Airworthiness directives › 2005-13-10
AD 2005-13-10 Airworthiness Directives; Cessna Aircraft Company Models 172R, 172S, 182T, T182T, 206H, and T206H Airplanes
Makes named: cessna. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
(c) This AD affects the following airplane models and serial numbers that are certificated in any category: Model Serial Nos. 172R 17281186 through 17281232. 172S 172S9476 through 172S9689, and 172S9691 through 172S9770. 182T 18281242 through 18281502, 18281506, and 18281507. T182T T18208212 through T18208357. 206H 20608195 through 20608223, 20608225, and 20608226. T206H T20608410 through T20608475, T20608477 through T20608501, T20608503, and T20608506.
Required actions
(e) To address this problem, you must do the following: Actions Compliance Procedures (1) Inspect any MC01-3A I.C. 9 (part number (P/N) S3100-297) or MC01-3A I.C. 10 (P/N S3100-344) main electrical power junction box for any incorrect amperage (amp) circuit beaker installed in place of the required 40-amp circuit breakers Within the next 30 days after August 9, 2005 (the effective dated date of this AD), unless already done Follow Cessna Service Bulletin No. SB05-24-01, January 31, 2005. (2) Replace any incorrect amp circuit breaker with the required 40-amp circuit breaker Before further flight after the inspection required by paragraph (e)(1) of this AD Follow Cessna Service Bulletin No. SB05-24-01, dated January 31, 2005. (3) Only install in any MC01-3A I.C. 9 (P/N S3100-297) or MC01-3A I.C. 10 (P/N S3100-344) main electrical power junction box the required 40-amp circuit breakers As of August 9, 2005 (the effective date of this AD) Not Applicable.
Unsafe condition
(d) This AD is the result of several reports of circuit breakers that are not the correct 40-amp circuit breaker installed in the MC01-3A I.C. 9 or MC01-3A I.C. 10 main electrical power junction box. The actions specified in this AD are intended to replace any incorrect circuit breaker installed in the MC01-3A main electrical power junction box, which could result in premature tripping of the power junction box main feeder circuit breakers and could lead to partial or complete loss of all electrical power on the airplane. This condition could lead to the loss of all navigation and communication equipment and lighting in the cockpit.
Affected ADs
(b) None.
Read the original on the Federal Register →
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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