What it approves
Installation of a VVIP Cabin Interior
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 ST11981IB
JET AVIATION AG AESCHENGRABEN 6 4051 BASEL
SWITZERLAND Part 25 Title 14 Code of Federal Regulations T00015AT Gulfstream Aerospace Corporation GVIII-G700
1. The installer must determine whether this design change is compatible with previously approved modifications.
(See Limitations and Conditions Continued on Page 3 of 3) 03/21/2025 03/24/2025 John Yoo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 3
1. Installation of a VVIP Cabin Interior in accordance with Jet Aviation AG Master Data List Document Number JBSL-M-04131MDL-001, Issue D, dated March 19, 2025, or later EASA approved revision.
(See Description of Type Design Change Continued on Page 3 of 3)
2. Maintenance in accordance with Jet Aviation AG Instructions for Continued Airworthiness Document Numbers JBSL-M-04131ICA-001, Issue A, dated February 13, 2025, and JBSL-M-04131ECA-001, Issue C, dated March 18, 2025, or later EASA accepted revision.
3. Operation in accordance with Jet Aviation AG Airplane Flight Manual Supplement Document Number JBSL-M-04131AFM-001, Issue A, or later EASA approved revision.
4. Operation in accordance with Gulfstream Airplane Flight Manual Supplement Document Number GC87006M001, Issue A, dated June 04, 2024, or later EASA approved revision.
2. The aircraft is not configured to support Flight Crew Sleeping Facility operational approval because Flight Crew Sleeping Facility door is modified to keep the door always open.
3. Flight Crew Sleeping Facility / Forward Crew Compartment is limited to a maximum 1 crew member at all times, including during TTOL.
4. Aircraft must be maintained in accordance with the "Airworthiness Limitations" section of Jet Aviation AG Instructions for Continued Airworthiness Document Number JBSL-M-04131ICA-001, Issue A, dated February 13, 2025, or later EASA approved revision.
5. Aircraft must be operated in accordance with the "Limitations" section of the Airplane Flight Manual Supplement Documents listed in the Description of Type Design Change section of this STC.
6. 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.
7. This STC is applicable to all serial numbers for this Make-Model ----------END---------- 3 3
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Gulfstream Aerospace Corporation | GVIII-G700 | T00015AT |