Term
| ENGINE FAILURE BELOW 2,000 FT AGL |
|
Definition
Safe Heading - Establish
FTS - Deploy |
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Term
| ENGINE FAILURE ABOVE 2,000 FT AGL |
|
Definition
Airspeed - Set 70 Kts
Safe Heading - Establish
FTS Site - Select (PO) |
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Term
| PROPULSION SYSTEM FAILURE (RED) |
|
Definition
Altitude - Level
Airspeed - 70 Kts |
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Term
FUEL SYSTEM FAILURE (RED)/
FUEL FLOW ALERT
(HUMS ALERT) |
|
Definition
Altitude - Level
Airspeed - 70 Kts |
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Term
| AV HIGH ENGINE TEMPERATURE |
|
Definition
Altitude - Level
Airspeed - 70 Kts |
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Term
| OIL STARVATION (HUMS CAUTION/ALERT) |
|
Definition
Altitude - Level
Airspeed - 70 Kts |
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Term
|
Definition
Altitude - Level
Airspeed - 70 Kts |
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|
Term
|
Definition
Altitude - Level
Airspeed - 70 Kts
Heading - Return to Base (RTB)
FTS Site - Select (PO) |
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|
Term
|
Definition
Fire, Fire, Fire on AV - Announce (CC)
Throttle - Idle
Engine - Cut |
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|
Term
|
Definition
Abort, Abort, Abort; Fire on Launcher- Announce (CC)
LHCU Launch Switch Cover - Closed (CC)
Throttle - Idle
Engine - Cut
LHCU Pressure Switch - Off (CC)
LHCU Safe Indicator - Verify (CC)
LHCU HPU Switch - Off (CC) |
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|
Term
|
Definition
Abort, Abort, Abort - Announce
LHCU Launch Switch Cover - Closed (CC)
Throttle - Idle
LHCU Pressure Switch - Off (CC)
LHCU Safe Indicator - Verify (CC)
LHCU HPU Switch - Off (CC) |
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|
Term
|
Definition
Safe Heading - Establish
Vehicle Lights - All OFF, as required
Airspeed - Set
Bus Voltage - Monitor for SLA
Li-ION Battery Status- >10 Minutes Remaining |
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|
Term
| GCS ELECTRICAL POWER FAILURE |
|
Definition
Heading - Return to Base (RTB)
Non-essential Components - Off |
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|
Term
|
Definition
Knob Control - Select
Payload - Cage (PO)
AV Uncontrollable
FTS- Deploy |
|
|
Term
|
Definition
Knob Control - Select
Payload - Cage (PO)
AV Uncontrollable
FTS- Deploy |
|
|
Term
|
Definition
Servo Status - Query
AV Controllability - Assess
AV Uncontrollable
FTS- Deploy |
|
|
Term
|
Definition
Knob Control - Select
Safe Heading - Establish
Altitude - Cycle |
|
|
Term
|
Definition
Knob- Roll - Select
Land - ASAP |
|
|
Term
|
Definition
Standby - Announce (CC)
LHCU Launch Switch - Release to Hold Position (CC)
LHCU Ready to Launch When Lit Lamp- Illuminated (CC)
LHCU Launch Switch - Launch (CC)
Step 1a - Step 1c: Repeat one more time (CC)
Launcher Fail - Announce (CC)
LHCU Launch Switch Cover - Closed (CC)
LHCU Pressure Switch - Off (CC)
LHCU Safe When Lit Lamp - Illuminated (CC)
LHCU HPU Switch - Off (CC)
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|
|
Term
| TALS ABORT BELOW DECISION POINT |
|
Definition
TALS Abort - Announce
AV Touchdown - Announce (CC)
Engine - Cut (As Required) |
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|
Term
|
Definition
|
|
Term
| MAXIMUM CONTINUOUS CLIMB RPM |
|
Definition
|
|
Term
| MAXIMUM CONTINUOUS CRUISE RPM |
|
Definition
|
|
Term
|
Definition
|
|
Term
| MAXIMUM STATIC FULL THROTTLE RPM |
|
Definition
|
|
Term
| MINIMUM STATIC FULL THROTTLE RPM |
|
Definition
|
|
Term
| ROTOR TEMPERATURE OPERATING RANGE |
|
Definition
|
|
Term
| MAX CONTINUOUS CYLINDER HEAD TEMPERATURE |
|
Definition
|
|
Term
| MAX TRANSIENT CYLINDER HEAD TEMPERATURE |
|
Definition
| > 259° C IS ALLOWED DURING CLIMB TO AN ALTITUDE OF 1,000 FT AGL |
|
|
Term
| MIN CYLINDER HEAD TEMPERATURE |
|
Definition
|
|
Term
| STATIC IDLE RPM (Payload and IFF on) |
|
Definition
|
|
Term
| BUS VOLTAGE (with engine operating) |
|
Definition
|
|
Term
| BATTERY FAIL- Lithium Ion Battery |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| TALS AUTOMATIC ABORT (HIGH) |
|
Definition
|
|
Term
| TALS AUTOMATIC ABORT (LOW) |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
| REFER TO MAXIMUM COMMANDED AIRSPEED CHART |
|
|
Term
| MAXIMUM REPORTED AIRSPEED (DESCENT) |
|
Definition
|
|
Term
CLIMB LAW-
LEGACY WING
INCREASED ENDURANCE |
|
Definition
|
|
Term
|
Definition
|
|
Term
FUEL CAPACITY
LEGACY WING
INCREASED ENDURANCE |
|
Definition
|
|
Term
| FUEL ON GROUND LIMIT W/ELECTRIC FUEL PUMP |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| MAX LAUNCH WEIGHT < OR EQUAL TO 9000' DENSITY ALTITUDE |
|
Definition
|
|
Term
| MAX LAUNCH WEIGHT 9000' TO 10,500 DA |
|
Definition
|
|
Term
| MAX LAUNCH WEIGHT < OR EQUAL TO 10,500 DA IE |
|
Definition
|
|
Term
| MAXIMUM HEADWIND/CROSSWIND |
|
Definition
|
|
Term
| TAKEOFF TAILWIND COMPONENT |
|
Definition
| REFER TO LAU NITROGEN PRE-CHARGE PRESSURE CHART |
|
|
Term
| APPROACH TAILWIND (AT LAND AV) |
|
Definition
|
|
Term
| LANDING TAILWIND COMPONENT (MAXIMUM) |
|
Definition
|
|
Term
|
Definition
REPORTED AIRSPEED OF GREATER THAN 90 KIAS DURING DESCENT ARE PROHIBITED
COMMANDED AIRSPEEDS IN EXCESS OF MAXIMUM AIRSPEED AS DEFINED IN MAXIMUM AIRSPEED CHART |
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|
Term
|
Definition
| FLIGHT INTO FORECAST MODERATE OR SEVERE ICING OR ANY LEVEL OF KNOWN ICING CONDITIONS IS PROHIBITED |
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