Navigate / EASA
Ask question Discover more Add to collection
AMC1 SPO.POL.110(a)(4) Mass and balance system – commercial operations with aeroplanes and helicopters and non-commercial operations with complex motor-powered aircraft

ED Decision 2014/018/R

LOADING - STRUCTURAL LIMITS

The loading should take into account additional structural limits such as the floor strength limitations, the maximum load per running metre, the maximum mass per cargo compartment, and/or the maximum seating limits as well as in-flight changes in loading.
Details
Source-Title: AMC1 SPO.POL.110(a)(4) Mass and balance system - commercial operations with aeroplanes and helicopters and non-commercial operations with complex motor-powered aircraft View latest amendments
Erulesid: ERULES-1963177438-14154 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