Limitations Flashcards

(52 cards)

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

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)

25
Crosswind Including Gusts (Launch/Recovery)
10 knots
26
Tailwind Component (Launch/Recovery)
5 knots
27
Tailwind Component at >7,500' Density Altitude (Launch/Recovery)
0 knots
28
Gust Limits for Launch
5 knots
29
Total Wind Limit in Flight
60 knots
30
Gust limit in flight
10 knots
31
Avionics Mainboard Operating Temperature Range
-15 C to 73 C
32
Avionics Fuselage Board Operating Temperature Range
-15 C to 85 C
33
Maximum Gross Take-Off Weight (MGTOW)
135 lbs
34
Max Fuel Capacity of AV Fuel Tanks
20 kg
35
AV Empty CG Range
98-120 mm
36
Flyable CG Range
90 - 136 mm
37
Allowed Barometric and GPS Difference during Launch
+/- 33 ft
38
Allowed Barometric and GPS Difference during Recovery
+/- 33 ft
39
Maximum Bank Angle
+/- 45 Degrees
40
Maximum Bank Angle (During missed Recovery)
+/- 25 Degrees
41
Operating Temperature Range of System
-4 to 120 F
42
Prohibited Flying Environments
1) Visible Moisture 2) Icing Conditions 3) Rain 4) Salt Spray 5) Salt Fog > 30 min
43
Minimum Distance from T-storms and/or Lightning
20 NM
44
Generator Voltage Range
27 - 29 V
45
Generator Current Range
0 - 23.2 A
46
Battery Voltage (Discharging)
18 - 25.2 V
47
Battery Current (Discharging)
2 - 15 A
48
Battery Voltage (Charging)
-18 to -25.2 V
49
Battery Current (Charging)
0.2 to 2.5 A
50
External Voltage
26 - 30 V
51
External Current
2 - 12.5 A
52
Gust Limit for Recovery
10 Knots