TCDS 4A25
STCs approved under this data sheet · 587
Current certificates first, most recently changed first.
Query with SQL
duckdb -csv -c "SELECT s.stc_number, s.description, s.holder, s.status, s.status_date FROM 'https://openairdocs.org/data/latest/faa_stc.parquet' s WHERE s.stc_number IN (SELECT stc_number FROM 'https://openairdocs.org/data/latest/faa_stc_model.parquet' WHERE tcds_number = '4A25') 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 FROM 'https://openairdocs.org/data/latest/faa_stc.parquet' s WHERE s.stc_number IN (SELECT stc_number FROM 'https://openairdocs.org/data/latest/faa_stc_model.parquet' WHERE tcds_number = '4A25') ORDER BY s.status = 'Current' DESC, s.status_date DESC, s.stc_number
Run 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 SA2865WEInstallation of RNAV Equipment (to perform Two-Segment Approaches) in accordance with FAA Approved United Air Lines Report Number F-1665, or later FAA approved revisions. United Air Lines FAA Approved Airplane Flight Manual Supplement to document No. DAC-33161 dated June 7, 1974, is required with this modification.STC SA3026WE-DRevise interior arrangement to increase coach seating in accordance with United Air Lines, Inc. Drawing List No. COA 2-4784, or later FAA approved revisions.STC SA3027WE-DRevise interior arrangement to twenty-one rows of coach seating in accordance with DAS-1-WE United Air Lines Drawing List No. COA 2-4826 dated April 26, 1976, or later FAA approved revisions.STC SA3030WE-DInstall a carry-on baggage module.STC SA3032WE-DInstall carry-on baggage module in place of one first class seat assembly in accordance with DAS-1-WE Approved United Air Lines Drawing List No. 3032 or later FAA approved revisions.STC SA3033WE-DRevise interior arrangement to increase coach seating in accordance with DAS-1-WE Approved United Air Lines, Inc. Drawing List COA 2-4857 and COA 2-4858 amended in accordance with DAS-1-WE Approved United Air Lines Drawing List dated June 3, 1977, or later FAA approved revisions.STC SA3038WE-DInstallation of dual Collins FD-109 Flight Director System in accordance with master list of drawings and related documents for United Air Lines Change Order Authorization No. 2-4950 dated April 27, 1977 or later FAA approved revision. Each system consists of one each of the following components. Roll computer P/N 522-4428-008, Pitch Computer P/N 522-4892-008, Instrument Amplifier P/N 522-3874-005, Control Panel P/N 522-4431-001, Horizon Flight Director Indicator P/N 522-4430-002, Course Deviation
Indicator P/N 522-2782-004, Pitch Mode Annunciator P/N R2901-159 and Roll Mode Annunciator P/N R2901-160. The Boeing DC-8-61 FAA Approved Aircraft Flight Manual DAC-33161 has been reviewed and no revision is required as a result of this change.STC SA3039WE-DInstalls galley units and all supporting structure including plumbing and wiring at three locations in the aircraft in accordance with DAS-1-WE Approved United Air Lines Drawing Lists COA 2-4874, 2-4896, 2-4869, 2-4887, and 2-4934, dated July 8, 1977, or later FAA approved revisions.STC SA3040WE-DInstallation of cabin new look, cabin refurbishment, in-flight entertainment installation, passenger seat procurement and rework, and internal partitions and stowage cabinet installation in accordance with United Air Lines Drawing List Nos. COA 2-4864, 2-4879, 2-4901, and 2-4918.STC SA305EAA) Inflight Motion Picture System provisions in accordance with Lockheed Report 2580, Rev. 7, dated October 1964 and Electro Magnetic Compatibility, Lockheed Report 2573, Rev. 2, dated October 1964. (Report 2580 Rev. 7 dated October 1963 is equivalent to EM 1800 Section Report 2580 Rev. 20 dated November 1964). (B) Inflight Motion Picture System provision in 3 Class DC-8 in accordance with EM 1801 Section of Lockheed Report 2580 Rev. 30, December 1964 and Electro Magnetic Compatibility Lockheed Report 2573, Rev. 9, dated November 1964. This installation must be accomplished on aircraft with STC SA759WE installed. (Report 2580 Rev. dated December 30, 1964, same as Rev. dated December 10, 1964, with E.O. 19472, 19473, 19474, 19475, 19487). ( See Continuation on Page 3).STC SA3189WEInstallation of United Air Lines NLG orifice support tube assembly P/N 6F13548-501 and -502 per FAA Approved United Air Lines Drawing No. 6F13548, Rev. "B" dated January 10, 1977, or later FAA approved revisions as an equivalent replacement for McDonnell Douglas NLG orifice support tube P/N 5598184 and 5717019.STC SA3351WE-DInstalls a 181 passenger all coach cabin seating configuration in accordance with United Air Lines DAS-1-WE, Approved Drawing List No. 3351 dated September 20, 1977 or later FAA approved revision.STC SA3356WE-DRevise interior arrangement to accommodate dual class, 12 first class and 177 coach passenger configuration in accordance with DAS-1-WE Approved United Air Lines Drawing List 3356, or later FAA approved revision.STC SA3357WE-DRetrofit of fuel quantity indicators and totalizers, Gull Airborne, Instruments, Inc. part numbers 206-009 and 206-016 seriesSTC SA3361WE-DInstalls a 16 first class/123 coach dual class seating configurationSTC SA3576WE-DRevise interior arrangement to accommodate 162 coach passenger configuration.STC SA3582WE-DInstallation of ARINC communications addressing and reporting system (ACARS).STC SA3584WE-DSeat mix change from 162 passenger all coach configuration to18F/129Y-147 passenger configuration.STC SA3586WE-DInstallation of a removable dual Delco C-IV inertial navigation system for navigation only.STC SA3587WE-DSeat mix change from 223 passenger all coach charter configuration to 238 passenger all coach charter configuration.STC SA3588WE-DSeat mix change from 223 passenger all coach charter configuration to 238 passenger all coach charter configuration.STC SA3593WE-DSeat mix change from 26 F/C and 156 coach passenger configuration to 26 F/C and 164 coach passenger configuration.STC SA3943WE-DRework of High-Frequency Communications System to install single-sideband capabilitySTC SA3945WE-DInstallation of a DC-8-51 landing gear on DC-8-52 airplane.STC SA4-1363Interior configurations as described on United Air Lines Approved Master Drawing List No. COA 20-25-20 Sheets No. 1 through 5. (DC-8, 2-class configurations).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 SA4091WEDeletion of a pair of excess Type I exits at Station 1124 in accordance with FAA Approved United Air Lines Drawing List No. 7782, Revision B, dated January 21, 1980, or later FAA approved revisions.STC SA479WEInstallation of Cargo Bins and Adapters in the passenger cabinSTC SA497EAInflight Motion Pictures Provisions in accordance with Lockheed Report 3052, "Technical Drawing Index, Inflight Motion Pictures," dated October 14, 1966, revised December 29, 1966, or revised May 9, 1967, and Lockheed Report 3056, "Technical Drawing List, Inflight Motion Pictures Pallet Assembly 1R-3000 (Rev. A)," dated October 18, 1966.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).STC SA65WEInstallation of a cockpit hydraulic replenishing system. See 15F-2044 Chg. B, 9F-4813 Chg. C, 6F-8140 Chg. C, 6F-8130 Chg. B, 3F-9025 Chg. A, 3F-9022, 3F-9023 Chg. A, IF-9882, 6F-8141 Chg. C. COA-2-1534 (ERs 1 - 4), App. V(UAL) to AFM SM-23889, App. IV (UAL) to AFM SM-23891, App. VII(UAL) to AFM LB-30582 or later FAA approved revisions.STC SA759WEInterior configuration as described on United Air Lines Master Drawing List No. COA 2-2458 Sheets No. 1 through 11 (DC-8, 3-class configurations).STC SA833WEInstallation of two triple seats in the main cabin and associated changes per United Air Lines Drawing No. 6F-8882 "E" change, "DC-8F Interior Arrangement" and the following drawings: (see Continuation Sheet)STC SA855WEInstallation - Passenger Entertainment System - Stereo and Monaural Tape Deck Audio per FAA Approved United Air Lines Report No. F-971.STC SA906WEModification of R. H. forward lounge as described by United Air Lines Approved Drawing List No. COA 2-2450 dated March 4, 1965, or later FAA approved revisions.STC SA2825CEInstallation of B&D Instruments & Avionics, Inc. Electronic N2 Gas Compressor Indicator. Data required: (1) B&D Instruments & Avionics, Inc. Installation Manual Part No. 55006-003-011, Revision A, dated April 6, 1992, or later "FAA Approved" revision; and (2) copy of this certificate.STC SA2826CEInstallation of optional set of B&D Instruments & Avionics, Inc. Electronic Exhaust Gas Temperature (EFT) Indicators.STC SA913NWInstallation of stowage unit.STC ST01202WI-DModification of an existing FAA approved Collins TPR-720, TPR-900 or TPR-901 Mode S transponder installation in Part 25 Aircraft using Collins Drawing Index as listed on AML No. ST01202WI-D, latest FAA approved revision.STC SA1341NMInstallation of CFMI CFM-56 engines and related changesSTC SA1386NMONE ONLY STC, SN 46095: Installation of Avionics and Electrical changes as described in McDonnell Douglas Serial Engineering Order No. 006STC SA2308WEInstallation of cargo barrier net.STC SA3749WEConversion of passenger airplane to cargo only configuration by installation of cargo door, cargo floor, and increasing maximum landing and zero fuel weight.STC SA8011SWInstallation of Collins DLC-800 ACARS and number 3 VHF transceiver.STC ST01293ATReplacement of flap hinge base fittings at flap station Xf219, with UPS designed fittings.STC SA293EATray carrier.STC ST00543ATIncrease in aircraft operating weights(Maximum takeoff weight - 315,000 lbs., maximum landing weight - 217,000 lbs., maximum zero fuel weight - 203,000 lbs.) (DC-8-51 s/n 45855 only)STC ST00558ATIncrease in aircraft operating weights (Maximum takeoff weight - 315,000 lbs., maximum landing weight - 217,000 lbs., maximum zero fuel weight - 203,000 lbs.) (DC-8-51 s/n 45410 only)STC ST00617ATIncrease in aircraft operating weights(maximum takeoff weight - 315,000 lbs., maximum landing weight - 217,000 lbs., maximum zero fuel weight - 203,000 lbs. (DC-8-51 s/n 45935 only)STC ST00794ATIncrease in aircraft operating weights(max takeoff weight - 328,000 lbs., max landing weight - 258,000 lbs., max zero fuel weiht - 245,000 lbs.) (DC-8-71 SN 46099 only)
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