# STC SA845GL

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Knots 2U, Ltd
- Description: Install stabilizer reinforcing plate.
- Status date: May 7, 1997
- Data sheets: 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/20B33FCB6E4DD70785256CC20058E7C3.0001
- Page: https://openairdocs.org/stc/SA845GL

## ADs that name it

- [AD 94-20-04 R2](https://openairdocs.org/ad/94-20-04-R2): Empennage aft fuselage · Remove V tail and install a Beech Model F33A straight tail (D'Shannon Products STC SA2149CE). Effective Jun 27, 2003
- [AD 94-20-04 R1](https://openairdocs.org/ad/94-20-04-R1) (historical): V-tail · Remove V tail and install a Beech Model F33A straight tail (D'Shannon Products STC SA2149CE). Effective Dec 10, 2002
- [AD 94-20-04](https://openairdocs.org/ad/94-20-04) (historical): V-Tail Structure · Remove V tail and install a Beech Model F33A straight tail (D'Shannon Products STC SA2149CE). Effective Nov 28, 1994

## Approved models (10)

- Raytheon Aircraft Company H35 (TCDS 3A15)
- Raytheon Aircraft Company J35 (TCDS 3A15)
- Raytheon Aircraft Company K35 (TCDS 3A15)
- Raytheon Aircraft Company M35 (TCDS 3A15)
- Raytheon Aircraft Company N35 (TCDS 3A15)
- Raytheon Aircraft Company P35 (TCDS 3A15)
- Raytheon Aircraft Company S35 (TCDS 3A15)
- Raytheon Aircraft Company V35 (TCDS 3A15)
- Raytheon Aircraft Company V35A (TCDS 3A15)
- Raytheon Aircraft Company V35B (TCDS 3A15)

---
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.