BHT-212-MM-1
5-00-00
Page 32 Rev. 14 26 JUN 2013 Export Classification C, ECCN EAR99
3. Install hydraulic filter elements.
Chapter 63 4. Install 0 to 500 PSIG (0 to 3447 kPa) gauge in quick
disconnect at rotor brake caliper. Slowly pull rotor brake handle
through travel. Cylinder should generate 240 to 260 PSI (1655
to 1793 kPA) at any handle velocity and shall maintain 150 PSI
(1034 kPa) minimum in over center position for 3 minutes.
Adjust as necessary.
5. Inspect rotor brake linings for wear (minimum thickness
0.150 inch (3.81 mm)).
Chapter 32 LANDING GEAR SYSTEM
— General Visual Inspection
1. If installed, emergency float reservoir pressure indicator for
proper charge indication.
2. If installed, floats for proper stowage and condition.
3. Landing gear crosstube assemblies, skid tubes, and skid
shoes, for condition and security of attachment. Inspect
crosstube retention cap (rubber bumper pads) for condition and
security of attachment.
4. Tail skid for deformation and security of attachment.
5. Fuselage supports for wear, damage, and security of
attachment.
6. If installed, landing gear forward crosstube crew step
fittings for corrosion, damage, and security in area of
attachment.
— Restoration
1. Torque check crosstube to skid tube saddle bolts.
2. Torque check forward and aft crosstube support fittings U
bolts to 80 to 100 inch-pounds (9.0 to 11.3 Nm).
5-9. 100 HOURS/12 CALENDAR MONTHS — PART A (CONT)
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
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