Airworthiness directives › 2011-19-01
AD 2011-19-01 Airworthiness Directives; Airbus Airplanes
Applicability*9
This AD applies to Airbus Model A318-111, A318-112, A318-121, A318-122, A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-111, A320-211, A320-212, A320-214, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231, and A321-232 airplanes; certificated in any category; all manufacturer serial numbers.
Compliance
You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done.
Required actions
This paragraph restates the requirements of paragraph (g) of AD 2011-19-01, Amendment 39-16806 (76 FR 56279, September 13, 2011). For Airbus Model A319-131, -132, and -133, A320-231, -232, and -233, and A321-131 and -231 series airplanes, except those airplanes on which Airbus Modification 32943 has been incorporated in production: Within 10 days after August 13, 2004 (the effective date of AD 2004-15-14, Amendment 39-13748 (69 FR 45243, July 29, 2004)), revise the Limitations section of the Airbus A318/319/320/321 AFM to include the information in Temporary Revision (TR) 4.02.00/20, dated May 3, 2004. This may be done by inserting a copy of this TR into the AFM. When this TR has been included in general revisions of the AFM, those general revisions may be inserted into this AFM, provided the relevant information in the general revisions is identical to that in this TR. Accomplishing the actions required by paragraph (j) of this AD terminates the requirements of this paragraph.
Unsafe condition
This AD was prompted by reports of transient loss of certain systems and the potential for an inadvertent error by flightcrew to use the IDG switch instead of the GEN switch when doing a certain airplane flight manual (AFM) display unit failure procedure. We are issuing this AD to prevent transient loss of certain systems, which could result in the reduced ability of the flightcrew to cope with adverse flight conditions.
Affected ADs
This AD revises AD 2011-19-01, Amendment 39-16806 (76 FR 56279, September 13, 2011).
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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