AD 2013-10-05

final rule
Data completeness: 70%

Airworthiness Directives; Eurocopter Deutschland GmbH Helicopters

AD Number
2013-10-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2013-0445
FR Citation
78 FR 31394

Applicability

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

Unsafe Condition

A short circuit on the yaw Smart Electro-Mechanical Actuator (SEMA) 'ACTIV' input to ground can lead to the seizure of all SEMA units. Combined with an inoperative Autotrim in Pitch or Roll, or combined with an inoperative Autotrim in Cyclic and Yaw axis, this could significantly reduce the pilot's reaction time to stabilize the helicopter, resulting in possible loss of helicopter control.

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

Required Actions

Insert a statement into the operating limitations section of the MBB-BK 117C-2 Rotorcraft Flight Manual prohibiting operation under IFR or Night VFR with the autotrim inoperative in pitch or roll, or combined inoperative autotrim in cyclic and yaw axis.

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 30 days, whichever comes first.

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

Affected Aircraft

Eurocopter Deutschland GmbH Model MBB-BK 117 C-2 helicopters, certificated in any category.

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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