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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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 (a)  Zone 741 Right Main Landing Gear 742 Right Main Landing Gear Body Door 743 Right Main Landing Gear Oleo Door
 TASK 06-30-00-222-008
 10. Major Zone 800 - Doors______________________
 A. General
 (1)
Subzone 820 - Lower Half of Fuselage, Right

 (a)  Zone 821 No. 1 Cargo Door
 822 No. 2 Cargo Door


 (2)
Subzone 830 - Upper Half of Fuselage, Left

 (a)  Zone 831 Left No. 1 Passenger Door 832 Left No. 2 Passenger Door 835 Left No. 3 Emergency Exit Door 836 Left No. 4 Passenger Door

 (3)
Subzone 840 - Upper Half of Fuselage, Right


 (a)  Zone 841 Right No. 1 Passenger Door 842 Right No. 2 Passenger Door
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 06-30-00
 ALL  ú ú 01 Page 216 ú Sep 20/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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757 MAINTENANCE MANUAL
 845 Right No. 3 Emergency Exit Door 846 Right No. 4 Passenger Door
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 ALL  ú ú 01 Page 217 ú Sep 20/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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757 MAINTENANCE MANUAL
 FUSELAGE (MAJOR ZONES 100 AND 200)
__________________________________ ACCESS DOORS AND PANELS - MAINTENANCE PRACTICES
_______________________________________________
 1.  General (Fig. 201)_______
 A.  The major zone 100 contains the lower half of the fuselage but does not include Section 48.
 B.  The major zone 100 contains the sub-zones. These sub-zones are identified by the first two numbers and followed by a zero as shown below:
 (1)  
Sub-zone 110 Airplane nose to aft end of Main Equipment Center (BSTA 159.0 to 560.0)

 (2)  
Sub-zone 120 Aft end of Main Equipment Center to front spar of wing center section (BSTA 560.0 to 900.0)

 (3)
Sub-zone 130  Wing Center Section (BSTA 900.0 to 1040.0)

 (4)  
Sub-zone 140 Main Landing Gear (MLG) Wheel Well (BSTA 1040.0 to 1180.0)

 (5)  
Sub-zone 150 Compartment Aft of MLG Wheel Well through Aft Cargo Compartment (BSTA 1180.0 to 1480.0)

 (6)
Sub-zone 160  Bulk Cargo Compartment (BSTA 1480.0 to 1720.0)

 (7)
Sub-zone 190  Wing-to-body Fairings


 C.  The major zone 200 contains the upper half of the fuselage, but does not include Section 48.
 D.  The major zone 200 contains the sub-zones. These sub-zones are identified by the first two numbers and followed by a zero as shown below:
 (1)
Sub-zone 210  Control Cabin (BSTA 199.09 to 297.0)

 (2)
Sub-zone 220  Passenger Cabin (BSTA 297.0 to 440.0)

 (3)
Sub-zone 230  Passenger Cabin (BSTA 440.0 to 900.0)

 (4)
Sub-zone 240  Passenger Cabin (BSTA 900.0 to 1180.0)

 (5)
Sub-zone 250  Passenger Cabin (BSTA 1180.0 to 1720.0)


 E.  Each sub-zone is divided into zones that are identified by the first two numbers of the sub-zone followed by a number that is not zero. See tables.
 F.  The access doors and panels in a zone are identified by the zone number followed by two letters or by three letters. Each access door or panel has a different identifier.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 06-41-00
 ALL  ú ú 01 Page 201 ú May 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

 G. The top collector drawing numbers for the fuselage access panels are:
 (1)  100N1141
 100N1142
 100N1143
 100N1146
 100N1149

 TASK 06-41-00-222-001
 2. Fuselage Access Doors and Panels
________________________________
 A. General
 (1)  
For locations of access doors and panels, refer to Fig. 201.
 
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