STC SA1-37

Supplemental type certificate · Avionics Inc

Holder
Avionics Inc · United States
Status
Current · Reissued
Status date
August 7, 1972
Applied
February 21, 1957
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheets
TCDS3A13TCDS5A6

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

What it approves

Installation of Tactair T-3 automatic pilot and optional installation of Tactair AH-1 altitude hold device (for use with Tactair T-3 autopilot).

What the certificate saysOCR

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number 5A1-37.

This certificate issued to: Avionics, Inc.

'Terminal Building Lunken Airport Cincinnati, Onio Part 3 of the CIVII Air Regulations.

Original Product - Type-bertificate Number: 5A6; 3A13 Make: Cessna Model: *180, *180A, B, C, D, E, F; 182, 182A, B, Description of Type Design Change:

Installationoof Tactair T-3 Automatic Pilot in accordance with Tactair Installation Instructions Form CA-1 Rev. U dated 9/30/64 and Tactair Drawing No. D-521, Sheets No. 1 Rev. I and No. 2 Rev. V, both dated 10/9/64.

B. Optional installation of Tactair AH-1 Altitude Hold Device (for use with Tactair T-3 Autopilot) in accordance with Tactair Installation Instructions Form TAH-1 Rev. DD dated 8/11/64, pages 1 through 6, 9 and 10.

Installation "A" requires FAA approved Airplane Flight Manual Supplement, Form CA-3 Rev. F dated 3/2/65.

Installation "'B" requires FAA approved Airplane Flight Manual Supplement Form TAH-3 dated 6/16/58.

This cortificate and the supporting data whiches Sedation pat son Spot Pare Doffel until survendered, suspended, vevcked, or a termination date is otherwise established by the Ildministrator of the Federal Aviation Administration .

Date of Application: 21 February 1957 Date Reissued: 7 August 1972 Date of Issuance: . 27 February 1957 Paloamended: 11/7/57; 7/10/58; 2/16/59; 8/23/60;

FEDERAL AVIATION By Direction of the Administrator /17/62; 12/17/62; 3/2/6 Samuel Stayder for W. F. NORTON (Siguature ) * MINISTRATO Chief, Engineering and Manufacturing Branch (Title)

FAA FORM 81.10-2 (10-68) Page 1 of 2

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA1-37 Date Reissued: 7 August 1972 Limitations and Conditions: (Cont'd):

* 3° The approval of the Cessna Models 180 and 180A also includes those aircraft equipped with Edo Amphibious Gear, Item 217 of Aircraft Specification 5A6, Revision 34 or earlier.

This approval should not be incorporated in any aircraft of these specific models on which other approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those previously incorporated approved modifications will not introduce any adverse effect upon the airworthiness of the aircraft.

.. .END...

47 PAGE 2 OF 2 PAGES

FEDERAL AVIATION AGENCY Form Approved, Budget Bureau No. 04-R015 Supplemental Type Certificate

1. NAME AND ADDRESS OF APPLICANT lactair, Incorporated Bridgeport Montgomery County, Pennaylvania INSTRUCTIONS - Submit in triplicate to local FAA Flight Standards Inspector. Copy will be returned to applicant upon issuance.

Supplemental Type Certificate APPLIED FOR:

AIRCRAFT ENGINE PROPELLER

ORIGINAL MODEL DESIGNATION Cesena Models 180 thru 180F*, 182 thru 182D NEW MODEL DESIGNATION (If desired)

3. DESCRIPTION OF CHANGE Installation of Tactair T-3 Automatic Pilot per Tactair Installation Instruc- tions Form CA-1 Revision U dated 9/30/64, end Tactair Drawing No. D-52L Sat. 1 Rev. T and Sht, 12 Rev. V both dated 10/9/64.

180A, 180B/TAA Approved Airplane Flight Manual for Cesana Nodels 1800 thru Supplement to FAA Approved Airplane Flight Manual for Cessna Models 180, 180F and 182 thru 182D, For CA-3 Revision F dated 3-2-65 required with this installation.

*Includes Model 180 and 180A equipped with Item 217 EDO Amphibious Gear.

| Form TAH-1 Revision DD dated 8/21/64 Pe 6/16/58 required with this Installation of Tactair AH-l Altitude Hold Device as an accessory item for AH-1 Altitude Hold to be in accordance with Tactair Installation Instructions addition to basic T-3 Autopilot, when installed as above. FlightManua. Supplement Form TAH-: dated thru 6, 9 & 10. Installation of TaR Approved metallation.

• WILL DATA BE AVAILABLE FOR SALE OR RELEASE TO OTHER PERSONS? YES NO

b. WILL PARTS BE MANUFACTURED FOR SALE (Ref, CAR 1.55,)? YẸS NO

5. SIGNATURE AND TITLE OF APPLICANT September 30, 1964 Date of Application: Names Do / Walter M. Templin, Chief Engineer SIGNATURE Kares TITLE

6. To be completed by FAA

NATURE AND LOCATION OF DATA Airplane Flight Manual Supplement approved by W. F. Norton 2/27/57. Drawings and Installation Instructions, Form 1600, approved 2/18/57 by B. J. Salvedori (DER 1-31) revised 8/15/57. Conformity inspections dated 2/21/57 & 9/11/57 conducted by Models 180C, 180D, 182C and 182D approved by FS-1100A based on statement signed verified by Cessna letter 810-135 dated 10/24/58 signed by 0. T. Wells, IOR 3-1. letter 810-35 dated 10/8/57. Similarity of Model 180A with 180B and 182A with 1828 by O. I. Wells. Inspector Van Artsdalen. Similarity of 180, 180A, 182 and 182A verified by Cesse ORIGINAL TYPE CERTIFICATE NO. FAA APPROVAL (Continued on reverse) Original signed by 3A13, 5A6 W. Oleksak Supplemental Type Certificate NO. P. A. Gibson Amends BAL 3 SIGNATURE SA1-37 ated 12/17/62

DATE OF APPROVAL March 2, 1965 Chiel, Engineering and Manufacturing Branch TITLE 3540 Form FAA-2417 (5-59)

Item 6 - Nature and Location of Data - continued:

Conformity inspection for the amphibious models 180 and 180A dated 11/7/57 was conducted by N. J. Geraci. Revision C to Flight Manual Supplement to include 180 through 180D, 182 through 182D and amphibious models 180 and 180A approved 7/20/60. Filed in Cessne 180 STC file, Eastern Region.

Data regarding part 2 of change:

Conformity dated 7/1/58 by B« S. Van Artsdalen.

Installation Instructions (Form TAH-1) dated 4/18/58 and referenced drawings.

Approved Flight Manual Supplement TAH-3 dated 6/16/58.

Data located in Beech 35 STC file, Eastern Region.

letter of 4/2/62 to Tactair, Inc. Addition of Cesana Model 180E approved by EA-219 based upon IMCR 0. I. Welle' by ZA-216. No conformity inspection necessary, Cessna model 1005, same as 1000 and 150D. FAA Approved Airplane Flight Manual Supplement, Rev. D dated 5/17/62, epproved dated. 5/27/62 IMCE 3-1. Cesana model 180F added per Cessna letter of 10/3/62 signed by 0. T. Welle, No conformity inspection necessary since Cesana Model 150F same as 150E.

FAA Approved Airplane Flight Manual Supplement CA-3, Rev. # dated 12/17/62 approved by SA-216.

1-190, on Form FAA-1600 dated 10-26-64. JactaiT Forms CAL ReY. U, CA-3 ReV. I JAI ReV. DD, TAI-3 no reT, draving D-521 Sht, fl Rev. T and Sht. f2 Rev. V approved by J. Reyner, Dai and Approval Basis: CAR 3 dated 11/1/49.

Deta located in Cesana 160 SIC File, Fastern Region.

FEDERAL AVIATION AGENCY Supplemental Type Certificate

1. NAME AND ADDRESS OF APPLICANT Tactair, Incorporated Bridgeport Montgomery County, Pennsylvania Form Approved, Budget Bureau No. 04-R015 INSTRUCTIONS - Submit in triplicate to local FAA Flight Standards Inspector.. Copy will be returned to applicant upon issuance..

Supplemental Type Certificate APPLIED FOR:

AIRCRAFT ENGINE PROPELLER

ORIGINAL MODEL DESIGNATION Cessna Models 180 thru 180F*, 182 thru 182D NEW MODEL DESIGNATION (If desired)

3. DESCRIPTION OF CHANGE

1. | Installation of Tactair T-3 Automatic Pilot per Taguair Installation Instructions Form CA-1 Revision U dated 9/30/64, and Tartai Drawing No. D-521 Sht.

#1 Rev. T and Sht. #2 Rev. V both dated 10/9/64.

180F and 182 thru 182D, Form CA-3 Rev; 180A, 180B/FAA Approved Airplane Flight M Supplement to FAA Approved Airplane Flight Manual for Cassna Models 180, ted 3-2-65 required with this -or Cessna Models 180C thru installation.

*Includes Model 180 and 180A equir 217 EDO Amphibious Gear.

2. Installation of Tactair AH- st Device as and bo! sessory item for Form TAH-1 Revision DD ge FlightManual Supplement AH-1 Altitude Hold to be: addition to basic T-3 Autopilot d, Packague With End provelation. ice with Tactair Jastallation Instructions Installed as above. Installation of 4a. WILL DATA BE AVAILABLE FO ALL OR TELEASE TO OTHER PER

b. WILL PARTS BE MANG FOR SALE (Re f 55)? * YES NO 50 SIGNATURE AND TLES OF OCANT AMEND REGION

SIGNATURE ptember 30, 1964 Date of Application:

Airplane Flight Mange Supplement approved by W. F. Norton 2/27/57. Drawings and Installation Instructions, Form 1600, approved 2/10/57 by B. J. Salvadori (DER 1-31) revised o/15/51 Conformity inspections dated 2/21/57 & 9/11/57 conducted by Models 180C, 180D, 188C and 18ED approved by FS-1100A based on statement signed verified by Cessna letter 810-138 dated 10/24/58 signed by O. T. Wells, IMCR 3-1. by O. I. Wells. letter 010-35 dated 10/0/57. Similarity of Model 180A with 180B and 182A with 182B Similarity of 180, 180A, 182 and 182A verified by Cessna ORIGINAL TYPE CERTIFICATE NO. FAA APPROVAL (Continued on reverse) ЗA13, 5A6 W.Oleksak Supplemental Type Certificate NO. (Amends SA1-37 A P. A. Gibson SIGNATURE SAI-37 dated 12/17/62)

DATE OF APPROVAL March 2, 1965 Chief, Engineering and Manufacturing Branch TITLE 3540 Form FAA-2417 (5-59)

Item 6 - Nature and Location of Lata - continued:

Conformity inspection for the amphibious models 180 and 180A dated 11/7/57 was conducted by N. J. Geraci. Revision C to Flight Manual Supplement to 180A approved 7/20/60. Filed in Cessna 180 STC file, Easter Region. include 180 through 180D, 182 through 182D and amphibious models 180 and Data regarding part 2 of change:

Conformity dated 7/1/58 by B. S. Van Artsdalen.

Installation Instructions (Form TAH-1) dated 4/18/58 and referenced drawings.

Approved Flight Manual Supplement TAH-3 dated 6/16/58.

Data located in Beech 35 STC file, Fastern Region.

letter of 4/2/62 to Tactair, Addition of Cessna Model 180E approved by EA-219 based upon IMCR 0. T. Wells' "Ine:

No conformity inspection necessary. Cessna model 180E same as 180C and 180D.

by EA-216. FAA Approved Airplane Flight Manual Supplement, Rev. D dated 5/17/62, approved Cessha model 180F added per Cessna letter of 10/3/62 signed by O. T. Wells;

DMCE 3-1.

No conformity inspection necessary since Cessna Model 180F same as 180E.

FAA Approved Airplane Flight Manual Supplement CA-3, Rev. E dated 12/17/62 approved by EA-216.

Tactair Forms CA-1 Rev. U, CA-3 Rev. F, TAH-1 Rev. DD, TAH-3 no rev., drawing D-521 Sht. #l Rev. T and Sht. #2 Rev. V approved by J. Reyner, DER 1-190, on Form FAA-1600 dated 10-26-64.

Approval Basis: CAR 3 dated 11/1/49.

Data located in Cessna 180 SIC file, Eastern Region.

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 · 12

MakeModelData sheet
The Cessna Aircraft Company1805A6
The Cessna Aircraft Company180A5A6
The Cessna Aircraft Company180B5A6
The Cessna Aircraft Company180C5A6
The Cessna Aircraft Company180D5A6
The Cessna Aircraft Company180E5A6
The Cessna Aircraft Company180F5A6
The Cessna Aircraft Company1823A13
The Cessna Aircraft Company182A3A13
The Cessna Aircraft Company182B3A13
The Cessna Aircraft Company182C3A13
The Cessna Aircraft Company182D3A13