A320系列-短停维护工作单

地点 Station:日期 Date:

20__年(Y)__月(M)__日(D)

航班号

Flight

No.：

审核

REVIEWED BY

项次

ITEM

工作者

MECH

检查者

EXAMINER

工作内容

JOB DESCRIPTION

批准

APPROVED BY

机 外 项 目 OUTSIDE ITEM

按照《短停绕机检查路线图》，绕飞机一周，完成以下检查。

注：必须按规定路线绕飞机一周，对飞机进行全面检查。路线中的数字与工作单

中的步骤顺序一致，目的是提醒检查者在该处检查的重点。飞机外表蒙皮及飞机

上的漏水孔，工作单虽未提及，检查者仍应注意蒙皮是否有明显损坏，漏水孔是

否有不正常的液体漏出，部件无松动或丢失。确信各系统的进出口无堵塞，过压

释放圆盘无丢失。

According to Walk-around check route showed on page 7, complete

inspections as below.

NOTE:refer to Walk-around check route,walk around the aircraft and

complete all inspections for aircraft.The number showed on the check

route is corresponding to the step on the job card, reminding the

maintenance crew the key points of the step. The maintenance crew are

required to check the skin for no obvious damage, drain holes for no

leakage, parts for no missing and not loose nevertheless these items

are not on the job card. All system air inlets and outlets must not

be blocked. Crew oxygen cylinder overpressure relief indicator disc

must be present.

A319/A320/A321飞机短停维护工作单

A319/A320/A321 Aircraft Transit Job Card

机号A/C REG :

B-

工时Man Hour:

1.0_MH

负责人

Responsible

person:

①、 检查前起落架状态应正常：

Inspect and make sure that nose landing gear for normal.

(a)检查缓冲支柱的镜面高度应正常；

Inspect the dimension "H" for the shock absorber for normal.

(b)前起落架、前叉组件、锁撑组件及其附属部件的结构无损伤、渗漏；

Inspect and make sure that nose landing gear，Drag Strut

assembly,Lockstay assembly and the structure of the

accessories are not found with damage and leakage.

(c)机轮状态完好，无轮缘损伤,检查轮胎磨损情况在规定范围内；

Inspect wheels for normal,there are no signs of flange

damage and the wear of tires are in the specified limits.

(d)机轮轮毂内外半轮连接螺栓无剪断或脱落（如可见）；

Inspect and make sure that there are no stripped or

crushed threads for the attachment bolts between inner

half?wheel assembly and outer half?wheel assembly（If visible）.

(e)轮胎压力无明显不足。

Inspect and make sure that there are no obvious insufficient

pressure on the tires.

编写

PREPARED BY

1

M

AV

项次ITEM

工作者

MECH

检查者

EXAMINER 工作内容

JOB DESCRIPTION

1 M AV ②、检查右主起落架状态应正常：

Inspect and make sure that RH main landing gear is normal.

(a)刹车装置状态良好,如果刹车系统超温（机组报告、ECAM显示或AIDS有

刹车超温报告）,完成相应检查；

Inspect and make sure that brake assemblies status are

normal,if overtemperature occur on the brake system

(Crew report,ECAM display or Brake overtemperature-report

of AIDS),perform the related inspection.

(b)检查缓冲支柱的镜面高度应正常；

Inspect the dimension "H" for the shock absorber for normal.

(c)右主起落架、侧撑杆组件、锁撑组件及其附属部件的结构无损伤、渗漏； Inspect and make sure that RH main landing gear，Side-Stay

assembly and Lock Stay assembly and accessories' structure

damage and leakage not be found.

(d)机轮状态完好，无轮缘损伤,检查轮胎磨损情况在规定范围内；

Inspect and make sure that wheels status are normal,there

are no signs of flange damage and the wear of tires are in

the specified limits.

(e)机轮轮毂内外半轮连接螺栓无剪断或脱落（如可见）；

Inspect and make sure that there are no stripped or

crushed threads for the attachment bolts between inner

half?wheel assembly and outer half?wheel assembly（If visible）.

(f)轮胎压力无明显不足。

Inspect and make sure that there are no obvious insufficient

pressure on the tires.

③、检查左主起落架状态应正常：

Inspect and make sure that LH main landing gear is normal.

(a)刹车装置状态良好,如果刹车系统超温（机组报告、ECAM显示或AIDS有刹

车超温报告）,完成相应检查；

Inspect and make sure that brake assemblies are normal,

if overtemperature occurs on the brake system(Crew

report,ECAM display or Brake overtemperature-report of AIDS),perform the related inspection.

(b)检查缓冲支柱的镜面高度应正常；

Inspect the dimension "H" for the shock absorber for normal.

(c)左主起落架、侧撑杆组件、锁撑组件及其附属部件的结构无损伤、渗漏； Inspect and make sure that LH main landing gear，Side-Stay

assembly and Lock Stay assembly and the structure of the

accessories are not found with damage and leakage.

(d)机轮状态完好，无轮缘损伤,检查轮胎磨损情况在规定范围内；

Inspect and make sure that wheels status are normal,there

are no signs of flange damage and the wear of tires are in

the specified limits.

(e)机轮轮毂内外半轮连接螺栓无剪断或脱落（如可见）；

Inspect and make sure that there are no stripped or

crushed threads for the attachment bolts between inner

half?wheel assembly and outer half?wheel assembly（If visible）.

(f)轮胎压力无明显不足。

Inspect and make sure that there are no obvious insufficient

pressure on the tires.

四川航空股份有限公司SICHUAN AIRLINES

检查右后机身无损坏、凹坑，其下表面无渗漏。

目视检查垂直尾翼、方向舵水平安定面、APU余油管及其舱门下部表面无

检查左后机身无损坏、凹坑，其下表面无渗漏。

四川航空股份有限公司SICHUAN AIRLINES 检查左机翼前缘无损坏、凹坑，翼尖、机翼后缘、飞行舵面无损坏和渗漏。

四川航空股份有限公司SICHUAN AIRLINES

四川航空股份有限公司SICHUAN AIRLINES

四川航空股份有限公司SICHUAN AIRLINES

短停绕机检查路线图 Walk-around check route

注：M-机械；AV-电子 (供外站维护人员使用参考)