N989AF
STCs that may be installed · 92
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 = '7860107'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '30148')
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 = '7860107'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '30148')
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 · Saab SAAB 340B
STC ST01305WI-DModification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision.STC ST12461IBInstallation of Cockpit Voice Recorder with optional RIPS UpgradeSTC ST00885LAInstallation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.STC ST03875NYInstallation of interior placards, signs and markingsSTC SA1673GLInstallation of landing gear harnesses.STC SA2622NMInstallation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101)STC ST03885ATInstallation of an Avionica, Inc. avCM Cellular ModuleSTC ST04751NYInstallation of Provisions for Underwing StoresSTC ST02472ATInstallation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIIISTC ST00215IBInstallation of saf-Tglo ECO Photoluminescent Aisle Path Marking SystemsSTC ST03424CHCertification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D TranspondersSTC ST04575ATInstallation of the Rockwell Collins ALT-1000+/ -4000+ with 5G FilteringSTC ST04562NYInstallation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking SystemsSTC ST00098IBIntroduction of ADS-B OutSTC ST01436WIProvides substitute floor panels in the cabin and cargo compartments.STC ST01701WIInstallation of a Collins HF-220 High Frequency Communication SystemSTC ST01894WIPassenger to Cargo Service Conversion via the installation of a Class E Cargo Compartment.STC ST03497ATInstallation of a Automatic Dependent Surveillance-Broadcast (ADS-B) System (data broadcast only, no cockpit display).STC ST03548ATInstallation of a Redundant GPS Signal to the Universal UNS-1K Flight Management System and associated hardwareSTC ST04683NYInstallation of an upgrade of Universal (UNS) Flight Management System, LPV monitor and/or an
upgrade of TDR-94D for MODE S and ADS-B outSTC ST04671NYDual Garmin GTN-650 Xi GPS/NAV/COMMsSTC SA9075SC-DRecore of Hamilton Standard Heat Exchangers 779215-1 and 779215-2 for installation on the SAAB SF340A and 340B in accordance with Honeywell LORI Sealed Drawing List SDL3400-1, Revision B, dated 10 October 2005 or later FAA approved revision.STC ST04177ATInstallation of a Talon Aerospace LED Replacement General Purpose LampsSTC ST03687NYInstallation of Alternate Cargo Net LocationSTC ST00146WI-DInstallation of Bendix/King CAS 66A TCAS I System.STC ST00224WI-DInstallation of Bendix/King CAS 67A TCAS II System.STC ST03688NYConversion of the main passenger cabin to a class E cargo compartment for the carriage of freight and change to the location of rapid decompression vents for planned future bulk cargo loading operationsSTC ST02635LAModification to replace the existing Mode S Transponder system with the ACSS NXT-600 Mode S Transponder with ADS-B OutSTC ST04467ATInstallation of the dual Becker Avionics BXT6513-(000) ADS-BSTC SA04179NYInstallation of the Special Mission Equipment ProvisionsSTC ST04179NYInstallation of the Special Mission Equipment ProvisionsSTC ST04012NYInstallation of the Garmin GTX-3000 Automatic Dependent Surveillance-Broadcast
(ADS-B) Out SystemSTC ST04340NYInstallation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0STC ST09518SCInstallation of cabin and cargo floorboards.STC ST03242NYReplacement of certain Goodrich pneumatic deicer bootsSTC ST02499AKApproval of the Thomas Global Systems TFD8601Active Matrix Liquid Crystal Display installedSTC ST04136CHInstallation of a TFD-8601 EFIS (Electronic Flight Instrument System) DisplaySTC ST02530SEInstallation of Securaplane Sealed Lead Acid BatteriesSTC ST03776NYModification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II)STC ST00881WI-DModification of a TCAS II system installation to Change 7.0 or Change 7.1STC ST01254ATEnlarge Class 'C' cargo compartment by relocating cargo bay bulkhead forward to F.S. 594.1.STC ST04238ATUpgrade of Honeywell Traffic Collision Avoidance Systems II (TCAS II) Processor Software from TCAS II Version 7.0 to TCAS II Version 7.1STC ST02516LAReplacement of existing ELT with ACK E-04 ELT Beacon and Sensor Systems S65-1231 ELT AntennaSTC ST01712WIModification of a Rockwell Collins, Inc. AHC-85( ) (AHRS) installationSTC ST03262NYInstallation of Quality Aircraft Interiors Oxygen Cylinder Restraint System (OCRS), P/N OCRS-1730-QAI, Models A & DSTC ST01474WI-DModication of a Rockwell Collins Weather Radar System installation.STC ST03135NYActivation of Free Directional Gyro ModeSTC SA2470CEInstallation of B&D Instruments & Avionics, Inc. Electronic Propeller Gear Box Oil Pressure/Temperature Indicator. Data required: (1) for the Model SF340A, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7330-003-011, dated January 23, 1989, or later FAA Approved revision; (2) for the Model SF340B, B&D Instruments and Avionics, Inc. Installation Manual Part No. 7330-003-011, Revision B, dated August 29, 1989, or later FAA Approved revision; and (3) copy of this certificate.STC SA2471CEInstallation of B&D Instruments & Avionics, Inc. Electronic Engine Oil Pressure/Temperature Indicator. Data required: (1) for the Model SF340A, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7380-003-024, dated January 23, 1989, or later FAA Approved revision; (2) for the Model SF340B, B&D Instruments and Avionics, Inc. Installation Manual Part No. 7380-003-024, dated August 29, 1989, or later FAA Approved revision; and (3) copy of this certificate.STC SA2472CEInstallation of B&D Instruments & Avionics, Inc. Electronic Gas Generator Speed Indicator. Data required: (1) for the Model SF340A, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7320-003-011, dated January 23, 1989, or later FAA Approved revision; for the Model SF340B, B&D Instruments and Avionics, Inc. Installation Manual Part No. 7320-003-011, Revision B, dated August 29, 1989, or later FAA Approved revision; (2) for the SF340A or SF340B, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7321-004-011 dated September 12, 1989, or later FAA Approved revision; and (3) copy of this certificate.