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SEARCH BRIEFING
1. Objective 1.1. Number of Survivors/Description/Medical Condition 1.2. Signaling Devices/Equipment 1.3. Specialized Aircraft Equipment Required2. Search Area3. On Scene Search and Rescue (SAR) Forces/On Scene Commander (OSC) 3.1. Establish ...
MISSION CHECKLISTS
1. Low Level Checklist: 1.1. Route/Hazards – Briefed 1.2. NVGs –On as Required 1.3. Before Landing Checklist – Complete 2. FENCE IN/OUT Checklist: 2.1. F – Fire Power/Fuel – Check Weapons/Fuel Computations 2.2. E – Electronic...
SIGNALS/COMMUNICATIONS
SIGNALS/COMMUNICATIONS/EQUIPMENTFORMATION LIGHT SIGNALS SIGNAL MEANING Single Flash (tail position light) Go to Trail Two Flashes (tail position light) Stagger Left Three Flashes (tail position light) Stagger Right Dot – Dot ...
INSTRUMENT PROCEDURES
1. INSTRUMENT DEPARTURE BRIEFINGNote: Accomplish immediately before initial simulated/actual instrument profile.2. Navigation/Communication Radio Settings3. Departure Instructions/Restrictions4. Emergency Return Approach 4.1. DA (Precision) or MDA (No...
MSN#24199001
Initial Report: "Time: 1202 UTC ( local 10:00) Aircraft: F-16 Callsign: WOOL12/“FANTUM” Location: N36 36 866 W115 26.552 elev 3497ft CFIT - No chute spotted, WOOL11 is on scene. No contact with WOOL12. Contact Fatness 64 on 288.8" -@Jester [Chann...
MSN#24179001
Initial Report: "for pickup - 1xMustard :D" - @Jester [Channel #the-hooch] Mission Generated: 1hr 14min later. (FP Attached) "For whoever gets to it first, Here is FP for MSN# 24179001 w/ current Weather (Subject to change based on response...
[FF-1] Main Rotor Considerations
Dissymmetry of Lift. There is a difference in lift between the advancing half of the rotor disk and the retreating half. In directional flight, the aircraft relative wind is added to the rotational relative wind on the advancing blade and subtracted on the ret...
[FF-3] Tail Rotor Considerations
Tail Rotor Considerations. Many pilots do not appreciate the effect that the tail rotor has onpower applied. The torque indicator displays power supplied by the engines to the entire drive train, not just the main rotor. As with collective changes, if you move...
[FF-2] Retreating Blade Stall
Retreating Blade Stall. The speed of the airflow over the retreating blade (the blade moving away from the direction of flight) decreases as forward speed increases. The retreating blade, however, must produce an amount of lift equal to that of the advancing b...
[FF-4] Power
Settling with Power. Settling with power can occur at any airspeed or altitude combinationwhenever power required exceeds power available. This condition is not to be confused with power settling or vortex ring state. Power Settling or Vortex Ring State. Powe...
[FF-5] Slopes and Dynamic Rollovers
Slope Operations. When the helicopter rests on a slope, the mast is nearly perpendicular to the inclined surface, while the plane of the main rotor must parallel the true horizon or tilt slightly up-slope (refer to the flight manual for specific slope operatio...
[FF-6] Performance and Energy
G-Loading. Load factor, expressed in Gravity (G) units, is the total load imposed on an aircraft, divided by the aircraft weight. Load factor during a turn varies with the angle of bank. Airspeed during a turn does not affect load factor, because for a given b...
[MP-4] Combat Mission Planning Considerations
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