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CS-VLA 903  Engine

ED Decision 2003/18/RM

(a)                            The engine must meet the specifications of CS-22 Subpart H.

(b)                            Restart capability. An altitude and airspeed envelope must be established for the aeroplane for in-flight engine restarting and the installed engine must have a restart capability within that envelope.
Details
Source-Title: CS-VLA 903 Engine View latest amendments
Erulesid: ERULES-1963177438-7823 Compare versions
Domain: Initial airworthiness
Amendedby: Initial issue
Applicabilitydate: 14 November, 2003
Entryintoforcedate: 14 November, 2003
Regulatorysource: ED Decision 2003/18/RM Navigate
Regulatorysubject: CS-VLA
Typeofcontent: CS (Certification specification)
Origin: EASA
Category: EAR