# STC SA01847CH

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: McCauley Propeller Systems, United States
- Description: Installationof McCauley Propeller Model 3AF32C512/82NEA-5.5.
- Applied: February 28, 2002
- Status date: September 23, 2005
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A10](https://openairdocs.org/tcds/3A10)
- Certificate PDF: https://openairdocs.org/files/sha256/df/c6/dfc6398a6346f246f0d8e39b8d4f7778933dd67c89cb120c3501a9cb0dc1531a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/33D95C9525E6541C862571560067FAAE.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01847CH

## ADs that name it (0)

None.

## Approved models (5)

- The Cessna Aircraft Company 310J ([TCDS 3A10](https://openairdocs.org/tcds/3A10))
- The Cessna Aircraft Company 310K ([TCDS 3A10](https://openairdocs.org/tcds/3A10))
- The Cessna Aircraft Company 310L ([TCDS 3A10](https://openairdocs.org/tcds/3A10))
- The Cessna Aircraft Company 310N ([TCDS 3A10](https://openairdocs.org/tcds/3A10))
- The Cessna Aircraft Company E310J ([TCDS 3A10](https://openairdocs.org/tcds/3A10))

## What the certificate says

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: SA01847CH This certificate issued to: McCauley Propeller Systems 7751 East Pawnee Wichita, KS 67207 Certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airoorthiness requirement's of Part 3 of the Civil Air Pegulations.

(See Type Certificate Data Sheet 3A10 for the complete certification basis).

Original Product - Type Certificate Number : 3A10 Make: Cessna Aircraft Company Model:

310J, E310J, 310K, 310L and 310N Description of Type Design Change:

Installation of McCauley Propeller Model 3AF32C512/82NEA-5.5 in accordance with McCauley Technical Report No. 958, No Revision, dated February 26, 2002, or later FAA Approved revision.

1. Compatibility of this design change with previously approved modifications must be determined by the installer.

2. FAA Approved Airplane Flight Manual Supplement, TR 959, no rev., dated June 9, 2003, or later FAA approved revision is required.

3. Aircraft are not approved to fly into known icing condition. Propeller deice installation is optional.

4. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

Date of Application: February 28, 2002 Date Reissued: September September 2005 Date of Issuance: June 12, 2003 Date ded:

FEDERAL AVIATION on 2:9 1 (Signature) Thaddeus D. Krolicki, Jr.

TOMINISTRATO Manager, Propulsion Branch Chicago Aircraft Certification Office (Title) 47

## Every issue (1)

- September 23, 2005: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/df/c6/dfc6398a6346f246f0d8e39b8d4f7778933dd67c89cb120c3501a9cb0dc1531a)

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