AD 2012-15-03

final rule
Data completeness: 70%

Airworthiness Directives; Embraer S.A. Airplanes

AD Number
2012-15-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2011-1251
FR Citation
77 FR 44437

Applicability

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

Unsafe Condition

Damage on the rod end of the retracting actuator rod of the main landing gear (MLG), which may result in MLG extension with no hydraulic damping and consequent damage to the locking mechanism and collapse of the MLG.

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

Required Actions

Perform a one-time general visual inspection to determine if a certain part number is installed on the MLG retraction actuator. If necessary, perform a general visual inspection for discrepancies (such as cracks, damage, and movement) between the actuator rod end and shock strut lug of the MLG retraction actuator. If any discrepancy is found, replace the MLG retraction actuator, and as applicable, replace the anti-rotation pin and the attachment bolt with a new pin and bolt. Replace the actuator with a new actuator having a certain part number, and modify the attachment points.

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

Compliance Time

Before further flight

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Affected Aircraft

Embraer S.A. Model ERJ 190-100 STD, -100 LR, -100 ECJ, and -100 IGW airplanes.

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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