AD 2005-17-14

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes; Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model A300 C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes); and Model A310-200 and -300 Series Airplanes

AD Number
2005-17-14
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2005-20794
FR Citation
70 FR 50157

Applicability

TypeManufacturerModelDetails
aircraft Airbus A300 B2 and B4 Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes; Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model A300 C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes); and Model A310-200 and -300 Series Airplanes

Unsafe Condition

Desynchronization of one of the three rudder servo actuators, if combined with an engine failure, could result in the loss of the related hydraulic system and, potentially, loss of one of the two synchronized actuators. This condition could create additional fatigue loading and possible cracking on the attachment fittings and could result in the inability of the remaining synchronized actuator to maintain the commanded rudder deflection, which could result in reduced controllability of the airplane.

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

Required Actions

Perform new repetitive tests/inspections/analyses of the rudder servo actuators. Take related investigative/corrective actions if necessary. Reporting any discrepancy must be done in accordance with the applicable referenced Airbus service bulletin.

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

Compliance Time

Within the compliance times specified in the referenced Airbus service bulletin.

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

Affected Aircraft

Airbus Model A300 B2 and B4 Series Airplanes; Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model A300 C4-605R Variant F Airplanes (collectively called A300-600 Series Airplanes); and Model A310-200 and -300 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

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

View Official Source ↗ Find More ADs for Airbus A300 B2 and B4

Related Airworthiness Directives

2007-07-08 Recurring

final rule

Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes Equipped With General Electric CF6-50 Engines

Unsafe Condition: could result in reduced controllability of the airplane.

Effective: May 10, 2007 Category: aircraft

2007-04-11

final rule

Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes

Unsafe Condition: The FAA is superseding an existing airworthiness directive (AD), which applies to all Airbus Model A300 B2, B4-100, and B4-200 series airplanes. That AD currently requires supplemental structural i...

Effective: Apr 3, 2007 Category: aircraft

2006-26-10

final rule

Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes

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

Effective: Feb 21, 2007 Category: aircraft

2006-15-04 Recurring

final rule

Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes; and Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes)

Unsafe Condition: could result in reduced structural integrity of the fuselage, and consequent rapid decompression of the airplane.

Effective: Aug 24, 2006 Category: aircraft

View all Airbus ADs →