# STC SA2906SW

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Avicon Development Corporation
- Description: Installation of AVICON AF1 fuel flow processor.
- Status date: January 30, 1979
- Data sheets: 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A16, 3A16, 3A16, 3A16, 3A15, 5A3, 5A3, 3A16, 3A15, 3A15, 3A15, 3A16, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A24, 3A24, 3A24, 3A24, 3A24, A4CE, A16CE, A16CE, 3A21, 3A21, 3A21, 3A21, 3A21, 3A21, 3A21, 3A21, 3A21, 3A21, 3A21, 3A21, 3A21, 3A21, 3A10, 3A10, 3A10, 3A10, 3A10, 3A10, 3A10, 3A25, 3A25, 3A25, 3A25, 3A25, 3A25, 3A25, 3A25, A2CE, A6CE, A6CE, A6CE, A6CE, 3A25, 3A25, A7CE, A7CE, A7CE, A7CE, A7CE, A7CE, A7CE, A7CE, A7CE, A7CE, A7CE, A7CE, 3A24, 3A24, A9CE, A9CE, A9CE, A4CE, A4CE, A4CE, A4CE, A4CE, A4CE, 3A17, A16CE, A16CE, 3A21, 3A21, 3A21, 3A21, 3A21, 3A21, 3A10, 3A10, 3A10, A6CE, A6CE, A6CE, A6CE, A6CE, A4CE, A4CE, A4CE, A4CE, A4CE, A4CE, A4CE, A4CE, A4CE, A4CE, A4CE, A4CE, A4CE, A4CE, A4CE, A4CE, A4CE, A4CE, A4CE, A4CE, A7SO
- Certificate PDF: https://openairdocs.org/files/sha256/8b/c8/8bc81782617530deb1d31a1882cf44d7c0085f2575165db194527f7922e29c07
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/61CB630AA14436D685256CC20008CA91.0001
- Page: https://openairdocs.org/stc/SA2906SW

## ADs that name it

None.

## Approved models (134)

- Beechcraft Corporation 35-33 (TCDS 3A15)
- Beechcraft Corporation 35-A33 (TCDS 3A15)
- Beechcraft Corporation 35-B33 (TCDS 3A15)
- Beechcraft Corporation 35-C33 (TCDS 3A15)
- Beechcraft Corporation 35-C33A (TCDS 3A15)
- Beechcraft Corporation 36 (TCDS 3A15)
- Beechcraft Corporation 95-55 (TCDS 3A16)
- Beechcraft Corporation 95-A55 (TCDS 3A16)
- Beechcraft Corporation 95-B55 (TCDS 3A16)
- Beechcraft Corporation 95-C55 (TCDS 3A16)
- Beechcraft Corporation A36 (TCDS 3A15)
- Beechcraft Corporation A45 (Military T-34A; B-45) (TCDS 5A3)
- Beechcraft Corporation D45 (Military T-34B) (TCDS 5A3)
- Beechcraft Corporation D55 (TCDS 3A16)
- Beechcraft Corporation E33 (TCDS 3A15)
- Beechcraft Corporation E33A (TCDS 3A15)
- Beechcraft Corporation E33C (TCDS 3A15)
- Beechcraft Corporation E55 (TCDS 3A16)
- Beechcraft Corporation F33 (TCDS 3A15)
- Beechcraft Corporation F33A (TCDS 3A15)
- Beechcraft Corporation G33 (TCDS 3A15)
- Beechcraft Corporation J35 (TCDS 3A15)
- Beechcraft Corporation M35 (TCDS 3A15)
- Beechcraft Corporation N35 (TCDS 3A15)
- Beechcraft Corporation P35 (TCDS 3A15)
- Beechcraft Corporation S35 (TCDS 3A15)
- Beechcraft Corporation V35 (TCDS 3A15)
- Beechcraft Corporation V35A (TCDS 3A15)
- Beechcraft Corporation V35B (TCDS 3A15)
- Cessna Aircraft Company 185A (TCDS 3A24)
- Cessna Aircraft Company 185B (TCDS 3A24)
- Cessna Aircraft Company 185C (TCDS 3A24)
- Cessna Aircraft Company 185D (TCDS 3A24)
- Cessna Aircraft Company 185E (TCDS 3A24)
- Cessna Aircraft Company 206 (TCDS A4CE)
- Cessna Aircraft Company 207 (TCDS A16CE)
- Cessna Aircraft Company 207A (TCDS A16CE)
- Cessna Aircraft Company 210 (TCDS 3A21)
- Cessna Aircraft Company 210-5 (205) (TCDS 3A21)
- Cessna Aircraft Company 210-5A (205A) (TCDS 3A21)
- Cessna Aircraft Company 210A (TCDS 3A21)
- Cessna Aircraft Company 210B (TCDS 3A21)
- Cessna Aircraft Company 210C (TCDS 3A21)
- Cessna Aircraft Company 210D (TCDS 3A21)
- Cessna Aircraft Company 210E (TCDS 3A21)
- Cessna Aircraft Company 210F (TCDS 3A21)
- Cessna Aircraft Company 210G (TCDS 3A21)
- Cessna Aircraft Company 210H (TCDS 3A21)
- Cessna Aircraft Company 210K (TCDS 3A21)
- Cessna Aircraft Company 210L (TCDS 3A21)
- Cessna Aircraft Company 210M (TCDS 3A21)
- Cessna Aircraft Company 310C (TCDS 3A10)
- Cessna Aircraft Company 310D (TCDS 3A10)
- Cessna Aircraft Company 310E (TCDS 3A10)
- Cessna Aircraft Company 310F (TCDS 3A10)
- Cessna Aircraft Company 310G (TCDS 3A10)
- Cessna Aircraft Company 310H (TCDS 3A10)
- Cessna Aircraft Company 310J (TCDS 3A10)
- Cessna Aircraft Company 320 (TCDS 3A25)
- Cessna Aircraft Company 320-1 (TCDS 3A25)
- Cessna Aircraft Company 320A (TCDS 3A25)
- Cessna Aircraft Company 320B (TCDS 3A25)
- Cessna Aircraft Company 320C (TCDS 3A25)
- Cessna Aircraft Company 320D (TCDS 3A25)
- Cessna Aircraft Company 320E (TCDS 3A25)
- Cessna Aircraft Company 320F (TCDS 3A25)
- Cessna Aircraft Company 336 (TCDS A2CE)
- Cessna Aircraft Company 337 (TCDS A6CE)
- Cessna Aircraft Company 337A (TCDS A6CE)
- Cessna Aircraft Company 337B (TCDS A6CE)
- Cessna Aircraft Company 337C (TCDS A6CE)
- Cessna Aircraft Company 340 (TCDS 3A25)
- Cessna Aircraft Company 340A (TCDS 3A25)
- Cessna Aircraft Company 401 (TCDS A7CE)
- Cessna Aircraft Company 401A (TCDS A7CE)
- Cessna Aircraft Company 401B (TCDS A7CE)
- Cessna Aircraft Company 402 (TCDS A7CE)
- Cessna Aircraft Company 402A (TCDS A7CE)
- Cessna Aircraft Company 402B (TCDS A7CE)
- Cessna Aircraft Company 411 (TCDS A7CE)
- Cessna Aircraft Company 411A (TCDS A7CE)
- Cessna Aircraft Company 414 (TCDS A7CE)
- Cessna Aircraft Company 421A (TCDS A7CE)
- Cessna Aircraft Company 421B (TCDS A7CE)
- Cessna Aircraft Company 421C (TCDS A7CE)
- Cessna Aircraft Company A185E (TCDS 3A24)
- Cessna Aircraft Company A185F (TCDS 3A24)
- Cessna Aircraft Company A188 (TCDS A9CE)
- Cessna Aircraft Company A188A (TCDS A9CE)
- Cessna Aircraft Company A188B (TCDS A9CE)
- Cessna Aircraft Company P206 (TCDS A4CE)
- Cessna Aircraft Company P206A (TCDS A4CE)
- Cessna Aircraft Company P206B (TCDS A4CE)
- Cessna Aircraft Company P206C (TCDS A4CE)
- Cessna Aircraft Company P206D (TCDS A4CE)
- Cessna Aircraft Company P206E (TCDS A4CE)
- Cessna Aircraft Company R172J (TCDS 3A17)
- Cessna Aircraft Company T207 (TCDS A16CE)
- Cessna Aircraft Company T207A (TCDS A16CE)
- Cessna Aircraft Company T210F (TCDS 3A21)
- Cessna Aircraft Company T210G (TCDS 3A21)
- Cessna Aircraft Company T210H (TCDS 3A21)
- Cessna Aircraft Company T210J (TCDS 3A21)
- Cessna Aircraft Company T210K (TCDS 3A21)
- Cessna Aircraft Company T210L (TCDS 3A21)
- Cessna Aircraft Company T310P (TCDS 3A10)
- Cessna Aircraft Company T310Q (TCDS 3A10)
- Cessna Aircraft Company T310R (TCDS 3A10)
- Cessna Aircraft Company T337B (TCDS A6CE)
- Cessna Aircraft Company T337C (TCDS A6CE)
- Cessna Aircraft Company T337D (TCDS A6CE)
- Cessna Aircraft Company T337E (TCDS A6CE)
- Cessna Aircraft Company T337F (TCDS A6CE)
- Cessna Aircraft Company TP206A (TCDS A4CE)
- Cessna Aircraft Company TP206B (TCDS A4CE)
- Cessna Aircraft Company TP206C (TCDS A4CE)
- Cessna Aircraft Company TP206D (TCDS A4CE)
- Cessna Aircraft Company TP206E (TCDS A4CE)
- Cessna Aircraft Company TU206A (TCDS A4CE)
- Cessna Aircraft Company TU206B (TCDS A4CE)
- Cessna Aircraft Company TU206C (TCDS A4CE)
- Cessna Aircraft Company TU206D (TCDS A4CE)
- Cessna Aircraft Company TU206E (TCDS A4CE)
- Cessna Aircraft Company TU206F (TCDS A4CE)
- Cessna Aircraft Company TU206G (TCDS A4CE)
- Cessna Aircraft Company U206 (TCDS A4CE)
- Cessna Aircraft Company U206A (TCDS A4CE)
- Cessna Aircraft Company U206B (TCDS A4CE)
- Cessna Aircraft Company U206C (TCDS A4CE)
- Cessna Aircraft Company U206D (TCDS A4CE)
- Cessna Aircraft Company U206E (TCDS A4CE)
- Cessna Aircraft Company U206F (TCDS A4CE)
- Cessna Aircraft Company U206G (TCDS A4CE)
- Piper Aircraft Inc. PA-34-200T (TCDS A7SO)

## 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.

Wnittfl &tatu nf amrtica ©cpartmtnt of ^transportation— federal Station administration upplemental ICgpe Certificate SA2906SW Project AS140SW-S AR-214 Avicon Development Corporation 701 N. Central Expressway Dallas, Texas 75080 Civil Air ., and Part 23 of the Federal Aviation Regulations.

See Limitations and Conditions see Limitations and Conditions gee Limitations and Conditions ,: installation of AVICCK AFl Fuel Flow Processor according to Installation Drawing A900133 Revision B dated 12/21/78, or later FAA approved revision.

1. This modification is eligible on aircraft listed on Eligibltty List, Sheets 1, 2, 3, 4 attached to this TC, or later FAA approved list,

2. This Installation is not eligible 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.

>us 10, 1978 January 30, 1979 Don P. Watson Chief, Engineering and Manufacturing Branch (Tait)

1 his ctrtificatt may bi traraftrred rn acrordance uiil/l f-AR 21.47.

FAA Few. 8(10-2(10-46)

AIRPLANE EFFECTIVITY LIST ^•- SA2906SW THE AF1-1 ( ) KIT IS APPLICABLE TO THE FOLLOWING AIRPLANES:

TC EEECIf

MODEL ENGINE 3A1S 5A3 33 A33 333 C33 C33A E33 H33A E33C F33 F33A C^.i AS:J35 '13:>'3S P3.r 53 E V3C V35-TC V3SA CCNT.

**COMT.**

TON'!.

**CONT .**

**CGNT.**

**CONT .**

**CONT.**

CON? .r*)N'T.t!J*T.

**CONT .**

ro:'T.TO:;T.•"!0!/T .

"Trr.O'T.T.

"ONT .

**CO.'.T , CONT .**

225HP 2251IP 2251 IP 225HP 2851IP 225HP 2 35 HP 235i!P 2 2 5HP

235)IP 2601!P 240HP 2SOIIP 2501IP 260HP 260!!?

2SE1IP 2351IP 2851IP 2 8 5! IP IO-470-J IO-470-J IO-470-K IO-470-K IO-520-B IO-470-K IO-520-B IO-520-B IO-470-K IO-520-T1 IQ-/t70-N IO-470-G I-,-470-r lO-j^n-c TO-470-N IO-470-M IO-S20-B 10-520-11 TSin-520-0 IO-520-B V3SI1 '.'."Sr-Ti"!

36 A36 A4Stlie;

rrii-T^ •-'. i - * CONT.

**CONT.**

29SIIP 285HP #% + *• <~ TSIO-520-P IO-520-L i "" i~. 10- ITO-N 47P-N 3A17 3A24 A9CE A: s 3.MSPA A Li "ONT. 3DOHP COST. 300HP TO-4-0-F IO-520-P IO-S20-D TO-520-n Ifl-520-n .FEDERAL AVIATION ADMIWi3TBAT!5BI SOLTTfJV/EST REGION

FLIGHT STANDARDS DJWSIM ENGIHEERING. AP?JIOV£D

**OUBJECT TQ INSPECTION**

AIRPLANE EFFECTIVITY LIST SA2906SW SINGLE ENGINES (API-1) CONTINUED:

Page 2 CESSNA-CON'T.

TC A4CE A16TE MODEL 206 u:o2,AU206B-F U206G TU206A-F TU206G P20S.A-E TP206A-E 207,A 210, 210T ZIC^.-'l Tl'lOF-A T210J-L 210-S.SA ENGINE CONT.

**CONT.**

**CONT.**

**CONT.**

**CONT.**

**CONT.**

**CONT.**

**CONT.**

CO!,T.

**CONT .**

CO^.T .

**CONT .**

**CONT .**

**CONT .**

**CONT.**

ro/.'T .

**CCNT.CONT.**

**CONT .**

28SHP 285HP 300HP 300HP 285HP 3 101 IP 285HP 285MP 3 00! IP 300HP siniip 260I1P 2fiO!iP 2S5HP 2SSHP SOrJIIP 235HP 283HP .ilOi;p IO-520-A IO-S20-A IO-520-F IO-S2G-L TSIO-520-C TSIO-520-M IO-S2C-A I0-520-r 10-S20-1;

IO-52C-A TSn-F23 Tr,IO-520' TS10-52'- DEPAIU.'.'iLiJT OF FEDt;;AL A.UTION ADMINISTRATIO couTiJvvesT REGION FLIGi-iT STANDARDS DIVISION ENfilNEERING APPROVED

**SUBJECT TO INSPECTION**

AIRPLANE EFFECTIVITY LIST SA2906SW Page 3 THE AFi-2 ( ) KIT 1^ APPLICABLE TO THE FOLLOWING AIRPLANES TC BEECH

MODEL ENGINE 95-55 CESSNA 3A23 A2CF A6CE ^ ns-rss 310C 310D-310H HOJ-310.T T510 3:0-1 320A 320C 320D 340 340 A To?

COOT. 26UHP IO-470-I C1NT. 28SHP 10-520- CONT, iUSUP M-520-C CONT. 26PHP IG-J7C-L CONT. 260HP IO-470-L CDirr.CON'T.

**CONT.**

**CONT.**

**CONT.**

**CONT.**

**CONT.**

**CONT.**

**CONT.**

**CONT .**

**CONT.**

**CONT .**

**CONT.**

**CONT.**

26C:IP 260HP 260HP 285MP 260HP 260 PH 260HP 26CMP 2 60 1 IP 230KP 280HP 230HP 285H?

310HP 10-^70-0 IO-470-D IO-470-U TSIO-520-B TSIO-47I5-R 7310— 170-B "31.1-470-5 T5I^-470-C TSIO-470-0 TSIO-520--J TSIO-S20-!* TSI'l-520-:-, TSIO-S20-1T TSTO-S20-N CONT. 210HP TO-360-*.

210HP 2io;;p210HP CONT.

**CONT.**

**CDOT.**

SOUTH',VE3T REGION rUGJ-T STANDARDS DIVISION

**ENGINEERS APPROVED**

SUSJECT TO INSPECTION IO-360-C/G n-360-c/p TS10-3&0-A/"

AIRPLANE EFFECTIVITY LIST SA2906SW TWIN ENGINES CAF1-2J CONTINUED:

Page 4 CESSNA COH'T.

**TC A7CE MODEL 401 4Q1A 401B 402 402A 402B 411 411A 414 421A 4213 4 21C ENGINE CONT.**

**CONT.**

**CONT.**

**CONT.**

**CONT.**

**CONT.**

**CONT.**

**CONT.**

**CONT.**

**CONT.**

**CONT.**

**CONT.**

300HP 300HP 300HP 300HP 3 00 HP 300HP 340HP 340PH 310HP 37SI1P 375HP 37511P TSIO-520E TSIO-520E TSIO-520E TSIO-520E TSIO-520E TSIO-520E GTSIO-520-C GTSIO-520-C TSIO-520-J GTSIO-520-D GTSIO-520-H GTSIO-520-L P!P?3R A750 PA-34-200T CONT. 200HP I.TSIO-360-E DEPAR i F ...ANSPORTATION

•- •- . jiiiT REGION FLIb,.V .laNDARDS DIVISION

IHGIHEERING APPROVED SUBJECT TO INSPECTIOf*

## Every issue (1)

- January 30, 1979: Issued, Current. [certificate](https://openairdocs.org/files/sha256/8b/c8/8bc81782617530deb1d31a1882cf44d7c0085f2575165db194527f7922e29c07)

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