N151FL
STCs that may be installed · 208
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 = '242270A'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '03004')
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 = '242270A'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '03004')
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 · Convair 340
STC SA2622NMInstallation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101)STC ST04672CHInstallation of FreeFlight Systems RA-5500 Radio Altimeter systemSTC ST03424CHCertification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D TranspondersSTC SA01967WIUse of GAMI G100UL High Octane Unleaded AvgasSTC SA863EAIncorporation of DME Corporation emergency evacuation slide lighting systemSTC SA3275SOInstallation of a CAS-81 TCAS II system.STC SA3276SOInstallation of a dual TRA-67 mode S transponder system.STC ST00559ATInstallation of RDR-4B Weather Radar/Windshear SystemSTC ST00771SEInstallation of the MK VII Enhanced Ground Proximity Warning System (EGPWS)(Tracor (convair) 340-31)STC ST01737SE: Installation of the RDR-4000 Doppler Radar System in accordance with Master Drawing List 756-0174-001, Revision (E), dated August 20, 2006, or later FAA approved revisions.STC ST01629WI-DCONFIURATION 1
Installation of a Honeywell TPA-100B TCAS II Processor with Change 7.1 and Goodrich Electronic Flight Bag System with In-Trail Procedures Activation in accordance with Honeywell Master Drawing List 756-0234-001, revision A, dated June 3, 2011 or later FAA approved revision.
CONFIGURATION 2
Installation of a Honeywell TPA-100B TCAS II Processor with Change 7.1 in accordance with Honeywell Master Drawing List 756-0234-001, revision A, dated June 3, 2011 or later FAA approved revision.STC ST00442NYInstallation of Kalowna Flightcraft cargo compartment conversion.STC ST00870NYInstallation of a Fruehauf Floor and Cargo Net.STC ST04220CHInstallation of a FreeFlight 2101 I/O Approach Plus GPS Navigation SystemSTC ST03410CHModification from a dual autopilot to a single autopilot configuration, by installing a configuration adapter in place of the existing FZ-450STC ST03006ATInstallation of the Honeywell MK VI Enhanced Ground Proximity Warning System (EGPWS) to a Kelowna Flightcraft (Convair) Model 340/440STC ST03005ATInstallation of the Collins Traffic Collision Avoidance System 4000 (TCAS II)STC SA3-419General interior floor plan arrangement.STC SA3-420Main cabin seat installations(including divan and seat belts).STC SA3-421Installation of auxiliary power unit.STC SA3-486Interior cabin configuration - general floor plan (20 passenger configuration).STC SA3-487Janitrol heater installation(100,000 BTU).STC SA3-488Installation of radar nose, Bendix ANT-1B antenna and pitot modification (including Radome fabrication).STC ST02839CHReduction of payload to 7500 lbs. Installation of placard per Rezich & Rezich drawing RR002STC SA5002NMInstallation of provisions for side looking radar.STC ST01824NYInstallation of Northern Airborne Technology Satphone.STC SA1992NMInstallation of a de-icing system on Rolls Royce RK45524A engine inlet cowl.STC SA2220NMThis modification splits the nose fairing assembly P/N 906425-201, Rev. M P/N 9064135-1, Rev. A, and P/N 1914-1, Rev. C. (440 MILITARY C-131E MODIFIED IN ACCORDANCE WITH STC SA4-1100)STC SA3105NMInstallation of a de-icing system externally on the Dowty Rotol Part Number (C) 4CM/71 Propeller Spinner.STC ST01798LAInstallation of a flight deck doorSTC SA125CEInstallation of Hoskins Supplemental Model B of F High Intensity Wing Tip Lights, Model C or 30-0329-3 Dual Tail Light, with or without Model 2 High Intensity Fuselage Lights.STC SA379CEInstallation of Hoskins Twilighter MK V High Intensity Aircraft Lighting System. This is a Supplemental Condenser Discharge (Strobe) Light System, consisting of five (5) Light Units and a Power Supply.STC ST03004NYInstallation of new MIL-C-5015 connectors at the wing to fuselage interface must be in accordance with Kelowna Flightcraft Ltd.Master Drawing List K116-00002 Revision NC, dated March 20, 2009 or later Transport Canada approved revision.STC ST02737NYThe installation of new annunciator hoodSTC SA1097SOInstallation of two (2) double seats to increase passenger configuration from 44 to 48.STC SA1248SOInstallation of single point seat belt and shoulder harness restraint systems for the pilot's, co-pilot's, forward observer's and flight attendant's seat assemblies.STC ST1035SOInstallation of a combination passenger/cargo interior to include all cargo, 44 passenger/cargo, 10 passenger/cargo, and 6 passenger/cargo configurations. (340 MODIFIED IN ACCORDANCE WITH STC SA4-1100) (440 MILITARY C-131E MODIFIED IN ACCORDANCE WITH ST C SA4-1100STC SA6088NMConversion of the 6A6 Type Certified Aircraft into a Model CV 5800 by installation of Allison 501-D22G Engines per STC SA4-1100, Hamilton Standard Propellers per STC SA1825NM and lengthening the fuselage 14 ft. 3.0 inches with all design changes.STC ST02671NYPalletized Cargo InteriorSTC ST02591CHInstallation of dual Honeywell TRA-45A TDU/Radio Altimeter IndicatorsSTC ST02488NYThe installation of Honeywell TCAS II System.STC ST02489NYThe installation of Honeywell Mark VI Enhanced Ground Proximity Warning SystemSTC ST03062ATInstallation of a single Sandel P/N ST3400-001 Terrain Awareness and Warning System with Remote Magnetic Indicator (TAWS/RMI) in accordance with DC Aerospace Report No. MDL-2524, Revision A, dated March 4, 2005 or later FAA
approved revision.STC ST00525WI-DModification of Collins 618M-4 VHF COMM Receiver Transmitter Installation to a 618M-5 VHF COMM Receiver Transmitter installation with either a Gables G7406-02 or Avtech 7522-1-2 VHF COMM Receiver Transmitter Control Series using with Collins Installation Instructions as listed on AML No. ST00525WI-D, or later FAA approved revisions.STC SA7772SWReplacement of existing torquemeters.STC ST01901NYModification of Propeller Feathering System.STC ST02782ATModification of a cargo restraint system in accordance with DER Services Master Document List No. MDL-2003-228-1, dated December 1, 2003, or later FAA approved revision.STC ST00976LAInstallation of a 2100 US Gallon Retardant Tank system. Approval applies to basic aircraft of specified models modified with STC SA4-1100, installation of Allison turboprop engines; STC SA3574WE, installation of gross weight increase kit; and STC SA3294WE, installation of max zero fuel weight increase kit.STC SA1988SOModify cabin pressurization system using General Air Services, Inc., drawing no. CV60-014 dtd 9/2/86, or later FAA approved revision.STC SA2495SOInstallation of cargo door IAW General Air Services Drawing List, Cargo Door Installation, dtd 1/23/89, or later FAA approved revision..