# STC SR00202IB

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: AEROLITE AG, Switzerland
- Description: Installation of Emergency Medical Services (EMS) Equipment, either P/N 135-0238317-501 or P/N
135-0238317-502
- Applied: March 3, 2023
- Status date: March 13, 2026
- Product: Aircraft, Rotorcraft
- Certification basis: Part 27
- Foreign approvals: EASA 10064985 Rev. 5
- Data sheets: [TCDS H88EU](https://openairdocs.org/tcds/H88EU)
- Certificate PDF: https://openairdocs.org/files/sha256/41/31/4131efdc323017e583f113f9946a0033ccacece4555a57adb2963620f746819b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104145818320260317135521.0001
- DRS record last changed: March 17, 2026
- Page: https://openairdocs.org/stc/SR00202IB

## ADs that name it (0)

None.

## Approved models (2)

- Airbus Helicopters Deutschland GmbH (AHD) EC135P3 ([TCDS H88EU](https://openairdocs.org/tcds/H88EU))
- Airbus Helicopters Deutschland GmbH (AHD) EC135T3 ([TCDS H88EU](https://openairdocs.org/tcds/H88EU))

## 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.

**IMPORT SR00202IB**

AEROLITE AG 6373 ENNETBUERGEN, SWITZERLAND Part 27 Title 14 Code of Federal Regulations H88EU Airbus Helicopters Deutschland GmbH EC135P3, EC135T3

1. This STC is applicable only to:

a. Airbus Helicopters Deutschland GmbH model EC135T3, S/N 2001 and above, equipped with the Helionix cockpit variant.

(See Limitations and Conditions Continued on Page 3 of 4) 02/03/2023 06/11/2024 10/10/2024 03/13/2026 John Yoo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 4

1. Installation of Emergency Medical Services (EMS) Equipment, either P/N 135-0238317-501 or P/N 135-0238317-502, in accordance with Aerolite Master Document List (MDL) MDL-17-005, Revision Y, dated January 27, 2026, or later EASA approved revisions.

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

2. EMS Equipment 135-0238317-501 configuration for either EC135P3 or EC135T3 models, equipped with the Helionix cockpit variant:

a. Maintenance in accordance with Aerolite Instructions for Continued Airworthiness Operations Manual OPM-135-0238317-501, Revision J, dated February 7, 2025, or later EASA approved revision.

b. Operation in accordance with Aerolite Flight Manual Supplement FMS-135-0238317-501, Revision K, dated September 25, 2024, or later EASA approved revision.

3. EMS Equipment 135-0238317-502 configuration for either EC135P3 or EC135T3 models, equipped with the Helionix cockpit variant:

a. Maintenance in accordance with Aerolite Instructions for Continued Airworthiness Operations Manual OPM-135-0238317-502, Revision F, dated August 19, 2025, or later EASA approved revision.

b. Operation in accordance with Aerolite Flight Manual Supplement FMS-135-0238317-502, Revision F, dated January 26, 2026, or later EASA approved revision.

b. Airbus Helicopters Deutschland GmbH model EC135P3, S/N 2006 and above, equipped with the Helionix cockpit variant.

2. 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.

3. Maintenance must be in accordance with the "Airworthiness Limitation" Section of the Operations Manual 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 on Page 4 of 4) 3 4

The certification basis for the modified Airbus Helicopters Deutschland GmbH EC135P3 and EC135T3 is as shown on TCDS H88EU with the following exceptions:

- 14 CFR 21.21(b)(1) and 27.562(b): Emergency Landing Dynamic Conditions;

ELOS Memo Number ST11664IB-R-C-1, dated March 27, 2024.

- 14 CFR 27.807(b) Emergency Exits; ELOS Memo Number ST11664IB-R-27.807, dated April 24, 2024; acceptance of EASA CRI D-01.

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## Every issue (2)

- March 13, 2026: Amended, Current. [certificate](https://openairdocs.org/files/sha256/41/31/4131efdc323017e583f113f9946a0033ccacece4555a57adb2963620f746819b)
- October 10, 2024: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/d8/6e/d86edaa5f14c8089378df6c2acdd378a9fe910db1734aa073226dfd954970485)

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