u.s. Department of Transportation Federal Aviation Administration 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: Transport Airplane Directorate Aircraft Certification Service 1601 Lind Avenue Southwest Renton, Washington 98057 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.
Transcript
u.s. Departmentof Transportation
Federal AviationAdministration
DEC 2 1 1009
In ReplyRefer To: 100S-09-259
Mr. Vladimir NovicovCertification Project ManagerCivil Aviation Authority ofIsraelP.O. Box 8Ben Gurion AirportTel Aviv 70100Israel
Dear Mr. Novicov:
Transport Airplane DirectorateAircraft Certification Service
1601 Lind Avenue SouthwestRenton, Washington 98057
Subject: Transmittal of Federal Aviation Administration (FAA) Supplemental TypeCertificate (STC) ST02040SE for IAI 767-300BDSF
In accordance with paragraph 3.0.3(g) of the Bilateral Aviation Safety Agreement and theassociated Implementation Procedures for Airworthiness between the United States ofAmerica and the State of Israel, the Civil Aviation Authority of Israel (CAAI) provided theStatement of Compliance, reference CAAI Letter Number G386-C 171209002, datedDecember 17,2009, confirming that the subject aircraft modification is in compliance withthe applicable FAA requirements listed in the FAA Issue Paper G- I Stage 4 rev. I datedDecember 10,2009, for the subject airplane. Based on this, the FAA has issued the subjectSTC. The original STC is enclosed with this letter. The FAA requests the CAAI to transmitthe STC to Israel Aerospace Industries (lAI) Ltd.
In additions to the FAA STC we have also enclosed the following FAA approveddocuments:
1. Signed approval pages of Section 9 on Airworthiness Limitations and CertificationMaintenance Requirements (CMR) of thc 767 Supplementary Maintenance PlanningDocument (MPD), IAI document numbcr TR 368-00-00-94 I07 Rev. R datedNovember 2009.
2. Original Signed page of the Airplane Flight Manual Supplement, IAI document numberTR 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 50airworthiness directivcs requiring AMOCs is also being sent to the lAI.
100S-09-259
We appreciate the cooperation and support of the CAAI and IAI for the subject STCprocess. Please extend our sincere thanks and appreciation to IAI.
2
If you have any questions, please contact Mr. Kanji Patel, Program Manager, by telephoneat (425) 917-6407, by facsimile at 1-425-917-6590, or by E-Mail at [email protected].
Sincerely,
Jeffrey E. DuvenManager, Seattle AircraftCertification Office
5?'Nr'¥lh;.n "/~/I'"¥-,..sp" r;;r",~p"" Conversion of a Boeing 767-300 passenger configuration airplane to a specialfreighter (SF) configuration in accordance with Israel Aerospace Industries, LTD. (IAI) Master Document List (MDL) TR-371-00-00-C0010 Revision New, dated December 8, 2009, or later Federal Aviation Administration (FAA) approved revisions. The freighterconfiguration is designated as 767-300 BDSF. The modification includes an electrically operated left side main deck cargo doorwith 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 decksrnoke detection system, a modification of the air conditioning distribution system to a freighter configuration, accommodations fort"ree (3) supernumeraries in the flight deck, in addition to existing two crew and one observer positions making a total occupancyof 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 & BalanceControl 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. Thisapproval should not be extended to other aircraft of this model on which other previously approved modifications are incorporatedunless 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 certificateand the following IAI FAA approved documents, or later FAA-approved revisions, must be maintained as part of the permanentrecords for the modified aircraft.
(Limitations and Conditions continued on Page 3 of 5)
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Document Number DESCRIPTION Revision for Revision or ApprovalFAA STC FAA approval
Date371-00-00-C0010 Master Document List New December 8, CAAI approval
2009 accepted371-00-00-C0011 AJC Effectivity list B767-300BDSF New December 8, CAAI approval
conversion 2009 accepted371-00-00-C0757 767 -300BDSF Conversion E December 8, CAAI approval
Compliance Check List 2009 accepted371-00-00-C0489-EUA Airplane Flight Manual November 18, FAA
Supplement for Boeing 767-300 New 2009Special Freighter
371-08-00-C0510- Supplement to Weight & Balance A December 2, CAAI approvalCDI1 Control & Loadina Manual 2009 accepted
368-00-00-94107 767-200SF/-300BDSF Section 9 December 15 FAAon Airworthiness Limitations and R 2009CMRs of SupplementaryMaintenance Planning Document(MPDl
Concurrent installation of STC Number ST02767CH dated October 15, 2009 for the Main Cargo LoadingSystem Modification, is required for the installation of this STC.
The Instructions for Continued Airworthiness, IAI Document 371-00-00-C0004, Revision New, datedSeptember 16, 2009, or later FAA-accepted revisions, must be incorporated into the operator's maintenanceprogram.
This modification may not be installed after August 30, 2010, unless (1) previously approved electrical wiringinterconnection system (EWIS) instructions for continued airworthiness (ICA) have been approved by the FAAOversi9ht 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 ruleapplicability to the operator of the changed aircraft. An applicant for an operating rule applicability change mustobtain any change in operating rule applicability through consultation with their responsible certificatemanagement office (CMO).
STC ApplicabilityThe design approval under this STC is applicable to the design configuration of Boeing Model 767-375, SerialNumber 24086. Applicability to other Boeing Model 767-300 series airplanes is identified in the IAI documentTR 371-00-00-C0011.
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STC CompatibilityThe design approved under this STC is compatible with the 767-300 type design and other STC's incorporatedin Boeing Model 767-375 Serial Number 24086 at the time of approval. Compatibility of this design change withother previously approved designs or modifications on any Model 767-300 Series airplanes must bedetermined by the user and installer of the approved data.
Rights to Design Data and Installation of the DataPossession of the STC document does not constitute rights to the design data or installation of the approveddesign data. The STC and its supporting data (drawings, instructions, specifications, etc.) are the property ofthe STC holder. II is incumbent upon the user to contact the STC holder to obtain rights for the use of the STCand the design data contained herein. If the holder agrees to permit another person to use this certificate toalter the product, the holder shall give the other person written evidence of that permission.
Availability of Copies of STCAnyone may request a copy of the STC in writing. An FAA response letter must accompany copies of the STCwith the following statement referencing the STC number: "Possession of the Supplemental Type Certificatedoes not constitute rights to the installation of the modification or the design data contained therein. The STCand related information (drawings, data, specifications etc.) are the property of the STC holder. The FederalAviation Administration will not release proprietary data without authorization from the holder. The user isrequired to obtain installation approval and/or data rights from the STC holder.
Based on 14 CFR !l!i 21.115 and 21.101, and the FAA policy for significant changes in FAAOrder 8110.48, the certification basis for the Boeing Model 767-300 series passenger to Freighter is asfollows:
a. The type certification basis for Boeing Model 767-300BDSF series airplanes is shown on TCDS A1NMfor 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 ofapplication, September 25,2006, is based upon part 25 as amended by Amendment 25-119. Basedon 14 CFR 99 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48,the certification basis for this modification of the 767-300 is as follows:
Regulations at the latest amendment 25-0 through 25-119
* Exemption 9853 dated April 10, 2009 provides relief from the requirements of Sections 25.7850>;25807(g)(1) and (i)(1); 25.810(a)(1); 25.813(b)(1), (b)(2), and (b)(6); 25.857(e); and 25.1447(c)(1) to allow forthe carriage of supernumeraries on the 767 -300BDSF.
** ~ 25.869 is at latest amendment for changes related to ECS distribution system. main deck cargocompartment, supernumeraray area. and wire re-routing, and at Amendment 25-72 for the data recorderrelocation.
*** ~ 25.1353 is at latest amendment except for voice data recorder location, which is at Amdnement 25-42.
Concurrent Change
The certification basis for the following change is the original certification basis for the Model 767-300 asshown on TCDS A1NM:
Replacement of the lower lobe cargo (Class C) smoke detectors. Same as the new detectors in themain deck (Class E)
Part 26 regulations
Based on ~ 21.101 (g), applicable provisions of part 26 are included in the certification basis. For any futurepart 26 amendments. the holder of this STC must demonstrate compliance with the applicable sections.
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Special Conditions:
Exemptions:
Equivalent SafetyFindings:
TCDS Notes:
OptionalRequirements:
Special conditions that are part of the certification basis for the 767 -300Series apply to the airplane operating in the 767-300BDSF configuration.unless otherwise noted.
Exemption 9853 dated April 10, 2009 provides relief from the requirements ofSections 25.7850); 25.807(g)(l) and (i)(l); 25.810(a)(l); 25.813(b)(l), (b)(2),and (b)(6); 25.857(e); and 25.1447(c)(1) to allow for the carriage ofsupernumeraries on the 767-300BDSF.
Equivalent Level of Safety Findings have been made for the followingregulation(s): SS 25.855(i), 25.857(c)(1) and documented in TAD ELOSMemo 5T1 0123SE-T-ES-l
All Notes in TCDS A1NM that apply to the 767-300 Series also apply to anairplane operated in the 767-300BDSF configuration.
All optional requirements in TCDS A 1NM that apply to the 767-300 Seriesalso apply to an airplane operated in the 767 -300BDSF configuration.
Compliance to Part 121.313 UH2) must be shown prior to operation under Part 121. This FAA Regulationstates that after October 1, 2003, for transport category, all-cargo airplanes that had a door installed betweenthe pilot compartment and any other occupied compartment on or after January 15, 2002, each such doormust meet the requirements of Sec. 25.795(a)(1) and (2) in effect on January 15, 2002; or the operator mustimplement a security program approved by the Transportation Security Administration for the operation of allairplanes in that operator's fleet.
All other changes resulting from the Passenger to Freighter Product Level Change are either Secondary orNot Affected in accordance with S 21.101 and AC 21.101-1.
If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the otherperson written evidence of that permission.
