# TCDS 7A5: Nardi S.A. - Type: Type certificate data sheet - Status: Current - Holder: Nardi S.A. - Revision: 3 - Revised: February 16, 2022 - Product: Aircraft, Small Airplane - Registered aircraft: 4, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/3a/37/3a37030d6dc83492a0d27782fcb39f59c3b64d89893bb6ffac75c32b6a6f61b3 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8B20CC50BA03C7E6862587F3006ACD3C.0001 - Page: https://openairdocs.org/tcds/7A5 ## Models (1) As the data sheet lists them. - FN-333 ## 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 7A5 Revision 3 NARDI FN-333 February 16, 2022 TYPE CERTIFICATE DATA SHEET NO. 7A5 This data sheet which is a part of type certificate No. 7A5 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 NARDI S. A. Milan, Italy I - Model FN-333, 4 PCAmM (Normal Category), approved December 15, 1958 Engine Continental IO-470-P Fuel * 91/96 Minimum grade aviation gasoline Engine limits * For all operations, 2600 r.p.m. (250 hp.) Propeller and 1. Hartzell HC82X20-5L/L8433-H propeller limits 2 blades, metal, constant speed with reversible pitch Maximum diameter 84 in. Maximum diameter 81 in. (No further reduction permitted) Pitch settings at 30 in. sta.: Low 13°, high 27°30', reversed -14° 2. Hartzell HCA3X20-5L/L8433-6B 3 blades, metal, constant speed with reversible pitch Maximum diameter 78 in. Maximum diameter 76 in. (No further reduction permitted) Pitch settings at 30 in. sta.: Low 12°30", high 28°30', reversed -14°30' Airspeed limits *Vne (never exceed) 206 m.p.h. (178 knots) *Vno (max. structural cruising) 162 m.p.h. (140 knots) #Vp (maneuvering speed) 146.5 m.p.h. (127 knots) *Vfe (flaps extended in all positions) 125 m.p.h. (109 knots) *Vle (landing gear extended) 125 m.p.h. (109 knots) *Vfle (wing floats extended) 125 m.p.h. (109 knots) *Vwre (water rudder extended) 206 m.p.h. (178 knots) C.G. range *(+110) to (+117) (landing gear extended) Empty weight C.G. range None Datum Nose of aircraft Leveling means Datum pads on left door frame Maximum weight *3270 lb. No. seats 4 (2 at +52.1, 2 at +95.3) Maximum baggage *300 lb. (+95.3) Fuel capacity 65.8 U.S. gal. (two wing tanks, 32.9 U.S. gal. ea.) (+107.5) Oil capacity 3.5 U.S. gal. (+141.6). See NOTE 1 for data on system oil. Control surface movements Wing flaps Down 45° Aileron Up 25° Down 18° Elevator tab Up 23° Down 23° Elevator Up 25° Down 20° Rudder Right 25° Left 25° Stabilizer Fixed Page No. 1 2 Rev. No. 3 3 ׀ 7A5 2 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. 7A5 issued December 25, 1958. Date of Application for Type Certificate December 3, 1957. Each aircraft and any replacement parts manufactured in Italy must be clearly identified as imported. 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 Italiano (RAI) containing the following statement: "The airplane covered by this certificate has been examined and found to comply with U.S. Civil Air Regulations Part 3, dated May 15, 1956, including Amendments 3-1, 3-2, 3-3, 3-4 and 3-5, and conforms to TC 7A5." Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification. In addition, the following item of equipment is required: (a) Pre-stall warning indicator, Safe Flight Instrument Corp. 164.S Import Requirement 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 provided for each aircraft at the time of original certification. The certificated empty weight and corresponding center of gravity locations must include system oil of 1 lb. at (+141.6). NOTE 2. The following placards must be displayed on the instrument panel in full view of the pilot: (a) "THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE IN COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE FORM OF PLACARDS, MARKINGS. NO ACROBATIC MANEUVERS, INCLUDING SPINS, ARE APPROVED." (b) "WARNING: REVERSING PROPELLER IN FLIGHT PROHIBITED. OPERATE REVERSE LEVER IN LOW PITCH ONLY. MAXIMUM 2400 RPM IN REVERSE PITCH." (c) In addition to the above placards, the prescribed operating limitations indicated by "*" under Section I above, must be displayed by permanent markings. NOTE 3. This aircraft is approved for night flying when the prescribed equipment is installed. .....END..... ``` ## ADs (1, in force first) - [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022 ## Registered aircraft by registry model (OpenAirDocs) - [Nardi FN-333](https://openairdocs.org/model/nardi-fn-333): 4 aircraft (registry code 6080102) ## STCs approved under this data sheet (34) - [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc. - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder.. Garmin International Inc. - [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc. - [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics - [STC SA04568CH](https://openairdocs.org/stc/SA04568CH): Installation of the uAvionix tailBeaconX, a tail mounted position light with integrated Automatic Dependent Surveillance - Broadcast (ADS-B) Out and 1090MHz Mode-S transponder functionality. uAvionix Corporation - [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc. - [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).. Garmin International Inc. - [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc. - [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 SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc. - [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 SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation - [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems.. Garmin International Inc - [STC SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation - [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation - [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 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 SA02442AK PAGE 2](https://openairdocs.org/stc/SA02442AK%20PAGE%202): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC - [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 SA02016SE-D](https://openairdocs.org/stc/SA02016SE-D): Installation of Garmin GTS 800, GTS 820 or GTS 850 Traffic System. Garmin International Inc - [STC SA593CH](https://openairdocs.org/stc/SA593CH): Install Champion SlickSTART magneto booster system.. Champion Aerospace LLC - [STC SA2683NM](https://openairdocs.org/stc/SA2683NM): Installation of Precise Flight, Inc. stand-by vacuum system (SVS). Precise Flight Inc - [STC SA798EA](https://openairdocs.org/stc/SA798EA): Installation of Monitair exhaust gas combustion monitor kit.. Rosemount Engineering Co - [STC SA538CE](https://openairdocs.org/stc/SA538CE): Extend spray rails 29-1/2-inch rearward.. Kenosha Aviation Svc Inc - [STC SA001410BO](https://openairdocs.org/stc/SA001410BO) (historical): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation - [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.