What it approves
Installation of S-TEC System 60 pitch stabilization system Model ST-057.
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.
^Department of Transportation—Jfntaal 9tnation SUmntistration Supplemental 'Cgpe Certificate SA5205SW-D -tr/ytft* A4mfnr-4mna
- S-TEC Corporation 946 Pegram Wolters Industrial Park Mineral Wells, Texas 76067 in mt faflf fntyfnjtfr £\t fAt /ttm'taft'tw* mn</ efnt/t'A C "i V 1 1 Air 1A15 PIPER PA-24 (PA-24-180), PA-24-250, PA-24-260, AND PA-24-400 Installation of S-TEC System 60 Pitch Stabilization System, Model ST-057, with Optional Automatic Electric Trim System according to Bulletin No. 160, Revision 3, dated 6-03-92 and Master Drawing List No. 9254, Revision C, dated 6-03-92 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.)
: 5-19-83 9-13-83 SXc6n*niL&*a£i>r-^'jA* &...m*~^: 4-10-86, 6-10-92, Revision 2 ittat) Williafn J. Thomas DAS Staff Coordinator, DAS 5 SW (TtiU) fine of not exceeding tljDOO, or imprisonment not exceeding 3 yean, or both.
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•Department of Transportation— .federal action administration Supplemental ICgpe Certificate(Continuation £heet) SA5205SW-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 8958-1, dated 9-13-83 is required for Piper Models PA-24 (PA-24-180), PA-24-250, and PA-24-260, S/N 24-4803 & 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/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 8958-2, dated 6-10-92 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/or later FAA Approved revisions of the above supplement.
4. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89652, dated 4-10-86 is required for Piper Model PA-24-400 and/or later FAA Approved revisions of the above supplement.
5. Compatibility of this modification with other previously approved modifications must be determined by the installer.
.•Inv alteration of this catifuatt is puniihablt by a fiat of not txcttding 17,000, or imprisonment not txcetding 3 years, or bmh.
f AA FONM •tio.a-i (to^») This artificalt mty bi umtjtntd in oceorJanet with FAR .V.V~ PAGC 2 OF 2 PAGES
TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and ZJP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and %1P code) Extent of Authority (if licensing agreement):
Signature of grantor (In ink):
U.S. GOVERNMENT PRINTING OFFICE r 1966 OF —205-579
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.