What it approves
Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System, Model ST-607, with Optional Autotrim System. Limited to Piper models PA-23-250 and PA-E23-250, s/n 27-2000 through s/n 27-7554172. Eligible on same models when equipped with approved turbocharged engines (250 hp) and/or wing tip tanks per STC SA1480WE.
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.
Number SA09123AC-D
This Certificate issued to S-TEC Corporation One S-TEC Way Mineral Wells Municipal Airport Mineral Wells, TX 76067-9236
Part 3 of the Civil Aviation Regulations. 1A10 Original Product Type Certificate Number :
Make : Piper Model : PA-23-250, PA-E23-250, and PA-23-235
Installation of S-TEC Sy stem 55/55X Two Axis Autom atic Flight Guidance System, Model ST-607, according to Master Drawing List No. 92810, Revision C, dated 8-08-07 or later FAA Approved revisions of the above data (14 Volt System).
(See Continuation Sheet, Page 3, a part of this STC.)
1. Compatibility of this modification with other previously approved modifications must be determined by the installer.
Date of application : 10-04-95 Date of issuance : 10-12-95 Date reissued :
Date amended : 2-19-01, 8-29-07 By direction of the Administrator
(Signature)
James W. Smisek DAS 100.2 DAS Administrator, DAS700096SW (Title)
FAA Form 8110-2-1(10-69) Page 2 of 4
Transfer the ownership of Supplemental Type Certificate Number
to (Name of transferee)
(Address of transferee) (Number and street)
(City, State, and ZIP code)
from (Name of grantor) (Print or type)
(Address of grantor) (Number and street)
(City, State, and ZIP code)
Signature of grantor (In ink):
FAA Form 8110-2-1(10-69) Page 3 of 4
Number SA09123AC-D Date Amended 8-09-07
Limitations and Conditions (con’t.)
2. Also eligible when equipped with approved turboc harged engines (250 H. P.), and/or wing tip tanks per STC: SA 1480WE and/or, Turbocharged Lycomi ng IO-540-C1B5 or IO-540-C1C5 engines in accordance with FAA Sealed Roto-Master (Rajay) Drawing List No. RJ0700 STC SA539WE and/or, Modified nose, gear doors, nacelle fairings, and wing tips STC SA636SW.
3. FAA/DAS Approved Pilot’s Operating Handbook and/ or Airplane Flight Manual Supplement, P/N 891202, dated 10-12-95 is required for Piper Models PA-23-250 and PA-E23-250, S/N 27-2000 through S/N 27-7554172 And The Above Models When Equipped With Approved Turbocharged Engines (250 H.P.) And/Or Wing Tip Tanks Per STC SA1480WE or later FAA Approved revisions of the above supplement.
4. FAA/DAS Approved Pilot’s Operating Handbook and/ or Airplane Flight Manual Supplement, P/N 891202, Revision 1, dated 2-19-01 is required fo r Piper models PA-23-250 and PA-E23-250, S/N 27-2000 through S/N 27-7554172 and the above models when equipped with approved turbocharged engines (250 H.P.) and/or wing tip tanks per STC SA1480WE for S-TEC System 55/55X or later FAA Approved revisions of the above supplement.
5. FAA/DAS Approved Pilot’s Operating Handbook and/ or Airplane Flight Manual Supplement, P/N 891202, Revision 2, dated 8-09-07 is required for Piper Aircraft, Inc. Model: PA-23-250, PA-E23- 250, and PA-23-235 and/or when e quipped with approved turbocharged engines (250 H. P.) and/or wing tip tanks per STC: SA 1480WE and/or Turbocharged Lycoming IO-540-C1B5 or IO-540- C1C5 engines in accordance with FAA Sealed Roto-Master (Rajay) Drawing List No. RJ0700 STC SA539WE and/or Modified nose, gear doors, n acelle fairings, and wing tips STC SA636SW for S- TEC System 55/55X or later FAA Approved revisions of the above supplement.
6. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.
FAA Form 8110-2-1(10-69) Page 4 of 4
Number SA09123AC-D Date Amended 8-09-07
Certification Basis: used for this STC
CAR 3.18 (11-01-59) CAR 3.661 (11-01-59) FAR 23.303 Amdt - CAR 3.171 (01-15-58) CAR 3.665 (11-01-59) FAR 23.305 Amdt 23-45 CAR 3.172 (01-15-58) CAR 3.667 (11-01-59) FAR 23.307 Amdt - CAR 3.173 (01-15-58) CAR 3.668 (11-01-59) FAR 23.561(e) Amdt 23-48 CAR 3.174 (01-15-58) CAR 3.669 (11-01-59) FAR 23.603 Amdt 23-23 CAR 3.231(a) (10-56) CAR 3.681 (03-01-63) FAR 23.605(a) Amdt 23-23 CAR 3.291 (09-15-57) CAR 3.691 (03-01-63) FAR 23.607 Amdt 23-48 CAR3.292 (09-15-57) CAR 3.693 (11-01-59) FAR 23.609 Amdt - CAR3.293 (09-15-57) CAR 3.694 (11-01-59) FAR 23.611 Amdt 23-48 CAR3.294 (09-15-57) CAR 3.695 (11-01-59) FAR 23.777(a,b) Amdt 23-49 CAR3.295 (09-15-57) CAR 3.696 (11-01-59) FAR 23.1301 Amdt 23-20 CAR3.296 (09-15-57) CAR 3.697 (11-01-59) FAR 23.1309 Amdt 23-49 CAR3.335 (03-15-57) CAR 3.735 (11-01-59) FAR 23.1329 Amdt 23-49 CAR3.337 (03-15-57) CAR 3.755(a) (11-01-59) FAR 23.1357 Amdt 23-43 CAR3.344 (09-15-57) CAR 3.762 (11-01-59) FAR 23.1365 Amdt 23-49 CAR3.345 (09-15-57) CAR 3.765(a) (11-01-59) FAR 23.1367 Amdt – CAR3.381 (09-15-57) CAR 3.777 (11-01-59) FAR 23.1431 Amdt 23-49 CAR3.384(a) (09-15-57) CAR 3.779 (11-01-59) FAR 1529 Amdt 23-26 CAR3.386(d) (11-01-59) CAR 3.384(a) (11-01-59) FAR 1555(a) Amdt 23-45 CAR 3.652 (10-01-59) FAR 23.301(a) Amdt 23-48 FAR 1581(a) Amdt 23-45
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ADs that name this STC · 0
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