Model FA2100 CVR
Instruction Manual
Installation & Operation
165E1846–00
Jan. 01/03
Rev. 07
Page 12
NAMEPLATE INFO:
NAME: MOUNT, HARD, CVR
PN: 178–E0919–00 REV [X]
SN: XXXXX
DATE: MM/YY
5.38 MAX
OUTSIDE
4X 0.182
$
.010
100
°
CSK
(CG)
9.06
5.60
$
.50
CL
3.50
4.12
5.02
$
.02
INSIDE
2.38
1.00 MAX
(CG)
.75
$
.50
.80 MAX
16.41 MAX
4.00 MAX
CLEARANCE HOLES
FOR #8 SCREWS
3.500
$
.005
SUGGESTED MOUNTING HOLE PATTERN
9.062
$
.005
COMP
ANY LOGO
NOTES:
1.
UNDIMENSIONED FEATURES (SUCH AS SIDE RAILS, TABS, FLANGES, AND WEIGHT-REDUCING HOLES) MAY VARY
PICTORIALLY FROM THIS DRAWING.
2.
WEIGHT 1.3 LBS. MAX.
3.
CONNECTOR MOUNTING HOLE IS DESIGNED FOR:
(CRIMP) PN 063–98–01474 (CANNON DPXBMA–57–33S–0001)
(SOLDER) PN 9300–435 (CANNON DPXB–57–33S–0001)
4.
SUGGESTED MOUNTING HARDWARE:
TO ATTACH CONNECTOR TO MOUNT: 8 EACH 4–40 X 7/16 PAN HEAD SCREWS PN 229–02–00076 (MS51957–16) OR
EQUIV, AND 4–40 SELF-LOCKING NUTS, PN 16165 (ESNA PN 68–1660–40) OR EQUIV.
TO ATTACH MOUNT TO AIRCRAFT: 4 EACH #8 100
T HEAD SCREWS MS24693–( ) OR EQUIV (LENGTH AS REQD),
AND SELF-LOCKING NUTS MS21044–C08 OR EQUIV.
905–E0919–18H
Figure 4.
Outline and Dimensions, CVR Mount, Part Number 178E0919–00
