FAC 1 201 ALL Failure of the FAC 2 204 ALL Loss of the FAC 1 GENERAL Bus 207 ALL Loss of the FAC 2 GENERAL Bus 208 ALL Loss of the FAC 1 Bus Feedback 209 ALL Loss of the FAC 2 Bus Feedback 210 ALL Loss of the FAC 1 HLTY MON OWN 211 ALL Discrete Signal Loss of the FAC 1 HLTY MON OPP 212 ALL Discrete Signal Loss of the FAC 2 HLTY MON OPP 213 ALL Discrete Signal Loss of the FAC 2 HLTY MON OWN 214 ALL
 22-CONTENTS Page 5 May 01/05 R CES


 AUTO FLIGHT
 TABLE OF CONTENTS
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 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
 
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