CSP−900RMM−2 MD Helicopters, Inc.
Rotorcraft Maintenance Manual
Page 604
Revision 35
25-10-00
(a). No damage permitted.
(4). Examine carpet for cuts, tears, correct
installation, or other unserviceable
conditions.
(5). Examine composite or laminated panels
for correct installation and condition.
(6). Examine panels for dents, scratches,
and impact damage.
NOTE: Repairs are not recommended for
scratches or dents which are less than 1.20
inch (30.5 mm) from a fastener or 1.97
inch (50.0 mm) from edge of panel.
(a). Repair scratches or dents with filler
compound (C812).
NOTE: Repairs are not recommended when the
center of the damage is less than 1.97 inch
(50.0 mm) from a fastener or 3.15 inch
(80.0 mm) from edge of panel.
(b). Repair holes or impact damage on
composite honeycomb panels.
1). The maximum repair dimension is
1.57 inch (39.9 mm).
(7). Make sure you can read the placards
and decals.
(8). Make sure placards and decals are
correctly installed.
(9). Examine checklist and magnetic
compass card for condition.
(10). Make sure you can read checklist and
magnetic compass card.
E. Seat Operational Test
(1). Operate seat adjust lever under front of
crew seat.
(2). Make sure position lock pin mechanism
releases.
(3). Hold lock mechanism unlocked and
move seat forward-up and aft-down.
(a). Make sure seat moves smoothly
through full travel.
(4). Move seat forward-up and aft-down
and release lock mechanism at each
lock position.
(a). Make sure seat locks in all positions
and lock pins fully engage.
F. Seat Restraint System Operational Test
(1). Latch lap belt and shoulder harness.
(a). Make sure latch mechanism operates
correctly.
(b). Make sure straps do not disengage
from buckle unless released by
buckle operation.
(2). Move manual control handle forward to
the manual lock position.
(a). Make sure straps lock.
(b). Do again at one other position.
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