STC ST12295IB

Supplemental type certificate · JET AVIATION AG

Holder
JET AVIATION AG · Switzerland
Status
Current · Issued
Status date
February 10, 2026
Applied
December 15, 2025
Product
Aircraft · Large Airplane
Certification basis
Part 25
Data sheet
TCDSA16WE
Foreign approvals
EASA 10088759 Rev0 12/02/2025

From FAA DRS, with our copy of the certificate PDF. DRS record last changed February 13, 2026.

What it approves

Installation of Cabin Modification

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.

IMPORT ST12295IB

JET AVIATION AG AESCHENGRABEN 6 4051 BASEL

SWITZERLAND Part 25 Title 14 Code of Federal Regulations A16WE The Boeing Company 737-700

1. This STC is applicable to serial number 32805 for the applicable model.

(See Limitations and Conditions Continued on Page 3 of 4) 12/15/2025 02/10/2026 John Yoo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 4

1. Installation of Cabin Modification in accordance with Jet Aviation AG Master Data List Number JBSL-M-03920MDL-001, Issue B, dated December 1, 2025, or later EASA approved revisions. This modification reconfigures the existing First Class Area to a Majlis Area and replace previous seats with new ones in the Business Class Area.

(See Description of Type Design Change Continued on Page 3 of 4)

2. Maintenance in accordance with Jet Aviation AG Instructions for Continued Airworthiness Document Number JBSL-M-03920ICA-001, Issue B, dated November 11, 2025, or later EASA accepted revision.

3. Operation in accordance with Jet Aviation AG Airplane Flight Manual Supplement Document Number JBSL-M-03920AFM-001, Issue D, dated December 15, 2025, or later EASA approved revision.

2. Embodiment of FAA STC ST12059IB is a prerequisite to the installation of this STC.

3. Operation must be in accordance with the Limitation Section of the Aircraft Flight Manual Supplement listed in the Description of Type Design section of this STC.

4. The installer must determine whether this design change is compatible with previously approved modifications.

5. 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 changes that are not significant in FAA order 8110.48A, the certification basis for this modification are as follows:

a. The Type Certification basis for the 737-700 series is shown on TCDS A16WE for parts not changed or not affected by the change.

b. The Type Certification basis for the 737-700 series is shown on TCDS A16WE for parts changed or affected by the change with the following additions:

(See Certification Basis on Page 4 of 4) 3 4

14 CFR 25 Amendments 25-1 through 25-153 for Sections 25.29, 25.301, 25.302, 25.303,

25.305, 25.307, 25.321, 25.337, 25.341, 25.365, 25.561, 25.562 except (c)(5)(6), 25.601,

25.603, 25.605, 25.609, 25.613, 25.619, 25.625, 25.785, 25.787, 25.789, 25.791, 25.795,

25.811, 25.812, 25.813, 25.815, 25.851, 25.853, 25.856, 25.899, 25.903, 25.1310, 25.1316,

25.1317, 25.1351, 25.1357, 25.1360, 25.1411, 25.1423, 25.1431, 25.1439, 25.1441, 25.1447,

25.1450, 25.1501, 25.1519, 25.1529, 25.1541, 25.1557, 25.1561, 25.1581, 25.1585, 25.1701

Special Federal Aviation Regulation (SFAR) No. 109 Article 2, 4(a), 4(b), 5, 9, 11, 12, 15(b), Effective 06/08/2009 ----------END----------

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 1

MakeModelData sheet
The Boeing Company737-700 SeriesA16WE