§25.995 Fuel valves.

14 CFR 25 · Powerplant · Fuel System Components · at 25-153 (current)

Text in force at 25-153: from 25-40, effective 2 May 1977.

In addition to the requirements of Sec. 25.1189 for shutoff means, each fuel valve must-- [(a) [Reserved.]] (b) Be supported so that no loads resulting from their operation or from accelerated flight conditions are transmitted to the lines attached to the valve.

42 FR 15043 · Source

Version history

Version	Effective	Published
25-40	2 May 1977	42 FR 15043
25-0	1 Feb 1965	29 FR 18291

Rulemaking for 25-40

other 75-10 27 Feb 1975
Notice of Airworthiness Review Program No. 2; Notice No. 75-10; Issued on 02/27/75. Notice of Airworthiness Review Program No. 3; Notice No. 75-19; Issued on 05/13/75.
final rule 14606, 14324 10 Mar 1977

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 25-40
Airbus Defence and Space S.A C-212-VA entry 3 at 25-0
GULFSTREAM AEROSPACE LP (GALP) GALAXY entry 2 at 25-40
GULFSTREAM AEROSPACE LP (GALP) GULFSTREAM 200 entry 2 at 25-40
GULFSTREAM AEROSPACE LP (GALP) Gulfstream G150 entry 2 at 25-40
Gulfstream Aerospace Corporation GVII-G500 entry 2 at 25-40
Gulfstream Aerospace Corporation GVII-G600 entry 2 at 25-40
Textron Aviation Inc. 4000 entry 1 at 25-40
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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