BS ISO 8267-2:2019 PDF

BS ISO 8267-2:2019 PDF

Name:
BS ISO 8267-2:2019 PDF

Published Date:
09/26/2019

Status:
Active

Description:

Aircraft. Tow bar attachment fittings interface requirements-Regional aircraft

Publisher:
British Standard / International Organization for Standardization

Document status:
Active

Format:
Electronic (PDF)

Delivery time:
10 minutes

Delivery time (for Russian version):
200 business days

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$48.006
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This document specifies the interface requirements for tow bar attachment fittings on the nose gear (when towing operations are performed from the nose gear) of conventional tricycle type landing gears of commercial civil transport aircraft.

Its purpose is to achieve tow bar attachment fittings interface standardization by aircraft mass category (which determines tow bar forces) in order to ensure that a single type of tow bar with a standard connection can be used for all aircraft types within or near that mass category, so as to assist operators and airport handling companies in reducing the number of different tow bar types used.

This document is applicable to all new models of regional aircraft within the specified maximum ramp mass range which enter service or are designed after its date of publication.

Cross References:
ISO 8267-1


All current amendments available at time of purchase are included with the purchase of this document.
File Size : 1 file , 1.1 MB
ISBN(s) : 9780580955440
Note : This product is unavailable in Russia, Ukraine, Belarus
Number of Pages : 14
Product Code(s) : 30347616, 30347616, 30347616
Published : 09/26/2019
Same As : BS ISO 8267-2:2019

History

BS ISO 8267-2:2023
Published Date: 12/20/2023
Aircraft. Tow bar attachment fittings interface requirements-Regional aircraft
$48.006
BS ISO 8267-2:2019
Published Date: 09/26/2019
Aircraft. Tow bar attachment fittings interface requirements-Regional aircraft
$48.006
BS C 21-1:1997
Published Date: 06/15/1997
Specification for interface requirements for aircraft noseleg to towbar attachment fittings.-Transport aircraft with a maximum ramp mass over 50000 kg (110000 lb)
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