N1889P
STCs that may be installed · 406
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 = '7101806'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '41508')
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 = '7101806'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '41508')
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 · Piper PA-18S
STC SA1-155McCauley fixed pitch MET-L-PROP1A170/GM7448 with Lycoming O-290-D2 engine.STC SA1-156McCauley fixed pitch MET-L-PROP1A170/GM7446 with Lycoming O-290-D engine.STC SA1-32McCauley fixed pitch MET-L-PROP1A170/GM7450 and 1A170/GM7452 with Lycoming O-290-D2 engine.STC SA1-41McCauley fixed pitch MET-L-PROP1A170/GM7450, 1A170/GM7452 and1A170/GM7454 propellers with Lycoming O-320-A1A engine.STC SA1-59McCauley fixed pitch MET-L-PROP1A170/GM7448 and 1A170/GM7450 with Lycoming O-290-D engine.STC SA01860NYInstallation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.STC SA02007AKInstallation of main landing gear long step no. 3195.STC ST01920CHInstallation of modified Grumman AA-5B exhaust system assembly, P/N SUTN201 or P/N SUTN301. Only for those PA-18 series aircraft equipped with Lycoming O-320 or O-360 series engines, whether by original factory installation or by STC.STC SA4008NMInstallation of removable panels on the battery box slides.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 SA02236AKFabrication and installation of F. Atlee Dodge Heavy Duty Standard Length Main Landing Gear, P/N 3225A, in accordance with F. Atlee Dodge Master Data List No. 3225-1.5, Revision: None dated March 14, 2005, or later FAA approved revisions.STC SA02087CHInstallation of MT-Propeller model MTV-15-C/200-50 or MTV-15-B/210-58 constant speed propellerSTC SA02234AKInstallation of a high Pressure Brake Master Cylinder assembly DCA1248-1260.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 SA02655ATInstallation of JAARS Model F5K Automatic Flight Following System (AFFS) in Helio H-295 type aircraft.STC SA590ALInstall extended baggage compartment.STC SA5-65Installation of Goodyear 25 x 11.0 - 4 Type IV tires with tubes on Goodrich Model 841696 4-inch wheels on main landing gear, using Alaskan Aircraft Equipment Supply Model A-1 rim adaptersSTC SA01944CHModify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index, per ASTM Specification D-439 or D-4818 of any volatility class, A through E, or 82UL AVGAS per ASTM D-6227.STC SA767GLSuperseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index.STC SA8075SWInstallation of fiberglass covering. (M-62 SERIES PT-19) (G-73 SCHWEIZER)STC SA2167NMInstallation of the Precise Flight stand-by vacuum system (SVS).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 SA1008WEInstallation of Poly-Fiber covering material.STC SA02204AKFabrication of replacement engine exhaust system assembly. Limited to airplanes equipped with FAA approved installations of Textron Lycoming O-320 model series engines having a compression ratio of 8.5:1 and a rated power of 160 hp for all operations.STC SA489EAInstallation of ARP Inc. carburetor ice detection systemSTC SA1064GLSurrendered and incorporated into STC SA00478CH.STC SA02520ATInstallation of M-20 Oil Separator, model 600-WP.STC SA02189AKFabrication and installation of p/n 3344 main landing gear safety cable kit for 3-inch extended main landing gear. Applies only to planes modified by installation of 3-inch extended main landing gear per STCs SA02152AK or SA02175AK.STC SA02170AKInstallation of McCauley propellers, Models 1A175-GM8241 through 1A175-GM8244.STC SA2687NMInstallation of Truboplus/ Electronics Int'l gauges and switches.STC SA159CEInstallation of Pee-Kay Model 1800 floats.STC SA71GLInstallation of air filtersSTC SA02156AKFabrication and installation of a lightweight battery rack under pilot's seat.STC SA4077NMInstallation of replacement aft fuselage section.STC SA4095NMReplacement fuselage assembly with optional features.STC SA02152AKFabrication and installation of F. Atlee Dodge 3-inch extended Main Landing Gear, P/N 3284.STC SA11RMInstallation of modified axles, wheels and brakesSTC SA00083DEInstallation of an additional cross tube to the upper cabin structure.STC SA00116DEInstallation of Replacement Vertical Stabilizer.STC SA00142DEInstallation of a replacement horizontal stabilizer.STC SA00150DEInstallation of Replacement Elevator Frame.STC SA00151DEInstallation of replacement Rudder Frame.STC SA02138AKFabrication and installation of a light weight battery and bracket under the rear seat.STC SA1526NMInstallation of Piper landing gear vee assemblies, P/Ns 10033-5, 10033-6 with P/Ns J-10033-( ).STC SA1544NMInstallation of cabane vee.STC SA1548NMInstallation of hydra strut.STC SA1554NMInstallation of Jensen Aircraft fuel valve plug No. 011-2.