STC SA10207SC

Supplemental type certificate · Pratka Allen J

Holder
Pratka Allen J · United States
Status
Current · Issued
Status date
January 30, 2004
Applied
May 7, 1999
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS2A13

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of Lycoming O-360-A3A engine, Senenich 76EM8-S5-0-60 propeller, B & C Specialty Products L-40 alternator, LR3B-14 voltage regulator, and Knisley Exhaust System Inc muffler

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.

rJi Stairs (Of America jprpavtmcut nf (Emitsportatuiit - Jrfefrrral ^bmitti strati on (CertificateProject Number ST5887SC-A, (PWH) 4/' /../yetstMtfs* sAio207sc 286(> 2nd Street Pleasanton, TX 78064 /tyr Mr ff/ff-rr/ftv /ffff/rf/ fS/fi /dt /tsttS/fi/tfvt.± rt/t'/ t-fstf/t/ tftt-3-t SYyftfsvwfr/'/-j fy S/ffS'/ 3 fy /#/• (JlVll Air ' s f •'*&"/ ft tfsstt/'r-s' / 2A 1 ^ F .- Piper PA-28-140 '-//'•irri/'/'>'rfi /•/.Jp/,r '^r.jiyf/ Y,/ff,,yr.- Installation of Lycoming 0-360-A3A engine, Senenich 76EM8-S5-0-60 propeller, B & C Specialty Products L-40 alternator, LR3B-14 voltage regulator, and Knisley Exhaust System Inc.

muffler in accordance with Photograph Set I thru 12. The Airplane Flight Manual Supplement, dated January 30, 2004, or later KAA approved revision is required.

^/j/fHf/rr/rr's,.; ,rnr/Y,r-/,,/fY/,-f,->.- Descriptive data pertaining to this design change are considered inadequate for duplication in other airplanes. This approval is limited to only the installation made in a Piper Model PA-28-140. Serial No. 28-20983. This S"I C does not permit manufacturing of parts for multiple installations. The Sensenith 76EM8-S5- 0-60 propeller blade diameter limits are: not over 76 inehes and nol under 75.5 inches. The I.ycoming 0-360-A3A engine is limited to a maximum of 2550 RPM. The airplane is limited 10 Normal Category operations with: (a). Gross weight remaining al 2150 pounds, and (b). All acrobatic maneuvers, including spins are prohibited.

. J»/i i-if/y/Snt/r ri/if -irHy''/n/'/'"/. .irttyti-f/'-r/. rrii jiy t/a/rr ird/r* i* Mr f'ti.it.j /ft- rt/yirfinf -i/trf// /-istitfrsi //: >^r> / "ft/// ff ff /<'/vstir/u/if/< f/ft/r- /-j r//irrrrivr r-i/nf'/r'-^ft/ f-r/ Mf • f.r^ii/'/ii'/f-rr/r-f ,•/"/'/'/'"'/"•" -• May 7, 1999 F-/f-i-i/fftfin • January 30, 2004 i't'-i-,tfir/-• S. Flrances Cox^— JManager, Spc Southwest Region Ray fl-lrreratitjn af this certifJcaCe i* pumiahable by a fine of noc exC**rJing Sl.OOD, or impriaonnent noc exceeding 3 years, or This certificate way fce transferred in accordance ^ith FflJ? 2FAA Form ailQ-2{10-6B) Page 1 o£ 2

INSTKUCTION.S The transfer rndorsrmrni hrlow may be used (o noliK ihr ;i](|jii>|>riate FAA I'c^lnniil Ofliie t>l" chr iranslcr uf ihis Supplomcnlal Type Ccnilitdti- ['he ['AA «ill rciiiiu1 thi- ccrlilKalc in the name o! ihc Iransleree ami lonvard ii lo him.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number __ ID (.Nantr oj transferee) (Address of transferee). i and tirat) (City, Slate, and £IP mk) from (Name of grantor) (Print or typf) (Address of grantor) r and Itrtrt) , Stale, and </P lodr ) Extent of Auihority (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 · 1

MakeModelData sheet
Piper Aircraft Inc.PA-28-1402A13