# STC SA147SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Cruse Aviation, Inc
- Description: Installation of Edo model 439-2705 or 289-2700 amphibious floats.
- Status date: March 22, 1963
- Data sheets: 3A24, 3A24, 3A24, 3A24, 3A24, 3A24
- Certificate PDF: https://openairdocs.org/files/sha256/f7/d4/f7d47165d320652a9fc04db9f62e09d4ca8cd18c6643759a476e24070717b98f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/957F245F6CAE709586257D43005D8B54.0001
- Page: https://openairdocs.org/stc/SA147SW

## ADs that name it

None.

## Approved models (6)

- Cessna Aircraft Company 185 (TCDS 3A24)
- 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)

## 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.

**FEDERAL AVIATION AGENCY**

**SUPPLEMENTAL TYPE CERTIFICATE FORM APPROVED, BUDGET BUREAU NO. O4-R015**

**INSTRUCTIONS - SUBMIT IN TRI PLICATE TO PAA FLIGHT STANDARDS INSPECTOR.**

**COPY WILL BE RETURNED TO APPLICANT UPON**

**ISSUANC E**

1. NAME AND ADDRESS OF APPLICANT Cruse Aviation, Inc.

^501 TBlephone Road Houston, Texas

2. SUPPLEMENTAL TYPE CERTIFICATE APPLIED FOR:

**IX 1 AIRCRAFT 1 I ENGINE L J PROPELLER**

ORIGINAL MODEL DESIGNATION Cessna ldf> Series NEW MODEL DESIGNATION (If dtmi,fd)

DESCRIPTION OF CHANGE Installation of BOo1*39-2705 or model 269-2700floats inaccordance with Cruse Aviation, Inc. Drawing and Data list dated 10/10/62 for model 1*39-2705 and Drawing and Data List Ho. 2 dated 2/U/63 for acdel2d9-2700.

KMBi In addition to placards required by aircraft irow 3A24 the following placards are required}

1. lAstttifloatlon and direction of landing aear controls (supplied by Mo as fart of float kits).

2. ty water rudder control: "tetter rudder up for take off ant iMOlng".

3. On instrument panel when amphibious floats are installed i "Maximum gross wsigbt 3,000 Ibs."

**. WILL DATA BE AVAILABLE FOR SALE OR RELEASE TO OTHER PERSONS! ffl YES Lj NO

b. WILL PARTS BE MANUFACTURED FOR SALE (Saf. CAB 1.55.17 LJ YES LS NO 5- SIGNATURE AND TITLE OF APPLICANT October ID, 196*2 SIGNATURE

**DATE OF APPLICATION TITLE**

6. To t» Completed b^

NATURE AND LOCATION OF DATA Drawing and Data List dated 10/10/62, Drawing & Data List No. 2 dated 2/11/63 with data listed thereon, and Flight Test Report on file at SV-2LO.

Deference Project A188SUS.

Applicable CAR'S saae as original certification.

**ORI6INAL TYPE CERTIFICATE NO.**

-""LEMENTAL TYPE CERTIFICATE NO.

3AU78U

ATE OF APPROVAL , October 22, 1962 March 22, 1963

**FAA APPROVAL**

SI GMATURE H. H. Slaue*ter Chief, ttagineerlng and Manufacturing Branch Tl TLE FORM FAA-2417 (5-591

## Every issue (1)

- March 22, 1963: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/f7/d4/f7d47165d320652a9fc04db9f62e09d4ca8cd18c6643759a476e24070717b98f)

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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.