MIL N 25161C (Amendment3) nozzle aerial pressure refueling type ma 2 (12 feb 1981)

ID:52961

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页数:12页

时间:2023-03-23

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上传者:战必胜
,.
AMENDMENT 3
12 February 1981
AMENDMENT 2
10 August 1971
MILITARY SPECIFICATION
NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2
This amendment forms a part
of MLlltary Specification MIL-KJ-25161C,
dated 10
Departments
Add:
July 1969, and is approked for use by all
and Agencies of the i)epar!ment of Defense.
PAGE 1
*nl.2
CAB
1s”
.
The
MA-2 nozzle shall be of the types and classes
specified herein.
1.2.1 T’Vna
a. ~:
Nozzle capable of off-center disconnects up to
15 degrees maximum
(see
3.9.1).
b. XY.Q!L2:
Nozzla capable of off-center disconnects up to 22-1/2 degrees
maximum (see 3.9.1}.
1.2.2 g.j+me$
a. Q&%Ul:
NOZZh capable of operating in
temperature range and fuel tempe~a?mre
range
b. 4LwLB:
Nozzle
capable of operatkng in
temperature range and fuel temperature range
PAGE 5
the
-67QF to 160QF ambient
of
-6~oF ~0 1350~.
the
-670F to 3500F ambient
of -6ToF to 2000F.~
3.9 Lime 19:
Delete and substitute
After line 19 “(o)” add:
‘(p)
[q)
‘(o] ImmersioLI (leakage) (4.6. 15)n.
Emergency
disconnect
(Type 2
~OZZl@ Ody)
(4.6.16)
Disassembly and inspection
(4.6.17)n.
PAGE
6
3.9.1 Line 12 (7th sentence):
.
after “22-1/2 degrees” insert
“for Type 2 and 15
degrees for Type Ifr.
Line 15 (8th sentence): after
the words ‘breakage of nozzle partsm, add
“or, for Type 2 nozzles, permanent set of any Partw.
Fsc 1680
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