# STC SH2244NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Arnav Systems Inc, United States
- Description: Installation of Silver Instruments Fueltron IIIPT-1GS, IIIPT-1PS, IIIPT-1LS, or IIIPT-1KS digital fuel flow indicating system.
- Applied: November 2, 1983
- Status date: April 29, 1991
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H7EU](https://openairdocs.org/tcds/H7EU)
- Certificate PDF: https://openairdocs.org/files/sha256/fe/c4/fec4cf2c7e53466d37fa511c9bdc5a7a73358920fa6ca602417debafa46ba63c
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B7FB932B044C3336862579D80065C002.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SH2244NM

## ADs that name it (0)

None.

## Approved models (2)

- Agusta S.p.A. A109A ([TCDS H7EU](https://openairdocs.org/tcds/H7EU))
- Agusta S.p.A. A109AII ([TCDS H7EU](https://openairdocs.org/tcds/H7EU))

## 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: SH2244NM This certificate issued to: Arnav Systems, INC.

Part 27 of the Federal Aviation Regulations:

Original Product - Type berlificate Number: HTEU Make: Agusta Model: A109A, A109A 11 Description of Type Design Change: Installation of Silver Instruments Fueltron IIIPT-IGS, TIPI-IPS, IIIPT-ILS, or IIIPT-IKS digital fuel flow indicating system in accordance with FAA approved Silver Instruments Master Drawing List No. A02032, dated October 7, 1983, or later FAA approved revision.

Similaliens and bandilions Approval of this change in type design applies basically to the above model helicopter. This approval should not be extended to other aircraft of this model on which other previously approved modifications 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 helicopter. A copy of this Certificate, and FAA Approved Silver Instruments Rotorcraft Flight Manual Supplement S229, dated January 6, 1984, must be aintained as part of the permanent records for the moditied helicopter This certificate and the supporting data which is the basis for approval shall reman on gecuntu su vendered, suspended, versked, or a lermination date is sherwise estaldished by the Administrator of the Federal Aviation Administration Date of Application: November 2, 1983 Date Reissued: April 29, 1991 Date of Issuance: January 6, 1984 Date Amended: April 29, 1991 FEDERAL AVIATION By Direction of the Administrator Nam GAmie * MINISTRATIO Seattle Aircraft Certification Office Manager, Aircraft Modification Branch (Title) 47 FAA FOR 8110-2 (10-68)

## Every issue (1)

- April 29, 1991: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/fe/c4/fec4cf2c7e53466d37fa511c9bdc5a7a73358920fa6ca602417debafa46ba63c)

---
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.