STC SA5795NM

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA5795NM This certificate issued to: Israel Aircraft Industries Intl., Ltd.

Part 25 of the Federal Aviation Regulations. See Page 2 of this STC for the Certification Basis.

Original Product - Type Certificate Number: A20WE Make: Boeing Model: 747-100 Series Description of Type Design Change:

Modification of Boeing 747-100 passenger to 747-100 Special Freighter airplane including, but not limited to, installation of a main deck side cargo door, main deck floor, powered cargo loading system, interior and associated systems in accordance with FAA Approved Israel Aircraft Industries (IAI) Intl. Ltd. s Master Drawing List Document No. 366-53-00-19901 Revision J, dated December 11, 1992, or equipment removals per alternate Master Drawing List Document No. TR-366-53-00-28467 Revision B, dated April 13, 1995, or later FAA approved revisions, and reclassification of the lower lobe cargo compartments from Class C to Class E.

Approval of this change in type design applies to the above model aircraft 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 on the airworthiness of that aircraft. A copy of this amended Certificate, IAl Master Drawing List Document No. 366-53-00-19901, and alternate Master Drawing List TR-366-53-00-28467, and an approved Airplane Flight Manual Supplement must be maintained as part of the permanent records for the modified aircraft. (See Continuation Sheet 2).

Date of Application: March 20, 1991 Date Reissued:

Date of Issuance: November 25, 1992 Date Amended: May 25, 1993; April 14, 1995 STATION By Direction of the Administrator Nondee 1 (Signature) *OMINST RATION Acting Manager, Seattle Aircraft Certification Office (Title)

47.

FAA FORM B110-2(10-68)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA5795NM Limitations and Conditions: (Continued):

Limitations and Conditions: of Type Certificate Data Sheet A20WE apply except as outlined below:

Eligible Serial All Boeing Model 747-100 Series airplanes listed in the IAI Airplane Flight Manual Number: Supplement 306-91-00-19903 with maximum weight limitations as follows:

Taxi Weight - 738,000 Ibs Landing Weight - 585,000 Ibs.

Zero Fuel Weight - 526,500 Ibs.

C.G. Range: See the FAA approved Israel Aircraft Industries' Airplane Flight Manual Supplement 366- 91-00-19903. The vertical C.G. of the total payload is restricted to WL 250.00 or below.

Maximum Weights: See the FAA approved Airplane Flight Manual Supplement 366-91-00-19903.

Maximum Cargo: See the FAA approved Weight & Balance Control and Loading Manual Boeing Document D6-13700 and the IAI Supplement referenced in the AFM Supplement 366-91-00-19903.

Fuel and Oil See the FAA approved Weight & Balance Control and Loading Manual Boeing Document Capacity: D6-13700 and the AI Supplement referenced in the applicable AFM Supplement.

Certification For unmodified structures and systems, the same as shown on Type Certificate Data Basis: Sheet A20WE for the Model 747-100 Series Airplanes.

For new or extensively modified systems and structures, the same as shown on Type Certificate Data Sheet A20WE for the Model 747-100 Series airplane except where superseded by the following Sections of Part 25 as amended by Amendments 25-1 25-38 (Section 25.685 Control System Details) 25-72 (Section 25.783 Doors for Main Deck Side Cargo Door only) 25-54 (Section 25.1529 Instructions for Continued Airworthiness) Part 36 See Type Certificate Data Sheet A20WE and the AFM Supplement.

Production Basis: None

FAA FORM 8110-2-f (10-69) PAGE 3 OF 5 PAGES

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA5795NM Limitations and Conditions: (continued):

Required Equipment: The basic equipment as prescribed in the applicable airworthiness regulations must be installed in the aircraft.

Service Information: Applicable Boeing documents and Israel Aircraft Industries Intl., Ltd.'s Supplemental Structural Inspection Documents (SSID) 366-5300-1921-0, 336-53-00-15047, Structural Repair Manual (SRM) 366-53-0028149 and Maintenance Manual Supplement 306-53-00-19904 applicable to all 747-100 modified in accordance with the STC. Israel Aircraft Industries Service Bulletins and other service information when FAA approved will carry a statement to that effect.

NOTES:

1. The aircraft loading instructions are provided in Weight & Balance Control and Loading Manual Boeing Document D6-13700 and the IAl Supplement 366-08-00-19204. This manual must be in each aircraft at the time of original certification and at all times thereafter, except in the case of operators having an approved weight control system.

2. The 747-100 Special Freighter operations must be in accordance with the FAA approved Israel Aircraft Industries Airplane Flight Manual Supplement 366-91-00-19903. Each approved AFM Supplement lists the applicable airplane Serial Numbers. All placards required in either the FAA approved AFM Supplement, the applicable operating rules or the certification basis must be installed in the airplane.

3. Required structural inspections for all models 747-100 modified in accordance with this STC are contained in the Israel Aircraft Industries Supplemental Structural Inspection Documents. (SSID) 366-53-00-19216 and 366-53-00-15047.

4. Information essential to proper maintenance of the aircraft modified in accordance with this STC is contained in the AI's Maintenance Manual Supplement 366-53-00-19904.

The lAl's Model designation for airplanes modified in accordance with this STC is "B747-100 Series Special Freighter." This model designation appears on the FAA approved IAl's AFM supplements, Structural Repair Manual Supplement 366-53-00-28149 and Maintenance Manual Supplement 366-53-00- 19904 and all other service documents. This model designation does not alter or replace the original Boeing 747-100 Series Model designation.

FAA FORM 8110-2-1 (10-69) PAGE 4 OF 5 PAGES

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA5795NM Limitations and Conditions: (continued):

6. Modifications installed per the following ST's require compatibility with the modifications installed per this STC, SA5795NM.

Installation of Cargo Transfer System per STC SA5865NM.

b. Installation of Cargo Conveyer System per STC ST11CH.

c. Installation of the Smoke Door and Ladder in the upper deck floor at the crew ladder hatch per STC SA2580SW-D.

d. Installation of Galleys per STC SA148ONM.

7. Operational Requirements: The Federal Aviation Regulations (FAR) 21.50 requires that maintenance procedures for continued airworthiness (maintenance and inspection program), as applicable to this change in type design, be made available to the U.S. operators and their regulatory authority at the time the aircraft is returned to service.

FAA FORM 8110-2-1 (10-69) PAGE 5 OF 5 PAGES