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时间:2011-04-17 09:22来源:蓝天飞行翻译 作者:航空
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

 ~.............................................................................. | Left Engine - No. 1 | | Table 202 | ................................................................................
 |   DOOR OR PANEL  |  |
 |  IDENTIFICATION  |  |
 |  NUMBER  |  RB211 ENGINE NACELLE STRUT  |
........... ..........  EQUIPMENT/COMPONENTS ACCESSIBLE THROUGH  |
 |  LEFT  |  RIGHT  |  ACCESS DOOR OR PANEL  |

 ................................................................................ | 431AL | | Hydraulics Fuel and Electronics Access| | 432AL | | Hydraulics Fuel and Electronics Access| | 433AL | | Nose Cowl Anti-Ice Duct, Starter Duct and Pressure| | | | Relief T/R Hydraulic Engine Controls| | 433BL | | Nose Cowl Anti-Ice Duct and High Pressure Duct Clamp,| | | | T/R Hydraulic Engine Controls| | 433CL | | Pre-Cooler, Thermal Switches, Fire Nozzle| | 433DL | | Hydraulics, Fuel and Electrical| | 433EL | | Hydraulics, Fuel and Electrical| | 433FL | | Outbd Strut-to-Wing Attach Pin| | | 433GR | Thrust Reverser Access and Pressure Relief Door| | | 433HR | High Pressure Duct, Intermediate Pressure Check| | | | Valve and Thermal Switch| | | 433JR | Pre-Cooler and Thermal Switch| | | 433KR | Hydraulics, Fuel and Electrical| | | 433LR | Pressure Regulating Valve and Pressure Relief| | | 433MR | Inbd Strut-to-Wing Attach Pin| | 434AL | | Hydraulics Installation| | 434BL | | Wing Fuel Tank| | 434CL | | Hydraulic and Fire Extinguishing Plumbing| | | 434DR | Wing Fuel Tank| 2.........….........…..........................................................1
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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 ALL  ú ú 01 Page 206 ú Sep 28/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

 ~.............................................................................. | Right Engine - No. 2 | | Table 203 | ................................................................................
 |   DOOR OR PANEL  |  |
 |  IDENTIFICATION  |  |
 |  NUMBER  |  RB211-535E4 ENGINE  |
........... EQUIPMENT/COMPONENTS ACCESSIBLE THROUGH..........  |
 |  LEFT  |  RIGHT  |  ACCESS DOOR OR PANEL  |

 ................................................................................ | 412AL | | P1 Probe| | 412BL | | TAI and Pressure Relief| | | 412BR | P1 Tube Bulkhead Connection| | 413AL | | Fan Cowl and Fancase| | 413BL | | Starter Air Valve| | 413CL | | IDG Oil Fill and Level Indicator| | | 414AR | Fan Cowl and Fancase| | | 414BR | Oil Filler and Pressure Relief| | | 414CR | Master Chip Detector| | 415AL | | Thrust Reverser Cowl| | 415BL | | Thrust Reverser Hydraulics and C-Duct Hinge| | 415CL | | Translating Cowl/Actuator Ram| | 415DL | | Translating Cowl/Actuator Ram| | 415EL | | Translating Cowl/Actuator Ram| | 415FL | | Thrust Reverser Access Panel| | 415GL | | Translating Cowl/Actuator Ram| | 415HL | | Translating Cowl/Actuator Ram| | 415JL | | Translating Cowl/Actuator Ram| | | 416AR | Thrust Reverser Cowl| | | 416BR | Thrust Reverser Hydraulics and C-Duct Hinge| | | 416CR | Translating Cowl/Actuator Ram| | | 416DR | Translating Cowl/Actuator Ram| | | 416ER | Translating Cowl/Actuator Ram| | | 416FR | Translating Cowl/Actuator Ram| | | 416GR | Translating Cowl/Actuator Ram| | | 416HR | Translating Cowl/Actuator Ram| | 422AL | | P1 Probe| | 422BL | | TAI and Pressure Relief| | | 422BR | P1 Tube Bulkhead Connection| | 423AL | | Fan Cowl and Fancase| | 423BL | | Starter Air Valve| | 423CL | | IDG Oil Fill and Level Indicator| | | 424AR | Fan Cowl and Fancase| | | 424BR | Oil Filler and Pressure Relief| | | 424CR | Master Chip Detector| | 425AL | | Thrust Reverser Cowl| | 425BL | | Thrust Reverser Hydraulics and C-Duct Hinge|
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 06-43-00
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 ú  01  Page 207
 ú  Sep 28/00 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
 
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