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STC SA845GL

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Supplemental type certificate · Knots 2U, Ltd

Certificate· on FAA DRS
Holder
Knots 2U, Ltd · United States
Status
Current · Reissued
Status date
May 7, 1997
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS3A15

From FAA DRS. DRS record last changed December 6, 2025.

What it approves

Install stabilizer reinforcing plate.

ADs that name this STC · 3

An AD can apply because an STC is installed, or mention one in its text.

AD 94-20-04 R2Empennage aft fuselage · Remove V tail and install a Beech Model F33A straight tail (D'Shannon Products STC SA2149CE)Effective Jun 27, 2003 · Supersedes AD 94-20-04 R1 · Cited in the textAD 94-20-04 R1HistoricalV-tail · Remove V tail and install a Beech Model F33A straight tail (D'Shannon Products STC SA2149CE)Effective Dec 10, 2002 · Replaced by AD 94-20-04 R2 · Cited in the textAD 94-20-04HistoricalV-Tail Structure · Remove V tail and install a Beech Model F33A straight tail (D'Shannon Products STC SA2149CE)Effective Nov 28, 1994 · Replaced by AD 94-20-04 R1 · Cited in the text

Approved models · 10

MakeModelData sheet
Raytheon Aircraft CompanyH353A15
Raytheon Aircraft CompanyJ353A15
Raytheon Aircraft CompanyK353A15
Raytheon Aircraft CompanyM353A15
Raytheon Aircraft CompanyN353A15
Raytheon Aircraft CompanyP353A15
Raytheon Aircraft CompanyS353A15
Raytheon Aircraft CompanyV353A15
Raytheon Aircraft CompanyV35A3A15
Raytheon Aircraft CompanyV35B3A15