B STA B STA 1928.568 2021.893
B STA 1662.250
FWD
LEFT SIDE VIEW
NOTES:
INTERSECTION OF ROOT CHORD
AND REAR SPAR CENTERLINE
INTERSECTION OF ROOT CHORD
AND RUDDER HINGE LINE
Vertical Stabilizer Station Diagram Figure 201
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757 MAINTENANCE MANUAL
HORIZONTAL STABILIZER AND ELEVATOR STATION DIAGRAM - MAINTENANCE PRACTICES
__________________________________________________________________________
1. General_______
A. The horizontal stabilizer and elevator station diagram gives the location of the structural components on the horizontal stabilizer and elevator.
TASK 06-23-00-202-001
2. Horizontal Stabilizer and Elevator Station Diagram (Fig. 201)__________________________________________________
A. Procedure
S 222-002
(1) See Fig. 201 for the horizontal stabilizer and elevator station diagram.
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MAINTENANCE MANUAL
HSBL
HSBL
297.000
0.0
ELEVSTA 76.547
244.501 STA
196.514
148.528
TOP VIEW
NOTE: ALL DIMENSIONS ARE MEASURED ALONG OR PARALLEL TO HORIZONTAL STABILIZER REFERENCE PLANE.
RIBS BETWEEN REAR SPAR AND ELEVATOR HINGE LINE ARE PERPENDICULAR TO HINGE LINE. RIBS BETWEEN FRONT AND REAR SPAR ARE PERPENDICULAR TO REAR SPAR.
Horizontal Stabilizer Station Diagram Figure 201
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757 MAINTENANCE MANUAL
WING STATION DIAGRAM - MAINTENANCE PRACTICES
____________________________________________
1. General_______
A. The wing station diagram gives the location of the structural components on the wing.
TASK 06-24-00-202-001
2. Wing Station Diagram (Fig. 201)____________________
A. Procedure
S 222-002
(1) Refer to Fig. 201 for the wing station diagram which gives the location of structural components on the wing.
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WING
NAC WING TIP
TOP VIEW
Wing Station Diagram Figure 201
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757 MAINTENANCE MANUAL
ENGINE AND NACELLE STATION DIAGRAM - MAINTENANCE PRACTICES
__________________________________________________________
1. General_______
A. The engine and nacelle station diagram gives the location of the engine and nacelle structural components on the airplanes.
TASK 06-25-00-202-001
2. Engine and Nacelle Station Diagram (Fig. 201)__________________________________
A. Procedure
S 222-002
(1) Refer to Fig. 201 for the location of nacelle structural components on the engine.
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