# STC ST00254BO

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Simmonds Precision Products Inc
- Description: Installation of replacement fuel tank sensors and associated in-tank wiring.
- Status date: October 11, 2007
- Data sheets: A35EU, A35EU, A35EU, A35EU
- Certificate PDF: https://openairdocs.org/files/sha256/71/0b/710b46de70728e9edf628a3f38de40c86950fce34441f83938c7ef9d2df8d0c2
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0A56E03186AD9A428625737D006C54A0.0001
- Page: https://openairdocs.org/stc/ST00254BO

## ADs that name it

None.

## Approved models (4)

- Airbus A310-203 (TCDS A35EU)
- Airbus A310-204 (TCDS A35EU)
- Airbus A310-221 (TCDS A35EU)
- Airbus A310-222 (TCDS A35EU)

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

This Certificate issued to Simmonds Precision Products, Inc.

Goodrich Corporation – Fuel & Utility Systems 100 Panton Road Vergennes, VT 05491

Part 25 of the Federal Aviation Regulations.

Original Product Type Certificate Number : A35EU Make : Airbus Model : A310-200, -300 Series Description of Type Design Change:

Installation of replacement fuel tank sensors and associated in-tank wiring in accordance with Goodrich Master Drawing List No. T3092-MDL-0101, Revision B, dated September 24, 2007, or later FAA-approved revision.

1. Instructions for Continued Airworthiness, Goodrich document no. T3092-0005-01, Revision F, dated October 11, 2007, or later FAA-accepted revision, shall be made available to the operator at the time of installation.

2. The installer must determine whether this design change is compatible with previously approved modifications.

Date reissued : July 6, 2007

Date amended : October 11, 2007

( Signature) Robert G. Mann Manager Boston Aircraft Certification Office

( Title) Date of application : May 11, 2007

Date of issuance : June 1, 2007

FAA Form 8110-2-1(10-69) Page 2 of 2

Number ST00254BO

If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

Certification Basis :

Model A310-200, -300 Series Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the installation of Goodrich replacement fuel tank sensors and associated in-tank wiring in the Airbus Model A310-200, -300 Series airplane is as follows:

a. The type certification basis for Airbus Model A310-200, -300 series airplanes is shown on TCDS A35EU for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by the change since the reference date of application, May 11, 2007, is based upon part 25 as amended by Amendment 25-116. Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be:

Regulations at the latest amendment 25-0 through 25-116

25.29, 25.301-25.307, 25.869, 25.901, 25.952, 25.981(a)(b), 25.1301, 25.1309, 25.1316, 25.1337,

25.1529 Note: Compliance to 25.981(a)(b) is limited to the changed in-tank components only.

--------------------------------------------------- END ---------------------------------------------------

## Every issue (3)

- October 11, 2007: Amended, Current. [certificate](https://openairdocs.org/files/sha256/71/0b/710b46de70728e9edf628a3f38de40c86950fce34441f83938c7ef9d2df8d0c2)
- July 6, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/74/51/74510220c7057cb8afac9b1502256c6f2a99b6ab88b600b13a253ca93c118eb1)
- June 1, 2007: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/a5/bf/a5bfa8eaf72175e10607525c14b9d59ad7ade8b2e031684884af8fbfa883fb88)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.