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AMC1 SPO.POL.110(a)(3) Mass and balance system – commercial operations with aeroplanes and helicopters and non-commercial operations with complex motor-powered aircraft

ED Decision 2014/018/R

FUEL LOAD

The mass of the fuel load should be determined by using its actual relative density or a standard relative density.

Details
Source-Title: AMC1 SPO.POL.110(a)(3) Mass and balance system - commercial operations with aeroplanes and helicopters and non-commercial operations with complex motor-powered aircraft View latest amendments
Erulesid: ERULES-1963177438-14146 Compare versions
Domain: Air operations
Applicabilitydate: 1 July, 2014
Entryintoforcedate: 1 July, 2014
Regulatorysource: ED Decision 2014/018/R Navigate
Regulatorysubject: Part-SPO
Typeofcontent: AMC to IR (Acceptable means of compliance to implementing rule)
Parentir: SPO.POL.110 Mass and balance system - commercial operations with aeroplanes and helicopters and non-commercial operations with complex motor-powered aircraft
Origin: EASA
Category: EAR