Cessna 510 Mustang Structural Repair Manual page 9

A60935
Forward
Pressure
Bulkhead
FS 144.000
Baggage
Compartment
Floor
WL 88.00
Strut Extended
FS 132.773
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Figure 2 : Sheet 1 : Major Structural Members Location
Aft
Pressure
Bulkhead
FS 321.000
Main Spar
Centerline
Strut Extended
FS 305.16
FOR TRAINING PURPOSES ONLY
ISSUE 02 , JAN 2018
Model 510 Structural Repair Manual (Rev 2)
Forward Engine
Beam Centerline
FS 362.750
Aft Engine
Beam Centerline
FS 380.35
(TCS 151.35)
Engine Forward
Beam Top Edge
WL 112.65
Print Date: Wed Mar 21 05:09:46 CDT 2018
51-00-02-0 (Original Issue)
Engine Aft
Beam Top Edge
WL 111.30
7010T1002
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