Honeywell AD-54257@ - Manual

Honeywell AD-54257@

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Table of Contents:

  • Page 2 – Description of Change
  • Page 4 – PROPRIETARY NOTICE
  • Page 5 – Record of Revisions
  • Page 6 – Record of Temporary Revisions
  • Page 7 – List of Effective Pages
  • Page 10 – Table of Contents; Section
  • Page 12 – A FEDERAL AVIATION ADMINISTRATION (FAA); B ENHANCED GROUND–PROXIMITY WARNING; List of Illustrations; Figure
  • Page 15 – List of Tables; Table
  • Page 17 – Introduction; The PRIMUS; WARNING; 60 Digital Weather Radar System.
  • Page 19 – System Configurations
  • Page 20 – PRIMUS
  • Page 22 – Weather Radar Indicator
  • Page 23 – Typical PRIMUS
  • Page 24 – Operating Controls; WC–660 Weather Radar Controller.
  • Page 25 – WI–650/660 Weather Radar Indicator Front Panel View; Alphanumerics are white, and WX is displayed in the mode field.
  • Page 27 – on each side of the aircraft heading. If a return; Selected Range
  • Page 28 – DISPLAY AREA; A rotary switch is used to select the following functions:; OFF– This position turns off the radar system.
  • Page 29 – Rainfall Rate
  • Page 30 – of the aircraft heading. No radar
  • Page 31 – GAIN; TILT; ccw rotation tilts beam downward to –15
  • Page 32 – OFF – This position removes all power from the LSS.; scan or the faster update 24; RANGE
  • Page 33 – WC–660 WEATHER RADAR CONTROLLER OPERATION; WC–660 Weather Radar Controller Configurations
  • Page 34 – This switch position turns on RCT.
  • Page 35 – on each side of the aircraft heading. If a return with certain
  • Page 36 – ccw rotation tilts beam downward 0; OFF – In this position all power is removed from the LSS.
  • Page 37 – RADAR
  • Page 38 – When displaying checklist, the TGT function is inoperative.
  • Page 41 – Normal Operation; PRELIMINARY CONTROL SETTINGS; Table 4–1 gives the power–up procedure for the PRIMUS; Step; Preset Position
  • Page 42 – OUTPUT POWER IS RADIATED IN TEST MODE.
  • Page 43 – Scan Shown
  • Page 44 – Standby
  • Page 45 – of the aircraft centerline.; Radar Mode – Ground Mapping
  • Page 46 – Test Mode; - TEXT FAULT – A plain English text indicating the failure is placed
  • Page 47 – Radar Facts; RADAR OPERATION
  • Page 48 – Positional Relationship of an Airplane and
  • Page 49 – Antenna Beam Slicing Out Cross Section of Storm
  • Page 50 – Sea Returns
  • Page 51 – TILT MANAGEMENT; Radar Beam Illumination High Altitude
  • Page 52 – Radar Beam Illumination Low Altitude
  • Page 53 – When ground targets are displayed, move the tilt angle upward in 1
  • Page 54 – Approximate Tilt Setting for Minimal Ground Target Display
  • Page 56 – Ideal Tilt Angle
  • Page 57 – Convective Thunderstorms; Unaltered Tilt
  • Page 58 – Proper Tilt Technique
  • Page 59 – Fast Developing Thunderstorm; Low Altitude Tilt Management
  • Page 60 – shown in figure 5–16.; Antenna Size and Impact on Tilt Management; look down angle looks down 100 ft per mile.; Rules of Thumb
  • Page 61 – STABILIZATION; Several sources of error exist in any stabilization system.; Dynamic Error; can be detected and compensated. However, the point is; Accelerative Error; LASEREF
  • Page 62 – ) to reduce the effect of lateral; Antenna Mounting Error
  • Page 63 – LEVEL FLIGHT STABILIZATION CHECK; Select the 50–mile range.; Stabilization in Straight and Level Flight Check Procedure
  • Page 64 – Ground Return Indicating Misalignment (Upper Right); wx; Ground Return Indicating Misalignment (Upper Left)
  • Page 65 – Roll Gain Error; Place the aircraft in 20; Stabilization in Turns Check Procedure
  • Page 66 – Symmetrical Ground Returns – Good Roll Stabilization; Understabilization in a Right Turn
  • Page 67 – Overstabilization in a Right Turn; Roll Stabilization Inoperative in a Turn
  • Page 68 – Pitch Gain Error; PITCH STABILIZATION CHECK; Complete the steps listed in table 5–3.; Pitch Stabilization In–Flight Check Procedure
  • Page 69 – Understabilized in Pitch–Up; Overstabilized in Pitch–Up
  • Page 70 – INTERPRETING WEATHER RADAR IMAGES; Weather Radar Images
  • Page 71 – This meeting can form a thunderstorm.
  • Page 72 – Radar and Visual Cloud Mass
  • Page 73 – Squall Line
  • Page 74 – WEATHER DISPLAY CALIBRATION; airborne radars and color families in a Nexrad display. To
  • Page 75 – Display Levels Related to dBZ Levels (Typical)
  • Page 76 – VARIABLE GAIN CONTROL
  • Page 79 – With REACT Selected
  • Page 80 – Shadowing; DO NOT FLY INTO THE SHADOW BEHIND THE CELL.; Turbulence Probability
  • Page 81 – Probability of Turbulence Presence
  • Page 82 – Turbulence levels are listed and described in table 5–8.; Turbulence Levels (From Airman’s Information Manual); Hail Size Probability
  • Page 83 – Spotting Hail
  • Page 84 – Rain Coming From Unseen Dry Hail; Familiar Hailstorm Patterns
  • Page 85 – . Assuming that a storm has dissipated during; Overshooting a Storm
  • Page 86 – to the right. Always switch to long range before entering such; Short– and Long–Blind Alley
  • Page 87 – Azimuth Resolution; Azimuth Resolution in Weather Modes
  • Page 88 – RADOME
  • Page 89 – WEATHER AVOIDANCE; Weather Display; Severe Weather Avoidance Procedures
  • Page 92 – Three of the most common erratic motions are:; Right Turning Echo. This is the most frequently
  • Page 94 – Typical Hook Pattern
  • Page 95 – AVOID V–NOTCH BY 20 MILES; echo movement; V–Notch Echo, Pendant Shape
  • Page 96 – AVOID PENDANT BY 20 MILES; Sixty percent produce funnel clouds or tornadoes.; STORM MOTION; The Classic Pendant Shape
  • Page 97 – AVOID STEEP RAIN GRADIENTS BY 20 MILES
  • Page 98 – Crescent Shape; Line Configurations
  • Page 99 – AVOID LINE ECHO WAVE PATTERNS (LEWP) BY 20 MILES
  • Page 100 – AVOID BOW–SHAPED LINE OF ECHOES BY 20 MILES
  • Page 101 – Additional Hazards; TURBULENCE VERSUS DISTANCE FROM STORM CORE
  • Page 102 – GROUND MAPPING; Ground Mapping Display
  • Page 103 – TILT Setting for Maximal Ground Target Display
  • Page 105 – , the limit recommended; MPEL Boundary
  • Page 106 – PITCH AND ROLL TRIM ADJUSTMENTS; Trim
  • Page 108 – Level Fight Stabilization Check; Select the 50–mile range and GMAP mode.
  • Page 109 – Symmetrical Ground Returns; Ground Return Indicating Misalignment (Right)
  • Page 110 – Ground Return Indicating Misalignment (Left); ROLL OFFSET ADJUSTMENT
  • Page 111 – and is adjustable by the GAIN knob.; In–Flight Roll Offset Adjustment Procedure
  • Page 112 – Roll Offset Adjustment Display – Initial; Roll Offset Adjustment Display – Final
  • Page 113 – PITCH OFFSET ADJUSTMENT; Fly to an altitude of 10,000 feet AGL or greater.; Pitch Offset Adjustment Procedure
  • Page 114 – ROLL STABILIZATION CHECK; Roll Stabilization (While Turning) Check Procedure
  • Page 115 – Symmetrical Ground Returns, Level Flight; Understabilization in a Right Roll
  • Page 116 – Overstabilization in a Right Roll; ROLL GAIN ADJUSTMENT; Roll Gain Adjustment Procedure
  • Page 117 – While flying with a steady roll angle of at least 20
  • Page 119 – Understabilized in Pitch Up
  • Page 120 – PITCH GAIN ADJUSTMENT; Pitch Gain Adjustment Procedure
  • Page 121 – In–Flight Troubleshooting
  • Page 122 – TEST MODE WITH TEXT FAULTS ENABLED; Description; Pilot message; Fault Data Fields
  • Page 123 – Fault Annunciation on Weather Indicator
  • Page 124 – Radar Indication With Text Fault Enabled (On Ground); PILOT EVENT MARKER; 60 System Description and
  • Page 125 – FAULT CODE AND TEXT FAULT RELATIONSHIPS; Table 8–2 lists the relationship between:; Text Faults
  • Page 128 – Table 8–3 describes the pilot messages.; Pilot MSG; Pilot Messages
  • Page 129 – Honeywell Product Support
  • Page 130 – 4–HOUR EXCHANGE/RENTAL SUPPORT CENTERS
  • Page 131 – CUSTOMER SUPPORT CENTERS – NORTH AMERICA (; CUSTOMER SUPPORT CENTERS – REST OF THE WORLD
  • Page 132 – PUBLICATION ORDERING INFORMATION; Additional copies of this manual can be obtained by contacting:; E–MAIL
  • Page 133 – TERMS
  • Page 136 – Federal Aviation Administration
  • Page 137 – Precautions; GENERAL
  • Page 138 – COMBUSTIBLE MATERIALS; SUBJECT: THUNDERSTORMS
  • Page 139 – Hazards; SQUALL LINES
  • Page 140 – C, much of the remaining water
  • Page 141 – Schematic Cross Section of a Thunderstorm; As hailstones fall through air whose temperature is above 0
  • Page 142 – LOW CEILING AND VISIBILITY
  • Page 143 – DO’S AND DON’TS OF THUNDERSTORM FLYING
  • Page 145 – RELATIONSHIP BETWEEN TURBULENCE AND REFLECTIVITY
  • Page 147 – TURBULENCE ABOVE STORM TOPS
  • Page 148 – EXTRAPOLATION TO DIFFERENT CLIMBS
  • Page 149 – Appendix B; Enhanced Ground–Proximity; SYSTEM OPERATION
  • Page 150 – PUSH BUTTON CONTROLS
  • Page 151 – Related EGPWS System Operation; The
  • Page 152 – EGPWS Display; green
  • Page 153 – EHSI Display Over KPHX Airport
  • Page 154 – EGPWS Test; EGPWS Test Display
  • Page 155 – Index
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Summary

Page 2 - Description of Change

Highlights Page 1 of 1 August 2003 HoneywellAerospace Electronic SystemsCES–PhoenixP.O. Box 21111Phoenix, Arizona 85036–1111U.S.A. TO: HOLDERS OF THE PRIMUS R 660 DIGITAL WEATHER RADAR SYSTEM PILOT’S MANUAL, HONEYWELL PUB.NO. A28–1146–111 REVISION NO. 3 DATED AUGUST 2003 HIGHLIGHTS Pages that have b...

Page 4 - PROPRIETARY NOTICE

ASSOCIATE MEMBER Member of GAMA General Aviation Manufacturer’s Association E PRIMUS and LASEREF are U.S. registered trademarks of HoneywellDATA NAV is a U.S. trademarks of Honeywell E 2003 Honeywell International Inc. PROPRIETARY NOTICE This document and the information disclosed herein are proprie...

Page 5 - Record of Revisions

PRIMUS R 660 Digital Weather Radar System A28–1146–111 REV 3 RR–1/(RR–2 blank) Record of Revisions Record of Revisions Upon receipt of a revision, insert the latest revised pages and disposeof superseded pages. Enter revision number and date, insertion date,and the incorporator ’s initials on the Re...

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