# STC SA09643SC

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Original Primary Category Aircraft Training School (TOPCAT)
- Description: Modification to remove the Standard Airworthiness Certificate and placing them in 'Special Airworthiness Certificate-Primary Category' to allow the pilot-owner to perform preventative maintenance beyond what is allow under Part 43, Appendix A.
- Status date: March 11, 2003
- Data sheets: 3A19, 3A19
- Certificate PDF: https://openairdocs.org/files/sha256/17/d7/17d72cef2d18888afe39e2acfeaa19c4f2e101a298d340634e6b27410fe60ebe
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/319E541C556E45BA86257D3C005F5ED6.0001
- Page: https://openairdocs.org/stc/SA09643SC

## ADs that name it

None.

## Approved models (2)

- Cessna Aircraft Company 150 (TCDS 3A19)
- Cessna Aircraft Company 152 (TCDS 3A19)

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

QPf ^Department of tUrunspnriatum - ^Fefteral .Afaiation JV&mivri straiten .•j^y Ylff/,/,rff/f ;

rvf/rfif^ MaS Mr r ffirrrfff >t-i -y-irrr/r Project Number SA7323SC-A (RDK) SA09643SC The original Primary Category Aircraft Training School (TOPCAT) 137 Aviator Drive #11 Fort Worth, TX 76179 in Mr ps' /ff Mr /r/r?-tf-t/ifi /irrr/rfr/ rff'M /df tsir4.i rfyifi/-r-/itfst/4 r"/ • '/rrr/ 3 3A19 Cessna trsir/ rr</,t/rYfffi-) Civil Air •jf?Je |50; 152 Jdrfsifrr: Modification to remove the Standard Airworthiness Certificate for Cessna aircraft models 150 and 152 and placing them in "Special Airworthiness Certificate - Primary Category" for the purpose of allowing the piloi-owner to perform prevents five maintenance beyond what is allowed under Part 43, Appendix A.

The allowed preventative maintenance items are listed below:

- Pilot-Owners are required to successfully complete FAA Approved "TOPCAT Courses for Pilot-Owners of Primary Category Aircraft" for Cessna 150 Series and Cessna 152 Series aircraft.

Compatibility of this design change with previously approved modifications must be determined by the installer. If the holder agrees to permit another person to use this certificate to alier the product, the holder shall give the other person written evidence of thai permission.

• Mt'-l rrr/r/fffe/f asie/Mr f/f^ffr. •iufytrsii&f .r . -'T;nia/-ieyt . ' r/n/rt rMt'rw t* Mr f-aM-) /&*• fr/ytfffftrAAaMfrstiffffi isi r'/ >-s- cr /'•fr/itsta/eon r^r/f f'-i f/4rrrfi-}r r-i/anfadrtf Mr , ,f,f6>f/su'*l,&vr.Sfy ost.- November 5, 1999 .• July 24. 2000 '-• March 11, 2003, Rev. 1 Manager, Special Cemfiralion Office Southwest Region (Title) Any alteracJon of thiff certificate is punishable by a fine of not exceeding1 $1,000, or in^nsonnrent not ing 3 ysars, or both.

FAA Form 8110-3(10-68) This terrrificate transferred in with FAN 21.47.

1NMRIIUIIONS Tin- Udiisfrr fiuloisrmrnl below may he used to nolil> I lie appiopi iaie FA.\ I'eg ion a 1 Office of [lie irjnsfcT uf this Supplrnifnlal Type Ortihi-alr l*hc f- A A "'ill rtLSM.]*1 tin- <:rrul]< iilc in ihr nanuL ot thr (i-anslcrft and l;irvvanl 11 lo him.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number _..___ to (Name of transferee) (Address of transferee).__ (fiurabt* and street) ':ity,SlaU,and^!PiaJft frnm (Name uf grantor) (Print or type) ._ (Address vj grantor) (Jfttmbti and Ifrrrt) t Cift. State, and £IP aaUI Extent of Authority (if licensing agreement):

Signature of grantor (In ink):.

JUnitcti ^titles ODf America ptpartment of ^Jratispnrtation - ^fe&etal Atnation ^ministration ((Einttinitattrm SA09643SC Date ol Issuance: July 24. 2UOQ Date Amended: March 11, 2003 (Continued):

Replacement of flexible air ducting Replacement of fuel quick-drain valves and filler cap gaskets and seals Replacement of hour/hobbs meters Replacement of wheel brake pads, discs Replacement of propellers Perform cylinder compression check Replacement of engine accessory drive belts Engine oil change Replacement of navigation and communications radios where alterations to electrical circuitry are not involved Removal of exhaust manifolds for gasket replacement as long as removal of other components is not required Replacement of starters Replacement of alternators Replacement of generators Replacement of vacuum pumps Fabrication/replacement of '/3-inch diameter or less hard lines, regardless of their use (i.e.. fuel, electrical, hydraulic, vent vacuum, etc.)

Check control cable condition and tension (rigging or adjustment is not permissible) Windshield scratch removal Sheet metal repair of aircraft skin damage of less than 2 inches Bleeding of brake system Replacement of valve cover gaskets Replacement of engine and vacuum system air filters Service and/or replacement of shimmy damper Lubrication and/or replacement of the tachometer cable (not to include the cable housing) Replacement of the voltage regulator (adjustment not permitted) Removal or installation of the approved wheel pants (speed fairings) with appropriate weight and balance computations and changes in the aircraft's weight and balance records and the aircraft's equipment list Cleaning or replacement of the air/oil separators when installed in accordance with FAA approved data Installation of approved oil quick-drains and their replacement NOTE: Guidance information on Primary Category approvals can be found in Advisory Circular (AC) 21-37.

-End- Any a iteration of this cectifIcate is punishable by a fins of not e^ceedin^ $l,Q&Qt or imprisonnrsnc n&t exceeding 3 years, or both.

FAA Fotjn SL10-2-H10-69] Page 3 of 3 This certificate jnay be transferred in accordance with FAR 21.47.

## Every issue (1)

- March 11, 2003: Amended, Current. [certificate](https://openairdocs.org/files/sha256/17/d7/17d72cef2d18888afe39e2acfeaa19c4f2e101a298d340634e6b27410fe60ebe)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.