From: rdd@cactus.org (Robert Dorsett)
Subject: 747 dimensions and weights: here they are.
Organization: Capital Area Central Texas UNIX Society, Austin, Tx
Date: Fri, 9 Oct 1992 10:03:10 GMT

From AC 150/5325-5C, "Aircraft Data," 6/29/87, which appears to have been
discontinued.  Note the vertical clearance of wingtips; that's a pretty
neat figure (especially the SP!).


Dimensions:


-100B, -200B, -200C, 300 (?!):
------------------------

195'8"	Wingspan
231'10"	Length overall
64'3"	Height overall
84'0" 	Wheelbase
109'5"	Nose of centerline of main gear
36'1"	Wheel track (tread)
39'9"	Centerline of fuselage to centerline of inboard engine
69'10"	Centerline of fuselage to centerline of outboard engine
77'3"	Outside of main gear to wingtip
3'9"	Vertical clearance of inboard engine at max. weight
4'11"	Vertical clearance of outboard engine at max. weight
40'0"	Centerline of fuselage to approximate pivot point based on
                maximum nosewheel steering angle or locked wheels
17'7"	Vertical clearance of wingtip at max. weight
151'0" 	Turn Radius



-200C, -200F
------------

195'8"	Wingspan
231'10"	Length overall
64'8"	Height overall
84'0" 	Wheelbase
109'5"	Nose of centerline of main gear
36'1"	Wheel track (tread)
39'9"	Centerline of fuselage to centerline of inboard engine
69'10"	Centerline of fuselage to centerline of outboard engine
77'3"	Outside of main gear to wingtip
3'9"	Vertical clearance of inboard engine at max. weight
6'0"	Vertical clearance of outboard engine at max. weight
40'0"	Centerline of fuselage to approximate pivot point based on
                maximum nosewheel steering angle or locked wheels
17'7"	Vertical clearance of wingtip at max. weight
151'0" 	Turn Radius

SP
--

195'8"	Wingspan
184'9""	Length overall
65'10"	Height overall
67'4" 	Wheelbase
92'9"	Nose of centerline of main gear
36'1"	Wheel track (tread)
39'2"	Centerline of fuselage to centerline of inboard engine
69'6"	Centerline of fuselage to centerline of outboard engine
77'4"	Outside of main gear to wingtip
3'7"	Vertical clearance of inboard engine at max. weight
5'7"	Vertical clearance of outboard engine at max. weight
40'0"	Centerline of fuselage to approximate pivot point based on
                maximum nosewheel steering angle or locked wheels
17'2"	Vertical clearance of wingtip at max. weight
151'0" 	Turn Radius


-400 (Tentative; data's old)
----------------------------

211'0"	Wingspan
231'10"	Length overall
64'3"	Height overall
84'0" 	Wheelbase
109'5"	Nose of centerline of main gear
36'1"	Wheel track (tread)
39'2"	Centerline of fuselage to centerline of inboard engine
69'6"	Centerline of fuselage to centerline of outboard engine
84'9"	Outside of main gear to wingtip
3'9"	Vertical clearance of inboard engine at max. weight
6'0"	Vertical clearance of outboard engine at max. weight
40'0"	Centerline of fuselage to approximate pivot point based on
                maximum nosewheel steering angle or locked wheels
24'5"	Vertical clearance of wingtip at max. weight
158'0" 	Turn Radius


Weights (pounds):

		MTOW		Landing
-100	735,000		564,000
-200B	833,000		630,000
-200BC	833,000		630,000
-200C	833,000		630,000
-200F	833,000		630,000
-300	833,000		574,000
-300C	833,000		605,000
-SP		696,000		450,000
-400	850,000		630,000

The -100, -200, -300C, and SP series came in about five variants each, 
with widely varying max. weights.  The -300 came in about 10 variants.  
The -400 has at least six.  The variations are a result of 
configuration and engine selection.

Note that the -400 weight data is a bit low; the actual airplane
is around 25K higher.




---
Robert Dorsett
rdd@cactus.org
...cs.utexas.edu!cactus.org!rdd

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