STC SA3489SW-D

Supplemental type certificate · Century Flight Systems Inc

Holder
Century Flight Systems Inc · United States
Status
Current · Amended
Status date
March 31, 1997
Applied
December 10, 1991
Product
Aircraft · Small Airplane
Certification basis
Part 21
Data sheet
TCDS3A15

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of a Century automatic flight system model AK996 consisting of a Century 2010/2030/2031/2050/2051 autopilot

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

United States of America iurait of dfcangpnriattou -Jfeitetal j^iriation Oferftftcate SA3489SW-D certificates i< Century Flight Systems, Inc.

3003 FM 11 95 P.O. Box610 Mineral Wells, TX 76067 t^wcl&4i<;^^wt/i&£olk>€t^^ 3 ofiftw Civil Aeronautics 3A1 5 BEECH 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, E33C, F33, F33A, (S/N 315 & Below), F33C, (S/N CJ- 30 & Below), and G33.

Installation of a Century Automatic Flight System, Model AK996 consisting of a Century 2010/2030/2031/2050/2051 Autopilot per Bulletin No. 2054, dated 01-03-92, Revision 3 dated 03-17-97 and Master Drawing List No. 87A1218, dated 01-03-92, Revision C dated 03-17-97 (14 Volt System) or later FAA/DAS Approved Revision.

FAA/DAS Approved Supplement to Pilot's Operating Handbook and/or FAA/DAS Approved Airplane Flight Manual Supplements P/N 68S1053, dated 01-06-92 Rev. 2 dated 03-24-97 or later FAA/DAS Approved Revision and Century 2000 Autopilot Operator's Manual P/N 68S1035, dated 07- 15-86 Rev. 02-07-97 or later FAA Approved Revision. Century Yaw Damper Kit No. YK997, STC SA3449-D is compatible with, but not required by this modification.

This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of the aircraft.

arid' && mfifi&vtirup tteUa' i& the- &a&t& fiyv ajifvunnU' 12-10-91 01-10-92 .- 12-21-92 Rev. 2; 03-31-97 Rev. 3 (Signature) William R. Watson DAS Staff Coordinator DAS 7 SW (Title) Anv alteration of this certificate is punishable bv a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both.

FAA Foim 8110-2(10-68)

.NSTRUCTIONS: The tracer endorsement below m.y be used to notify the appropriate FAA Regional Office of the transfer of this Supplemental Type Certificate.

The FAA will reissue the certificate in the name of the transferee and forward it to him.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee)_ (Address of transferee) from (Name of grantor) (Print or type).

(Address of grantor) I Cit>: Stalt, Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

ADs that name this STC · 0

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

No AD in this release names this STC

Approved models · 12

MakeModelData sheet
Beechcraft Corporation35-333A15
Beechcraft Corporation35-A333A15
Beechcraft Corporation35-B333A15
Beechcraft Corporation35-C333A15
Beechcraft Corporation35-C33A3A15
Beechcraft CorporationE333A15
Beechcraft CorporationE33A3A15
Beechcraft CorporationE33C3A15
Beechcraft CorporationF333A15
Beechcraft CorporationF33A3A15
Beechcraft CorporationF33C3A15
Beechcraft CorporationG333A15