TCDS 1A13
STCs approved under this data sheet · 219
Current certificates first, most recently changed first.
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duckdb -csv -c "SELECT s.stc_number, s.description, s.holder, s.status, s.status_date FROM 'https://openairdocs.org/data/latest/faa_stc.parquet' s WHERE s.stc_number IN (SELECT stc_number FROM 'https://openairdocs.org/data/latest/faa_stc_model.parquet' WHERE tcds_number = '1A13') ORDER BY s.status = 'Current' DESC, s.status_date DESC, s.stc_number"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT s.stc_number, s.description, s.holder, s.status, s.status_date FROM 'https://openairdocs.org/data/latest/faa_stc.parquet' s WHERE s.stc_number IN (SELECT stc_number FROM 'https://openairdocs.org/data/latest/faa_stc_model.parquet' WHERE tcds_number = '1A13') ORDER BY s.status = 'Current' DESC, s.status_date DESC, s.stc_number
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
STC SA593CHInstall Champion SlickSTART magneto booster system.STC SA02033ATModification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.STC SA01473SEInstallation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote TranspondeSTC SA4005NMPrecise Flight Inc. Pulselite Control SystemSTC SA1512WEInstallation of exhaust gas temperature monitoring systems Model EGT-1.STC SA2557NMInstallation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system.STC SA01695SEInstallation of an antennaSTC SA00759NYInstallation of Northeast Engineering landing gear actuator rod.STC SA03251ATFor Lake Model 250, including this model incorporating STC SA469NE, replace existing propeller with MT-Propeller model no. MTV-9-B-C-R(M)/CRLD193-109 (reversing type) per MT-Propeller Installation, Doc. No. E-1261, dated 11/10/2005 or later FAA approved revision or, install Propeller model no. MTV-9-B/LD193-109 (non-reversing type) per Doc. No. E-1262, dated 11/10/2005 or later FAA approved revision.STC SA1179GLInstallation of a Shadin Co. fuel flow indicator.STC SA01860NYInstallation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.STC SA03217ATInstallation of improved Horizontal Stabilizer Attachment Fitting XLS KitSTC SA01377ATInstallation of Textron Lycoming IO-360-A1B6. Bartow FL 33830STC SA02153NYInstallation of Lake Central Air Services Horizontal Stabilizer Attachment Fitting.STC SA01487SEInstallation 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.STC SA00680SEInstallation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.STC SA01158WIInstallation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.STC SA2683NMInstallation of Precise Flight, Inc. stand-by vacuum system (SVS)STC SA00161BOInstallation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.STC SA01157LAInstallation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument.STC SA02154AKInstallation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display, P/N 430-0270-500.STC SA02217AKInstallation 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.STC SA10BOIInstallation of dual Lycoming Alternators, P/N 32C19553, in accordance with Lake Aircraft Drawing 4-7785, dated August 24, 1993 or later FAA-approved revisions.STC SA469NEInstallation of Lycoming turbocharged engine model TIO-540-AA1AD in accordance with Lake Aircraft Drawing List 250T, Revision E or later Federal Aviation Administration (FAA) approved revision.STC SA4NEInstallation of the Hartzell HC-E2YR-1BLF/FL7666A-2 or HC-E2YK-1BL/L7666A-2 Extended Hub Propeller on aircraft equipped with Lycoming IO-360-A1B6 engine in accordance with Aerofab, Inc. Drawing No. 160013L (Rev.E) dated December 23, 1980.STC SA631CEInstall Lycoming IO-360-A1B engine, Hartzell HC-C2YK-1BL/L7666A-2 propeller and remove wing fillets.
Data Required: Lake 4 Sales Engineering Report 62568, Rev. 9/9/68, Drawings L-0254 Rev. 3, E.O. 2-1165A, L-0255, L-2075, L-2076, L-2077, 2-5200 Rev. D, 2-6000 Rev. H, 2-7752, 2-7757 Rev. B, copy of this certificate and AFMS dated March 14, 1969.STC SA745NERemoval of rear bench seat and relocation of middle seats in accordance with Aerofab Inc. Drawing 170046, dated September 29, 1989.STC SA781EAConversion of the Lake LA-4 Amphibian to LA-4 Seaplane. Modifications consist primarily of removing landing gears and covering resultant openings with skin in accordance with Aerofab, Inc. drawing list dated January 30, 1969.STC SA7NEInstallation of the 3-bladed Hartzell HC-C3YR-1 RLF/FL 7663-8R propeller on aircraft equipped with Lycoming IO-360-A1B6 engine and Hartzell hydraulic governor Model F-2 in accordance with Aerofab Inc. Drawing No. 160015, dated March 11, 1974.STC SA822EAEligible for increase in gross weight to 2600 lb. with 200 h.p. engine installed per STC SA631CE.
Aerofab, Inc. Supplement No. 4, approved May 26, 1970, to Lake LA-4 Flight Manual, is required.STC SA855EAInstallation of a cabin air heat exchanger on the following model aircraft:
1. Lake LA-4 in accordance with Drawing No. 170040, Rev. A.
2. Lake LA-4-200 in accordance with Drawing No. 170042, Rev. A.STC SA876EA1. Models LA-4-200, LA-4, LA-4A, LA-4P:
Installation of Auxiliary Fuel System in accordance with Aerofab Drawings No. 180004, Rev. G, dated June 8, 1971,
and 180009, Rev. D, dated February 10, 1971.
2. Model LA-4-200: Increase of Gross Weight to 2690 pounds.
Limitations and Conditions (Continued):
(b) Aerofab Inc. Airplane Flight Manual Supplement:
(i) No. 5, FAA approved June 24, 1971, revised July 18, 1975, for Lake LA-4, LA-4A, LA-4P, LA-4-200 Flight Manual Dated July 11, 1960, revised April 11, 1973, or:
(ii) No. 4, FAA approved December 28, 1973, revised July 18, 1975, for Lake LA-4-200 Flight Manual reissued December 28, 1973.
is required for operations at 2690 lb. Gross Weight.STC SA92NE1. Installation of Symbolic Displays FT-101 fuel flow system in accordance with Lake Aircraft Drawing 100.
2. Installation of Symbolic Displays FT-101 or Alcor Tru-Flo fuel flow system in accordance with lake Drawing No.
100, Revision B or later FAA approved Revision.STC SA969NEInstallation of lighting panel in accordance with Lake Aircraft Drawing No. 4-7359.STC SA970NEInstallation of wing filler for auxiliary fuel tanks, miscellaneous structural modifications and optional radome, dual alternator system, bow compartment covers, upper fin revision, disassembly provisions and dual rudder/aileron electric trim system in accordance with Aerofab, Inc. Drawing List 4-0001, Revision I, dated October 23, 1996, or later FAA-approved revision. The installation is applicable in the following configurations:
United States of America
Department of Transportation - Federal Aviation Administration
Supplemental Type Certificate
(Continuation Sheet)
___________________________________________________________________________________________________________________________________
Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both.
___________________________________________________________________________________________________________________________________
FAA Form 8110-2-1(10-69) PAGE 4 of 4 PAGES This certificate may be transferred in accordance with FAR 21.47.
United States of America
Department of Transportation -- Federal Aviation Administration
Supplemental Type Certificate
_____________________________________________________________________________________________________________________________________
Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both.
_____________________________________________________________________________________________________________________________________
FAA Form 8110-2(10-68) PAGE 1 of 1 PAGES This certificate may be transferred in accordance with FAR 21.47.
CONFIGURATION 1:
Basic installation with aft seats installed in accordance with Configuration 1 of STC SA469NE. Optional items may be installed in any combination as follows:
Option 1: Radome
In accordance with drawings 150017, 190011, 190018 and 190019.
Mass with an equivalent weight of 35 lbs. may be installed with a center of gravity no farther forward than 6.61 inches aft
of bulkhead 190011-11, as defined in Aerofab, Inc. Engineering Report 4-250-2, dated November 4, 1991, and drawing
190019.
This STC does not approve the installation of a radar, antenna, wave guide or transmitter, nor radar/radome system
compatibility.
Option 2: Dual Alternator System
In accordance with drawings 4-7781 and 4-7782.
Option 3: Bow Compartment Covers
In accordance with drawing 4-3501.
Option 4: Upper Fin Revision
In accordance with drawing 4-2652, Revision C.
Option 5: Disassembly Provisions
In accordance with drawing 300015.
Option 6: Dual Rudder/Aileron Electric Trim System
In accordance with drawing 4-3519 and STC SA1142SO.
CONFIGURATION 2:
Same as Configuration 1 except aft sets installed in accordance with Configuration 2 of STC SA469NE and aft seat weight restriction placard installed in accordance with drawing 4-7003.STC SA00156BOInstallation of MT-Propeller MTV-12-B-C-R(M)/CRLD 188-119a propeller in accordance with MT-Propeller Report No. E-820-E, dated January 14, 2002, or later FAA-approved revisions or MTV-12-B/LD188-119a propeller in accordance with MT-Propeller Report No. E-958, dated February 10, 2004, or later FAA-approved revisions.STC SA10126SCInstallation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision.STC SA00954SEInstallation of J.P. Instruments (JPI) Primary Temperature Indicating System in accordance with JPI Installation Manual for the EDM 711, Report 106P, Revision B, dated August 2, 2001, or later FAA approved revision.STC ST01700NYInstallation of the following Aerospace Logic aircraft instruments: EGT-100 Exhaust Gas Temperature Indicator, CHT-100 Cylnder Head Temperature INdicator, FL-100 Dual Fuel Level Indicator, FP-100 Fuel Pressure and Ammeter Indicator, OL-100 Oil Pressure and Temperature Indicator, and VA-100 Voltmeter and Ammeter Indicator.STC SA00165BOInstallation of Avidyne Corporation Datalink Coupler, part number 700-00015-000 per Avidyne Corporation Master Document List, Document No. AVACP-006 dtd 1/2/93 or later FAA-approved revisions.STC SA00695SEReplacement of certain Rotomaster and Rayjay scavenge pumpsSTC SA489EAInstallation of ARP Inc. carburetor ice detection systemSTC SA02520ATInstallation of M-20 Oil Separator, model 600-WP.STC SA8887SW-DInstallation of S-TEC System 55 two axis automatic flight guidance system, ST-557.STC SA7092NMInstallation of an engine Electronic Digital Tachometer Horizon Model P-1000, P/N P100200- .STC SA09470SCInstallation of Starter Indicator light system.STC SA00930SEInstallation of vortex generators on the wing and flap surfaces in accordance with Drawing Package MA2153, Revision IR, dated January 26, 2001, and Installation Manual MA2154, Revision IR, dated May 29, 2001, or later FAA approved revision of either of these documents.STC SA01279NYInstallation of a wing reinforcement kit.STC SA2687NMInstallation of Truboplus/ Electronics Int'l gauges and switches.STC SA71GLInstallation of air filters
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