Sch 25ATSO-C1002 — Refrigerated cargo unit load container

Schedule 25 ATSO-C1002 — Refrigerated cargo unit load container

(subsection 13.2 (1), table, item 5)

This Schedule applies to a refrigerated cargo unit load container that:

(a) is for carriage as main 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.

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.

(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: