Aircraft Specs. Flashcards
A/C: Height?
2,60m (6ft 6,5in)
A/C: Length?
7,00m (23ft)
A/C: Wing span
8,85m (29ft)
A/C: Wheel track?
2,20m (7ft 2,5in)
A/C: Wheel base?
1,58m (5ft 2,5in)
Wing area, reference.?
11,9 m^2 (128sqft)
Wing: Sweep forward?
5 degrees
Wing: Airfoil thickness?
10%
Wing: Dihedral?
1,5 degrees
Wing: Mounting angle of incidence wing chord to fuselage datum?
+2,8 degrees nose up
Horizontal tail: span?
2,8m (9ft 2in)
Horizontal tail: Area, reference?
2,10 m^2 (22,6 sqft)
Horizontal tail: Sweep?
0 degrees
Horizontal tail: Airfoil thickness?
12 %
Horizontal tail: Dihedral?
0 degrees
Vertical tail: Height?
1,32m (4ft 4in)
Vertical tail: Area, reference?
1,52 m^2 (16,3sqft)
Vertical tail: Airfoil thickness?
12%
Vertical tail: Sweep, leading edge?
36%
Vertical tail: Sweep, trailing edge?
8%
The aircraft is powered by an…?
Avco Lycoming, four cylinder, horizontally opposed, air cooled, direct drive, fuel injection engine type I0-360-A1B6
State engine type
I0-360-A1B6
Engine rated maximum continuous power?
200hp at 2700 RPM (at standard sea-level)
Propeller diameter?
74 inches