AD 2003-01-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron | Inc | Airworthiness Directives; Bell Helicopter Textron, Inc. Model 204B, 205A, 205A-1, 205B and 212 Helicopters |
| aircraft | Bell | Helicopter Textron | Airworthiness Directives; Bell Helicopter Textron, Inc. Model 204B, 205A, 205A-1, 205B and 212 Helicopters |
Unsafe Condition
Cracking of the main rotor grip in the lower tang, which could lead to separation of a main rotor blade and subsequent loss of control of the helicopter.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the main rotor grip for cracks. Replace the grip if a crack is found. Inspect the grip surface for corrosion or other damage if delamination of the buffer pad is found, and repair or replace the grip if necessary. Determine and record the hours time-in-service (TIS) and engine start/stop cycles for each grip. Report inspection results and information to the FAA.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight if a crack is found; otherwise, within the specified inspection intervals.
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Affected Aircraft
Bell Helicopter Textron, Inc. Model 204B, 205A, 205A-1, 205B, and 212 helicopters.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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