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BS M 89:1996

Current

Current

The latest, up-to-date edition.

Aircraft ground support equipment. Stability requirements for loading and servicing equipment

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

09-15-1996

Committees responsible
National foreword
Introduction
Specification
1 Scope
2 Normative reference
3 Definitions
4 Objectives
5 Systems classification
6 Calculation formula
7 Test methods
Figures
1 Representation of some parameters
2 Variation of 'shape factor' with aspect ratio for
    rectangular plates
3 Determination of the distance from the centre of
    gravity to the pivot point

Gives criteria for determining stability of aircraft loading and servicing equipment including wind loads, together with systems and formula relating to stability. It also gives methods of testing.

1.1 This International Standard specifies:

  1. the criteria to be used to determine stability of aircraft loading and servicing equipment, including wind loads;
  2. the classification of systems recommended to achieve stability;
  3. the formula to be used for calculating steady-state wind stability;
  4. the recommended test methods applicable to equipment.

1.2 The intent of this International Standard is not to specify equipment design, but rather to define uniform criteria, calculation and testing methods in order to provide a safe work environment under all predictable circumstances for the users of aircraft loading and servicing equipment.

1.3 This International Standard specifies the worldwide requirements recognized by aircraft and equipment manufacturers as well as airlines and handling agencies.

In addition, it shall be applied with due reference to national governmental regulations of the country where the equipment is to be operated.

1.4 This International Standard applies to aircraft loading and servicing equipment, typically but not exclusively defined as follows:

  • container and pallet loaders (see ISO 6967 and ISO 6968);
  • catering trucks (see ISO 10841);
  • passenger stairs (see ISO 12056);
  • maintenance and fueling access platforms, when operated in a static position on an aircraft.

1.5 This International Standard does not apply to:

  • forklifts;
  • aircraft de-icers;
  • any equipment with rotating booms,

and more generally any equipment the normal mode of operation of which includes moving in the elevated position.

Committee
ACE/57
DevelopmentNote
Also numbered as ISO 11995. Supersedes 94/700683 DC. (02/2002)
DocumentType
Standard
Pages
14
PublisherName
British Standards Institution
Status
Current
Supersedes

BS M 90:1997 Aircraft ground support equipment. Self-propelled passenger stairs for large capacity aircraft. Functional requirements
ICC 2015 INT. SOLAR ENERGY PRO. & COMM. : 2015 2015 (ISEP[TM]) INTERNATIONAL SOLAR ENERGY PROVISIONS[TM] COMMENTARY
BS M 87:1996 Aircraft ground support equipment. Catering vehicle for large capacity aircraft. Functional requirements

SIA A92.7 : 2014 AIRLINE GROUND SUPPORT VEHICLE-MOUNTED VERTICAL LIFT DEVICES
BS M 74:1994 Air cargo equipment. Basic requirements for aircraft loading equipment
ISO 10841:1996 Aircraft — Catering vehicle for large capacity aircraft — Functional requirements
ISO 6967:2006 Aircraft ground equipment — Main deck loader — Functional requirements
SAE ARP 1328 : 2012 AIRCRAFT GROUND SUPPORT EQUIPMENT - WIND STABILITY DETERMINATION
ISO 6968:2005 Aircraft ground equipment — Lower deck loader — Functional requirements
ISO 12056:1996 Aircraft — Self-propelled passenger stairs for large capacity aircraft — Functional requirements

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