[{"data":1,"prerenderedAt":-1},["ShallowReactive",2],{"detail-sidebar-cat-0-en-105":3,"doc-seo-651061-105":59,"doc-detail-651061-en":131},{"code":4,"msg":5,"data":6},0,"success",[7,13,18,23,28,33,38,43,48,51,55],{"id":8,"doc_module":4,"doc_module_name":9,"category_name":10,"show_sort_weight":11,"slug":12},1,"Document","Story & Novel",90,"story-novel",{"id":14,"doc_module":4,"doc_module_name":9,"category_name":15,"show_sort_weight":16,"slug":17},2,"Literature",80,"literature",{"id":19,"doc_module":4,"doc_module_name":9,"category_name":20,"show_sort_weight":21,"slug":22},4,"Exam",70,"exam",{"id":24,"doc_module":4,"doc_module_name":9,"category_name":25,"show_sort_weight":26,"slug":27},5,"Comic",60,"comic",{"id":29,"doc_module":4,"doc_module_name":9,"category_name":30,"show_sort_weight":31,"slug":32},6,"Technology",50,"technology",{"id":34,"doc_module":4,"doc_module_name":9,"category_name":35,"show_sort_weight":36,"slug":37},7,"Healthcare",40,"healthcare",{"id":39,"doc_module":4,"doc_module_name":9,"category_name":40,"show_sort_weight":41,"slug":42},8,"Research & Report",30,"research-report",{"id":44,"doc_module":4,"doc_module_name":9,"category_name":45,"show_sort_weight":46,"slug":47},9,"Religion & Spirituality",20,"religion-spirituality",{"id":46,"doc_module":4,"doc_module_name":9,"category_name":49,"show_sort_weight":46,"slug":50},"World Cup","world-cup",{"id":52,"doc_module":4,"doc_module_name":9,"category_name":53,"show_sort_weight":52,"slug":54},10,"Lifestyle","lifestyle",{"id":56,"doc_module":4,"doc_module_name":9,"category_name":57,"show_sort_weight":24,"slug":58},19,"General","general",{"code":4,"msg":60,"data":61},"ok",{"site_id":62,"language":63,"slug":64,"title":65,"keywords":66,"description":67,"schema_data":68,"social_meta":124,"head_meta":126,"extra_data":128,"updated_unix":130},105,"en","cirrus-design-section-9-tks-anti-ice-system-poh-supplement","Cirrus Design Section 9 - TKS Anti-Ice System - POH Supplement","","POH Supplement for the Cirrus Design SR22 / SR22T TKS Anti-Ice System provides FAA-approved operating guidance for flight into known icing (FIKI) with defined tank capacity and anti-ice installation applicability. It specifies limitations and required operating procedures, including immediate exit from icing upon first anti-ice malfunction, prohibitions for freezing rain/freezing drizzle, and airspeed, weight, and takeoff restrictions. It also outlines environmental detection cues, minimum operating temperature, system temperature limits, and performance references to Section 5.",{"@graph":69,"@context":123},[70,84,106],{"@type":71,"itemListElement":72},"BreadcrumbList",[73,77,79,82],{"item":74,"name":75,"@type":76,"position":8},"https://docshare.wps.com","Home","ListItem",{"item":78,"name":9,"@type":76,"position":14},"https://docshare.wps.com/document/",{"item":80,"name":35,"@type":76,"position":81},"https://docshare.wps.com/document/healthcare/",3,{"item":83,"name":65,"@type":76,"position":19},"https://docshare.wps.com/document/cirrus-design-section-9-tks-anti-ice-system-poh-supplement/651061/",{"url":83,"name":65,"@type":85,"image":86,"author":91,"headline":65,"publisher":94,"fileFormat":97,"inLanguage":63,"description":67,"dateModified":98,"datePublished":99,"encodingFormat":97,"isAccessibleForFree":100,"interactionStatistic":101},"DigitalDocument",{"url":87,"@type":88,"width":89,"height":90},"https://docshare.wps.com/thumbnails/cirrus-design-section-9-tks-anti-ice-system-poh-supplement/651061.png","ImageObject",300,407,{"name":92,"@type":93},"Damian","Person",{"url":74,"name":95,"@type":96},"DocShare","Organization","application/pdf","2026-11-13","2026-10-24",true,{"@type":102,"interactionType":103,"userInteractionCount":105},"InteractionCounter",{"@type":104},"ViewAction",18,{"@type":107,"mainEntity":108},"FAQPage",[109,115,119],{"name":110,"@type":111,"acceptedAnswer":112},"What does this POH Supplement apply to when the TKS Anti-Ice System is installed?","Question",{"text":113,"@type":114},"When the TKS Anti-Ice System is installed on the aircraft, this POH Supplement is applicable and must be inserted into the Supplements Section of the Pilot’s Operating Handbook. The supplement adds to, supersedes, or deletes information in the basic POH.","Answer",{"name":116,"@type":111,"acceptedAnswer":117},"What must the pilot do at the first sign of an anti-ice system malfunction?",{"text":118,"@type":114},"The aircraft must immediately exit icing conditions when the first sign of an Anti-Ice System malfunction occurs.",{"name":120,"@type":111,"acceptedAnswer":121},"Which icing-related weather conditions are prohibited or must be avoided?",{"text":122,"@type":114},"Flight into freezing rain or freezing drizzle is prohibited. Tests and defined known icing conditions do not include freezing rain, freezing drizzle, mixed conditions, or severe icing; flight in these conditions must be avoided.","https://schema.org",{"og:url":83,"og:type":125,"og:title":65,"og:site_name":95,"og:description":67},"article",{"robots":127,"canonical":83},"index,follow",{"doc_id":129,"site_id":62},651061,1792900347,{"code":4,"msg":5,"data":132},{"doc_id":129,"user_id":133,"nickname":92,"user_avatar":134,"doc_module":4,"category_id":34,"category_name":35,"doc_title":65,"doc_description":67,"doc_content":135,"file_id":136,"file_url":137,"file_type":138,"file_size":139,"view_count":105,"is_deleted":4,"is_public":8,"is_downloadable":8,"audit_status":8,"page_count":140,"language":141,"language_code":63,"site_id":62,"html_lang":63,"table_of_contents":142,"faqs":143,"seo_title":144,"seo_description":67,"update_tm":145,"read_time":146,"preview_page_count":4},137451208677,"https://ap-avatar.wpscdn.com/davatar_155a257f0dc6eb9ab79c44ca47cae57d","Cirrus Design Section 9  \nSR22 / SR22T Supplements  \nPilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement  \nfor the  \nTKS Anti-Ice System  \n• Approved for Flight Into Known Icing (FIKI)  \n• 8.0 gallon usable capacity.  \n• 4.0 gallon tank in each wing.  \nWhen the TKS Anti-Ice System is installed on the aircraft, this POH Supplement is applicable and must be inserted in the Supplements Section of the Pilot’s Operating Handbook. This document must be carried in the airplane at all times. Information in this supplement adds to, supersedes, or deletes information in the basic Pilot’s Operating Handbook  \n• Note •  \nThis POH Supplement Change, dated Revision 05: 09-20-12, supersedes and replaces the Revision 04 release of this POH Supplement dated 12-17-10.  \nP/N 13772-134 1 of 48  \nRevision 05: 09-20-12  \nSection 9 Cirrus Design  \nSupplements SR22 / SR22T  \nSection 1-General  \nThis system, when compliant with the Kinds of Operation Equipment List and Minimum Dispatch Fluid Quantity, allows flight in icing conditions as defined by Title 14 of the Code of Federal Regulations (CFR) Part 25, Appendix C-Envelopes for Continuous Maximum and Intermittent Maximum Icing.  \nSection 2-Limitations  \nIn icing conditions the airplane must be operated as described in the operating procedures section of this manual. Where specific operational speeds and performance information have been established for such conditions, this information must be used.  \nAt the first sign of Anti-Ice System malfunction, the aircraft must immediately exit icing conditions.  \nEnvironmental Conditions  \nFlight into freezing rain or freezing drizzle is prohibited.  \nKnown icing conditions are defined by FAR Part 25, Appendix C. These conditions do not include, nor were tests conducted in all icing conditions that may be encountered such as freezing rain, freezing drizzle, mixed conditions or conditions defined as severe. Flight in these conditions must be avoided. Some icing conditions not defined in FAR Part 25 have the potential of producing hazardous ice accumulations, which exceed the capabilities of the airplane’s Anti-Ice System, and/or create unacceptable airplane performance including loss of control.  \nInadvertent operation in freezing rain, freezing drizzle, mixed conditions, or conditions defined as severe may be detected by:  \n• Visible rain at temperatures below 41°F (5°C) OAT.  \n• Droplets that splash or splatter on impact at temperatures below below 41°F (5°C) OAT.  \n• Ice on or behind the wing or horizontal tail panels that cannot be removed with Anti-Ice System HIGH flow.  \n• Unusually extensive ice accreted on the airframe in areas not normally observed to collect ice.  \n2 of 48 P/N 13772-134 Revision 05: 09-20-12  \nCirrus Design Section 9  \nSR22 / SR22T Supplements  \n• Accumulation of ice on the upper surface or lower surface of the wing aft of the protected area.  \n• Accumulation of ice on the propeller spinner farther back than normally observed.  \nIf the airplane encounters conditions that are determined to contain freezing rain, freezing drizzle, or severe icing, immediately exit condition by changing altitude, turning back, or if clear air is known tobe immediately ahead, continue on course. Once clear of these weather conditions, report encountered weather to air traffic control  \n• Note •  \nThe National Weather Service's Automated Surface Observing Systems (ASOS) program does not report freezing drizzle. It is the pilot's responsibility to evaluate and understand weather along the intended route and identify any potential weather hazards thru evaluation of, but not limited to, Current Observations, Pilot Reports, Area Forecasts, AIRMETS, SIGMETS, and NOTAMS.  \nAirspeed Limitations  \nMinimum airspeed for flight into known icing conditions ......... 95 KIAS*  \n*Includes all phases of flight, including approach, except as required for takeoff and landing.  \nMax airspeed Anti-Ice System operation........ 177 KIAS and 204 KTA","cbCaifaOXfOcRywT","https://ap.wps.com/l/cbCaifaOXfOcRywT","pdf",740137,48,"English","# Section 1 - General\n## Kinds of operation and compliance basis\n# Section 2 - Limitations\n## Operational exit criteria and prohibited conditions\n## Environmental conditions and detection cues\n## Airspeed, weight, takeoff, and performance limits\n## Minimum operating temperature","[{\"question\":\"What does this POH Supplement apply to when the TKS Anti-Ice System is installed?\",\"answer\":\"When the TKS Anti-Ice System is installed on the aircraft, this POH Supplement is applicable and must be inserted into the Supplements Section of the Pilot’s Operating Handbook. The supplement adds to, supersedes, or deletes information in the basic POH.\"},{\"question\":\"What must the pilot do at the first sign of an anti-ice system malfunction?\",\"answer\":\"The aircraft must immediately exit icing conditions when the first sign of an Anti-Ice System malfunction occurs.\"},{\"question\":\"Which icing-related weather conditions are prohibited or must be avoided?\",\"answer\":\"Flight into freezing rain or freezing drizzle is prohibited. Tests and defined known icing conditions do not include freezing rain, freezing drizzle, mixed conditions, or severe icing; flight in these conditions must be avoided.\"}]","Cirrus Design Section 9 - TKS Anti-Ice System - POH Supplement | PDF",1792859000,121]