STC SA6069SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Amended
Status date
October 13, 1992
Applied
May 14, 1986
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS1A15

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

What it approves

Installation of S-TEC manual electric trim system, Model ST-358.

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.

Bqjartrarnt of transportation—Jfataal 3tnarion administration Supplemental "Cgpe Certificate SA6069SW-D S-TEC Corporation 946 Pegram Wolters Industrial Park Mineral Wells, Texas 76067 yy< fturtt fJM>i£h <&*J£jmt/a/timA' **»** efru&£umA, Civil Air 1A15 piper PA-24 (PA-24-180), PA-24-250, PA-24-260, Installation of S-TEC Manual Electric Trim System, Model ST-358, according to Bulletin No. 458, Revision 2, dated 9-01-92 and Master Drawing List No. 92376, Revision B, dated 9-01-92 and/or later FAA Approved revisions of the above data (14 Volt System).

1. Also eligible on Piper Models PA-24 (PA-24-180), PA-24-250, and PA-24-260 When Modified In Accordance With STC SA4-1351 or STC SA4-1235 As Applicable (Wing Tip Tanks) .

(See Continuation Sheet, Page 2, a part of this STC.)

5-14-86 2L*~**~J:

6-06-86 9Ls,.*~mAJ. 9-23-86, 10-13-92, Revision 2 *--2_— William J. ThomasHAS (Till*) Any alteration oftUs ttrtifitat* it pttnifkablt ty a fin* of not txettding SI ,000, or imprisonment not txtttding 3 years, ot both.

Tkit ojrti/fettt may *r timtftmd m ucnrdtntt witk FAR 21.17.

*** ta«> •! to-1 ( l*-M|

United £ksuzi of 3atm Bepartment of Transportation— federal SMation administration Supplemental ICgpe Certificate (Continuation £hett) SA6069SW-D, Revision 2 Limitations and Conditions (con't.)

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89667, dated 6-06-86 is required for Piper Models PA-24 (PA-24-180), PA-24-250, and PA-24-260, S/N 24-4803 and Below (Except S/N 24-4783) And The Above Models When Modified In Accordance With STC SA4-1351 or STC SA4-1235 As Applicable (Wing Tip Tanks) and PA-24-400 and/or later FAA Approved revisions of the above supplement.

3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89667-1, dated 10-13-92 is required for Piper Models PA-24 (PA-24-180), PA-24-250, and PA-24-260 And The Above Models When Modified In Accordance With STC SA4-1351 or STC SA4-1235 As Applicable (Wing Tip Tanks) and PA-24-400 and/or later FAA Aprpoved revisions of the above supplement.

4. Compatibility of this modification with other previously approved modifications must be determined by the installer.

. lnv alteration of this certificate is punishable by afint of not exceeding tl,000, or imprisonment not exceeding 3 years, or hnih.

PA* FORM «iiu.l-i (104*1 TAii tatiftalt mty Iti ttmtfirrni in accordant! with b'AR :'/.•*?.

PAGE 2 or 2 PAGES

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee)——————————__———————————-———— (Address of transferee) ———————————————-———— (City.Staff. *ndZIP from (Name of grantor) (Print or type) ————-———————-——————— (Address of grantor) (Xvmltr fitJ tit«ti 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 · 4

MakeModelData sheet
Piper Aircraft Inc.PA-241A15
Piper Aircraft Inc.PA-24-2501A15
Piper Aircraft Inc.PA-24-2601A15
Piper Aircraft Inc.PA-24-4001A15