JA74-001 Dual USB Charging Port
Installation and Operating Manual
Rev A
Page B3
2. Description of the System/Alteration
Jupiter Avionics JA74-001 Dual USB Charging Port with interface to [include equipment/systems as appropriate].
Refer to Appendix A of this manual for interconnect information. Refer to aircraft manufacturer approved
interconnect for actual installation.
3. Control, Operation Information
Refer to section 3 of this manual.
4. Servicing Information
N/A
5. Maintenance Instructions
Maintenance of the JA74-001 is ‘on condition’ only. Periodic maintenance is not required. Refer to the
JA74-001 Maintenance Manual.
6. Troubleshooting Information
Refer to the JA74-001 Maintenance Manual.
7. Removal and Replacement Information
Refer to Section 2 of this manual - the JA74-001 Installation and Operating Manual. If the unit is removed and
reinstalled, a functional check of the equipment should be conducted.
8. Diagrams
Refer to Appendix A of this manual - the JA74-001 Installation and Operating Manual - for installation drawings
and interconnect examples.
9. Special Inspection Requirements
N/A
10. Application of Protective Treatments
N/A
11. Data: Relative to Structural Fasteners
JA74-001 and appropriate mounting hardware installation, removal and replacement should be in accordance
with applicable provisions of AC 43.13-1B and AC 43.13-2A.
12. Special Tools
N/A
13. This Section is for Commuter Category Aircraft Only
A.
Electrical loads
: Refer to Section 1 of the JA74-001 Installation and Operating Manual.
B.
Methods of balancing flight controls
: N/A.
C.
Identification of primary and secondary structures
: N/A.
D.
Special repair methods applicable to the airplane
: N/A.
14. Overhaul Period
No additional overhaul time limitations.
15. Airworthiness Limitation Section
N/A
