Airworthiness directives › 2005-11-06
AD 2005-11-06 Airworthiness Directives; Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes
Makes named: pilatus. Models named: PC-12, PC-12/45. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
(c) This AD affects Models PC-12 and PC-12/45 airplanes, Manufacturers Serial Numbers (MSN) 101 through 620, that are certificated in any category.
Required actions
(e) To address this problem, you must do the following: Actions Compliance Procedures (1) Insert Temporary Revision No. 11 (Report No. 02211) or No. 40 (Report No. 01973-001) into the Limitations Section of the PC-12 Pilot's Operating Handbook (POH) Within the next 90 days after July 18, 2005 (the effective date of this AD), unless already done 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 modify the POH as specified in paragraph (e)(1) of this AD. Make an entry into 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) Replace the pitch actuator, part number (P/N) 985.92.03.161, with an improved design pitch actuator, P/N 985.92.03.164; and make the associated wiring and circuit breaker changes (as applicable) Within the next 18 months after July 18, 2005 (the effective date of this AD), unless already done Follow Pilatus PC12 Service Bulletin No. 22-004, dated December 21, 2004. (3) Remove the Temporary Revision to the POH specified in paragraph (e)(1) of this AD after the pitch actuator is replaced as required in paragraph (e)(2) of this AD Before further flight after the pitch actuator is replaced with an improved design pitch actuator 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 modify the POH as specified in paragraph (e)(3) of this AD. Make an entry into the aircraft records showing compliance with this portion of the AD following section 43.9 of the Federal Aviation Regulations (14 CFR 43.9). (4) Do not install a P/N 985.92.03.161 pitch actuator As of July 18, 2005 (the effective date of this AD) Not applicable.
Unsafe condition
(d) This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. The actions specified in this AD are intended to prevent an out-of-trim condition from occurring when the flaps are at a 40-degree flight phase and the pilot disconnects the autopilot. This condition could lead to reduced ability to control the airplane.
Affected ADs
(b) None.
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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