# STC SE445GL

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Shadin Avionics
- Description: Incorporation of a fuel flow transducer.
- Status date: June 8, 2006
- Data sheets: E14EA, E14EA, E14EA, E14EA, E14EA, E14EA, E14EA, E14EA, E14EA, E14EA, E14EA, E14EA, E14EA
- Certificate PDF: https://openairdocs.org/files/sha256/d9/60/d96043d7858095eee4f119d084b24109b362cca9807e0fb190a9ff21438db04d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/85CD9C09AFFF8572862575E50058D929.0001
- Page: https://openairdocs.org/stc/SE445GL

## ADs that name it

None.

## Approved models (13)

- Textron Lycoming AVCO Corporation LTIO-540-F2BD (TCDS E14EA)
- Textron Lycoming AVCO Corporation LTIO-540-J2BD (TCDS E14EA)
- Textron Lycoming AVCO Corporation TIO-540-A1A (TCDS E14EA)
- Textron Lycoming AVCO Corporation TIO-540-A1B (TCDS E14EA)
- Textron Lycoming AVCO Corporation TIO-540-A1C (TCDS E14EA)
- Textron Lycoming AVCO Corporation TIO-540-A2A (TCDS E14EA)
- Textron Lycoming AVCO Corporation TIO-540-A2B (TCDS E14EA)
- Textron Lycoming AVCO Corporation TIO-540-A2C (TCDS E14EA)
- Textron Lycoming AVCO Corporation TIO-540-AB1AD (TCDS E14EA)
- Textron Lycoming AVCO Corporation TIO-540-C1A (TCDS E14EA)
- Textron Lycoming AVCO Corporation TIO-540-F2BD (TCDS E14EA)
- Textron Lycoming AVCO Corporation TIO-540-J2BD (TCDS E14EA)
- Textron Lycoming AVCO Corporation TIO-540-S1AD (TCDS E14EA)

## 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.

Number SE445GL This certificate issued to

Part 13 of the Civil Air Regulations.

(See Type Certificate Data Sheet E14EA for complete certification basis.)

Incorporation of a Fuel Flow Transducer in accordance with Shadin Company Report number 4020, revised September 14, 1988, or later FAA approved revision.

1) This approval should not be extended to other engines of these models on which other previsouly approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any other previously approved modifications will introduce no adverse effect upon the airworthiness of these engines.

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.

Shadin Avionics 6831 Oxford Street St. Louis Park, MN 55426 E14EA Make : Lycoming Model : T10-540-A1A, -A2A, -A2B, -A1C, -A2C, -A1B, -C1A, -F2BD, -J2BD, -S1AD, AB1AD, LT10-540-F2BD, and –J2BD Date of application : July 31, 1980

Date of issuance : September 15, 1980

Date reissued : June 8, 2006

Date amended : October 12, 1984, October 31, 1985, December 16, 1988

( Signature) Charles L. Smalley Manager, Systems & Flight Test Branch Chicago Aircraft Certification Office

(Title)

## Every issue (1)

- June 8, 2006: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/d9/60/d96043d7858095eee4f119d084b24109b362cca9807e0fb190a9ff21438db04d)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.