Subject: Transmittal of Federal Aviation Administration (FAA) Supplemental Type Certificate (STC) ST02040SE for IAI BDSF

u.s. Department of Transportation Federal Aviation Administration Transport Airplane Directorate Aircraft Certification Service 1601 Lind Avenue So...
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u.s.

Department of Transportation

Federal Aviation Administration

Transport Airplane Directorate Aircraft Certification Service 1601 Lind Avenue Southwest Renton, Washington 98057

DEC 2 1 1009 In Reply Refer To: 100S-09-259 Mr. Vladimir Novicov Certification Project Manager Civil Aviation Authority ofIsrael P.O. Box 8 Ben Gurion Airport Tel Aviv 70100 Israel Dear Mr. Novicov: Subject: Transmittal of Federal Aviation Administration (FAA) Supplemental Type Certificate (STC) ST02040SE for IAI 767-300BDSF In accordance with paragraph 3.0.3(g) of the Bilateral Aviation Safety Agreement and the associated Implementation Procedures for Airworthiness between the United States of America and the State of Israel, the Civil Aviation Authority of Israel (CAAI) provided the Statement of Compliance, reference CAAI Letter Number G386-C 171209002, dated December 17,2009, confirming that the subject aircraft modification is in compliance with the applicable FAA requirements listed in the FAA Issue Paper G- I Stage 4 rev. I dated December 10,2009, for the subject airplane. Based on this, the FAA has issued the subject STC. The original STC is enclosed with this letter. The FAA requests the CAAI to transmit the STC to Israel Aerospace Industries (lAI) Ltd. In additions to the FAA STC we have also enclosed the following FAA approved documents: 1. Signed approval pages of Section 9 on Airworthiness Limitations and Certification Maintenance Requirements (CMR) of thc 767 Supplementary Maintenance Planning Document (MPD), IAI document numbcr TR 368-00-00-94 I07 Rev. R dated November 2009. 2. Original Signed page of the Airplane Flight Manual Supplement, IAI document number TR 371-00-00-C0489-EUA Rev. New. 3. A copy of FAA Issue Paper ES-I Stage 4 dated December 16,2009, closcd. 4. A copy of FAA IP G-I Stage 4 Rev. I dated December 10,2009, closed. A separate lettcr 100S-09-260 approving altcrnate methods of compliance (AMOC) for 50 airworthiness directivcs requiring AMOCs is also being sent to the lAI.

100S-09-259

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We appreciate the cooperation and support of the CAAI and IAI for the subject STC process. Please extend our sincere thanks and appreciation to IAI. If you have any questions, please contact Mr. Kanji Patel, Program Manager, by telephone at (425) 917-6407, by facsimile at 1-425-917-6590, or by E-Mail at [email protected]. Sincerely,

Jeffrey E. Duven Manager, Seattle Aircraft Certification Office Enclosures

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¥-,..sp" Conversion of a Boeing 767-300 passenger configuration airplane to a special freighter (SF) configuration in accordance with Israel Aerospace Industries, LTD. (IAI) Master Document List (MDL) TR-371-00-00C0010 Revision New, dated December 8, 2009, or later Federal Aviation Administration (FAA) approved revisions. The freighter configuration is designated as 767-300 BDSF. The modification includes an electrically operated left side main deck cargo door 5?'Nr'¥lh;.n

with a control and warning panel, a redesigned floor beams and posts, floor panels replacement, cargo loading system provisions, a 99 barrier design, modification of passenger accommodations to a Class E cargo compartment with new linings and a main deck srnoke detection system, a modification of the air conditioning distribution system to a freighter configuration, accommodations for t"ree (3) supernumeraries in the flight deck, in addition to existing two crew and one observer positions making a total occupancy of six persons, control cable rerouting, design, and redesign of avionics and electrical system to accommodate freighter features. Operating weight limits update as approved and is specified in the applicable Airplane Flight Manual (AFM) and Weight & Balance Control and Loading manual supplements . .~;'.n(ff./h;VI4"u,,/ 1)';.,,,..41',;""4.' Approval of this change in type design applies to the aircraft model listed above 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 and the following IAI FAA approved documents, or later FAA-approved revisions, must be maintained as part of the permanent records for the modified aircraft. (Limitations

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Any alteration of this certificate is punishable by aline of not exceeding $/,000, This certificate may be transferred in accordance

or imprisonment not exceeding 3 years. or both. with FAR 2/.47.

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Document

Number

December 21, 2009

DESCRIPTION

Revision for FAA STC

371-00-00-C0010

Master Document List

New

371-00-00-C0011

AJC Effectivity list B767-300BDSF conversion 767 -300BDSF Conversion Compliance Check List Airplane Flight Manual Supplement for Boeing 767-300 Special Freighter Supplement to Weight & Balance Control & Loadina Manual 767-200SF/-300BDSF Section 9 on Airworthiness Limitations and CMRs of Supplementary Maintenance Planning Document (MPDl

New

371-00-00-C0757 371-00-00-C0489-EUA

371-08-00-C0510CDI1 368-00-00-94107

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Revision or FAA approval Date December 8, 2009 December 8, 2009 December 8, 2009 November 18, 2009 December 2, 2009 December 15 2009

Approval

CAAI approval accepted CAAI approval accepted CAAI approval accepted FAA

CAAI approval accepted FAA

Concurrent installation of STC Number ST02767CH dated October 15, 2009 for the Main Cargo Loading System Modification, is required for the installation of this STC. The Instructions for Continued Airworthiness, IAI Document 371-00-00-C0004, Revision New, dated September 16, 2009, or later FAA-accepted revisions, must be incorporated into the operator's maintenance program. This modification may not be installed after August 30, 2010, unless (1) previously approved electrical wiring interconnection system (EWIS) instructions for continued airworthiness (ICA) have been approved by the FAA Oversi9ht Office (Refer to 14 CFR part 26 9 26.11). This engineering approval of a changed type certificate limitation does not permit a change in operating rule applicability to the operator of the changed aircraft. An applicant for an operating rule applicability change must obtain any change in operating rule applicability through consultation with their responsible certificate management office (CMO). STC Applicability The design approval under this STC is applicable to the design configuration of Boeing Model 767-375, Serial Number 24086. Applicability to other Boeing Model 767-300 series airplanes is identified in the IAI document TR 371-00-00-C0011.

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