• Shopping Cart
    There are no items in your cart

IP 468 : 2001

Withdrawn

Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

DETERMINATION OF THE FREEZING POINT OF AVIATION TURBINE FUELS - AUTOMATIC OPTICAL METHOD

Withdrawn date

23-07-2013

Published date

12-01-2013

Sorry this product is not available in your region.

Defines an automatic procedure for the determination of the freezing point of aviation turbine fuels over the temperature range of -40 degree C to -70 degree C. The results obtained are equivalent to those obtained using the manual test method IP 16, but a small bias of less than 0,5 degree C has been observed.

DocumentType
Standard
PublisherName
Energy Institute (formerly Institute of Petroleum - IP)
Status
Withdrawn

DEFSTAN 91-87/3(2002) : 2002 TURBINE FUEL, AVIATION KEROSENE TYPE, CONTAINING FUEL SYSTEM ICING INHIBITOR NATO CODE: F-34 JOINT SERVICE DESIGNATION: AVTUR/FSII

Access your standards online with a subscription

Features

  • Simple online access to standards, technical information and regulations.

  • Critical updates of standards and customisable alerts and notifications.

  • Multi-user online standards collection: secure, flexible and cost effective.