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bhaynie
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Ground Taxi
- -ground track +/-3 ft
- -27-30% TQ
- -May need more for high gross weights, slopping terrain
- Note:may reduce TQ to 22-24 for temp periods minimal cyclic displacement
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Hover Flight
- -Announce intentions use of hold modes
- -Announce when terminate
- -Announce forced landing or SE flyaway plan
- -Announce hover height
- -Check for Proper Control Response and CG
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VMC Take Off
- -Maintain heading +/-10 below 50' or until clear of obstacles (through ETL for min power TO)
- -accelerate to desired airspeed +/-10 knots
- -Apply TO power until desired altitude, VSSE AS or as conditions permit
- -Announce type of TO and abort point
- -Determine dir and type of TO by analyzing power available, wind, long axis and obstacles
- VMC TO from ground (10% above hover power)
- VMC TO from hover (10% above hover power)
- VMC level acceleration TO (10% above hover power if available)
- -when conditions permit accel through VSSE prior to climb
- -maintain heading 50' AGL or clear of obstacles then place in trim
- VMC limited power TO (hover power)
- (select ENG page and monitor TQ and TGT during TO)
- -Announce and zero the stabilator
- From Hover(hover power limit)
- establish climb after ETL (consider accel to MAX END/R/C prior to climb)
- Note - after ETL for acceleration a 5 deg nose low is recommended
- VMC TO sand/dust (Max TQ available)
- -select ENG page and FLT page
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VMC Approach
- -Announce when begin approach
- -Announce terminate hover/ground, intended point of landing, any deviation
- -Announce use of manual stabilator
- -evaluate wind direction and magnitude
- -below 50' AGL align with landing direction
- VMC to mountain/pinnacle brief escape route in a case of go-around
- -reduce AS to slightly above ETL but not below min Dual Engine AS when OGE power is not available until the rate of closure can be determined
- -go around should be determined before going below ETL
- VMC to confinded area-reconnaissance - size, suitability of surface, barriers to approach, direction TD point, TO dir, winds
- -perform low recon
- -go around should be determined before going below ETL
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Slope Operations
- -heading +/-5 deg
- -Brief limits 7 nose up, 12 nose down, 10 roll
- -Brief dynamic roll-over pivot ppoint, rolling motion, exceed critical angle
- -Set the brakes
- -Select a FLT page
- -put AC in wind, if possible
- -adjust to center cyclic and simultaneously lower collective with no less than 25% TQ
- -Before TO, announce initiation of ascent
- -neutral cyclic until 25% TQ
- -abort landing if - upslope landing gear begins to slide, AC brakes do not hold, cyclic stop encountered, comfort margin exceeded
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Roll-On Landing
- -Announce intent to perform roll-on, intended point of landing, and breaking
- -TD at or above ETL
- -Landing alignment +/-5 deg
- -before TD, confirm brakes released, tail wheel locked and area suitable for the landing
- -50' align with runway
- -when simulating IGE power limited establish admin power 10% below hover power
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Single Engine Landing
- -Airspeed at or above VSSE until 10 to 20ft above TD
- -Constant approach angle to first 1/3 of usable landing surface
- -alignment +/-5 deg
- -Announce intended point of landing and braking
- -prior to TD confirm brakes released, tail wheel is locked and area suitable for landing
- -below 50' AGL align with landing direction
- -maintain VSSE until 10 to 20 ft above TD
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