AD 2006-25-03

final rule
Data completeness: 80%

Airworthiness Directives; Airbus Model A300 Airplanes

AD Number
2006-25-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2006-25634
FR Citation
71 FR 70862

Applicability

TypeManufacturerModelDetails
aircraft Airbus A300 Airworthiness Directives; Airbus Model A300 Airplanes
aircraft Aviat Various Airworthiness Directives; Airbus Model A300 Airplanes

Unsafe Condition

Failure of pitch trim system 2 to deflect the trimmable horizontal stabilizer at maximum rate, which could result in loss of high-speed trim and consequent reduced controllability of the airplane.

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

Required Actions

Inspect and test pitch trim system 2 to ensure its availability and capability to deflect the trimmable horizontal stabilizer at high speed of trim. Revise the maintenance program to include periodic testing of pitch trim system 2.

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

Compliance Time

Before further flight

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

Affected Aircraft

Airbus Model A300 airplanes, except for Model A300 B4-203 and A300 B2-203 in the forward facing crew cockpit (FFCC) configuration. Model A300-600 series airplanes are not affected.

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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