Technical data

13773-001
6-00
Page 2
F. Horizontal Stabilizer
Span .................................................................................................... 13.17 ft ..................... 4.01 m
Area..................................................................................................... 25.75 ft².................... 2.39 m²
Aspect Ratio .......................................................................................... 5.59 ........................ 5.59
G. Elevator
Span .................................................................................................... 12.00 ft ..................... 3.66 m
Area....................................................................................................... 7.73 ft².................... 0.72 m²
H. Vertical Stabilizer
Span ...................................................................................................... 5.52 ft ..................... 1.65 m
Area..................................................................................................... 15.93 ft².................... 1.48 m²
Aspect Ratio .......................................................................................... 1.84 ........................ 1.84
I. Rudder
Span ...................................................................................................... 5.42 ft ..................... 1.65 m
Area....................................................................................................... 5.26 ft².................... 0.49 m²
J. Landing Gear
Wheel Track (Main To Main) ................................................................ 10.50ft ...................... 3.20 m
Wheel Base (Main To Nose).................................................................. 7.26 ft ..................... 2.21 m
3. ACCESS PANELS
A. Cabin Floor (See Figure 6-005)
Maintenance practices pertinent to the cabin floor access panels are found in Chapter 53, Fuselage.
(Refer to 53-20)
B. Wing (See Figure 6-006)
Maintenance practices pertinent to the wing access panels are found in Chapter 57, Wings. (Refer to
57-30)
C. Empennage (See Figure 6-007)
Maintenance practices pertinent to the empennage access panels are found in Chapter 53, Fuselage.
(Refer to 53-30)
4. CONTROL SURFACE TRAVELS AND CABLE TENSION SETTINGS
A. Aileron
Aileron Up Travel:12.5° +/- 1.0°
Aileron Down Travel: 12.5° +/- 1.0°
Aileron Trim Deflection:6.0° +/- 1.0°
Aileron Cable Tension:30-40 lb
B. Elevator
Elevator Up Travel:25.0° +/- 1.0°
Elevator Down Travel: 15.0° +/- 1.0°
Elevator Trim Deflection:-11.5° +/- 0.5°, +17° + 1°/-2°
Elevator Cable Tension:30-40 lb
30 Nov 2000