# STC SE35WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Garrett Turbine Engine Company 
Division of Garret Corporation, United States
- Description: Modification of the fuel control, linkage to permit 75% r.p.m. for low ground idle.
- Applied: February 13, 1967
- Status date: February 9, 1981
- Product: Engine
- Certification basis: Part 21
- Data sheets: [TCDS E2WE](https://openairdocs.org/tcds/E2WE)
- Certificate PDF: https://openairdocs.org/files/sha256/c8/62/c862eec63cf0a262d27bf88d7c91c18ba5f799dfe6286d7e5eaa877f7bdceeb0
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3C4333F9BAA2BB2386257361006F697F.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SE35WE

## ADs that name it (0)

None.

## Approved models (1)

- Honeywell International Inc. TPE331-47 ([TCDS E2WE](https://openairdocs.org/tcds/E2WE))

## 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.

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i)epartmentof1:ransportation-jederal s:llliations:ldminiStretion ~upplcmcntBI~HPCQ:crtificBtC ~ SE35WE JrL'~-aa/",~4, Garrett Turbine Engine Company, A Division of the Garrett Corporation 402 S. 36th St.

Phoenix, Arizona 85034 ~~ d",z,/h ..Aa7r~~~,d",?n,/"./k/,./6~''';',?/''v"k.z~d~h:'TU/''U~i~~-<~4~, ~~"'jW~k-~#ru.-/4/h"'ffl,"".d'~_7",~~/4,!,9-/ 13 -¥~ Civil Air tLrnd.(~H'~-.~ ~</-aa/'~m/_ E2WE Ju', Garrett (Ai Research) vlt~Id' TPE331-4 7 Turboprop Engi ne, SIN 61402, (; r~- (;' SIN 61403, SIN 61406, SIN 61407, SIN 61409 9J-&1c"'i\/.wn,,!,Jr!d:'~,n,fik'r' Modi fication of the fuel control linkage to pennit 75% r.p.m. for low ground idle. Modification Number 869344-1. Change C.

"£'TUln/u~"'1dC.~d,4~., •.•, This approval should not be extended to toher speci fic engines of this model on which other previously approved modifications are incorporated unless it is detennined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that engine.

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February 9, 1981 Engineering &Manufacturing Branch (T'flt) A '!)-'alina/ion of this urtifieatr ,'j punishable b}' a fin, of not (xcudin,'i SI,OOO. or Imprisonmtnl nol rxcudin.e. 3 ,rca,s, or both.

fAA f()LloO8110-2 (10-68) Page 1 of 2 Pag' TillS (tTl/fiealt m~. bt trrmsfaud In auordanu wIll, !-.4/' -./ +7

## Every issue (1)

- February 9, 1981: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/c8/62/c862eec63cf0a262d27bf88d7c91c18ba5f799dfe6286d7e5eaa877f7bdceeb0)

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