AD 2014-19-01

final rule
Data completeness: 80%

Airworthiness Directives; Embraer S.A. Airplanes

AD Number
2014-19-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2014-0390
FR Citation
79 FR 55604

Applicability

TypeManufacturerModelDetails
aircraft Embraer S Airworthiness Directives; Embraer S.A. Airplanes
aircraft Aviat Various Airworthiness Directives; Embraer S.A. Airplanes

Unsafe Condition

Cracks beyond acceptable limits in the carbon discs of the left hand (LH) and right hand (RH) brake assemblies.

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

Required Actions

Inspect for cracks in the stator pressure plate on both LH and RH brake assemblies following Embraer Phenom Service Bulletin No. 505-32-0011, Revision 01. Repair or replace as necessary.

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

Compliance Time

Within 50 flight hours after the effective date of this AD.

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

Affected Aircraft

Embraer S.A. Model EMB-505 airplanes, all serial numbers, equipped with part number DAP00097-01 or DAP00097-02 brake assembly, 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 4, 2026

Rights: U.S. Government Public Domain

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