Cessna 180
STCs that may be installed · 622
In force first, then newest. The registry doesn’t record which STCs an aircraft has.
Query with SQL
duckdb -csv -c "SELECT s.stc_number, s.description, s.holder, s.status, s.status_date, m.matched_model
FROM (
SELECT stc_number, min(matched_model) AS matched_model
FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_stc.parquet'
WHERE aircraft_model_code IN ('2072602')
GROUP BY stc_number
) m JOIN 'https://openairdocs.org/data/latest/faa_stc.parquet' s USING (stc_number)
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, m.matched_model
FROM (
SELECT stc_number, min(matched_model) AS matched_model
FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_stc.parquet'
WHERE aircraft_model_code IN ('2072602')
GROUP BY stc_number
) m JOIN 'https://openairdocs.org/data/latest/faa_stc.parquet' s USING (stc_number)
ORDER BY 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.
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 SA01436SECockpit sunvisor retrofit kit.STC SA00796SEInstallation of vortex generators on the wings and tail surfaces of the above model aircraftSTC SA777NEInstallation of Cessna louvers.STC SA00144WIInstallation of 18 gallon nylon auxiliary fuel tanks on airplanes equipped with standard range 64 gallon capacity bladder tank or 62 gallon fiberglass fuel tanks. (180K thru S/N 18053000)STC SA2346CEInstallation of standard range 56 or 62 gallon capacity or long range77 gallon capacity fiberglass fuel tanks in place of original bladder fuel tanks. (180K THRU S/N 18053000 AND LATER; AIRPLANES ORIGINALLLY EQUIPPED WITH BLADDER FUEL TANKS)STC SA2382CEInstallation of fuel caps.STC SA02839ATModification of the main landing gear bulkhead to improve static strength and fatigue characteristics.STC 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 SA695GLSuperseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index.STC SA02795ATInstallation of a PXE7300SR, In-Flight Entertainment SystemSTC SA5-12Installation of canvas hammock seat.STC SA00424SEInstallation of Precise Flight Model 100(electric) Speedbrake System.STC SA2106NMInstallation of Precise Flight Speedbrake System.STC SA2164NMInstallation of the Precise Flight standby vacuum system (SVS).STC SA10126SCInstallation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision.STC SA01077SEInstallation of fluoropolymer film.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 SA2382NMInstallation of Aileron and Flap Gap Seals.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 SA4-394Installation of George M. Adams DGA-2000 wheels and Bodell Mfg Model BMI-252 brakes.STC SA561WE12.7-gallon auxiliary fuel tank.STC ST02547ATInstallation of a voice alert system.STC SA1-611Install 300 series dry vacuum pump conversion kits.STC SA3692NMCockpit sun visor installation.STC SA8950SWInstallation of a McCauley propeller model no. C2A34C204/90DBC-8, Spinner P/N 0752637K200 and Teledyne Continental model O-470-U-TS engine.STC SA00164BOInstallation of a Continental O-470-R engine with a McCauley 2A36C, 2A34C, 2A34C66 or 2A34C203 propeller.STC SA01163SEInstallation of ARNAV Systems RCOM-100 Globalstar Satellite Telephone per ARNAV Systems, Inc., RCOM-100 Installation Guide, Part Number 570-8050BSTC SA00419NYInstallation of cockpit utility light.STC SA489EAInstallation of ARP Inc. carburetor ice detection systemSTC SA00023SEInstallation of modified control yoke and instrument panel.STC SA10070SCInstallation of Hartzell 3-bladed propeller.STC SA10082SCInstallation of Texas Skyways engine mount.STC SA2577CEInstallation of main fuel cell bladders as replacements for original bladders. (T210 SERIES SPECIFIC SERIAL NUMBERS AFFECTED)STC SA1005SCInstallation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate.STC SA09018SCInstallation of modified engine and propeller systemSTC SA02520ATInstallation of M-20 Oil Separator, model 600-WP.STC SA00709LAInstallation of control wheel. Includes provisions only for a push-to-talk (PTT) switch. Separate FAA approval of PTT switch is required.STC SA5824NMInstallation of an engine electronic digital tachometer, Model P-1000.STC SA2832SOInstallation of a combination radio/throttle/gust lock.STC SA2-1178Replacement of right front seat with stretcher.STC SA09964SCInstallation of engine mount heat shields.STC SA1-426Auxiliary seat in baggage compartment.STC SA02387ATInstallation of engine cowling and firewall fasteners.STC SA261NWInstallation of automatic flagman Model No 5STC SA09470SCInstallation of Starter Indicator light system.STC SA00496SEInstallation of Oregon Aircraft Design Engine Mount Heat Shields.STC SA02165AKInstallation of ARNAV Systems, Inc., MFD 5200 CDU, p/n 453-2550; MFD 5115 RPU, P/N 453-2530-08, DR-100 Receiver, P/N 453-0160; and EMM 35 Engine Trend Monitor, P/N 453-5030.STC SA2687NMInstallation of Truboplus/ Electronics Int'l gauges and switches.
Back to Cessna 180