N797AL
STCs that may be installed · 199
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 = '302198B'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '52035')
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 = '302198B'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '52035')
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 · Mcdonnell Douglas DC-8-63
STC SA2622NMInstallation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101)STC SA3180NMInstallation of Spacelite 8 Interior Retrofit Kits.STC SA3169NMInstallation of floor proximity emergency escape marking system.STC SA3166SOInstallation of an Expanded parameters Digital Flight Data RecorderSTC ST01078ATInstallation of an expanded, 17-parameters, Allied Signal, or Loral-Fairchild, Digital Flight Data Recorder (DFDR)STC ST01174CHInstallation of UPS Aviation Technologies ADS-B provisions and Honeywell Mode-S System.STC ST01936WIInstallation of LED lightsSTC SA2534SW-DReplacement of Switch assembly Int'l Inflatables Co. P/N 68748, with DME Corp. P/N L-140 in emergency evacuation slide lighting system.STC SA2539SW-DReplacement of light assembly, International Inflatables Co. P/N68555-1 with DME Corp. EL-104, EL-104A, and EL-104B in emergency slide lighting system.STC SA863EAIncorporation of DME Corporation emergency evacuation slide lighting systemSTC ST02580ATLithium cell battery pack to replace currently approved alkaline battery pack used in escape slide emergency light system.STC SA5720NMInstallation of the Mark VII ground proximity and windshear warning system.STC SA502NEInstallation of Inflight Services Video System, for Hawaiian Air.STC SA3421NMInstallation of Hughes-Avicom video entertainment system.STC SA1066NMInstallation of a Video Projection SystemSTC ST00347BOModification to upgrade a BendixKing CAS 67A TCAS II system to CAS 67B TCAS II Change 7.1STC SA3140SOInstallation of a replacement coalescer filter, P/N 22D10 or 22D10-2.STC ST00881WI-DModification of a TCAS II system installation to Change 7.0 or Change 7.1STC SA7076NMInstallation of Stretcher Carrier.STC ST01067LAInstallation of Litton LTR-97 fiber optic gyro systems.STC ST01467LA-DInstallation of Universal Avionics Terrain Avoidance Warning System and MFD-640 Multi Function Display(s).STC ST01468LA-DInstallation of Universal Avionics Flight Management System.STC SA1511GLInstallation of Type "C" containers.STC SA1775GLIncorporate maximum permissible quick turn-around landing weight (flaps 35º)STC SA1794GLIncorporate anti-skid system inoperative and/or auto-ground spoilers inoperative landing field length data for Operations using 35° landing flaps.STC SA2303SOInstallation of standard equipment as as required by AC120-29.STC ST00670CHInstallation of single or dual II Morrow, Apollo 2101/2102 GPS Navigation Management Computer Systems.STC SA1421GLInstallation of Supplemental Electric Heater.STC SA1462GLInstallation of ABX Cargo Handling System.STC SA3496NMInstallation of ABX-C Cargo Container assemblySTC ST369CHApprove autopilot and/or flight director coupled approach with 35 landing flap selection.STC SA7729SWInstallation of digital fuel quantity indicators, fuel totalizer, and capacitive fuel compensator units.STC SA2304SOInstallation of dual Bendix EFS-10 with MFD and dual Collins FDS-85 system.STC SA2306SOInstallation of the Sperry directional gyro system.STC SA2307SOInstallation of the third vertical gyro system.STC SA2308SOInstallation of the dual IDC Series 35900 mach/airspeed indicator system.STC SA2310SOInstallation of the dual Kollsman/IDC 28007-427 encoding altimeters with standby altimeter system.STC SA2313SOInstallation of the Bendix RDR-4A radar system.STC SA2318SOInstallation of the door warning system.STC SA1360GLInstall Parker Hannifin Freon Air Conditioning System.STC SA1616GLInstallation of Ametek digital fuel flow/fuel used indicator P/N10250N010F01.STC SA1733GLInstallation of Vickers PV3-160-4B hydraulic pump.STC SA1761GLInstallation of Kollsman P/N 35900-A2284 Mach airspeed indicator.STC SA2320SOInstallation of the Fairchild F-800 digital flight data recorder system.STC ST117CHInstallation of expanded parameters.STC ST125CHInstallation of JET model AI-330 attitude indicator.STC ST53CHReplacement of McD PN 4642526 compressor check valve flapper assembly with ABX Air, PN A04574.STC SA2827WE-DInstallation of Collins FPC-75 part number 622-2615-012 or 622-2615-212 Ground Proximity Warning System Computer in conformance with United Airlines DAS-1-WE Approved Master List of drawings and documents for STC No. SA2827WE-D dated February 26, 1979 or later approved revisions. An alternate approved configuration consists of part number 622-2615-011 Rev. N or part number 622-2615-211 GPWS computer and a part number 622-2668-011 Barometric Altitude Computer installed in conformance with DAS-1-WE Approved Master List of drawings and related documents or later FAA approved revision (Continued on page 3.)STC SA4-9181. Aircraft wiring in accordance with Douglas Aircraft Co. Service Change #17 (UAL COA-0-1456) to provide an operational Aircraft Flight Data Rrecorder conforming to CAR Amendment 40-6, paragraph 40.208 with the following additions to assure recording of data during takeoff and landing roll:
a. Relay to provide automatic start of recording when nose landing gear reaches airborne condition on takeoff.
b. Time delay relay to turn off recorder one minute after nose landing gear reaches "on ground" condition, on landing.
c. Installation of standard toggle switch on Systems Engineer's Console, to permit Second Officer to turn on recorder at start of takeoff run.
2. Install Waste King Flight Data Recorder #5424, TSO-C51.STC SA611WEInterior configuration - 120 passenger single class 5-abreast seating per United Air Lines approved drawing lists: COA 2-2083 (Sheet #1 Revision February 17, 1964, Sheet #2 dated December 4, 1963, Sheet #3 Revision dated February 27, 1964 and, COA 2-2099 Revision dated December 17, 1963).