Airworthiness directives › 2007-10-15
AD 2007-10-15 Airworthiness Directives; Cessna Aircraft Company Models 208 and 208B Airplanes
Makes named: cessna. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to Models 208 and 208B, all serial numbers, that are certificated in any category.
Unsafe condition
This AD results from our determination that the revisions dated February 20, 2007, to the S1 Known Icing Equipment AFM supplement are necessary and should be incorporated into the Airplane Flight Manual (AFM)/Pilot's Operating Handbook (POH); and that a low airspeed awareness system should be required when operating in known icing conditions. We are issuing this AD to assure that the pilot has enough information and the necessary equipment to prevent loss of control of the airplane while in-flight during icing conditions. New Actions Required by this AD (e) Unless already done, within the next 90 days after the effective date of this AD, incorporate the applicable new S1 Known Icing Equipment AFM supplement, dated February 20, 2007, into the AFM/POH: Document Affects (1) Model 208 (675 SHP) FAA-approved Flight Manual Supplement S1 “Known Icing Equipment,” Cessna document D1352-S1-10, dated February 20, 2007, or later FAA-approved revision that incorporates the same information Cessna Model 208 airplanes with a Pratt & Whitney of Canada Ltd., PT6A-114A turboprop engine installed (675 SHP) or FAA-approved engine of equivalent or higher horsepower installed, equipped with airframe deicing pneumatic boots, that are not currently prohibited from flight in known or forecast icing (2) Model 208 (600 SHP) FAA-approved Flight Manual Supplement S1 “Known Icing Equipment,” Cessna document D1307-S1-09, dated February 20, 2007, or later FAA-approved revision that incorporates the same information Cessna Model 208 airplanes with a Pratt & Whitney of Canada Ltd., PT6A-114 turboprop engine installed (600 SHP) or FAA-approved engine of equivalent horsepower installed, equipped with airframe deicing pneumatic boots, that are not currently prohibited from flight in known or forecast icing. (3) Model 208B (675 SHP) FAA-approved Flight Manual Supplement S1 “Known Icing Equipment,” Cessna document D1329-S1-10, dated February 20, 2007, or later FAA-approved revision that incorporates the same information Cessna Model 208B airplanes with a Pratt & Whitney of Canada Ltd., PT6A-114A turboprop engine installed (675 SHP) or FAA-approved engine of equivalent or higher horsepower installed, equipped with airframe deicing pneumatic boots, that are not currently prohibited from flight in known or forecast icing. (4) Model 208B (600 SHP) FAA-approved Flight Manual Supplement S1 “Known Icing Equipment,” Cessna document D1309-S1-10, dated February 20, 2007, or later FAA-approved revision that incorporates the same information Cessna Model 208B airplanes with a Pratt & Whitney of Canada Ltd., PT6A-114 turboprop engine installed (600 SHP) or FAA-approved engine of equivalent horsepower installed, equipped with airframe deicing pneumatic boots, that are not currently prohibited from flight in known or forecast icing. Note: The above supplements require the installation of a functional low airspeed awareness system. Cessna Service Bulletin CAB06-11 and Service Kit SK 208-171, both dated October 9, 2006, provide instructions for such an installation. (f) 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 insert the information into the POH specified in all paragraphs (e)(1) through (e)(4) of this AD. Make an entry into the aircraft records showing compliance with this portion of the AD in accordance with section 43.9 of the Federal Aviation Regulations (14 CFR 43.9). Actions Retained From AD 2006-06-06 (g) The actions in paragraphs (h) and (i) of this AD below are retained in this AD from AD 2006-06-06. The new actions required by this AD in paragraph (e) above terminate the requirement for the actions in paragraphs (h) and (i) of this AD. (h) No later than March 27, 2006 (3 days after March 24, 2006, which is the effective date of AD 2006-06-06), incorporate the following revisions into the Airplane Flight Manual (AFM), unless already done: Affected airplanes Incorp
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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