# STC SA00479WI

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Raytheon Aircraft Services Inc, United States
- Description: Installation of a carbo web 'Z' net in forward fuselage and a loaders chair.
- Applied: September 13, 1996
- Status date: November 6, 1996
- Product: Aircraft, Small/Large Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/61/f6/61f6861faeada64e75e3e543a119f620607a1a954a263403066e20ab06c402d5
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A7E86F259CCDC67785256CC1007DC95B.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00479WI

## ADs that name it (0)

None.

## Approved models (1)

- Beechcraft Corporation 1900C ([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: SA00179W1 This certificate issued to: Raytheon Aircraft Services P.O. Box 9162 Mid-continent Airport Wichita, KS 67277 Certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meels the airoorthiness requirement's of Purt 23 of the Federal Aviation Regulations.

Original Product - Typo Certificate Number: A24CE Make: Beech Model: 1900C Description of Type Design Change: Installation of a cargo web "Z" net in the forward fuselage and a loaders chair. The "Z" net and loaders chair cannot both be installed in the airplane at the same time. Installation of the two configurations are per Raytheon Aircraft Services Top Drawing 1900C0100, N/C, dated September 20, 1996, and stamped "FAA Approved" on November 6, 1996, or later FAA approved revision Limitations and Conditions: • Compatibility of this design change with previously approved modifications must be determined by the installer. Supplemental Type Certificate (STC) SA00421WI must be installed prior to or concurrently with the STC. FAA Approved Airplane Flight Manual Supplement (AFMS) P/N 1900C90021, dated November 6, 1996, or later FAA Approved revision is required equipment, when this STC is installed.

Date of Application: September 13, 1996 Date Reissued:

Date of Issuance: November 06, 1996 Date Amended:

FEDERAL AVIATION By Direction of the Administrator (Signature) © Ronald K. Rathgeber TOMINSTRATO Associate ACO Mgr, Airframe & Services Wichita Aircraft Certification Office (Title)

## Every issue (1)

- November 6, 1996: Issued, Current. [certificate](https://openairdocs.org/files/sha256/61/f6/61f6861faeada64e75e3e543a119f620607a1a954a263403066e20ab06c402d5)

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