Airworthiness directives › 2006-03-16
AD 2006-03-16 Airworthiness Directives; Hamburger Flugzeugbau GmbH Model HFB 320 HANSA Airplanes
Models named: HFB 320 HANSA. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to all Hamburger Flugzeugbau GmbH Model HFB 320 HANSA airplanes, certificated in any category.
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. Airworthiness Limitations Revision (f) Within 30 days after the effective date of this AD: Revise the Limitations section of the HFB 320 Hansa Airplane Flight Manual (AFM) to state the following (or insert a copy of this AD into the Limitations section): “Do not operate the airplane beyond 15,000 total flight cycles, or 15,000 total flight hours, whichever occurs first.” (g) This limitation may be removed from the HFB 320 Hansa AFM after the Manager, International Branch, ANM-116, FAA, approves analysis that would substantiate continued safe operation beyond the designed life limit of 15,000 total flight cycles, or within 15,000 total flight hours on the airplane, whichever occurs first. Alternative Methods of Compliance (AMOCs) (h)(1) The Manager, International Branch, ANM-116, has the authority to approve AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19. (2) Before using any AMOC approved in accordance with § 39.19 on any airplane to which the AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate Holding District Office. Related Information (i) German airworthiness directive 2002-158, effective October 3, 2002, also addresses the subject of this AD. Material Incorporated by Reference (j) None. Issued in Renton, Washington, on January 31, 2006. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 06-1147 Filed 2-7-06; 8:45 am] BILLING CODE 4910-13-P
Unsafe condition
This AD results from a report that all airplanes in operation might have met or exceeded the designed life limit for the primary structure. We are issuing this AD to prevent continued operation of an airplane beyond its designed life limit for the primary structure, which could result in reduced structural integrity of the airplane.
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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