Boeing 727-243

STCs that may be installed · 837

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 ('138408D')
    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.

STC ST09159SCInstallation of Masushita Avionics audio in-flight entertainment system.Panasonic Avionics CorporationSTC SA8760SWInstallation of a Collins TCAS II system.Executive Aircraft Completions LLCSTC SA1350NMInstallation of a 2777 gallon auxiliary fuel system consisting of a 1565 gallon forward tank system in aft cargo compartment. (727-2M7)DTAA IncSTC 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.Rockwell Collins IncSTC ST00572DE-DInstallation of an ARINC Messanger ACARS Modification and an Electronic Flight Bag (EFB) at the Second Officers position.ARINC IncSTC ST01856LAInstallation of Cabin Interior Noise Reduction Kit.Aircraft Technical Development Inc. dba Aerocon Engineering CompanySTC ST01584SEInstallation of ELS/EHS Mode S System Upgrade.Northwest Aerospace Technologies IncSTC ST01333WI-DModification of a Collins Airshow 400 System.Rockwell Collins IncSTC ST01307WI-DModification of a Collins TVI-920/TVI-920D Vertical Speed/TCAS Indicator installationRockwell Collins IncSTC SA1705GLInstall cargo handling system.ABX Air IncorporatedSTC SA1706GLInstallation of Type C containers.ABX Air IncorporatedSTC ST03089ATInstallation of Honeywell MK VII Enhanced Ground Proximity Warning System (EGPWS)Aircraft Engineering & Installation Services IncSTC ST02132CHInstallation of a Honeywell Mark VII Enhanced Ground Proximity Warning System with Terrain Display and Runway Awareness Advisory System (RAAS).Mayday Avionics IncSTC ST03072ATInstallation of a Sandel ST3400 Terrain Awareness Warning SystemJanzAir Consulting ServicesSTC ST03071ATInstallation of Avionics System for Reduced Vertical Separation Minimum (RVSM) Provisions into a Boeing 727-200 aircraft in accordance with Avionics Support Group, Inc Master Drawing List (MDL) No. 23509-MDL Rev A, dated 05/27/04, or later FAA approved revision.Avionics Support Group IncSTC ST00210BOInstallation of Universal Avionics Terrain Awareness Warning System (TAWS).Avionics Group IncSTC SA1303NMInstallation of overhead enclosed compartmentsHeath Tecna Inc.STC SA2042NMInstallation of contemporary enclosed rack interior.Heath Tecna Inc.STC ST10378SCInstallation of a Universal Avionics Systems Multi-Function Display.Aircraft Systems & MfgSTC ST00795ATApproval of maximum zero fuel weight increase (155,000 lbs.) and maximum landing weight increase(164,000 lbs.). Data pertaining to this modification are considered inadequate for duplication in other aircraft.This approval is limited to the installation in the Boeing 727-200, (Serial Number 20938 only).Structural Integrity EngineeringSTC ST01043ATApproval of increased operating weights.Structural Integrity EngineeringSTC ST03011ATInstallation of Sandel ST3400 Terrain Awareness and Warning System (TAWS)D C Aerospace · Lists 727 SeriesSTC ST00053BOInstallation of a Simmonds Precision Products fuel quantity indicating system incorporating a volumetric top-off function.Simmonds Precision Products IncSTC ST10279SCInstallation of Avtech Display Switching Unit with a Honeywell EGPWS in accordance with Aircraft Systems and Manufacturing Top Drawing List 5644-0001-00, Revision B, dated September 1, 2004, or later FAA approved revision. FAA approved Airplane Flight Manual Supplement Document No. 5644-2160-00, Revision I.R., dated September 2, 2004, is required.Aircraft Systems & MfgSTC ST01946NYCockpit voice recorder replacement with Universal CVR 30B or CVR120.MidCanada Mod CenterSTC ST00903NYInstallation of 100-gallon supplemental potable water tank, plumbing and water sterilization system.PATS Aircraft LLCSTC ST01423NYInstallation of one MagnaStar C-2000 Terrestrial Telephone System and three 60Hz Avionics Frequency Converters. Approved for 727-200 serial number 21474.PATS Aircraft LLCSTC ST02509ATInstallation of an executive passenger cabin interior in accordance with Jormac Aerospace Master Drawing List No.HOR1-MDL-000, Revision B, dated May 8, 2002, or later FAA approved revision. Limited to installation on serial number 21474 ONLY.PATS Aircraft LLCSTC ST00971LAInstallation of an Atlas Standard Oven and Coffee Maker and Modifications.B/E Aerospace Inc.STC ST00770LAIncreased aircraft main deck cargo floor capacity between Fuselage Stations 740 to 950.Structural Integrity EngineeringSTC ST02846ATOne time installation of the Honeywell EDZ-805 Electronic Flight Instrument (EFI) System on Boeing 727-212, serial number 21945, in accordance with Jossair Engineering Report 1452MD01, Revision D, dated April 21, 2004, Master Document List and Compliance Check List- Installation of a Honeywell EDZ-805 Electronic Flight Instrument (EFI) System.Jossair CompanySTC ST02847ATOne time installation of the Honeywell P880 Primus Radar System and LSZ-850 Lightning Strike Sensor System on Boeing 727-212, serial number 21945Jossair CompanySTC ST02848ATOne time installation of the Honeywell FMZ-2000 Flight Management System (FMS) on Boeing 727-212, serial number 21945.Jossair CompanySTC SA298NEInstallation of Simmonds Precision Computerized Fuel Quantity Indicator System in accordance with Simmonds Precision Installation Drawing List, Report Numbers E-2447, Revision E; and E-2523(optional), no revision, or later FAA-approved revisions.Simmonds Precision Products IncSTC SA365NEInstallation of Simmonds Precision computerized volumetric top-off units.Simmonds Precision Products IncSTC ST00626CHInstallation of replacement immersion heater.Aircraft Food Service Equipment RepairSTC ST00633ATApproval of maximum zero fuel weight increase from 138,000 pounds to 146,000 pounds. (727-200 SERIES S/N 19483, 19484, 19486, 19491, 20180, 20184, 20185, 20187, 20995, 20996, 19480, 19492, 19481, 19482, 19485, 20191 ONLY)Structural Integrity EngineeringSTC ST00671ATApproval of maximum landing weight increase from 160,000 pounds to 164,000 pounds. (727-200 SERIES S/N 21930 AND 21931 ONLY)Structural Integrity EngineeringSTC ST00719ATApproval of increased operating weights as substantiated by the design data listed in Structural Integrity Engineering (SIE) Master Report List or Master Document List No. SIE-28-703, no revision, dated February 24, 1995, or later FAA approved revision. Aircraft with Increase of Maximum Takeoff or Landing Weight must also be modified in accordance with: Drawing SIE-28-901 (taxi weight up to 183,000 lb, landing weight to 164,000 lb), 28-904 (taxi weight up to 178, 500 lbs, landing weight to 164,000 lbs), 28-905 (taxi weight up to 191,000 lb, landing weight to 164,000 lbs), Rev NC or later FAA approved revisions.Structural Integrity EngineeringSTC ST00720ATApproval of maximum zero fuel weight and maximum landing weight (Flaps 30) increases to 157,500 pounds and 166,000 pounds, respectively. (727-200 SERIES S/N 22080 ONLY)Structural Integrity EngineeringSTC ST00778LAInstallation of splitter locks and floor modifications to increase the main deck cargo floor capacity.Structural Integrity EngineeringSTC ST00779LAInstallation of side vertical restraints in accordance with approved Master Drawing List SIE 37-703, Revision A, dated May 25, 1999, or later FAA approved revisions. Structural Integrity Engineering FAA Approved Airplane Flight Manual Supplement, SIE 37-607 dated May 26, 1999, or later FAA approved revisions and Weight and Balance Supplement, SIE 37-608, dated February 9, 1999, or later FAA approved revisions, are required as part of this modification.Structural Integrity EngineeringSTC ST00901ATApproval of increased operating weights as substantiated by the design data listed in SIE-28-902. (727-200 S/N 21269, 21245 ONLY)Structural Integrity EngineeringSTC ST00949ATApproval of increased operating weights as substantiated by the design data listed in SIE Master Report List SIE-28-717. (727-200 SERIES S/N 21161 ONLY)Structural Integrity EngineeringSTC ST01013ATApproval of increased operating weights. Limited to installation on serial numbers 21327, 21328, 21329, 21330, and 21331 ONLY.Structural Integrity EngineeringSTC SA5904NMInstallation of a II Morrow Apollo 2001 Navigation Management System, in accordance with the applicable data listed on the attached FAA AML SA5904NM, or later FAA approved revision.Garmin AT Inc. · Lists 727 SeriesSTC ST00089BOInstallation of a BFGoodrich Aerospace Fire Detection and Suppression System. Suppression feature of Fire Detection and Suppression System has been certified for a maximum of 60 minutes from the activation of the suppression agent.)Simmonds Precision Products IncSTC ST01835CHInstallation of reinforced flightdeck door and venting system.National Aircraft Service Inc.STC ST01522LAModification of existing ACSS Traffic Alert and Collision Aviodance System (TCAS II)Aviation Communication and Surveillance Systems (ACSS) LLCSTC ST09249SCInstallation of dual Honeywell/ Trimble HT9100 FMS/GPS navigation systems.Aircraft Systems & Mfg
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