AD 2013-16-06

final rule
Data completeness: 80%

Airworthiness Directives; Eurocopter Deutschland GmbH Helicopters

AD Number
2013-16-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2011-1285
FR Citation
78 FR 48599

Applicability

TypeManufacturerModelDetails
aircraft Eurocopter Deutschland GmbH Airworthiness Directives; Eurocopter Deutschland GmbH Helicopters

Unsafe Condition

Debonding of the erosion protective shell (abrasion strip) on the leading edge of each main rotor blade, which could lead to an unbalanced main rotor, high vibrations, damage to the tail boom or tail rotor, and loss of control of the helicopter.

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

Required Actions

Inspect for debonding of the abrasion strip on the leading edge of each main rotor blade. If debonding is detected, replace the main rotor blade with an airworthy one before further flight.

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

Compliance Time

Within 50 flight hours time-in-service (TIS).

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

Affected Aircraft

Eurocopter Deutschland GmbH Model BO-105A, BO-105C, BO-105LS A-1, BO-105LS A-3, and BO-105S helicopters with main rotor blades part numbers 105-15103, 105-15141, 105-15141V001, 105-15143, 105-15150, 105-15150V001, 105-15152, 105-81013, 105-87214, 1120-15101, or 1120-15103, where the main rotor blade erosion protective shell was replaced between September 2006 and March 2010.

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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