.................................................................................
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
71-11-00
ALL ú ú N01 Page 204 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 | 37| 8 | AB.AB| 0.40 | 0.300| | | | | | | 0.10 | | | ................................................................................. | ALL | 38| 8 | AC.AC| 0.15 | | | | | | | | 0.05 | | | ................................................................................. | MAS 206 | 39| 8 | AD.AD| | | Measured from the cold nozzle | | | | | | | | location: | | | | | | | | Inboard strut -| | | | | | | | 0.71-0.89 at forward end | | | | | | | | 0.61-1.05 at aft end | | | | | | | | Outboard strut -| | | | | | | | 0.61-0.79 at forward end | | | | | | | | 0.51-0.71 at aft end | .................................................................................
| ALL EXCEPT| 39| 8 | AD.AD| | | Measured from the cold nozzle |
| MAS 206 | | | | | | location: |
| | | | | | | Inboard strut - |
| | | | | | | 0.71-0.89 at forward end |
| | | | | | | 0.61-0.79 at aft end |
| | | | | | | Outboard strut - |
| | | | | | | 0.61-0.79 at forward end |
| | | | | | | 0.51-0.69 at aft end |
................................................................................. | ALL | 40| 8 | AE.AE| +0.05 | 0.027| | | | | | | -0.09 | | | ................................................................................. | ALL | 41| 8 | AE.AE| 0.23 | 0.200| | | | | | | 0.11 | | | ................................................................................. | ALL | 42| 8 | AF.AF| +0.01 | | | | | | | | -0.04 | | | ................................................................................. | ALL | 43| 8 | AF.AF| 0.10 | 0.06 | | | | | | | 0.02 | | | ................................................................................. | ALL | 44| 9 | AH.AH| 0.15 | | | ................................................................................. | ALL | 45| 9 | AI.AI| 0.02 | | | | | | | | 0.00 | | | .................................................................................
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
71-11-00
ALL ú ú N08 Page 205 ú Oct 18/00
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 | 46| 9 | AK.AK| 0.09 | 0.06 | | | | | | | 0.03 | | | ................................................................................. | ALL | 47| 9 | AL.AL| 0.25 | 0.212| | | | | | | 0.06 | | | ................................................................................. | ALL | 48| 9 | AL.AL| +0.120 | 0.030| | | | | | | -0.120 | | | ................................................................................. | ALL | 49| 10 | AM.AM| 0.09 | 0.06 | | | | | | | 0.03 | | | ................................................................................. | ALL | 50| 10 | AM.AM| +0.03 | 0.00 | | | | | | | -0.03 | | | ................................................................................. | ALL | 51| 10 | AN.AN| 0.09 | | 0.09-0.18 on the aft edge of the| | | | | | 0.03 | | latch bolt only. | ................................................................................. | ALL | 52| 10 | AP.AP| +0.050 | 0.00 | | | | | | | -0.050 | | | ................................................................................. | ALL | 53| 10 | AQ.AQ| +0.03 | | | | | | | | -0.03 | | | ................................................................................. | ALL | 54| 10 | AQ.AQ| 0.09 | 0.06 | | | | | | | 0.03 | | | ................................................................................. | ALL | 55| 11 | AR.AR| 0.29 | 0.26 | | | | | | | 0.23 | | | ................................................................................. | ALL | 56| 11 | AR.AR| 0.12 | 0.10 | | | | | | | 0.08 | | | ................................................................................. | ALL | 57| 11 | AR.AR| 0.20 | | | | | | | | 0.01 | | | ................................................................................. | ALL | 58| 11 | AR.AR| 0.15 | | | | | | | | 0.03 | | | ................................................................................. | ALL | 59| 11 | AR.AR| 0.16 | 0.12 | | | | | | | 0.04 | | | ................................................................................. | ALL | 60| 11 | AR.AR| 0.12 | | | | | | | | 0.02 | | | .................................................................................
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