# TCDS A13EA: Found Brothers Aviation Limited - Type: Type certificate data sheet - Status: Current - Holder: Found Brothers Aviation Limited - Revision: 0 - Revised: January 1, 1970 - Product: Aircraft, Small Airplane - Certification basis: Part 23 - Data sheet PDF: https://openairdocs.org/files/sha256/4c/7c/4c7c5db6f1fc3f0a74f007c454bc0fca62070bf1384c5a2ccb7f8e327366b772 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A5A7176B44BE096485256737004EE254.0001 - Page: https://openairdocs.org/tcds/A13EA ## Models (1) As the data sheet lists them. - FBA Centennial 100 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text Page No. 1 2 3 Rev. No. - - - DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A13EA FOUND BROTHERS FBA Centennial "100" January 1, 1970 TYPE CERTIFICATE DATA SHEET NO. A13EA This data sheet which is a part of Type Certificate No. A13EA 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 Found Brothers Aviation Limited P.O. Box 160 Grand Bend, Ontario, Canada I - Model FBA Centennial "100" (Normal Category), Approved 3 December 1968 by the FAA and 19 July 1968 by the Canadian Department of Transport (DOT) Engine Lycoming IO-540-G1D5. Fuel 100/130 minimum grade aviation gasoline Engine limits Maximum for all operations, 290 h.p. at 2,575 r.p.m. Full throttle at sea level. At propeller r.p.m.'s below 2,350 engine manifold pressure is not to exceed 23" hg. See NOTE 2. Propeller and propeller limits Hartzell variable pitch propeller, HC-92WK-1D/W9350-4.6 Diameter: Nominal 88 inches Pitch settings at station 30: Low 13.5°; High 29.4° Constant speed governor, Hartzell F-6-5A. Airspeed limits (CAS) Vne (Never exceed) 186 m.p.h. (161 knots) Vp (Maneuvering) 148 m.p.h. (128 knots) Vno (Maximum) 148 m.p.h. (128 knots) Vfe (Flaps extended) 109 m.p.h. ( 95 knots) C.G. range LANDPLANE AND SKIPLANE Gross Weight Fwd. limit Aft limit 3,500 lb. Sta. 82 (18.6% MAC) Sta. 87 (26.4% MAC) SEAPLANE 3,620 lb. Sta. 83 (20.2% MAC) Sta. 87 (26.4% MAC) Empty weight C.G. range None Datum Datum is 65 in. ahead of the center line of the main landing gear pick-up lugs. M.A.C. 63.5 in. (Leading edge of M.A.C. is 5.2 in. aft of datum.) Leveling means Aircraft cabin floor - level laterally and longitudinally. Maximum weight Landplane and skiplane - 3,500 lb. Seaplane - 3,620 lb. Minimum crew 1 (pilot) Number of seats 6 including pilot. (2 at Sta. 82.2, 2 at Sta. 117.2, and 2 at Sta. 148.9.) A13EA Page 2 Maximum baggage No separate defined baggage compartment - limited by maximum weight. Fuel capacity 54 Imperial gal. (65 U.S. gal.) (Sta. 82), 27 Imperial gal. (32.5 U.S. gal.) in each wing tank. 50.5 Imperial gal. (60.6 U.S. gal.) usable. See NOTE 1(b) for data on unusable fuel. Oil capacity 11 Imperial qt. (13.2 U.S. qt.) maximum (Sta. 22.6) including oil cooler. Oil cooler capacity 1 Imperial qt. (1.2 U.S. qt.) (Sta. 15). 11 Imperial qt. (13.2 U.S. qt.) usable. Control surface movements Wing flap 0° Up 45° Down Aileron 18° Up 12° Down Elevator 30° Up 25° Down Trim tab 26° Up 16° Down Gear tab 10° Up 8.3° Down Rudder 26° Left 26° Right Serial Nos. eligible 101 and up. The Canadian Department of Transport Certificate of Airworthiness for export endorsed as noted under "Import Eligibility" must be submitted for each individual aircraft for which application for certification is made. Import eligibility A U.S. Airworthiness Certificate may be issued on the basis of the Canadian Department of Transport "Certificate of Airworthiness for Export" signed by or for the Minister of Transport. This form must contain the following statement: "This certifies that the aircraft described below has been manufactured in conformity with data forming the basis for D.O.T. Type Approval No. A-88, Issue 1 (FAA Type Certificate No. A13EA)." Certification basis FAR 23 dated 1 February 1965, and Amendments 23-1 to 23-3 inclusive. Application for Type Certificate 24 October 1966. Required 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 items of equipment are required: (a) Aircraft Flight Manual (DOT Approved) dated 19 July 1968; (b) Stall Warning Indicator, Instrument Panel Dwg. 4R2036 and Wing Dwg. 4R1001. Optional equipment Landing gear 201. Ski Installation (a) Airglass LW 3600 skis. Ski installation to Found Bros. Dwg. 4E8015. 202. High Flotation Gear Installation (a) Type III Tires; Tire size 11.00 x 12; 8 ply rating. Installation to Found Bros. Dwg. 4R8011, Issue 3. 203. Float Installation (a) Edo Model 582-3430 Floats. Float Installation to Found Bros. Dwg. 4R8019 Issue 4. NOTE 1. (a) Current weight and balance report including list of equipment included in the certificated empty weight, and loading instructions when necessary, must be in each aircraft at the time of original certification and at all times thereafter. (b) The certificated empty weight and corresponding center of gravity locations must include unusable fuel of 25.3 lb. (82.0 in.). A13EA Page 3 NOTE 2. The following placards must be placed in clear view of the pilot: (a) THIS AIRCRAFT MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE IN COMPLIANCE WITH THE OPERATING LIMITATIONS IN THE FORM OF PLACARDS, MARKINGS AND MANUALS." (b) "NO ACROBATIC MANEUVERS, INCLUDING SPINS, ARE APPROVED." (c) "DO NOT EXCEED 23" HG M.A.P. BELOW 2,350 R.P.M." (d) "DAY VFR OPERATION ONLY." (e) "DEMONSTRATED CROSSWIND VELOCITY 12 M.P.H." (f) "FLIGHT IS NOT PERMITTED WITH RIGHT HAND ELEVATOR AILERON CONTROL INSTALLED." The following placard must be placed in clear view of the pilot when the aircraft is operated in the seaplane configuration: (g) "USE OF FULL FLAP (THIRD NOTCH) IS NOT APPROVED." NOTE 3. To detect cracks in the welded joint between the lower end of the main landing gear leg, P/N 4R8005-17 and -18, and wheel axle block, P/N 4R8005-24, accomplish the following at intervals not to exceed 100 hours' in service and after each suspected heavy landing: (a) Perform a magnetic particle, fluorescent, or visible dye penetrant inspection of the welded area for cracks and evidence of incipient failure or an equivalent inspection approved by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region. (b) In the event of cracks or evidence of incipient failure being found, repair part in accordance with an approved repair scheme or replace with a part of the same part number that has been inspected in accordance with paragraph (a) and certified airworthy. (c) In the event of the inspection indicating the leg to be free of cracks or incipient failure, re-paint inspected area in accordance with the manufacturer's specifications. (Canadian Department of Transport Airworthiness Directive CF-69-13 covers this subject). NOTE 4. The Found Brothers Aviation Limited Model FBA Centennial "100" aircraft is built to the Found Bros. Drawing List, Report No. 4D-60, Issue I, dated 18 July 1968. - 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 ## STCs approved under this data sheet (46) - [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 SA12428CH](https://openairdocs.org/stc/SA12428CH): Installation of the Lycoming Engines Electronic Ignition System (EIS). Lycoming Engines, An Operating Division of AVCO Corporation - [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, 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 SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc. - [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation 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 SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. 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 SA01435LA](https://openairdocs.org/stc/SA01435LA): Installation of engines modified with Firewall Forward Technologies LLC modified camshaft. Centri-Lube Technologies LLC - [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 SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV).. Genesys Aerosystems 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 SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne 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 SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies - [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 SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation - [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 SA02212AK](https://openairdocs.org/stc/SA02212AK): Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Seaplanes North LLC - [STC SA00382BO](https://openairdocs.org/stc/SA00382BO): Installation of Globalstar Antenna and Cradle provisions to support a Globalstar GPS-1700 in non-composite airplanes. Avidyne Corporation - [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation - [STC SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation - [STC SA02119SE PAGE 1](https://openairdocs.org/stc/SA02119SE%20PAGE%201): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc - [STC SA02442AK PAGE 1](https://openairdocs.org/stc/SA02442AK%20PAGE%201): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC - [STC SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System. Garmin International Inc - [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 SA03148NY](https://openairdocs.org/stc/SA03148NY): The installation of the Latitude Technologies Corporation S100 Tracking System. Latitude Technologies Corporation - [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 SA02293AK](https://openairdocs.org/stc/SA02293AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV).. Chelton Flight Systems Inc. - [STC SA593CH](https://openairdocs.org/stc/SA593CH): Install Champion SlickSTART magneto booster system.. Champion Aerospace LLC - [STC SA02795AT](https://openairdocs.org/stc/SA02795AT): Installation of a PXE7300SR, In-Flight Entertainment System. PS Engineering Incorporated - [STC SA5159NM](https://openairdocs.org/stc/SA5159NM): Installation of chip detector system.. Northwest Aircraft Inc - [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 SA01435DE](https://openairdocs.org/stc/SA01435DE) (historical): Installation of engines, modified with a Firewall Forward Technologies.. Centri-Lube Technologies LLC - [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.