STC ST00313BO

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therefore as specified hereon meets the airworthiness requirements of of Original Product 7\SH&HUWLILFDWH1XPEHU Make:

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Amended FebruaU\ 26, 25 Number:

ST00313BO FedEx Express 3640 Hacks Cross Road, Building D, 1st Floor Memphis, TN 38125 Certifies that the change in the type design for the following product with the limitations and conditions Part 25 the Federal Aviation Regulations A2NM Installation of a Rockwell Collins Head Up Display Model HGS-6700 with a Kollsman Enhanced Flight Vision System with the addition of a Copilot Monitor (HUD Repeater) on a Boeing 757-200 in accordance with FedEx Engineering Report No. 11-077, Revision H, dated February 7, 2025, or later FAA-approved revision.

 FedEx Aircraft Flight Manual Supplement, Engineering Report No. 10-120, Revision 5, dated February26, 2025, 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 )

BB 3DJH of 5 Boeing 757-200 Series October 17, 2008 July 12, 2011 March 17, 2017 July 5, 2012, February 20, 2014, February 1, 2021, February 26, 2025 for Manager, East Certification Branch

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Date oI transfer:

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Amended FebrXDU\ 26, 25 Number: ST00313BO 3DJH of 5

QHZDLUFUDIWDLUFUDIWHQJLQHRUSURSHOOHUPXVWSURYLGHWKDWSHUVRQZLWKDZULWWHQOLFHQVLQJDJUHHPHQWDFFHSWDEOHWRWKH)$$ 5HI&)5  )$$)RUP  683(56('(635(9,286(',7,21 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Amended FebrXaU\ 26, 25 (Continuation Sheet) Number: ST00313B0   Instructions for Continued Airworthiness (ICA) for the 757-200, FedEx EngineeringReport No.

10-068, Revision F, dated June 14, 2024, or later FAA acceptedrevisions, shall be made available to the operator at the time of installation.

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

 Required structural inspections for compliance with 14 CFR 25.571 on the 757-200are listed in Section 15, Airworthiness Limitations, of the Instructions for ContinuedAirworthiness (ICA) for the 757-200, FedEx Engineering Report No. 10-068 Revision F,dated June 14, 2024, or later FAA- approved revisions.

 This approval should not be extended to other aircraft of this model on which otherpreviously approved modifications are incorporated unless it is determine by theinstaller that the interrelationship between this change and any of those otherpreviously approved modifications will produce no adverse effect upon theairworthiness of that airplane.

 Electrical Wiring Interconnection Systems (EWIS) Instructions for ContinuedAirworthiness are listed in Section 3.2, Required Airplane Maintenance, Inspection, orAlternation, of the Instructions for Continued Airworthiness, FedEx Engineering ReportNo. 10-068, Revision F, dated June 14, 2024, or later FAA-approved revisions.

&HUWLILFDWLRQ%DVLV 2ULJLQDO67&  14 CFR Part 25 Regulations %DVHGRQ&)5††DQGDQGWKH)$$SROLF\IRUVLJQLILFDQWFKDQJHVLQ)$$2UGHU WKHFHUWLILFDWLRQEDVLVIRUWKH%RHLQJVHULHVDLUFUDIWPRGLILHGE\WKHLQVWDOODWLRQRID 5RFNZHOO&ROOLQV+HDGVXS'LVSOD\DQGD.ROOVPDQ(QKDQFHG)OLJKW9LVLRQ6\VWHPLVDVIROORZV D 7KHW\SHFHUWLILFDWLRQEDVLVIRUWKH%RHLQJVHULHVDLUFUDIWLVVKRZQRQ7&'6$10IRUSDUWV QRWFKDQJHGRUQRWDIIHFWHGE\WKHFKDQJH E 7KHFHUWLILFDWLRQEDVLVIRUSDUWVFKDQJHGRUDIIHFWHGE\WKHFKDQJHVLQFHWKHUHIHUHQFHGDWHRI DSSOLFDWLRQ2FWREHULVEDVHGXSRQSDUWDVDPHQGHGE\DPHQGPHQW%DVHG RQ&)5††DQGDQG)$$SROLF\IRUVLJQLILFDQWOHYHOFKDQJHVLQ)$$2UGHU WKHFHUWLILFDWLRQEDVLVIRUWKLVPRGLILFDWLRQZDVGHWHUPLQHGWREH  5HJXODWLRQVDWWKHODWHVWDPHQGPHQWOHYHOWKURXJK    &)5††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of 5

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14 CFR §§  25.301  5.303  25.581  25.601

25.607  25.609  25.619  25.621

25.623  25.771(a)(e)  25.1321(a)(e)  25.1331(a)(3)

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25.1525  25.1541 Special Conditions Number 25-407-6& dated June 11, 2010. Boeing 757-200 with Enhanced Flight Vision System.

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 part 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 at the noted Amendment levels:

14 CFR §§  26.11 (26-0)6.47 (26-1)  26.49 (26-1) &HUWLILFDWLRQ%DVLV FebruDr\1  Amendment):

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Installation of Copilot Monitor (HUD Repeater) 14 CFR Part 25 Regulations %DVHGRQ&)5††DQGDQGWKH)$$SROLF\IRUVLJQLILFDQWFKDQJHVLQ)$$2UGHU WKHFHUWLILFDWLRQEDVLVIRUSDUWVFKDQJHGRUDIIHFWHGE\WKLVFKDQJHVLQFHWKHUHIHUHQFHGDWHRI WKHDPHQGPHQWDSSOLFDWLRQ July 21, 2023LVEDVHGXSRQSDUWDVDPHQGHGE\$PHQGPHQW DQGLVGHWHUPLQHGWREHWKHIROORZLQJ (1' 5HJXODWLRQVDWWKHODWHVWDPHQGPHQWOHYHOWKURXJK &)5††23 25.301(a)(b)(c) 25.303 25.305(a)(b)

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25.605(a) 25.607 25.609(a)(b) 25.611(a)

25.613(a)(b) 25.619(a)(b)(c) 25.623 25.625(a)(b)

25.771(a)(e) 25.773 25.853(a) 25.1301(a)

25.1307(c) 25.1309(a-d) 25.1321(e) 25.1322(a)(b)(3)(d)(e)

25.1351(a)(1)

25.1353(a)(c)(d) 25.1357(a) 25.1431(a)(c)(d)

25.1501 25.1519 25.1523 25.1529

25.1581(a) 25.1585(a) 25.1713(c) 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 part 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 at the noted Amendment levels:

14 CFR §§  26.11(c)(1)(d)(4) (26-0) 3DJH5 of 5