Airworthiness Directive · Amendment 39-15127 · Airbus Model A310 and A300-600 Series Airplanes
Airbus Model A310 and A300-600 Series Airplanes
Superseded. A later AD replaced this one: AD 2015-08-06. Comply with the one in force.
This AD applies to all Airbus Model A310 series airplanes and Model A300-600 series airplanes, certificated in any category.
Note 1: This AD requires revisions to certain operator maintenance documents to include new inspections. Compliance with these actions is required by 14 CFR 91.403(c). For airplanes that have been previously modified, altered, or repaired in the areas addressed by these inspections, the operator may not be able to accomplish the inspections described in the revisions. In this situation, to comply with 14 CFR 91.403(c), the operator must request approval for an alternative method of compliance according to paragraph (h) of this AD. The request should include a description of changes to the required inspections that will ensure the continued damage tolerance of the affected structure. The FAA has provided guidance for this determination in Advisory Circular (AC) 25.1529-1.
The FAA is adopting a new airworthiness directive (AD) for all Airbus Model A310 and A300-600 series airplanes. This AD requires revising the Airworthiness Limitations section of the Instructions for Continued Airworthiness by incorporating new and revised certification maintenance requirements. This AD results from the manufacturer determining that additional and revised certification maintenance requirements are necessary in order to ensure continued operational safety of the affected airplanes. We are issuing this AD to prevent safety-significant latent failures that would, in combination with one or more other specific failures or events, result in a hazardous or catastrophic failure condition of avionics, hydraulic systems, fire detection systems, fuel systems, or other critical systems.
You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done.
Within three months after the effective date of this AD, revise the Airworthiness Limitations section of the Instructions for Continued Airworthiness by incorporating Airbus A300-600 Certification Maintenance Requirements (CMRs) AI/ST5/829/85, Issue 12, dated February 2005 (for Model A300-600 series airplanes); or Airbus A310 CMR AI/ST5/849/85, Issue 12, dated February 2005 (for Model A310 series airplanes); as applicable. Accomplish the actions specified in the applicable CMRs at the intervals specified in the applicable CMRs, except as provided by paragraph (g) of this AD. Where the CMRs specify to contact the Direction Générale de l'Aviation Civile (DGAC), operators are required to contact the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, for such approvals. The actions must be accomplished in accordance with the applicable CMRs.
For tasks identified in MSI 78.30.00, “Thrust Reverser Actuation and Cowling,” of Section 2, “CMR ‘Two Star’ Tasks,” of Airbus A300-600 CMR AI/ST5/829/85, Issue 12, dated February 2005; and Airbus A310 CMR AI/ST5/849/85, Issue 12, dated February 2005: The initial compliance time is within 2,000 flight cycles or 12 months after the effective date of this AD, whichever occurs later. Thereafter, actions identified in MSI 78.30.00 must be accomplished within the repetitive interval specified in the applicable CMRs. Where the CMRs specify to contact the DGAC, operators are required to contact the Manager, International Branch, ANM-116, for such approvals. The actions must be accomplished in accordance with the applicable CMRs.
The aircraft, engines and makers this AD names, by the model designations in its text. A model listed here may still be outside the AD's serial ranges.
