N8BZ
STCs that may be installed · 175
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do. In force first, then newest.
Query with SQL
duckdb -csv -c "SELECT m.matched_by, s.stc_number, s.description, s.holder, s.status, s.status_date, m.matched_model
FROM (
SELECT stc_number, min(side) AS side, arg_min(matched_by, side) AS matched_by, arg_min(matched_model, side) AS matched_model
FROM (SELECT stc_number, 1 AS side, 'airframe' AS matched_by, matched_model FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_stc.parquet' WHERE aircraft_model_code = '2400108'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '41511')
GROUP BY stc_number
) m JOIN 'https://openairdocs.org/data/latest/faa_stc.parquet' s USING (stc_number)
ORDER BY m.side, 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 m.matched_by, s.stc_number, s.description, s.holder, s.status, s.status_date, m.matched_model
FROM (
SELECT stc_number, min(side) AS side, arg_min(matched_by, side) AS matched_by, arg_min(matched_model, side) AS matched_model
FROM (SELECT stc_number, 1 AS side, 'airframe' AS matched_by, matched_model FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_stc.parquet' WHERE aircraft_model_code = '2400108'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '41511')
GROUP BY stc_number
) m JOIN 'https://openairdocs.org/data/latest/faa_stc.parquet' s USING (stc_number)
ORDER BY m.side, s.status = 'Current' DESC, s.status_date DESC, s.stc_numberRun 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.
Airframe · Consolidated Aeronautics LAKE LA-4-200
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 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 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 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 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 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 SA02520ATInstallation of M-20 Oil Separator, model 600-WP.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 filtersSTC SA09396AC-DInstallation of S-TEC System 30 ALT Altitude Hold System, Model ST-848.STC SA09394AC-DInstallation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems, Model ST-847-20/30.STC SA01224ATInstallation of wheel hub cabs with valve stem access door.STC SA5925NMInstallation of oil pressure/temperature instrument.STC SA5924NMInstallation of RPM instrument.STC SA00288DEInstallation of a Dorsal fin fairing.STC SA00363SEInstallation of main landing gear doors.STC SA01065ATInstallation of glare shield.STC SA00061LAInstallation of JPI digital tachometer.STC SA2628SOReplacement of McCauley disc, P/N D-30804-3, with Appalachian Accessories' stainless steel brake disc, P/N 75-90.STC SA3205SOInstallation of Appalachian stainless steel brake discs.STC SA00215NYInstallation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system.STC SA08997AC-DInstallation of S-TEC System 60 pitch stabilization system, Model ST-581.STC SA2278SOReplacement of Gerdes brake discs, P/N A-1634-B, with Appalachian Accessories' stainless steel brake discs, P/N 75-86.STC SA00462ATReplacement of Appalachian stainless steel brake discs P/N 75-23 with Appalachian steel brake disk part number AA-47.STC SA00216ATInstallation of carbon steel brake discs.STC SA00210ATInstallation of carbon steel brake discs that have melonite surface treatment, P/N AA-90.STC SA5656NMInstallation of burglar alarm system.STC SA7207SW-DInstallation of S-TEC System 40/50 single and two axis automatic flight guidance systems, Model ST-316-40/50.STC SA5926NMInstallation of manifold pressure instrument.STC SA00009NYInstallation of wing leading edge fairing.STC SA00010NYInstallation of induction filter air scoop.STC SA1626NM PAGE 1Installation of Electronics Int'l Digital EGT/CHT Instruments and accessories. (201 Series)STC SA1142SOInstallation of an adjustable trim tab on the rudder.STC SA2350NM PAGE 1Installation of Electronics International Inc digital carburetor/outside air temperature gaugesSTC SA4721NMInstallation of SynCon alarm system.STC SA7206SW-DInstallation of S-TEC System 60 two axis automatic flight guidance system, model ST-315.STC SA4302NMInstallation of Electronics Int'l digital automatic engine analyzer.STC SA3862NM PAGE 1Installation of Electronics International Primary TIT/EGT/CHT instruments, remote switches and associated accessories.STC SA1977SOInstallation of Appalachian Accessories stainless steel brake discs P/N 73-47.