例行工卡模板2014年5月后执行

1、Completion Date(完成日期)：YYYY / MM / DDCHINA SOUTHERN AIRLINES中国南方航空公司由于飞机构型或改装等 ，对于不适用本次维修工作的整份工卡，工作者应在此处盖“N/A”章，叙述不适用的原因，签字并经检验员盖章确认后关闭。Job Card 工:Mechanical/Inspection (RII)CABINA20J534195-01-2机械必检客舱A/C TypeA319/A320/A3机种： 21A/C Tail No.飞机号： B-XMaint. StationSHE维修站：Work Order 工作指令号： Workorder Date工系

2、统产生，或按生产下发的工作指令单填写JC SEQ No.顺序号：Threshold 首检NOTEInterval 间隔NOTEMan Hours 工时0.5Labor 人力2Elapsed 停场时间0.5Revision 修订2011-11-01Version 版本R9Written/Revised By 编写/修订宋阳 2011-12-30Station 站位N/AStringer 桁条N/ARelated Card 相关工卡N/AReference Documents 参考文件53-41-00-210-835-AReviewed/Approved By审核/批准付玉生 2012-01-30

3、Zone 区域261 262Access Panel 接近盖板N/AMRS No. MRS 号S53-41-144 S53-41-142JC Title工卡标题CABIN FLOOR STRUCTURE AFT ENTRANCE AREA(CPCP)口区域座舱地板结构(CPCP)Mech机械员Insp检验员Tools & Equipment 工具和设备：Not Required不需Parts & Material 部件和航材：P/N 件号QTY 数量 DESIGNATION 名称REMARK 备注1 11-026AS REQSOLVENTGENERALAPP/适用性:ALL/所

4、有飞机按需PURPOSEFrom/来源:通用溶剂53-41-00-210-835-A2 15-005AS REQCORROSIONAPP/适用性:ALL/所有飞机按需PREVENTIVEFrom/来源:TEMPORARY53-41-00-210-835-A PROTECITIVECOMPOUND防腐剂3 15-006AS REQCORROSIONAPP/适用性:ALL/所有飞机按需PREVENTIVEFrom/来源:TEMPORARY53-41-00-210-835-A PROTECITIVECOMPOUND防腐剂4 15-007AS REQCORROSIONAPP/适用性:ALL/所有飞机按

5、需PREVENTIVEFrom/来源:TEMPORARY53-41-00-210-835-A PROTECITIVECOMPOUND防腐剂Aircraft Effectivity 飞机适用范围:ALL填写工卡关闭日期航材页，盖相应Page 页码1 of 8Job CardA20J534195-01-2工：JC Title工卡标题CABIN FLOOR STRUCTURE AFT ENTRANCE AREA(CPCP)口区域座舱地板结构(CPCP)Mech机械员Insp检验员5 15-008AS REQCORROSIONAPP/适用性:ALL/所有飞机按需PREVENTIVEFrom/来源:TE

6、MPORARY53-41-00-210-835-A PROTECITIVECOMPOUND防腐剂6 19-003AS REQLINT-FREECOTTONAPP/适用性:ALL/所有飞机按需CLOTHFrom/来源:不掉毛的布53-41-00-210-835-AWork Content 工作内容：CABIN FLOOR STRUCTURE AFT ENTRANCE AREA口区域座舱地板结构MRS NO: S53-41-142INTERVAL NOTE：T: 5YE I: 5YE间隔注：T: 5YE I: 5YENOTE: CREDIT CAN BE TAKEN FROM PREVIOUS A

7、CCOMPLISHMENT OF TASK 534147-01-1 OR TASK 534147-01-2 OR TASK 534147-01-3 (ACCORDING TO TASK APPLICABILITY).NOTE: IN CASE SUFFICIENT ACCESS TO LATERAL SHEAR WEBS IS NOT POSSIBLE DUE TO GALLEY CONFIGURATION,THE GALLEY MUST BE REMOVED TO GET ACCESS TO THE INSPECTION AREA.TPS : APPLICATION OF TPS TYPE

8、1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2注：从上一次完成任务534147-01-1和534147-01-2和534147-01-3 开始计算时间间隔（根据工作适用性）。注：万一由于厨房构型的 不能充分接近横向剪切板则必须拆卸厨房以接近检查区域。TPS：施加I型临时保护系统然后再施加II型。MRS NO: S53-41-144NTERVAL NOTE：T: 6YE I: 6YE间隔注：T: 6YE I: 6YENOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 534147

9、-01-1 OR TASK 534147-01-2 OR TASK 534147-01-3 (ACCORDING TO TASK APPLICABILITY).NOTE: IN CASE SUFFICIENT ACCESS TO LATERAL SHEAR WEBS IS NOT POSSIBLE DUE TO GALLEY CONFIGURATION, THE GALLEY MUST BE REMOVED TO GET ACCESS TO THE INSPECTION AREA.TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICA

10、TION OF TPS TYPE 2注：从上一次完成任务534147-01-1和534147-01-2和534147-01-3 开始计算时间间隔（根据工作适用性）。Aircraft Effectivity 飞机适用范围: ALLPage 页码2 of 8Job CardA20J534195-01-2工：JC Title工卡标题CABIN FLOOR STRUCTURE AFT ENTRANCE AREA(CPCP)口区域座舱地板结构(CPCP)Mech机械员Insp检验员注：万一由于厨房构型的不能充分接近横向剪切板则必须拆卸厨房以接近检查区域。TPS：施加 I 型临时保护系统然后再施加 II

11、型。TASK 53-41-00-210-835-ADetailed Visual Inspection of Cabin Floor Structure and Structure below AFT Entrance Area, between FR66 and FR68 and Lateral Shear Plates FR68 and FR70(CPCP)详细目视检查客舱地板结构和口区域下方结构，在框 66 和框 68，横向剪切板 FR68 和 FR70 之间(CPCP)1. Job Set-up工作准备Subtask 53-41-00-010-172-AA. Get Access接近(

12、1) If necessary, remove the cabin attendant seat(s) (Ref. TASK 25-22-41-000-001) or (Ref. TASK 25-22-42-000-001).根据需要，拆下客舱乘务员座椅（Ref. TASK 25-22-41-000-001 ）或（ Ref. TASK25-22-42-000-001）。(2) Remove the applicable floor panels between FR66 and FR68 (Ref. TASK 53-42-12-000-002).拆下介于 FR66 和 FR68 之间有关的地板

13、（Ref. TASK 53-42-12-000-002）。(3) Remove the lower door frame lining at FR68, LH/RH.在 FR68 左/右拆下下部门框衬层。(4) Remove the side lateral galley lining.拆下侧横向厨房衬层。(5) If necessary, remove the aft galley (Ref. TASK 25-33-41-000-001) or (Ref. TASK 25-33-41-000-002) or (Ref.TASK 25-33-41-000-008) or (Ref. TASK

14、25-33-43-000-001) or (Ref.TASK 25-33-45-000-001).根据需要，拆下后厨房（参考 TASK 25-33-41-000-001 或 TASK 25-33-41-000-002 或TASK 25-33-41-000-008 或 TASK 25-33-43-000-001 或TASK 25-33-45-000-001）。NOTE: The removal of the aft galley is only necessary if you cannot get access to the lateral shear plates.注：只有当无法接近到横向剪

15、切板处时，才有必要拆下后厨房。XXAircraft Effectivity 飞机适用范围: ALLPage 页码3 of 8Job CardA20J534195-01-2工：JC Title工卡标题CABIN FLOOR STRUCTURE AFT ENTRANCE AREA(CPCP)口区域座舱地板结构(CPCP)Mech机械员Insp检验员(6) Cleaning the inspection area with the CLEANING AGENTS (Material No. 11-026) and a clean lint-free cloth MISCELLANEOUS(Mater

16、ial No.19-003).用清洁剂(材料号 11-026)和一块不起毛的布（材料号 19-003）来清洁待检查区域。2. Procedure如果不是必检 卡，则不需检验(Ref. Fig. Cabin Floor Structure - FR66 thru FR70 SHEET 1)员盖章(Ref. Fig. Lateral Shear Plates - Inspection Area SHEET 1) (参考图：隔框 66 到 70 之间的客舱地板结构，第一页)(参考图：检查区域横向剪切板，第一页)Subtask 53-41-00-210-136-AA. Detailed Visual

17、Inspection Procedure详细目视检查程序(1) Do a detailed visual inspection of the cabin floor structure and the structure below the aft entrance area. Do this between FR66 and FR68 and the lateral shear plates between FR68 and FR70.详细目视检查客舱地板结构和口区域下部结构，在FR66 和FR68 以及FR68 和FR70之间的横向剪切板之间进行。(a) Make sure that yo

18、u examine the floor structure.确保检查地板结构。(b) Look for corrosion and other damage to the mparts.查看金属部件上是否有腐蚀和其它的损伤。如果此步不适用，且属已知代码，(2) If you find corrosion damage:需加盖“N/A”章+代码。此类 N/A 项目1_如果发现有腐蚀损伤：无需在“N/A页”作再次说明。(a) Refer to the ASRM SRM 51220000 for teral corrosion-protection data.参考 ASRM SRM 51220000

19、 一般腐蚀保护数据。(b) Repair the corroded areas (Ref. TASK 51-74-11-300-001).修理腐蚀区域（参考TASK 51-74-11-300-001）。(3) If you find damage to the mparts:如果金属部件发现有损伤： 1_Aircraft Effectivity 飞机适用范围: ALLPage 页码4 of 8Job CardA20J534195-01-2工：JC Title工卡标题CABIN FLOOR STRUCTURE AFT ENTRANCE AREA(CPCP)口区域座舱地板结构(CPCP)Mech机

20、械员Insp检验员(a) Refer to the ASRM SRM 51110000 for the class of the damage.参考 ASRM SRM 51110000 对损伤进行鉴定。(b) Refer to the ASRM SRM 51111100 for the permitted damage limits.参考 ASRM SRM 51111100 中的所的损伤限制范围。(c) Repair the minor damage (Ref. TASK 51-73-11-300-001 or Ref. TASK 51-73-11-300-004).修理微小损伤(参考 TAS

21、K 51-73-11-300-001 或 参考TASK 51-73-11-300-004)。(4) If you find other damage to the m parts that is more than the limits for minor damage, you must:如果金属部件上发现有超出微小损伤限制范围的其它损伤，必须：(a) Refer to the ASRM for the material details, the item identification and th action/repair data:如果此步不适用，且不参考 ASRM 材料详细说明、损伤

22、鉴定以及工作/修理数据：属已知代码，需加盖“N/A”章。此类 N/A1) For the floor structure, refer to the ASRM SRM 534114.项目需在“N/A对于地板结构，参考 ASRM SRM 534114。页”作说明。3. Close-up关闭Subtask 53-41-00-916-089-A使用的材料，需后附“例行工A. Corrosion Protection:卡航材用料单”进行。防腐：(1) Apply STORAGE PRE ATION (Material No. 15-005) or STORAGE PRESERVATION (Mater

23、ia o. 15-006) to the cabin floor structure (Ref. TASK 51-75-13-916-002).在客舱地板结构上涂一层防腐剂(材料号 15-005)或防腐剂(材料号 15-006)(Ref. TASK51-75-13-916-002)。(2) Apply STORAGE PRESERVATION (Material No. 15-007) or STORAGE PRESERVATION (Material No. 15-008) or equivalent to the cabin floor structure (Ref. TASK 51-75

24、-13-916-002).在客舱地板结构上涂一层防腐剂(材料号 15-007)或防腐剂(材料号 15-008)或等效防腐剂(Ref. TASK 51-75-13-916-002)。如果某些步骤不必执行且其相应栏内没有划线时，工作者仅需在没有执行的步骤签写“N/A”和代码但不必签名。Page 页码5 of 8Job Card工：A20J534195-01-2Mech机械员Insp检验员CABIN FLOOR STRUCTURE AFT ENTRANCE AREA(CPCP)口区域座舱地板结构(CPCP)JC Title工卡标题Subtask 53-41-00-410-168-AB.Close A

25、ccess关闭接近XX(1)Make sure that the work area is clean and clear of tool(s) and other items.确保该工作区域是清洁的，并且没有工具和其它物品。(2)If necessary, install the aft galley (Ref. TASK 25-33-41-400-001) or (Ref. TASK 25-33-41-400-002) or (Ref.TASK 25-33-41-400-008) or (Ref. TASK 25-33-43-400-001)or (Ref.TASK 25-33-45-40

26、0-001).根据需要，安装后厨房（参考 TASK 25-33-41-400-001 或 TASK 25-33-41-400-002 或TASK 25-33-41-400-008 或 TASK 25-33-43-400-001 或TASK 25-33-45-400-001）。(3)Install the side lateral galley lining.安装侧横向厨房衬层。(4)Install the lower door frame lining at FR68, LH/RH.在 FR68 左/右安装下门框衬层。(5)Installtheapplicablefloorpanelsbetw

27、eenFR68toFR68(Ref.TASK 53-42-12-400-002).在 FR66 到 FR68 之间安装有关的地板（Ref. TASK 53-42-12-400-002）。(6)If necessary, Install the cabin attendants seat(s) (Ref. TASK 25-22-41-400-001) (Ref. TASK 25-22-42-400-001).根据需要，安装客舱乘务员座椅（ Ref. TASK 25-22-41-400-001 ）（ Ref. TASK25-22-42-400-001）。度量采用标准写法根据相关工卡增加内容：（1）

28、Measure and write down dimension H如：毫米用 mm 表示即可HH： 165 mm 测量并DimensionH/描述性语言需中英文对照（2）Make sure the seat condition is good.确保座椅状态良好。Seat condition/座椅状态： 座椅状态良好 / The seat condition is good。确保数据符合工卡要求, 度量单位与工卡一致。）（3）Torque the valve between 50 and 60 lbf·in。拧紧活门，力矩为 50 至 60 磅·英寸Torque Values/力矩值： 55 lbf&#