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FAA STC category

Aircraft connectivity STCs

Satellite communications, broadband, antennas, telephony, and connected-aircraft systems. This directory contains 1,301 selected records listed with status Current in their cited FAA DRS snapshots and links every entry to its source.

Showing 1,081–1,200 of 1,301Page 10 of 11
ST01275WI-DAircraft connectivity

Modification of a Collins VHF-900 communication system installation with Gables G7404-23 or G7404-123 Radio Tuning Panels to a Collins VHF-2100 VDL Mode 3 capable communication system installation with Gables G7424-302 Radio Tuning Panels in accordance with: (1) Collins Master Data List RCA-0016-001, Revision -, dated September 28, 2004, (2) Collins Airplane Flight Manual Supplement RCA-0079-001, Revision -, dated January 4, 2005, and (3) Collins Maintenance Manual Supplement RCA-0074-001, Revision -, dated January 4, 2005 or later FAA approved revisions to (1), (2) or (3).

FAA holder: Rockwell Collins Inc

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SA970NEAircraft connectivity

Installation of wing filler for auxiliary fuel tanks, miscellaneous structural modifications and optional radome, dual alternator system, bow compartment covers, upper fin revision, disassembly provisions and dual rudder/aileron electric trim system in accordance with Aerofab, Inc. Drawing List 4-0001, Revision I, dated October 23, 1996, or later FAA-approved revision. The installation is applicable in the following configurations: United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) ___________________________________________________________________________________________________________________________________ Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. ___________________________________________________________________________________________________________________________________ FAA Form 8110-2-1(10-69) PAGE 4 of 4 PAGES This certificate may be transferred in accordance with FAR 21.47. United States of America Department of Transportation -- Federal Aviation Administration Supplemental Type Certificate _____________________________________________________________________________________________________________________________________ Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. _____________________________________________________________________________________________________________________________________ FAA Form 8110-2(10-68) PAGE 1 of 1 PAGES This certificate may be transferred in accordance with FAR 21.47. CONFIGURATION 1: Basic installation with aft seats installed in accordance with Configuration 1 of STC SA469NE. Optional items may be installed in any combination as follows: Option 1: Radome In accordance with drawings 150017, 190011, 190018 and 190019. Mass with an equivalent weight of 35 lbs. may be installed with a center of gravity no farther forward than 6.61 inches aft of bulkhead 190011-11, as defined in Aerofab, Inc. Engineering Report 4-250-2, dated November 4, 1991, and drawing 190019. This STC does not approve the installation of a radar, antenna, wave guide or transmitter, nor radar/radome system compatibility. Option 2: Dual Alternator System In accordance with drawings 4-7781 and 4-7782. Option 3: Bow Compartment Covers In accordance with drawing 4-3501. Option 4: Upper Fin Revision In accordance with drawing 4-2652, Revision C. Option 5: Disassembly Provisions In accordance with drawing 300015. Option 6: Dual Rudder/Aileron Electric Trim System In accordance with drawing 4-3519 and STC SA1142SO. CONFIGURATION 2: Same as Configuration 1 except aft sets installed in accordance with Configuration 2 of STC SA469NE and aft seat weight restriction placard installed in accordance with drawing 4-7003.

FAA holder: Revo Inc

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