taa32-gcr25020r2關(guān)于機(jī)型翼上應(yīng)急出口處座椅靠背向后斜倚調(diào)節(jié)構(gòu)型說明

1、編碼：F-EPM-19-01TJA MED航空公司維修工程部TECHNICAL ADVISORY技術(shù)通告PAGE頁碼OF總頁/13本 TA 發(fā)送至：HNAT:質(zhì)量管理部 維修控制部 技術(shù)服務(wù)部 培訓(xùn)管理部 中南維修華北維修西北維修云南維修重慶維修維修GCR:服務(wù)部 工程部其他:GCAMSUBJECT：Configuration Explanation for Backrest Recline Operation adjacent to Overwing Exit in A319/320 fleet題目：關(guān)于 A319/320 機(jī)型翼上應(yīng)急出口處座椅靠背“（向后）斜倚調(diào)節(jié)”構(gòu)型說明分類/CAT.

2、：CAD/A使用和信和放行標(biāo)準(zhǔn) 信息 其它信息D息DESCRIPTION：內(nèi)容：本通告適用機(jī)型 Aircraft M:A32本通告適用飛機(jī) Applicability:ALL參考資料 References:EASA TCDS No.EASA.A.064, LOPA DWG NO. 319-25-11293,320-25.35052,319-25.21637,32025.28672, 320-25.34952 HNATMDA1302-03-01, 10 D252 78056, ERT/ 334-201原因 Reason of Revi :由于原 R0 版“表二：A319/320 機(jī)隊?wèi)?yīng)急出口處座

3、椅靠背（向后）斜倚調(diào)節(jié)構(gòu)型 ”的信息被整合到了海航技術(shù)工程網(wǎng)的 “飛機(jī)構(gòu)型差異 ，因此 R1 刪除“表二：A319/320 機(jī)隊?wèi)?yīng)急出口處座椅靠背（向后）斜倚調(diào)節(jié)構(gòu)型 ”的信息。 Because table two “backrest recline configuation difference list” has been egrated o “Aircraft Configuration Information”platform,we delete the table two his R1 revi .由于海技工程網(wǎng) ，R2 修改正文附圖。R2 revised the figures A

4、 due to w ge changed.以前相關(guān)通告處理 Relation of TAs revi s:R2 版本完全替代 R1 版，R2 版生效后，終止 R1 版。This R2 fully supercedes R1,and terminates R1 after R2 is effective.背景/Background：A319/320 內(nèi)機(jī)隊，部分飛機(jī)應(yīng)急出口處的旅客座椅靠背可（向后）斜倚調(diào)節(jié)，給一線 帶來困擾。為了方便一線 判斷 A319/320 機(jī)隊?wèi)?yīng)急出口處的座椅靠背是否為“（向后）斜倚調(diào)節(jié)”構(gòu)型，特下發(fā)本 TA 進(jìn)行說明。The backrest recline can b

5、e operated in some PAX seat adjacent to overwing exit in some A319/320 aircraft，t bring some confufor some maenanceel. This TA is ied to explahe configuration for backrest recline operation adjacent to overwing exit.正文/Text：旅客座位布局圖（Layout of Passengermodations 縮寫：LOPA）是對于客艙旅客座椅分布、安裝非常重要的 工程圖紙。A319/3

6、20 飛機(jī)應(yīng)急出口處旅客座椅靠背是否可調(diào)節(jié)，通常在 LOPA 圖上可以找到依據(jù)信息。LOPA 圖上常見表示座椅靠背限制信息的子母代碼如下表一（不僅限于表中所列，詳細(xì)可參見相應(yīng) LOPA 圖紙）。一線 可通過LOPA圖上信息和相應(yīng)旅客座椅 CMM，確認(rèn)座椅靠背調(diào)節(jié)是否為“（向后）斜倚調(diào)節(jié)”構(gòu)型。LOPA is a very important drawing regarding PAX seat arrangement and installation in cabin. Generally,we are ableTA NO.通告REVI版次EFFECT DATE生效日期PREPARED編寫RE

7、VIEWED審核APPROVED批準(zhǔn)TAA32-GCR25-02022016-08-19PAGE頁碼OF總頁2/3SUBJECT：Configuration Explanation for Backrest Recline Operation adjacent to Overwing Exit in A319/320 fleet題目：關(guān)于 A319/320 機(jī)型翼上應(yīng)急出口處座椅靠背“（向后）斜倚調(diào)節(jié)”構(gòu)型說明to confirm if the backrest recline of PAX seat adjacent to overwing exit can be operated or n

8、ot in accordance with the effective LOPA drawing. The abbreviation letters indicate the PAX seat backrest operated limi ion information shown in LOPA drawing able one.Ma enaceel can verify the backrest limi ion information via effective LOPA drawing and CMM.表一/Table One為了便于一線 了解“A319/320 機(jī)隊?wèi)?yīng)急出口處座椅靠背

9、“（向后）斜倚調(diào)節(jié)”構(gòu)型差異，在核查 A319/320 飛機(jī)型號型號審定數(shù)據(jù)單 EASA TCDS No.EASA.A.064 和改裝設(shè)計審定基礎(chǔ)（針對運(yùn)營中的布局改裝）相關(guān)文件基礎(chǔ)上，以當(dāng)前有效 LOPA 圖和 CMM 為依據(jù)，編制了“A319/320 機(jī)隊?wèi)?yīng)急出口處座椅靠背“（向后）斜倚調(diào)節(jié)”構(gòu)型 ”（注：此在 TA R01 版生效后，已終止）。In order to facili e ma enaceel to know recline configuration differen for the PAX seat adjacent to overwing exit in A319/32

10、0 fleet. We make a backrest recline configuation difference list shown able two after verification of EASA TCDS No.EASA.A.064 and modification designbasis (for layout modification during operation) relevants and in accordance with the effective LOPA drawing and CMM (Note:This list is terminated afte

11、r TA R01 revi ).原 TA R00 版“表二：A319/320 機(jī)隊?wèi)?yīng)急出口處座椅靠背（向后）斜倚調(diào)節(jié)構(gòu)型”的信息被整合到了海航技術(shù)工程，一線可通過“飛機(jī)構(gòu)型差異了解 A319/320 機(jī)隊?wèi)?yīng)急出口處座椅靠背（向后）斜倚調(diào)節(jié)構(gòu)型信息。（ 路徑： 海航技術(shù)工程網(wǎng)維修工程飛機(jī)構(gòu)型差異信息，如附圖 1/2 所示）。Because table two “backrest recline configuation difference list” in R00 has been egrated o “Aircraft Configuration Information”platform.M

12、a enanceel can get the recline configuration information from the platform.(Ac s route：HNAT ranetMa enance EngineeringAircraft Configuration Information.shown in figure 1/2).在涉及客艙旅客座椅拆裝工作時，一線 需嚴(yán)格按照有效 LOPA 圖信息并參考 AMM25-22-00 要求，重新安裝 旅客座椅。對于翼上應(yīng)急出口處的旅客座椅，依據(jù)有效 LOPA 及座椅 CMM 信息或參考飛機(jī)構(gòu)型差異信息（如附圖 1/2 所示），確定座椅

13、靠背“（向后）斜倚調(diào)節(jié)”構(gòu)型，確保旅客座椅靠背“（向后）斜倚調(diào)節(jié)符合符合原適航審定要求。Duringplishment of removal/installation task, ma enanceel must strictly re-install PAX seat in accordance with effective LOPA and AMM25-22-00.Ma enanceel ensure t the backrest recline configuration of PAX seat adjacent to overwing exit in accordance with e

14、ffective LOPA and CMM or refer to aircraft configuration information, and make sure the recline configuration meet the existing requirements.受影響的相關(guān)手冊/Affected Manual: N/A受影響的相關(guān)工卡/Affected Task Card: N/A網(wǎng)的“飛機(jī)構(gòu)型差異AbbrRBNO RECLINE AND NO BREAK OVER 不可（向后）斜倚調(diào)節(jié)且不可（向前）轉(zhuǎn)折LNNO BREAK OVER AND LIMITED RECLINE有限（向后）斜倚調(diào)節(jié)且不可（向前）轉(zhuǎn)折NBNO BREAK OVER不可（向前）轉(zhuǎn)折LRLIMITED RECLINE有限（向后）斜倚調(diào)節(jié)NRNO RECLINE不可（向后）斜倚調(diào)節(jié)注意：本表信息縮寫代碼/英文全稱為通用參考信息，以方便一線理解其中含義，請以有效LOPA 圖信息說明為準(zhǔn)。縮