Menu
0
Total price
0 €
PRICES include / exclude VAT
Homepage>BS 2C 8:1988 Specification for rail and stud configuration for aircraft passenger equipment and cargo restraint
Sponsored link
sklademVydáno: 1988-02-29
BS 2C 8:1988 Specification for rail and stud configuration for aircraft passenger equipment and cargo restraint

BS 2C 8:1988

Specification for rail and stud configuration for aircraft passenger equipment and cargo restraint

Format
Availability
Price and currency
Anglicky Secure PDF
Immediate download
154.05 €
You can read the standard for 1 hour. More information in the category: E-reading
Reading the standard
for 1 hour
15.41 €
You can read the standard for 24 hours. More information in the category: E-reading
Reading the standard
for 24 hours
46.22 €
Anglicky Hardcopy
In stock
154.05 €
Označení normy:BS 2C 8:1988
Počet stran:10
Vydáno:1988-02-29
ISBN:0 580 16518 3
Status:Standard
DESCRIPTION

BS 2C 8:1988


This standard BS 2C 8:1988 Specification for rail and stud configuration for aircraft passenger equipment and cargo restraint is classified in these ICS categories:
  • 49.045 Structure and structure elements

1.1 This International Standard specifies the geometry and the partial dimensions of rails and studs used for securing passenger equipment and for cargo restraint, necessary to ensure interchangeability of these items.

1.2 Individual strength requirements will determine the complete rail shape, such as incorporating the standard section integrally into an I-beam extrusion.

1.3 The overall shape of the studs above the top of the rail will depend upon the application. The upper portion may be cylindrical to fit into the tubular structure of a seat or galley unit. Alternatively, it may have a ring attached to serve as a tiedown point for a rope or strap.

1.4 The rail imparts loads in the upward, downward, sideward, forward and aft directions. Forward and aft loads are applied to the track by means of a “shear plug”, a part of the pin assembly (or structure to which the stud is joined) which engages in the rail notches [20,8 mm (0.800 in) in diameter], but this is not included in this International Standard.

In the case of seat attachment or similar application, the downward load is applied to the upper face of the rail by a fitting which is also part of the seat, but this is not included in this International Standard.


Geometry of aircraft floor rails.