# STC SA02394CH-D

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Hartzell Propeller Inc, United States
- Description: Installation of Hartzell propeller de-ice components.
- Applied: February 1, 2007
- Status date: March 26, 2007
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/02/f6/02f6c9c3b6217e7bc297c3382c205d5b94004e31fe378dd742b8530e82754434
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/040F34870DBA9F5D862572AE005804C4.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02394CH-D

## ADs that name it (0)

None.

## Approved models (14)

- Raytheon Aircraft Company 200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company 200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company 200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company 200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company 300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company 300LW ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company A200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company A200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company B200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company B200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company B200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company B200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company B300C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))

## 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: SA02394CH-D This certificate issued to Hartzell Propeller Inc.

One Propeller Place Piqua, OH 45356-2634 Part 23 of the Federal Aviation Regulations.

(See Type Certificate Data Sheet A24CE for the complete certification basis).

Original Product -Type Certificate Number: A24CE Make: Raytheon Aircraft Company Model: 200, 200C, 200CT, 200T, B200, B200C, B200CT, B200T, A200C, A200CT and 300, 300LW, B300, B300C Description of Type Design Change:

Installation of the Hartzell propeller de-ice components listed in the Limitations and Conditions section below in accordance with Hartzell Manual 180 Revision 1 dated November, 2006, or later FAA Approved revisions.

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

(Continued....)

Date of Application: February February1,2007 Date Reissued:

Date of Issuance: March 26,2007 Date Amended:

By Direction of the Administrator FEDERAL AVIATION B=<D (Signature) Brian E. Meyer TOMINSTRATO DAS administrator Hartzell DAS-100082-CE (hitle) 000, or imprisonment not exceeding 3 years, or both FAA FORK 8110-2110-681 PAGE 1 Of

United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Limitations and Conditions: continued...

2. No Airplane Flight Manual Supplement is required.

3. The following Hartzell propeller de-ice components (part numbers) are approved on aircraft models 200, 200C, 200CT, 200T, B200, B200C, B200CT, B200T, A200C, A200CT when equipped with Hartzell HC-E4N- 3G/D9390SK-1R propellers:

4H2271-10 de-ice boots on blades;

3H2092-4 wire harness;

4H2674-2 slip ring;

1H1150-3 terminal strip;

2H1365 tapped eyelet.

4. The following Hartzell propeller de-ice components (part numbers) are approved on aircraft models 300, 300LW, B300 and B300C when equipped with Hartzell HC-B4MP-3C/M10476(N)(S)K propellers:

4H2575-10 de-ice boots on blades;

3H2092-2 wire harness;

4H2444-1 slip ring:

1H1150-3 terminal strip.

5. This modification did not increase the noise level and was not considered an acoustical change as defined in 14 CFR 21,93(b).

6. 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.

...END...

47.

## Every issue (1)

- March 26, 2007: Issued, Current. [certificate](https://openairdocs.org/files/sha256/02/f6/02f6c9c3b6217e7bc297c3382c205d5b94004e31fe378dd742b8530e82754434)

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