AFM VFR Flashcards
Wing Span
9.00m / 29.5ft
Overall Height
2.50m / 8.2ft
Stabilator Span
2.90m / 9.5ft
Wing Surface
11.9m2 / 128.1ft
Mean Geometric Chord
1,322m / 4,337ft
Aspect ratio
6.8
Engine manufacturer
Bombardier Rotax
Engine Model
912 iSc Sport
Engine Type
4cyl 1352cc horizontally-opposed twins
MAX TO POWER
100hp @ 5800rpm
MAX CONTINUOUS POWER
98hp @ 5500rpm
Propeller blades
2 laminated wood composite
Propeller diameter
1800mm / 180cm / 5ft 10.9in
Propeller type
Variable pitch propeller at constant speed
MAX LANDING WEIGHT
720kg
MAX TO WEIGHT
720kg
Wing Loading
60.50kg/m2
Power Loading
7.20 kg/hp
Fuel specification
AVGAS 100LL
Engine Oil Specification
Only oil with RON424 classification
Water / Radiator ratio
50:50
10L til US Gallons
2.6
Vne
Never Exceed
135KIAS / 136CAS
Vno
Maximum Structural Cruising Speed
107KIAS / 108CAS
Va
Design Manoeuvring Speed
102KIAS / 103CAS
Vo
Operating Manoeuvring Speed
102KIAS / 103CAS
Vfe Flap 1 (TO)
Maximum Speed flap extended
106KIAS / 105CAS
Vfe Flap 2 (LAND)
Maximum Speed flap extended
96KIAS / 95CAS
White arc
Positive Flap Operating Range
45-96KIAS
Green arc
Normal Operating Range
50-107KIAS
Yellow arc
Manoeuvres must be conducted with
caution and only in smooth air.
107-135KIAS
Red Line
Maximum speed for all operations.
135KIAS
Minimum oil pressure below 3500rpm
0.8bar (12psi)
Minimum oil pressure above 3500rpm
2.0bar (29psi)
Maximum oil pressure normal
5.0bar (73psi)
Maximum oil pressure for start and warm-up
7.0bar (102psi)
Oil temperature min for starting
-20°C
Oil temperature minimum
50°C
Oil temperature maximum
130°C
Coolant temperature maximum
120°C
EGT Maximum
950°C
Manifold Air Temperature Maximum in-flight
60°C
Fuel Pressure minimum
2.8 bar
Acceptable 2.5 bar
Fuel Pressure maximum
3.2 bar
Acceptable 3.5 bar
Maximum negative acceleration
-0.5g for max 5sec
Fuel capacity
140l
131.6 Usable
Max fuel imbalance
30l
Min-Max oil level
2.5l–3l
Outside Air temp min-max
-25°C – 38°C
TO+Landing surfaces
Hard paved or grass
Load Factor Limits
no flap
+3.8g & -1.9g
Load Factor Limits
Flaps extended
+1.9g & 0g
COG
Forward og Aft limits
Forward
1.753 m (5.75 ft) (23% MAC)
aft of datum up to 550 kg
1.780 m (5.84 ft) (25% MAC)
aft of datum for MTOW
Aft datum
1.889 m (6.20 ft) (33% MAC)
Datum måles fra?
Propeller support flange without spacer
(the aircraft must be levelled in the longitudinal plane)
Approved Maneuvers
This is a normal category aircraft.
No aerobatic maneuvers operations include:
- Any manoeuvre pertaining to “normal” flight
- Stalls (except whip stalls)
- Lazy eights
- Turns in which the angle of bank is not more than 60°
- Chandelle
Baggage Loading Limit
30 kg / 66 lb
Maximum operating altitude
13.000ft AMSL