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HELICOPTER REGISTRATION NO. * * * * * THIS SUPPLEMENT MUST BE CARRIED IN THE HELICOPTER AT ALL TIMES IF EQUIPPED WITH THE RA-4500 RADAR ALTIMETER. CHAPTERS 1, 2, 3, AND 4 ARE FAA APPROVED. FAA APPROVED BY: TIMOTHY P. SMYTH, MANAGER...
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UNCONTROLLED COPY WHEN DOWNLOADED OR PRINTED INTENTIONALLY LEFT BLANK Report No. 28-AC-071 Oct 20/15 This electronic document is not linked to a subscription for revision control or distribution. Refer to the Optional Equipment Supplement Publications Status link under the Technical Support Page of the Enstrom Helicopter website for the current revision level of this Rotorcraft Flight Manual Supplement.
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UNCONTROLLED COPY WHEN DOWNLOADED OR PRINTED ENSTROM 480B RFM SUPPLEMENT LOG OF REVISIONS Rev. Date FAA Approved Mar 28/16 R. D. McElroy Approved by the Manager, Southwest Flight Test Section, AIR-713 Federal Aviation Administration Ft. Worth, TX Rev. 1 Report No. 28-AC-071 Mar 16/18 This electronic document is not linked to a subscription for revision control or distribution.
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UNCONTROLLED COPY WHEN DOWNLOADED OR PRINTED ENSTROM 480B RFM SUPPLEMENT EASA LOG OF REVISIONS FAA Approval Rev. Date EASA Approved on Behalf of EASA Rev. 1 Report No. 28-AC-071 Mar 16/18 This electronic document is not linked to a subscription for revision control or distribution. Refer to the Optional Equipment Supplement Publications Status link under the Technical Support Page of the Enstrom Helicopter website for the current revision level of this Rotorcraft Flight Manual Supplement.
UNCONTROLLED COPY WHEN DOWNLOADED OR PRINTED ENSTROM 480B RFM SUPPLEMENT ROTORCRAFT FLIGHT MANUAL SUPPLEMENT RA-4500 RADAR ALTIMETER TABLE OF CONTENTS CHAPTER DESCRIPTION PAGE Supplement Cover Page Log of Revisions ..........i EASA Log of Revisions ....... ii Table of Contents........iii List of Figures ...........
UNCONTROLLED COPY WHEN DOWNLOADED OR PRINTED ENSTROM 480B RFM SUPPLEMENT ROTORCRAFT FLIGHT MANUAL SUPPLEMENT RA-4500 RADAR ALTIMETER LIST OF FIGURES FIGURE DESCRIPTION PAGE RA-4500 System Interface ......7-2 RAD-40 Display Panel ......7-2 LIST OF TABLES TABLE DESCRIPTION PAGE Intro-1 List of Abbreviations ...... INTRO-2 Approved Software Version .....1-1...
UNCONTROLLED COPY WHEN DOWNLOADED OR PRINTED ENSTROM 480B RFM SUPPLEMENT LIST OF EFFECTIVE PAGES PAGE DATE Mar 16/18 Mar 16/18 Mar 16/18 Oct 20/15 Mar 16/18 Oct 20/15 INTRO-1 Oct 20/15 INTRO-2 Oct 20/15 Oct 20/15 Oct 20/15 Oct 20/15 Oct 20/15 Oct 20/15 Oct 20/15...
UNCONTROLLED COPY WHEN DOWNLOADED OR PRINTED ENSTROM 480B RFM SUPPLEMENT INTENTIONALLY LEFT BLANK Report No. 28-AC-071 Oct 20/15 This electronic document is not linked to a subscription for revision control or distribution. Refer to the Optional Equipment Supplement Publications Status link under the Technical Support Page of the Enstrom Helicopter website for the current revision level of this Rotorcraft Flight Manual Supplement.
INTRO-1 INTRODUCTION Intro-1. General This supplement contains the operating instructions, procedures, and limitations for the RA-4500 Radar Altimeter. The supplement is divided into two basic parts, the FAA approved RFM Supplement and Supplemental Data provided by the Enstrom Helicopter Corporation (Enstrom).
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UNCONTROLLED COPY WHEN DOWNLOADED OR PRINTED INTRO-2 ENSTROM 480B RFM SUPPLEMENT INTENTIONALLY LEFT BLANK Report No. 28-AC-071 Oct 20/15 This electronic document is not linked to a subscription for revision control or distribution. Refer to the Optional Equipment Supplement Publications Status link under the Technical Support Page of the Enstrom Helicopter website for the current revision level of this Rotorcraft Flight Manual Supplement.
1-2. Software Version The system must utilize the approved software version listed in Table 1-1. Table 1-1. Approved Software Version Approved Software Version Component (or later FAA approved version) RA-4500 300A RAD-40 0200 FAA Approved: Mar 28/16 Report No. 28-AC-071 Oct 20/15 This electronic document is not linked to a subscription for revision control or distribution.
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UNCONTROLLED COPY WHEN DOWNLOADED OR PRINTED ENSTROM 480B RFM SUPPLEMENT INTENTIONALLY LEFT BLANK FAA Approved: Mar 28/16 Report No. 28-AC-071 Oct 20/15 This electronic document is not linked to a subscription for revision control or distribution. Refer to the Optional Equipment Supplement Publications Status link under the Technical Support Page of the Enstrom Helicopter website for the current revision level of this Rotorcraft Flight Manual Supplement.
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UNCONTROLLED COPY WHEN DOWNLOADED OR PRINTED ENSTROM 480B RFM SUPPLEMENT CHAPTER 2. NORMAL PROCEDURES 2-1. General Refer to the basic RFM 2-2. Starting Engine (ref. basic RFM paragraph 2-19) 1. Check that the RAD-40 switch is set to ON. 2. After avionics master switch ON, check the RAD-40 status display sequence as follows: a.
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UNCONTROLLED COPY WHEN DOWNLOADED OR PRINTED ENSTROM 480B RFM SUPPLEMENT INTENTIONALLY LEFT BLANK FAA Approved: Mar 28/16 Report No. 28-AC-071 Oct 20/15 This electronic document is not linked to a subscription for revision control or distribution. Refer to the Optional Equipment Supplement Publications Status link under the Technical Support Page of the Enstrom Helicopter website for the current revision level of this Rotorcraft Flight Manual Supplement.
UNCONTROLLED COPY WHEN DOWNLOADED OR PRINTED ENSTROM 480B RFM SUPPLEMENT CHAPTER 3. EMERGENCY PROCEDURES 3-1. General Refer to the basic RFM. 3-2. Abnormal Procedures 1. Four dashes in the altitude field are displayed if the altimeter cannot guarantee the validity of the altitude. If this occurs below 2,500 feet AGL: a.
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UNCONTROLLED COPY WHEN DOWNLOADED OR PRINTED ENSTROM 480B RFM SUPPLEMENT INTENTIONALLY LEFT BLANK FAA Approved: Mar 28/16 Report No. 28-AC-071 Oct 20/15 This electronic document is not linked to a subscription for revision control or distribution. Refer to the Optional Equipment Supplement Publications Status link under the Technical Support Page of the Enstrom Helicopter website for the current revision level of this Rotorcraft Flight Manual Supplement.
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UNCONTROLLED COPY WHEN DOWNLOADED OR PRINTED ENSTROM 480B RFM SUPPLEMENT CHAPTER 4. PERFORMANCE DATA 4-1. General Refer to the basic RFM. FAA Approved: Mar 28/16 Report No. 28-AC-071 Oct 20/15 This electronic document is not linked to a subscription for revision control or distribution. Refer to the Optional Equipment Supplement Publications Status link under the Technical Support Page of the Enstrom Helicopter website for the current revision level of this Rotorcraft Flight Manual Supplement.
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UNCONTROLLED COPY WHEN DOWNLOADED OR PRINTED ENSTROM 480B RFM SUPPLEMENT INTENTIONALLY LEFT BLANK FAA Approved: Mar 28/16 Report No. 28-AC-071 Oct 20/15 This electronic document is not linked to a subscription for revision control or distribution. Refer to the Optional Equipment Supplement Publications Status link under the Technical Support Page of the Enstrom Helicopter website for the current revision level of this Rotorcraft Flight Manual Supplement.
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UNCONTROLLED COPY WHEN DOWNLOADED OR PRINTED ENSTROM 480B RFM SUPPLEMENT CHAPTER 6. WEIGHT/BALANCE AND LOADING 6-1. General Refer to the basic RFM. Report No. 28-AC-071 Oct 20/15 This electronic document is not linked to a subscription for revision control or distribution. Refer to the Optional Equipment Supplement Publications Status link under the Technical Support Page of the Enstrom Helicopter website for the current revision level of this Rotorcraft Flight Manual Supplement.
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UNCONTROLLED COPY WHEN DOWNLOADED OR PRINTED ENSTROM 480B RFM SUPPLEMENT INTENTIONALLY LEFT BLANK Report No. 28-AC-071 Oct 20/15 This electronic document is not linked to a subscription for revision control or distribution. Refer to the Optional Equipment Supplement Publications Status link under the Technical Support Page of the Enstrom Helicopter website for the current revision level of this Rotorcraft Flight Manual Supplement.
4. The RA-4500 radar altimeter system is powered by the aircraft electrical system and is protected by a 3 amp circuit breaker (RA) located on the lower left side of the circuit breaker panel.
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(RAD-40) Tone Generator (if equipped) ANTENNA ANTENNA Audio Panel/ VOX/ICS Figure 7-1. RA-4500 System Interface Table 7-1. Altitude Display Sensitivity Altitude AGL Shown to Nearest -99 to 120 feet 1 foot 120 to 200 feet 2 feet 200 to 500 feet...
UNCONTROLLED COPY WHEN DOWNLOADED OR PRINTED ENSTROM 480B RFM SUPPLEMENT 7-2. Power On 1. After power on, the RAD-40 performs a set of self-tests and a display test. The RAD-40 software version will display for approximately 3 seconds during the self-test. The RAD-40 will then display the altitude information.
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UNCONTROLLED COPY WHEN DOWNLOADED OR PRINTED ENSTROM 480B RFM SUPPLEMENT c. Above 2,500 feet AGL, the unit may unlock and attempt to relock causing erratic altitude output. d. Rapid Descent - The radar system provides normal operation at a descent rate of 1,500 feet per minute or less below 2,000 feet AGL.
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