TCDS 4A25

STCs approved under this data sheet · 587

Current certificates first, most recently changed first.

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  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')
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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.United Airlines IncSTC 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.United Airlines IncSTC 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.United Airlines IncSTC SA3030WE-DInstall a carry-on baggage module.United Airlines IncSTC 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.United Airlines IncSTC 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.United Airlines IncSTC 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.United Airlines IncSTC 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.United Airlines IncSTC 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.United Airlines IncSTC 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).United Airlines IncSTC 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.United Airlines IncSTC 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.United Airlines IncSTC 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.United Airlines IncSTC SA3357WE-DRetrofit of fuel quantity indicators and totalizers, Gull Airborne, Instruments, Inc. part numbers 206-009 and 206-016 seriesUnited Airlines IncSTC SA3361WE-DInstalls a 16 first class/123 coach dual class seating configurationUnited Airlines IncSTC SA3576WE-DRevise interior arrangement to accommodate 162 coach passenger configuration.United Airlines IncSTC SA3582WE-DInstallation of ARINC communications addressing and reporting system (ACARS).United Airlines IncSTC SA3584WE-DSeat mix change from 162 passenger all coach configuration to18F/129Y-147 passenger configuration.United Airlines IncSTC SA3586WE-DInstallation of a removable dual Delco C-IV inertial navigation system for navigation only.United Airlines IncSTC SA3587WE-DSeat mix change from 223 passenger all coach charter configuration to 238 passenger all coach charter configuration.United Airlines IncSTC SA3588WE-DSeat mix change from 223 passenger all coach charter configuration to 238 passenger all coach charter configuration.United Airlines IncSTC SA3593WE-DSeat mix change from 26 F/C and 156 coach passenger configuration to 26 F/C and 164 coach passenger configuration.United Airlines IncSTC SA3943WE-DRework of High-Frequency Communications System to install single-sideband capabilityUnited Airlines IncSTC SA3945WE-DInstallation of a DC-8-51 landing gear on DC-8-52 airplane.United Airlines IncSTC 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).United Airlines IncSTC 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.United Airlines IncSTC 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.United Airlines IncSTC SA479WEInstallation of Cargo Bins and Adapters in the passenger cabinUnited Airlines IncSTC 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.United Airlines IncSTC 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).United Airlines IncSTC 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.United Airlines IncSTC 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).United Airlines IncSTC 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)United Airlines IncSTC SA855WEInstallation - Passenger Entertainment System - Stereo and Monaural Tape Deck Audio per FAA Approved United Air Lines Report No. F-971.United Airlines IncSTC 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.United Airlines IncSTC 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.Teledyne ControlsSTC SA2826CEInstallation of optional set of B&D Instruments & Avionics, Inc. Electronic Exhaust Gas Temperature (EFT) Indicators.Teledyne ControlsSTC SA913NWInstallation of stowage unit.AIM Aviation IncSTC 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.Rockwell Collins IncSTC SA1341NMInstallation of CFMI CFM-56 engines and related changesBoeing CompanySTC SA1386NMONE ONLY STC, SN 46095: Installation of Avionics and Electrical changes as described in McDonnell Douglas Serial Engineering Order No. 006Boeing CompanySTC SA2308WEInstallation of cargo barrier net.Boeing CompanySTC SA3749WEConversion of passenger airplane to cargo only configuration by installation of cargo door, cargo floor, and increasing maximum landing and zero fuel weight.Boeing CompanySTC SA8011SWInstallation of Collins DLC-800 ACARS and number 3 VHF transceiver.United Parcel ServiceSTC ST01293ATReplacement of flap hinge base fittings at flap station Xf219, with UPS designed fittings.United Parcel Service CompanySTC SA293EATray carrier.Lockheed Aircraft Service CoSTC 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)Aircraft Modification Design ServicesSTC 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)Aircraft Modification Design ServicesSTC 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)Aircraft Modification Design ServicesSTC 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)Aircraft Modification Design Services
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