BELL HELICOPTER 430 Maintenance Manual page 19

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