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Airworthiness directives › 2005-02-01

AD 2005-02-01 Airworthiness Directives; The Lancair Company Models LC40-550FG and LC42-550FG Airplanes

2005-01-21
2005-01-19
39-13945
FAA-2005-20048
Airframe
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Applicability*9

(c) This AD affects the following airplane models and serial numbers that are certificated in any category:   Model Serial Nos. LC40-550FG 40004 through 40079. LC42-550FG 42002 through 42062.

Required actions

(e) To address this problem, you must do the following:   Actions Compliance Procedures (1) To address the unsafe condition, do the following: (i) Using pen and ink, make the following notation in the takeoff distance chart (Figure 5-7) in Section 5 of the FAA-approved Airplane Flight Manual (AFM): “Caution: See Service Bulletin SB-05-001 for takeoff performance correction.” (ii) Insert a copy of Lancair Mandatory Service Bulletin SB-05-001, dated January 4, 2005, into Section 5 of the FAA-approved AFM. Before further flight after January 21, 2005 (the effective date of this AD) The owner/operator holding at least a private pilot certificate as authorized by section 43.7 of the Federal Aviation Regulations (14 CFR 43.7) may do the flight manual changes requirement of this AD. Make an entry in the aircraft records showing compliance with this portion of the AD following section 43.9 of the Federal Aviation Regulations (14 CFR 43.9). (2) Lancair will include this information into the next revision of the FAA-approved AFM. Incorporation of the revision that includes this information into Section 5 of the FAA-approved AFM is considered terminating action for paragraphs (e)(1)(i) and (e)(1)(ii) of this AD At any time as terminating action The owner/operator holding at least a private pilot certificate as authorized by section 43.7 of the Federal Aviation Regulations (14 CFR 43.7) may do the flight manual changes requirement of this AD. Make an entry in the aircraft records showing compliance with this portion of the AD following section 43.9 of the Federal Aviation Regulations (14 CFR 43.9).

Unsafe condition

(d) This AD results from flight testing that revealed that the takeoff distance values for the affected airplanes could not be duplicated. We are issuing this AD to prevent potential impact with terrain or obstruction during takeoff due to incorrect takeoff distance values.

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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