taa32-gcr32008r5關(guān)于五架飛機(jī)主輪及剎車轂檢查以及更換說明

1、表格編碼：F-EPM-19-01TJA MEDTA NO.REVI版次EFFECT DATE生效日期PREPARED編寫REVIEWED審核APPROVED批準(zhǔn)PAGE頁碼OF總頁TAA32-GCR32-008R52014-11-1413SUBJECT:The Instruction of inspection and replacement related to the main wheels and brakes ofB-1849，B-1850，B-1851，B-1618，B-1619 aircrafts題目:關(guān)于 B-1849，B-1850，B-1851, B-1618,B-1619 五

2、架飛機(jī)主輪及剎車轂檢查以及更換說明分類/CAT.：CAD/AD Operation/Maenance Information/使用和信息 Part Information/Maenance/Dispatch Standard/和放行標(biāo)準(zhǔn) Others/其它信息信息本通告適用機(jī)型/Applicable A/C Type: A320本通告適用飛機(jī)/Applicable A/C Tail Number：B-1849，B-1850，B-1851，B-1618，B-1619參考資料/Reference：AMM 32-42-27，AMM 32-41-11，IPC 32-41-01-01K,IPC 32-4

3、2-05-01D原因/Reason For Revi：因 B-1851 飛機(jī)完成機(jī)輪剎車改裝，R1 版修改了 B-1851 飛機(jī)主輪/剎車檢查以及更換標(biāo)準(zhǔn)R1 REVISES INSPECTION AND REPLACEMENT STANDARD OF B-1851 A/C DUE TO EMBODIMENT OF WHEEL/BRAKE MOD.R2 版以加入新飛機(jī) B-1618R2 VERREVISING FOR THE NEW AIRCRAFT B-1618因 B-1850 飛機(jī)完成機(jī)輪剎車改裝，R3 版修改了 B-1850 飛機(jī)主輪/剎車檢查以及更換標(biāo)準(zhǔn)R3 REVISES INSPE

4、CTION AND REPLACEMENT STANDARD OF B-1850 A/C DUE TO EMBODIMENT OF WHEEL/BRAKE MOD.因 B-1849 飛機(jī)完成機(jī)輪剎車改裝，R4 版修改了 B-1849 飛機(jī)主輪/剎車檢查以及更換標(biāo)準(zhǔn)R4 REVISES INSPECTION AND REPLACEMENT STANDARD OF B-1849 A/C DUE TO EMBODIMENT OF WHEEL/BRAKE MOD.R5 版以加入新飛機(jī) B-1619R5 VERREVISING FOR THE NEW AIRCRAFT B-1619以前相關(guān)通告處理/Di

5、sal Of Previous TA：TAA32-GCR32-008 R5 生效的同時(shí)R4 版。TAA32-GCR32-008 R5 supersedes TAA32-GCR32-008 R4.背景/Background：B-1618，B-1619 飛機(jī)選用了 GOODRICH 的主輪以及剎車轂，其他飛機(jī)（B-1851,B-1850,B-1849 飛機(jī)已完成改裝工作）選用的為 MESSIER 的主輪以及剎車轂，工程將安排工作 改為 MESSIER 構(gòu)型。在改裝工作未全部完成，同時(shí)空客手冊(cè)未完成 前，為提示工作者日常 的注意事項(xiàng)，特下發(fā)此 TA 予以說明。Distribution To:本 TA

6、 發(fā)送至：采購部市場(chǎng)銷售部各中心/分部/飛行部/Flight Department安全監(jiān)察部各機(jī)型過站外站運(yùn)行控制部服務(wù)部TJA MEDSUBJECT:The Instruction of inspection and replacement related to the main wheels and brakes of B-1849，B-1850，B-1851，B-1618 ，B-1619aircraftsPAGE頁數(shù)OF總頁題目:關(guān)于 B-1849，B-1850，B-1851，B-1618，B-1619 五架飛機(jī)主輪及剎車轂檢查以及更換說明23The configuration of t

7、he main wheels and brakes of B-1618，B-1619 aircrafts is GOODRICH,Which is not identical with our Fleet（B-1850，B-1851 ,B-1849 had embodied）,The engineering department will arrange the modification work to unify the configuration.I e this TA is to promote the daily work attention fot the worker before

8、 the embodiment and the manuals revised.正文/Content：一:對(duì)于 B-1618,B-1619 飛機(jī)， 改裝未完成前，日常 的注意事項(xiàng)。更換：B-1618，B-1619 飛機(jī)主輪和剎車在改裝前與A320 機(jī)隊(duì)構(gòu)型不一致，當(dāng)更換 B-1618，B-1619 飛機(jī)主輪或者剎車轂時(shí)，請(qǐng)以這架飛機(jī)手冊(cè)內(nèi)容為準(zhǔn)，選用 GOODRICH 構(gòu)型主輪或者剎車轂。檢查標(biāo)準(zhǔn)：GOODRICH 主輪和 MESSIER 主輪檢查標(biāo)準(zhǔn)一致，標(biāo)準(zhǔn)參考 TAA32-GCR32-003。對(duì)于件號(hào)為 2-1684 的 GOODRICH 剎車轂，確認(rèn)裝機(jī)的新剎車轂指示銷長度在 52.6

9、 mm (2.07 in.) 到54.1 mm (2.13 in.)之間，如裝機(jī)件指示銷長度大于標(biāo)準(zhǔn)最大值，更換此件，其他檢查標(biāo)準(zhǔn)與 MESSIER 剎車轂相同。具體標(biāo)準(zhǔn)依據(jù) TAA32-GCR32-002。注: 當(dāng)前適用于 B-1618，B-1619 飛機(jī)主輪件號(hào)為 3-1530，剎車轂件號(hào)為：2-1684。二：B-1850，B-1851,B-1849 飛機(jī)已完成改裝，由 GOODRICH 構(gòu)型變?yōu)?MESSIER 構(gòu)型，由于空客還未 手冊(cè)，所以 B-1850，B-1851，B-1849 飛機(jī)手冊(cè)中關(guān)于主輪以及剎車相關(guān)信息不再適用于飛機(jī)當(dāng)前構(gòu)型。在更換 B-1850，B-1851，B-184

10、9 飛機(jī)主輪以及剎車相關(guān) 時(shí)，請(qǐng)選用 MESSIER 構(gòu)型主輪以及剎車轂，具體更換程序以及 信息請(qǐng)以適用 B-9948 飛機(jī) 冊(cè)為準(zhǔn)。主輪檢查更換標(biāo)準(zhǔn)請(qǐng)參考 TAA32-GCR32-003，剎車檢查以及更換標(biāo)準(zhǔn)請(qǐng)參考 TAA32-GCR32-002.1：The daily ma anance attention before embodiment for B-1618，B-1619.A. Replace component:The main wheels and brakes of B-1618，B-1619 are GOODRICH products which are not identi

11、cal with oth lanes of TJA A320 fleet.Please refer to the manuals contents related with GOODRI ain wheels and breaks when replacing the main wheels and brakes of B-1618，B-1619.TJA MEDSUBJECT:The Instruction of inspection and replacement related to the main wheels and brakes of B-1849，B-1850，B-1851，B-

12、1618,B-1619 aircraftsPAGE頁數(shù)OF總頁題目:關(guān)于 B-1849，B-1850，B-1851, B-1618，B-1619 五架飛機(jī)主輪及剎車轂檢查以及更換說明33B. Standard of inspection:The inspect standard of main wheels betn GOODRICH and MESSIER is identical with our fleet,details see TAA32-GCR32-003.FOODRICH BRAKES, P/N 2-1684: the distance of the new brake assy

13、 indicator should be betn52.6 mm (2.07 in.) and 54.1 mm (2.13 in.).If the distance is moren theum value， replace the brake assy .For detailed inspection and replacement standard please refer to TAA32-GCR32-002. NOTE: for B-1618 ,B-1619 aircrafts ,the applicable main wheel part number is 3-1530,brake

14、 is2-16842：B-1850，B-1851,B-1849 had embodied the wheel/brake MOD,changing GOODRICH configuration to MESSIER configuration.As the related manuals are not revised ime,the manuals related about the main wheels and brake assy of B-1850，B-1851,B-1849 are not applicable for the current configuration . Ple

15、ase choose MESSIER configuration main wheel and brake assy when replacing the main wheel and brake assy ofB-1850，B-1851,B-1849 aircrafts.For detailed replacment and installation procedure and components information ， please refer to manuals which are applicable for B-9948 aircraft ； please refer to TAA32-GCR32-003 for the standard of inspection and replacing of main wheel，TAA32-GCR32