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BS M 84:1995

Withdrawn

Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

View Superseded by

Air cargo equipment. Certified aircraft container for air cargo. Specification and testing

Available format(s)

Hardcopy , PDF

Withdrawn date

30-10-2018

Superseded by

BS ISO 10327:2014

Language(s)

English

Published date

15-09-1995

€165.94
Excluding VAT

Committees responsible
National foreword
Introduction
Specification
1. Scope
2. Normative references
3. Base
4. Superstructure
5. Design loads
6. Destination placard holder
7. Tare weight objectives
8. Materials and processes
9. Markings
10. Test No.1: Horizontal load test, operational loads
11. Test No.2: Upward load test, operational loads
12. Test No.3: Base strength
13. Test No.4: Cyclic test and bridging and cresting
14. Test No.5: Resistance to racking
15. Test No.6: Hanging load test
16. Test No.7: Local indentation
17. Test No.8: Water tightness test
Figure
1. Deflection limits out of the maximum ULD contour
2. Cycling test device
3. Local indentation loading

Specifies the basic requirements for the specification and testing of containers. Gives minimum requirements for a certified aircraft container not exclusively designed for lower deck and wide body aircraft.

Committee
ACE/57
DevelopmentNote
Supersedes 92/86149 DC (08/2005)
DocumentType
Standard
Pages
16
PublisherName
British Standards Institution
Status
Withdrawn
SupersededBy
Supersedes

BS M 88:1996 Air cargo equipment. Pressure equalization requirements for cargo containers

ISO 11242:1996 Aircraft — Pressure equalization requirements for cargo containers
BS M 71:1994 Air cargo equipment. Interline pallets
BS M 72:1994 Air cargo equipment. Minimum airworthiness requirements and test conditions for certified air cargo unit load devices
ISO 4116:1986 Air cargo equipment — Ground equipment requirements for compatibility with aircraft unit load devices
BS 2C 8:1988 Specification for rail and stud configuration for aircraft passenger equipment and cargo restraint

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