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

TC APPROVED BHT-430-MM-2
4-00-00
1 NOV 2012 Rev. 19 Page 7
ECCN EAR99
MAIN ROTOR CONTROLS
Main Rotor Pitch Link Assembly 430-010-411-105/-107 10,000
Drive Hub Assembly 430-010-410-101 10,000
Drive Idler Link Assembly 430-010-409-105 10,000
Drive Link Assembly 430-010-408-101 10,000
Rotating Ring Assembly 430-010-401-101 10,000
Non-rotating Ring Assembly 430-010-402-101 10,000
Cyclic Link Assembly 430-010-412-105 10,000
Swashplate Support Assembly 430-010-404-101 10,000
Swashplate Ball and Sleeve Assembly 430-010-403-101 10,000
Collective Lever Assembly 430-010-405-105 10,000
Collective Idler Link Assembly 430-010-407-101 10,000
Cyclic Lever Assembly 430-010-406-101 10,000
Actuator Support Assembly 222-040-125-001 5000
CONTROL SYSTEM BOLTS AND PINS
Pitch Horn to Universal Bolt 50-047C6-36 5000
Universal to Pitch Link Bolt 50-047C6-28 5000
Pitch Link to Rotating Ring Bolt 50-047C6-32 5000
Drive Hub to Drive Hub Bolt 20-057C5-19 5000
Drive Hub to Idler Link Bolt 50-047C6-99 5000
Idler Link to Drive Link Bolt 50-047C6-99 5000
Drive Link to Rotating Ring Bolt 50-047C6-49 5000
Non-rotating Ring to Cyclic Link Bolt 50-047C6-32 5000
Cyclic Link to Cyclic Lever Bolt 50-047C6-32 5000
Table 4-1. Airworthiness Limitations Schedule (Cont)
COMPONENT PART NUMBER AIRWORTHINESS LIFE
1