AD 2001-02-51

final rule
Data completeness: 70%

Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-145 and EMB-135 Series Airplanes

AD Number
2001-02-51
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-NM-16-AD
FR Citation
66 FR 8756

Applicability

TypeManufacturerModelDetails
aircraft Embraer EMB- 145 and EMB-135 Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-145 and EMB-135 Series Airplanes

Unsafe Condition

The actuator for the horizontal stabilizer is inadequate, potentially causing the horizontal stabilizer to fail to move in response to a pitch trim command from the flight crew after takeoff and during the climb phase. This could result in high pitch control forces and possible loss of control of the airplane.

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

Required Actions

Revise the FAA-approved Airplane Flight Manual (AFM) to include a maximum airspeed limitation for airplane retrimming after takeoff and during the climb phase. Install placards to alert the flight crew to this maximum speed.

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

Compliance Time

Within 3 days after the effective date of this AD.

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

Affected Aircraft

Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-145 and EMB-135 series airplanes, certificated in any category, with serial numbers listed in the AD.

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.