Aircraft Data Flashcards
Wingspan
10.67m
Length of Fuselage
7.25m
Wheel gauge
3.05m
Engine
Lycoming 0-320-D3G, 160PS, 2700rpm/min, horizontally opposed, 4 cylinders, air cooled, direct drive
Propeller
Sensenich 72’-74’ fixed pitch
Fuel
50USG (190l), 48 USG (182l) usable, AVGAS 100 (green) or 100LL (blue)
Oil
8 quarts (7.8l)
Mass limits
Ramp mass 2447lbs = 1058kg, Starting mass 2440lbs = 1055kg, landing mass 2440lbs = 1055kg, baggage compartment 50lbs = 23kg
VNE
160kt IAS
VNO
126kt IAS
VFE
103kt IAS
VA
1055kg - 111kt, 694kg - 88kt
Yellow arc
126 - 160kt
Green arc
50 - 126kt
White arc
44 - 103kt
Oil pressure
25 - 100psi
Positive load
3.8g
V best glide
73kt (1055kg)
Vy
79kt IAS, Power full, Pitch +9°
Vx
63kt IAS
Vapp 40
63kt IAS, Power 1600, Pitch 0°
Vapp 25
70kt IAS, Power 1600, Pitch 0°
VR
55kt IAS, initial Rotate +9°
V cruise climb
87kt IAS, Power full, Pitch +7°
V cruise
~110kt IAS, 2500 RPM, Pitch +2°
Vp clean
90kt IAS, 2300 RPM, Pitch +2°
Vp 10 level
85kt IAS, 2200 RPM, Pitch +2°
Vp 10 descent
85kt IAS, 1600 RPM, Pitch -1°
Vp 25 decent
75kt IAS, 1600 RPM, Pitch - 1°
Max crosswind
17kt
Max Tailwind
5kt
V min Flaps 10
58kt IAS
V min Flaps Up
Vx = 63kt IAS
Vp clean descent (0 Flaps Approach)
90kt, 1600 RPM, Pitch - 1
Vapp clean (0 Flaps Approach)
75kt, 1600 RPM, Pitch +2
