WOHA33_5677BLNS 6C221_146_EOA33-92-0019

Hong Kong Airlines Limited香港航空有限公司F-D-099Hong Kong Airlines MEDHong Kong Airlines LimitedWO NO/工作指令号SEQ NO/序列号WOHA335677_146_221DM 5677221Training and Qualification/培训和资格Technical Record/技术记录ETOPSNONETitleImprove Wire Routing in PylonMcd&Rev/厂家工卡&修订日期标题改装吊架附近的线路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BLNS/3EOA33-92-0019R15机身/AirframeSMTL /AIRP01:00/27:00Baseline/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SB A330-92-3130/R04EOA33-HKG92-0013R10Written/编写Reviewed/审核Approved/批准2018-12-202018-12-212018-12-21Accomplished完工签署Complete Date完工日期Station维修站SHAREASON & DESCRIPTION/原因及描述A330运营人报告了数次吊架区域的线束损伤，线束损伤可能导致压力传感器8HA1/8HA2和9HA1/9HA2传输错误的数据。下发EO改装吊架区域的布线。Several events of wiring being damaged in pylon area have been reported to Airbus by A330 operators,this will lead to potential system misbehaviour of the pressure transducers 8HA1/8HA2 and 9HA1/9HA2.Issue EO to modify the wiring installation in pylon area.R01 由于新引进飞机BLNN，增加 适用性。修改EO控 制信息。R01 Due to the new delivery aircraft BLNN,update the effectivity.Revise EO control information. R02 依据文件由“A330-92-3130 R00”改为“A330-92-3130 R01”。修改航材信息,删除“923130A08R00，923130A10R00，923130A09R02，923130A05R02，923130A07R02，923130A11R02，923130A12R00，923130A06R00，F9239026700100 ，EN6049-007-08-5”，增加“923130A05R05，923130A06R03，923130A07R05，923130A08R03，923130D01R01，923130A09R04，923130A10R02，923130A11R04，923130A12R02”，修改施工步骤。由于 新引进飞机BLNR，BLNS增加适用性R02 Baseline change from “A330-92-3130 R00 ”to“A330-92-3130 R01”.Modify the material information ，delete923130A08R00，923130A10R00，923130A09R02，923130A05R02，923130A07R02，923130A11R02，923130A12R00，923130A06R00，F9239026700100，EN6049-007-08-5”,increase“923130A05R05，923130A06R03，923130A07R05，923130A08R03，923130D01R01，923130A09R04，923130A10R02，923130A11R04，923130A12R02”，revised work steps.Due to the new delivery aircraft BLNR,BLNS，update the effectivity. R03 由于新引进飞机BLNU，BLNT增加 适用性。R03 Due to the new delivery aircraft BLNU,BLNT update the effectivity. R04 延长完工期限R04 To extend the deadline R05 修改航材信息由“923130A09R04，923130A10R02，923130A12R02，923130A11R04”改为“923130A09R02和923130A09S01 ，923130A10R00和923130A10S01，923130A12R00和923130A12S01，923130A11R02和923130A11S01”.由“923130A05R05，923130A07R05，923130A06R03，923130A08R03”改为“923130A05R02和923130A05S01，923130A07R02和923130A07S01，923130A06R00和923130A06S01，923130A08R00和923130A08S01”.修改施工步骤和依据 文件为“A330-92-3130 R02”。R05 revised the material information change from“923130A09R04，923130A10R02，923130A12R02，923130A11R04 ”to“923130A09R02 and 923130A09S01，923130A10R00 and 923130A10S01，923130A12R00 and 923130A12S01，923130A11R02 and 923130A11S01”.change from“923130A05R05，923130A07R05，923130A06R03，923130A08R03”to“923130A05R02 and 923130A05S01，923130A07R02 and 923130A07S01，923130A06R00 and 923130A06S01，923130A08R00 and 923130A08S01”. revise work steps and baseline“A330-92-3130 R02”.版本变化/REVISION改版原因/REASON修改内容/CHANGE DESCRIPTIONR05-R061.新引进飞机BLHD适用此EO。New introduced aircraft BLHD apply to this EO.2.延长完工期限.To extend the deadline.1.增加新引进飞机BLHD的适用性。Add the aircraft BLHD to the effectivity.2.将完工期限延长至2019.12.30.Extend the deadline to 30 DEC 2019.R06-R07依据SB给出的航材信息有误，此EO目前无法执行。Due to wrong spare PN listed in SB, unable to execute this EO.修改控制信息，暂不安排执行此EO。Revise the PLAN&CONTROL information to temporarily terminate this EO.R07-R08参考文件A330-92-3130改版。Reference document a330-92-3130 revision.1.修改参考文件版本为R03。2.修改航材信息。3.修订正文。1.revise the reference document version R03.2.revise the material information.3.revise the cotent.R08-R091.新引进飞机BLHB适用此EO。New introduced aircraft BLHB apply to this EO.1.增加新引进飞机BLHB的适用性。Add the aircraft BLHB to the effectivity.R09-R10参考文件A330-92-3130改版。Reference document a330-92-3130 revision.1.修改参考文件版本为R04。2.修改航材信息。3.修订正文。1.revise the reference document version R04.2.revise the material information.3.revise the cotent.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1CML11-026SOLVENT GENERAL PURPOSECH1ALLN/A2CML08-004SEALANTCH1ALL必需/Necessary3CML19-008LIGATURE CORDCH1ALLN/A4CML19-009LOCKWIREAS1ALL必需/Necessary5CML09-005INTERFAY SEALANTCH1ALLN/A6CML16-024Primer Paint(由AERODUR-37045和S66/22R两部分组成)CH1ALLN/A7RL6000SATAPECH1ALLN/A8923130A09R02KITAS1BLNS必须9923130A10R00KITAS1BLNS必须10923130A11R02KITAS1BLNS必须11923130A12R00KITAS1BLNS必须12923130D01R01KITAS2ALLN/A13923130A09S01KITAS1BLNS必须14923130A10S01KITAS1BLNS必须15923130A11S01KITAS1BLNS必须16923130A12S01KITAS1BLNS必须17923130A10S02KITAS1BLNS必需/Necessary18923130A12S02KITAS1BLNS必需/Necessary19923130A09S02KITAS1BLNS必需/Necessary20923130A11S02KITAS1BLNS必需/NecessaryPARTS 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IMPORTANT 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 * HKE Approval No: AI /218/1215, JMM 133 * HNAT Approval No.: D.101115, JMM 047* CASL Approval No: AI / 101 / 798 * AMECO Approval No.: D100001, JMM 001* HNAT- North West Approval No.: D.500023, JMM 049 * HAECO Approval No: DAI / 1 / 853 * SMECO Approval No.: D.400009, JMM 081* HNAT- YN Approval No.: D.4108, JMM 134 * TAECO Approval No.: DAI / 89 / 1295 * CEA Approval No.: D.200002, JMM 112 * HNAT Approval No.: D.3039, JMM 076 * THAECO Approval No.: D.101661, JMM 124 * CEA-Jiangsu Approval No.: D.200047, JMM 117 * SPRING Approval No.: D.200081, JMM 121 * SIAEC Approval No: AWI / 01 * STARCO Approval No.: D.200078,JMM 039* GAMECO Approval No.: D.300001, JMM 006* THAI Approval No.: AI / 147 / 0910 * Other: * Signature:_ Authorization No.:_ Date:_EOA33-92-0019 R15 W/O:5677 AC:BLNS页码：65 / 65工卡Job card:EOA33-92-0019TITLEImprove Wire Routing in PylonPerfInsp标题改装吊架附近的线路工作者检查者改装左侧吊架线束Modification of the routing in the LH pylon警 告：确保遵守参考手册中所有警告和注意事项。WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES.注 意：确保遵守电气线路防护措施确保处于良好状态（电气和机械可用）。当执行维护工作，修理或改装时，确保电线，部件和工作区域整洁： - 在电线和部件上，放置保护层，如塑料袋，棉布等。 - 定期移除碎屑，其它污染物 这些防护措施将减少电线安装时的污染风险。如果发生污染，参考ESPM 20-55-00进行处理。CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE). 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.A. 概述/GENERAL(1) 标准施工/Standard Practices(a) 对于导线的安全和防护措施，参考AMM Task 20-11-11-911-803。For the wire locking safety procedures and warnings, refer to AMM Task 20-11-11-911-803.(b) 对于保险丝的安装，参考ESPM 20-51-12。For the installation of lockwire, refer to ESPM 20-51-12.(c) 对于绑带安装和工具使用，参考ESPM 20-33-35。For the lacing tape application and tooling, refer to ESPM 20-33-35.(d) 对于区域的识别，参考AMM 06-20-00, Page Block 001。For the identification of zones, refer to AMM 06-20-00, Page Block 001.(e) 对于接近盖板的识别，参考AMM 06-41-53, Page Block 001。For the identification of access panels, refer to AMM 06-41-53, Page Block 001.(f) 对于吊架站位和肋的识别，参考AMM 06-31-54, Page Block 001。For the identification of pylon stations and ribs, refer to AMM 06-31-54, Page Block 001.(g) 对于插头后壳和插头的安装，参考ESPM 20-44-16。For the installation of backshells and plugs, refer to ESPM 20-44-16.(h) 对于插头的安装，参考ESPM 20-48-24。For the installation of connectors, refer to ESPM 20-48-24.(i) 对于线束的连续性测试，参考ESPM 20-52-21。For continuity testing of electrical harnesses, refer to ESPM 20-52-21.(j) 对于管道的安装，参考ESPM 20-33-33。For the installation of conduits, refer to ESPM 20-33-33.(k) 对于管道安装保护，参考ESPM 20-33-30。For the installation of conduit protection, refer to ESPM 20-33-30.(l) 对于消耗件的规格，参考CML。For the specification of the material numbers (Mat. No.), refer to CML.(m) 按需使用CML11-026清洁工作区域。Clean the work areas with Non Aqueous Cleaner-General - - CML11-026 As required(n) 对于紧固件磅力矩，参考AMM 20-21-11-911-801。To torque tighten the standard threaded fasteners, refer to AMM Task 20-21-11-911-801.(o) 紧固件拆装，参考SRM 51-42-00。Remove and install the fasteners in accordance with SRM 51-42-00(p) 钻孔和去毛刺，参考SRM 51-44-11。Drill and deburr the holes in accordance with SRM 51-44-11.(q) 对于埋头孔的制作，参考SRM 51-46-11。To countersink the holes in accordance with SRM 51-46-11.(r) 剪裁铆钉到合适的长度。Cut the rivets to the necessary length.(s) 获取备用或替换紧固件，参考SRM 51-43-00。Obtain alternative and substitute fastener data in accordance with SRM 51-43-00.(t) 如果使用了替换件，确保使用相配套的螺帽和垫片，参考SRM 51-40-00。If alternative and substitute fasteners have to be used, you must make sure that the associated nut/collar are compatible in accordance with SRM 51-40-00 Mating Part column.(u) 如果此份EO的紧固件规范不满足SRM 51章的要求，参考SRM 51章的标准选择合适的替代件。同时选择合适的垫片。If the length of any fastener specified in this EO does not meet installation standards given in SRM Chapter 51, then a fastener of the same specification, or an approved substitute, with a length which meets the installation standards given in SRM Chapter 51 may be used. In addition, washers may be installed for fastener grip length in accordance with SRM Chapter 51.(v) 按需调整卡子的尺寸，参考ESPM 20-33-42。Adapt the clamp size as necessary, refer to ESPM 20-33-42.(w) 参考SRM 51-24-00使用密封剂。Apply sealant in accordance with SRM 51-24-00(x) 使用CML16-024按需涂保护涂层Renew the protective finish in accordance with Primer Paint- - Composite Structure CML16-024 As required(y) 保护涂层的填涂，参考SRM 51-75-12。Renew the protective finish in accordance with SRM 51-75-12(z) 对于跳开关的安全防护，参考AMM Task 20-16-00-912-801。For circuit breaker safety precautions, refer to AMM Task 20-16-00-912-801.(aa) 对于导线束的安装，参考ESPM 20-33-00。For the general installation of electrical wire harnesses, refer to ESPM 20-33-00.(ab) 将保留的硬件放到带有标识的塑料袋中并把装入组件的袋子密封。Put all the retained hardware in identified plastic bags and attach the bags to the related unit.(ac) 给所有拆除要保留的件进行贴标签，以便于后续的安装。Tag all the parts you must remove and retain to make the subsequent installation easier.B.准备/PREPARATION(1) 工作准备/Job Set-up 注释：执行维护工作前，以下构型为飞机基本构型： - 飞机在地面（起落架安全销和轮挡放置在位） - 发动机关车，反推关闭并锁定 - 飞机处于净构型 - 刹车设置 - 飞机电源断开 - 液压系统释压 - 可进入驾驶舱和客舱 - 所有的跳开关闭合 - 所有控制在NORM, AUTO 或OFF位NOTE: The items given in this note shall be considered as the basic Aircraft configuration before you start a maintenance task:- Aircraft on the ground resting on landing gear (the ground safety locks and the wheel chocks are in position on the landing gear)- Engine shut down, thrust reversers are closed and locked- Aircraft in clean configuration- Parking brake applied- Aircraft electrical network de-energized- Hydraulic systems depressurized- Access to the cockpit and cabin is available- All circuit breakers are in closed position- All controls in NORM, AUTO or OFF position.(a) 确保飞机电气接地，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.(b) 参考AMM Task 36-11-16-000-804，执行拆除BRPT (FIN 8HA1)前的准备工作。Do the preparation procedure as specified in the removal of the Bleed Regulated Pressure Transducer (FIN 8HA1), refer to AMM Task 36-11-16-000-804.(c) 参考AMM Task36-11-15-000-804，执行拆除BTPT (FIN 9HA1)前的准备工作。Do the preparation procedure as specified in the removal of the Bleed Transferred Pressure Transducer (FIN 9HA1), refer to AMM Task 36-11-15-000-804.(d) 参考AMM Task 36-11-42-000-804，执行拆除BAPE (FIN 7150HA1)的准备工作。Do the preparation procedure as specified in the removal of the Bleed Air Precooler Exchanger (FIN 7150HA1), AMM Task 36-11-42-000-804.(e) 参考AMM 05-24-50, Page Block 601拆下接近盖板454BL, 452CL, 454BR, 452CR, 453BL, 453BR。Remove the access panels 454BL, 452CL, 454BR, 452CR, 453BL, 453BR, refer to AMM 05-24-50, Page Block 601.(f) 拔出下列跳开关，设置安全夹并挂上警告牌：Open, safety/lock and tag this (these) circuit breaker(s):PANEL DESIGNATION FIN LOCATION SEE NOTES721VU GCU 1 4XU1 10 Q721VU GCU 2 4XU2 11 Q721VU GCU 2 4XU2 06 N注释：取决于飞机实际构型，跳开关的位置可能不同。NOTE: Depending on the aircraft configuration, circuit breaker(s) can have different locations.C. 步骤/PROCEDURE(1) 改装左侧吊架馈线Modify the feeders routing LH pylon(a) 为了方便接近，参考Fig. A-FBEAA Sheet 01，拆除：For better access, refer to Fig. A-FBEAA Sheet 01, remove:1 Duct Item (50) Retainand2 Clamps Item (51) Retain在断开的管路上安装防护盖。Put blanking plugs on the disconnected line ends.(b) 参考Fig. A-FBAAC Sheet 01, Fig. A-FBAAC Sheet 02, Fig. A-FBAAC Sheet 03, Fig. A-FBAAC Sheet 04, Fig. A-FBAAC Sheet 05 and Fig. A-FBAAC Sheet 06，改装馈线布线。Modify the feeder routing, refer to Fig. A-FBAAC Sheet 01, Fig. A-FBAAC Sheet 02, Fig. A-FBAAC Sheet 03, Fig. A-FBAAC Sheet 04, Fig. A-FBAAC Sheet 05 and Fig. A-FBAAC Sheet 06(c) 在3855VT，拆下保险丝和保护盖。On 3855VT, remove the lockwire and the cover protective.(d) 在3855VT，参考AWL断开导线On 3855VT, disconnect wires as per Aircraft Wiring List (AWL).(e) 从3855VC上脱开3855VCA。Disconnect 3855VCA from 3855VC.(f) 在断开的电插头上安装保护盖。Put a blanking cap on the disconnected electrical connector(g) 拆下/Remove:1 Clamp Item (12) Discard1 Spacer Cable Item (1) Discard和相关衬套/and associated bushings7 Bushing Item (44) Discard(h) 拆下/Remove:1 Support fairlead Item (3) Discard(i) 拆下/Remove:1 Plate Item (40) Discard(j) 临时，在旧板子item (40)相同的位置，放置新板子item (40)，对好定位孔。Temporarily, at the same position than the old plate item (40), put in position the new plate item 40 in accordance with the positioning hole.注释：注意从吊架结构到板item 40边缘孔的必须是埋头孔。NOTE: Be careful at the edge marging with the holes which must to be counterdrilled from the pylon structure to the plate item 40.(k) 参考SRM 51-44-00，给板item 40钻另外三个孔，匹配吊架结构上的孔。Drill the three other holes on the plate item 40 to match the holes of the pylon structure in accordance with SRM 51-44-00.(l) 给板item 40去毛刺。Remove and deburr the plate item 40.(m) 使用以下清洁剂按需清洁相关区域：Clean the area with:Non Aqueous Cleaner-General CML11-026 As required(n) 按需使用CML16-024填涂防护涂层，参考SRM 51-75-12Renew the protective finish in accordance with SRM 51-75-12Primer Paint- - Composite Structure CML16-024 As required(o)安装/Install:1 Plate F5493072020095 Item 40with4 Rivet NSA5415N32-15 Item 36按需填涂CML09-005Do the installation of the parts with:Polysulfide Sealant-General Purpose Interfay - CML09-005 As required(p) 在板item 40上，安装：On plate item 40, install:1 Bracket,Cable Support ABS0679-01 Item 10with2 Nut NSA5050-3 Item 62 Screw NAS1801-3-8 Item 172 Washer NAS1149C0332R Item 19(q) 在支架线束支撑item 10上，放置：On Bracket,Cable Support item 10, put in position:2 Support-Cable ABS0678B01 Item 1(r) 参考Fig. AFBAAC Sheet 03, Fig. A-FBAAC Sheet 04 and Fig. A-FBAAC Sheet 05，安装馈线和激励线到支撑结构item 1.Thru Support-Cable item 1, install feeders and excitation wires as shown on Fig. AFBAACSheet 03, Fig. A-FBAAC Sheet 04 and Fig. A-FBAAC Sheet 05(s) 在支架，线束支撑item 10，使用卡子固定线束支撑结构item1：On Bracket