[A320] 最新整理A321航线快速排故放行手册

A321 航线快速排故放行手册
（仅供参考）

目 录


第一章 A320驾驶舱及主要计算机布局图........................................................ 1
1.1驾驶舱布局图...............................................................................................1
1.1.1 驾驶舱总图................................................................................................. .......................... 1
1.1.2 头顶面板A、G、H图.......................................................................................................... 2
1.1.3 飞行控制面板区域图E......................................................................................................... 3
1.1.4 中央操作台B、D图............................................................................................................. 4
1.1.6 维护面板F图.........................................................................................................................5
1.2.跳开关详解图.............................................................................................................................5
71.2.1 头顶跳开关面板49VU ........................................................................................................ 5
U1.2.2 121VU.............................................................................................................. ........ ...... 6
U1.2.3 122VU...................................................................................................................................7
1.2.4 123VU第三观察员座椅后方跳开关面板..........................................................................8
1.3. 主要计算机位置图................................................................................................................. 9
1.3.1 主电子舱内主要计算机位置..............................................................................................9
1.3.1.1 惯导位置图..............................................................................................................10
1.3.2 前电子舱内主要计算机位置.............................................................................................11
1.3.2.1 雷达收发组位置......................................................................................................12
1.3.2.2 风挡及皮托管加温计算机位置图..........................................................................13
1.4 A320 飞机计算机常用跳开关位置及复位方法...................................................................14
1.4.1 ATA 21-24.............................................................................................................................14
1.4.2 ATA 26-32 ...........................................................................................................................15
1.4.3 ATA 34-77 ...........................................................................................................................16
第二章航线常用程序及放行标准............................................................................17
2.1 液压渗漏检查程序..................................................................................................................17
2.2 发动机渗漏检查程序.............................................................................................................20
发动机余油口漏油标准...............................................................................................................21
2.3 空速和高度误差检查表.........................................................................................................22
2.4 轮胎损伤检查及更换标准.....................................................................................................23
2.4.1 割伤定义..............................................................................................................................23
2.4.2 损伤类型.............................................................................................................................27
2.5 机组氧气放行标准.................................................................................................................28
2.6 雷达罩损伤检查程序...............................................................................................................33
2.7 发动机吸入外物或遭鸟击后的检查程序..............................................................................35
2.8 飞机与发动机结构损伤检查程序及部分部件查找索引......................................................37
2.9 发动机EGT超温后检查程序（未发生失速或喘振） ...........................................................38
第三章快速排故指引................................................................................................38
AVNCS SYS FAULT ...................................................................................................................38.
VENT BLOWER FAULT或VENT EXTRACT FAULT .............................................................38
A/ THR OFF或者无法计算飞行数据.........................................................................................39.
BCL 1(2) FAULT/ TR 1(2) FAULT/ DC ESS BUS FAULT/ BAT 1(2)FAULT/ AC BUS 1(2)FAULT
AIL SERVO FAULT副翼伺服故障............................................................................................40
ALTN LAW备用法则或DIRECT LAW直接法则........................................................................40
ELEV SERVO FAULT 升降舵伺服故障.....................................................................................41
FLAP/SLAT SYS 1/2 FAULT 1/2 号襟/缝翼系统故障...............................................................41
RESET FLAP TIP BRK 襟翼翼尖刹车复位................................................................................42
机组反映左翼（右翼）内燃油箱油量指示不准确.......................................................................42
B ELEC PUMP LO PR蓝系统电动泵压力低...............................................................................43
G/H/B RSVR LO AIR PR绿/黄/蓝液压油箱空气压力低...........................................................43
ENG 1/2 PUMP LO PR 1/2 号发动机驱动泵压力低.................................................................44
L+RWINDSHIELD .......................................................................................................................44
风挡雨刮失效................................................................................................................................45
ADR FAULT大气数据基准故障..................................................................................................45
IR FAULT惯性基准故障..............................................................................................................45
OVER SPEED 超速......................................................................................................................46
TCAS FAULT ..............................................................................................................................46
ENG1(2) BLEED ABNORM PR ENG1(2) BLEED FAULT ......................................................47
L(R) WING LEAK不放行...........................................................................................................47
ENG1(2) BLEED LEAK ..............................................................................................................48
ENG SENSOR FAULT ................................................................................................................48
ENG OVSPD PROT FAULT .......................................................................................................49
EPR MODE FAULT.......................................................................................................................49
COMPRESSOR VANE.................................................. ......................................................... 50
AIR EXCHANGER FAULT .........................................................................................................50
BEARING 4 OIL SYS .................................................................................................................50
EGT EXCEEDED DURING AIR START....................................................................................51

第一章 A320 驾驶舱及主要计算机布局图
1.1 驾驶舱布局图
1.1.1 驾驶舱总图
.............................................................................................
EGT EXCEEDED DURING AIR START

需要了解的相关参数	EGT 变化趋势以及最大值（CFDS 中31 章查看EIS 超限记录）、FF、引气压力、超温时间、N1 和N2 值及变化状况，启动模式
ATA章节	77	可复位相关的C/B
故障补充描述	需结合参数判断是指示故障还是真实超温
建议处理流程
1、阅读 PFR 报告有无相关信息 2、阅读 FADEC 的排故数据，初步判断故障原因，结合航线常用检查程序中的发动机EGT 超限图决定是否可以立即重启发动机。 注：只启动一台发动机时可能没有此数据 3、自动启动模式下 N2 小于50%时有保护，可尝试重启发动机 4、建议机组用人工方式启动发动机，冷转时间控制在 2 分钟内尽可能长