BHT-206A/B-SERIES-MM-1
5-00-00
30 APR 2013 Rev. 14
Page 151
Export Classification C, ECCN EAR99
SPECIAL INSPECTIONS
5-49.
10 TO 25 HOURS AFTER EACH INSTALLATION
DATA REFERENCE
INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
DATE: __________________W.O. _____________________
FACILITY: __________________________________________
HELICOPTER S/N: ___________________________________
REGISTRY NO.: _____________________________________
TOTAL TIME:_______________________________________
SIGNATURE:_______________
_________________________
SWASHPLATE ASSEMBLY
Chapter 62
1.
Check swashplate tilt friction. Value must be between 15 to
32 pounds (67 to 142 N), if not within limits, adjust to 15 to
32 pounds (67 to 142 N) and check tilt friction every 10 to
25 hours until it is stabilized.
Chapter 65
DISC PACK COUPLING
1.
Torque check disc pack coupling attaching hardware as
follows:
a.
Apply the minimum torque (50 inch-pounds (5.65 Nm))
required for the fasteners. If the fasteners do not move, the
check is completed. Check torque seal and apply as required.
b.
If the fastener(s) moved, do the steps that follow:
(1)
Remove the affected disc pack coupling and
examine the bolts, nuts (minimum tare torque, refer to
BHT-ALL-SPM) and washer for condition. Discard damaged
parts.
(2)
Examine the disc pack coupling for condition.
Discard damaged disc pack coupling.
c.
Install the removed disc pack coupling and repeat
torque check after 10 to 25 hours.
Summary of Contents for Bell 206A Series
Page 10: ......
Page 16: ......
Page 20: ......
Page 34: ......
Page 40: ......
Page 48: ......
Page 66: ......
Page 80: ......
Page 86: ......
Page 94: ......
Page 102: ......
Page 116: ......
Page 122: ......
Page 124: ......
Page 138: ......
Page 142: ......
Page 144: ......
Page 150: ......
Page 162: ......
Page 166: ......
Page 168: ......
Page 178: ......
Page 180: ......
Page 186: ......
Page 192: ......
Page 198: ......
Page 202: ......
Page 206: ......
Page 212: ......
Page 228: ......
Page 230: ......