What it approves
Installation of replacement fuel tank sensors and associated in-tank wiring.
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may 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.
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ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 4
Every issue · 3
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| October 11, 2007 | Amended, current | Certificate |
| July 6, 2007 | Reissued, earlier issue | Certificate |
| June 1, 2007 | Issued, earlier issue | Certificate |