TM 1-1520-238-104-4Change 3Table 4-1.Flight Symbology Definitions – continuedFig. 4-1Ref No.DescriptionSymbol Name6Acceleration CueA vectorial representation of the helicopter longitudinal and lateralacceleration; the display origin is normally the end of the velocity vector. Inthe hover and bob-up modes, when the velocity vector exceeds its maximumscale, the display origin changes to the center of the LOS reticle. TheAcceleration Cue will flash when the HARS inertial platform has gone intofree inertial mode, usually as a result of the LDNS going into memory.7Velocity VectorA vectorial representation of the helicopter longitudinal and lateral groundvelocities; in hover mode, maximum scale is 6 knots groundspeed; intransition mode 60 knots groundspeed. The velocity vector will flash whenthe HARS inertial platform has gone into the free inertial mode if MUX switchis in SEC.8Heading ScaleHelicopter magnetic heading scale.9Cued LOS ReticleA virtual reticle indicating the cued LOS to the appropriate crew member.Used with the cueing dots.10Missile ConstraintsIndicates the required orientation to align the helicopter into constraints forHellfire missile engagements. When all constraints for the mode ofengagement are satisfied, the box will go from ‘dashed’ to ‘solid’.11Radar AltitudeA digital display of radar altitude. Displays in 1-foot increments to 50 feet andin 10-foot increments above 50 feet.12Rate of ClimbAn analog display of rate of climb moving along the left side of the verticalscale. Tick marks designate 500 and 1000 fpm rates of climb or descent.13Radar Altitude VerticalScaleA vertical scale for the analog display of radar altitude. Tick marks designate10-foot increments from 0 to 50-feet, and 50-foot increments from 50 to 200feet. The scale is blanked when radar altitude is greater than 200 feet.14Radar Altitude VerticalTapeAn analog display of radar altitude moving within the vertical scale; alsoblanked above 200 feet.15Skid/Slip Lubber LinesRepresent the limits for ‘ball centered’ flight.16Skid/Slip BallIndicates the amount of skid or slip the helicopter is experiencing.17Cued LOS DOTIndicates the cued LOS location within the field of regard. The cued LOSDOT will flash when the HARS inertial platform has gone into the free inertialmode.18Field of ViewRepresents the instantaneous FOV of the crewmember sensor within thefield of regard.19Sensor Field ofRegardRepresents the total gimbal limits possible for the respective crew membersensor.20High Action DisplayRefer to paragraph 4.28.
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