AD 2018-02-08

final rule
Data completeness: 80%

Airworthiness Directives; Bell Helicopter Textron Helicopters

AD Number
2018-02-08
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2017-0895
FR Citation
83 FR 2358

Applicability

TypeManufacturerModelDetails
aircraft Textron Various Airworthiness Directives; Bell Helicopter Textron Helicopters
aircraft Bell Helicopter Textron Airworthiness Directives; Bell Helicopter Textron Helicopters

Unsafe Condition

A crack, corrosion, an edge void, loose or damaged adhesive squeeze-out, or an edge delamination in the M/R blade could lead to failure of the blade and subsequent loss of helicopter control.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Within 25 hours time-in-service (TIS) or 2 weeks, whichever occurs first, and thereafter at intervals not to exceed 25 hours TIS or 2 weeks, whichever occurs first, cleaning the upper and lower exposed surfaces of each M/R blade from an area starting at the butt end of the blade to three inches outboard of the doublers. Visually inspecting various M/R blade parts for a crack or corrosion. If there is a crack, corrosion, an edge void, loose or damaged adhesive squeeze-out, or an edge delamination, before further flight, repairing the M/R blade or replacing it with an airworthy M/R blade, depending on whether the condition is within maximum repair damage limits. Reporting information about any cracks found during the inspection to the FAA within 10 days.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 25 hours time-in-service (TIS) or 2 weeks, whichever occurs first

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Bell Helicopter Textron, Inc., P.O. Box 482, Fort Worth, TX 76101; Bell 204B, 205A, and 205A-1 helicopters with an HTC M/R blade part number (P/N) 204P2100-101 installed.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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