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FAA-listed STC holder

Teledyne Controls STCs

The Jun 30, 2026 FAA DRS snapshot lists 69 selected supplemental type certificates with status Current under Teledyne Controls. The records span 270 public aircraft directories and 4 modification categories. This is a research directory, not a claim that any specific kit or service is currently offered.

69
listed Current at snapshot
270
aircraft directories
4
modification categories
Sep 30, 2021
latest recorded revision

Modification mix

Other aircraft modifications50
Avionics15
Aircraft connectivity2
Engine and powerplant2

Aircraft represented

Boeing 737-700 Series712 STCsBoeing 737-800 Series675 STCsBoeing 767-300 Series596 STCsBoeing 737-300 Series522 STCsBoeing 747-400 Series518 STCsBoeing 757-200 Series510 STCsBoeing 737-200 Series433 STCsBoeing 737-400 Series411 STCsBombardier BD-700-1A10397 STCsBoeing 767-200 Series357 STCsBoeing 747-200B Series341 STCsBoeing 777-200 Series325 STCsBoeing 737-500 Series323 STCsBoeing 747-100 Series293 STCsBoeing 737-900 Series292 STCsBoeing 737-600 Series255 STCsBoeing 737-900ER Series235 STCsBoeing 747-200C Series200 STCsBoeing 747-300 Series200 STCsBoeing 747-200F Series192 STCs

Recently revised records

Showing the 69 most recently revised records. Category directories provide the complete paginated discovery path.

SA00959WIAvionics

Installation of SPIRENT Systems Wichita Cabin Information Display System in Cessna Model 525 aircraft. Data required: (1) Spirent Systems Installation Manual, Publication Number 90006-003-011, Revision B, dated April 2, 2001; (2) Spirent Systems Wichita Drawing Number 90006-003-015, Revision IR, FAA Approved Airplane Flight Manual Supplement (AFMS), dated April 12, 2001; or later FAA Approved Revisions to (1) or (2). or, Installation of SPIRENT Systems Wichita Cabin AvVisor Plus Information Display System in Cessna Model 525 aircraft. Data required: (3) Spirent Systems Installation Manual, Publication Number 90007-003-011, Revision C, dated January 9, 2003; (4) Spirent Systems Wichita Drawing Number 90007-003-016, Revision IR, FAA Approved Airplane Flight Manual Supplement (AFMS), dated January 10, 2003; or later FAA Approved Revisions to (3) or (4).

FAA holder: Teledyne Controls

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SA2470CEAvionics

Installation of B&D Instruments & Avionics, Inc. Electronic Propeller Gear Box Oil Pressure/Temperature Indicator. Data required: (1) for the Model SF340A, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7330-003-011, dated January 23, 1989, or later FAA Approved revision; (2) for the Model SF340B, B&D Instruments and Avionics, Inc. Installation Manual Part No. 7330-003-011, Revision B, dated August 29, 1989, or later FAA Approved revision; and (3) copy of this certificate.

FAA holder: Teledyne Controls

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SA2471CEAvionics

Installation of B&D Instruments & Avionics, Inc. Electronic Engine Oil Pressure/Temperature Indicator. Data required: (1) for the Model SF340A, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7380-003-024, dated January 23, 1989, or later FAA Approved revision; (2) for the Model SF340B, B&D Instruments and Avionics, Inc. Installation Manual Part No. 7380-003-024, dated August 29, 1989, or later FAA Approved revision; and (3) copy of this certificate.

FAA holder: Teledyne Controls

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SA2472CEAvionics

Installation of B&D Instruments & Avionics, Inc. Electronic Gas Generator Speed Indicator. Data required: (1) for the Model SF340A, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7320-003-011, dated January 23, 1989, or later FAA Approved revision; for the Model SF340B, B&D Instruments and Avionics, Inc. Installation Manual Part No. 7320-003-011, Revision B, dated August 29, 1989, or later FAA Approved revision; (2) for the SF340A or SF340B, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7321-004-011 dated September 12, 1989, or later FAA Approved revision; and (3) copy of this certificate.

FAA holder: Teledyne Controls

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SA2473CEAvionics

Installation of B&D Instruments & Avionics, Inc. Electronic Torque Indicator. Data required: (1) for the Model SF340A, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7300-003-011, dated January 23, 1989, or later FAA Approved revision; (2) for the Model SF340B, B&D Instruments and Avionics, Inc. Installation Manual Part No. 7300-003-011, Revision B, dated August 29, 1989, or later FAA Approved revision; (3) for the SF340A or SF340B, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7301-003-011 dated September 12, 1989, or later FAA Approved revision; and (4) copy of this certificate.

FAA holder: Teledyne Controls

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SA2493CEAvionics

Installation of B&D Instruments & Avionics, Inc. Electronic Interturbine Temperature Indicator. Data required: (1) for the Model SF340A, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7340-003-022, Revision A, dated March 13, 1989, or later FAA Approved revision; (2) for the Model SF340B, B&D Instruments and Avionics, Inc. Installation Manual Part No. 7340-003-022, Revision D, dated August 29, 1989, or later FAA Approved revision; and (3) copy of this certificate.

FAA holder: Teledyne Controls

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SA2494CEAvionics

Installation of B&D Instruments & Avionics, Inc. Electronic Propeller Speed Indicator. Data required: (1) for the Model SF340A, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7310-003-011, dated January 23, 1989, or later FAA Approved revision; (2) for the Model SF340B, B&D Instruments and Avionics, Inc. Installation Manual Part No. 7310-003-011, Revision B, dated August 29, 1989, or later FAA Approved revision; (3) for the SF340A or SF340B, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7311-004-011 dated September 12, 1989, or later FAA Approved revision; and (4) copy of this certificate.

FAA holder: Teledyne Controls

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ST00084WIEngine and powerplant

Replacement of the Exhaust Gas Temperature indicators with B&D Instruments Models 65006-003, 65006-004, 65006-005, 65006-006, 65006-007. Recording Exhaust Gas Temperature indictors in accordance with B&D Installation Manual 65006-003-011, Revision D dated November 19, 1996 or later FAA approved revision; and Flight Manual Supplement 65006-003-013 dated July 26, 1993, Flight Manual Supplement 65006-003-014 dated October 3, 1994, or Flight Manual Supplement 65006-003-015, 65006-003-16 or 65006-003-017 dated November 16, 1996.

FAA holder: Teledyne Controls

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ST00700WIEngine and powerplant

Installation of Penny & Giles Recording Exhaust-Gas Temperature Indicator 65009-004 EGT in accordance with: (1) Penny & Giles Aerospace, Inc. Recording EGT Model 65009 Installation Manual Document #65009-004-011, Revision -, dated May 1, 1998; and (2) Penny & Giles Aerospace, Inc. Airplane Flight Manual Supplement (AFMS) Drawing #65009-004-013, Revision "original", dated August 19, 1998; or later FAA Approved Revisions to (1) or (2).

FAA holder: Teledyne Controls

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