STC SA2905SW

Hmttfl £tat« of amrrica ©epartmtnt of transportation — jftdtral Stoiation administration upplemental t^pe Certificate SA2905SW Project A4139SW-S AR-214 Avicon Development Corporation 701 M. Central Expressway Richardson, Texas 75080 taafi<«rn&n&rj>Z?4ia^ 3 sdd&e Civil Air Part 23 of the Federal Aviation Regulations.

tkipinad .-%t>duct — .^^if^^^catf,,^tnt/f^ See Limitations and Conditions See Limitations and Conditions gee Limitations and Condition* : Inatallation of AVICOH TZl Rial Flow Totalieer System according to Inatallation Drawing A900119 Revision A dated 12/20/78 or later FAA approved revision.

1. This modification is eligible on aircraft listed on Eligibility List, Sheets

1. 2, 3, 4 attached to this STC, or later FAA approved list.

2. This installation is not ellgibile to replace an existing required system on the airplane.

3. Compatibility of this modification with other previously approved modifications must be determined by the installer.

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- ^?t7?Jt>(^»^i>»^.^^ .w!te?tn'rnAdni/i-i< id &e July 10, 1978 January 30, 1979 'S/% _/• I7^*v / fl r-'/'/,Sfff''efir*€fifat-rl\*jf trif -• fai'fttftt± ArrttDh&w (Signature) Don P. Watson Chief, Engineering and Manufacturing Branch

T/in certificate may be transferred in accordance with t-AR 21.47.

FAAFom 8NO-I(10-A8)

AIRPLANE EFFECTIVITY LIST SA2905SW THE AF1-1 ( ) KIT IS APPLICABLE TO THE FOLLOWING AIRPLANES Page 1 iEECIi TC 3A15 MODEL 33 A3 3 353 C33 C33A E33 E33A E33C F33 F33A ENGINE 5A3 VT.-TC V3EA V35A-TC V3E!i Y35I.-T'' 36 A43 CON'T.

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225iiP 225HP 22S;iP 22511P 2SCIIP 225iIP 235MP 235IIP 22SHP 2S5rtP 260MP 240HP 250HP 250I1P 250!iP 2 60 i'P 28 SUP 235HP 28S11P 295HP Hsw 285HP ZR^MD * IO-470-J IO-470-J IO-470-K IO-'J,70-K IO-520-B in-470-K IO-520-B IO-520-B TO-470-K IO-520-B I 0-4 70 -N IO-470-G IO-470-C in—I "^-cTr....<7<%_',j TO-170-N IO-J20-B 10-52"'- li T5TO-S20- D in-S20-P.

lo-s:"?"' IO-520-li 3A17 3A24 A9CE IS: A-..

Ai55~, A133 TO-4-0-F io-s.?o-n DEPARTMENT OF TRANSPCKTATtD!*

SOUTHWEST REGION FLiGiiT STANDARDS DIVISION ENGtfEErtlNG APPROVED ,SUBJECT TO INSPECTION

AIRPLANE EFFECTIVITY LIST SA2905SW SINGLE ENGINES (AF1-1) CONTINUED:

Page 2 CESSNA-CQS'T.

TC MODEL A4CE 206 U202.A U206B-F U206G TU206\-F T11236G 1*201, A-E TP206A-E ENGINE CONT.

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285HP 285HP 300HP 300IIP 235HP 310HP 285HP 28SHP iA2I 207, A 2103/J 21QD-J, T213J-L 21C-S,5A IO-52C-A 10-520-A IO-S20-F IO-52C-L TSIO-520-r TSIO-520-'!

IO-520-A !0-520-r CONT. 300HP IO-520-P CONT. 3QOIIP CONT. 3101iP c-yrr. 2e.au?

CONT. 260HF CON 2951-iP F1-52C-A CC.-CT. 2i5;!P IO-323-J TONT. 500HP TO-n:C-?

CONT. 285HP TaiO-S20- ' CONT. 285IIP TSrO-320-.

CONT. 31011P TSlG-52fl-;- FEDERAL AVIATION ADMIJJI3TSATIOM

SOUTHWEST REGION FLIGHT STANDARDS DIVISION.

EHGIi'lEERiNQ APPROVED iUSJECT TO INSPECTION

AIRPLANE EFFECTIVITY LIST SA2905SW Page 3 THE AF1-2 ( ] KIT IS APPLICABLE TO THE FOLLOWING AIRPLANES TC BEECH

MODEL ENGINT JAI:.

3A23 A2CF A6CE 05-55 9S-C5S Ds-nssDS-C55 L/5-A35 *s-::53 31 DC SlO'.'olOH 31 ?J- 310.7 T310 520 320-1 52 OA 320B 320C 3 2 OD 3 2 OF.

"20T "40 340A "36 337 CONT.

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2CU.HP :SSHP2^5HP 2SSI1P 26CHP 260HP 260IIP 260IIP 260HP 285HP 260HP 260PH 260HP 260iiP 2 60 HP 280KP 280HP 230;1P 285HP 310HP 21 OH?

2101 1?

IO-470-L 10-520-:.* IO-320-C TO-320-C lO-'PG-L IO-470-L 10-470-0 IO-470-D IO-I70-U TSIO-520-n TSIG-470-3 TSIO-470-S TSID-47C-B TSIO-470-C TSIO-470-D TSin-520-^ TSIO-520-b TSI''-S20-L TSIO-520-K TSTO-S20-N TO-360-A 10-560-C/D '"ONT. 210;iP IO-7»dC CONT. "in:-!P TSIO-360-A/ DEPA8TM.NT OF t^AHSPORTATION

SOUTHWEST REGION FLIGiiT STANDARDS DIVISION.

ENGINEERING APPROVED SUBJECT TO INSPECTION:

AIRPLANE EFFECTIVITY LIST SA2905SW Page 4 TWIN ENGINES (AF1-2) CONTINUED:

CESSNA CON'T.

TC_ A7CE MODEL 401 401A 401B 402 40 2 A 402B 411 411A 414 421A 421B 421C ENGINE CONT.

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COOT.

300HP 3001 IP 300HP 300HP 300HP 300HP 340HP 340PH 310HP 375HP 375HP 3751iP TSIO-520E TSIO-520E TSIO-S20E TSIO-520E TSIO-520E TSIO-520E GTSIO-520-C GTSIO-520-C TSIO-520-J 2TSIO-520-D GTSIO-520-H GTSIO-520-L PIPER A7SO PA-34-200T COOT. 200HP LTSTO-360-E .*?.-. \ ' f SOU i'H-VEST REGION RIG; IT M'AKDARDS DIVISlOfl

ENGIWEERIHG APPROVED

UBJECT TO INSPECTION