# STC SA00812NY

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Technisonic Industries Limited, Canada
- Description: Installation of Technisonic Industries Limited TFM-138, A, and B (does not include TFM-138, s/n 1540 and up, TFM-138B, s/n 1500 and up).
- Applied: December 23, 1997
- Status date: September 12, 2005
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A12](https://openairdocs.org/tcds/3A12), [TCDS 3A13](https://openairdocs.org/tcds/3A13), [TCDS 3A24](https://openairdocs.org/tcds/3A24), [TCDS 5A6](https://openairdocs.org/tcds/5A6), [TCDS A37CE](https://openairdocs.org/tcds/A37CE), [TCDS A4CE](https://openairdocs.org/tcds/A4CE), [TCDS 2A13](https://openairdocs.org/tcds/2A13), [TCDS A3SO](https://openairdocs.org/tcds/A3SO), [TCDS 2A4](https://openairdocs.org/tcds/2A4), [TCDS 6A1](https://openairdocs.org/tcds/6A1)
- Certificate PDF: https://openairdocs.org/files/sha256/c0/b3/c0b3b4f8d10af625df284050507a9bc9b35bbe5987c4147fb3d56da94a316c5e
- Approved model list and other attachments: [SA00812NYaml.pdf](https://openairdocs.org/files/sha256/51/60/5160e90ec45a35811b4e6e2e6309a645724bea60bfc2fcaaa7d51328eadf5065)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/24BF2F30761EF1AF862570C700709D4F.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00812NY

## ADs that name it (0)

None.

## Approved models (141, first 50)

- The Cessna Aircraft Company 172 ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- The Cessna Aircraft Company 172A ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- The Cessna Aircraft Company 172B ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- The Cessna Aircraft Company 172C ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- The Cessna Aircraft Company 172D ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- The Cessna Aircraft Company 172E ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- The Cessna Aircraft Company 172F (USAF T-41A) ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- The Cessna Aircraft Company 172G ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- The Cessna Aircraft Company 172H (USAF T-41A) ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- The Cessna Aircraft Company 172I ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- The Cessna Aircraft Company 172K ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- The Cessna Aircraft Company 172L ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- The Cessna Aircraft Company 172M ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- The Cessna Aircraft Company 172N ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- The Cessna Aircraft Company 172P ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- The Cessna Aircraft Company 172Q ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- The Cessna Aircraft Company 172R ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- The Cessna Aircraft Company 180 ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180A ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180B ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180C ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180D ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180E ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180F ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180G ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180H ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180J ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180K ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182A ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182B ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182C ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182D ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182E ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182F ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182G ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182H ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182J ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182K ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182L ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182M ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182N ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182P ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182Q ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182R ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182S ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 185 ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- The Cessna Aircraft Company 185A ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- The Cessna Aircraft Company 185B ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- The Cessna Aircraft Company 185C ([TCDS 3A24](https://openairdocs.org/tcds/3A24))

All 141: https://openairdocs.org/stc/SA00812NY/models.md

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

FAA Form 8110-2(10-68) Page 1 of 3 IMPORT Number SA00812NY This certificate issued to Technisonic Industries Limited 240 Traders Blvd. E Mississauga, Ontario L4Z 1W7 Canada

Part * of the * Regulations.

Original Product -- Type Certificate Number : * *See attached FAA Approved Model List (AML) No. SA00812NY for list of approved airplane models and applicable airworthiness regulations.

All TFM-138 series transceiver models are manufactured to TIL Engineering Release 921012, Revision B, dated November 24, 1997. The TFM-403 is manufactured to TIL Engineering Release 941059, Revision A, dated October 27, 1999. The TFM-500 is manufactured to TIL Engineering Release 971083, Revision N/C, dated March 16, 1999.

The TFM-30 is manufactured to TIL Engineering Release 961082, Revision N/C, dated April 19, 1999. The Remote Control RC-500 model is manufactured to TIL Engineering Release 991097, Revision N/C, dated November 17, 1999. The TDFM-136 is manufactured to TIL Engineering Release 981087, Revision N/C, dated January 13, 2000. The TFM-550 is manufactured to TIL Engineering Release 991095, Revision N/C, dated March 1, 2000.

(See Continuation Sheets 2 and 3) Limitations and Conditions :

1. Compatibility of this design change with previously approved modifications must be determined by the installer.

2. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

(See Continuation Sheets 2 and 3)

Date of application : December 23, 1997

Date of issuance : March 23, 1998 Date reissued : December 2, 2002, March 14, 2003

Date amended : February 5,1999; February 15, 2000;

November 14, 2000; December 18; 2002, February 25, 2003;

April 8, 2004; September 12, 2005

( Signature) Anthony Socias Manager, New York Aircraft Certification Office

(Title)

FAA Form 8110-2-1(10-69) Page 2 of 3

Number SA00812NY Date of Amendment: September 12, 2005

Description of Type Design Change (Continued):

The RC-550 is manufactured to TIL Engineering Release 991099, Revision N/C, dated March 27, 2000. The ATC-550 is manufactured to TIL Engineering Release 991102, Revision N/C, dated March 20, 2000. The TDFM-600/ 6000 Series VHF / UHF Low / UHF High / 800 MHz Multi-Band Transceiver is manufactured to TIL Engineering Release 011210, Revision A, dated June 20, 2004. The Remote Control RC-6000 is manufactured to TIL Engineering Release 021213, Revision N/C, dated October 17, 2002. The TFM-530 VHF/VHF Low FM Multi-band Transceiver model is manufactured to TIL Engineering Release 031216, Revision N/C, dated April 2003. The TFM-566 VHF/VHF Low FM Multi-band Transceiver model is manufactured to TIL Engineering Release 031217, Revision N/C, dated April 2003. The AMS-6000 Audio Mode Selector model is manufactured to TIL Engineering Release 031220, Rev. N/C, dated August 2003, or later Transport Canada approved revision. The TFM-66 VHF Low Band FM Transceiver model is manufactured to TIL Engineering Release 031218, Rev. N/C, dated September 19, 2003, or later Transport Canada approved revision. The TFM-556 VHF High/VHF Low/UHF Multi-band FM Airborne Transceiver model is manufactured to TIL Engineering Release 031219, Rev. N/C, dated September 23, 2003, or later approved revision.

Configuration 1: Installation of Technisonic Industries Limited TFM-138, -138A, and -138B, (does not include TFM-138, s/n 1540 and up, TFM-138B, s/n 1500 and up) in accordance with TIL Installation and Operating Manual 95RE177, Revision E, dated April 1998, or later Transport Canada approved revision.

Configuration 2: Installation of Technisonic Industries Limited TFM-138B, in accordance with TIL Installation and Operating Instructions Manual 97RE221, Revision N/C, dated November 1997, or later Transport Canada approved revision.

Configuration 3: Installation of Technisonic Industries Limited TFM-138C, in accordance with TIL Installation and Operating Instructions Manual 96RE192, Revision B, dated January 1997, or later Transport Canada approved revision.

Configuration 4: Installation of Technisonic Industries Limited TFM-138 (s/n 1540 and up with F10-B Software), in accordance with TIL Installation and Operating Instructions Manual 98RE229, Revision N/C, dated March 1998, or later Transport Canada approved revision.

Configuration 5: Installation of Technisonic Industries Limited TFM-403, in accordance with TIL Installation and Operating Instructions Manual 95RE175, Revision A, dated July 1998, or later Transport Canada approved revision.

Configuration 6: Installation of Technisonic Industries Limited TFM-500 in accordance with TIL Installation and Operating Instructions Manual 98RE243, Revision N/C, dated May 1999, or later Transport Canada approved revision.

Configuration 7: Installation of Technisonic Industries Limited TFM-30 in accordance with TIL Installation and Operating Instructions Manual 98RE244, Revision N/C, dated August 1999, or later Transport Canada approved revision.

Configuration 8: Installation of Technisonic Industries Limited RC-500 in accordance with TIL Installation and Operating Instructions Manual 99RE260, Revision N/C, dated January 2000, or later Transport Canada approved revision.

Configuration 9: Installation of Technisonic Industries Limited TDFM-136 in accordance with TIL Installation and Operating Instructions Manual 99RE255, Revision A, dated March 2000, or later Transport Canada approved revision.

Configuration 10: Installation of Technisonic Industries Limited TFM-550 in accordance with TIL Installation and Operating Instructions Manual 99RE262, Revision A, dated April 2000, or later Transport Canada approved revision.

Configuration 11: Installation of Technisonic Industries Limited RC-550 in accordance with TIL Installation and Operating Instructions Manual 00RE270, Revision N/C, dated March 7, 2000, or later Transport Canada approved revision.

FAA Form 8110-2-1(10-69) Page 3 of 3

Number SA00812NY Date of Amendment: September 12, 2005

Description of Type Design Change (Continued):

Configuration 12: Installation of Technisonic Industries Limited ATC-550 in accordance with TIL Installation and Operating Instructions Manual 00RE269, Revision A, dated May 8, 2000, or later Transport Canada approved revision.

Configuration 13: Installation of Technisonic Industries Limited TDFM-600/ 6000 series VHF / UHF Low/UHF High/ 800 MHz Multi-Band Transceiver in accordance with TIL Installation and Operating Instructions Manual 01RE293, Revision F, dated July 2004, or later Transport Canada approved revision.

Configuration 14: Installation of Technisonic Industries Limited RC-6000 in accordance with TIL Installation and Operating Instructions Manual 02RE299, Revision A, dated November 2002, or later Transport Canada approved revision.

Configuration 15: Installation of Technisonic Industries Limited TFM-530 VHF/VHF Low FM Multi-band Transceiver in accordance with TIL Installation and Operating Instructions Manual 03RE317, Revision B, dated September 2003, or later Transport Canada approved revision.

Configuration 16: Installation of Technisonic Industries Limited TFM-566 VHF/VHF Low FM Multi-band Transceiver in accordance with TIL Installation and Operating Instructions Manual 03RE318, Revision B, dated September 2003, or later Transport Canada approved revision.

Configuration 17: Installation of Technisonic Industries Limited AMS-6000 Audio Mode Selector in accordance with TIL Installation and Operating Instructions Manual 03RE325, Rev. N/C, dated June 2003, or later Transport Canada approved revision.

Configuration 18: Installation of Technisonic Industries Limited TFM-66 VHF Low Band FM Transceiver in accordance with TIL Installation and Operating Instructions Manual 03RE320, Rev. N/C, dated March 2003, or later Transport Canada approved revision.

Configuration 19: Installation of Technisonic Industries Limited TFM-556 VHF High/VHF Low/UHF Multi-band FM airborne Transceiver in accordance with TIL Installation and Operating Instructions Manual 03RE328, Rev. N/C, dated September 2003, or later Transport Canada approved revision.

3. Maintenance of the TDFM-600/ 6000 series VHF/UHF Lo w/UHF High/800 MHz Multi-Band Transceiver and RC-6000 Remote Control Head must be in accordance with Technisonic Industries Limited Instructions for Continued Airworthiness MMS02030- 1, Rev. B, Transport Canada Accepted December 12, 2003.

4. Maintenance of the TFM-530 and TFM-566 VHF/VHF Low FM Tr ansceiver must be in accordance with Technosonic Industries Limited Instructions for Continued Airworthiness MMS03055-1, Revision N/C, dated October 7, 2003.

5. Pressure vessel penetrations are not included in this approval. Any required pre ssure vessel penetrations require a separate approval.

6. Maintenance of the AMS-6000 Audio Mode Selector must be in accordance with Technisonic Industries Limited Instructions for Continued Airworthiness MMS02030-1 Rev. C, dated August 30, 2005, or later Transport Canada approved revision.

7. Maintenance of the TFM-66 VHF Low Band FM Transceive r and TFM-556 VHF High/HF Low/UHF Multi-band FM Airborne Transceiver must be in accordance with Technisonic Industries Limited Instructions for Continued Airworthiness MMS03099-1 Rev. A, dated August 30, 2005.

8. A copy of this certificate and the FAA Approved Model Li st (AML) No. SA00812NY, issued March 23, 1998, or later FAA approved revisions, must be maintained as part of the permanent records for the modified aircraft.

…END...

### SA00812NYaml.pdf

FAA APPR OVED MODEL LIST (AML) NO. SA00812NY Techni sonic Industries Limited For Installation of the TFM-30, -138, -138A, -138B, -138C, -403, -500, RC-500, TFM-66, TDFM-136, TFM-530, TFM-550, TFM-556, TFM-566, RC-550 and 6000, ATC-550 and TDFM-600/6000 Issue Dat e: March 23, 1998

Cessna Cessna 172,172A/B/C/D/E/F/G/H/I/K/L/M/N/P/Q, 172R 9/12/2005 2/15/2000 CAR 3 2A4 9/12/2005 CAR 3 6A1 Twin Commander Twin Commander 10 9 560-F, 680, 680 E/F/FL/FL(P)/T/V/W, 681, 685, 690, 690A/B/C/D, 695, 695 A/B, 720 500, 500-A, 500-B, -500S, 500-U, 520, 560, 560-A, 560-E PA-32-260, -32-300, -32S-300, -32R-300, -32RT-300, -32RT-300T, -32-301, -32R-301(SP), -32R-301(HP), -32R-301T, -32-301T N/A CAR 3 A3SO Piper 8 CAR 32A13 7 PA-28-140, -28-150, -28-160, -28-180,-28-235, -28R-180 -28S-160, -28S-180,-28R-200, -28-151, -28-161, -28-181, -28R-201, -28R-201T,-28-236, -28RT-201, -28-201T Cessna 5 6 A37CE A4CE FAR 23 CAR 3206, P206, P206A/B/C/D/E, TP206A/B/C/D/E, U206, U206A/B/C/D/E/F/G, TU206A/B/C/D/E/F/G N/A N/A208,208A,B Cessna Cessna N/A N/A N/A185,185A/B/C/D/E, A185E/F 182,182A/B/C/D/E/F/G/H/J/K/L/M/N/P/Q/R, 182S,R182, T182, TR182 180,180A/B/C/D/E/F/G/H/J/K CAR 3 CAR 3 CAR 3 Cessna 5A6 3A13 3A24 4 3 2 1 N/A AML

**AMENDMENT DATE 3A12 CAR 3**

**CERTIFICATE**

**BASIS FOR**

**ALTERATION**

**ORIGINAL TYPE**

**CERTIFICATE NUMBER**

**AIRCRAFT MODEL**

**AIRCRAFT**

MAKE ITEM Piper FAA Approved:____________________________ Anthony Socias Manager, New York Aircraft Certification Office Amended: September 12,2005 Page 1 of 1

## Every issue (1)

- September 12, 2005: Amended, Current. [certificate](https://openairdocs.org/files/sha256/c0/b3/c0b3b4f8d10af625df284050507a9bc9b35bbe5987c4147fb3d56da94a316c5e), [SA00812NYaml.pdf](https://openairdocs.org/files/sha256/51/60/5160e90ec45a35811b4e6e2e6309a645724bea60bfc2fcaaa7d51328eadf5065)

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