# STC SA00763AT

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: FFC Manufacturing, United States
- Description: Installation of left hand and right hand fuel cell assemblies. (310 S/N PO240 and up, 401 S/N 1 thru B1200, 402 S/N 1 thru B1200)
- Applied: September 9, 1994
- Status date: April 29, 2009
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A10](https://openairdocs.org/tcds/3A10), [TCDS 3A25](https://openairdocs.org/tcds/3A25), [TCDS A7CE](https://openairdocs.org/tcds/A7CE)
- Certificate PDF: https://openairdocs.org/files/sha256/4c/c4/4cc49cc430e87cc463d646d8be50d40570a14ddbf21c4673fe453d72e89a0101
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C66C5AA8CC7FBBDC862575B5006DB62A.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00763AT

## ADs that name it (0)

None.

## Approved models (5)

- Cessna Aircraft Company 310 ([TCDS 3A10](https://openairdocs.org/tcds/3A10))
- Cessna Aircraft Company 340 ([TCDS 3A25](https://openairdocs.org/tcds/3A25))
- Cessna Aircraft Company 401 ([TCDS A7CE](https://openairdocs.org/tcds/A7CE))
- Cessna Aircraft Company 402 ([TCDS A7CE](https://openairdocs.org/tcds/A7CE))
- Cessna Aircraft Company 414 ([TCDS A7CE](https://openairdocs.org/tcds/A7CE))

## 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

Part * of the Regulations.

Description of Type Design Change: Installation of left and right side fuel cell assemblies in accordance with A/C Fuel Cells Worldwide, Inc., “Installation Instructions,” dated August 30 1994; A/C Fuel Cells Worldwide, Inc., Drawing C3803, Revision A dated July 19, 1998 (was Drawing C3803-1, No Revision, dated December 13, 1994) and Drawing C3804, Revision A, dated July 19, 1998 (was drawing C3804-1, No Revision, dated December 13, 1994); or FAA approved revision.

Limitations and Conditions: This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effects upon the airworthiness of the aircraft. 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.

(See continuation 3 of 3)

FFC Manufacturing 4010 Pilot Dr., Suite 103 Memphis, TN 38118 (See continuation 3 of 3) Make: Cessna Model: (See continuation 3of 3) Date reissued: July 31, 2002; April 29, 2009

Date amended: December 30, 1998

( Signature) Melvin D. Taylor Manager Atlanta Aircraft Certification Office

( Title)

Date of application: September 09, 1994

Date of issuance: May 01, 1995

FAA FORM 8110-2-1(10-69) PAGE 2 of 3 PAGES

Number SA00763AT

FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES

Number SA00763AT

Model Continuation:

Cessna A/W RQMT’S

310 S/N P0240 and UP TCDS No. 3A10, Rev. 59 CAR 3 340 S/N All TCDS No. 3A025, Rev. 25 CAR 3/ FAR 23 401 S/N 1 thru B1200 TCDS No. A7CE, Rev. 38 CAR 3 402 S/N 1 thru B1200 TCDS No. A7CE, Rev. 38 CAR 3 414 S/N All TCDS No. A7CE, Rev. 38 CAR 3

Limitations and Conditions: (Continuation)

FFC Manufacturing part numbers C3803-1 (left hand, assembly) and C3804-1 (right hand assembly) are replacements for Cessna part numbers 9910023-3 (left hand assembly) and 9910023-4 (right hand assembly), for the listed model aircrafts.

## Every issue (1)

- April 29, 2009: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/4c/c4/4cc49cc430e87cc463d646d8be50d40570a14ddbf21c4673fe453d72e89a0101)

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