116_269_EOA33-53-0003

Hong Kong Airlines Limited香港航空03110-01Hong Kong Airlines MEDHong Kong Airlines LimitedWO NO/工作指令号SEQ NO/序列号WOHA33961_269_116适航指令(AD) 961116TitleInspection of Rods in BellyMcd&Rev/厂家工卡&修订日期标题检查机腹整流罩内的撑杆A/C/飞机号/组别EO JC No./EO工卡EO JC Rev/工卡版本Workarea/工作区域Skill/工种Man Hour/工时BLND/1EOA33-53-0003R02机身/AirframeAIRP13:00Baseline/依据Operator EO/营运人EOEO Rev/EO版本Work Type/工作类别Threshold/首检Interval/重复检CAD 2012-MULT-04,AD 2012-0005,ASB A330-53-3186 R01EOA33-HKG53-0001R02Written/编写Reviewed/审核Approved/批准2012-05-042012-05-072012-05-08Accomplished完工签署Complete Date完工日期Station维修站PVGREASON & DESCRIPTION/原因及描述由于撑杆生产过程存在缺陷导致交付的撑杆存在裂纹(只存在于撑杆折边端部） 。故下发此EO对机腹整流罩内的某些撑杆进行检查。A rod manufacturing process defect has been identified at TAC that could have led to deliver rods with cracks (crimped end of the rod only).This Inspection EO requires to inspect some rods in the belly fairing. R01版改版原因：根据SB A330-53-3186R1修改工作步骤和FIGURE。Reason for R01:Revise the work instruction and FIGURES accordance to SB A330-53-3186R1.R02 版改版原因/Reason for R02:1. 在“依据文件”里添加AD信息/Add AD information in SOURCE.2. 在“有效性”里增加B-LNI、B-LNY、B-LNZ/Add B-LNI、B-LNY、B-LNZ in EFFECTIVITY.3. 修改控制信息/Change Control Information.TOOLS/工具TOOLS NECESSARY/必须工具ITEM项目P/N件号DESCRIPTION名称EQTP类型QTY数量APP适用性Conditions note互换信息及备注198F32204001001COLLAR, SAFETY - DOOR, NLGTO2ALL无298D27803000000LOCKING TOOL - FLAP/SLAT CONTROL LEVERTO1ALL无398F32104013000SAFETY COLLAR-DOOR MLGTO1ALL无TOOLS IF NECESSARY/视情工具ITEM项目P/N件号DESCRIPTION名称EQTP类型QTY数量APP适用性Conditions note互换信息及备注PARTS AND MATERIAL/航材NOTE:OPERATOR MUST GET AND INSTALL THE PARTS THAT CORRESPOND TO THE RELATIVE WORKORDER NO.注释：请工作者严格按照工作指令号领取预定的航材装机PARTS AND MATERIAL NECESSARY/必须航材ITEM项目P/N件号DESCRIPTION名称EQTP类型QTY数量APP适用性Conditions note互换信息及备注PARTS AND MATERIALIF NECESSARY/视情航材ITEM项目P/N件号DESCRIPTION名称EQTP类型QTY数量APP适用性Conditions note互换信息及备注1MS24665-153(32A3)PINAS36ALL视情/As Necessary2MS24665-300PIN COTTERAS6ALL视情/As Necessary3DAPCO2100SEALENTCH1ALL视情/As Necessary/CML09-012F4CML09-018SEALANTCH1ALL视情/As Necessary5CML05-013ACOMPOUNDCH1ALL视情/As Necessary6CML11-002CLEANERCH1ALL视情/As Necessary7CML05-002Non Hardening Jointing Putty - Medium Temp. AreaCH1ALL视情/As Necessary8CML15-005ACOMPOUNDCH1ALL视情/As Necessary9MIL-PRF-81733SEALANTCH1ALL视情/As Necessary/CML09-13B10F0003010400100ROD（禁订）AS2ALL视情/As Necessary11F0003010400300ROD（禁订）AS2ALL视情/As Necessary12F0003010400400ROD （禁订）AS2ALL视情/As Necessary13F0003010400500ROD（禁订）AS4ALL视情/As Necessary14F0003010400700ROD（禁订）AS2ALL视情/As Necessary15F0003010400800ROD（禁订）AS2ALL视情/As Necessary16F0003010400900ROD（禁订）AS1ALL视情/As Necessary17F0003010401100ROD（禁订）AS2ALL视情/As Necessary18F0003010401200ROD（禁订）AS2ALL视情/As Necessary19F0003010401400ROD（禁订）AS2ALL视情/As NecessaryIMPORTANT NOTE:In the event of any discrepancies between the Chinese instruction and the English instruction, the English procedure should prevail.Record Additional Work/Findings(If Applicable) Reference No. Certificate of Release to Service (* Tick as appropriate # Different crews should perform the work on each of the systems)Certifies that the work specified, except as otherwise specified, was carried out in accordance with HKAR-145and in respect to that work, The aircraft / aircraft components are considered ready for Release to Service. HKA Approval No: AI / 135 / 706 * HNAT Approval No.: JMM 076, D3039 * HNAT Approval No.: JMM 047, D101115* HNAT Approval No.: JMM 049, D500023 * CASL Approval No: AI / 101 / 798 * TAECO Approval No.: DAI / 89 / 1295 * HAECO Approval No: DAI / 1 / 853 * SIAEC Approval No: AWI / 01 * STARCO Approval No.: JMM 039, D.200078 * SMECO Approval No: JMM 081, D.400009 * Other: * Signature:_ Authorization No.:_ Date:_工卡Job card:EOA33-53-0003TITLEInspection of Rods in BellyPerfInsp标题检查机腹整流罩内的撑杆工作者检查者A. 通用信息/ General Information警 告：必须遵守所参考手册的所有警告和注意事项。WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONSINCLUDED IN THE REFERENCED PROCEDURES.注 意：遵守使线束和设备处于良好状态的警示信息。当执行设备维护、修理及改装时，尽可能地保持线束、电气设备及工组区域的洁净，执行下述要求：使用如塑料布、布匹等铺盖在上述设备上；经常性的去除线束、电气设备上的杂物及其他污染物。可减少安装电线时的污染和损伤。若污染,参照ESPM20-55-00处理。CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLYSERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS :- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS NECESSARY ON WIRING AND COMPONENTS.- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION.THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00.(1) 紧固件的拆装(参考SRM 51-42-00)。Remove and install the fasteners (Refer to SRM 51-42-00).(2) 紧固件的选择和替换参考SRM 51-43-00。For alternative and substitute fasteners，refer to SRM 51-43-00.(3) 螺纹紧固件的扭紧标准参考SRM 51-49-00 and AMM Task 20-21-11-911-801。Torque the standard threaded fasteners (Refer to SRM 51-49-00 and AMM Task 20-21-11-911-801).(4) 保护涂层的刷涂：Renew the protective finish with :参考SRM 51-23-12，按需刷涂临时防腐涂层15-005A。Corrosion Preventive Temporary Protective Compound 15-005A As required (Refer to SRM 51-23-12)(5) 紧固件的头部使用：On the head of the fasteners apply :按需刷涂09-013B防腐涂层Corrosion Inhibiting Brush Consistency 09-013B As required(6) 撑杆端部需打保险确保安全(参考 AMM Task 20-11-11-911-803)。Secure the rod ends with lock wire (Refer to AMM Task 20-11-11-911-803).B. 准备/PREPARATION(1) 确认飞机静电接地(参考 AMM Task 12-34-24-860-802)。Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802).(2) 打开MLG舱门(参考 AMM Task 32-12-00-010-801)。Open the MLG doors (Refer to AMM Task 32-12-00-010-801).(3) 参考AMM 06-41-53, Page Block 001, AMM Task 53-35-11-000-801, AMM Task 53-35-13-000-801 和AMM Task 53-35-13-000-802拆下下列接近面板：191BB, 191CB, 191QB, 192BB, 192CB, 192QB, 195CB, 196GB, 197BB, 197EB,197GB, 197HB, 198BB, 198EB, 198GB and 198HBRemove the following belly fairing access panels :(Refer to AMM 06-41-53, Page Block 001, AMM Task 53-35-11-000-801, AMM Task53-35-13-000-801 and AMM Task 53-35-13-000-802).191BB, 191CB, 191QB, 192BB, 192CB, 192QB, 195CB, 196GB, 197BB, 197EB,197GB, 197HB, 198BB, 198EB, 198GB and 198HB(4) 放置工作梯。 Put access platform(s) in position. (5) 拆下左侧后部整流罩(Refer to Fig. A-FBDAA and AMM Task 53-35-11-000-802) Remove the Aft Fillet Fairing from LH side for Access (Refer to AMM Task 53-35-11-000-802)1Aft Fillet FairingItem(30)保留/Retain(6) 拆下右侧后部整流罩(Refer to Fig. A-FBDAA and AMM Task 53-35-11-000-802) Remove the Aft Fillet Fairing from RH side for Access (Refer to AMM Task 53-35-11-000-802)1Aft Fillet FairingItem(31)保留/RetainC. 工作步骤/PROCEDURE(1) 一次性详细检查撑杆 Do a One Time Detailed Inspection of the Rods(a) 检查区域，参考Fig. A-FBAAA For the inspection area, refer to Fig. A-FBAAA.(b) 一次性详细检查撑杆（检查撑杆件号和生产厂家）。Do a one time detailed inspection of the rods. Identify the part number and the manufacturer of the rod.1) 若撑杆上的制造商标识为TAC或无制造商标识，执行步骤(2) HFEC检查TAC撑杆。If the manufacturer of the rod is TAC or if the manufacturer cannot be identified, go to (2) Do a HFEC Inspection of the TAC Rods.2) 若撑杆的制造商标识非TAC，执行恢复工作恢复飞机。If the manufacturer of the rod is not TAC, no further action is required.(c) 将后附表格1发送给TS结构科()。Send Table 1 to .(2) HFEC检查TAC撑杆Do a HFEC Inspection of the TAC Rods(a) 检查区域参考Fig. A-FBAAA For the inspection area, refer to Fig. A-FBAAA.(b) 依据NTM 51-10-08 HFEC检查TAC撑杆，参考Fig. A-FBBAA。Do a HFEC inspection of the TAC rods as per NTM 51-10-08.Refer to Fig. A-FBBAA.1) 若未发现裂纹，执行恢复工作。 If no crack is found, no further action is required. 2) 若发现裂纹，根据步骤C.(3)更换开裂的撑杆。 If crack is found replace the rod according to step C.(3).(c) 填写反馈表发送给TS结构科()。Fill out the feedback form and Send it to .(3) 更换撑杆Replace the Rods (a) 更换位于FR39处的机身腹部整流结构上部撑杆Replace the Upper Rods of the Belly Fairing Structure at FR391) 左侧拆除： Remove from LH side : Fig. A-FBCAA Sheet 03, Detail F2) 左侧安装： Install on LH side :Fig. A-FBCAA Sheet 03, Detail F注 释：在安装撑杆时，将撑杆调节至正确的长度，并在扭紧紧固件后打上保险。NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 3) 右侧拆除： Remove from RH side :Fig. A-FBCAA Sheet 03, Detail F4) 右侧安装： Install on RH side :Fig. A-FBCAA Sheet 03, Detail F注 释：在安装撑杆时，将撑杆调节至正确的长度，并在扭紧紧固件后打上保险。 NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners.(b) 更换位于FR39处的机身腹部整流结构侧向撑杆Replace the Lateral Rods of the Belly Fairing Structure at FR391) 左侧拆除： Remove from LH side :Fig. A-FBCAA Sheet 03, Detail F2) 左侧安装：Install on LH side :Fig. A-FBCAA Sheet 03, Detail F注 释：在安装撑杆时，将撑杆调节至正确的长度，并在扭紧紧固件后打上保险。NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 3) 右侧拆除： Remove from RH side :Fig. A-FBCAA Sheet 03, Detail F4) 右侧安装：Install on RH side :Fig. A-FBCAA Sheet 03, Detail F注 释：在安装撑杆时，将撑杆调节至正确的长度，并在扭紧紧固件后打上保险。NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. (c) 更换位于FR47处的机身腹部整流结构侧撑杆Replace the Lateral Rods of the Belly Fairing Structure at FR471) 左侧拆除：Remove from LH side :Fig. A-FBCAA Sheet 04, Detail G2) 左侧安装：Install on LH side :Fig. A-FBCAA Sheet 04, Detail G注 释：在安装撑杆时，将撑杆调节至正确的长度，并在扭紧紧固件后打上保险。NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 3) 右侧拆除：Remove from RH side :Fig. A-FBCAA Sheet 04, Detail G4) 右侧安装:Install on RH side :Fig. A-FBCAA Sheet 04, Detail G注 释：在安装撑杆时，将撑杆调节至正确的长度，并在扭紧紧固件后打上保险。NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. (d) 更换位于FR47处的机身腹部整流结构中心撑杆Replace the Central Rod of the Belly Fairing Structure at FR471) 拆下：Remove :Fig. A-FBCAA Sheet 03, Detail F2) 安装：Install :Fig. A-FBCAA Sheet 03, Detail F注 释：在安装撑杆时，将撑杆调节至正确的长度，并在扭紧紧固件后打上保险。NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. (e) 更换位于FR53.2处的机身腹部整流结构上部撑杆Replace the Upper Rods of the Belly Fairing Structure at FR53.21) 左侧拆除：Remove from LH side :Fig. A-FBCAA Sheet 03, Detail F2) 左侧安装：Install on LH side :Fig. A-FBCAA Sheet 03, Detail F注 释：在安装撑杆时，将撑杆调节至正确的长度，并在扭紧紧固件后打上保险。NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 3) 右侧拆除：Remove from RH side :Fig. A-FBCAA Sheet 03, Detail F4) 右侧安装：Install on RH side :Fig. A-FBCAA Sheet 03, Detail F注 释：在安装撑杆时，将撑杆调节至正确的长度，并在扭紧紧固件后打上保险。NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. (f) 更换位于FR53.2处的机身腹部整流结构侧向撑杆Replace the Lateral Rods of the Belly Fairing Structure at FR53.21) 左侧拆下：Remove from LH side :Fig. A-FBCAA Sheet 04, Detail H2) 左侧安装：Install on LH sideFig. A-FBCAA Sheet 04, Detail H注 释：在安装撑杆时，将撑杆调节至正确的长度，并在扭紧紧固件后打上保险。NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 3) 右侧拆除：Remove from RH side :Fig. A-FBCAA Sheet 04, Detail H4) 右侧安装： Install on RH sideFig. A-FBCAA Sheet 04, Detail H注 释：在安装撑杆时，将撑杆调节至正确的长度，并在扭紧紧固件后打上保险。NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. (g) 更换位于FR53.2处的机身腹部整流结构中心撑杆Replace the Center Rods of the Belly Fairing Structure at FR53.21) 左侧拆除：Remove from LH side :Fig. A-FBCAA Sheet 05, Detail J2) 左侧安装：Install on LH side :Fig. A-FBCAA Sheet 05, Detail J注 释：在安装撑杆时，将撑杆调节至正确的长度，并在扭紧紧固件后打上保险。NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 3) 右侧拆除：Remove from RH side :Fig. A-FBCAA Sheet 05, Detail J4) 右侧安装：Install on RH side :Fig. A-FBCAA Sheet 05, Detail J注 释：在安装撑杆时，将撑杆调节至正确的长度，并在扭紧紧固件后打上保险。NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. (h) 更换位于FR53.4处的机身腹部整流结构上部撑杆Replace the Upper Rods of the Belly Fairing Structure at FR53.41) 左侧拆除：Remove from LH side :Fig. A-FBCAA Sheet 05, Detail K 2) 左侧安装:Install on LH side :Fig. A-FBCAA Sheet 05, Detail K注 释：在安装撑杆时，将撑杆调节至正确的长度，并在扭紧紧固件后打上保险。NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 3) 右侧拆除： Remove from RH side :Fig. A-FBCAA Sheet 05, Detail K4) 右侧安装：Install on RH side :Fig. A-FBCAA Sheet 05, Detail K注 释：在安装撑杆时，将撑杆调节至正确的长度，并在扭紧紧固件后打上保险。NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. (i) 更换位于FR53.4处的机身腹部整流结构侧向撑杆Replace the Lateral Rods of the Belly Fairing Structure at FR53.41) 左侧拆除：Remove from LH side :Fig. A-FBCAA Sheet 05, Detail K2) 左侧安装：Install at LH side :Fig. A-FBCAA Sheet 05, Detail K注 释：在安装撑杆时，将撑杆调节至正确的长度，并在扭紧紧固件后打上保险。NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 3) 右侧拆除：Remove from RH side :Fig. A-FBCAA Sheet 05, Detail K4) 右侧安装：Install at RH side :Fig. A-FBCAA Sheet 05, Detail K注 释：在安装撑杆时，将撑杆调节至正确的长度，并在扭紧紧固件后打上保险。NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. (j) 更换位于FR53.9处的机身腹部整流结构侧向撑杆Replace the Lateral Rods of the Belly Fairing Structure at FR53.91) 左侧拆除：Remove from LH side :Fig. A-FBCAA Sheet 03, Detail F2) 左侧安装：Install at LH side :Fig. A-FBCAA Sheet 03, Detail F注 释：在安装撑杆时，将撑杆调节至正确的长度，并在扭紧紧固件后打上保险。NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 3) 右侧拆除：Remove from RH side :Fig. A-FBCAA Sheet 03, Detail F4) 右侧安装：Install at RH side :Fig. A-FBCAA Sheet 03, Detail F注 释：在安装撑杆时，将撑杆调节至正确的长度，并在扭紧紧固件后打上保险。NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. (k) 更换位于FR48处的MLG舱门上位锁的撑杆Replace the Rods of the Supports of the MLG Door Uplock at FR481) 左侧拆除：Remove from LH side :Fig. A-FBCAA Sheet 06, Detail L2) 左侧安装：Install on LH side :Fig. A-FBCAA Sheet 06, Detail L注 释：在安装撑杆时，将撑杆调节至正确的长度，并在扭紧紧固件后打上保险。NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on