# STC ST04425CH

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: StandardAero Business Aviation Services LLC, United States
- Description: Installation of a Honeywell One Aero Edge Node (1AEN) in accordance with StandardAero Master Data List 1037081, Revision (B), dated June 9, 2020 or later FAA approved revision.
- Applied: August 6, 2019
- Status date: June 11, 2020
- Product: Aircraft
- Certification basis: Part 14, Part 21, Part 25
- Data sheets: [TCDS T00008NY](https://openairdocs.org/tcds/T00008NY), [TCDS A28NM](https://openairdocs.org/tcds/A28NM), [TCDS A46NM](https://openairdocs.org/tcds/A46NM), [TCDS T00063IB](https://openairdocs.org/tcds/T00063IB), [TCDS A16WE](https://openairdocs.org/tcds/A16WE), [TCDS A1NM](https://openairdocs.org/tcds/A1NM), [TCDS A2NM](https://openairdocs.org/tcds/A2NM), [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS T00001SE](https://openairdocs.org/tcds/T00001SE), [TCDS T00021SE](https://openairdocs.org/tcds/T00021SE), [TCDS A56NM](https://openairdocs.org/tcds/A56NM)
- Certificate PDF: https://openairdocs.org/files/sha256/c1/92/c1924d41df8f123a5720c56d0c7a4d580af13a86da2e982c1f7b689da7ccb203
- Approved model list and other attachments: [AML ST04425CH.pdf](https://openairdocs.org/files/sha256/cb/d0/cbd08bd92982d79b858392192e66ef4e1fd5c61b357f72baa69a2fca84ec0dc3)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7DB88FC535C43E3B8625859000706E4F.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/ST04425CH

## ADs that name it (0)

None.

## Approved models (80, first 50)

- Airbus Canada Limited Partnership BD-500-1A10 ([TCDS T00008NY](https://openairdocs.org/tcds/T00008NY))
- Airbus SAS A318-111 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A318-112 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A318-121 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A318-122 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A319-111 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A319-112 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A319-113 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A319-114 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A319-115 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A319-131 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A319-132 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A319-133 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A319-151N ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A320-211 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A320-212 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A320-214 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A320-216 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A320-231 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A320-232 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A320-233 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A320-251N ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A320-252N ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A320-253N ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A320-271N ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A320-272N ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A320-273N ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A321-111 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A321-112 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A321-131 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A321-211 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A321-212 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A321-213 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A321-231 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A321-232 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A321-251N ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A321-251NX ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A321-252N ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A321-252NX ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A321-253N ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A321-253NX ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A321-271N ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A321-271NX ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A321-272N ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A321-272NX ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))
- Airbus SAS A330-201 ([TCDS A46NM](https://openairdocs.org/tcds/A46NM))
- Airbus SAS A330-202 ([TCDS A46NM](https://openairdocs.org/tcds/A46NM))
- Airbus SAS A330-203 ([TCDS A46NM](https://openairdocs.org/tcds/A46NM))
- Airbus SAS A330-223 ([TCDS A46NM](https://openairdocs.org/tcds/A46NM))
- Airbus SAS A330-243 ([TCDS A46NM](https://openairdocs.org/tcds/A46NM))

All 80: https://openairdocs.org/stc/ST04425CH/models.md

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

Part 25 of the Federal Aviation Regulations. (See AML number ST04425CH for complete certification basis)

Installation of a Honeywell One Aero Edge Node (1AEN) in accordance with StandardAero Master Data List 1037081, Revision (B), dated June 9, 2020 or later FAA approved revision.

1. The installer must determine whether this design change is compatible with previously approved modifi cations.

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

StandardAero Business Aviation Services, LLC 1200 North Airport Drive Springfield, IL 62707 *See attached Federal Aviation Administration (FAA) Approved Model List (AML) number ST04425CH for approved aircraft models And applicable airworthiness regulations. Make: * Model: *

Date of application : August 6, 2019

Date of issuance: June 11, 2020 Date reissued :

(Signature) Dan Trigg, ODA Administrator StandardAero Business Aviation Services, LLC, Springfield, IL ODA-100079-CE

(Title)

Transfer the ownership of Supplemental Type Certificate Number

to (Name of transferee)

(Address of transferee)

(Number and street)

(City, State, and Zip code)

from (Name of grantor) (Print or type)

(Address of grantor)

(Number and street)

(City, State, and Zip code)

Signature of grantor (In ink):

### AML ST04425CH.pdf

Federal Aviation Administration (FAA) Approved Model List (AML) Number ST04425CH

StandardAero Business Aviation Services, LLC

FOR

Installation of a Honeywell One Aero Edge Node (1AEN) Revision A, June 11, 2020 Page 1 of 14

FAA APPROVED MASTER DATA LIST FAA ACCEPTED INSTRUCTIONS FOR CONTINUED AIRWORTHINESS ITEM AIRCRAFT MAKE AIRCRAFT MODEL TCDS NO. NUMBER/ REVISION* APPROVAL DATE* NUMBER/ REVISION* APPROVAL DATE* AML REVISION*/ DATE* 1 Yabora Industria Acronautica S.A.

ERJ 170-100 STD ERJ 170-100 LR ERJ 170-100 SU ERJ 170-100 SE ERJ 170-200 STD ERJ 170-200 LR ERJ 170-200 SU A56NM 1037081 Revision B June 9, 2020 1037983 Revision B April 20, 2020 Revision:A June 11, 2020 2 THE BOEING

COMPANY 717-200 A6WE 1037081 Revision B June 9, 2020 1037983 Revision B April 20, 2020 Revision:A June 11, 2020 3 THE BOEING

COMPANY 737-700 SERIES 737-800 SERIES 737-900ER SERIES A16WE 1037081 Revision B June 9, 2020 1037983 Revision B April 20, 2020 Revision:A June 11, 2020 4 THE BOEING

COMPANY 757-200 SERIES 757-300 SERIES A2NM 1037081 Revision B June 9, 2020 1037983 Revision B April 20, 2020 Revision:A June 11, 2020 5 THE BOEING

COMPANY 767-300 SERIES 767-400ER SERIES A1NM 1037081 Revision B June 9, 2020 1037983 Revision B April 20, 2020 Revision:A June 11, 2020 6 THE BOEING

COMPANY B777-200 SERIES B777-200LR SERIES B777-300ER SERIES T00001SE 1037081 Revision B June 9, 2020 1037983 Revision B April 20, 2020 Revision:A June 11, 2020 7 THE BOEING

COMPANY 787-8 787-9 T00021SE 1037081 Revision B June 9, 2020 1037983 Revision B April 20, 2020 Revision:A June 11, 2020 8 AIRBUS SAS A318 Model -111 A318 Model -112 A318 Model -121 A318 Model -122 A319 Model -111 A319 Model -112 A319 Model -113 A28NM 1037081 Revision B June 9, 2020 1037983 Revision B April 20, 2020 Revision:A June 11, 2020

Federal Aviation Administration (FAA) Approved Model List (AML) Number ST04425CH

StandardAero Business Aviation Services, LLC

FOR

Installation of a Honeywell One Aero Edge Node (1AEN) Revision A, June 11, 2020 Page 2 of 14 8 AIRBUS SAS A319 Model -114 A319 Model -115 A319 Model -131 A319 Model -132 A319 Model -133 A319 Model -151N A320 Model -211 A320 Model -212 A320 Model -214 A320 Model -231 A320 Model -232 A320 Model -233 A320 Model -251N A320 Model -271N A320 Model -216 A320 Model -252N A320 Model -272N A320 Model -253N A320 Model -273N A321 Model -111 A321 Model -112 A321 Model -131 A321 Model -211 A321 Model -231 A321 Model -212 A321 Model -213 A321 Model -232 A321 Model -271N A321 Model -251N A321 Model -253N A321 Model -272N A321 Model -252N A321 Model -251NX A321 Model -252NX A321 Model -253NX A321 Model -271NX A321 Model -272NX A28NM 1037081 Revision B June 9, 2020 1037983 Revision B April 20, 2020 Revision:A June 11, 2020

Federal Aviation Administration (FAA) Approved Model List (AML) Number ST04425CH

StandardAero Business Aviation Services, LLC

FOR

Installation of a Honeywell One Aero Edge Node (1AEN) Revision A, June 11, 2020 Page 3 of 14 9 AIRBUS SAS A330-201 A330-202 A330-203 A330-223 A330-243 A330-301 A330-302 A330-303 A330-321 A330-322 A330-323 A330-341 A330-342 A330-343 A46NM 1037081 Revision B June 9, 2020 1037983 Revision B April 20, 2020 Revision:A June 11, 2020 10 AIRBUS SAS A350-941 T00063IB 1037081 Revision B June 9, 2020 1037983 Revision B April 20, 2020 Revision:A June 11, 2020 11 AIRBUS CANADA

**LIMITED**

PARTNERSH IP BD-500-1A10 T00008NY 1037081 Revision B June 9, 2020 1037983 Revision B April 20, 2020 Revision:A June 11, 2020 *Or later FAA Approved Revision/Date

FAA Approved:

Dan Trigg,ODA Administrator StandardAero Business Aviation Services, LLC Springfield, Illinois FAA ODA-100079-CE

Issued Date: June 11, 2020

Federal Aviation Administration (FAA) Approved Model List (AML) Number ST04425CH

StandardAero Business Aviation Services, LLC

FOR

Installation of a Honeywell One Aero Edge Node (1AEN) Revision A, June 11, 2020 Page 4 of 14 Certification Basis for Alteration:

The certification basis for the changed aircraft as described in this AML is as follows:

AML Item 1

Based on 14 CFR §§ 21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the Yabora Industria Acronautica S.A. ERJ 170-100 STD, ERJ 170-100 LR, ERJ 170-100 SU, ERJ 170-100 SE, ERJ 170-200 STD, ERJ 170-200 LR AND ERJ 170-200 SU aircraft, Installation of a Honeywell One Aero Edge Node (1AEN) is as follows:

a. The type certification basis for Yabora Industria Acronautica S.A. ERJ 170-100 STD, ERJ 170-100 LR, ERJ 170-100 SU, ERJ 170-100 SE, ERJ 170-200 STD, ERJ 170-200 LR AND ERJ 170-200 SU aircraft is shown on TCDS A56NM 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 6, 2019 is based upon TCDS A56NM and §§ 14 CFR Part 25. Based on 14 CFR §§ 21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the baseline modification was determined to be:

Regulations at the amendment level in TCDS A56NM

25.1(a, b)(25-0), 25.301(a, b)(25-23), 25.303(25-23), 25.305(a, b)(25-86), 25.307(a)(25-72), 25.561(a-d)(25-91), 25.601(25-0), 25.603(a, b)(25-46)

25.605(a)(25-46), 25.609(a)(25-0), 25.613(a, b)(25-112), 25.619(a-c)(25-23), 25.625(a-c)(25-72), 25.789(a)(25-46), 25.1307(c)(25-72)

25.1351(a)(25-72), 25.1501(a)(25-42), 25.1519(25-0), 25.1529(25-54), 25.1581(a-d)(25-72), 25.1585(a)(25-105).

Regulations at later amendment level

25.611(a, b)(25-123), 25.1301(a)(25-123), 25.1309(a, b, d, e)(25-123), 25.1353(a)(25-123), 25.1357(a-c)(25-123), 25.1431(a, c, d)(25-113).

Federal Aviation Administration (FAA) Approved Model List (AML) Number ST04425CH

StandardAero Business Aviation Services, LLC

FOR

Installation of a Honeywell One Aero Edge Node (1AEN) Revision A, June 11, 2020 Page 5 of 14

AML Item 2

Based on 14 CFR §§ 21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for The Boeing Company 717-200 aircraft, Installation of a Honeywell One Aero Edge Node (1AEN) is as follows:

a. The type certification basis for The Boeing Company 717-200 aircraft is shown on TCDS A6WE 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 6, 2019 is based upon TCDS A6WE and §§ 14 CFR Part 25. Based on 14 CFR §§ 21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the baseline modification was determined to be TCDS A6WE

Regulations at the amendment level in TCDS A6WE

25.1(a, b)(25-0), 25.301(a, b)(25-23), 25.303(25-23), 25.307(a)(25-72), 25.601(25-0), 25.603(a, b)(25-46), 25.605(a)(25-46), 25.609(a)(25-0)

25.619(a-c)(25-23), 25.625(a-c)(25-72), 25.789(a)(25-46), 25.1307(c)(25-72), 25.1351(a)(25-72), 25.1501(a)(25-42), 25.1519(25-0), 25.1529(25-54)

25.1581(a-d)(25-72).

Regulations at later amendment level

25.305(a, b)(25-86), 25.561(a-d)(25-91), 25.611(a, b)(25-123), 25.613(a, b)(25-112), 25.1301(a)(25-123), 25.1309(a, b, d, e)(25-123)

25.1353(a)(25-123), 25.1357(a-c)(25-123), 25.1431(a, c, d)(25-113), 25.1585(a)(25-105).

Federal Aviation Administration (FAA) Approved Model List (AML) Number ST04425CH

StandardAero Business Aviation Services, LLC

FOR

Installation of a Honeywell One Aero Edge Node (1AEN) Revision A, June 11, 2020 Page 6 of 14

AML Item 3

Based on 14 CFR §§ 21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the The Boeing Company 737-700 Series, 737-800 Series, 737-900ER Series aircraft, Installation of a Honeywell One Aero Edge Node (1AEN) is as follows:

a. The type certification basis for The Boeing Company 737-700 Series, 737-800 Series, 737-900ER Series aircraft is shown on TCDS A16WE 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 6, 2019 is based upon TCDS A16WE and §§ 14 CFR Part 25. Based on 14 CFR §§ 21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the baseline modification was determined to be TCDS A16WE.

Regulations at the amendment level in TCDS A16WE

25.1(a, b)(25-0), 25.301(a, b)(25-23), 25.303(25-23), 25.305(a, b)(25-86), 25.307(a)(25-72), 25.561(a-d)(25-91), 25.601(25-0), 25.603(a, b)(25-46)

25.605(a)(25-46), 25.609(a)(25-0), 25.619(a-c)(25-23), 25.625(a-c)(25-72), 25.789(a)(25-46), 25.1307(c)(25-72), 25.1351(a)(25-72), 25.1501(a)(25-42)

25.1519(25-0), 25.1529(25-54), 25.1581(a-d)(25-72), 25.1585(a)(25-105).

Regulations at later amendment level

25.611(a, b)(25-123), 25.613(a, b)(25-112), 25.1301(a)(25-123), 25.1309(a, b, d, e)(25-123), 25.1353(a)(25-123), 25.1357(a-c)(25-123)

25.1431(a, c, d)(25-113).

Federal Aviation Administration (FAA) Approved Model List (AML) Number ST04425CH

StandardAero Business Aviation Services, LLC

FOR

Installation of a Honeywell One Aero Edge Node (1AEN) Revision A, June 11, 2020 Page 7 of 14

AML Item 4

Based on 14 CFR §§ 21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the The Boeing Company 757-200 Series, 757-300 Series aircraft, Installation of a Honeywell One Aero Edge Node (1AEN) is as follows:

a. The type certification basis for The Boeing Company 757-200 Series, 757-300 Series aircraft is shown on TCDS A2NM 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 6, 2019 is based upon TCDS A2NM and §§ 14 CFR Part 25. Based on 14 CFR §§ 21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the baseline modification was determined to be TCDS A2NM.

Regulations at the amendment level in TCDS A2NM

25.1(a, b)(25-0), 25.301(a, b)(25-23), 25.303(25-23), 25.307(a)(25-72), 25.601(25-0), 25.603(a, b)(25-46), 25.605(a)(25-46), 25.609(a)(25-0)

25.619(a-c)(25-23), 25.625(a-c)(25-72), 25.789(a)(25-46), 25.1307(c)(25-72), 25.1351(a)(25-72), 25.1501(a)(25-42), 25.1519(25-0), 25.1529(25-54)

25.1581(a-d)(25-72).

Regulations at later amendment level

25.305(a, b)(25-86), 25.561(a-d)(25-91), 25.611(a, b)(25-123), 25.613(a, b)(25-112), 25.1301(a)(25-123), 25.1309(a, b, d, e)(25-123)

25.1353(a)(25-123), 25.1357(a-c)(25-123), 25.1431(a, c, d)(25-113), 25.1585(a)(25-105).

Federal Aviation Administration (FAA) Approved Model List (AML) Number ST04425CH

StandardAero Business Aviation Services, LLC

FOR

Installation of a Honeywell One Aero Edge Node (1AEN) Revision A, June 11, 2020 Page 8 of 14

AML Item 5

Based on 14 CFR §§ 21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the The Boeing Company 767-300 Series, 767-400 ER Series aircraft, Installation of a Honeywell One Aero Edge Node (1AEN) is as follows:

a. The type certification basis for The Boeing Company 767-300 Series, 767-400 ER Series aircraft is shown on TCDS A1NM 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 6, 2019 is based upon TCDS A1NM and §§ 14 CFR Part 25. Based on 14 CFR §§ 21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the baseline modification was determined to be TCDS A1NM.

Regulations at the amendment level in TCDS A1NM

25.1(a, b)(25-0), 25.301(a, b)(25-23), 25.303(25-23), 25.305(a, b)(25-86), 25.307(a)(25-72), 25.601(25-0), 25.603(a, b)(25-46), 25.605(a)(25-46)

25.609(a)(25-0), 25.619(a-c)(25-23), 25.625(a-c)(25-72), 25.789(a)(25-46), 25.1307(c)(25-72), 25.1351(a)(25-72), 25.1501(a)(25-42), 25.1519(25-0)

25.1529(25-54), 25.1581(a-d)(25-72).

Regulations at later amendment level

25.561(a-d)(25-91), 25.611(a, b)(25-123), 25.613(a, b)(25-112), 25.1301(a)(25-123), 25.1309(a, b, d, e)(25-123), 25.1353(a)(25-123)

25.1357(a-c)(25-123), 25.1431(a, c, d)(25-113), 25.1585(a)(25-105).

Federal Aviation Administration (FAA) Approved Model List (AML) Number ST04425CH

StandardAero Business Aviation Services, LLC

FOR

Installation of a Honeywell One Aero Edge Node (1AEN) Revision A, June 11, 2020 Page 9 of 14

AML Item 6

Based on 14 CFR §§ 21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the The Boeing Company 777-200 Series, 777-200LR Series, 777-300ER Series aircraft, Installation of a Honeywell One Aero Edge Node (1AEN) is as follows:

a. The type certification basis for The Boeing Company 777-200 Series, 777-200LR Series, 777-300ER Series aircraft is shown on TCDS T00001SE 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 6, 2019 is based upon TCDS T00001SE and §§ 14 CFR Part 25. Based on 14 CFR §§ 21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the baseline modification was determined to be TCDS T00001SE.

Regulations at the amendment level in TCDS T00001SE

25.1(a, b)(25-0), 25.301(a, b)(25-23), 25.303(25-23), 25.305(a, b)(25-86), 25.307(a)(25-72), 25.561(a-d)(25-91), 25.601(25-0), 25.603(a, b)(25-46)

25.605(a)(25-46), 25.609(a)(25-0), 25.619(a-c)(25-23), 25.625(a-c)(25-72), 25.789(a)(25-46), 25.1307(c)(25-72), 25.1351(a)(25-72), 25.1501(a)(25-42)

25.1519(25-0), 25.1529(25-54), 25.1581(a-d)(25-72).

Regulations at later amendment level

25.611(a, b)(25-123), 25.613(a, b)(25-112), 25.1301(a)(25-123), 25.1309(a, b, d, e)(25-123), 25.1353(a)(25-123), 25.1357(a-c)(25-123)

25.1431(a, c, d)(25-113), 25.1585(a)(25-105).

Federal Aviation Administration (FAA) Approved Model List (AML) Number ST04425CH

StandardAero Business Aviation Services, LLC

FOR

Installation of a Honeywell One Aero Edge Node (1AEN) Revision A, June 11, 2020 Page 10 of 14

AML Item 7

Based on 14 CFR §§ 21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the The Boeing Company 787-9, 787-8 aircraft, Installation of a Honeywell One Aero Edge Node (1AEN) is as follows:

a. The type certification basis for The Boeing Company 787-9, 787-8 aircraft is shown on TCDS T00021SE 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 6, 2019 is based upon TCDS T00021SE and §§ 14 CFR Part 25. Based on 14 CFR §§ 21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the baseline modification was determined to be TCDS T00021SE.

Regulations at the amendment level in TCDS T00021SE

25.1(a, b)(25-0), 25.301(a, b)(25-23), 25.303(25-23), 25.305(a, b)(25-86), 25.307(a)(25-72), 25.561(a-d)(25-91), 25.601(25-0), 25.603(a, b)(25-46)

25.605(a)(25-46), 25.609(a)(25-0), 25.611(a, b)(25-123), 25.613(a, b)(25-112), 25.619(a-c)(25-23), 25.625(a-c)(25-72), 25.789(a)(25-46)

25.1301(a)(25-123), 25.1307(c)(25-72), 25.1309(a, b, d, e)(25-123), 25.1351(a)(25-72), 25.1353(a)(25-123), 25.1357(a-c)(25-123)

25.1431(a, c, d)(25-113), 25.1501(a)(25-42), 25.1519(25-0), 25.1529(25-54), 25.1581(a-d)(25-72), 25.1585(a)(25-105).

Regulations at later amendment level None

Federal Aviation Administration (FAA) Approved Model List (AML) Number ST04425CH

StandardAero Business Aviation Services, LLC

FOR

Installation of a Honeywell One Aero Edge Node (1AEN) Revision A, June 11, 2020 Page 11 of 14

AML Item 8

Based on 14 CFR §§ 21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the Airbus SAS A318 Model -111, A318 Model -112, A318 Model -121, A318 Model -122, A319 Model -111, A319 Model -112, A319 Model -113, A319 Model -114, A319 Model -115, A319 Model -131, A319 Model -132, A319 Model -133, A319 Model -151N, A320 Model -211, A320 Model -212, A320 Model - 214, A320 Model -231, A320 Model -232, A320 Model -233, A320 Model -251N, A320 Model -271N, A320 Model -216, A320 Model -252N, A320 Model -272N, A320 Model -253N, A320 Model -273N, A321 Model -111, A321 Model -112, A321 Model -131, A321 Model -211, A321 Model -231, A321 Model -212, A321 Model -213, A321 Model -232, A321 Model -271N, A321 Model -251N, A321 Model -253N, A321 Model -272N, A321 Model -252N, A321 Model -251NX, A321 Model -252NX, A321 Model -253NX, A321 Model -271NX, A321 Model -272NX aircraft, Installation of a Honeywell One Aero Edge Node (1AEN) is as follows:

a. The type certification basis for Airbus SAS A318 Model -111, A318 Model -112, A318 Model -121, A318 Model -122, A319 Model - 111, A319 Model -112, A319 Model -113, A319 Model -114, A319 Model -115, A319 Model -131, A319 Model -132, A319 Model - 133, A319 Model -151N, A320 Model -211, A320 Model -212, A320 Model -214, A320 Model -231, A320 Model -232, A320 Model - 233, A320 Model -251N, A320 Model -271N, A320 Model -216, A320 Model -252N, A320 Model -272N, A320 Model -253N, A320 Model -273N, A321 Model -111, A321 Model -112, A321 Model -131, A321 Model -211, A321 Model -231, A321 Model -212, A321 Model -213, A321 Model -232, A321 Model -271N, A321 Model -251N, A321 Model -253N, A321 Model -272N, A321 Model -252N, A321 Model -251NX, A321 Model -252NX, A321 Model -253NX, A321 Model -271NX, A321 Model -272NX aircraft is shown on TCDS A28NM 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 6, 2019 is based upon TCDS A28NM and §§ 14 CFR Part 25. Based on 14 CFR §§ 21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the baseline modification was determined to be TCDS A28NM.

Regulations at the amendment level in TCDS A28NM

25.1(a, b)(25-0), 25.301(a, b)(25-23), 25.303(25-23), 25.601(25-0), 25.603(a, b)(25-46), 25.605(a)(25-46), 25.609(a)(25-0), 25.619(a-c)(25-23)

25.789(a)(25-46), 25.1501(a)(25-42), 25.1519(25-0), 25.1529(25-54).

Regulations at later amendment level

25.305(a, b)(25-86), 25.307(a)(25-72), 25.561(a-d)(25-91), 25.611(a, b)(25-123), 25.613(a, b)(25-112), 25.625(a-c)(25-72), 25.1301(a)(25-123)

25.1307(c)(25-72), 25.1309(a, b, d, e)(25-123), 25.1351(a)(25-72), 25.1353(a)(25-123), 25.1357(a-c)(25-123), 25.1431(a, c, d)(25-113)

25.1581(a-d)(25-72), 25.1585(a)(25-105).

Federal Aviation Administration (FAA) Approved Model List (AML) Number ST04425CH

StandardAero Business Aviation Services, LLC

FOR

Installation of a Honeywell One Aero Edge Node (1AEN) Revision A, June 11, 2020 Page 12 of 14

AML Item 9

Based on 14 CFR §§ 21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the Airbus SAS A330-201, A330-202, A330-203, A330-223, A330-243, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342, A330-343 aircraft, Installation of a Honeywell One Aero Edge Node (1AEN) is as follows:

a. The type certification basis for Airbus SAS A330-201, A330-202, A330-203, A330-223, A330-243, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342, A330-343 aircraft is shown on TCDS A46NM 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 6, 2019 is based upon TCDS A46NM and §§ 14 CFR Part 25. Based on 14 CFR §§ 21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the baseline modification was determined to be TCDS A46NM.

Regulations at the amendment level in TCDS A46NM

25.1(a, b)(25-0), 25.301(a, b)(25-23), 25.303(25-23), 25.601(25-0), 25.603(a, b)(25-46), 25.605(a)(25-46), 25.609(a)(25-0), 25.619(a-c)(25-23)

25.789(a)(25-46), 25.1501(a)(25-42), 25.1519(25-0), 25.1529(25-54), 25.1581(a-d)(25-72), 25.1585(a)(25-105).

Regulations at later amendment level

25.305(a, b)(25-86), 25.307(a)(25-72), 25.561(a-d)(25-91), 25.611(a, b)(25-123), 25.613(a, b)(25-112), 25.625(a-c)(25-72), 25.1301(a)(25-123)

25.1307(c)(25-72), 25.1309(a, b, d, e)(25-123), 25.1351(a)(25-72), 25.1353(a)(25-123), 25.1357(a-c)(25-123), 25.1431(a, c, d)(25-113).

Federal Aviation Administration (FAA) Approved Model List (AML) Number ST04425CH

StandardAero Business Aviation Services, LLC

FOR

Installation of a Honeywell One Aero Edge Node (1AEN) Revision A, June 11, 2020 Page 13 of 14

AML Item 10

Based on 14 CFR §§ 21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the Airbus SAS A350-941 aircraft, Installation of a Honeywell One Aero Edge Node (1AEN) is as follows:

a. The type certification basis for Airbus SAS A350-941 aircraft is shown on TCDS T00063IB 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 6, 2019 is based upon TCDS T00063IB and §§ 14 CFR Part 25. Based on 14 CFR §§ 21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the baseline modification was determined to be TCDS T00063IB.

Regulations at the amendment level in TCDS T00063IB

25.1(a, b)(25-0), 25.301(a, b)(25-23), 25.303(25-23), 25.305(a, b)(25-86), 25.307(a)(25-72), 25.561(a-d)(25-91), 25.601(25-0), 25.603(a, b)(25-46)

25.605(a)(25-46), 25.609(a)(25-0), 25.611(a, b)(25-123), 25.613(a, b)(25-112), 25.619(a-c)(25-23), 25.625(a-c)(25-72), 25.789(a)(25-46)

25.1301(a)(25-123), 25.1307(c)(25-72), 25.1309(a, b, d, e)(25-123), 25.1351(a)(25-72), 25.1353(a)(25-123), 25.1357(a-c)(25-123)

25.1431(a, c, d)(25-113), 25.1501(a)(25-42), 25.1519(25-0), 25.1529(25-54), 25.1581(a-d)(25-72), 25.1585(a)(25-105).

Regulations at later amendment level None

Federal Aviation Administration (FAA) Approved Model List (AML) Number ST04425CH

StandardAero Business Aviation Services, LLC

FOR

Installation of a Honeywell One Aero Edge Node (1AEN) Revision A, June 11, 2020 Page 14 of 14

AML Item 11

Based on 14 CFR §§ 21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the Airbus Canada Limited Partnership BD-500-1A10 aircraft, Installation of a Honeywell One Aero Edge Node (1AEN) is as follows:

a. The type certification basis for Airbus Canada Limited Partnership BD-500-1A10 aircraft is shown on TCDS T00008NY 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 6, 2019 is based upon TCDS T00008NY and §§ 14 CFR Part 25. Based on 14 CFR §§ 21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the baseline modification was determined to be TCDS T00008NY

Regulations at the amendment level in TCDS T00008NY

25.1(a, b)(25-0), 25.301(a, b)(25-23), 25.303(25-23), 25.305(a, b)(25-86), 25.307(a)(25-72), 25.561(a-d)(25-91), 25.601(25-0), 25.603(a, b)(25-46)

25.605(a)(25-46), 25.609(a)(25-0), 25.611(a, b)(25-123), 25.613(a, b)(25-112), 25.619(a-c)(25-23), 25.625(a-c)(25-72), 25.789(a)(25-46)

25.1301(a)(25-123), 25.1307(c)(25-72), 25.1309(a, b, d, e)(25-123), 25.1351(a)(25-72), 25.1353(a)(25-123), 25.1357(a-c)(25-123)

25.1431(a, c, d)(25-113), 25.1501(a)(25-42), 25.1519(25-0), 25.1529(25-54), 25.1581(a-d)(25-72), 25.1585(a)(25-105).

Regulations at later amendment level None

## Every issue (1)

- June 11, 2020: Issued, Current. [certificate](https://openairdocs.org/files/sha256/c1/92/c1924d41df8f123a5720c56d0c7a4d580af13a86da2e982c1f7b689da7ccb203), [AML ST04425CH.pdf](https://openairdocs.org/files/sha256/cb/d0/cbd08bd92982d79b858392192e66ef4e1fd5c61b357f72baa69a2fca84ec0dc3)

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