# TCDS 7A11: Aeromere S.A. - Type: Type certificate data sheet - Status: Current - Holder: Aeromere S.A. - Revision: 2 - Revised: February 15, 2022 - Product: Aircraft, Small Airplane - Data sheet PDF: https://openairdocs.org/files/sha256/f8/e7/f8e7e8be4731f23e2a400525924a42569a93823d92a11db305a0f4d5dc360702 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DD5195F51E655D14862587F3006B13A7.0001 - Page: https://openairdocs.org/tcds/7A11 ## Models (1) As the data sheet lists them. - Falco F.8.L. ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text 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- ``` ## ADs None name its models. ## STCs approved under this data sheet (22) - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA239SW](https://openairdocs.org/stc/SA239SW): Installation of Alcor exhaust gas temperature (EGT) indicator kits. Alcor LLC - [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc. - [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd. - [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio.. Peregrine - [STC SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine - [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC - [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc. - [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King) - [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine - [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine - [STC SA01435SE](https://openairdocs.org/stc/SA01435SE): Installation of J.P. Instruments (JPI) Primary Engine Data Management System. J. P. Instruments - [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc. - [STC SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine - [STC SA02015SE-D](https://openairdocs.org/stc/SA02015SE-D): Installation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System.. Garmin International Inc - [STC SA593CH](https://openairdocs.org/stc/SA593CH): Install Champion SlickSTART magneto booster system.. Champion Aerospace LLC - [STC SA489EA](https://openairdocs.org/stc/SA489EA): Installation of ARP Inc. carburetor ice detection system. Aircraft & Rotorcraft Products (ARP) Inc - [STC SA5159NM](https://openairdocs.org/stc/SA5159NM): Installation of chip detector system.. Northwest Aircraft Inc - [STC SA308EA](https://openairdocs.org/stc/SA308EA): Installation of carburetor ice detection system 105AP in single and twin engine aircraft and single engine helicopters powered by Continental, Franklin, and Lycoming type engines equipped with Marvel-Schebler MA-2, MA-3, MA-4, MA-4-5, MA-6 and HA-6 series carburetors. (Normal,Utility and Acrobatic Category airplanes and helicopters equipped with engines and carburetors as described.). Alfred R Puccinelli - [STC SA00765DE PAGE 1](https://openairdocs.org/stc/SA00765DE%20PAGE%201) (historical): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine - [STC SA02153LA-D](https://openairdocs.org/stc/SA02153LA-D) (historical): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc - [STC SA02153LA](https://openairdocs.org/stc/SA02153LA) (historical): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System.. Garmin AT Inc. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.