CSP-HMI-3 MD Helicopters, Inc.
MAINTENANCE MANUAL
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Revision 7
95-10-20
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.
D. Weight and Balance Data
(Ref. Table 901) Changes in weight and
balance resulting from the installation of the
RCA26BK-1 or 510-1A12 Attitude Gyro
Indicator, noise filter, switch, circuit breaker,
support assembly, associated hardware, and
wire harness(es) are listed. Ensure that the
changes are incorporated in helicopter weight
and balance records as instructed (Ref. Sec.
08-10-00).
Table 901. Weight and Balance Data
Configuration
Weight
Pounds (kg)
Arm
inches (cm)
Moment
in−lb (kg cm)
369H90038 or 369D294501
Added +2.8 (+1.2701) +43.0 (+109.22) +120.4 (+13.87.15)
Removed 0.0 0.0 0.0
Net Change +2.8 (+1.2701) +43.0 (+109.22) +120.4 (+13.87.15)
G95-1021A
1.25 INCH
(3.175 CM)
0.75 INCH
(19.05 MM)
0.168-0.175 INCH
(4.2672-4.4450 MM)
DIA. HOLE
E26
0.87 INCH
(22.098 MM)
TB103
1.19 INCH
(3.0226 CM)
0.112-0.116 INCH
(2.8448-2.9464 MM)
DIA. HOLE (2 PLCS)
1.50 INCH
(3.81 CM)
PITOT TUBE
INSTRUMENT PANEL LOWER SUPPORT
C
BEAD
L
C
BEAD
L
Figure 904. Terminal Board Installation (Slim−Line Instrument Panel)
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