TCDS 7A11

FEDERAL AVIATION AGENCY 7A11 Revision 2 AEROMERE Falco F.8.L February 15, 2022 TYPE CERTIFICATE DATA SHEET NO. 7A11 This data sheet which is a part of type certificate No. 7A11 prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Civil Air Regulations. Type Certificate Holder AEROMERE S.A., Trento, Italy I. Model Falco F.8.L, (Utility and Acrobatic Categories), Approved June 26, 1961 Engine Lycoming O-320-A1A Fuel 80/87 Minimum grade aviation gasoline Engine limits For all operations, 2700 r.p.m. (150 hp) Propeller and Hartzell HC-82XL-IF/7636D-4, 2 bladed metal Propeller limits Pitch setting at 30 in. station: Low 12 degrees High 25.5 degrees Diameter: Maximum 76 in. minimum 72 in. Minimum allowable for repairs 70 in. (no further reduction permitted) Hartzell HC-C2YL-1/7663-4, 2 bladed metal Pitch setting at 30 in. station: Low 13 degrees High 30 degrees Diameter: Maximum 72 in. minimum 70 in. (no further reduction permitted) Airspeed limits Vne (never exceed) Vno (Max. Struc. cruising) Vp (Maneuvering speed) Vfe (Flaps extended 20 degrees) Vfe (Flaps extended 45 degrees) Vle (Landing gear extended) Utility 240 m.p.h. 185 m.p.h. 140 m.p.h. 112 m.p.h. 100 m.p.h. 125 m.p.h. Acrobatic 240 m.p.h. 185 m.p.h. 155 m.p.h. 112 m.p.h. 100 m.p.h. 125 m.p.h. C.G. range Datum Maximum weight No. of seats Maximum baggage (+68.5) to (+74.8) Front surface of the engine flange Utility Acrobatic 1720 lb. 1650 lb. 2 (+85.2) 2 (+85.2) 88 lb. (+109.9)22 lb. (+109.9) Fuel capacity Front tank, 18.5 U.S. gal. (+44.8) Rear tank, 13.2 U.S. gal. (+128.4) Oil capacity 8 qt. (+21.6) Page No. 1 2 Rev No. 2 2 ׀ 7A11, Rev 2 Page 2 Control surfaces movements Wing flaps Down 45 degrees Ailerons Up 24 degrees Down 16 degrees Elevator Up 24 degrees Down 16 degrees Elevator tab Up 20 degrees Down 20 degrees Rudder Right 20 degrees Left 20 degrees Stabilizer Fixed Serial Nos. eligible The Registro Aeronautico Italiano (RAI) Certificate of Airworthiness endorsed as noted below under "Certification basis" must be submitted for each individual aircraft for which application for certification is made. Certification basis CAR 10. Type Certificate No. 7A11 issued June 26, 1961. Application for Type Certificate dated July 1, 1958. Import Requirement A U.S. Airworthiness Certificate may be issued on the basis of a Certificate of Airworthiness for Export signed by a representative of the Registro Aeronautico Italino (RAI) containing the following statement: "The airplane covered by this certificate has been examined and found to comply with U.S. Civil Air Regulation Part 3, dated May 15, 1956, including Amendments 3-1, 3-2, 3-3 and conforms to T.C. 7A11." Refer to the applicable bilateral agreement to verify eligibility for import into the United States of both new and used aircraft based on the scope of the agreement, to identify any required statements by the exporting authority on the export certificate of airworthiness (or equivalent document), and for procedures for coordinating exceptions to conformity statements on these documents. Refer to FAA Order 8130.2, Airworthiness Certification of Aircraft, for requirements for issuance of an airworthiness certificate for imported aircraft. NOTE 1. Current weight and balance report including list of equipment in certificated empty weight, and loading instructions, must be in each aircraft at the time of original certification and at all times thereafter except in the case of operators having an approved weight control system. The certificated empty weight and corresponding center of gravity locations must include system oil of 1 lb. at (+21.6). NOTE 2. The following placard must be displayed on the instrument panel in full view of the pilot: "THIS AIRCRAFT MUST BE OPERATED AS AN AEROBATIC CATEGORY AIRCRAFT, IN ACCORDANCE WITH THE LIMITATIONS INDICATED IN THE PLACARDS, MARKINGS AND MANUALS, FOR OPERATIONS OF AIRCRAFT IN UTILITY CATEGORY REFER TO FLIGHT MANUAL. MAXIMUM WEIGHT FOR AEROBATIC CATEGORY: 1650 LBS. -END-