-------------------------------------------------------------------------------FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA | | | | DOOR | REF. -------------------------------------------------------------------------------
3FP1 SENSOR-ANGLE OF ATTACK, 1 127 824 34-11-19
3FP2 SENSOR-ANGLE OF ATTACK, 2 128 824 34-11-19
3FP3 SENSOR-ANGLE OF ATTACK, 3 127 824 34-11-19
11FP1 SENSOR-TAT, 1 121 34-11-18
11FP2 SENSOR-TAT, 2 122 34-11-18
9DA1 PROBE-PITOT, 1 125 812 34-11-15
9DA2 PROBE-PITOT, 2 126 822 34-11-15
9DA3 PROBE-PITOT, 3 125 812 34-11-15
7DA1 PROBE-L STATIC, 1 127 824 34-11-16
7DA2 PROBE-L STATIC, 2 127 824 34-11-16
7DA3 PROBE-L STATIC, 3 121 811 34-11-16
8DA1 PROBE-R STATIC, 1 128 824 34-11-16
8DA2 PROBE-R STATIC, 2 128 824 34-11-16
8DA3 PROBE-R STATIC, 3 122 811 34-11-16
19FP1 ADM-L TOTAL PRESSURE NONE 125 812 34-11-17
19FP2 ADM-R TOTAL PRESSURE 126 822 34-11-17
19FP3 ADM-STBY TOTAL PRESSURE 125 812 34-11-17
19FP4 ADM-R STATIC PRESSURE 128 824 34-11-17
19FP5 ADM-L STATIC PRESSURE 127 824 34-11-17
19FP6 ADM-R STATIC PRESSURE 128 824 34-11-17
19FP7 ADM-L STATIC PRESSURE 127 824 34-11-17
19FP8 ADM-STBY STATIC PRESSURE 121 811 34-11-17
R 1EFF : 001-049, 101-105, 151-199, 201-203, 1 34-18-00Page 4
1 1 Config-1 May 01/05 1 1 1CES 1
3. System Description
__________________
A. Reporting Function Each ADIRS BITE message is described in the following pages, with the corresponding fault description and the consequences on the system and in the cockpit.
(1) General
-IR faults are classified as follows:
. class 1 faults
. class 2 faults
. class 3 faults.
-ADR faults:
. class 1 faults
. class 2 faults
. class 3 faults.
-Common faults (IR + ADR)
. class 1 faults
. class 2 faults
. class 3 faults.
NOTE : Bit 13 of ADR label 270 indicates an ADR fault (bit 13 = 1)
____
-use of i, j, k indexes in BITE messages: . barring explicit restriction, ADIRUi stands for ADIRU 1, ADIRU 2 or ADIRU 3
. ADMi, ADMj, or ADMk: i, j, and k values are specified below the message.
-ECAM messages: . xxx stands for CAPT or F/O, depending on the ADIRU side (1 or 2)
. the letter in parentheses indicates the color used to display the text: (A) Amber, (C) Cyan and (W) White.
(2) Inertial reference faults
-Class 1 External Faults
(Ref. Fig. 002, 003)
-Class 1 Internal Faults
(Ref. Fig. 004, 005, 006, 007, 008, 009)
-Class 2 External Faults
R **ON A/C 001-049, 101-105, 151-199, 201-203,
Post SB 34-1147 For A/C 001-004,
(Ref. Fig. 010)
R 1EFF : 001-049, 101-105, 151-199, 201-203, 1 34-18-00Page 5 1 1 Config-1 May 01/05 1 1 1CES 1
ADIRS BITE - IR System - Class 1 External Faults 1/2
Figure 002
R 1EFF : 001-049, 101-105, 151-199, 201-203, 1 34-18-00Page 6 1 1 Config-1 May 01/05 1 1 1CES 1
ADIRS BITE - IR System - Class 1 External Faults 2/2
Figure 003
R 1EFF : 001-049, 101-105, 151-199, 201-203, 1 34-18-00Page 7 1 1 Config-1 May 01/05 1 1 1CES 1
ADIRS BITE - IR System - Class 1 Internal Faults 1/6
Figure 004
R 1EFF : 001-049, 101-105, 151-199, 201-203, 1 34-18-00Page 8 1 1 Config-1 May 01/05 1 1 1CES 1
ADIRS BITE - IR System - Class 1 Internal Faults 2/6
Figure 005
R 1EFF : 001-049, 101-105, 151-199, 201-203, 1 34-18-00Page 9 1 1 Config-1 May 01/05 1 1 1CES 1
ADIRS BITE - IR System - Class 1 Internal Faults 3/6
Figure 006
R 1EFF : 001-049, 101-105, 151-199, 201-203, 1 34-18-00Page 10 1 1 Config-1 May 01/05 1 1 1CES 1
ADIRS BITE - IR System - Class 1 Internal Faults 4/6
Figure 007
R 1EFF : 001-049, 101-105, 151-199, 201-203, 1 34-18-00Page 11 1 1 Config-1 May 01/05 1 1 1CES 1 中國航空網 m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM NAVIGATION 導航2(82)
