MIL I 5014F (修正4) 内管气动管飞机 (1992年11月16日) [S S由SEA AS50144]

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时间:2023-03-23

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上传者:战必胜
MIL-I-5014F
Amendment 4
16 November 1992
SUPERSEDING
AMENDMENT 3
18. February 1980
MILITARY SPECIFICATION
INNER TUBE, PNEUMATIC TIRE, AIRCIWFT
This amendment forms a Dart of Militarv Specification
MIL-I-5014F, dated 1 Octobe; 1971, and is ~pp;oved for use by all
the Departments and Agencies of the Department of Defense.
PAGE 8
Table VI, add note 2, “(2) For H-60 tail wheel inntertube use
Valve Figure 5.”
TABLE VI - Physical Characteristics of Tube (1) for
Type VI (low profile) Casings
Class
Size
Thickness
Weight
Unbalance Valve
(rein) (in)
(max) (max)
Figure
(pounds)
(in 02) Number
Crown
Base
Nose Wheel
15X6.O-6
0.060 0.060
2.12 8
1, (2)
Tubes
22X7.11.50 .065
.090
3.75 6
1
(l)Tube in table inactive for new design.
(2)For H-60 tail wheel innertube use valve Figure 5.
Beneficial comments (recommendations, additions, deletions) and
any pertinent which may be of use in improving this document
should be addressed to:
HQ AFLC
CASO/LODS, Federal Center,
Battle Creek, MI, 49016, by using the self-addressed
Standardization Document improvement
Proposal (DD Form 1426)
appearing at the end of this document or by letter.
FSC 2620
DISTRIBUTION STATEMENT A. Approved for public release,
distribution is unlimited.
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