Technical data

13773-001
6-00
Page 1
DIMENSIONS AND AREAS
1. GENERAL
This section describes those diagrams and text which shows the area, dimensions, stations, access doors,
and physical locations of the structural members of the airplane. Also included is the cardinal rigging
dimensions.
2. AIRPLANE DIMENSIONS AND AREAS
The airplane is divided into reference points in inches. These reference points provide a means of quickly
identifying the locations of components. Three axes are used as reference points.
The following terms are used for the reference points:
FS - Fuselage Station is a horizontal reference designation starting in front of the nose of the airplane
WS - Wing Station is measured outboard from the centerline of the fuselage to the wing tip.
WL - Water Line is a vertical reference designation measured parallel to the ground.
BL - Buttock Line is a horizontal reference designation starting at the airplane centerline. Right or left is
added to indicate direction from airplane centerline.
A. General
Length (Overall)................................................................................... 25.92 ft .....................7.90 m
Height (Maximum) ................................................................................. 4.75 ft ..................... 1.45 m
Wing Span (Overall) ............................................................................ 38.25 ft ................... 11.65 m
Propeller Diameter (Maximum) ............................................................. 6.50 ft ..................... 1.98 m
Wheel Track (Main To Main) ................................................................ 10.83 ft ..................... 3.30 m
B. Cabin
Cabin Width......................................................................................... 49.00 in. ............... 124.00 cm
Cabin Height........................................................................................ 50.00 in. ............... 127.00 cm
Cabin Length ..................................................................................... 122.00 in. ............... 309.00 cm
Cabin Volume .................................................................................... 137.00 ft³.................... 3.83 m³
Baggage Compartment Height............................................................ 39.00 in. ................. 99.00 cm
Baggage Compartment Width............................................................. 40.00 in. ............... 101.00 cm
Baggage Compartment Length ........................................................... 36.00 in. ................. 91.00cm
Baggage Compartment Volume .......................................................... 32.00 ft³.................... 0.90 m³
C. Wings
Span .................................................................................................... 38.25 ft ................... 11.65 m
Area................................................................................................... 144.90 ft².................. 13.46 m²
Wing Loading ...................................................................................... 23.46 lb/ft² ............ 114.45 kg/m²
Aspect Ratio ........................................................................................ 10.00 ...................... 10.00
Wing Dihedral........................................................................................ 4.50 °...................... 4.50°
D. Flaps
Span ...................................................................................................... 8.80 ft ..................... 2.68 m
Area..................................................................................................... 10.80 ft².................... 1.00 m²
E. Ailerons
Span ...................................................................................................... 4.70 ft ..................... 1.43 m
Area....................................................................................................... 4.37 ft².................... 0.41 m²
30 Nov 2000