F.  Flaps:
Inboard Flaps
Type - Triple Slotted
Span - 123.38 inches

Outboard Flaps
Type - Triple Slotted
Span - 194.80 inches

Leading Edge
Type - 2 position
Span - 106.70 inches

G.  Slats: Span (total) - 385.36 inches
H.  Spoilers: Span (total) - 157.40 inches
I.  Horizontal Stabilizer Surfaces: Span - 428.78 inches Root Chord (theoretical, at body centerline) - 151 inches Tip Chord (theoretical) - 60 inches Sweepback (25 percent chord line) - 30 degrees Dihedral (chord plane with respect to body reference plane) - 7 degrees Incidence (variable) - 3 degrees up to 14 degrees down Aspect Ratio -4.04
J.  Vertical Stabilizer Surface: Height - 242 inches Root Chord (theoretical, leading edge at body station 971.81) - 205 inches Tip Chord (theoretical) - 62 inches Sweepback (25 percent chord line) - 35 degrees Aspect Ratio - 1.81
6-12-0 
Page 202  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  500 Apr 15/66 

K.  Fuselage: Height of body reference plane (top of floor beam WL 208.1) above ground at main gear -
102.10 inches Angle of body reference plane with respect to ground line - 0° 58 minutes (nose down) Body Station at main gear wheel center - 698 Height (maximum cross section) - 158 inches

Above body reference plane - 98.40 inches
Below body reference plane - 59.60 inches
Height to centerline of windows above body reference plane - 38 inches
Length - 1167 inches
Width (maximum width 24.40 inches above body reference plane) - 148 inches

L.  Landing Gear:
Main Wheel Tread - 206 inches
Wheel Base - 448 inches
Main Gear, wheels and tires - 40 x 14
Nose Gear, wheels and tires - 24 x 7.7

3.  Areas
A.  Wing (basic) - 943.70 square feet
B.  Wing (exposed, including trailing and leading edge extensions) - 980 square feet
C.  Flaps
Trailing Edge (retracted) - 96.26 square feet
Trailing Edge (extended) - 181.26 square feet

D.  Ailerons (total, both sides aft of hinge line, including 3.88 square feet of tab area aft of tab hinge line) - 26.90 square feet
E.  Horizontal tail surfaces (total, including area within fairing) - 312 square feet
F.  Vertical tail surface (total) - 224.35 square feet

 Based on 10.000 inches rolling radius (2.50 inches strut extension) for the nose gear and 16.50 inches rolling radius (1.00 inch strut extension) for the main gear. The rolling radius for either gear is determined by measuring from the center of the hub to the ground, while the airplane is in a taxi condition.
500 
May 01/99  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  6-12-0 Page 203 

 Principal Dimensions  500 
6-12-0  Figure 201  Nov 15/67 
Page 204 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 

EFFECTIVITY
Standard Passenger Airplanes

515  Body Station Diagram 
Aug 15/68  Figure 201  6-22-0 
Page 201 

BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
EFFECTIVITY
Passenger/Cargo Convertible Airplanes

515  Body Station Diagram 
Aug 15/68  Figure 201  6-23-0 
Page 201 

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

500  Vertical Stabilizer and Rudder Station Diagram 
Feb 20/87  Figure 201  6-31-0 
Page 201 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 

HORIZONTAL STABILIZER AND ELEVATOR STATION DIAGRAMS
500 Nov 15/67 Page 201 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.

500  Wing Station Diagram 
May 20/82  Figure 201  6-51-0 
Page 201 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 

500  Engine and Nacelle Station Diagram 
Aug 15/71  Figure 201  6-61-0 
Page 201 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.