§25.1519 Weight, center of gravity, and weight distribution.

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 airplane weight, center of gravity, and weight distribution limitations determined under Secs. 25.23 through 25.27 must be established as operating limitations.

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

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