Aircraft Overview - Pipistrel ALPHA Trainer LSA Pilot Operating Handbook

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ALPHA Trainer LSA
Pilot Operating Handbook

1.5. AIRCRAFT OVERVIEW

Basic Dimensions
Length
Span
Height
Wing
Area
Mean aerodynamic chord
Aspect ratio
Horizontal Tail
Area
Vertical Tail
Area
Weights
Maximum takeoff weight
Design empty weight
Design useful load
Maximum baggage weight
Performance
Top speed
Cruise speed (5300 RPM)
Endurance at cruise speed
Best climb
Best angle climb
Stall speed full flap (+2)
Stall speed clean (0)
Fuel **
Total capacity
Unusable fuel
Engine
Max power rating (5 min.)
Max continuous power
*only when solid baggage compartment (p/n 6023077) is installed and
CG limitations are respected.
** Please see chapter 2 - Limitations - for information about approved fuel
types.
POH-162-00-40-001
PAGE REV. 0
Metric
Imperial
6.5 m
21' 4"
10.50 m
34' 6"
2.05 m
6' 9"
9.51 m²
102.4 ft²
0.90 m
2' 11.4"
11.8
Metric
Imperial
1.08 m²
11.6 ft²
1.1 m²
11.8 ft²
550 kg
1212 lb
279 kg
615 lb
271 kg
597 lb
10 kg*
22 lb*
120 KIAS (SL)
100 KIAS (SL)
3h + 30' reserve
76 KIAS (V
)
1220 ft/min
Y
58 KIAS (V
)
x
37 KIAS
43 KIAS
Metric
Imperial
50 L
13.2 US gal
2 L
0.5 US gal
59.6 kW at 5800 RPM
58 kW at 5500 RPM
SECTION 1
GENERAL
PAGE
1-5

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