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.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Piper Aircraft Inc. | PA-28-140 | 2A13 |