# STC SA2822CE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: John's Aircraft and Upholstery, United States
- Description: Install Bennetts seat converter stowage compartment.
- Applied: August 1, 1988
- Status date: April 17, 1992
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A21EU](https://openairdocs.org/tcds/A21EU)
- Certificate PDF: https://openairdocs.org/files/sha256/68/7a/687ae4fdd53534b8b487074dae4949424753863e6474e01bc95bb12ddc801de5
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/898D599E57A8BCBD85256CC20008C9A0.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA2822CE

## ADs that name it (0)

None.

## Approved models (3)

- British Aerospace (Scotland) HP 137 Jetstream Mk. 1 ([TCDS A21EU](https://openairdocs.org/tcds/A21EU))
- British Aerospace (Scotland) HP Jetstream Model 3101 ([TCDS A21EU](https://openairdocs.org/tcds/A21EU))
- British Aerospace (Scotland) HP Jetstream Series 200 ([TCDS A21EU](https://openairdocs.org/tcds/A21EU))

## 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: SA2822CF This certificate issued to: John's Aircraft and Upholstery Services 429 North St. Francis Wichita, KS 67202 Puri 23 of thEedera1 Aviation Begin sent one pate on the go coticate Bat shedents and AT·De Certificate Data Sheet.

Make: British Aerospace Model: Mode1 Jetstream Mk.1, Series 200, and Description of Type Design Change:

Install Bennetts Seat Converter Stowage Compartment on passenger seat (s) per installation instructions attached to each compartment in accordance with drawings and data called out on John's Aircraft and Upholstery Drawing List No. AV-DL-2, stamped "FAA Approved" with a date of April 17, 1992, or later.

Limitations and Conditions: This appliance may not be installed on any seat located immediately behind a passenger, nor adjacent to ar emergency exit. 2. This approval should not be extended to other specific airplanes of this model on which other previously approvec modifications are incorporated, unless it is determined that the interrelationship between this approved modifications will introduce no adverse effect upon the change and any of these other previously airworthiness of that airplane.

August 1, 1988 Date of Issuance: . April 17, 1992 Date Amended:

FEDERAL AVIATION By Direction of the Administrator Xaurence A. Hesson (Signature ) "OMINISTRAT Wichita Aircraft Certification Office Lawrence A. Herron, Manager (Title) 47 FAA FORM 8110-2 (10-68)

## Every issue (1)

- April 17, 1992: Issued, Current. [certificate](https://openairdocs.org/files/sha256/68/7a/687ae4fdd53534b8b487074dae4949424753863e6474e01bc95bb12ddc801de5)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.