# TCDS 2A11: Lockheed Martin Aeronautics Company - Type: Type certificate data sheet - Status: Current - Holder: Lockheed Martin Aeronautics Company - Revision: 5 - Revised: July 23, 2012 - Product: Aircraft, Small Airplane - Certification basis: Part 3, CAR 3 - Registered aircraft: 1, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/32/69/3269b910194e172c08c604e95192085fe87c51489e553e6eac08d6e6d68860d7 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/579D12EF309E8FC386257A450047A21B.0001 - Page: https://openairdocs.org/tcds/2A11 ## Models (1) As the data sheet lists them. - 402-2 ## 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. 5 4 - DEPARTMENT OF TRANSPORATION FEDERAL AVIATION ADMINISTRATION 2A11 Revision 5 LOCKHEED 402-2 July 23, 2012 TYPE CERTIFICATE DATA SHEET NO. 2A11 This data sheet which is a part of type certificate No. 2A11 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 Lockheed Martin Aeronautics Company 86 South Cobb Drive Marietta, GA 30063 Type Certificate Holder Record Lockheed Aircraft International 510 West Sixth Street Los Angeles 14, California I - Model 402-2, 6 PCLM (Normal Category), Approved April 5, 1960 Engines Continental IO-470-R (See NOTE 3 for serial No. 1) Continental TSIO-470-B Fuel Continental IO-470-R Engine: 91/96 minimum grade aviation gasoline Continental TSIO-470-B Engine: 100/130 minimum grade aviation gasoline Engine limits Continental IO-470-R Engine: For all operations, 2600 r.p.m. (250 hp.) Continental TSIO-470-B Engine: For all operations: 2600 r.p.m., 35 in.Hg. (260 hp.) sea level 2600 r.p.m., 35 in.Hg. (260 hp.) 12,500 ft. Propeller and propeller limits McCauley D2A36C33/90M-4 Diameter: Maximum 86 in., mi nimum allowable for repairs 84 in. No further reduction permitted. Continental IO-470-R Engine: Pitch Setting at 36 in. radius: Low 9.0°, High 22.3° Continental TSIO-470-B Engine: Pitch setting at 36 in. radius: Low 10.0°, High 27.5° (See NOTE 3 for serial No. 1) Airspeed limits Never exceed 176 m.p.h. (153 knots) Maximum structural cruising 140 m.p.h. (122 knots) Maneuvering 133 m.p.h. (116 knots) Flaps extended 100 m.p.h. ( 87 knots) C.G. range (+211.1) to (+216.5) at 3532 lb. (+204.5) to (+216.5) at 2700 lb. or less Straight line variation between (+204.5) at 2700 lb. and (+211.1) at 3532 lb. 2A11 2 Empty weight C.G. range None. Datum 191.67 in. forward of leading edge of wing at wing root; L. E. MAC (+192.43); MAC length 65.33 in. Leveling means Cabin floor - left center seat rail inside left cabin door. Maximum weight 3532 lb. No. seats 2 (+202); 2 (+230) or (+236); 2 (+261) Maximum baggage 200 lb. (+85) Fuel capacity 57 gal. total; 49 gal. usable (2 wing tanks +219) See NOTE 1 for unusable fuel. Oil capacity 3 gal. (+135) (Unusable Oil - 4 qt.) Applicable to either engine. See NOTE 1 for system oil. Control surface movements Wing Flaps Down 27° + 1° Aileron Up 10° + 1° Down 11° + 1° Elevator Up 25° + 1/2° Down 16° + 1° Rudder Right 20° + 1° Left 19° + 1° Horizontal Stabilizer (Minus) 1/2° + 1/2° to (Minus) 5 1/2° + 1/2° Serial Nos. eligible 1, 2, 1007, 1009, 1010, 1011, 1016, 1019, 1020, 1021, and 1025. See NOTE 3 for special configuration eligible for Serial No. 1 only. Certification basis CAR 3 effective May 15, 1956 th rough amendments 3-5 effective October 1, 1959. Type Certificate No. 2A11 issued April 5, 1960 Date of Application for Type Certificate March 31, 1959 Production basis None. Prior to original certification of each aircraft, a FAA representative must perform a detailed inspection for workmanship, material and conformity with the approved technical data, and a check of the flight characteristics. Equipment The basic required equi pment 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) All items noted as standard equipmen t in the Manufacturer's approved equipment list. (b) Continental IO-470-R Engine: FAA Approved Airplane Fli ght Manual dated January 10, 1961. Continental TSIO-470-B Engine: FAA Approved Airplane Fli ght Manual dated December 14, 1960. (See NOTE 3 for serial No. 1) NOTE 1. Current weight and balance report including list of equipment included in certificated empty weight, and loading instructions when necessary, must be provided for each aircraft at the time of original certification. The certificated empty weight and corresponding center of gr avity locations must include system oil of 1 lb. at (+135) and unusable fuel of 48 lb. at (+219). NOTE 2. The following placard must be displaye d in front and in clear view of pilots: "THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE IN COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE FORM OF PLACARDS, MARKINGS, AND MANUAL." 3 2A11 NOTE 3. Airplane Serial No. 1 is the same as Serial No. 2 and subsequent when equipped with the Continental IO-470-G Engine, McCauley Propeller Model B2A36C31/90M-4 and associated cowling, engine baffling and structural changes in accordance with Lockheed Report ER- 4325. Fuel, Oil, and Propeller Limits are same as for the IO-470- R Engine except that fuel capacity is 60 gal. total, 52 gal. usable. FAA Approved Airplane Flight Manual dated April 5, 1960 is required with this installation. NOTES 1 and 2 are applicable. NOTE 4. Model 402-2 aircraft, manufactured in Mexico by Lockheed Azcarate S.A., may become eligible for U.S. airworthiness certificate upon compliance with the provisions of CAR 1.67(b), subject, in addition, to the following conditions which are stipulated in the Provisional Agreement, dated July 19, 1961, between the Governments of the United States and Mexico: (1) Application is made for issuance of a United States airworthiness certificate within 30 days after the date the Mexican airworthiness certificate was issued; (2) The Mexican Government certifies that such individua l airplane conforms to the type design approved by the United States and is in a safe operating condition; and, (3) An FAA representative conducts a sa tisfactory airworthiness inspection in the United States, before issuing the airworthiness certificate. NOTE 5. Ski installation may be made in accordance with Lockheed Aircraft International drawing list revision dated March 5, 1962, (Report ER4326). Fluidyne Flight Manual Supplement dated February 12, 1962, is applicable to this installation. -END- ``` ## ADs (2, in force first) - [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023 - [AD 93-14-12](https://openairdocs.org/ad/93-14-12): Crewmember Protective Breathing Equipment Units · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 201 more. Effective Sep 2, 1993 ## Registered aircraft by registry model (OpenAirDocs) - [Lockheed Aircraft Intl 402-2](https://openairdocs.org/model/lockheed-aircraft-intl-402-2): 1 aircraft (registry code 5263406) ## STCs approved under this data sheet (43) - [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.. TCW Technologies, LLC - [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, 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 SA5581SW](https://openairdocs.org/stc/SA5581SW): Installation of ALCOR true-flow/ totalizer system. Alcor LLC - [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 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 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 SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc. - [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation - [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc - [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 SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation - [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [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 SA01229SE PAGE 1](https://openairdocs.org/stc/SA01229SE%20PAGE%201): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. 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 SA01933LA-D PAGE 1](https://openairdocs.org/stc/SA01933LA-D%20PAGE%201): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA10682SC](https://openairdocs.org/stc/SA10682SC): Installation of alternator and voltage regulator. Hartzell Engine 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 SA02717NY PAGE 1](https://openairdocs.org/stc/SA02717NY%20PAGE%201): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC - [STC SA02825NY PAGE 1](https://openairdocs.org/stc/SA02825NY%20PAGE%201): Installation of Aerospace Logic Aircraft Instruments. Aerospace Logic Inc. - [STC SA01692SE](https://openairdocs.org/stc/SA01692SE): Installation of a Garmin GMX 200 Multi-Function Display. 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 SA01487SE-D](https://openairdocs.org/stc/SA01487SE-D): Installation of a GDL 69 or GDL 69A XM Satellite Receiver. Garmin International Inc - [STC SA01473SE](https://openairdocs.org/stc/SA01473SE): Installation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote Transponde. Garmin AT Inc. - [STC SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc - [STC SA01695SE](https://openairdocs.org/stc/SA01695SE): Installation of an antenna. Garmin AT Inc. - [STC SA01487SE](https://openairdocs.org/stc/SA01487SE): Installation of a GDL 69 or GDL 69A XM Satellite Receiver in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0217-00, Revision A, dated December 20, 2004, or later FAA approved revision.. Garmin AT Inc. - [STC SA02154AK](https://openairdocs.org/stc/SA02154AK): Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display, P/N 430-0270-500.. Garmin AT Inc. - [STC SA02217AK](https://openairdocs.org/stc/SA02217AK): Installation of Garmin AT Model GDL90 UAT Data Link System, in accordance with Garmin AT, Inc., GDL 90 UAT Master Data List, P/N 560-0278-01, Revision A, dated November 12, 2004, or later FAA approved revision.. Garmin AT Inc. - [STC SA334SW](https://openairdocs.org/stc/SA334SW): Installation of InterAv Alternator.. InterAv, Inc - [STC SA02717NY](https://openairdocs.org/stc/SA02717NY) (historical): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC - [STC SA01933LA](https://openairdocs.org/stc/SA01933LA) (historical): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin AT Inc. - [STC SA01229SE](https://openairdocs.org/stc/SA01229SE) (historical): Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios.. 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