CSP-HMI-3
MD Helicopters, Inc
.
MAINTENANCE MANUAL
96-00-00
Page 603
Revision 13
The information disclosed herein is proprietary to MD Helicopters, Inc.
Neither this document nor any part hereof may be reproduced or transferred to
other documents or used or disclosed to others for manufacturing or any other
purpose except as specifically authorized in writing by MD Helicopters, Inc.
Copyright
©
1999
−
2016 by MD Helicopters, Inc.
G96-0033-3
NOTE 1
NOTES:
1.
MOLD FLASH OR OTHER MOLD IMPERFECTIONS WHICH DO NOT
CAUSE VOIDS BETWEEN GROMMET AND WIRE AFTER CONTACT IS
INSTALLED.
2.
SLIGHT IMPERFECTIONS, MINOR SCUFFS, SCRATCHES, GOUGES,
CUTS, AND TEARS IN CAVITY SEPARATOR.
3.
A GOUGE, CUT, TEAR, CRACK, OR CHIP ON INNER OR OUTER
PERIMETER OF PIN BARRIER CONE THAT DOES NOT EXCEED 50%
O
O
CO
ACCEPTABLE DEFECTS
MATING FACE, PIN INSERT)
NOTE 2
NOTE 3
Figure 602. Accept/Reject Criteria for Connector Defects (Sheet 3 of 6)
G96-0033-4
UNACCEPTABLE DEFECTS
MATING FACE, PIN INSERT)
NOTE 1
NOTES:
1.
A GOUGE, CUT, TEAR, CRACK, OR CHIP WHICH ENTERS INNER
PERIMETER OF PIN BARRIER CONE, OR EXCEEDS 50% OF WALL
WIDTH.
2.
A GOUGE, CUT, TEAR, CRACK, OR CHIP WHICH EXTENDS FROM
OUTER EDGE OF GROMMET FACE TO A PIN BARRIER CONE.
3.
A GOUGE, SPLIT, OR CRACK ALONG CIRCUMFERENCE AT BASE
OF PIN BARRIER CONE.
4.
A GOUGE, CUT, TEAR, CRACK, OR CHIP WHICH EXTENDS FROM
PIN BARRIER CONE TO ANOTHER PIN BARRIER CONE.
5.
SEVERE GOUGE, CUT, TEAR, CRACK, OR CHIP IN CAVITY
S
O
NOTE 2
NOTE 3
NOTE 4
NOTE 5
NOTE 6
Figure 602. Accept/Reject Criteria for Connector Defects (Sheet 4 of 6)
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