Douglas DC-8-51
STCs that may be installed · 148
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 ('3021920')
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.
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 ('3021920')
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_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.
STC SA2622NMInstallation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101)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 SA3421NMInstallation of Hughes-Avicom video entertainment system.STC 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 SA228EAInstallation of Inflight Motion Picture system.STC ST01067LAInstallation of Litton LTR-97 fiber optic gyro systems.STC SA1511GLInstallation of Type "C" containers.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 SA1033WEInstallation of either single or dual Collins AL-101 Radio Altimeter System(s) in accordance with FAA Approved United Air Lines Report Nos. F-1038 and No. F-1054.STC SA1034WEInstallation control and annunciation circuitry to implement Flight Director "Go-Around" command modes in accordance with the UAL FAA approved drawing list dated August 11, 1965, revised August 16, 1965. UAL FAA approved Airplane Flight Manual Supplementary Log of pages as listed.
Type Manual Approved Dated Appendix
DC-8-21, 31, 32, 33 SM 23889 1-19-60, 3-60, 2-1-60 and V
11-28-60 respectively
DC-8-51, 52, 53 LB 30582 10-10-61, 4-28-61 and 4-28-61 resp. VII
DC-8-51, 52, 53 LB 30757 1-26-62 IV
DC-8F-54, 55 LB 31180 1-29-63, 6-19-64 respectively IVSTC SA1080WEInstallation of cargo bins and seat track adaptors per United Air Lines Approved Drawing List No. COA T-2115 revised October 11, 1965, or later FAA approved revisions.STC SA1184WEInstallation - Cockpit Voice Recorder, United Data Control, Inc., per approved United Air Lines Report No. F-1067 for the DC-8F-54 and DC-8F-55 and Report No. F-1015 for DC-8-12, -21, -31, -32, -33, -51, -52.STC SA1538WEInstallation of Fairchild Model 13920-301 or 15630-601 Flight Data Recorder and Honeywell P/N 180 VI Central Air Data Computer in accordance with FAA Approved United Air Lines Report F-1174 dated September 8, 1967, revised November 13, 1967, or later FAA approved revision.STC SA1603WEReplacement of DC-8 reverser system - primary reverser cover door - JT3D engine with improved door designed and fabricated by United Air LinesSTC SA1830WEInstallation of aft facing cabin attendant seat at approximately station 450STC SA2211WEInstallation of Bendix Third Attitude Indicator to meet the requirements of 14 CFR 121.305(j)STC SA2284WEAlternate Seating Arrangement in accordance with FAA Approved United Air Lines Drawing List COA 2-4097 or later FAA approved revisions.STC SA2333WEProvides for the interchangeability and installation of door mounted inflatable emergency slides in accordance with FAA Approved United Air Lines Drawing No. 15F-4593.STC SA2573WEInstallation of interior modifications.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 SA2835WE-DInstallation of enclosed overhead stowage compartments, improved ceiling and sidewall lighting, relocation of motion picture project compartment refurbishment in accordance with United Airlines Drawing List No. COA 2-4629.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 SA3030WE-DInstall a carry-on baggage module.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 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 SA3357WE-DRetrofit of fuel quantity indicators and totalizers, Gull Airborne, Instruments, Inc. part numbers 206-009 and 206-016 seriesSTC 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 SA479WEInstallation of Cargo Bins and Adapters in the passenger cabinSTC 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 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 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 ST01170ATONE ONLY STC, SN 45685: Increase in aircraft operating weights.
Back to Douglas DC-8-51