WOHA33_1165153_338_EOA33-53-0012

Hong Kong Airlines Limited香港航空03110-01Hong Kong Airlines MEDHong Kong Airlines LimitedWO NO/工作指令號(hào)SEQ NO/序列號(hào)WOHA331165_338_1531165153TitleFuselage-NLG Bay upper Panel Inspection for Possible Interference between Fastener Thread and Stringer Y=0Mcd&Rev/廠家工卡&修訂日期標(biāo)題機(jī)身-前起落架艙上部蓋板緊固件的螺紋和桁條Y=0之間的干涉檢查A/C/飛機(jī)號(hào)/組別EO JC No./EO工卡EO JC Rev/工卡版本W(wǎng)orkarea/工作區(qū)域Skill/工種Man Hour/工時(shí)BLNK/1EOA33-53-0012R00機(jī)身/AirframeAIRP04:15Baseline/依據(jù)Operator EO/營運(yùn)人EOEO Rev/EO版本W(wǎng)ork Type/工作類別Threshold/首檢Interval/重復(fù)檢SB A330-53-3221R00EOA33-HKG53-0008R00Written/編寫Reviewed/審核Approved/批準(zhǔn)2014-01-282014-01-292014-01-29Accomplished完工簽署Complete Date完工日期Station維修站SHAREASON & DESCRIPTION/原因及描述空客接到關(guān)于15A隔框處的前起落架盒內(nèi)部的螺釘和內(nèi)部頭頂蓋板Y=0處肋相磨損的報(bào)告。損傷的原因是由于1030VB安裝機(jī)構(gòu)的連接螺釘過長造成。完成該EO可盡早發(fā)現(xiàn)可能存在的損傷和避免更重大的修理。In the Nose Landing Gear box at frame 15A, some cases of contact between a screw (mechanical installation of the 1030VB) and the rib at Y=0 of the overhead panel of the landing gear box were reported. The damage is due to too long screw attaching the mechanical installation of the 1030VB.Accomplishment of EO will allow early detection of possible damage on the rib at Y=0 of the overhead panel of the Landing gear box and thus avoid a more important repair.TOOLS/工具TOOLS NECESSARY/必須工具ITEM項(xiàng)目P/N件號(hào)DESCRIPTION名稱EQTP類型QTY數(shù)量APP適用性Conditions note互換信息及備注TOOLS IF NECESSARY/視情工具ITEM項(xiàng)目P/N件號(hào)DESCRIPTION名稱EQTP類型QTY數(shù)量APP適用性Conditions note互換信息及備注PARTS AND MATERIAL/航材NOTE:OPERATOR MUST GET AND INSTALL THE PARTS THAT CORRESPOND TO THE RELATIVE WORKORDER NO.注釋：請(qǐng)工作者嚴(yán)格按照工作指令號(hào)領(lǐng)取預(yù)定的航材裝機(jī)PARTS AND MATERIAL NECESSARY/必須航材ITEM項(xiàng)目P/N件號(hào)DESCRIPTION名稱EQTP類型QTY數(shù)量APP適用性Conditions note互換信息及備注PARTS AND MATERIALIF NECESSARY/視情航材ITEM項(xiàng)目P/N件號(hào)DESCRIPTION名稱EQTP類型QTY數(shù)量APP適用性Conditions note互換信息及備注1NAS1096-3-16SCREWAS1ALL視情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 * 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 * AMECO Approval No.: JMM001,D101131* Other: * Signature:_ Authorization No.:_ Date:_工卡Job card:EOA33-53-0012TITLEFuselage-NLG Bay upper Panel Inspection for Possible Interference between Fastener Thread and Stringer Y=0PerfInsp標(biāo)題機(jī)身-前起落架艙上部蓋板緊固件的螺紋和桁條Y=0之間的干涉檢查工作者檢查者警 告：確認(rèn)遵守所參考手冊的所有警告和注意事項(xiàng)。WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES.注 意：遵守使線束和設(shè)備處于良好狀態(tài)的警示信息。當(dāng)執(zhí)行設(shè)備維護(hù)、修理及改裝時(shí)，盡可能地保持線束、電氣設(shè)備及工組區(qū)域的潔凈，執(zhí)行下述要求：使用如塑料布、布匹等鋪蓋在上述設(shè)備上；經(jīng)常性的去除線束、電氣設(shè)備上的雜物及其他污染物。可減少安裝電線時(shí)的污染和損傷。若污染,參照ESPM20-55-00處理。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; ASNECESSARY 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.IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.注釋：本EO的工作步驟中涉及其他文件時(shí)，如果使用的是“參照”字樣且有其他可接受的替代方法時(shí)，該替代方法可以被使用；如果使用的是“按照”字樣時(shí)，工作者必須使用AIRBUS指定文件中的工作步驟。NOTE: The accomplishment instructions of this EO refer to procedures included in other AIRBUS documents. When the words refer to are used and the operator has an accepted alternative procedure, the accepted alternative procedure can be used. When the words in accordance with are included in the instruction, the procedure in the AIRBUS document must be used.A. 通用信息/GENERAL(1) 工卡533221-910-001-001-標(biāo)準(zhǔn)施工Subtask 533221-910-001-001 - Standard Practices(a) 區(qū)域識(shí)別，參考AMM 06-20-00, Page Block 001 和 Manual Front Matter, Zone List。For the identification of zones, refer to AMM 06-20-00, Page Block 001 and Manual Front Matter, Zone List.(b) 獲取標(biāo)準(zhǔn)螺紋緊固件的力矩值，參考AMM Task20-21-11-911-801。To torque tighten the standard threaded fasteners refer to AMM Task 20-21-11-911-801.(c) 拆除和安裝緊固件，參考SRM 51-42-00。For the removal and installation of fasteners refer to SRM 51-42-00.(d) 恢復(fù)漆層，按照SRM 51-75-12。Renew the protective finish in accordance with SRM 51-75-12.(e) 獲取替換的緊固件，參考SRM 51-43-00。For alternative and substitute fasteners refer to SRM 51-43-00.B. 準(zhǔn)備/PREPARATION(2) 工卡533221-941-001-001-工作開始Subtask 533221-941-001-001 - Job Set-up(a) 在執(zhí)行維護(hù)前飛機(jī)應(yīng)處于以下基本狀態(tài)下：The following items shall be considered as the basic Aircraft configuration before you start a maintenance task:- 飛機(jī)在地面上以起落架靜止支撐（地面安全鎖和輪檔在起落架上安裝到位）。Aircraft on the ground resting on landing gear (the ground safety locks and the wheel chocks are in position on the landing gear).- 發(fā)動(dòng)機(jī)關(guān)車，反推關(guān)閉并鎖上。Engine shut down, thrust reversers closed and locked.- 飛機(jī)處于干凈的構(gòu)型。Aircraft in clean configuration.- 飛機(jī)處于停留剎車應(yīng)用狀態(tài)。Parking brake applied.- 飛機(jī)電源斷開。Aircraft electrical network de-energized.- 液壓系統(tǒng)處于釋壓狀態(tài)。Hydraulic systems depressurized.- 可接近駕駛艙和客艙。Access to the cockpit and cabin is available.- 所有的跳開關(guān)處于關(guān)閉狀態(tài)。All circuit breakers are in closed position.- 所有的控制處于正常、自動(dòng)或者關(guān)閉狀態(tài)。All controls in NORM, AUTO or OFF position.(b) 確保飛機(jī)接地，參考AMM Task 12-34-24-860-802。Make sure that the aircraft is electrically grounded, refer to AMM Task 12-34-24-860-802.(c) 參考AMM Task 32-22-00-010-801打開前起落架艙門Open the NLG doors, refer to AMM Task 32-22-00-010-801.(d) 在123 和124區(qū)域放置接近工作梯。Put access platform(s) in position at zones 123 and 124.C.施工步驟 PROCEDURE(1) 工卡543034-010-002-001-詳細(xì)檢查緊固件螺紋和長桁Y=0之間的間隙。Subtask 533221-832-001-001 - Do a Detailed Inspection of the Gap between the Fastener Thread and the Stringer at Y=0. (a) 詳細(xì)檢查緊固件螺紋和長桁Y=0之間可能存在的干涉。參考Fig. A-FBAAA Sheet 01,Fig. A-FBAAA Sheet 02 and Fig. A-FFAAA Sheet 01。Do a detailed inspection of a possible interference between fastener thread and stringer Y=0.Refer to Fig. A-FBAAA Sheet 01,.Fig. A-FBAAA Sheet 02 and.Fig. A-FFAAA Sheet 01.1 間隙檢查。Do the inspection of the gap.a 如果間隙大于0 mm (0in):If the gap is greater than 0 mm (0 in): 無需進(jìn)一步的工作。No further action.b 如果間隙不大于0 mm (0 in):If the gap is not greater than 0 mm (0 in): 在下次起飛前執(zhí)行步驟（2）工卡533221-833-001-001。Do step (2) SUBTASK 533221-833-001-001 before next flight.(b)發(fā)送檢查報(bào)告Figure A-FRAAA - Sheet 01到S 和 。Send Inspection Report Figure A-FRAAA - Sheet 01 to S and .(2) 工卡533221-833-001-001- 根據(jù)檢查結(jié)果，更換螺釘和執(zhí)行長桁Y=0的損傷去除工作。Subtask 533221-833-001-001- Depending on the inspection results, replace the Screw and Do the Rework of the Stringer at Y=0.(a) 拆除盒子1030VB和和板，根據(jù)SRM 51-42-00。Remove the box 1030VB and the plate: In accordance with SRM 51-42-00.1 參考Fig. A-FBCAA Sheet 01拆除盒子。Remove the box:Refer to Fig. A-FBCAA Sheet 012 參考Fig. A-FBBAA Sheet 01 和 Fig. A-FBBAA Sheet 02拆除螺釘。Remove the screw: Refer to Fig. A-FBBAA Sheet 01 and Fig. A-FBBAA Sheet 02.3 參考Fig. A-FBCAA Sheet 01拆除板。Remove the plate: Refer to Fig. A-FBCAA Sheet 01.(b)在下次起飛前，參考Fig. A-FFAAA Sheet 01 執(zhí)行長桁Y=0的損傷去除工作。Do the rework of the stringer at Y=0 before next flight. Refer to Fig. A-FFAAA Sheet 01.1 參考Fig. A-FABAA檢查損傷深度。Check the damage depth.Refer to Fig. A-FABAA.a 如果損傷深度小于1 mm (0.039 in)。If the damage depth is lower than 1 mm (0.039 in): 在下次起飛前，按照Fig. A-FABAA執(zhí)行長桁的損傷去除工作。Rework the stringer in accordance with Fig. A-FABAA before next flight. 在下次起飛前，按照SRM 51-75-12恢復(fù)漆層。Renew the protective finish in accordance with SRM 51-75-12 before next flight.無需進(jìn)一步的工作。No further action.b 如果損傷深度大于或等于1 mm (0.039 in)：If the damage depth is not lower than 1 mm (0.039 in): 在下次起飛前，聯(lián)系結(jié)構(gòu)工程師。Contact structure engineer before next flight.(c)在下個(gè)起飛前安裝1030VB盒子和板，參考AMM Task 20-21-11-911-801，按照SRM 51-42-00和SRM 51-43-00。Install the box 1030VB and the plate before next flight:Refer to AMM Task 20-21-11-911-801,In accordance with SRM 51-42-00 and SRM 51-43-00.1 參考Fig. A-FBCAA Sheet 01安裝板。Install the plate:Refer to Fig. A-FBCAA Sheet 01.2 參考Fig. A-FBBAA Sheet 01和Fig. A-FBBAA Sheet 02安裝螺釘。Install the screw:Refer to Fig. A-FBBAA Sheet 01 and Fig. A-FBBAA Sheet 02.3參考Fig. A-FBCAA Sheet 01安裝盒子。Install the box: Refer to Fig. A-FBCAA Sheet 01.4 發(fā)送檢查報(bào)告Figure A-FRAAA - Sheet 01到S 和 。Send Inspection Report Figure A-FRAAA - Sheet 01 to S and .D.測試 TEST無/NoneE.收尾 CLOSE-UP(1) 工卡533221-942-001-001-收尾Subtask 533221-942-001-001 - Close-up(a) 確認(rèn)工作區(qū)域清潔，無工具和其它設(shè)備。Make sure that the work areas are clean and clear of tools and other items of equipment.(b) 挪開工作梯。Remove the access platform(s).(c) 關(guān)閉前起落架艙門，參考AMM Task 32-22-00-410-801。Close the NLG doors, refer