STC SA1091SW

Supplemental type certificate · Century Flight Systems Inc

Holder
Century Flight Systems Inc · United States
Status
Current · Reissued
Status date
July 9, 1984
Applied
September 18, 1969
Product
Aircraft · Small Multi-Engine
Certification basis
Part 21
Data sheet
TCDS1A10

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

What it approves

Installation of Mitchell automatic flight system FD/AP 282-184 consisting of flight director/autopilot with optional automatic electric pitch trim and automatic aileron stabilizer back-up

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.

iSte*a4j£a£i&n&'- £J**:ut Btpartment of ^transportation — .federal atoiation administration Supplemental 'Cgpe Certificate SA1091SW Century Flight Systems, Inc.

P.M. 1195 P. 0. Box 610 Mineral Wells, TX 76067 ma£> aj**rw tf> 'Sa Civil Air 1 A 1 U Piper PA-23-235, PA-23-250, PA-E23-250 -JttAfnfiit&n, 4tf,,tySLe -S'*A*&n Installation of Mitchell Automatic Flight System Model FD/AP 282-184 consisting of Flight Director/Autopilot with optional automatic electric pitch trim and automatic aileron stabilizer back-up (Piper AutoFlite Model AK185) according to Mitchell Bulletin No. 396 dated March 12, 1971.

See Continuation Sheet, Page 2, a part of this STC . September 18, 1969 November 6, 1969 "ith other A Jtapproved modifications fU: i-F tf dne 4-26-71; 7-9-84, Revision 2 Don P. Watson Manager, Aircraft Certification Division Southwest Region

This certificate may be transferred in accordance uiith f-AR 21.17.

FAAFCMH II 10-2 (10-41)

Uitod JStara of antrira Bepartmem of ^transportation— federal Station administration Supplemental TCgpt Certificate(Continuation £heet) SA1091SW, Revision 2, dated 7-9-84 Limitations and Conditions:

FAA Approved Airplane Flight Manual Supplement dated 4-26-71 required for Automatic Flight System Model FD/AP 282-184.

FAA Approved Airplane Flight Manual Supplement dated 11-7-69 required for AutoFlite Model AK185.

When Automatic Flight System Model FD/AP 282-184 is installed on aircraft modified per STC SA909WE or modified per Aircraft Specification Item 113 C(g) , installation of AutoFlite Model AK185 is not eligible.

Any alteration of this cettifieatt is punishable by a Jim of not exceeding fl,000, or imprisonment not exceeding 3 years, or both.

FAA FORM AMO-Z-1 (1040) Tfo eahjieiat may tt tiauftnid in aaordanct with FAR 21.47.

I NS I R 11; 1 IONS The transfer endorsement below may he used to notil> the ,i|>|in>priaic I-'A A r'cgiiinal Office (if the ti'dnUci i)l this Supplemental Ty|i< Ceniiicair.

1 he F A A ^ill [Tissue the rertiht ate in f lie name ol the transferee and lor v\ arc] n 10 turn.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name oj transferee) (Address of transferee)._._.,_ (Jtumbtr and ttreetj (Ci/>, Slab, ami ZIP cad,) from (Name ofg'antnr) (Print 01 type) (Address oj grantor) r anil slreel) ICitf,SlaU, a 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 · 3

MakeModelData sheet
Piper Aircraft Inc.PA-23-2351A10
Piper Aircraft Inc.PA-23-2501A10
Piper Aircraft Inc.PA-E23-2501A10