CSP−900RMM−2 MD Helicopters, Inc.
Rotorcraft Maintenance Manual
Page 602
Revision 35
25-10-00
9G25−025
25
SPACER
FIXED FITTING
0.1 IN
(2.54 mm)
MAIN
TUBE
SEAT
FRAME
CREW
SEAT
Figure 601. Seat EAS Inspection
C. Seat Restraint System Inspection (Area
1)
(1). Examine restraint system for correct
installation and operation as follows:
(a). Belt adjust mechanism for correct
operation and condition.
1). No damage permitted.
(b). Deleted.
(c). Inertia reel for damage, wear, and
smooth operation as follows:
1). Make sure harness strap cannot be
pulled out of inertia reel when fully
extended.
2). With tension released, harness
strap must automatically retract
back into reel mechanism.
3). Apply a sudden forward pull on
seat belt or shoulder strap to make
sure inertia reel locks.
4). Examine handle and cable of
manual lock system for condition
and correct operation.
5). No defects permitted.
(2). Examine belts and straps for cleanli
ness, damage, and wear.
NOTE: Light wear, frays, and rough spots
caused by normal operation of the buckles,
latches, and releases are permitted.
To Next Page
Loading...
