BELL HELICOPTER 430 - Table 4-1. Airworthiness Limitations Schedule (Cont); CONTROL SYSTEM BOLTS AND PINS (CONT); TAIL ROTOR AND CONTROLS; TRANSMISSION AND DRIVE SYSTEM

BHT-430-MM-2 TC APPROVED
4-00-00
Page 8 Rev. 19 1 NOV 2012
ECCN EAR99
CONTROL SYSTEM BOLTS AND PINS (CONT)
Cyclic Lever to Actuator Bolt 50-047C8-31 5000
Collective Lever to Idler Link Bolt 50-047C8-135 5000
Idler Link to Swashplate Support Bolt 50-047C8-82 5000
Collective Lever to Actuator Bolt 50-047C8-31 5000
Actuator to Actuator Support Bolt 50-047C8-31 5000
Ball Sleeve to Collective Lever Pin 430-010-442-101 5000
Collective Lever to Cyclic Lever Pin 430-310-455-101 5000
TAIL ROTOR AND CONTROLS
Tail Rotor Blade Assembly 222-016-001-123 5000
Tail Rotor Yoke Assembly 222-012-702-109 5000
Tail Rotor Trunnion Assembly 222-012-703-107 5000
TRANSMISSION AND DRIVE SYSTEM
Main Rotor Mast Assembly 430-040-130-101 10,000
Tail Rotor Output Shaft 222-042-402-005 5000
PYLON SYSTEM
Pylon Fluid Mount 430-310-200-103/-105/-107 10,000
FIRE PROTECTION SYSTEM
Cartridge Fire Extinguisher 13083-5 6 years in service or
total life
Float Reservoir 222-325-021-101 15 years
Float Reservoir 222-025-875-101 15 years
Table 4-1. Airworthiness Limitations Schedule (Cont)
COMPONENT PART NUMBER AIRWORTHINESS LIFE
1
4
2
5
3
3