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1.2 CERTIFICATION BASIS
The certification basis is JAR-23, published on 11-Mar-1994, including Amdt. 1, and additional requirements as laid down in CRI A-01.

1.3 WARNINGS, CAUTIONS AND NOTES
Special statements in the Airplane Flight Manual concerning the safety or operation of the airplane are highlighted by being prefixed by one of the following terms:
WARNING
means that the non-observation of the corresponding procedure leads to an immediate or important degradation in flight safety.
CAUTION
means that the non-observation of the corresponding procedure leads to a minor or to a more or less long term degradation in flight safety.
NOTE

draws the attention to any special item not directly related to safety but which is important or unusual.
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1.4  DIMENSIONS
NOTE

All dimensions shown below are approximate.
Overall dimensions
Span : 13.42 m 44 ft

'
13.55 m 44.5 ft including ACL Length : 8.56 m 28 ft 1 in Height : 2.49 m 8 ft 2 in
Wing
Airfoil : Wortmann FX 63-137/20 - W4
Wing Area : 16.29 m2 175.3 sq.ft.
Mean aerodynamic chord : 1.271 m 4 ft 2 in
Aspect ratio : 11.06
Dihedral : 5°
Leading edge sweep : 1°

Aileron
Area (total, left + right) : 0.66 m2 7.1 sq.ft.

Doc. No. 7.01.05-E  Rev. 5  15-Nov-2007  Page 1 - 5 

Wing flaps 
Area (total, left + right)  :  2.18 m2  23.4 sq.ft. 
Horizontal tail 
Area  :  2.35 m2  25.3 sq.ft. 
Elevator area  :  0.66 m2  7.1 sq.ft. 
Angle of incidence  :     -1.1° relative to longitudinal axis of airplane 
Vertical tail 
Area  :  2.43 m2  26.2 sq.ft. 
Rudder area  :  0.78 m2  8.4 sq.ft. 
Landing gear 
Track  :  2.95 m  9 ft 8 in 
Wheelbase  :  1.735 m  5 ft 8 in 
Nose wheel  :  5.00-5; 10 PR, 120 mph 
Main wheel  : 15x6.0-6; 6 PR, 120 mph 

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1.5 DEFINITIONS AND ABBREVIATIONS
(a) Airspeeds

CAS: Calibrated Airspeed. Indicated airspeed, corrected for installation and instrument errors. CAS equals TAS at standard atmospheric conditions (ISA) at MSL. IAS: Indicated Airspeed as shown on an airspeed indicator. ' KCAS: CAS in knots. ' KIAS: IAS in knots. TAS: True Airspeed. The speed of the airplane relative to the air. TAS is CAS corrected for errors due to altitude and temperature. vA: Maneuvering Speed. Full or abrupt control surface movement is not permissible above this speed. vFE: Maximum Flaps Extended Speed. This speed must not be exceeded with the given flap setting. vLO: Maximum Landing Gear Operating Speed. This speed may not be exceeded during the extension or retraction of the landing gear. vLE: Maximum Landing Gear Extended Speed. This speed may not be exceeded if the landing gear is extended. vmCA: Minimum Control Speed. Minimum speed necessary to be able to control the airplane in case of one engine inoperative. vNE: Never Exceed Speed in smooth air. This speed must not be exceeded in any operation.
　
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