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62 Cards in this Set
- Front
- Back
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Max operational RPM |
8000 for 2 mins |
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Max continuous climb RPM |
7800 |
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Max continuous cruise RPM |
7500 |
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Minimum in-flight RPM |
3800 |
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Maximum static full throttle RPM |
7200 |
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Minimum static full throttle RPM |
6300 |
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Rotor temperature operating range on ground/flight |
64-175°C |
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Max continuous cylinder head temperature |
249°C |
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Max transient CHT |
>259°C is allowed on climb to 1000ft AGL |
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Min cylinder head temperature |
80°C |
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Static idle RPM (payload and IFF ON) |
3600-3840 |
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Bus voltage (with engine operating) |
28 +- 2 VDC |
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LIB battery fail |
< 10 min remaining |
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Allowable fluctuation (with no change to electrical load) |
< 3 different values with in 30 seconds |
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Roll KNOBS |
+- 20°AOB |
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Commanded roll tolerance |
+- 6°AOB |
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Roll TALS |
+- 25°AOB |
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Pitch |
+ 20°, -15° |
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Launcher pitch angle (as reported in the GCS) |
8°-12° |
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Maximum commanded airspeed (descent) |
80kts |
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TALS automatic abort |
<52 or > 78 KIAS for 2 seconds |
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Normal range |
65 - 110 KIAS |
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Low airspeed alert |
55 KIAS |
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Turbulence (rough air) |
70 KIAS |
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Descent law |
70 - 90 KIAS |
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Climb law |
62 KIAS |
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Max flight time (reg) |
9 hr |
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Fuel on ground reported in the GCS |
10L |
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Fuel Capacity (reg) |
58L |
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Oil Capacity |
3.1L |
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Service ceiling |
15000 ft MSL |
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Min safe FTS deploy |
500 ft AGL |
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Min altitude |
ELOS |
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Up tp 10,000 ft density altitude |
467 lbs |
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> 10,000 ft density altitude |
450 lbs |
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Maximum tailwind upon selecting "land AV" |
0 kts |
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Maximum headwind/crosswind |
20 kts, gusts to 25 kts |
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Maximum tailwind during TALS auto recover |
5 kts |
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Relative humidity |
95% non-condensing |
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Prohibited maneuver 1 |
Reported airspeed of greater than 90 KIAS during decent
Commanded airspeed in excess of max airspeed chart |
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Prohibited maneuver 2 |
Flight into forcast moderate or servere icing or any known level of icing conditions |
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< 410 LBS < 210 FT |
5 |
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> 410 LBS < 210 ft |
6 |
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< 410 LBS > 210 ft |
7 |
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Min climb out RPM |
6600 RPM up to 800ft AGL |
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> 410 LBS > 210 FT |
8 |
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Propulsion system failure |
1. Altitude - Level 2. Airspeed - 70 kts |
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Autopilot failure |
1. Knobs - select 2. Payload - cage If AV uncontrollable or unable to verify control of AV within 10 seconds: 3. FTS - Deploy |
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AV Generator Failure |
1. Safe heading - Establish 2. AV Lights - Off (as required) 3. Airspeed - Set 4. Lithium-ion Battery Status - Monitor |
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Engine failure above 2000 ft AGL |
1. Airspeed - 70 kts 2. Safe heading - Establish 3. FTS site - select |
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AV fire on launcher |
1. 'Abort, abort, abort fire on launcher!' - Announce (CC) 2. LHCU Launch switch cover - closed (CC) 3. Throttle - idle 4. Engine - cut |
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Oil starvation (hums caution & alert) |
1. Altitude - level 2. Airspeed - 70 kts |
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Tals abort below decision point |
1. 'Tals abort' - Announce 2. 'AV touchdown' - Announce (CC) 3. Engine - cut (as required) |
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Low oil pressure |
1. Altitude - level 2. Airspeed - 70 kts |
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Fuel system failure (fuel flow alert (hums alert)) |
1. Altitude - level 2. Airspeed - 70 kts |
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Magnetometer failure |
1. Knobs Roll - select 2. Land - as soon as possible |
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Engine failure below 2000 ft AGL |
1. Safe heading - Establish 2. FTS - Deploy |
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In-flight servo failure |
1. Servo status - query 2. AV control - assess If AV uncontrollable: 3. FTS - Deploy |
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Uncontrolled flight |
1. Knobs - select 2. Payload - cage If AV uncontrollable: 3. FTS - Deploy |
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Stuck throttle (low rpm) |
1. Knobs - select 2. Safe heading - Establish 3. Altitude - cycle |
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Autolaunch abort |
1. 'Abort, abort, abort!' - Announce 2. LHCU Launch switch cover - closed (CC) 3. Total sticks - select 4. Throttle slider - idle |
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Gcs electical power failure |
1. Heading - RTB 2. Non-essential components - off |
