What it approves
Conversion of Passenger airplane to Freighter configuration by installing a large Main Deck Cargo Door, upper deck Class E cargo compartment, floor reinforcement and other associated modifications.
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.
Part 25 of the Federal Aviation Regulations.
Conversion of Passenger airplane to Freighter configuration by installing a large Main Deck Cargo Door, upper deck Class “E” cargo compartment, floor reinforcement and other associated modifications in accordance with the following Elsinore Engineering Documentation:
Master Drawing List 2101-02, Rev. A, dated 02/06/98, or later FAA approved revision.
Index List 2101-01, Rev. A, dated 02/11/98, or later FAA approved revision.
1. The following documents, or later FAA approved versions, must be maintained as part of the permanent records of the modified aircraft:
a. A copy of this certificate
b. A300-B2/B4 Flight Manual FM Supplement Revision 07, dated Jul 15/06
c. 2101-45 Revision A, dated 11/14/97, Instructions for Continued Airworthiness
d. 2101-03 Revision N/C, dated 11/20/97, Weight and Balance/Cargo Loading Manual
e. WBMS 300 116 08/97 Issue 2, dated November 1997, Weight and Balance Manual Supplement, Chapters 3 and 4.
Airbus Deutschland GmbH Kreetslag 10 D-21129 Hamburg Germany A35EU Make: Airbus Model: A300 B4-2C, B4-103, B4-203 Date of application: September 1, 1995
Date of issuance: February 11, 1998 Date reissued: April 1, 1998, August 7, 2001, September 10, 2001, November 1, 2002 Date amended:
February 12, 2007 By direction of the Administrator
( Signature) Anthony Socias Manager New York Aircraft Certification Office
( Title)
FAA Form 8110-2-1(10-69) Page 2 of 2
Number ST00177LA-D Date of Amendment: February 12, 2007
2. This approval must be supplemented with a separate STC for an approved Main Deck Cargo Loading System in accordance with Daimler-Benz Aerospace Airbus Cargo Loading System Cover Specification 2550 M1F 0002-02.
3. 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.
4. The Installer must determine whether this design change is compatible with previously approved modifications.
Service and Operating Information:
Before September 28, 2003 Service and repair instructions (bulletins, letters, etc.), the structural repair manual, aircraft flight manual and overhaul and maintenance manuals which contain a statement that the document is LBA approved are accepted by the FAA and are considered as FAA approved. These approvals pertain to type design only.
On or after September 28, 2003 Service and repair instructions (bulletins, letters, etc.), the structural repair manual, aircraft flight manual and overhaul and maintenance manuals which contain a statement that the document is European Aviation Safety Agency (EASA) approved are accepted by the FAA and are considered as FAA approved. These approvals pertain to type design only.
…END…
ADs that name this STC · 2
An AD can apply because an STC is installed, or mention one in its text.