AD 2011-12-04

final rule
Data completeness: 70%

Airworthiness Directives; BRP-Powertrain GmbH & Co. KG Rotax 912 F3, 912 S2, 912 S3, 912 S4, 914 F2, 914 F3, and 914 F4 Reciprocating Engines

AD Number
2011-12-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2011-0456
FR Citation
76 FR 33984

Applicability

TypeManufacturerModelDetails
aircraft Aviat Various Airworthiness Directives; BRP-Powertrain GmbH & Co. KG Rotax 912 F3, 912 S2, 912 S3, 912 S4, 914 F2, 914 F3, and 914 F4 Reciprocating Engines
engine Rotax 912 F3 Airworthiness Directives; BRP-Powertrain GmbH & Co. KG Rotax 912 F3, 912 S2, 912 S3, 912 S4, 914 F2, 914 F3, and 914 F4 Reciprocating Engines

Unsafe Condition

Deviation in hardening of certain Part Number (P/N) 944072 washers exceeds the hardness of the design specification, affecting the magneto ring flywheel hub installation.

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

Required Actions

Replace the washer securing the magneto ring flywheel hub with a new washer of the same part number.

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

Compliance Time

Within 10 flight hours or at next maintenance after the effective date of the AD, whichever occurs first.

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

Affected Aircraft

BRP-Powertrain GmbH & Co. KG Rotax 912 F3, 912 S2, 912 S3, 912 S4, 914 F2, 914 F3, and 914 F4 reciprocating engines, with specific serial number ranges.

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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