Division Cessna 208 Series Aeroplanes - AD/CESSNA 208/21 Amdt 1 - Low Airspeed Awareness System - Cessna 208 Series Aeroplanes

Cessna 208 Series Aeroplanes

AD/CESSNA 208/21 Amdt 1	Low Airspeed Awareness System	8/2007 DM

<table cellspacing="0" cellpadding="0" style="width:510.3pt; margin-top:0pt; margin-bottom:0pt; border-collapse:collapse"><tbody><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Applicability:</span></p></td><td colspan="2" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Model 208 and 208B aeroplanes, equipped with the optional Cessna ‘flight into known icing equipment package’.</span></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Requirement:</span></p></td><td colspan="2" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p class="Note" style="margin-left:21.3pt; text-indent:-21.3pt"><span style="font-style:normal">1.</span><span style="width:12.3pt; text-indent:0pt; display:inline-block"> </span><span style="font-style:normal">Incorporate the following new S1 ‘Known Icing Equipment’ Aircraft Flight Manual (AFM) supplement into the applicable AFM/Pilot’s Operating Handbook (POH):</span></p></td></tr><tr style="height:5.1pt"><td rowspan="4" style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span></span></p></td><td style="width:201.9pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="text-align:center"><span style="font-weight:bold">AFM/POH Supplement</span></p></td><td style="width:201.95pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="text-align:center"><span style="font-weight:bold">Affected Aeroplane</span></p></td></tr><tr style="height:5.1pt"><td style="width:201.9pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Model 208 (675 SHP) FAA-approved Flight Manual Supplement S1 “Known Icing Equipment,” Cessna document D1352-S1-10, dated 20 February 2007, or later FAA-approved revision that incorporates the same information.</span></p></td><td style="width:201.95pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Model 208 aeroplanes with a Pratt &amp; Whitney of Canada Ltd (PWC),</span><br><span>PT6A-114A turboprop engine installed (675 SHP) or FAA-approved engine of equivalent or higher horsepower installed, equipped with airframe de-icing pneumatic boots, which are not currently prohibited from flight in known or forecast icing.</span></p></td></tr><tr style="height:5.1pt"><td style="width:201.9pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Model 208 (600 SHP) FAA-approved Flight Manual Supplement S1 “Known Icing Equipment,” Cessna document D1307-S1-09, dated 20 February 2007, or later FAA-approved revision that incorporates the same information.</span></p></td><td style="width:201.95pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Model 208 aeroplanes with a PWC PT6A-114 turboprop engine installed (600 SHP) or FAA-approved engine of equivalent horsepower installed, equipped with airframe de-icing pneumatic boots, which are not currently prohibited from flight in known or forecast icing.</span></p></td></tr><tr style="height:5.1pt"><td style="width:201.9pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Model 208B (675 SHP) FAA-approved Flight Manual Supplement S1 “Known Icing Equipment,” Cessna document D1329-S1-10, dated 20 February 2007, or later FAA-approved revision that incorporates the same information.</span></p></td><td style="width:201.95pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Model 208B aeroplanes with a PWC PT6A-114A turboprop engine installed (675 SHP) or FAA-approved engine of equivalent or higher horsepower installed, equipped with airframe de-icing pneumatic boots, which are not currently prohibited from flight in known or forecast icing.</span></p></td></tr></tbody></table>

	The original issue of this Directive was issued to assure that the pilot has enough information and the necessary equipment to prevent loss of control of the aeroplane while flying in icing conditions. This Amendment continues that action.
	This Amendment is issued to clarify the applicability of the original issue following advice from the FAA. The Amendment limits the applicability to aeroplanes equipped with the optional Cessna flight into known icing equipment package and removes the requirement to install a LSA system, noting that the LSA system must be installed when the AFM Supplement S1 is incorporated in the AFM/POH.
	AD/CESSNA 208/20 Amdt 1 will be cancelled once the compliance period of this Directive has passed.
	The original issue of this Directive became effective on 5 July 2007.

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