# STC SA4357WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Arnav Systems Inc, United States
- Description: Installation of Silver Instruments Fueltron III PT-1 or III PT-1G digital fuel flow indicating system.
- Applied: June 10, 1981
- Status date: April 29, 1991
- Product: Aircraft, Small/Large Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/2f/35/2f35550b5e09e3ab0736d2fef4f9afab122fb78d3338d46158c504d492754a1e
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0DE22B30015F7C9885256CC2000E3BD1.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA4357WE

## ADs that name it (0)

None.

## Approved models (4)

- Hawker Beechcraft Corporation 200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation A200 (C-12A) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation A200 (C-12C) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200 ([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 SAA357WE This certificate issued to: Arnav Systems, InC.

Purt 23 of the Federal Aviation Regulations.

Original Product - Type bertificate Number: A24CE Make:

Beech Model:

200, A200, B200 Description of Type Design Change: Installation of Silver Instruments Fueltron III PT-1 or III PT-1G digital fuel flow indicating system in accordance with FAA approved Master Drawing List A01591, Revision "B", dated March 12, 1982, or later FAA approved revision.

Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to other aircraft of this model on which other previously approved moditications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate, and FAA Approved Silver Instruments Airplane Flight Manual Supplement S164 dated July 10, 1981, or later FAA approved revision must be maintained as part of the permanent records for the modified aircraft.

This certificate and the supporting data which is the basis for approval shall remain in effeel until sur vendered, suspended, revoked, or a lermination dale is etherwise established by the Administrater / the Federal Aviation Administration Date of Application: June 10, 1981 Sule missee April 29, 1991 Date of Issuance: JUly 10, 1981 Jale unenduApril 20, 1982; April 29, 1991 FEDERA AVIATION By Direction of the Administrator rania Grie TAHINIST RAN DO Manager, Aircraft Modification Branch Seattle Aircraft Certification Office (Title) 47 FAA FORM 8110-2 (10-68)

## Every issue (1)

- April 29, 1991: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/2f/35/2f35550b5e09e3ab0736d2fef4f9afab122fb78d3338d46158c504d492754a1e)

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