What it approves
Installation of S-TEC System 60 pitch stabilization system Model ST-111 with optional electric trim system.
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.
• . Slta*Aca&-t>- ttmcrd Sow of 3arrica Btpartmcnt of transportation —federal atnarion administration Supplemental t^pe Certificate SA5213SW-D S-TEC Corporation Rt, 4, Bldg, 946 Wolters Industrial Complex Mineral Wells, TX 76067 t4iiit'rtrr 2 A 1 3 PIPER ^tf J& '3SLa PA-28-140, PA-28-150, PA-28-160, PA-28-180 AND PA-28-235 na£ .
l I Ml P Installation of S-TEC System 60 Pitch Stabilization System, Model ST-111, with Optional Automatic Electric Trim System according to Bulletin No, 214, Revision 3, dated 3-11-85 and Master Drawing List No, 92121, Revision C, dated 3-11-85 and/or later FAA Approved revisions of the above data (14 Volt System), -
1. Eligible only on Piper Model PA-28-235, S/N 28-10003 through S/N 28-7210023.
2. Piper Model PA-28-235, S/N 28-10720 through S/N 28-7210023 not eligible for Optional Automatic Electric Trim System.
(See Continuation Sheet, Page 2, a part of this STC.)
aA^jF&jy^^ Je*^rijsn*a£U>n^ && SXdfntnt^fa/^r-^f^Jin^ 6-08-84, 4-03-85, Revision 26-24-83 10-04-83 (Signature) Harold W. Holdeman DAS Staff Coordinator, DAS 5—__
T/ta arti/tcale may ke tnuu/imj in tcttrJanet with FAR 21.47.
fAA Paw I110-1 (10-*«)
tinitrd £tatu of SLntnca Btpartment of ^transportation—federal a&iation administration topplemcntal HTjipe Certificate(CDntinuation ^hEtt) SA5213SW-D, Revision 2 Limitations and Conditions (con't).
3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89141-1, dated 10-04-83 is required for Piper Models PA-28-140, PA-28-150, PA-28-160, PA-28-180, S/N 28-1 through S/N 28-7205318 and PA-28-235, S/N 28-10003 through S/N 28-10719 and/or later FAA Approved revisions of the above supplement,
4. FAA Approved Supplement to Pilot's Operating Handbook arid/or FAA Approved Airplane Flight Manual, P/N 89142-1, dated 10-04-83 is required for Piper Models PA-28-235, S/N 28-10720 through S/N 28-7210023 and/or later FAA Approved revisions of the above supplement,
5. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89492, dated 6-08-84 is required for Piper Model PA-28-180, S/N 28-E13 and S/N 28-7305001 and up, and/or later FAA Approved revisions of the above supplement.
6. Compatability of this modification with other previously approved modifications must be determined by the installer.
!• ..'-' ;' •'.' <•/ this i certificate is puni shablt by a fine c/f not exccdiny, Sl.^fiO, or imprisonment nut exreedin^ J it'.'.vi, i-t !"•!'• A.-, f OR-.- 8HU-2-I (10-69) This certificate may be trantjirrtd in accordance irith i~Alt -I >' PAGE 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, Slate, and £IP code) from (Name of grantor) (Print or type) .
(Address of grantor) (Number and street) (City, State, and ^IP code) Extent of Authority (if licensing agreement):
Signature of grantor (In ink):.
U.S. GOVERNMENT PRINTING OFFICE : 1966 OF — 205-579
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