What it approves
Installation of Air Filtration
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___
Part of .
ST04537NY Kilroy Aviation, LLC 5485 Airport Terminal Road, Unit A Salisbury, MD 21804 25 Federal AviationRegulations T00011AT Yaborã Indústria Aeronáutica S.A.
EMB-145LR, EMB-135KL
1. Installation of Air Filtration in Embraer EMB-145LR and EMB-135KL series aircraft per the Listing, Master Data - Installation, Kilroy Aviation Document J536-0030-001, revision A, dated 09/22/2020, or later FAA-approved revisions.
See continuation sheet 3 through end.
1. The installer must determine whether this design change is compatible with existing installed approved modifications.
2. 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. See continuation sheet 3 through end.
05/30/2020 10/06/2020 for Timothy J. Hadsall Acting Manager, New York ACO Branch Compliance & Airworthiness Division Aircraft Certification Service 3
FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___
ST04537NY 3
ST04537NY Date of Issuance: October 06, 2020
Description of Type Design Change: (continued)
2. ICA. Comply with FAA-accepted Instructions for Continued Airworthiness (ICA), Kilroy Aviation Document J535-ICA, revision "-", dated 09/02/2020 or later FAA-accepted revisions.
3. ALS. There are no Airworthiness Limitations associated with this modification.
4. EWIS ICA. The FAA has reviewed the applicant's assessment of existing Electrical Wiring Interconnection System Instructions for Continued Airworthiness (EWIS ICA) and found that no additional EWIS ICA tasks are required.
5. AFMS. There are no changes to the Airplane Flight Manual.
Limitations and Conditions: (continued) End of Limitations
Certification Basis:
1. Based on 14 CFR §§ 21.101 and 21.115, and the FAA policy for non-significant changes in FAA Order 8110.48, the certification basis for the Embraer EMB-145LR and EMB-135KL series for this design change modification is listed below.
a. For parts not altered or affected by the design change, as shown on Type Certificate Data Sheet (TCDS) T00011AT.
b. For parts altered or affected by the design change since the reference date of project application May 30, 2020, the certification basis is based upon 14CFR parts 25 & 26 as amended through Amendment 25-84 et al., and through Amendment 26-6 as listed in the TCDS.
Regulations at the amendment level in TCDS: 14 CFR §§ 25.29, 25.301, 25.303, 25.305,
25.307, 25.561, 25.601, 25.603, 25.605, 25.607, 25.609, 25.611, 25.613, 25.625, 25.831, 25.853,
25.1301, 25.1309, 25.1501, 25.1529, 26.11.
Regulations above the TCDS amendment level: None
c. Applicable provisions of 14 CFR part 26 are included in the certification basis and listed above. For any future Part 26 amendments, the holder of this STC must demonstrate compliance with the applicable sections as listed in the TCDS.
END 3 3
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