Limitations Flashcards

1
Q

Cylinder Head Temperature (CHT) Range

A

120-210 C

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2
Q

OAT for no Preheat

A

Preheat always required

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3
Q

CHT for Cold Engine Start

A

120 C

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4
Q

CHT for Warm Engine Start

A

110 C

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5
Q

Minimum CHT for Engine Run-Up

A

150 C

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6
Q

Engine RPM Range

A

3,000 - 7200 RPM

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7
Q

Minimum RPM required for Launch

A

Per Launch Chart

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8
Q

RPM Range at Min Throttle in Flight

A

3,000 - 3,500 RPM

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9
Q

RPM Range at Max Throttle in Flight

A

5,300 - 7,200 RPM

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10
Q

RPM Range at Min Throttle on the Ground

A

3,000 - 3,500 RPM

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11
Q

RPM Range at Max Throttle on the Ground

A

5,300 - 6,100 RPM

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12
Q

Launch Pressure range for AV Launch

A

150 - 2,200 PSI

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13
Q

Launch Speed range for AV Launch

A

20 - 63.3 Knots

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14
Q

Max AV Capture Weight

A

135 lbs

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15
Q

Max AV Capture Energy

A

22.3 KJ (16,447.6 ft-lbs)

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16
Q

AV Capture Speed Range

A

38.9 - 58.3 Knots

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17
Q

Effective Directional Antenna Range

A

50 Nautical Miles

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18
Q

Effecitve Omni-Directional Antenna Range

A

10 Nautical Miles

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19
Q

Max Launch & Recovery Altitude @ Max Gross Takeoff Weight (MGTOW)

A

7,500 ft DA

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20
Q

Maximum Operating Altitude

A

20,000 ft

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21
Q

Minimum Airspeed

A

Autopilot Min Airspeed Schedule

22
Q

Maximum Airspeed

A

110 Knots

23
Q

List the 5 Prohibited Maneuvers for Recovery

A

1) Intentional Inside Captures
2) Recovery without Differential GPS (DGPS)
3) Ignore Clear to land (CTL) recovery mode
4) Commanding airspeed changes >8 kts IAS at or below 500 ft. AGL
5) Commanding ‘Sync Baro to GPS’ inside FAF

24
Q

Max Headwind including gusts (Launch/Recovery)

A

25 knots

25
Q

Crosswind Including Gusts (Launch/Recovery)

A

10 knots

26
Q

Tailwind Component (Launch/Recovery)

A

5 knots

27
Q

Tailwind Component at >7,500’ Density Altitude (Launch/Recovery)

A

0 knots

28
Q

Gust Limits for Launch

A

5 knots

29
Q

Total Wind Limit in Flight

A

60 knots

30
Q

Gust limit in flight

A

10 knots

31
Q

Avionics Mainboard Operating Temperature Range

A

-15 C to 73 C

32
Q

Avionics Fuselage Board Operating Temperature Range

A

-15 C to 85 C

33
Q

Maximum Gross Take-Off Weight (MGTOW)

A

135 lbs

34
Q

Max Fuel Capacity of AV Fuel Tanks

A

20 kg

35
Q

AV Empty CG Range

A

98-120 mm

36
Q

Flyable CG Range

A

90 - 136 mm

37
Q

Allowed Barometric and GPS Difference during Launch

A

+/- 33 ft

38
Q

Allowed Barometric and GPS Difference during Recovery

A

+/- 33 ft

39
Q

Maximum Bank Angle

A

+/- 45 Degrees

40
Q

Maximum Bank Angle (During missed Recovery)

A

+/- 25 Degrees

41
Q

Operating Temperature Range of System

A

-4 to 120 F

42
Q

Prohibited Flying Environments

A

1) Visible Moisture
2) Icing Conditions
3) Rain
4) Salt Spray
5) Salt Fog > 30 min

43
Q

Minimum Distance from T-storms and/or Lightning

A

20 NM

44
Q

Generator Voltage Range

A

27 - 29 V

45
Q

Generator Current Range

A

0 - 23.2 A

46
Q

Battery Voltage (Discharging)

A

18 - 25.2 V

47
Q

Battery Current (Discharging)

A

2 - 15 A

48
Q

Battery Voltage (Charging)

A

-18 to -25.2 V

49
Q

Battery Current (Charging)

A

0.2 to 2.5 A

50
Q

External Voltage

A

26 - 30 V

51
Q

External Current

A

2 - 12.5 A

52
Q

Gust Limit for Recovery

A

10 Knots