TM 1-1520-240-10Change 20 4-1-21No.SymbolSourceRange/Description1 Angle of Pitch ScaleHUD System"30_(10_units, tic marks flash when angle of pitch isu"30_)2 Bearing to Waypoint -PointerDoppler0 - 359_ (cursor will invert “V” when aircraft is moving awayfrom the waypoint)3 Compass ReferenceScaleHUD System0 - 359_ (10_ units)4 Aircraft Heading FixIndexHUD SystemFixed Reference Mark5 Angle of Roll - PointerVertical Gyro, Co-pilot"30_(right turn moves pointer to right, pointer flashesu"30_)6 Angle of Roll - ScaleHUD System"30_(10_units)7 Barometric Altitude(MSl)Air Data Trans-ducer-1500 to 20,000 feet (set during adjustment mode)8 Adjust/Program ModeMessageHUD SystemADJ or PROG9 OK/FAILHUD SystemOK or FAIL10 Velocity VectorDoppler0 - 15 knots/15 kilometers, 0-359_11 Rate of Climb PointerAir Data Trans-ducer"2000 feet-per-minute (used with vertical speed scale, No.15)12 Radar Altitude (AGL) -NumericRadar Altimeter,Pilot0 - 1000 feet (0 - 200 feet, 1 foot units; 200 -1000 feet, 10feet units; disappears above 999 feet, and reappears below950 feet)13 Minimum AltitudeWarningRadar Altimeter,PilotBlinking square around symbol - No. 12, set on pilot’s radaraltimeter (use low set index)14 Radar Altitude (AGL)Analog BarRadar Altimeter,Pilot0 - 200 feet (disappears at 250 feet, reappears at 225 feet;digital readout symbol, No. 12)15 AGL Vertical Speed -ScaleHUD System0 -200 feet/"2000 feet-per-minute16 HUD Fail MessageHUD SystemCPM, SDR, SDA, PS, PDU, CPDU, NAV, PGM; can becleared from the display by selecting “ACK” (See NOTE)17 Trim (Slide Ball)Inclinometer"2 balls (left/right)18 MST, MEM, HOOKMessagesMaster CautionPanelMST, MEM, HOOK; cannot be cleared from the display byselecting “ACK”NOTE: After ACK is used to acknowledge a fault, the fault will not reappear until BIT is selected or power is cycledoff and on.Figure 4-1-9. CH-47D HUD Master Mode Symbology Display (Sheet 2 of 3)
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