Airworthiness directives › 2004-23-17
AD 2004-23-17 Airworthiness Directives; Mooney Airplane Company, Inc., Model M20M Airplanes
Makes named: mooney. Models named: M20M. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
(c) This AD affects Model M20M airplanes, serial numbers 27-0001 through 27-0321, that are certificated in any category.
Required actions
(e) To address this problem, you must do the following: Actions Compliance Procedures (1) Remove the existing radiant heat shield, part number (P/N) 600182-501 (A), and replace with the new radiant heat shield, P/N 600182-501 (B), and install the new heat shield deflector, P/N 600505-001. Remove the existing V-band clamp, P/N 55677-340M or 40D21162-340M, and install the new V-band clamp, P/N NH1009399-10 or 40D23255-340M Within 10 hours time-in-service (TIS) after December 1, 2004 (the effective date of this AD), unless already done. If you have already incorporated all parts of Mooney Airplane Company, Inc. Service bulletin M20-283, dated January 3, 2004, then you only have to replace the tailpipe V-band clamp with the new configuration V-band clamp, P/N NH109399-10 or 40D23255-340M Follow Mooney Airplane Company, Inc. Service Bulletin M20-283A, dated March 30, 2004. (2) Modify the hydraulic brake fluid poly line Within 10 hours TIS after December 1, 2004 (the effective date of this AD), unless already done. If you have already incorporated all parts of Mooney Airplane Company, Inc. Service Bulletin M20-283, dated January 3, 2004, then you only have to replace the tailpipe V-band clamp with the new configuration V-band clamp, P/N NH109399-10 or 40D23255-340M Follow Mooney Airplane Company, Inc. Service Bulletin M20-283A, dated March 30, 2004.
Unsafe condition
(d) This AD is the result of an in-flight cockpit fire. We are issuing this AD to prevent the V-clamp from detaching from the turbocharger and to prevent exposure of the firewall to hot exhaust gases, which could result in an in-flight fire. An in-flight fire could lead to loss of control of the airplane and passenger injury.
Read the original on the Federal Register →
You just looked this one up by hand
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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