Airworthiness directives › 2015-02-13
AD 2015-02-13 Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (Embraer) Airplanes
Models named: EMB -135ER, -135KE, -135KL, -135LR, -145, -145ER, -145MR, -145LR, -145XR, -145MP. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to Empresa Brasileira de Aeronautica S.A. (Embraer) Model EMB -135ER, -135KE, -135KL, -135LR, -145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP airplanes, certificated in any category, all serial numbers.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
Within 60 days after the effective date of this AD: Revise the maintenance or inspection program, as applicable, by incorporating EMBRAER EMB145 Temporary Revision (TR) 15-3, dated August 26, 2013, to the Airworthiness Limitation Requirements of the EMBRAER EMB145 Maintenance Review Board Report MRB 145/1150; and EMBRAER EMB145 TR 15-4, dated August 26, 2013, to the Airworthiness Limitation Requirements of the EMBRAER EMB145 Maintenance Review Board Report MRB-145/1150; as applicable. (1) The compliance times depend on the airplane model, and the pre-modification and post-modification conditions specified in EMBRAER EMB145 TR 15-3, dated August 26, 2013, to the Airworthiness Limitation Requirements of the EMBRAER EMB145 Maintenance Review Board Report MRB 145/1150; and EMBRAER EMB145 TR 15-4, dated August 26, 2013, to the Airworthiness Limitation Requirements of the EMBRAER Maintenance Review Board Report MRB-145/1150; as applicable. (2) The initial compliance times for the tasks specified in EMBRAER EMB145 TR 15-3, dated August 26, 2013, to the Airworthiness Limitation Requirements of the EMBRAER EMB145 Maintenance Review Board Report MRB 145/1150; and EMBRAER EMB145 TR 15-4, dated August 26, 2013, to the Airworthiness Limitation Requirements of the EMBRAER Maintenance Review Board Report MRB-145/1150; as applicable; are at the applicable threshold compliance times specified in EMBRAER EMB145 TR 15-3, dated August 26, 2013; and EMBRAER EMB145 TR 15-4, dated August 26, 2013; or within 600 flight cycles after the effective date of this AD, whichever occurs later. For the purposes of this AD, the initial compliance times (identified as “Threshold” or “T” in the service information) are expressed in “total flight cycles.”
Unsafe condition
This AD was prompted by our determination of the need to revise the airplane airworthiness limitations to the pylons and fuselage. We are issuing this AD to prevent fatigue cracking of various structural elements, which could affect the structural integrity of the airplane.
Affected ADs
None.
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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