AFM VFR Flashcards

1
Q

Wing Span

A

9.00m / 29.5ft

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2
Q

Overall Height

A

2.50m / 8.2ft

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3
Q

Stabilator Span

A

2.90m / 9.5ft

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4
Q

Wing Surface

A

11.9m2 / 128.1ft

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5
Q

Mean Geometric Chord

A

1,322m / 4,337ft

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6
Q

Aspect ratio

A

6.8

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7
Q

Engine manufacturer

A

Bombardier Rotax

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8
Q

Engine Model

A

912 iSc Sport

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9
Q

Engine Type

A

4cyl 1352cc horizontally-opposed twins

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10
Q

MAX TO POWER

A

100hp @ 5800rpm

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11
Q

MAX CONTINUOUS POWER

A

98hp @ 5500rpm

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12
Q

Propeller blades

A

2 laminated wood composite

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13
Q

Propeller diameter

A

1800mm / 180cm / 5ft 10.9in

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14
Q

Propeller type

A

Variable pitch propeller at constant speed

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15
Q

MAX LANDING WEIGHT

A

720kg

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16
Q

MAX TO WEIGHT

A

720kg

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17
Q

Wing Loading

A

60.50kg/m2

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18
Q

Power Loading

A

7.20 kg/hp

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19
Q

Fuel specification

A

AVGAS 100LL

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20
Q

Engine Oil Specification

A

Only oil with RON424 classification

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21
Q

Water / Radiator ratio

A

50:50

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22
Q

10L til US Gallons

A

2.6

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23
Q

Vne

A

Never Exceed
135KIAS / 136CAS

24
Q

Vno

A

Maximum Structural Cruising Speed
107KIAS / 108CAS

25
Q

Va

A

Design Manoeuvring Speed
102KIAS / 103CAS

26
Q

Vo

A

Operating Manoeuvring Speed
102KIAS / 103CAS

27
Q

Vfe Flap 1 (TO)

A

Maximum Speed flap extended
106KIAS / 105CAS

28
Q

Vfe Flap 2 (LAND)

A

Maximum Speed flap extended
96KIAS / 95CAS

29
Q

White arc

A

Positive Flap Operating Range
45-96KIAS

30
Q

Green arc

A

Normal Operating Range
50-107KIAS

31
Q

Yellow arc

A

Manoeuvres must be conducted with
caution and only in smooth air.
107-135KIAS

32
Q

Red Line

A

Maximum speed for all operations.
135KIAS

33
Q

Minimum oil pressure below 3500rpm

A

0.8bar (12psi)

34
Q

Minimum oil pressure above 3500rpm

A

2.0bar (29psi)

35
Q

Maximum oil pressure normal

A

5.0bar (73psi)

36
Q

Maximum oil pressure for start and warm-up

A

7.0bar (102psi)

37
Q

Oil temperature min for starting

A

-20°C

38
Q

Oil temperature minimum

A

50°C

39
Q

Oil temperature maximum

A

130°C

40
Q

Coolant temperature maximum

A

120°C

41
Q

EGT Maximum

A

950°C

42
Q

Manifold Air Temperature Maximum in-flight

A

60°C

43
Q

Fuel Pressure minimum

A

2.8 bar
Acceptable 2.5 bar

44
Q

Fuel Pressure maximum

A

3.2 bar
Acceptable 3.5 bar

45
Q

Maximum negative acceleration

A

-0.5g for max 5sec

46
Q

Fuel capacity

A

140l
131.6 Usable

47
Q

Max fuel imbalance

A

30l

48
Q

Min-Max oil level

A

2.5l–3l

49
Q

Outside Air temp min-max

A

-25°C – 38°C

50
Q

TO+Landing surfaces

A

Hard paved or grass

51
Q

Load Factor Limits
no flap

A

+3.8g & -1.9g

52
Q

Load Factor Limits
Flaps extended

A

+1.9g & 0g

53
Q

COG
Forward og Aft limits

A

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)

54
Q

Datum måles fra?

A

Propeller support flange without spacer
(the aircraft must be levelled in the longitudinal plane)

55
Q

Approved Maneuvers

A

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

56
Q

Baggage Loading Limit

A

30 kg / 66 lb

57
Q

Maximum operating altitude

A

13.000ft AMSL