MIL-S-6144A
3.1.2
Type II Installation - The component materials used
for Type II Installation shall substantially consist of rigidized fibrous glass
insulation, equivalent or similar to that conforming to MIL-B-5924, suitably
contained or otherwise protected (see 3.4 and 3.7) and installed with flexible
trim material separately attached to the aircraft structure.
3.1.3
Type III Installation - The construction of the Type III
Installation shall substantially consist of rigidized fibrous glass insulation, equivalent
or similar to that conforming to MIL-B-5924 suitably contained or otherwise
protected (see 3.5 and 3.8) and installed with rigid lining material separately
attached to the aircraft structure. Alternately, rigid lining material may be
attached over a Type I (blanket) Installation, as is typified in Figure 1 (a) for part
of a cargo compartment installation, Figure 2 (a) depicts a typical installation in
which the rigid trim is attached as a separate unit over insulating material,
Figure 2 (b) depicts an alternate approach in which the insulating material is
cemented to the rigid trim and, as a unit, is attached to the aircraft structure.
3.2
Attachment of Materials - The means used to affix. support or
seal the thermal-soundproofing installation shall consist of one, or several, of
the following:
Mechanical Fasteners
A.
1.
Quick Release
(a)
Curtain (Style 1 of MIL-F-10884)
(b)
Snap (Style 2 of MIL-F-10884)
(c)
Slide (V-F-106)
Quarter-turn (MIL-F-5591)
(d)
(e)
Latch, Flush Type (NAS 442)
2.
Studs - Plastic, Serrated, with push-on clip.
3.
Screws, Machine - (FF-S-92 or Equivalent}
4.
Screws, Self-tapping - (MIL-S-6033 or Equivalent)
B.
Nylon Tape Fasteners (MIL-F-21840)
C.
Lacing, Nylon
Adhesive (MIL-A-3316 or Equivalent)
D.
3
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