§25.1511 Flap extended speed.

14 CFR 25 · Operating Limitations and Information · Operating Limitations · at 25-153 (current)

Text in force at 25-153: from 25-0, effective 1 Feb 1965.

The established flap extended speed VFE must be established so that is does not exceed the design flap speed VF chosen under Secs. 25.335(e) and 25.345, for the corresponding flap positions and engine powers.

29 FR 18291 · Source

Version history

Version	Effective	Published
25-0	1 Feb 1965	29 FR 18291

Rulemaking for 25-0

nprm 64-28 14 May 1964
final rule 5066 3 Nov 1964

Aircraft using this section

Airbus Defence and Space S.A C-212-CB entry 3 at 25-0
Airbus Defence and Space S.A C-212-CC entry 3 at 25-0
Airbus Defence and Space S.A C-212-CD entry 3 at 25-0
Airbus Defence and Space S.A C-212-CE entry 3 at 25-0
Airbus Defence and Space S.A C-212-DD entry 3 at 25-0
Airbus Defence and Space S.A C-212-EE entry 3 at 25-0
Airbus Defence and Space S.A C-212-EE entry 4 at 25-0
Airbus Defence and Space S.A C-212-VA entry 3 at 25-0
GULFSTREAM AEROSPACE LP (GALP) GALAXY entry 2 at 25-0
GULFSTREAM AEROSPACE LP (GALP) GULFSTREAM 200 entry 2 at 25-0
GULFSTREAM AEROSPACE LP (GALP) Gulfstream G150 entry 2 at 25-0
Gulfstream Aerospace Corporation GVII-G500 entry 2 at 25-0
Gulfstream Aerospace Corporation GVII-G600 entry 2 at 25-0
Textron Aviation Inc. 4000 entry 1 at 25-0
The Boeing Company 767-200 entry 4 at 25-0
The Boeing Company 767-300 entry 4 at 25-0
su Beriev Be-200ES-E entry 3 at 25-0

Report an issue

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