AD 2021-10-14

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

AD Number
2021-10-14
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2021-0143
FR Citation
86 FR 27268

Applicability

TypeManufacturerModelDetails
aircraft Airbus Helicopters Deutschland GmbH Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters
aircraft Aviat Various Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

Unsafe Condition

aging of the elastomeric material in a tension torsion strap (TT-strap) could affect the structural characteristics of the TT-strap, leading to premature failure of a TT-strap, resulting in loss of control of the helicopter.

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

Required Actions

replace certain TT-straps with serviceable parts and implementation of a new storage life limit for TT-straps, as specified in an EASA AD.

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

Compliance Time

Within 50 flight hours

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

Affected Aircraft

Airbus Helicopters Deutschland GmbH Model BO-105A, BO-105C, BO-105S, and BO-105LS A-3 helicopters, certificated in any category, equipped with a tension torsion strap (TT-strap) as identified in EASA AD 2019-0024.

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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