Textron Bell 206A Series, Руководство по обслуживанию

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BHT-206A/B-SERIES-MM-1
5-00-00
Page 144
Rev. 14 30 APR 2013 Export Classification C, ECCN EAR99
Table 5-4. Special Inspections
COMPONENT
INSPECTION SCHEDULE
HOURS AFTER INITIAL INSTALLATION
INITIAL
1 TO 5
HOURS
3 TO 8
HOURS
10 TO 25
HOURS
100 ±10
HOURS
Main Rotor Hub Mast Nut Torque Check
(
paragraph 5-47 )
X
Pillow Block Retention Bolts Torque
Check (
paragraph 5-48 )
X
Tail Rotor Gearbox Torque Check
(
paragraph 5-49 )
X
Swashplate Tilt Friction ( paragraph
5-49 )
X
Disc Pack Coupling Torque Check
(
paragraph 5-49 )
X
Power Plant Torque Check ( paragraph
5-50 )
X
Tailboom Attachment Torque Check
(
paragraph 5-50 )
X
Transmission Top Case Torque Check
(
paragraph 5-50 )
X
Fuel System ( paragraph 5-46 ) Immediately after maintenance or component
change
NOTES:
Retouch corrosion preventive compound and anti-slippage marks as required after torque check.
Repeat torque check every 100 flight hours.
Torque check must be repeated every 10 to 25 hours until the torque is stabilized. After torque has
stabilized, repeat torque check every 300 flight hours.
If fastener is improperly torqued:
• Inspect nuts and bolt threads, and shank for damage.
• Inspect engine mounts and supporting structure for damage.
Repeat the swashplate tilt friction check every 300 flight hours.
Complete fuel system operational check immediately after fuel system maintenance or component
change (
paragraph 5-46 ).
1
2
4
3
5
1
2
3
4
5