STC SA00135MC

Supplemental Type Certificate Number SA00135MC

This certificate issued to: L3Harris Technologies Integrated Systems L.P.

7500 Maehr Road Waco, TX 76705

Part 23 of the Federal Aviation Regulations.

Original Product Make: Air Tractor Type Certificate Number: A19SW Model: AT-802

Installation of a mission system, updated cockpit configuration, crew oxygen system, and an increase in maximum operating altitude in accordance with L-3 Communications Integrated Systems L.P. Sealed Drawing List 60026.23.012, Revision G, dated March 17, 2016, or later FAA approved revision.

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

This design change is valid only for Air Tractor AT-802 series airplanes.

(Limitations and Conditions continued on page 3 of 3)

Date of Application: August 20, 2014 Date Reissued: May 4, 2023 Date of Issuance: March 22, 2016 Date Amended:

Signature

Title Loyd R. Hamilton ODA-750173-SW Administrator

Supplemental Type Certificate Number SA00135MC

To (Name and address of transferee)

From (Name and address of grantor)

Number: SA00135MC Date of Re-Issuance: May 4, 2023 Description of Type Design Change: (Continued) FAA Approved Airplane Flight Manual Supplement:

L-3 Communications Integrated Systems L.P. Document No. 60026.21.002, Revision IR, approved March 22, 2016, or later FAA approved revisions are a required part of this STC when the applicable item is installed.

FAA Approved Instructions for Continued Airworthiness (ICA):

L-3 Communications Integrated Systems L.P. Document No. 60026.23.015, Revision A, dated February 16, 2016, or later FAA accepted revisions are a required part of this STC when the applicable item is installed.

Limitations and Conditions: (Continued) The installer must determine whether this design change is compatible with previously approved modifications.

If the holder agrees to permit another person to use this certificate to alter a product, the holder must 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 the AT-802 airplane is as follows:

a. The type certification basis for AT-802 airplanes is shown on TCDS A19SW for 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 of application, August 20, 2014, is as shown in TCDS A19SW plus later amendment levels for the following paragraphs:

23.45(a) (Amdt 62), 23.65 (Amdt 62), 23.69(a) (Amdt 50), 23.141 (Amdt 45), 23.143(a)(2)(3)(4), (b), (c) (Amdt 50),

23.145 (Amdt 50), 23.155 (Amdt 50), 23.157(a)(2), (b)(1)(3)(4), (c)(2), (d)(1)(3)(4) (Amdt 50), 23.161(a), (b)(1),

(c)(1)(i)(ii)(2)(3)(4)(i)(ii)(iii) (Amdt 50), 23.175(a)(1)(3)(4), (b)(1)(i)(ii)(2) (Amdt 50), 23.177 (Amdt 62), 23.181(a), (b),

(d) (Amdt 62), 23.201(a), (b)(1)(2)(3), (c), (d), (f)(1)(5)(6)(7) (Amdt 62), 23.203(a), (b), (c)(1)(5)(6)(7) (Amdt 62),

23.207(a) (Amdt 50), 23.251 (Amdt 62), 23.253 (Amdt 62), 23.901(b)(1), (e)(1) (Amdt 53), 23.903(e)(3), (f), (g) (Amdt

62), 23.991(a)(2), (b), (c), (d) (Amdt 43), 23.1041 (Amdt 51), 23.1043(a), (b) (Amdt 51), 23.1045 (Amdt 51), 23.1091(a) (Amdt 51), 23.1441(a), (b), (c) (Amdt 43), 23.1443(b)(3) (Amdt 62), 23.1445 (Amdt 62), 23.1447(a), (c), (f) (Amdt 62),

23.1451 (Amdt 49), and 23.1453 (Amdt 49).

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A Type Certificate holder who allows a person to use the Type Certi ficate to manufacture a new aircraft, aircraft engine, or propeller must provide that person with a written licensing agreement acc e ptable to the FAA. (Ref. 14 CFR 21.55).