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Honeywell Aerospace Electronic Systems CES–Phoenix P.O. Box 21111 Phoenix, Arizona 85036–1111 U.S.A. TO: HOLDERS OF THE PRIMUS 660 DIGITAL WEATHER RADAR SYSTEM PILOT’S MANUAL, HONEYWELL PUB. NO. A28–1146–111 REVISION NO. 3 DATED AUGUST 2003 HIGHLIGHTS Pages that have been revised are outlined below. Remove and insert the affected pages listed. The revision number has been added to the bottom of the revised pages and revision bars have been used to indicate the revised or added text. Insert t
ページ3に含まれる内容の要旨
Honeywell Aerospace Electronic Systems CES–Phoenix P.O. Box 21111 Phoenix, Arizona 85036–1111 U.S.A. PRIMUS 660 Digital Weather Radar System Pilot’s Manual Revised August 2003 Printed in U.S.A. Pub. No. A28–1146–111–03 February 1998
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PROPRIETARY NOTICE This document and the information disclosed herein are proprietary data of Honeywell. Neither this document nor the information contained herein shall be used, reproduced, or disclosed to others without the written authorization of Honeywell, except to the extent required for installation or maintenance of recipient’s equipment. NOTICE – FREEDOM OF INFORMATION ACT (5 USC 552) AND DISCLOSURE OF CONFIDENTIAL INFORMATION GENERALLY (18 USC 1905) This document is being furnished in
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PRIMUS 660 Digital Weather Radar System Record of Revisions Upon receipt of a revision, insert the latest revised pages and dispose of superseded pages. Enter revision number and date, insertion date, and the incorporator’s initials on the Record of Revisions. The typed initials H are used when Honeywell is the incorporator. Revision Revision Insertion Number Date Date By 1 Aug 1999 Aug 1999 HI 2 Dec 1999 Dec 1999 HI 3 Aug 2003 Aug 2003 H A28–1146–111 Record of Revisions REV 3 RR–1/(RR–2 blank
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PRIMUS 660 Digital Weather Radar System Record of Temporary Revisions Upon receipt of a temporary revision, insert the yellow temporary revision pages according to the filing instructions on each page. Then, enter the temporary revision number, issue date, and insertion date on this page. Date the Temporary Revision Was Insertion of Removal of Temporary Incorporated Temporary Temporary Revision by a Regular Revision, Revision, No. Issue Date Revision Date/By Date/By
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PRIMUS 660 Digital Weather Radar System List of Effective Pages Original . . 0 . . Feb 1998 Revision . . 1 . . Aug 1999 Revision . . 2 . . Dec 1999 Revision . . 3 . . Aug 2003 Subheading and Page Revision Subheading and Page Revision Title Page 3 3–4 0 3–5 0 Record of Revisions 3–6 0 RR–1/RR–2 3 3–7 0 3–8 0 Record of Temporary Revisions 3–9 0 RTR–1/RTR–2 0 3–10 0 3–11 0 List of Effective Pages 3–12 0 LEP–1 3 3–13 0 LEP–2 3 3–14 0 LEP–3/LEP–4 3 3–15 0
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PRIMUS 660 Digital Weather Radar System Subheading and Page Revision Subheading and Page Revision Radar Facts (cont) Maximum Permissible Exposure Level (MPEL) 5–13 0 6–1/6–2 3 5–14 0 5–15 0 In–Flight Adjustments 5–16 0 7–1 0 5–17 0 7–2 0 5–18 0 7–3 0 5–19 0 7–4 0 5–20 0 7–5 0 5–21 0 7–6 0 5–22 0 7–7 0 5–23 0 7–8 0 5–24 0 7–9 0 5–25 0 7–10 0 5–26 0 7–11 0 5–27 0 7–12 0 5–28 0 7–13 0 5–29 0 7–14 0 5–30 0 7–15/7–16 0 5–31 0
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PRIMUS 660 Digital Weather Radar System Subheading and Page Revision Subheading and Page Revision Appendix A (cont) A–6 0 A–7 0 A–8 0 A–9 0 A–10 0 A–11 0 A–12 0 A–13/A–14 0 Appendix B B–1 1 B–2 1 B–3 1 B–4 1 B–5 1 B–6 1 Index Index–1 1 Index–2 1 Index–3 1 Index–4 1 Index–5 1 Index–6 1 Index–7 1 Index–8 1 A28–1146–111 List of Effective Pages REV 3 LEP–3/(LEP–4 blank)
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PRIMUS 660 Digital Weather Radar System Table of Contents Section Page 1. INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-1 2. SYSTEM CONFIGURATIONS . . . . . . . . . . . . . . . . . 2-1 3. OPERATING CONTROLS . . . . . . . . . . . . . . . . . . . . 3-1 WI–650/660 Weather Radar Indicator Operation . . . 3-1 WC–660 Weather Radar Controller Operation . . . . . 3-10 4. NORMAL OPERATION . . . . . . . . . . . . . . . . . . . . . . . 4-1 Preliminary Control Settings . . . . .
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PRIMUS 660 Digital Weather Radar System Table of Contents (cont) Section Page 5. RADAR FACTS (CONT) Additional Hazards . . . . . . . . . . . . . . . . . . . . . . . . 5-55 Ground Mapping . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-56 6. MAXIMUM PERMISSIBLE EXPOSURE LEVEL (MPEL) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-1 7. IN–FLIGHT ADJUSTMENTS . . . . . . . . . . . . . . . . . . 7-1 Pitch and Roll Trim Adjustments . . . . . . . . . . . . . . .
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PRIMUS 660 Digital Weather Radar System Table of Contents (cont) A FEDERAL AVIATION ADMINISTRATION (FAA) ADVISORY CIRCULARS (CONT) Subject: Thunderstorms . . . . . . . . . . . . . . . . . . . . . . A–3 Purpose . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A–3 Cancellation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A–3 Related Reading Material . . . . . . . . . . . . . . . . . . . A–3 General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
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PRIMUS 660 Digital Weather Radar System Table of Contents (cont) List of Illustrations (cont) Figure Page 5–1 Positional Relationship of an Airplane and Storm Cells Ahead as Displayed on Indicator . . . . . . . . . 5-2 5–2 Antenna Beam Slicing Out Cross Section of Storm During Horizontal Scan . . . . . . . . . . . . . . . . . . . . . . 5-3 5–3 Sea Returns . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-4 5–4 Radar Beam Illumination High Altitude 12–Inch Radiator . . . . . .
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PRIMUS 660 Digital Weather Radar System Table of Contents (cont) List of Illustrations (cont) Figure Page 5–32 Probability of Turbulence Presence in a Weather Target . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-35 5–33 Hail Size Probability . . . . . . . . . . . . . . . . . . . . . . . . . . 5-37 5–34 Rain Coming From Unseen Dry Hail . . . . . . . . . . . . 5-38 5–35 Familiar Hailstorm Patterns . . . . . . . . . . . . . . . . . . . . 5-38 5–36 Overshooting a Stor
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PRIMUS 660 Digital Weather Radar System Table of Contents (cont) List of Illustrations (cont) Figure Page B–1 EHSI Display Over KPHX Airport With the EGPWS Display . . . . . . . . . . . . . . . . . . . . . . . . . . . . B–5 B–2 EGPWS Test Display . . . . . . . . . . . . . . . . . . . . . . . . . B–6 List of Tables Table Page 2–1 Dual Control Mode Truth Table . . . . . . . . . . . . . . . . . 2-3 2–2PRIMUS 660 Weather Radar Equipment List . . . . . 2-4 3–1 Target Alert Characteristics . . . .
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PRIMUS 660 Digital Weather Radar System Table of Contents (cont) List of Tables (cont) Table Page 7–4 Pitch Offset Adjustment Procedure . . . . . . . . . . . . . 7-8 7–5 Roll Stabilization (While Turning) Check Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-9 7–6 Roll Gain Adjustment Procedure . . . . . . . . . . . . . . . 7-11 7–7 Pitch Stabilization Check Procedure . . . . . . . . . . . . 7-12 7–8 Pitch Gain Adjustment Procedure . . . . . . . . . . . . . . 7-15
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PRIMUS 660 Digital Weather Radar System 1. Introduction The PRIMUS 660 Digital Weather Radar System is a lightweight, X–band digital radar with alphanumerics designed for weather detection (WX) and ground mapping (GMAP). The primary purpose of the system is to detect storms along the flightpath and give the pilot a visual indication in color of their rainfall intensity. After proper evaluation, the pilot can chart a course to avoid these storm areas. WARNING THE SYSTEM PERFORMS THE FUNCTIONS
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PRIMUS 660 Digital Weather Radar System The radar indicator is equipped with the universal digital interface (UDI). This feature expands the use of the radar indicator to display information such as checklists, short and long range navigation displays (when used with a Honeywell DATA NAV system) and electrical discharge data from Honeywell’s LSZ–850 Lightning Sensor System (LSS). NOTE: Refer to Honeywell Pub. 28–1146–54, LSZ–850 Lightning Sensor System Pilot’s Handbook, for more information.
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PRIMUS 660 Digital Weather Radar System 2. System Configurations The PRIMUS 660 Digital Weather Radar System can be operated in many configurations to display weather or ground mapping information on a radar indicator, electronic flight instrument system (EFIS) display, multifunction display (MFD), or on a combination of these displays. The various system configurations are summarized in the following paragraphs and shown in figure 2–1. NOTE: Other configurations are possible but not illustr
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PRIMUS 660 Digital Weather Radar System NOTES: 1. When WAIT, SECTOR SCAN, or FORCED STANDBY are activated, the radar operates as if in single controller configuration. This is an exception to the ability of each pilot to independently select modes. 2. In the dual configuration, the pilots can use the slave feature to optimize the update rate of each side’s weather radar display to meet the needs of the situation. With one controller turned off, both cockpit displays are updated on every sweep
