AD 2006-26-10

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes

AD Number
2006-26-10
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2006-25670
FR Citation
72 FR 1928

Applicability

TypeManufacturerModelDetails
aircraft Airbus A300 B2 and B4 Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes

Unsafe Condition

Failure of the servomotors of the pitch trim systems could result in uncommanded nose-up movement of the control surface of the pitch trim systems after disengagement of the autopilot in cruise.

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

Required Actions

Revise the airplane flight manual (AFM) to include procedures for resetting the trim and pitch trim levers after each landing. Determine which servomotor moves the pitch trim control wheel. Perform applicable other specified actions.

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

Airbus Model A300 B2 and B4 series 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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