CSP-HMI-3MD Helicopters, Inc.
MAINTENANCE MANUAL
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Copyright © 1999−2016 by MD Helicopters, Inc.
K. Directional Gyro Indicator Installation
(R/H Command T−Panel)
(Ref. Figure 201)
Consumable Materials
(Ref. Section 91−00−00)
Item
Nomenclature
CM704 Tie strap, nylon
CM706 Tie strap base
(1). Install directional gyro indicator to the
instrument panel, using screws,
washers, and post light assembly.
(2). Install circuit breaker (CB135).
(3). Position wiring harness on instrument
panel structure at existing tooling
holes. Secure wiring harness to instru
ment panel, using tie strap (CM704)
and tie strap bases (CM706) as re
quired.
L. Completion of Installation
(1). Check entire installation for complete
ness.
(2). Check all electrical wiring.
(3). Clean all foreign material from instru
ment panel.
(4). Perform operational check of completed
installation.
(5). Reinstall instrument panel left and
right fairing and hood.
M. Weight and Balance Data
Weight and balance data changes that result
from installation of the directional gyro
indicator are listed in Table 901. After
installation, incorporate changes to 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)
369H90039−501, −505, −509 and −701
Added +3.1 (+1.4061) 43.0 (109.22) +133.3 (+1535.78)
Removed 0.0 0.0 0.0
Change
+3.1 (+1.4061) 43.0 (109.22) +133.3 (+1535.78)