AD 2015-16469

final rule
Data completeness: 70%

Airworthiness Directives; Bell Helicopter Textron Canada

AD Number
2015-16469
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2014-0499
FR Citation
80 FR 38613

Applicability

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

Unsafe Condition

Fatigue failure of a tail rotor control tube bonded clevis, which could result in failure of the tail rotor control tube and subsequent loss of helicopter control.

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

Required Actions

Inspect the tail rotor control tube assembly (control tube) and either repair or replace the control tube.

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

Compliance Time

Before further flight

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

Affected Aircraft

Bell Helicopter Textron Canada Model 430 helicopters, serial number 49001 through 49121, with control tube assembly (control tube), part number (P/N) 430-001-007-101 installed.

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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