Limitations Flashcards

0
Q

Rotor speed limits

Power off

Minimum

A

90%

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1
Q

Rotor speed limits

Power off

Maximum

A

Tach reading

110%

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2
Q

Minimum oil quantity for takeoff

A

4 qt

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3
Q

Maximum gross weight: beta II

A

1370 lb (622 kg)

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4
Q

Minimum gross weight: beta II

A

920 lb (417kg)

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5
Q

Max per seat (including baggage compartment)

A

240 lb (109 kg)

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6
Q

Max in either bag compartment

A

50 lb (23 kg)

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7
Q

Minimum solo weight plus baggage and doors installed

A

130 lb (59 kg) with standard fuel or 135 lb (61 kg) with aux fuel

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8
Q

Datum line

A

100 inches forward of the main rotor shaft centerline

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9
Q

POH CG limit chart. Page #?

A

2-5

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10
Q

How to eliminate a low g condition

A

Immediately apply gentle aft cyclic

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11
Q

Is flight allowed with the governor off?

A

No

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12
Q

Maximum operating density altitude

A

14, 000 ft

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13
Q

What systems must be operational for dispatch?

A

alternator, RPM governor, low rotor RPM warning system, and OAT gauge

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14
Q

What seat for solo fight

A

Right

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15
Q

Doors off operation?

A

Approved either or both doors removed.

16
Q

VFR day is approved. T / F

17
Q

What illumination is required for night VFR

A

Landing, navigation, instrument, and anti-collision light. Also adequate celestial illumination.

18
Q

What kind of fuel does civic use.

19
Q

Main tank usable capacity

A

19.2 us gallons (73 liters)

20
Q

Optional aux tank usable capacity

A

10.5 US gallons (40 liters)

21
Q

Beta II (0-360-J2A engine) red line

A

24.1 in Hg

22
Q

Wind restrictions

A

Surface winds may not exceed 25 knots, including gusts.

Surface wind gust spreads may not exceed 15 knots.

Continued flight in moderate, severe, or extreme turbulence is prohibited.