§25.1503 Airspeed limitations: general

CS-25 · Subpart G — Operating Limitations And Information · at CS25-28 (current)

Text in force at CS25-28: from CS25-0, effective 17 Oct 2003.

When airspeed limitations are a function of weight, weight distribution, altitude, or Mach number, limitations corresponding to each critical combination of these factors must be established.

ED Decision 2003/002/RM · Source

Version history

Version	Effective	Published
CS25-0	17 Oct 2003	ED Decision 2003/002/RM

Rulemaking for CS25-0

easa decision ED Decision 2003/002/RM source

Aircraft using this section

No aircraft in the dataset reference this section.

Report an issue

Is something wrong with what you are looking at? Tell the maintainer; the report is filed against this page.