STC ST04576AT

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United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate January 31, 2025 Number ST04576AT:

AerSale, Inc.

9850 NW 41st. Street, Suite 400 Doral, FL 33178 25 Federal Aviation Regulations A16WE Boeing 737-600/-700/-800/-900 Series Installation of the AerAware Enhanced Flight Vision System (EFVS) on Boeing 737-600/-700/-800/-900 in accordance with AerSale Master Data List, AER-EFVS.737-MDL, Revision J, dated December 20, 2024, or later FAA-approved revision.

(Description of Type Design Change continued on page 3 of 4) Limitations and Conditions:

1. AerSale Aircraft Flight Manual Supplement, AER-EFVS.737-802 Revision -, dated December 6, 2023, or later FAA-approved revision, is required and must be carried in the aircraft during all flights.

(Limitations and Conditions continued on page 3 of 4)

December 20, 2019 April 24, 2024, January 31, 2025 December 6, 2023 (for) Manager, East Aircraft Certification Branch 4

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Too (Name and address of transferee):

Date oI transfer:

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Date Reissued: January 31, 2025 Number ST04576AT:

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Date Reissued: January 31, 2025 (Continuation Sheet) Number: _S__T0__4__57__6_AT Description of Type Design Change (continued):

There are other Boeing service modifications and provisions which are required to support compatible configurations for the installation of STC ST04576AT, which vary for different Boeing Model 737-600/-700/-800/-900 Series airplanes. See Section 6 of the FAA Approved Master Drawing List, AerSale Document AER-EFVS.737-MDL, Revision J, or later FAA Approved revisions, to determine specific prerequisite requirements to define compatible aircraft configurations for eligible aircraft under this STC.

Limitations (continued):

2. 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 of those other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane.

3. If the holder agrees to permit another person to use this certification to alter the product, the holder must give the other person written evidence of that permission.

4. Instructions for Continued Airworthiness (ICA), AER-EFVS.737-804, Revision B, dated August 23, 2023, or later FAA accepted revision, shall be made available to the operator at the time of installation.

5. Electrical Wiring Interconnection Systems (EWIS) Instructions for Continued Airworthiness, AER-EFVS.737-804, Revision B, dated August 23, 2023, or later FAA accepted revision, shall be made available to the operator at the time of installation.

Certification Basis:

14 CFR Part 25 Regulations 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 the Boeing 737-600/-700/-800/-900 series aircraft modified by the installation of the AerAware System is as follows:

a. The type certification basis for the Boeing Model 737-600/-700/-800/-900 series aircraft is shown on TCDS A16WE for parts not changed or not affected by the change.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Date Reissued: January 31, 2025 (Continuation Sheet) Number: _S__T0__4__57__6_AT

b. The certification basis for parts changed or affected by the change since the reference date of application, December 20, 2019, is based upon part 25 as amended by amendment 25-138. Based on 14 CFR §§21.115 and 21.101, and FAA policy for significant level changes in FAA Order 8100.48, the certification basis for this modification was determined to be the same as the B737-900 per TCDS A16WE.

Regulations at the TCDS A16WE amendment level, 25-0 through 25-91:

14 CFR §§ 25.23(b)(2)(3); 25.251(b); 25.301(a)(b)(c); 25.303; 25.305(a)(b)(e);

25.307(a); 25.321(a)(b)(c)(d); 25.365(a)(b)(c)(d)(e); 25.561(b)(3)(c)(1);

25.562(b)(1); 25.581(a)(b)(1)(2)(c)(1)(2); 25.601; 25.603(a)(b)(c);

25.605(a)(b); 25.607(a)(b)(c); 25.609(a)(b); 25.619(a)(b)(c);

25.625(a)(b)(c); 25.771(a)(c); 25.777(a)(b)(c); 25.785(d)(2); 25.787(a)(b);

25.789(a); 25.803(a)(c); 25.1307(c); 25.1321(a)(b)(e); 25.1322,

25.1333(a); 25.1351(a); 25.1363(b); 25.1381(a)(b); 25.1501; 25.1519;

25.1523; 25.1525; 25.1529; 25.1541; 25.1555(a); 25.1581(a)(2) Regulations at a later amendment (as noted):

14 CFR §§ 25.143(a)(b)(1)(3) (25-129); 25.571(a)(b)(e)(1) (25-132);

25.611 (25-123); 25.613(a)(b)(c) (25-112); 25.773(a)(d)(e) (25-144);

25.853(a) (25-116); 25.869(a)(3) (25-123); 25.1301(a) (25-123);

25.1302(a)(b)(c)(d) (25-137); 25.1309(a)(b)(c)(d) (25-123);

25.1316(a)(b) (25-134); 25.1317(a)(b)(c)(d) (25-122); 25.1323(f)(g) (25-109); 25.1329(g)(h)(i) (25-119); 25.1353(a)(c) (25-123); 25.1357(a)(c) (25-123); 25.1411(a)(b)(1) (25-116); 25.1419 (25-129); 25.1431(a)(c) (25-113); 25.1447(c)(2)(i) (25-116); 25.1459(e) (25-124); 25.1583(e)(h) (25-130); 25.1585(a)(b) (25-105) 14 CFR Part 26 Regulations Compliance has been found for the following regulations at the noted Amendment levels:

14 CFR §§ 26.11(b)(c) (26-7); 26.47(b)(c) (26-7) ------------------- END -------------------- 4 4