71-11-00
ALL ú ú N02 Page 208 ú Oct 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
~...........-...-....-......-..........-......-................................. | TABLE 201 | ................................................................................. | AIRPLANE |REF|FIG.| VIEW | LIMITS | AVG. | LIMIT DEVIATIONS | |EFFECTIVITY|NO.|201 | | | MAX | | ................................................................................. | ALL | 85| 14 | BE.BE| 0.80 | | | ................................................................................. | ALL | 86| 14 | BE.BE| 3.75 | | | ................................................................................. | ALL | 87| 14 | BF.BF| +0.120 | 0.065| | | | | | | -0.120 | | | ................................................................................. | ALL | 88| 15 | BG.BG| +0.080 | 0.057| | | | | | | -0.080 | | | ................................................................................. | ALL | 89| 15 | BH.BH| 0.125 | | | ................................................................................. | ALL | 90| 15 | BH.BH| 11.75 | | | ................................................................................. | ALL | 91| 15 | BH.BH| 1.00 | | | ................................................................................. | ALL | 92| 15 | BH.BH| 0.04 | | | ................................................................................. | ALL | 93| 15 | BI.BI| 0.18 | | | | | | | | 0.00 | | | ................................................................................. | ALL | 94| 15 | BI.BI| 0.15 | 0.125| | | | | | | 0.06 | | | ................................................................................. | ALL | 95| 15 | BI.BI| 0.06 | | | | | | | | 0.00 | | | ................................................................................. | ALL | 96| 15 | BI.BI| 0.18 | | | | | | | | 0.00 | | | ................................................................................. | ALL | 97| 15 | BI.BI| 0.25 | | | | | | | | 0.10 | | | ................................................................................. | ALL | 98| 15 | BJ.BJ| +0.06 | | | | | | | | -0.06 | | | ................................................................................. | ALL | 99| 16 | BK.BK| 0.06 | | | | | | | | 0.02 | | | ................................................................................. | ALL |100| 16 | BL.BL| +0.030 | | | | | | | | -0.030 | | | ................................................................................. | ALL |101| 16 | BM.BM| +0.030 | | | | | | | | -0.030 | | | .................................................................................
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
71-11-00
ALL ú ú N02 Page 209 ú Oct 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
~...........-...-....-......-..........-......-................................. | TABLE 201 | ................................................................................. | AIRPLANE |REF|FIG.| VIEW | LIMITS | AVG. | LIMIT DEVIATIONS | |EFFECTIVITY|NO.|201 | | | MAX | | .................................................................................
| ALL |102| 16 | BN.BN|RADIUS: | | |
| | | | | 0.07 | | |
| | | | | 0.05 | | |
................................................................................. | ALL |103| 16 | BN.BN| 0.42 | 0.382| | | | | | | 0.18 | | | ................................................................................. | ALL |104| 16 | BN.BN| +0.090 | 0.040| | | | | | | -0.090 | | | ................................................................................. | ALL |105| 16 | BO-BO| +0.060 | | | | | | | | -0.060 | | | ................................................................................. | ALL |106| 16 | BP.BP| +0.030 | | | | | | | | -0.030 | | | ................................................................................. | ALL |107| 17 | BR.BR| 0.09 | 0.03 | | | | | | | 0.00 | | | ................................................................................. | ALL |108| 17 | BR.BR| 0.16 | 0.12 | | | | | | | 0.08 | | | ................................................................................. | ALL |109| 17 | BS.BS| +0.060 |+0.050| | | | | | | -0.060 | | | ................................................................................. | ALL |110| 17 | BS.BS| 0.15 | 0.12 | | | | | | | 0.00 | | | ................................................................................. | ALL |111| 17 | BT.BT| 0.18 | 0.12 | | | | | | | 0.06 | | | ................................................................................. | ALL |112| 17 | BT-BT| 0.135 | 0.075| | | | | | | 0.015 | | | ................................................................................. | ALL |113| 17 | BT.BT| 0.16 | 0.09 | | | | | | | 0.02 | | | ................................................................................. | ALL |114| 17 | BT.BT| 0.135 | 0.075| | | | | | | 0.015 | | | ................................................................................. | ALL |115| 17 | BT.BT| 0.18 | 0.12 | | | | | | | 0.06 | | | ................................................................................. 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：747-400 AMM 飞机维护手册 动力装置 POWER PLANT 2(55)
