1
Q
Span, length, height?
A
13.42m, 8.59m, 2.49m
2
Q
Dihedral? Leading edge sweep?
A
5 degrees, 1 degree
3
Q
Landing gear track? wheelbase?
A
2.894m, 1.735m
4
Q
Engines?
A
Textron Lycoming (LH) IO-350-M1A, (RH) LIO-350-M1A
5
Q
Va?
A
> 1542kg, 126 kias
up to 1542kg, 120 kias
6
Q
Vfe?
A
app, 137 kias
ldg, 111 kias
7
Q
Vle?
A
194 kias
8
Q
Vlor?
A
156 kias
9
Q
Vmca?
A
65 kias
10
Q
Vne?
A
194 kias
11
Q
Von?
A
155 kias
12
Q
Vsse?
A
80 kias
13
Q
Vyse?
A
90 kias
14
Q
Max cont RPM?
A
2700
15
Q
Manifold pressure limitations?
A
Take off - FULL throttle
AEO - 5 minutes
OEI - No limit
16
Q
Max continuous power?
A
160 HP
17
Q
Prop diameter
A
72.05”
18
Q
MRampW
A
1795
19
Q
MTOW
A
1785
20
Q
MLW
A
1700
21
Q
MZFW
A
1650
22
Q
Max load in nose baggage
A
30
23
Q
Max load in cockpit baggage
A
45
24
Q
Max load in baggage extension
A
18
25
Max combined cockpit and extension
45
26
Approved manoeuvres
- All normal flight manoeuvres
- Stalling (except power on stalls with a fuel imbalance)
- Lazy eights, chandelles, steep turns and similar manoeuvres in which a aob not more than 60 degrees is attained
27
G limits?
Positive: 3.8, with flaps (app/ldg) 2.0
Negative: -1.52 (at Va), 0 (at Vne)
28
Max operating alt
18,000ft PA
29
Fuel quantity, max permissible difference
Main tanks: 2x 25.5 usg
Aux tanks: 2x 13.7 usg
(1.0 unusable per main tank 0.5 unusable per aux tank)
5 usg difference
30
Flying
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Decks in class (6)
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