STC SA8849SW

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Poss ession of this Supplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructio ns, specifications, flight manual supplements, etc.) is the property of the ST C holder.

FAA Form 8110-2 (5/14) Page 1 of 3

Number: SA8849SW

This certificate issued to: LB Aircraft Engineering 6355 NW 36th St Miami Springs, FL 33166-7027

Part 25 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: A16WE Make: Boeing Model: 737-200, -400, -700, -800 Series

Description of Type Design Change: Original installations of Honeywell MCS-3000 Inmarsat Satellite Communications system with Canadian Marconi CMA-2102 antenna with a molded antenna adapter plate, in accordance with SIP Technical Services Master Data List 7305-DL-001, Revision E, dated July 15, 2002, or later FAA approved revisions, or, Later installations (starting 2017) of Honeywell MCS-7120 Inmarsat Satellite Communication System with Esterline/Canadian Marconi CMA-2102SB antenna with a machined adapter plate in accordance with LB Aircraft Engineering Master Data List LB- SAT.737-MDL, Revision C, dated September 11, 2017, or later FAA approved revisions.

Limitations and Conditions: "For Original installations, FAA Approved Flight Manual Supplement, SIP Technical Services Document 7305-FM-001, Revision D, dated August 14, 2002, or later FAA approved revisions, is part of this STC. SIP Technical Services Instructions for Continued Airworthiness 7305-ICA-S01, Revision IR, dated July 12, 2002, or later FAA approved revisions, for maintenance and inspections.

For Later installations, FAA Approved Flight Manual Supplement, LB Aircraft Engineering Document LB-SAT.737-AFM, Revision IR, dated October 12, 2017, or later FAA approved revisions, is part of this STC. Apply LB Aircraft Engineering Instructions for Continued Airworthiness LB-SAT.737-ICA, Revision B, dated August 02, 2017, or later FAA approved revisions, for maintenance and inspections…” (See continuation sheet 3 of 3)

Date of Application: February 09, 1994 Date Reissued: November 10, 1998, June 14, 1999, September 22, 2000 April 15, 2009, September 17, 2014, October 10, 2014

Date of Issuance: July 04, 1994 Date Amended: September 22, 1994, April 8, 1999, March 24, 2000 August 14, 2002, October 12, 2017

Signature Title (for) Christina M. Underwood AIR-7AO Manager, Atlanta ACO Branch

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitu te rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.

FAA Form 8110-2 (5/14) Page 2 of 3

Transfer the ownership of Supplemental Type Certificate Number: SA8849SW

To (Name and address of transferee)

From (Name and address of grantor)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA8849SW

Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitu te rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.

FAA Form 8110-2 (5/14) Page 3 of 3

Date of Issuance: July 04, 1994 Date Amended: October 12, 2017

Limitations and Conditions (Continued): " …This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. 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.”

Certification Basis: Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for parts changed or affected by the change since the reference date of application, March 21, 2017, is based upon 14 CFR Part 25 as amended by Amendment 25-144. Based on Order 8110.48, the certification basis for this modification was determined to be:

Regulations at the latest amendment 25-0 through 25-144

§21.93 (b)(1), Amdt. 21-97 §25.1 (a)(b), Orig. §25.23 (a)(b), Orig.

§25.29, Amdt. 25-72 §25.301 Amdt. 25-23 §25.303 Amdt. 25-23 §25.305 (a)(b), Amdt. 25-86 §25.307 (a), Amdt. 25-139 §25.365 (a)(b), Amdt. 25-87 §25.561 (b)(3)(c), Amdt. 25-91 §25.571 (a)(b), Amdt. 25-132 §25.601 Orig.

§25.603 Amdt. 25-46 §25.605 (a), Amdt. 25-46 §25.609 Orig.

§25.611, Amdt. 25-123 §25.613 Amdt. 25-112 §25.625 (a)(b)(c), Amdt. 25-72 §25.771 (a), Amdt. 25-4 §25.773 (a), Amdt. 25-144 §25.777 (a)(c), Amdt. 25-46 §25.789 (a), Amdt. 25-46 §25.863 (a), Amdt. 25-46 §25.869 (a)(1,3), Amdt. 25-123 §25.1301, Amdt. 25-123 §25.1309 (a)(b)(c)(d), Amdt. 25-123 §25.1322 (a)(b)(c)(d)(e), Amdt. 25-131 §25.1351 (a)(1), Amdt. 25-72 §25.1353 (a)(c), Amdt. 25-123 §25.1357 (a)(c)(d)(e)(f) Amdt. 25-123 §25.1363 (b), Orig. §25.1381 Amdt. 25-72 §25.1431 (a)(c)(d), Amdt. 25-113 §25.1501, Amdt. 25-42 §25.1519, Orig. §25.1529 Amdt. 25-54 §25.1541 (a)(b), Orig. §25.1555 (a), Orig. §25.1581(a)(2)(d), Amdt 25-72 §25.1585 (a)(1), Amdt. 25-105

14 CFR Part 36 regulations: Based on 14 CFR § 21.93(b)(1) (Amdt 21-81), No Acoustical Change has been found for the 14 CFR Part 36 noise levels regulations.

14 CFR Part 26 regulations: Based on 14 CFR § 21.101(g), applicable provisions of 14 CFR Part 26 are included in the certification basis. For any future 14 CFR 26 amendments, the holder of this STC must demonstrate compliance with the applicable sections. As of the issuance date of this STC, compliance has been found for the following regulations: 14 CFR §§ 26.11 (Amdt 26-

0) and 14 CFR §26.47 (Amdt 26-1).

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