# STC SA1204NW

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Flightcraft Inc, United States
- Description: Installation of a recalibrated dial face on the United Instruments Fuel Flow Gauge
- Applied: March 13, 1981
- Status date: March 27, 1981
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS 3A15](https://openairdocs.org/tcds/3A15)
- Certificate PDF: https://openairdocs.org/files/sha256/5c/10/5c1008292887dc1398336b9bc1d31dc76a21e1637835c5425966cd1097bae86a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/741569C834AF04A886257A3A0067BD34.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA1204NW

## ADs that name it (0)

None.

## Approved models (2)

- Hawker Beechcraft Corporation F33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation V35B ([TCDS 3A15](https://openairdocs.org/tcds/3A15))

## 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: SA1204NN This certificate issued to: Flighteraft, Inc.

Part 3 s$ the CiViI Air Regulations, dated May 15, 1956, as amended by 3-8.

Original Product - Type Certificate Number: 3A15 Make: Beech Model: V35B, F33A Description of Type Design Change: Installation of a recalibrated dial face, part number FLT 1005-10-1 on the United Instruments Fuel Flow Gauge (part number 6331) in accordance with Flightcraft, Inc. Master Document List 1005 and Installation Instruction No. 1005-01.

NOTE: This STC is applicable to those Beech V35B and F33A aircraft with the Continental TS10-520-D engine installed.

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 modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate shall be maintained as part of the permanent records for the modified aircraft.

March 27, 1981 I ate unvended: 4/20/52 FEDERAL AVIATION lion of the Sids sinistraler Lamell Medeman TOMINIST RAN O Aunchief, Seattle Area Aircraft Certification Office, ANM-100S ( Signalure ) (Title)

47.

## Every issue (1)

- March 27, 1981: Issued, Current. [certificate](https://openairdocs.org/files/sha256/5c/10/5c1008292887dc1398336b9bc1d31dc76a21e1637835c5425966cd1097bae86a)

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