POH 4.1 General Information Flashcards
POH.4.1.1 Powerplant
Righ Engine (continental)
LTSIO-360-E or LTSIO-360-EB
Left Engine (Continental)
TSIO-360-E or TSIO-360-EB
Rated Horsepower (sea level)
200
Rated Horsepower (12,000 ft)
215
Rated Speed (rpm)
2575
Max Manifold Pressure (in. Hg.)
40
Compression Ratio
7.5:1
POH.4.1.2 Fuel and Oil
AVGAS ONLY
FUEL (Total)
128 US GAL
(Usable)
123 US GAL
MAX OIL
8 US Quarts
MIN OIL
6 US Quarts
POH.4.1.3 Baggage Area
Maximum Baggage (lbs) Forward Compartment
100
Maximum Baggage (lbs) Rear Compartment
100
POH.4.1.4 Dimensions
Wingspan (ft)
38.9
Wing Area (sq ft)
208.7
Length (ft)
28.5
Height (ft)
9.9
Wing Loading (lbs per sq ft)
22
Power Loading (lbs per hp) (sea level)
11.4
Power Loading (lbs per hp) (12,000 ft)
10.6
Propeller Diameter (in.)
76
Turn Radius (ft)
33.2
Gross Weight (lb)
4570
Take off Run, flaps up, sea level (ft)
1100
Takeoff Distance Over 50-ft Obstacle, flaps up, sea level
1460’
Takeoff Run (f) short field effort, flaps 25º
900
Takeoff Distance Over 50-ft Barrier (ft) (short field effort, 25º)
1240
Rate of Climb, sea level (ft per min)
1340
Rate of Climb, sea level, single engine (ft per min)
225
Service Ceiling (ft)
25000’**
Service Ceiling, engine out (ft
13400
Absolute Ceiling (ft
25000**
Absolute Ceiling, engine out (ft)
14800
STANDARD FUEL CAPACITY
Range at best power mixture (mi)
75% power, 16,000 ft
With 45 min. reserve
626
No reserve
742
55% power, 16,000 ft
With 45 min. reserve
701
No reserve
830
*4570 lbs Maximum Takeoff Weight; 4342 lbs Maximum Landing Weight **Maximum Operating Altitude
Stalling Speed, gear and flaps down, power off (kts)
60
Stalling Speed, gear down and flaps up. power off (kts)
66
Fuel Consumption, 75% power, both engines (gph)
23.6
Fuel Consumption, 65% power, both engines (gph)
20.5
Landing Roll (flaps down) (ft)
1380*
Landing Over 50-ft Barrier (flaps down) (short field effort) (ft)
2090*
*4342 lb G.W., Maximum Landing Weight
