N78708
STCs that may be installed · 367
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 = '7101202'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '41505')
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 = '7101202'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '41505')
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-12
STC SA02267AKInstallation of a Lycoming O-360-A2A and a McCauley 1A200-FA8242 fixed pitch propellerSTC SA02316AKInstallation of 8.50-6 and 8.50-10 tiresSTC 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 SA02171AKInstallation of a 24-gallon right wing fuel tank, P/N DC18049-24G-25R and 24-gallon left wing fuel tank, P/N DC10849-24G-32L.STC SA4005NMPrecise Flight Inc. Pulselite Control SystemSTC SA02299AKInstallation of a replacement fuel selector valve.STC SA02295AKInstallation of a high capacity fule gascolator assembly.STC SA10EAMetal covering of fabric wings according to Drawing #5P-10005, dated November 17, 1961 and Change Notice #1, dated January 6 15, 1962 and optional metallizing of aileronsSTC SA01516SEReplacement of the Scott Master Brake Cylinder (Non-Vented Diamphram type) with a Steve s Aircraft Model SA6-01 Master Cylinder with a vented reservoir.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 SA01063CHInstallation of a Scott Model 3200 Tail Wheel with the AESI #T.S.05P Tail Spring.STC SA1-373Installation of Lycoming O-290-D(125 hp) or O-290-D2 (135 hp) engine; Sensenich M-74DM propeller; PA-18 engine baffles; Harrison#AP13SJ03-01 oil cooler.STC SA3633NMFabrication of North River Avia. Model 8400 brake booster assembly, and modify Scott Avia. Model B-711 brake master cylinders.STC SA02228AKInstallation of Leading Edge Exhaust Systems, LLC LEESPA12 ESA-180, LEESPA12ESA-SM, and LEESPA12ESA-LM Exhaust Systems.STC SA4-977Installation of Fiberglass rudder post mount for either Grimes or Whelen WRM rotating beacons.STC SA00680SEInstallation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.STC SA00132SEFabrication of F. Atlee Dodge aft fuselage weld-on fittings for the mounting of Edo Model 89-2000 floats.STC SA01553SEInstallation of a structural and systems modifications.STC SA01158WIInstallation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.STC 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 SA01104CHInstallation of Swing Type Engine Mount.STC SA01074CHInstallation of Air-Energy Service Inc. Leading Edge, Part Number AESI #1511.STC SA01412SEInstallation of Piper PA-18 rudder and trim systemSTC 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 SA900GLSuperseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index.STC SA02115AKFabrication and installation of 30.5 gallon wing fuel tank sight gages.STC SA5781NMInstallation of Model 3140-51630.5 gallon wing fuel tanks.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 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 SA1008WEInstallation of Poly-Fiber covering material.STC SA01155SEInstall a Lycoming O-360-A4M engine and McCauley 1A200/FA propellerSTC SA489EAInstallation of ARP Inc. carburetor ice detection systemSTC SA02195AKInstallation of Lycoming O-360-A2A engine, McCauley 1A200/FA8242 propeller, custin engine mount and pressure cowling. Eligible for installation on serial number Piper PA-12, serial number 12-572 ONLY.STC SA1052GLSurrendered and incorporated into STC SA00478CH.STC SA1424GLSurrendered and incorporated into STC SA241CH.STC SA02520ATInstallation of M-20 Oil Separator, model 600-WP.STC SA00932SEInstallation of the Stewart wing tip assemblySTC SA02188AKFabrication and installation of p/n 3284 three-inch extended PA-18 type main landing gear, together with p/n 3164-4 extended shock strut assemblies. Applies to those models previously modified by SA148AL, SA543AL, or SA669AL, or for Piper PA-12S models, planes must have been converted to landplane configuration.STC SA02190AKFabrication and installation of p/n 3344A main landing gear safety cable kit for 3-inch extended main landing gear. Applies only to those aircraft previously modified by STCs such as SA02188AK.STC SA09470SCInstallation of Starter Indicator light system.STC SA02170AKInstallation of McCauley propellers, Models 1A175-GM8241 through 1A175-GM8244.STC SA2687NMInstallation of Truboplus/ Electronics Int'l gauges and switches.STC SA71GLInstallation of air filters