Aero Commander 680-E
STCs that may be installed · 194
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 ('0141604')
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 ('0141604')
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 SA1089SWInstallation of 59 gallon wing auxiliary fuel tank according to Drawing List 60400 dated 10/5/69, revised 5/1/70.STC SA01158WIInstallation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.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 SA00770SEInstallation of two (2) Hartzel Model HC-B3Z20-2A/10151(B)-8(R), or two (2) HC-93Z20-2C/10151(B)-8(R) propellers on the above model aircraft, per James Metzger s Document JM0001, Revision A, dated January 10, 2000, or later FAA approved revision.STC ST02547ATInstallation of a voice alert system.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 SA489EAInstallation of ARP Inc. carburetor ice detection systemSTC SA00481DEInstallation of an Aircraft Noise Control (ANC) System.STC SA8597SWInstallation of P/N DF062-507, upper center fuel tank bladder cells as a replacement for original bladder P/N 5630062-507.STC SA02520ATInstallation of M-20 Oil Separator, model 600-WP.STC SA29SWAuxiliary outboard fuel tank.STC SA00804SEInstallation of an engine failure indicator system, also referred to as a 'low Thrust Detector system.'STC SA71GLInstallation of air filtersSTC SA1017EAInstallation of vertical tail floodlightsSTC SA2-884Installation of Collins AP-102 autopilot.STC SA1381GLReplace standard wing tip assembly with winglet tip assembly.STC SA1565GLInstallation of flap gap wing fairings.STC SA01444ATInstallation of an Enviro Systems AirConditioner.STC SA199SWInstallation of four auxiliary fuel cells in each outer wing panel between stations 127 and 163.STC SA01820ATInstallation of Exhaust Deflectors.STC SA1007NWInstallation of a low thrust detector system.STC SA157NEInstallation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent.STC SA8386SW-DInstallation of S-TEC yaw damper system, Model ST-529.STC SA09163AC-DInstallation of S-TEC System 40/50 single and two axis automatic flight guidance systems, Model ST-634-40/50.STC SA8385SW-DInstallation of S-TEC System 65 two axis automatic flight guidance system, Model ST-528.STC SA1-385Installation of B.F. Goodrich lightweight reservoir type pneumatic de-icing system.STC SA1-520Electrothermal propeller deicing system.STC SA102EAPump type pneumatic deicing system.STC SA132EAInstall electrothermal propeller deicing system.STC SA00061LAInstallation of JPI digital tachometer.STC SA1-552Pesco 2 P-R400-BRD fuel pumps.STC SA2903SWInstallation of wing flap gap seals.STC SA5656NMInstallation of burglar alarm system.STC SA2844CEInstallation of a plastic cap enclosure over the anti-collision strobe light system.STC SA3477WEReplacement installation of tail cone assembly.STC SA3493WEReplacement installation of vertical tip assembly.STC SA585SWInstallation of Nose Cone.STC SA660WEInstallation of HRD-type fire extinguishing system. (AND STC SA111WE)STC SA458EAInstallation of nose cap radome kit No. 3066X-R.STC SA290GLInstall Cleveland conversion kit No. 199-74 on listed models which use MIL-H-5606 brake fluid (red oil) or kit No. 199-74A on listed models which use Skydrol brake fluid (nonpetroleum base).STC SA2386SWInstallation of S.A.F.E., EGT, CHT Systems.STC SA2569WEInstallation of battery temperature monitor system.STC SA863SWModified instrument panel.STC SA321EAInstall wheels P/N 301174, P/N's2-993 and/or 2-1107.STC SA584WEInstallation of oil filter assemblies.STC SA1675WEInstallation of exhaust gas temperature monitoring systems EGT-2.STC SA1332SWModification of fuselage for camera and navigation sight installationSTC SA1125SWModification of fuselage for installation of aerial survey camera and navigation sight
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