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 ALL  ú ú N01 Page 202 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 | 16| 5 | O.O | +0.01 | | | | | | | | -0.03 | | | ................................................................................. | ALL | 17| 6 | P.P | +0.02 | | | | | | | | .0.02 | | | ................................................................................. | ALL | 18| 6 | S-S | 0.09 | | | | | | | | 0.03 | | | ................................................................................. | ALL | 19| 6 | S.S | +0.02 | | | | | | | | -0.02 | | | ................................................................................. | ALL | 20| 6 | T.T | 0.40 | | | | | | | | 0.25 | | | ................................................................................. | ALL | 21| 6 | T.T | 0.37 | | | | | | | | 0.25 | | | ................................................................................. | ALL | 22| 6 | T.T | 0.18 | | | | | | | | 0.02 | | | ................................................................................. | ALL | 23| 6 | T.T | 0.26 | 0.20 | | | | | | | 0.17 | | | ................................................................................. | ALL | 24| 6 | U.U | +0.120 | 0.060| | | | | | | -0.120 | | | ................................................................................. | ALL | 25| 7 | V.V | 0.16 | | | | | | | | 0.04 | | | ................................................................................. | ALL | 26| 7 | W.W | 0.16 | | | .................................................................................
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 71-11-00
 ALL  ú ú N01 Page 203 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 | 27| 7 | X.X | 0.32 | 0.30 | | | | | | | 0.19 | | | ................................................................................. | ALL | 28| 7 | X.X | +0.08 | 0.04 | | | | | | | -0.08 | | | ................................................................................. | ALL | 29| 7 | Y.Y | 0.40 | 0.280| | | | | | | 0.16 | | | ................................................................................. | ALL | 30| 7 | Y.Y | 0.30 | | | | | | | | 0.08 | | | ................................................................................. | ALL | 31| 7 | Y.Y | 0.24 | | | | | | | | 0.07 | | | ................................................................................. | ALL | 32| 7 | Z.Z | 0.30 | 0.240| | | | | | | 0.06 | | | ................................................................................. | ALL | 33| 7 | Z.Z | 0.30 | 0.240| | | | | | | 0.06 | | | ................................................................................. | ALL | 34| 7 | AA.AA| 0.30 | 0.240| | | | | | | 0.06 | | | ................................................................................. | ALL | 35| 7 | AA-AA| 0.30 | 0.240| | | | | | | 0.06 | | | .................................................................................
 | ALL | 36| 8 | AB.AB|  +0.140  | 0.100| A +0.080 step is permitted at  |
 |  |  |  |  |  -0.140  |  | the leading edge of the skirt  |
 |  |  |  |  |  |  | fairing.  The step may change  |
 |  |  |  |  |  |  | aft of the leading edge by  |
 |  |  |  |  |  |  | +0.120.  The wave length of this|
 |  |  |  |  |  |  | change must agree with the  |
　
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