Airworthiness directives › 2006-03-17
AD 2006-03-17 Airworthiness Directives; Polskie Zaklady Lotnicze Spolka zo.o. Model PZL M26 01 Airplanes
Applicability*9
(c) This AD affects Model PZL M26 01, serial numbers 1APP01-01 and 1AP002-01 through 1AP002-06, that are certificated in any category.
Required actions
(e) To address this problem, you must do the following: Actions Compliance Procedures (1) Inspect fuselage frame No. XI for any cracks Before further flight after February 24, 2006 (the effective date of this AD). Thereafter, repetitively inspect every 20 hours time-in-service (TIS) until you do the installation of reinforcement modifications for fuselage frame No. XI required by paragraph (e)(2)(ii) of this AD Follow Polskie Zaklady Lotnicze Sp. zo.o. Bulletin No. E/62.018/2005, dated November 30, 2005. (2) If you find any cracks in fuselage frame No. XI as a result of any inspection required by paragraph (e)(1) of this AD, you must: (i) Remove and replace any cracked fuselage frame No. XI; and (ii) Do the installation of reinforcement modifications for fuselage frame No. XI. Before further after the inspection required by paragraph (e)(1) of this AD. The installation of reinforcement modifications required by paragraph (e)(2)(ii) of this AD is the terminating action for the repetitive inspection requirements of paragraph (e)(1) of this AD Follow Polskie Zaklady Lotnicze Sp. zo.o. Bulletin No. E/62.018/2005, dated November 30, 2005. (3) Do not install any fuselage frame No. XI without also the reinforcement modifications required by paragraph (e)(2)(i) of this Ad As of February 24, 2006 (the effective date of this AD) Follow Polskie Zaklady Lotnicze Sp. zo.o. Bulletin No. E/62.018/2005, dated November 30, 2005.
Unsafe condition
(d) This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the European Aviation Safety Agency (EASA), the airworthiness authority, for the European Union. We are issuing this AD to detect and correct cracks in fuselage frame No. XI, which could result in failure of this frame. This failure could lead to the failure of the tail section 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