AD 2005-13-33

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes

AD Number
2005-13-33
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2005-20861
FR Citation
70 FR 36833

Applicability

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

Unsafe Condition

Reports of pitch trim disconnect caused by insufficient length in the wiring to the pitch torque limiter lever.

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

Required Actions

Modify the wiring of the autopilot pitch torque limiter switch by performing all applicable actions specified in Airbus Service Bulletin A300-22-0117.

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

Compliance Time

Within 20 months after the effective date of this AD.

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

Affected Aircraft

Airbus Model A300 B2-1A, B2-1C, B2K-3C, B2-203, B4-2C, B4-103, and B4-203 airplanes, certificated in any category, as identified in Airbus Service Bulletin A300-22-0117.

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.