Document ID: chunk:federal_register_of_legislation:F2017C01160:reg:7:p13
Version: federal_register_of_legislation:F2017C01160
Segment Type: reg
Provision Reference: reg 7 (pt 13/24)
Character Range: 47046–50267

cabin (upper deck) cargo in transport category aeroplanes; and
(b) will be connected to the aeroplane's electrical system; and
(c)  is manufactured by an article manufacturer.

2 Definitions
       In this Schedule:
NAS 3610 means the document called the National Aerospace Standard (NAS) 3610, Cargo Unit Load Devices – Specification for, published by the Aerospace Industries Association of America, Inc., as existing from time to time.
RTCA/DO-160D means the RTCA Document RTCA/DO-160D, Environmental Conditions and Test Procedures for Airborne Equipment, as existing from time to time, or a later version of RTCA Document RTCA/DO-160, as existing from time to time.
RTCA/DO-178B means the RTCA Document RTCA/DO-178B, Software Considerations in Airborne Systems and Equipment Certification, as existing from time to time.
RTCA/DO-178C means the RTCA Document RTCA/DO-178C, Software Considerations in Airborne Systems and Equipment Certification, as existing from time to time.
RTCA/DO-254 means RTCA Document RTCA/DO-254, Design Assurance Guidance for Airborne Electronic Hardware, as existing from time to time.
Technical Instructions has the meaning as defined in regulation 92.010 of CASR.
ULD Technical Manual 13th means the ULD Technical Manual 13th, published by the International Air Transport Association, as existing from time to time.

3 Minimum performance standard — general
       (1)The refrigerated cargo unit load container must meet the requirements mentioned in the following:
(a) NAS 3610;
(b) AS/NZS 1677.2:1998, Refrigerating systems, Part 2: Safety requirements for fixed applications (Category 2 Occupancy Classification), as existing from time to time;
(c) SAE ARP 1308, Preferred Electrical Connectors for Aerospace Vehicles and Associated Equipment, as existing from time to time;
(d) SAE ARP 1199, Selection, Application, and Inspection of Electric Overcurrent Protective Devices, as existing from time to time;
(e) SAE ARP 1870, Aerospace Systems Electrical Bonding and Grounding For Electromagnetic Compatibility and Safety, as existing from time to time.
       (2)The container must meet the requirements mentioned in the following sections of the ULD Technical Manual 13th:
(a) Standard Specification 50/4 – Certified Aircraft Container;
(b) Standard Specification 80/1 – Requirements for Thermal Containers:
 (i) 4.7 Spillage; and
 (ii) 4.8 Pressurization; and
 (iii) 8 Markings;
(c) Standard Specification 80/2 – Pressure Equalization Requirements for Aircraft and Shipping Containers.

4 Minimum performance standard — environmental test
       The refrigerated cargo unit load container must meet be tested in accordance with the test conditions mentioned in RTCA/DO-160D.

5 Minimum performance standard — software
       If the refrigerated cargo unit load container includes a digital computer, the software for the computer must be developed in accordance with RTCA/DO‑178B, RTCA/DO-178C or RTCA/DO-254.

6 Minimum performance standard — refrigeration unit
       (1)The refrigerant for the refrigerated cargo unit load container must:
(a) meet the requirements for refrigerants mentioned in clause 5.9 of Standard Specification 80/1 – Requirements for Thermal Containers of the