TCDS A3NW

Page No. 1 Rev No. 3 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A3NW AVIAN SKYHAWK Rev. 3 April 18, 2018 TYPE CERTIFICATE DATA SHEET NO. A3NW This data sheet which is a part of type certificate No. A3NW prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder AVIAN BALLOON Co. 12925 East Riverside Spokane, WA 99216 I - Model SKYHAWK, 4-place Hot Air Balloon, approved August 8, 1977 Air Heater Options specified in the latest FAA approved revision of Master Drawing List No. 76 Gondola Options specified in the latest FAA approved revision of Master Drawing List No. 76 Envelope Options specified in the latest FAA approved revision of Master Drawing List No. 76 Use of Series 76 -5800 Envelope requires an approved redundant burner system. See FAA Approved Balloon Flight Manual Supplement for Envelope Series 76-5800. Fuel LPG (See FAA Approved Balloon Flight Manual for required additives instruction.) Maximum Weight Gross weight limited to 1400 lbs. or to weight requiring maximum continuous envelope temperature of 250°F, whichever is less. See FAA Approved Balloon Flight Manual. (Weight includes the envelope weight.) Maximum Allowable Envelope Temperature 250°F Fuel Capacity See FAA Approved Balloon Flight Manual Serial Numbers Eligible 1 and on Certification Basis FAR 31, effective July 1, 1964, including Amendments 31-1 and 31-2. Production Basis 731NM Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (See Certification Basis) must be installed in the aircraft for certification. Additional required items of equipment are listed in the FAA Appr oved Avian Balloon Flight Manual. NOTE 1 Reserved NOTE 2 Reserved NOTE 3 Information essential to the proper maintenance of the balloon is contained in the Manufacturer’s Maintenance Manual provided with each balloon . The approved service lives, mandat ory inspections or other approved supplemental procedures of components are listed in the latest FAA accepted revision of Document No. ICA-1. .....END.....