| DOCUMENT | TITLE | COMPLIANCE | DATE |
|---|---|---|---|
| BELL HELICOPTER | |||
| 412-24-197 | Cap Angle, P/N 212-030-191-001, Special Inspection Interval, Reduction of (Models: 212, 407, 412, 429) | Alert | 4/22/2024 |
| 412-24-198 | Upper Left Hand Tailboom Attachment Fitting, Sealant Removal of (Model: 412EP) | Alert | 4/22/2024 |
| 407-24-135 | Cyclic Control AFCS Kit Incorrect Hardware, Inspection Of (Model: 407) | Alert | 5/21/2024 |
| 429-24-63 Rev. A | Tail Rotor Blade 429-016-101-105 Abrasion Strip, Inspection of (Model: 429) | Alert | 5/30/2024 |
| 505-24-40 | Tail Rotor Segmented Driveshaft Assembly, One-Time Inspection Of (Model: 505) | Alert | 6/10/2024 |
| 206-24-143 | Tail Rotor Segmented Driveshaft Assembly, One-Time Inspection Of (Models: 206A/B, TH-67) | Alert | 6/20/2024 |
| 206L-24-189 | Tail Rotor Segmented Driveshaft Assembly, One-Time Inspection Of (Models: 206L, 206L-1, 206L-3, 206L-4) | Alert | 6/20/2024 |
| 407-24-137 | Main Rotor Expandable Blade Bolt 406-310-103-103, Removal from Service (Model: 407) | Alert | 7/18/2024 |
| 206-24-144 | Swashplate Outer Ring and Collective Lever, Clearance Check of (Models: 206A/B, TH-67) | Alert | 7/25/2024 |
| 206L-24-190 | Swashplate Outer Ring and Collective Lever, Clearance Check of (Models: 206L, 206L-1, 206L-3, 206L-4) | Alert | 7/25/2024 |
| 407-24-136 | Standard and High Landing Gear Forward Crosstubes, Inspection of (Model: 407) | Alert | 7/25/2024 |
| 206L-24-55 | Cyclic and Collective Flight Controls Rigging Requirements (Models: 206L, 206L-1, 206L-3) | Operational | 5/15/2024 |
| 407-24-25 | AFCS Uncommanded Pitch Up With Loss Of SBAS Signal (Model: 407) | Operational | 6/27/2024 |
| 204B-24-29 | Main Rotor Hub Pillow Block Inspection Requirements (Models: 204B, 205A1, 205B, 212) | Informational | 5/14/2024 |
| 205A1-24-46 | Main Rotor Hub Pillow Block Inspection Requirements (Models: 204B, 205A1, 205B, 212) | Informational | 5/17/2024 |
| 205B-24-30 | Main Rotor Hub Pillow Block Inspection Requirements (Models: 204B, 205A1, 205B, 212) | Informational | 5/17/2024 |
| 212-24-77 | Main Rotor Hub Pillow Block Inspection Requirements (Models: 204B, 205A1, 205B, 212) | Informational | 5/17/2024 |
| 412RSAF-24-18 | Collective Stick Tube Inspection, Change of (Model: 412RSAF) | Informational | 5/17/2024 |
| 212-24-76 Rev.A | Collective Stick Tube Special Inspection, Change of (Models: 212, 412) | Informational | 5/28/2024 |
| 412-24-96 Rev.A | Collective Stick Tube Special Inspection, Change of (Models: 212, 412) | Informational | 5/28/2024 |
| 407-24-129 | Main Rotor Blade Bolts, Overhaul Requirement Clarification (Model: 407) | Informational | 6/10/2024 |
| 212-24-78 | Introduction of Bell MissionLink Revision 2 (Models: 212, 407, 412, 429) | Informational | 6/20/2024 |
| 407-24-130 | Introduction of Bell MissionLink Revision 2 (Models: 212, 407, 412, 429) | Informational | 6/20/2024 |
| 412-24-97 | Introduction of Bell MissionLink Revision 2 (Models: 212, 407, 412, 429) | Informational | 6/20/2024 |
| 429-24-23 | Introduction of Bell MissionLink Revision 2 (Models: 212, 407, 412, 429) | Informational | 6/20/2024 |
| 505-24-40 | Safran Helicopter Engines, Arrius 2R Service Bulletin No. 319 72 4853 (Module M02, Gas Generator, High Pressure Turbine Blades) (Model: 505) | Informational | 6/20/2024 |
