PULSELITE STARLIGHT INSTALLATION MANUAL MODEL 2401S
Contents
1. 1 1 Revise number of output channels 2 12 Revise connector reference numbers 2 14 Revise connector pinout B 2 3 Revise switch function 2 6 Revise Figure 2 8 Block Diagram C 2 6 Revise Pulselite CB specification in diagram 2 7 Revise wording to reflect values of circuit breaker REVISION C 02 15 2001 L FAA Inventory PULSELIT 2401S 805 1C doc DATE 01 20 00 01 20 00 01 20 00 11 27 00 11 27 00 02 15 01 02 15 01 PAGE NAME DJC DJC DJC DJC DJC MAO MAO PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 24015 1 GENERAL INFORMATION 1 1 INTRODUCTION This manual contains information regarding the physical mechanical and electrical characteristics as well as installation information pertaining to the Precise Flight Pulselite Model 24015 Control Unit For maintenance and repair information contact Precise Flight Inc 1 22 PRODUCT DESCRIPTION The Pulselite Model 24015 Control Units are a compact set of electrical components that will apply regulated pulsing power to the landing taxi or recognition lights instead of the normal steady on The Pulselite connects easily to an aircraft s external lighting system and may be installed on a wide variety of aircraft with differing light sequence combinations The control circuit of the Pulselite requires 24 28VDC The four separate controlled power circuits of the 2401S Model are to pulse four DC Powered2. The ground test results shall be recorded in the permanent aircraft records by the installing mechanic or a mechanic with the proper ratings 3 2 1 Procedures During the following tests the aircraft shall be supplied with adequate aircraft power at or above the minimum bus voltage for the aircraft The airplane should be located for proper radio reception and radar operation usually outside 3 2 2 Communications A Select Comm to a local frequency in the lower end of the COMM frequency band Check for clarity of reception and background noise with all Pulselite equipment operating Repeat for all Comm radios Remarks B Select Comm to a local frequency in the upper end of the COMM frequency band Check for clarity of reception and background noise with all Pulselite equipment operating Repeat for all Comm radios Remarks REVISION C 02 15 2001 PAGE 3 3 L FAA Inventory PULSELIT 2401S 805 1C doc PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 2401S C Verify that the intercom is free from noise and interference caused by the Pulselite installation Remarks 3 2 3 Ground Navigation Systems A VOR DME 1 Select VOR 1 receiver to a local frequency center CDI needle of HSI with TO indication Listen for background noise 2 Switch Pulselite equipment on and off check for interference and needle deviation 3 Repeat for all other VHF NAV radio
3. factory Contact Precise Flight Inc for a warranty return authorization requests for warranty payment must be submitted on a standard warranty claim form accompanied by the dealer invoice Authorized warranty work performed by the dealer will be limited to removal and re installation of units on an exchange basis Precise Flight Inc will bear the cost of warranty returns both ways via UPS surface delivery only Precise Flight reserves the right to use reconditioned parts in repairing the product or to use reconditioned units as warranty replacements For technical information and service call 1 800 547 2558 REVISION C 02 15 2001 PAGE 5 1 L FAA Inventory PULSELIT 2401S 805 1C doc 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 24015 6 APPENDIX A 6 1 1 PARTS LIST REVISION C 02 15 2001 L FAA Inventory PULSELIT 2401S 805 1C doc PRECISE FLIGHT INC PAGE 6 1
4. faulty connections Refer to Advisory Circular 43 13 2A NOTE Precise Flight recommends that Mil W 22759 wiring be utilized in the Pulselite installation DO NOT USE ALUMINUM WIRE NOTE Wiring precautions A Observe proper cable routing i e avoid tie wrap joining power lines to antenna leads intercom or radio leads B Be sure that all connections are sound i e avoid frayed or split conduit ends C Avoid sharp bends or undue strain on cables 2 7 1 Electrical Installation A After the Pulselite Control Unit has been properly mounted determine the lighting pulse mode Find the total wattage of the lamp s connected to the Pulselite Control Unit Divide the highest total wattage by the voltage The result will be the highest amperage rating on the Pulselite Control Unit Amperages should not exceed 20 amps or 600 Watts DC See Example below REVISION C 02 15 2001 PAGE 2 5 L FAA Inventory PULSELIT 2401S 805 1C doc PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 24015 PULSELITE CONTROL UNIT MODEL 2401S J2 1 AIN EXT LTS ls 28V DC A CHAT CH AT QUT A AIRCRAFT EXTERNAL BUS EXT LTS T eee E CH 2 PT US I DC PWR IN C CH C1 CH A2 OUT a AIRCRAFT EXTERNAL LIGHT 600 WATT MAX l x EXT LTS 28 VOLT DC 28 VDC AIRCRAFT EXTERNAL LIGHTS DC J
5. 28 VDC Switching Voltage Model 2401S 0 05 amps 600 Watt DC 4 Less than 200 ft AGL at Night amp IMC Conditions 50 to 158 F 45 C to 70 C 43 48 Pulses per minute 2 lights On 2 lights off Full power during Pulse Slight resistance through Pulselite Control Unit 02 15 2001 PAGE 1 2 sm PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 24015 1 5 UNITS AND ACCESSORIES SUPPLIED Pulselite Model 2401S Kit including a Pulselite Control Unit b Copy of the Supplemental Type Certificate c Switches or Switch Specification d Wire Harness or Wiring Harness Drawing e Installation Wiring Diagrams f Installation Drawing 1 6 INSTALLATION APPROVAL BASIS The person who performs or supervises the installation of the Pulselite Model 2401S may be required to prepare FAA form 337 See Fig 1 7 for a Sample Description of Work Accomplished Data that can be used as a basis for approval for return to service are A AC 43 13 1A Acceptable Methods Techniques and Practices Aircraft Inspection and Repair B AC 43 13 2A Acceptable Methods Techniques and Practices Aircraft Alterations C FAA approved Manufacturer s Installation Instructions Equipment installation procedures do not differ significantly among various aircraft The installation and operation of the Pulselite Model 24015 does not materially affect the aircraft operation or performance
6. 547 2558 PULSELITE MODEL 24015 1 10 AIRCRAFT CERTIFICATION Unless otherwise provided the Pulselite Model 2401S is approved by the following STC s 1 Type of Certification Supplemental Type Certificate 2 Certification Number NONE 3 Certification Basis Approved Model Listing 4 Certification Date NONE REVISION C 02 15 2001 PAGE 1 6 L FAA Inventory PULSELIT 2401S 805 1C doc ay PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 2401S 2 INSTALLATION 2 1 GENERAL The Pulselite Model 2401S should be installed according to this manual and AC 43 13 1A and 2A Cable harnesses and mechanical supports must be fabricated by the installing agency to these requirements or supplied by Precise Flight for specific aircraft installations This section contains interconnect diagrams mounting dimensions and other information pertaining to a Pulselite installation 2 2 UNPACKING AND INSPECTION Exercise care when unpacking the equipment Make a visual inspection of the unit for evidence of damage incurred during shipment If a claim for damage is to be made save the shipping container to substantiate the claim The claim should be filed with the transportation company Retain the container and packaging material after the equipment has been removed should equipment storage or reshipment become necessary 2 3 INITIAL BENCH CHECK Every Pulselite Model 2401S has been checke
7. INSTALLATION REPORT NO 08051 Serial Number PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE STARLIGHT INSTALLATION MANUAL MODEL 2401S THIS DOCUMENT CONTAINS PROPRIETARY INFORMATION ON THE PRECISE FLIGHT INC COMPANY AND ITS RECEIPT OR POSSESSION DOES NOT CONVEY ANY RIGHTS TO REPRODUCE DISCLOSE ITS CONTENTS OR TO MANUFACTURE USE OR SELL ANYTHING IT MAY DESCRIBE REPRODUCTION DISCLOSURE USE WITHOUT SPECIFIC WRITTEN AUTHORIZATION OF THE PRECISE FLIGHT INC COMPANY IS STRICTLY FORBIDDEN REVISION C 02 15 2001 PAGE i L FAA Inventory PULSELIT 2401S 805 1C doc REVISION C L FAA InventoryWPULSELIT 2401S 805 1C doc 02 15 2001 PAGE ii E PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 2401S TABLE OF CONTENTS TABLE OF CONTENTS LIST OF ACTIVE PAGES REVISIONS 1 GENERAL INFORMATION 11 INTRODUCTION 12 PRODUCT DESCRIPTION 13 TECHNICAL CHARACTERISTICS 1 4 FACTORY SETTINGS 1 5 UNITS AND ACCESSORIES SUPPLIED 1 6 INSTALLATION APPROVAL BASIS 17 FIGURE FAA FORM 337 18 ENVIRONMENTAL QUALIFICATIONS 19 FIGURE ENVIROMENTAL TEST TABLE 1 10 AIRCRAFT CERTIFICATION 2 INSTALLATION 21 GENERAL 2 3 UNPACKING AND INSPECTION 23 INITIAL BENCH CHECK 2 4 COOLING 2 5 MECHANICAL INSTALLATION 2 5 1 Mechanical installation Pulselite Control Unit REVISION C 02 15 2001 PAGE L FAA
8. ISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 24015 3 TESTING 3 1 INSTALLATION TESTING The following test procedure will evaluate the installation in the aircraft 1 Check wiring amp connections before applying power 2 Switch the Pulselite Unit to ON and verify that the appropriate Landing Taxi Recognition Lights are flashing on the aircraft 3 Switch the appropriate Landing Taxi Recognition Lights ON utilizing the existing switches and verify that the lights remain on without flashing 4 Switch the Pulselite Control Unit off and the existing Landing Taxi Recognition Light switches are off and verify that the Landing Taxi Recognition Lights are OFF REVISION C 02 15 2001 PAGE 3 1 L FAA Inventory PULSELIT 2401S 805 1C doc PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 24015 3 2 EMI RFI TESTING The following is an outline for determining that no detrimental Electro Magnetic Interference EMI or Radio Frequency Interference RFI is caused by the installation of a Precise Flight Pulselite product per FAR 23 1431 25 1431 27 1431 or 29 1431 These procedures are not necessarily all encompassing in that they may not include all of the equipment installed in the airplane If electronic and navigation equipment is installed which is not included in this document consult the equipment manufacturer an FAA approved
9. Inventory PULSELIT 2401S 805 1C doc 1 1 1 1 1 1 1 2 1 2 1 3 1 3 1 4 1 5 1 5 1 6 2 1 2 1 2 1 2 1 2 2 2 2 2 2 PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 24015 292 Mechanical installation Switches 2 3 2 6 FIGURE PHYSICAL DIMENSIONS 2 4 27 ELECTRICAL INSTALLATION 2 5 2 1 1 Electrical Installation 2 5 2 8 FIGURE BLOCK DIAGRAM 2 6 2 8 1 Determine the amperage on individual channels 2 7 2 9 FIGURE WIRE TABLE 2 7 2 10 FIGURE PINOUT TABLE 2 8 2 11 FIGURE CONNECTOR CONFIGURATION 2 9 3 TESTING 3 1 3 1 INSTALLATION TESTING 3 1 3 2 EMI RFI TESTING 3 2 3 2 1 Procedures 3 3 3 2 2 Communications 3 3 3 2 3 Ground Navigation Systems 3 4 3 2 4 Weather Radar 3 6 3 2 5 Autopilot and Flight Director 3 6 3 2 6 Conclusion 3 7 4 OPERATION 4 1 41 NORMAL OPERATION 4 1 5 DOCUMENTATION 5 1 5 1 DOCUMENTATION 5 1 5 2 RETURN AUTHORIZATION 5 1 5 3 WARRANTY SERVICE 5 1 6 APPENDIX A 6 1 6 1 1 PARTS LIST 6 1 REVISION C 02 15 2001 PAGE iii L FAA Inventory PULSELIT 2401S 805 1C doc E PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 24015 LIST OF ACTIVE PAGES REVISION C 02 15 2001 PAGE iv L FAA Inventory PULSELIT 2401S 805 1C doc PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 24015 REVISIONS REV NO PAGE DESCRIPTION A
10. The Sample Description of Work Accomplished Figure 1 7 is suggested language provided as a convenience to the installing agency The information and wording should be modified to correctly describe the particular installation Precise Flight Inc can assume no responsibility for the alteration of the airframe or electrical system REVISION C 02 15 2001 PAGE 1 3 L FAA Inventory PULSELIT 2401S 805 1C doc E PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 24015 8 Description of Work Accomplished If more space is required attach additional sheets Identify with aircraft nationality and registration mark and date work completed A The following components were installed PULSELITE UNIT MODEL 2401S S N SWITCH Switch P N B The Unit was installed in position in the aircraft according to instructions in the PRECISE FLIGHT INSTALLATION MANUAL MODEL 24018 P N dated insert current revision date of manual and guidance in FAA Advisory Circulars 43 13 1A chapter 11 and 43 13 2A Chapter 1 amp 2 C An electrical load analysis was performed and the revised continuous load of the alternator generator or other supply does not exceed 80 of capacity D complete operational test was performed according to PULSELITE 24015 Installation Manual P N 8034 date _ The equipment performed satisfactorily and did not adversely affect existing components or systems in the air
11. UNCTION BOX REF ma CH C1 OUT C AIRCRAFT EXTERNAL NOTE DO NOT TIE INPUTS TOGETHER LIGHT 600 WATT MAX 28 VOLT DC PULSELITE SWITCH 28V 06 LT CONTROL CH C2 OUT D BUS 15 F UNIT POWER AIRCRAFT EXTERNAL UNIT GND LIGHT 600 WATT MAX DC JUNCTION BOX REF al LJ 28 VOLT DC NOTE JUNCTION BOX ATTACHMENTS SHOWN HERE FOR ILLUSTRATION ONLY MAINTAIN AIRCRAFT BUS SEPARATION ON AIRCRAFT PULSELITE INSTALLATION 2 8 FIGURE BLOCK DIAGRAM REVISION C 02 15 2001 PAGE 2 6 L FAA Inventory PULSELIT 2401S 805 1C doc sm PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 2401S 2 8 1 Determine the amperage on individual channels Proper wire and circuit protection should be observed SEE Fig 2 9 CU WIRE AN CIRCUIT GAUGE BREAKER 2 9 FIGURE WIRE TABLE Approved wire specification is MIL W 22759 16 or equivalent Fuse specification is MIL F 15160 or equivalent Circuit breaker specification is MIL C 5809 or equivalent To protect the Pulselite control unit and insure proper installation it is important to check that ground terminal connector 1 pin E of the control unit is properly grounded to the aircraft frame with a No 20 gauge wire or equivalent ground strap Chassis of unit should be mounted to airframe and interfaces burnished to ensure a good ground Power input for the Pulselite Control Unit is through Connector 1 Pin F A single 1 to 5 Amp circu
12. aircraft lamps Up to 600 watts per Lamp Pulsing the landing lights enhances the aircraft flight path recognition quality and may be utilized any time the pilot desires By flashing the landing taxi and recognition lights approx 46 times per minute in a variety of patterns the Pulselite Control Unit creates an illusion of exaggerated motion that other pilots can immediately recognize and avoid Precise Flight recommends that the landing lights be turned on steady full time when the aircraft is within 200 AGL at night Due to possible disorientation the Pulselite should not be operated in clouds at night or on the ground The landing lights may be turned on steady rate by simply switching the original landing taxi recognition lights on REVISION C 02 15 2001 PAGE 1 1 L FAA Inventory PULSELIT 2401S 805 1C doc PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 2401S 1 3 TECHNICAL CHARACTERISTICS Weight Cooling Dimensions Operating Voltages Operating Current Maximum Load per Switching Circuit Number of circuits Usage limitations Ambient operating range 1 4 FACTORY SETTINGS Pulse rate Sequence normal Lamp brightness REVISION C L FAA Inventory PULSELIT 2401S 805 1C doc 1 95 pounds 0 88 kilograms Radiation and Convection 5 45 in W 7 63 in D 2 18 in H 13 84 cm W 19 38 cm D 5 54 cm H 28 VDC Control Voltage 11 29 VDC
13. craft as required by FAR 23 1301 FAR 23 1431 or FAR 25 1301 FAR 25 1431 FAR 27 1301 FAR 27 1431 FAR 29 1301 or FAR 29 1431 as applicable E The aircraft equipment list was revised to reflect these changes weight and balance data was revised and placed in the aircraft records A Precise Flight Inc PULSELITE Aircraft Flight Manual Supplement dated was placed in the aircraft 1 7 FIGURE FAA FORM 337 REVISION C 02 15 2001 PAGE 1 4 L FAA Inventory PULSELIT 2401S 805 1C doc sm PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 24015 1 8 ENVIRONMENTAL QUALIFICATIONS NOMENCLATURE PULSELITE MODEL NUMBER 24015 MANUFACTURER SPECIFICATION PULSELITE PERFORMANCE REQUIREMENTS MANUFACTURER PRECISE FLIGHT INC 63120 POWELL BUTTE RD BEND OR 97701 CONDITIONS DO160D DESCRIPTION OF TESTS CONDUCTED SECTION p w M HMMDTY 60 NOTREQUIRED CRASH SAFETY VIBRATION 80 7 CATEGORYC EXPLOSION 902 7 NOREURD FLUIDS SUSCEPTIBILITY NOT REQUIRED SAND AND DUST NOT REQUIRED AUDIO FREQUENCY 18 0 CATEGORY Z CONDUCTED SUSCEPTIBILITY 19 0 FUNGUS NOT REQUIRED E e SUSCEPTIBILITY SUSCEPTIBILITY RADIO FREQUENCY EMISSION CATEGORY B a 1 1 9 FIGURE ENVIROMENTAL TEST TABLE REVISION C 02 15 2001 PAGE 1 5 L FAA Inventory PULSELIT 2401S 805 1C doc E PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800
14. d for operation before shipment The installing agency can insure Pulselite operation before final installation by utilizing Paragraph 3 1 for this procedure REVISION C 02 15 2001 PAGE 2 1 L FAA Inventory PULSELIT 2401S 805 1C doc PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 24015 2 4 COOLING Elevated operating temperatures reduce reliability Forced air cooling is not required however allow approx 1 of space around the control unit for adequate convective cooling Space is most critical on the unit sides so that the heat sink fins may dissipate heat at the proper rate 2 5 MECHANICAL INSTALLATION Listed below are considerations to be examined before installing the Pulselite Model 2401S Close attention to these suggestions will assure optimum performance when completed 2 5 1 Mechanical installation Pulselite Control Unit REVISION C A Select a location for the Pulselite Control Unit which is suitably ventilated for avionics CAUTION The standard Pulselite Model 2401S is not approved for use in a potentially explosive environment refer to AC 43 13 2A Chapter 2 Radio Installation Locate Pulselite away from fire hazard zones highly explosive or corrosive areas potentially hazardous fluid areas e g water fuel hydraulic fluid or oxygen units etc The Pulselite Control Unit must be installed in a structurally substantiated locat
15. he landing taxi and recognition lights approx 46 times per minute in a variety of patterns Pulselite creates an illusion of exaggerated motion that other pilots can immediately recognize and avoid While the Pulselite has been tested throughout the entire landing phase of flight Precise Flight recommends that the landing lights be turned on steady full time when the aircraft is within 200 AGL at night The Pulselite system should not be operated in clouds at night or in the close proximity of other aircraft on the ground due to possible disorientation The landing lights may be turned on steady at any time by simply switching the original landing taxi recognition lights on The Pulselite will remain active until the Pulselite switch is turned OFF REVISION C 02 15 2001 PAGE 4 1 L FAA Inventory PULSELIT 2401S 805 1C doc sm PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 24015 5 DOCUMENTATION 5 1 DOCUMENTATION To ensure technical updates and notifications fill out and return the warranty document and a copy of the 337 if appropriate 5 2 RETURN AUTHORIZATION In order to expedite repair of units call the factory for a return authorization number before returning equipment for service 5 3 WARRANTY SERVICE Precise Flight warrants products in accordance with the warranty statement in effect at the time of equipment registration All repairs are performed at the
16. ion A typical wiring diagram and physical installation is provided in Appendix A Allow adequate space for installation of cables and connectors The Pulselite Control Unit should be installed in an avionics bay or other suitable location Although the Pulselite Control Unit can be installed in any axis the preferred orientation is with the fins vertical Use 4 10 32 pan head screws Burnish one fastener location to insure proper ground 02 15 2001 PAGE 2 2 L FAA Inventory PULSELIT 2401S 805 1C doc PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 2401S 2 5 2 Mechanical installation Switches A The switch s should be located near the existing Aircraft Landing Light switches REVISION C 02 15 2001 PAGE 2 3 L FAA Inventory PULSELIT 2401S 805 1C doc PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 24015 3 Feret HEDE PAOS A GIG S i 1 e j 5 450 4 950 a 2 188 7 0 196 i NG 5 875 5 375 0 195 Jp 4 950 2 6 FIGURE PHYSICAL DIMENSIONS REVISION C 02 15 2001 PAGE 2 4 L FAA Inventory PULSELIT 2401S 805 1C doc sm PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 24015 2 7 ELECTRICAL INSTALLATION All wiring should be secured to prevent chafing and
17. it breaker is required between the aircraft bus and this pin This pin provides internal control voltage for the Pulselite Control Unit The Pulselite circuit breaker s should be located in the existing aircraft circuit breaker panel However if this is not possible they may be located within the Pulselite switch panel REVISION C 02 15 2001 PAGE 2 7 L FAA Inventory PULSELIT 2401S 805 1C doc PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 24015 PULSELITE CONNECTOR PINOUT TABLE CONNECTOR 1 SHELL SIZE 20 CONNECTOR 2 SHELL SIZE 18 MS3102 20 17 P MS3102 18 10 P PIN VOLTAGE FUNCTION CHNL PIN VOLTAGE FUNCTION CHNL _ EAS EA AAA AAA AAA AAA Ci ei Baa D 28VDC DCOUTPUT 1 240 DCINPUT o2 OR T C j j cd E DCGND jJUNTGROUND CONTROL POWER MATING CONNECTOR MATING CONNECTOR MS 3106A 20 97 20 17 S MS 3106B 18 97 18 10 S 2 10 FIGURE PINOUT TABLE REVISION C 02 15 2001 PAGE 2 8 L FAA Inventory PULSELIT 2401S 805 1C doc PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 24015 2 11 FIGURE CONNECTOR CONFIGURATION ON Ww CONNECTOR 1 CONNECTOR 2 REVISION C 02 15 2001 PAGE 2 9 L FAA Inventory PULSELIT 2401S 805 1C doc sm PREC
18. repair station rated in the equipment involved or an FAA Avionics Inspector for applicable test procedures The evaluation will be with a series of equipment checks on the ground to determine that no detrimental EMI RFI effects are introduced into the aircraft by the Pulselite system The electrical systems installed in the aircraft will be referred to as the Pulselite system in this procedure The following tests should be performed by personnel familiar with aircraft systems and proper operation as well as the Pulselite equipment and its proper operation Any and all discrepancies shall be noted Any discrepancies noted during these procedures must be reported to Precise Flight Inc and evaluated for cause extent and as to what corrective action should be taken to correct the problem The aircraft may not be flown after discrepancies are found unless the Pulselite system is disconnected at the aircraft bus until such time as the problems have been corrected and the aircraft has successfully passed the ground portion of this test Only then may the aircraft be flown to complete this test REVISION C 02 15 2001 PAGE 3 2 L FAA Inventory PULSELIT 2401S 805 1C doc PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 24015 A record of this test shall be recorded in the aircraft logbook The entry should include date aircraft time and results including any discrepancies note
19. rn Pulselite equipment ON and compare compass heading THIS TEST MUST BE REPEATED WITH THE AIRCRAFT HEADED IN FOUR DIRECTIONS APPROXIMATELY 90 DEGREES APART Compass Readings PulseliteON PulseliteOFF 2 Remarks 3 2 4 Weather Radar CAUTION USE CAUTION WHEN OPERATING RADAR FOLLOW RADAR MANUFACTURERS RECOMMENDATIONS FOR SAFETY A Select WxRadar ON After proper warm up time select TEST mode and confirm proper operation Select MAP mode and note display Turn on Pulselite equipment and note any changes Remarks 3 2 5 Autopilot and Flight Director Turn on autopilot and perform ground check per the autopilot manufacturers instructions in the flight manual Turn on the Pulselite equipment and again perform check Note any discrepancies Remarks REVISION C 02 15 2001 PAGE 3 6 L FAA Inventory PULSELIT 2401S 805 1C doc PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 24015 3 2 6 Conclusion EMI Test Data Record Witness Date Location Comments REVISION C 02 15 2001 PAGE 3 7 L FAA Inventory PULSELIT 2401S 805 1C doc sm PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 2401S 4 OPERATION 4 1 NORMAL OPERATION Pulsing the landing lights tend to enhance the aircraft flight path recognition quality and may be utilized any time the pilot desires By flashing t
20. s 4 Tune VOR Nav 1 to a local VORTAC station with Pulselite equipment off Note distance on DME and listen for noise Turn Pulselite equipment on and compare distance readings and background noise Repeat for all other VHF NAV radios Remarks B LoranC 1 Observe Loran self test responses and signal to noise ratios Turn Pulselite equipment on and recycle Loran and compare results Remarks REVISION C 02 15 2001 PAGE 3 4 L FAA Inventory PULSELIT 2401S 805 1C doc PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 24015 C RNAV 1 VOR MODE Set to VHF on a local frequency center CDI and pilots HSI turn on Pulselite equipment and check for interference Remarks 2 DME MODE With Pulselite equipment off set to local VHF frequency and note DME reading Turn on Pulselite equipment and compare DME reading Verify reading with known distance Remarks RNAV MODE With Pulselite equipment off set local VHF frequency set 3 waypoint bearing to 180 and waypoint distance to 25 miles Center CDI and note RNAV readings Turn Pulselite equipment on and note any changes in RNAV readings Remarks REVISION C 02 15 2001 PAGE 3 5 L FAA Inventory PULSELIT 2401S 805 1C doc sm PRECISE FLIGHT INC 63120 POWELL BUTTE ROAD BEND OR 97701 800 547 2558 PULSELITE MODEL 24015 C Magnetic Compass With Pulselite equipment OFF note compass heading Tu
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