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Airworthiness directives › 2016-26-03

AD 2016-26-03 Airworthiness Directives; Airbus Defense and Space S.A. (Formerly Known as Construcciones Aeronauticas, S.A.) Airplanes

2017-02-08
2017-01-04
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Airframe
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Models named: CN-235, CN-235-100, CN-235-200, CN-235-300, C-295. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to Airbus Defense and Space S.A. (formerly known as Construcciones Aeronauticas, S.A.) Model CN-235, CN-235-100, CN-235-200, CN-235-300, and C-295 airplanes, certificated in any category, all manufacturer serial numbers.

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

This paragraph restates the requirements of paragraph (g) of AD 2013-23-02, with no changes. Within the times specified in paragraph (g)(1) or (g)(2) of this AD, as applicable: Perform a detailed visual inspection for damage (including, but not limited to, signs of electrical arcing and fuel leaks) of the electrical feeder cables of each fuel booster pump having part number (P/N) 1C12-34 or 1C12-46, in accordance with the instructions of Airbus Military All Operator Letter 235-025, dated July 29, 2013 (for Model CN-235 airplanes); or Airbus Military All Operator Letter 295-025, Revision 01, dated August 1, 2013 (for Model C-295 airplanes). (1) For each fuel booster pump that has not been replaced as of December 2, 2013 (the effective date of AD 2013-23-02): Prior to the accumulation of 300 total flight hours or within 5 flight cycles after December 2, 2013, whichever occurs later. (2) For each fuel booster pump that has been replaced as of December 2, 2013 (the effective date of AD 2013-23-02): Within 300 flight hours since the most recent fuel booster pump replacement, or within 5 flight cycles after December 2, 2013, whichever occurs later.

Unsafe condition

This AD was prompted by a report of an in-flight problem with the fuel transfer system. We are issuing this AD to prevent damage to certain fuel booster pumps, which could create an ignition source in the fuel tank vapor space, and result in a fuel tank explosion and consequent loss of the airplane.

Affected ADs

This AD replaces AD 2013-23-02, Amendment 39-17657 (78 FR 68688, November 15, 2013) (“AD 2013-23-02”).

Read the original on the Federal Register →

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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1