POH 4.1 General Information Flashcards
(50 cards)
1
Q
POH.4.1.1 Powerplant
A
2
Q
Righ Engine (continental)
A
LTSIO-360-E or LTSIO-360-EB
3
Q
Left Engine (Continental)
A
TSIO-360-E or TSIO-360-EB
4
Q
Rated Horsepower (sea level)
A
200
5
Q
Rated Horsepower (12,000 ft)
A
215
6
Q
Rated Speed (rpm)
A
2575
7
Q
Max Manifold Pressure (in. Hg.)
A
40
8
Q
Compression Ratio
A
7.5:1
9
Q
POH.4.1.2 Fuel and Oil
A
10
Q
AVGAS ONLY
FUEL (Total)
A
128 US GAL
11
Q
(Usable)
A
123 US GAL
12
Q
MAX OIL
A
8 US Quarts
13
Q
MIN OIL
A
6 US Quarts
14
Q
POH.4.1.3 Baggage Area
A
15
Q
Maximum Baggage (lbs) Forward Compartment
A
100
16
Q
Maximum Baggage (lbs) Rear Compartment
A
100
17
Q
POH.4.1.4 Dimensions
A
18
Q
Wingspan (ft)
A
38.9
19
Q
Wing Area (sq ft)
A
208.7
20
Q
Length (ft)
A
28.5
21
Q
Height (ft)
A
9.9
22
Q
Wing Loading (lbs per sq ft)
A
22
23
Q
Power Loading (lbs per hp) (sea level)
A
11.4
24
Q
Power Loading (lbs per hp) (12,000 ft)
A
10.6
25
Propeller Diameter (in.)
76
26
Turn Radius (ft)
33.2
27
Gross Weight (lb)
4570
28
Take off Run, flaps up, sea level (ft)
1100
29
Takeoff Distance Over 50-ft Obstacle, flaps up, sea level
1460'
30
Takeoff Run (f) short field effort, flaps 25º
900
31
Takeoff Distance Over 50-ft Barrier (ft) (short field effort, 25º)
1240
32
Rate of Climb, sea level (ft per min)
1340
33
Rate of Climb, sea level, single engine (ft per min)
225
34
Service Ceiling (ft)
25000'**
35
Service Ceiling, engine out (ft
13400
36
Absolute Ceiling (ft
25000**
37
Absolute Ceiling, engine out (ft)
14800
38
STANDARD FUEL CAPACITY
39
Range at best power mixture (mi)
75% power, 16,000 ft
With 45 min. reserve
626
40
No reserve
742
41
55% power, 16,000 ft
With 45 min. reserve
701
42
No reserve
830
43
*4570 lbs Maximum Takeoff Weight; 4342 lbs Maximum Landing Weight **Maximum Operating Altitude
44
Stalling Speed, gear and flaps down, power off (kts)
60
45
Stalling Speed, gear down and flaps up. power off (kts)
66
46
Fuel Consumption, 75% power, both engines (gph)
23.6
47
Fuel Consumption, 65% power, both engines (gph)
20.5
48
Landing Roll (flaps down) (ft)
1380*
49
Landing Over 50-ft Barrier (flaps down) (short field effort) (ft)
2090*
50
*4342 lb G.W., Maximum Landing Weight
