Airworthiness Directive · Amendment 39-19388 · Horizontal stabilizer
Airbus Defense and Space S.A. (Formerly Known as Construcciones Aeronauticas, S.A.) Airplanes
Superseded. A later AD replaced this one: AD 2024-24-04. Comply with the one in force.
This AD applies to Airbus Defense and Space S.A. Model airplanes, certificated in any category, specified in paragraphs (c)(1) and (c)(2) of this AD.
(1) Model CN-235, CN-235-100, CN-235-200, and CN-235-300 airplanes, all manufacturer serial numbers (MSN).
(2) Model C-295 airplanes, MSN 001 through 148 inclusive.
We are adopting a new airworthiness directive (AD) for all Airbus Defense and Space S.A. Model CN-235, CN-235-100, CN-235-200, and CN-235-300 airplanes; and certain Model C-295 airplanes. This AD was prompted by a report that cracks were found on the stabilizer-to- fuselage rear attachment fitting. This AD requires a detailed inspection of the upper and lower lugs of each horizontal stabilizer- to-fuselage rear attachment fitting, repair if necessary, and a report of findings. We are issuing this AD to address the unsafe condition on these products.
Within the compliance times specified in figure 1 or figure 2 to paragraph (g) of this AD, as applicable, accomplish a detailed inspection for cracks or rework of the upper and lower lugs of each horizontal stabilizer-to-fuselage rear attachment fitting (left- and right-hand sides), in accordance with the instructions of Airbus Defence and Space Alert Operators Transmission (AOT) AOT-CN235-55-0004, Revision 1, dated October 24, 2016; or Airbus Defence and Space AOT AOT-C295-55-0005, Revision 1, dated October 24, 2016; as applicable.
If, during the detailed inspection required by paragraph (g) of this AD, any discrepancy (i.e., cracking or rework) is detected, as specified in Airbus Defence and Space AOT AOT-CN235-55-0004, Revision 1, dated October 24, 2016; or Airbus Defence and Space AOT AOT-C295-55-0005, Revision 1, dated October 24, 2016; as applicable: Before further flight, contact the Manager, International Section, Transport Standards Branch, FAA; or the European Aviation Safety Agency (EASA); or Airbus Defense and Space S.A.'s EASA Design Organization Approval (DOA), for approved repair instructions. If approved by the DOA, the approval must include the DOA-authorized signature. Accomplish the repair accordingly within the compliance time specified in those instructions, including any repetitive post-repair inspections, if applicable.
Submit a one-time report of the findings (both positive and negative) of the inspection required by paragraph (g) of this AD to Airbus Defense and Space S.A., in accordance with Airbus Defence and Space AOT AOT-CN235-55-0004, Revision 1, dated October 24, 2016; or Airbus Defence and Space AOT AOT-C295-55-0005, Revision 1, dated October 24, 2016; as applicable; at the applicable time specified in paragraph (i)(1) or (i)(2) of this AD.
(1) If the inspection was done on or after the effective date of this AD: Submit the report within 60 days after the inspection.
(2) If the inspection was done before the effective date of this AD: Submit the report within 60 days after the effective date of this AD.
As of the effective date of this AD, no person may install, on any airplane, a horizontal stabilizer-to-fuselage rear attachment fitting, unless the part is new or it has been inspected in accordance with the instructions of Airbus Defence and Space AOT AOT-CN235-55-0004, Revision 1, dated October 24, 2016; or Airbus Defence and Space AOT AOT-C295-55-0005, Revision 1, dated October 24, 2016; as applicable; and no discrepancy was found. Before installation of the horizontal stabilizer-to-fuselage rear attachment fitting, contact the Manager, International Section, Transport Standards Branch, FAA; or the EASA; or Airbus Defense and Space S.A.'s EASA DOA, for approved instructions and do those instructions accordingly. If approved by the DOA, the approval must include the DOA-authorized signature.
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.
