Appareo Stratus Power Скачать руководство пользователя страница 9

600840-000041 Stratus Power Installation Instructions

Rev. 1.0

Last Revised: December 15, 2016

Page 9 of 12

Pin 2:

GROUND

Pin 1:

POWER

Figure 3: Harness

2. Verify input power and polarity.

a. Connect aircraft power and ensure that the breaker is pushed in.

b. On the power harness, place the negative probe of a multimeter on Pin 2 and the 

positive probe on Pin 1.

c. Measure the voltage across the two wires using a multimeter. The voltage 

reading should be equal to your aircraft power.

d. Disconnect aircraft power.

3. Connect the power receptacle into the header on the back of Stratus Power.

Figure 4: Back of Stratus Power

Содержание Stratus Power

Страница 1: ...ot be disseminated or redistributed without the written permission of Appareo Systems LLC APPAREO SYSTEMS LLC FARGO NORTH DAKOTA 58102 Stratus Power Installation Instructions Document Number 600840 000041 Document Type Certification Last Revised 15 December 2016 Rev 1 0 Sheet 1 of 12 Stratus Power Installation Instructions ...

Страница 2: ...in this guide Unauthorized replication of this guide is prohibited Appareo Appareo Systems Stratus Power and the Appareo and Stratus Power logos are either registered trademarks or trademarks of Appareo Systems LLC All other trademarks and registered trademarks are the sole property of their respective owners Appareo Systems LLC 1830 NDSU Research Circle North Fargo ND 58102 USA Visit us on the we...

Страница 3: ...uirements 6 1 9 Limitations for installation 6 1 10 Circuit protective device marking 6 2 Mounting Stratus Power 7 3 Wiring Stratus Power 8 4 Troubleshooting 10 Technical Assistance 10 Appendix A 11 List of Figures Figure 1 Mounting location 7 Figure 2 Installing Stratus Power 8 Figure 3 Harness 9 Figure 4 Back of Stratus Power 9 List of Tables Table 1 TSO compliance 5 Table 2 TSO deviations 5 Tab...

Страница 4: ...cumentation Document Number Title Appareo 600845 000028 Stratus Power Maintenance Manual FAA AC 43 13 1B Acceptable Methods Techniques and Practices Aircraft Inspection and Repair FAA AC 43 13 2B Acceptable Methods Techniques and Practices Aircraft Alterations FAA TSO C71 Airborne Static DC to DC Electrical Power Converter For Air Carrier Aircraft RTCA DO 160G Environmental Conditions and Test Pro...

Страница 5: ...alification testing was performed to DO 160G not DO 60 Table 2 TSO deviations 1 4 Environmental qualifications Stratus Power is tested to DO 160G The Stratus Power Environmental Qualification form is found in Appendix A of this document 1 5 Equipment specifications Characteristic Specification Width 1 848 inches 46 95 mm Height 1 848 inches 46 95 mm Depth 1 391 inches 35 32 mm Stratus Power Unit W...

Страница 6: ...153510 000040 1 Stratus Power Panel Cover 353070 000074 1 Screw 356060 000100 2 Power Connector Receptacle 251015 000115 1 Connector Terminals 251015 000116 2 Table 5 Supplied hardware 1 8 Unpacking inspection requirements When unpacking Stratus Power visually inspect for any damage to the unit or missing components If damage or missing parts are present contact Appareo 1 9 Limitations for install...

Страница 7: ...earance in the front and back of the unit based on the dimensions given in Table 3 ATTENTION Process may result in metal shavings Ensure that they do not fall behind the aircraft panel 3 Drill out a circle in the mounting location with a 1 inch drill bit using the measurements in Figure 1 Then cut the notch in the top of the hole Figure 1 Mounting location 4 Place the Stratus Power unit behind the...

Страница 8: ...gauge wiring and install it in accordance with FAA AC 43 13 1B and AC 43 13 2B Wire length and routing will vary by installation The installer must also supply a circuit protective device for use with Stratus Power Use a 2A breaker for 28V aircraft and a 4A breaker for 14V aircraft 1 Wire Stratus Power according to the diagrams below Provide a service loop Pin Pin Name Description 1 Power 10 32 VD...

Страница 9: ...er and ensure that the breaker is pushed in b On the power harness place the negative probe of a multimeter on Pin 2 and the positive probe on Pin 1 c Measure the voltage across the two wires using a multimeter The voltage reading should be equal to your aircraft power d Disconnect aircraft power 3 Connect the power receptacle into the header on the back of Stratus Power Figure 4 Back of Stratus P...

Страница 10: ... Power before connecting any devices 4 Troubleshooting Problem Troubleshooting Steps Stratus Power is not powering a device x Verify that the circuit protective device is functioning correctly x Verify that the polarity on the power connector is correct Technical Assistance For support please contact Appareo at support appareo com By mail 1830 NDSU Research Circle North Fargo ND 58102 United State...

Страница 11: ... 3 Equipment tested to Category F1 Operating High Temperature 4 5 4 Equipment tested to Category F1 In Flight Loss of Cooling 4 5 5 Equipment identified as Category X no test performed Altitude 4 6 1 Equipment tested to Category F1 Decompression 4 6 2 Equipment identified as Category X no test performed Overpressure 4 6 3 Equipment identified as Category X no test performed Temperature Variation 5...

Страница 12: ...ed to Category BXX Voltage average value dc 16 6 1 1 Equipment tested to Category BXX Abnormal Operating Conditions dc 16 6 2 Equipment tested to Category BXX Voltage Spike 17 0 Equipment tested to Category B Audio Frequency Conducted Susceptibility 18 0 Equipment tested to Category B Induced Signal Susceptibility 19 0 Equipment identified as Category X no test performed Radio Frequency Susceptibi...

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