Term
| ENGINE FAILURE BELOW 2,000 FEET AGL |
|
Definition
1. Safe Heading — Establish
2. FTS — Deploy |
|
|
Term
| ENGINE FAILURE ABOVE 2,000 FEET AGL |
|
Definition
1. Airspeed — Set 70 kts
2. Safe Heading — Establish
3. FTS Site — Select (PO) |
|
|
Term
| PROPULSION SYSTEM FAILURE (RED) |
|
Definition
1. Altitude — Level
2. Airspeed — 70 kts |
|
|
Term
FUEL SYSTEM FAILURE (RED) /
FUEL FLOW ALERT (HUMS Alert) |
|
Definition
1. Altitude — Level
2. Airspeed — 70 kts |
|
|
Term
| AV HIGH ENGINE TEMPERATURE |
|
Definition
1. Altitude — Level
2. Airspeed — 70 kts |
|
|
Term
| OIL STARVATION (HUMS CAUTION/ALERT) |
|
Definition
1. Altitude — Level
2. Airspeed — 70 kts |
|
|
Term
|
Definition
1. Altitude — Level
2. Airspeed — 70 kts |
|
|
Term
|
Definition
1. Altitude — Level
2. Airspeed — 70 kts
3. Heading — RTB
4. FTS Site — Select (PO) |
|
|
Term
|
Definition
1. Fire, Fire, Fire on AV — Announce (CC)
2. Throttle — Idle
3. Engine — Cut |
|
|
Term
|
Definition
1. Abort, Abort, Abort;Fire on Launcher — Announce(CC)
2. LHCU Launch Switch Cover—Closed(CC)
3. Throttle — Idle
4. Engine — Cut
5. LHCU Pressurize Switch — Off (CC)
5A. LHCU Safe Indicator — Verify (CC)
5B. LHCU HPU Switch — Off (CC) |
|
|
Term
|
Definition
1. Abort, Abort, Abort — Announce
2. LHCU Launch Switch Cover — Closed (CC)
3. Throttle — Idle
4. LHCU Pressurize Switch — Off (CC)
5. LHCU Safe Indicator — Verify (CC)
6. LHCU HPU Switch — Off (CC) |
|
|
Term
|
Definition
1. Safe Heading — Establish
2. Vehicle Lights — All OFF, as required
3. Airspeed — Set
4. Bus Voltage — Monitor for SLA
5. Li — ION Battery Status — > 10 Minutes Remaining |
|
|
Term
| GCS ELECTRICAL POWER FAILURE |
|
Definition
1. Heading — RTB
2. Non-essential Components — Off |
|
|
Term
|
Definition
1. Knob Control — Select
2. Payload — Cage (PO)
AV Uncontrollable
3. FTS — Deploy |
|
|
Term
|
Definition
1. Knob Control — Select
2. Payload — Cage (PO)
AV Uncontrollable / Controllability unverifiable within 10 seconds:
3. FTS — Deploy |
|
|
Term
| IN — FLIGHT SERVO FAILURE |
|
Definition
1. Servo Status — Query
2. AV Controllability — Assess
AV Uncontrollable
3. FTS — Deploy |
|
|
Term
|
Definition
1. Knob Control — Select
2. Safe Heading — Establish
3. Altitude — Cycle |
|
|
Term
|
Definition
1. Knob-Roll — Select
2. Land — ASAP |
|
|
Term
|
Definition
1. Standby — Announce (CC)
1a. LHCU Launch Switch — Release to Hold Position (CC)
1b. LHCU Ready to Launch When Lit Lamp — Illuminated (CC)
1c. LHCU Launch Switch — Launch (CC)
1d. Step 1a — Step 1c: Repeat one more time (CC)
1e. Launcher Fail — Announce (CC)
2. LHCU Launch Switch Cover — Closed (CC)
3. LHCU Pressurize Switch — Off (CC)
4. LHCU Safe When Lit Lamp — Illuminated (CC)
5. LHCU HPU Switch — Off (CC) |
|
|
Term
| TALS ABORT BELOW DECISION POINT |
|
Definition
1. TALS Abort — Announce
2. AV Touchdown — Announce (CC)
3. Engine — Cut (As Required) |
|
|
Term
|
Definition
|
|
Term
| Maximum Continuous Climb RPM |
|
Definition
|
|
Term
| Max 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
| >259º C is allowed during climb to an altitude of 1000 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
| Knobs or Points NAV AOB Maximum |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| TALS Automatic Abort (High) |
|
Definition
|
|
Term
| TALS Automatic Abort (Low) |
|
Definition
|
|
Term
| Alert Displayed (display turns yellow) |
|
Definition
|
|
Term
|
Definition
|
|
Term
| Maximum Reported Airspeed (Descent) |
|
Definition
|
|
Term
| Maximum Commanded Airspeed (Level Flight) |
|
Definition
|
|
Term
| Climb Law - Legacy Wing / Increased Endurance |
|
Definition
|
|
Term
|
Definition
|
|
Term
| Capacity - Legacy Wing / Increased Endurance |
|
Definition
|
|
Term
| GCS Reported Fuel on Ground Limit |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| Max launch weight ≤ 9000' Density Altitude |
|
Definition
|
|
Term
| Max launch weight 9000' to 10500 DA |
|
Definition
|
|
Term
| Max launch weight ≤ 10500 DA IE |
|
Definition
|
|
Term
| Headwind Component (Maximum) |
|
Definition
| 20 kts steady, gusting to 25 kts |
|
|
Term
| Crosswind Component (Maximum) |
|
Definition
| 20 kts steady, gusting to 25 kts |
|
|
Term
| Takeoff Tailwind Component |
|
Definition
| Refer to LAU Nitrogen Pre-charge Pressure Charts in Section 7-4 |
|
|
Term
| Approach Tailwind (at Land AV) |
|
Definition
|
|
Term
| Landing Tailwind Component (Maximum) |
|
Definition
|
|
Term
|
Definition
| Reported airspeeds of greater than 90 KIAS during descent are prohibited. Commanded airspeed in excess of maximum airspeed as defined in Section 7-3. |
|
|
Term
|
Definition
| Flight into forecast moderate or severe icing or any level of known icing conditions is prohibited. |
|
|
