| DOCUMENT | TITLE | COMPLIANCE | DATE |
|---|---|---|---|
| BELL HELICOPTER | |||
| 407-24-134 | Tailboom Attachment Hardware and Fittings, Inspection of (Model: 407) | Alert | 2/12/2024 |
| 429-23-60 Rev A | Tail Rotor Shaft Assembly 429-044-201-107, Inspection of and Introduction of Airworthiness Limitation Schedule (Model: 429) | Alert | 2/13/2024 |
| 412RSAF-24-53 | Cap Angle, P/N 212-030-191-001, Special Inspection Interval, Reduction of (Model: 412RSAF) | Alert | 2/22/2024 |
| 429-24-62 | Main Rotor Pitch Link Rod End 429-010-433-103, One Time Verification of (Model: 429) | Alert | 3/12/2024 |
| 429-24-63 | Tail Rotor Blade 429-016-101-105 Abrasion Strip, Inspection of (Model: 429) | Alert | 3/21/2024 |
| 206L-23-188 Rev A | Horizontal Stabilizer and Cargo Hook Fittings – Self Locking Inserts, Inspection of (Models: 206L, 206L-1, 206L-3, 206L-4) | Alert | 3/27/2024 |
| 429-16-29 Rev C | Fwd Center Firewall Welded Assembly 429-069-501-101/-109/-113 and Aft Center Firewall Welded Assembly 429-069-504-101/-103/-105, Inspection and Repair of (Model: 429) | Alert | 3/27/2024 |
| 205-24-122 | Inspection of Cap Angle, P/N 205-030-207-005, Introduction, of (Model: 205A/205A-1) | Alert | 4/22/2024 |
| 205B-24-77 | Inspection of Cap Angle, P/N 205-030-207-005, Introduction, of (Model: 205B) | Alert | 4/22/2024 |
| 212-24-169 | Inspection of Cap Angle, P/N 212-030-191-001, Introduction, of (Model: 212) | Alert | 4/22/2024 |
| 412-24-197 | Cap Angle, P/N 212-030-191-001, Special Inspection Interval, Reduction of (Model: 412/412EP) | Alert | 4/22/2024 |
| 412-24-198 | Upper Left Hand Tailboom Attachment Fitting, Sealant Removal of (Model: 412EP) | Alert | 4/22/2024 |
| 505-24-37 | Rotorcraft Flight Manual BHT-505-FM-1 Revision 11 and Associated Temporary Revision Cancelations and Updates, Introduction of (Model: 505) | Alert | 4/22/2024 |
| 429-24-71 | 429-010-108-101 and -105 Grip Assembly Corrosion Protection (Model: 429) | Technical | 2/28/2024 |
| 407-17-125 Rev A | Aft Fuselage 2-piece Upper Left Longeron Assembly 407-030-067-105, Installation of. (Model: 407) | Technical | 4/4/2024 |
| 407-07-78 Rev B | Aft Fuselage Bulkhead 407-030-027-101 at FS 231.4, Introduction of (Model: 407) | Technical | 4/9/2024 |
| 206L-24-189 | Main Rotor Mast 206-040-535-109 Airworthiness Life, Increase of (Model: 206L) | Informational | 3/21/2024 |
| 505-24-39 | Main Rotor Mast 206-040-535-109 Airworthiness Life, Increase of (Model: 505) | Informational | 3/21/2024 |
| 429-24-21 | Alternative Method of Compliance (AMOC) to Federal Aviation Administration (FAA) Airworthiness Directive (AD) 2024-07-51 (Model: 429) | Informational | 4/23/2024 |
| 429-24-22 | Global Alternative Means of Compliance (AMOC) with TCCA Airworthiness Directive (AD) CF-2024-11 (Model: 429) | Informational | 4/23/2024 |
