FAA STC category

Other aircraft modifications STCs

Current FAA supplemental type certificates outside the principal modification categories. This directory contains 11,384 selected records listed with status Current in the June 30, 2026 FAA DRS snapshot and links every entry to its source.

Showing 10,681–10,800 of 11,384Page 90 of 95

ST09719SC-DOther aircraft modificationsRevised Apr 4, 2001

Honeywell Traffic & Collision Avoidance System modification. FAA AFM report no. 36856-1 dtd 4/4/01 required. F90-01088-501 installation limited to serial number 097 only.

FAA holder: Dassault Falcon Jet

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SA4843SWOther aircraft modificationsRevised Apr 2, 2001

Installation of replacement of freon compressor with positive traction drive.

FAA holder: Zee Systems, Inc

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ST00214NYOther aircraft modificationsRevised Mar 29, 2001

Installation of full size waste carts P/N E500042, half size waste carts P/N E500043, full size meal/bev. carts P/N E500046,and half size meal/bev. Carts P/N E500048.

FAA holder: Driessen Aircraft Interior Systems USA, Inc

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ST00509NYOther aircraft modificationsRevised Mar 29, 2001

Installation of Lermer Corporation FS Waste Cart, HS Waste Cart, HS Meal/Bev Cart, FS Meal/Bev Cart.

FAA holder: Driessen Aircraft Interior Systems USA, Inc

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ST01074NYOther aircraft modificationsRevised Mar 29, 2001

Installation of inflight service full size meal cart P/N TM012001.

FAA holder: Driessen Aircraft Interior Systems USA, Inc

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SR01140LAOther aircraft modificationsRevised Mar 27, 2001

Installation of a Wescam nose mount.

FAA holder: Wescam

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ST00955WIOther aircraft modificationsRevised Mar 27, 2001

Installation of Phoenix Aerospace, Inc Solid State Voltage Regulator Model No. BG- 1010-24-SA, in place of existing voltage regulator.

FAA holder: Phoenix Aerospace, Inc

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ST00273CHOther aircraft modificationsRevised Mar 20, 2001

Installation of a Collins TCAS94 TCAS II System, with change 7 software.

FAA holder: Duncan Aviation

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ST01093LA-DOther aircraft modificationsRevised Mar 20, 2001

Upgrade of Honeywell Traffic Alert and Collision Avoidance System TCAS I (CAS 66A) to TCAS II (CAS 67A) with change 7. STC ST317CH is a required part of this STC.

FAA holder: Gulfstream Aerospace Corporation

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ST01148LAOther aircraft modificationsRevised Mar 20, 2001

Installation of windscreens and closets.

FAA holder: U.S. Technical

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SA2723SOOther aircraft modificationsRevised Mar 19, 2001

Installation of a digital passenger control unit.

FAA holder: Thales Avionics In-Flight Systems, LLC

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SA9025NM-DOther aircraft modificationsRevised Mar 19, 2001

Installation of BE Aerospace BE2000M Distributed Video System.

FAA holder: Thales Avionics In-Flight Systems, LLC

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SA9030NM-DOther aircraft modificationsRevised Mar 19, 2001

Installation of Puritan Bennett Aero Systems -- ACCTV Landscape System.

FAA holder: Thales Avionics In-Flight Systems, LLC

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ST00368LAOther aircraft modificationsRevised Mar 19, 2001

Installation of B/E digital passenger control units on KLM Royal Dutch Airlines MD-11 airplane.

FAA holder: Thales Avionics In-Flight Systems, LLC

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ST00541LAOther aircraft modificationsRevised Mar 19, 2001

Installation of B/E Digital passenger control units on KLM Royal Dutch Airlines 747-400.

FAA holder: Thales Avionics In-Flight Systems, LLC

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SA8404SW-DOther aircraft modificationsRevised Mar 16, 2001

Installation of S-TEC System 55/55X two axis automatic flight guidance system Model ST-550.

FAA holder: S-TEC Corporation

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ST00953WIOther aircraft modificationsRevised Mar 16, 2001

Installation of a Universal CVR-120 cockpit voice recorder system. Data required: (1) Duncan Aviation document list no. 10055400, Rev B, dtd 3/12/01; (2) Duncan Aviation Document No. 40011100, FAA Approved Flight Manual Supplement, dtd 3/16/01; or later FAA approved revisions.

FAA holder: Duncan Aviation, Inc

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SA09506AC-DOther aircraft modificationsRevised Mar 15, 2001

Installation of S-TEC System 30 Two Axis Automatic Flight Guidance System, Model ST-886-30,.

FAA holder: S-TEC Corporation

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SA09507AC-DOther aircraft modificationsRevised Mar 15, 2001

Installation of S-TEC System 30 Two Axis Automatic Flight Guidance System, Model ST-886-30.

FAA holder: S-TEC Corporation

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SA09508AC-DOther aircraft modificationsRevised Mar 15, 2001

Installation of S-TEc System 30 Two Axis Automatic Flight Guidance System, Model ST-886-30.

FAA holder: S-TEC Corporation

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SH188WEOther aircraft modificationsRevised Mar 15, 2001

Installation of stirrup assemblies.

FAA holder: Dallwig Barry C

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SH201WEOther aircraft modificationsRevised Mar 15, 2001

Installation of stirrup assemblies to directional control pedals for operation by handicapped pilot. (US ARMY OH-13E 205A).

FAA holder: Dallwig Barry C

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ST00618WI-DOther aircraft modificationsRevised Mar 15, 2001

Modification to install an Airborne Warning and Control System (AWACS) configuration to include multiple configurations of various non-essential mission systems.

FAA holder: Boeing Commercial Airplane Group

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SA09401AC-DOther aircraft modificationsRevised Mar 14, 2001

Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST-853,.

FAA holder: S-TEC Corporation

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SA09403AC-DOther aircraft modificationsRevised Mar 13, 2001

Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST-556,.

FAA holder: S-TEC Corporation

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SA8886SW-DOther aircraft modificationsRevised Mar 13, 2001

Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System, Model ST-556, with Optional Autotrim System.

FAA holder: S-TEC Corporation

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SA09298AC-DOther aircraft modificationsRevised Mar 12, 2001

Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST-751,.

FAA holder: S-TEC Corporation

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SA8250SW-DOther aircraft modificationsRevised Mar 9, 2001

Installation of AlliedSignal traffic alert and collision avoidance system(TCAS II).

FAA holder: Dassault Falcon Jet

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ST00949WIOther aircraft modificationsRevised Mar 9, 2001

Installation of Rockwell Collins Dual Attitude Heading Reference System (AHRS).

FAA holder: JetCorp

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ST01313CH-DOther aircraft modificationsRevised Mar 9, 2001

Installation of an AlliedSignal Airborne Flight Information System (AFIS).

FAA holder: Garrett Aviation Services

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SA09193AC-DOther aircraft modificationsRevised Mar 5, 2001

Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST-651,.

FAA holder: S-TEC Corporation

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SA09504AC-DOther aircraft modificationsRevised Mar 5, 2001

Installation of S-TEC Altitude Vertical Speed Selector/Altitude Alerter, Model ST-360.

FAA holder: S-TEC Corporation

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ST00287LA-DOther aircraft modificationsRevised Mar 5, 2001

Installation of PTC model 950 business class seats with provisions only modification for GTE Airfone Installation per BE Aerospace Services Division Master Drawing list MDL-0003 Rev B dtd 5/12/97 or latest revision. Responsible ACO is Los Angeles ACO, NM-L.

FAA holder: Midwest Express Airlines

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SA01079LAOther aircraft modificationsRevised Mar 2, 2001

Installation of Accessory Power Receptable in accordance with FAA Approved Master Drawing List, Document No. 206-APR-100, Rev IR, dtd 8/15/00 or later FAA approved revision.

FAA holder: Premier Aviation

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SA01080LAOther aircraft modificationsRevised Mar 2, 2001

Installation of Accessory Power Receptable in accordance with FAA Approved Master Drawing List, Document No. 172-APR-100, Rev IR, dtd 8/15/00 or later FAA approved revision.

FAA holder: Premier Aviation

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SA5493NMOther aircraft modificationsRevised Mar 2, 2001

Installation of Coltech Selcal per FAA approved Coltech, Inc. document no. 0200017-000 Rev A dtd 11/15/91 or later FAA approved revision.

FAA holder: Avtech Corporation

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ST5493NMOther aircraft modificationsRevised Mar 2, 2001

Installation of Coltech SELCAL.

FAA holder: Avtech Corporation

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SE995GLOther aircraft modificationsRevised Mar 1, 2001

Rebuilt modification of starter drive clutch assembly.

FAA holder: Aerotech

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SH1618NMOther aircraft modificationsRevised Mar 1, 2001

Installation of externally mounted ferry tanks.

FAA holder: Erickson Air Crane Inc. dba Erickson Air-Crane

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SH2908NMOther aircraft modificationsRevised Mar 1, 2001

Modification of the external loads lifting pendant and system.

FAA holder: Erickson Air Crane Inc. dba Erickson Air-Crane

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SH2910NMOther aircraft modificationsRevised Mar 1, 2001

Installation of Erickson EAC-4675 tail pipe extension.

FAA holder: Erickson Air Crane Inc. dba Erickson Air-Crane

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SH4746NMOther aircraft modificationsRevised Mar 1, 2001

Use of Mobil Oil Corp. 'Mobilgrease 28' synthetic grease to lubricate the main rotor head, swash plate and various associated linkages.

FAA holder: Erickson Air Crane Inc. dba Erickson Air-Crane

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SH5724NMOther aircraft modificationsRevised Mar 1, 2001

Use of Mobil Oil Corporation Mobilith SHC220 synthetic grease to lubricate selected components in place of the previously approved grease.

FAA holder: Erickson Air Crane Inc. dba Erickson Air-Crane

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SH5776NMOther aircraft modificationsRevised Mar 1, 2001

Installation of a tail pipe extension.

FAA holder: Erickson Air Crane Inc. dba Erickson Air-Crane

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SH726NWOther aircraft modificationsRevised Mar 1, 2001

Installation of Erickson EAC-4675 tail pipe extension.

FAA holder: Erickson Air Crane Inc. dba Erickson Air-Crane

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SH738NWOther aircraft modificationsRevised Mar 1, 2001

Installation of Erickson EAC-4675 tail pipe extension.

FAA holder: Erickson Air Crane Inc. dba Erickson Air-Crane

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SR00502SEOther aircraft modificationsRevised Mar 1, 2001

Fabrication and installation of Erickson Model 10333-101 (S-64E) or 10333-103 (S-64F) Water/Foam Cannon system.

FAA holder: Erickson Air Crane Inc. dba Erickson Air-Crane

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ST00435ATOther aircraft modificationsRevised Mar 1, 2001

Overhaul/repair of the Delco starter adapter drive (P/N 1971890) used with Delco starters P/N's 11096656 and 1109660.

FAA holder: Aerotech

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SA09132AC-DOther aircraft modificationsRevised Feb 28, 2001

Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST-612,.

FAA holder: S-TEC Corporation

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SA09133AC-DOther aircraft modificationsRevised Feb 28, 2001

installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST-612,.

FAA holder: S-TEC Corporation

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SA09134AC-DOther aircraft modificationsRevised Feb 28, 2001

Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST-6I2,.

FAA holder: S-TEC Corporation

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SA09135AC-DOther aircraft modificationsRevised Feb 28, 2001

Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST-612,.

FAA holder: S-TEC Corporation

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ST09840SCOther aircraft modificationsRevised Feb 28, 2001

Installation of a multi-zone environmental control system.

FAA holder: Schwartz Engineering Co

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SA01379CHOther aircraft modificationsRevised Feb 27, 2001

Installation of a fiberglass pressure cowling.

FAA holder: Turbine Conversions Ltd

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ST01134LAOther aircraft modificationsRevised Feb 22, 2001

Installation of Unit Load Device center of gravity offset limit kit.

FAA holder: Ventura Aerospace Inc.

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ST02287ATOther aircraft modificationsRevised Feb 21, 2001

Installation of a Collins TCAS II system (TCAS 4000).

FAA holder: Jet Aviation Associates, Ltd

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ST09853SCOther aircraft modificationsRevised Feb 21, 2001

Installation of modified compass heading switching system.

FAA holder: NASA Johnson Space Center

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SA09149AC-DOther aircraft modificationsRevised Feb 20, 2001

Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST-627,.

FAA holder: S-TEC Corporation

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SA9013NM-DOther aircraft modificationsRevised Feb 16, 2001

Installation of Claircom passenger phone system.

FAA holder: Claircom Communications Group LP

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SA09007AC-DOther aircraft modificationsRevised Feb 15, 2001

Installation of S-TEC System 55/55X two axis automatic flight guidance system, Model ST-587.

FAA holder: S-TEC Corporation

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SA09008AC-DOther aircraft modificationsRevised Feb 15, 2001

Installation of S-TEC System 55/55X two axis automatic flight guidance system, model ST-587.

FAA holder: S-TEC Corporation

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SA1990WEOther aircraft modificationsRevised Feb 15, 2001

Installation of Tritan Amphibious float model TA 3500.

FAA holder: Sea Emperor, Inc.

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SA2136WEOther aircraft modificationsRevised Feb 15, 2001

Installation of Tritan amphibious float Model TA 3500.

FAA holder: Sea Emperor, Inc.

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SA2164WEOther aircraft modificationsRevised Feb 15, 2001

Installation of Edo Model FD-3500A(TSO C-27-2) amphibious floats.

FAA holder: Sea Emperor, Inc.

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SA2253WEOther aircraft modificationsRevised Feb 15, 2001

Installation of Edo Model FD-3500-21 amphibious floats.

FAA holder: Sea Emperor, Inc.

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SA00124DEOther aircraft modificationsRevised Feb 14, 2001

Installation of Oilamatic preoiler system.

FAA holder: Oilamatic Inc

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SA02265ATOther aircraft modificationsRevised Feb 14, 2001

Installation of AlliedSignal Airborne Flight Information System (AFIS).

FAA holder: Aircraft Engineering & Installation Services Inc

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SA8405SW-DOther aircraft modificationsRevised Feb 14, 2001

Installation of S-TEC System 55/55X two axis automatic flight guidance system, Model ST-553.

FAA holder: S-TEC Corporation

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ST09635SCOther aircraft modificationsRevised Feb 13, 2001

Installation of a Dual GNS-XLS System.

FAA holder: Schwartz Engineering Co

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ST01058NYOther aircraft modificationsRevised Feb 12, 2001

Installation of Honeywell TCAS 2000 MOPS 7.00 and Collins TD94 Controller.

FAA holder: Execaire Inc

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ST02274ATOther aircraft modificationsRevised Feb 12, 2001

Installation of galleys. Represents FAA approval of galleys previously installed in US manufactured aircraft operated by an airline under registry of a Foreign Country and approved by cognizant Foreign Country Airworthiness Authority. Approved for serial numbers 25247 and 25248 (Model 737-429; S/N's 25219, 25419, 26537, and 26538 (Model 737-529).

FAA holder: CIT Aerospace

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SA7306SW-DOther aircraft modificationsRevised Feb 3, 2001

Installation of the Bendix Traffic Alert and Collision Avoidance System (TCAS).

FAA holder: Dassault Falcon Jet

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SA09002AC-DOther aircraft modificationsRevised Feb 2, 2001

Installation of S-TEC System 55/55X two axis automatic flight guidance system, Model ST-586.

FAA holder: S-TEC Corporation

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SA09003AC-DOther aircraft modificationsRevised Feb 2, 2001

Installation of S-TEC System 55/55X Two Axis automatic flight guidance system, Model ST-586.

FAA holder: S-TEC Corporation

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SA09017AC-DOther aircraft modificationsRevised Feb 2, 2001

Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST-596.

FAA holder: S-TEC Corporation

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SA09018AC-DOther aircraft modificationsRevised Feb 2, 2001

Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST-596.

FAA holder: S-TEC Corporation

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SA09261AC-DOther aircraft modificationsRevised Feb 2, 2001

Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST-586,.

FAA holder: S-TEC Corporation

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SA09432AC-DOther aircraft modificationsRevised Feb 2, 2001

Installation of S-TEC system 30 two axis automatic flight guidance system, Model ST-871.

FAA holder: S-TEC Corporation

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SA09201AC-DOther aircraft modificationsRevised Feb 1, 2001

Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST-563,.

FAA holder: S-TEC Corporation

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SA8894SW-DOther aircraft modificationsRevised Feb 1, 2001

Installation of S-TEC System 55 two axis automatic flight guidance system, Model ST-563, with optional autotrim system.

FAA holder: S-TEC Corporation

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SA8895SW-DOther aircraft modificationsRevised Feb 1, 2001

Installation of S-TEC System 55 two axis automatic flight guidance system.

FAA holder: S-TEC Corporation

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ST01351CH-DOther aircraft modificationsRevised Feb 1, 2001

Installation of Dual Universal UNS-1K Flight Management System.

FAA holder: ElectroSonics

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ST02261ATOther aircraft modificationsRevised Feb 1, 2001

Installation of two panel sidewall liner.

FAA holder: East Coast Avionics

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SA00874SEOther aircraft modificationsRevised Jan 31, 2001

Install two Pratt & Whitney PT6A-34 engines in place of PT6A-28 engines per Master Document List TFL-PA31T-D01, Revision IR, dated November 29, 2000, or later FAA approved revision. Inspect and maintain this modification in accordance with Instructions for Continued Airworthiness, Document TFL-PA31T-R34, Revision IR, dated November 29, 2000, or later FAA approved revision.

FAA holder: Teufel Nursery Inc

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ST09383SCOther aircraft modificationsRevised Jan 31, 2001

Installation of a Collins TCAS 94 system.

FAA holder: Schwartz Engineering Co

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SA01384CHOther aircraft modificationsRevised Jan 30, 2001

Installation of various de-icer harnesses.

FAA holder: SMR Technologies

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SA105NEOther aircraft modificationsRevised Jan 30, 2001

Installation of a Sperry Primus-800 ColoRadar system.

FAA holder: Bombardier Completion Center Inc

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SA156NEOther aircraft modificationsRevised Jan 30, 2001

Installation of a Sperry DATA NAV III system with skip and recall.

FAA holder: Bombardier Completion Center Inc

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ST00073NYOther aircraft modificationsRevised Jan 30, 2001

Installation of Bendix/King TCAS I System.

FAA holder: Bombardier Completion Center Inc

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ST01126LAOther aircraft modificationsRevised Jan 29, 2001

Installation of Rosemount Water vapor sensing system (WVSS).

FAA holder: Cotton John & Associates International

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SH7731SWOther aircraft modificationsRevised Jan 26, 2001

Personnel lifting device.

FAA holder: Mauck Lee E.

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ST01283NYOther aircraft modificationsRevised Jan 26, 2001

Installation of insulation blankets.

FAA holder: Magnifoam Technology

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ST02269ATOther aircraft modificationsRevised Jan 26, 2001

To upgrade the number of required parameters to be recorded by existing (Sundstrand/AlliedSignal 980-4100-( ) and 980-4120-( ) or Fairchild/Loral 17M703-274 and 17M903-274) flight data recorder.

FAA holder: Avionics Group Inc.

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SA8896SW-DOther aircraft modificationsRevised Jan 25, 2001

Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System, Model ST-566, with Optional Autotrim System.

FAA holder: S-TEC Corporation

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ST01121LAOther aircraft modificationsRevised Jan 24, 2001

Installation of Retrofit AudioFile Server (AFS) and Multimedia Data Loader (MDL).

FAA holder: Global Aviation

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ST01125LAOther aircraft modificationsRevised Jan 24, 2001

Modification of AlliedSignal CTCP36-150W auxiliary power unit (APU) which extends APU operating envelope from 30,000 feet to 37,000 feet. Approval of this change applies to the Hawker 800XP with STC ST00459NY installed with the AlliedSignal GTCP36-150W APU.

FAA holder: Lockheed Martin Management & Data Systems

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ST00896WI-DOther aircraft modificationsRevised Jan 22, 2001

Installation of GLS Data Recording Equipment.

FAA holder: Rockwell Collins Inc

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ST01118LAOther aircraft modificationsRevised Jan 22, 2001

Installation of high temperature, semi-rigid, coaxial fire/overheat detection wire harness cable assemblies. For Boeing 747-400 with G.E. CF6-80C2 powered airplanes only.

FAA holder: Meggitt Safety Systems, Inc.

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SA02262ATOther aircraft modificationsRevised Jan 19, 2001

Installation of an AlliedSignal GNS-XLs flight management system.

FAA holder: Aircraft Engineering & Installation Services Inc

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SA1712SWOther aircraft modificationsRevised Jan 19, 2001

Installation of oil pressure indicator.

FAA holder: Mitsubishi Heavy Industries America Inc.

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SA1732SWOther aircraft modificationsRevised Jan 19, 2001

Installation of Kratos 124.102 torque indicator.

FAA holder: Mitsubishi Heavy Industries America Inc.

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SA1736SWOther aircraft modificationsRevised Jan 19, 2001

Installation of Amtek oil pressure transmitter P/N 935A-5002.

FAA holder: Mitsubishi Heavy Industries America Inc.

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SA1764SWOther aircraft modificationsRevised Jan 19, 2001

Installation of Smith's 1400 encoding altimeter/alerter.

FAA holder: Mitsubishi Heavy Industries America Inc.

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SA1778SWOther aircraft modificationsRevised Jan 19, 2001

Installation of R.C. Allen Gyro.

FAA holder: Mitsubishi Heavy Industries America Inc.

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SA1779SWOther aircraft modificationsRevised Jan 19, 2001

Installation of Kollsman Dual Baro scale altimeter.

FAA holder: Mitsubishi Heavy Industries America Inc.

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SA1784SWOther aircraft modificationsRevised Jan 19, 2001

Installation of Flite phone II and III.

FAA holder: Mitsubishi Heavy Industries America Inc.

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SA1882SWOther aircraft modificationsRevised Jan 19, 2001

Installation of chart holder.

FAA holder: Mitsubishi Heavy Industries America Inc.

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SA1929SWOther aircraft modificationsRevised Jan 19, 2001

Installation of United Instruments encoding altimeter.

FAA holder: Mitsubishi Heavy Industries America Inc.

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SA1940SWOther aircraft modificationsRevised Jan 19, 2001

Installation of Gulton GB40 20 cell batteries or Marathon CA-5-20 cell batteries.

FAA holder: Mitsubishi Heavy Industries America Inc.

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SA2208SWOther aircraft modificationsRevised Jan 19, 2001

Installation of continuous ignition system.

FAA holder: Mitsubishi Heavy Industries America Inc.

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SA2233SWOther aircraft modificationsRevised Jan 19, 2001

Rewiring of auto-manual air conditioning switch.

FAA holder: Mitsubishi Heavy Industries America Inc.

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SA2316SWOther aircraft modificationsRevised Jan 19, 2001

Installation of ONTRAC II VLF system.

FAA holder: Mitsubishi Heavy Industries America Inc.

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SA2414SWOther aircraft modificationsRevised Jan 19, 2001

Installation of Bendix RNS-3500 area NAV system.

FAA holder: Mitsubishi Heavy Industries America Inc.

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SA2487SWOther aircraft modificationsRevised Jan 19, 2001

Installation of outside air temperature indicator.

FAA holder: Mitsubishi Heavy Industries America Inc.

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SA8129SWOther aircraft modificationsRevised Jan 19, 2001

Installation of Collins TCAS-94, TCAS II traffic alert collision avoidance system with -012 software and dual Collins TDR-(94 Mode S transponders Status003).

FAA holder: Gulfstream Aerospace Corporation

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SA8207SWOther aircraft modificationsRevised Jan 19, 2001

Installation of Collins TCAS-94 traffic alert and collision avoidance system with dual Collins TDR-94D Mode S transponders.

FAA holder: Gulfstream Aerospace Corporation

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SA996SWOther aircraft modificationsRevised Jan 19, 2001

Move air conditioning unit approximately 20-inches aft and enlarge luggage compartment.

FAA holder: Mitsubishi Heavy Industries America Inc.

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ST00940WIOther aircraft modificationsRevised Jan 19, 2001

Installation of a Collins TCAS 4000 TCAS II system. Data required: (1) Duncan Aviation, Inc., Document List No. 10055700, Rev C, dtd 1/19/01; (2) Duncan Aviation Document No. 40010700, FAA Approved Airplane Flight Manual Supplement, dtd 1/19/01; or later FAA approved revisions to (1) or (2).

FAA holder: Duncan Aviation, Inc

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ST01281NYOther aircraft modificationsRevised Jan 19, 2001

Installation of an Innovative solutions & Support, Inc. Standby Altimeter, P/N 9D-80110-24. (757-24APF, 767-34AF).

FAA holder: Innovative Solutions & Support, Inc.

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ST09597SCOther aircraft modificationsRevised Jan 19, 2001

Installation of Collins TCAS-94 System.

FAA holder: West Star Aviation

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