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| MIL-D-23222A(AS)
SYMBOLS AND ABBREVIATIONS. - The following symbols
6.4.3.7
and abbreviations are used herein:
ASW
Antisubmarine-warfare
Mach number
M
Side load factor
ny
Maximum symmetrical flight limit load
n Z
factor (i.e. the upper boundary of the
design V-n diagram).
Minimum symmetrical flight limit load
-nZ
factor (i.e. the lower boundary of the
design V-n diagram).
Maximum level flight speed specified for
vH
structural design.
Limit speed parameter in basic configura-
VL
tion specified for structural design.
Cruise speed as defined by the detail speci-
VC
fication.
Vmax
Maximum level flight speed as limited by power.
ADDENDA TO THIS SPECIFICATION. - This specification
6.5
shall be used as the standard form for the preparation
of addenda by NAVAIR for specific model helicopters. Addenda shall conform
to the following:
Agree with this specification in paragraph arrange-
(1)
ment, numbering, and headings, except that where a
paragraph is listed in the addendum as "not appli-
cable" or "not required" subsequent sub-paragraphs
will be omitted provided numbering sequence is not
affected.
(2)
Unless paragraphs of addenda completely supersede
corresponding paragraphs of this specification,
paragraphs will be listed as "applicable" (with
or without specific deviation or supplementary
requirements), "not applicable", or "not reequired".
General requirements or instructions will be desig-
nated as "applicable", or "not applicable", however,
requirements for specific data or action shall be
designated "required" or "not required" as applicable.
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