AGK Flashcards
Aircraft length
27’2”
Aircraft Height
8’11”
Aircraft Width
36’1”
Prop Diameter
76”
Prop Clearance
11.25”
Fuel type
100LL/100 AVGAS
Oil
Grade 40 or 50
Sump 8qt
Total 9qt
Max Engine speed
2700RPM
Max Oil temperature
245 F
Min oil pressure
20 psi
Max oil pressure
115 psi
Min static RPM
2300-2400 RPM
Max demonstrated crosswind
15kt Full flaps
20kt Flaps 10
Engine model
IO-360-L2A
Normally aspirated, Direct drive, Air-cooled, Horizontally opposed, Fuel injected, Four cylinder, 360 cu. in
Engine Power
180BHP at 2700 RPM
Weights
Ramp 2558
TO + LDG 2550
Standard empty mass
1663 lbs
Max load (fuel + PAX)
895 lbs
Baggage compartment loads
A - 120
B - 50
(Total adding to 120)
CG Limits
FWD 35” <1950lbs
41” @2550
AFT 47.3” at all weights
Load factor limits
Flaps up +3.8g -1.52g
Flaps full +3.0g
Purpose of horn balance
Reduce input forces
Purpose of mass balance
Reduce flutter
Type of flap on aircraft
Fowler
Instruments connected to pitot-static system
ASI, VSI, altimeter
Normal and Max tyre pressures
Nose: Max - 45 Normal 40
Main: Max - 38 Normal 35
Battery voltage
24v
Number of fuel drains
13