CSP-HMI-3
MD Helicopters, Inc
.
MAINTENANCE MANUAL
97-08-00
Page 905
Revision 12
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.
G97-0803-2A
INSTRUMENT
PANEL
CM 888
MICROPHONE
B
B
RMC-1S-A
CONTROL UNIT
SUPPOR
T
INSTRUMENT PANEL AND
CONTROL UNIT
EXISTING
NUTPLATE
STRUCTURAL LIGHTENING
HOLE (TYPICAL)
2.00-2.12 IN.
(5.08-5.384 CM)
HOO
D
0.299-0.311 IN.
(7.595-7.899 MM)
WL 40.40
1.25 IN. (38.10 CM)
CUTOUT IN FAIRING
GROMME
T
SIDE
FAIRING
STA
40.00
VIEW
B - B
NUTPLATE AND CUTOUT
LOCATIONS
STRUCTUR
E
EXISTING
NUTPLATE
STRUCTURE
STIFFENER
NUTPLATES FOR
CONTROL UNIT
SUPPORT (NOTE 2)
NOTES:
1.
DOUBLER ON FUSELAGE SKIN REQUIRES
SIX EQUALLY SPACED RIVETS.
2.
EXISTING RIVET HOLES ARE ENLARGED
FOR NUTPLATE INSTALLATIONS. DETERMINE
NUTPLATE LOCATIONS FROM EXISTING
RIVETS ABOVE AND BELOW EXISTING
NUTPLATES, STRUCTURE LIGHTENING
HOLES, AND STRUCTURE STIFFENER AS SHOWN.
Figure 901. Modification and Reinforcement dimensions (Sheet 2 of 2)
Содержание 369-500
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