# STC SR02114NY-D - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Diagnostic Solution International LLC, United States - Description: Installation of a Honeywell Chadwick Model 15175 VXP System - Applied: January 27, 2006 - Status date: December 14, 2020 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 27 - Data sheets: [TCDS H88EU](https://openairdocs.org/tcds/H88EU) - Certificate PDF: https://openairdocs.org/files/sha256/26/70/26708955ba36e2b2a3072a4b791be04ec8a936066380cce4c8c43454c60ef1a4 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/FA9CC989A50870DF862586CB0051B056.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SR02114NY-D ## ADs that name it (0) None. ## Approved models (9) - Airbus Helicopters Deutschland GmbH EC135 P1 ([TCDS H88EU](https://openairdocs.org/tcds/H88EU)) - Airbus Helicopters Deutschland GmbH EC135 P2 ([TCDS H88EU](https://openairdocs.org/tcds/H88EU)) - Airbus Helicopters Deutschland GmbH EC135 P2+ ([TCDS H88EU](https://openairdocs.org/tcds/H88EU)) - Airbus Helicopters Deutschland GmbH EC135 T1 ([TCDS H88EU](https://openairdocs.org/tcds/H88EU)) - Airbus Helicopters Deutschland GmbH EC135 T2 ([TCDS H88EU](https://openairdocs.org/tcds/H88EU)) - Airbus Helicopters Deutschland GmbH EC135 T2+ ([TCDS H88EU](https://openairdocs.org/tcds/H88EU)) - Airbus Helicopters Deutschland GmbH EC135P3 ([TCDS H88EU](https://openairdocs.org/tcds/H88EU)) - Airbus Helicopters Deutschland GmbH EC135T3 ([TCDS H88EU](https://openairdocs.org/tcds/H88EU)) - Airbus Helicopters Deutschland GmbH EC635T2+ ([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. FAA Form 8110-2 (5/14) Page 1 of 3 Number: SR02114NY-D This certificate issued to: Diagnostic Solutions International LLC 2580 East Philadelphia, Unit C Ontario, CA 91761 Part 27 of the Federal Aviation Regulations. Make: Eurocopter Deutschland GmbH H88EU Model: EC135 Description of Type Design Change: Installation of a Honeywell Chadwick Model 15175 VXP System in accordance with: 1. Keystone Helicopter Installation Drawing List IDL01152, revision B, dated 4/26/2006 or later FAA approved revision or 2. Honeywell Master Drawing List 159-08340-0001, revisi on -, dated 10/13/2010 or later FAA Approved revision. 1) The installation is limited to the EC135 P2, EC135 T2, EC135 P2+ and EC135 T2+ models. 2) Helicopter Instructions for Continued Airworthiness, Honeywell Chadwick Model 15175 VXP System Installed in Eurocopter Model EC135 P2, Report No. IC01152, revision -, dated 4/26/2006 or later FAA accepted revision or Honeywell Instructions for Continued Airworthiness, document no. 18645, revision -, dated 8/18/2010 or later FAA accepted revision must be made available to the operator at the time of installation. 3) The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect on the airworthiness of the aircraft. 4) If the holder agrees to permit another person to use this ce rtificate to alter the product, the holder shall give the other person written evidence of that permission. Date of Application: January 27, 2006 Date Reissued: June 5, 2009; March 24, 2020, December 14, 2020 Date of Issuance: May 10, 2006 Date Amended: October 26, 2010 By Direction of the Administrator Signature Original signed by Tina Miller for Charlene Combs Title Program Manager, Wichita ACO Branch FAA Form 8110-2 (5/14) Page 2 of 3 Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: SR02114NY-D To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement): United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SR02114NY-D FAA Form 8110-2 (5/14) Page 3 of 3 Certification Basis: Based on 14 CFR ยงยง 21.101 and 21.115 and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this change is as follows: a. The type certification basis for par ts not changed or not affected by this change is shown on TCDS H88EU. b. The certification basis for parts changed or affected by this change since the date of application, January 27, 2006, is determined to be: Regulations at the latest amendment: None. Regulations at an intermediate amendment: None. Regulations at the amendment level on TCDS H88EU: 2X.XXXX27.301 (a)(b)(c) Amdt. 27-0; 27.303 Amdt. 27-0; 27.305 (a) Amdt. 27-0; 27.307 (a) Amdt. 27-26; 27.337 (a)(b)(1)(2) Amdt. 27-26; 27.561 (a)(b)(3)(i)(ii)(iii)(iv)(v)(c)(1)(2)(3)(4)(5) Amdt. 27-30; 27.601 (a)(b) Amdt. 27-0; 27.603 (a)(b)(c) Amdt. 27-16; 27.605 (a) Amdt. 27-16; 27.607 (a)(b) Amdt. 27-4; 27.609 (a)(1)(2)(3)(b) Amdt. 27-0; 27.613 (a)(b)(1)(2)(d)(1) Amdt. 27-26; 27.1301 (a)(b)(c)(d) Amdt. 27-0; 27.1307 (d)(e) Amdt. 27-0; 27.1309 (b) Amdt. 27-21; 27.1351 (a)(1)(2)(b)(1)(i) Amdt. 27-13; 27.1357 (a)(1)(2)(c)(1)(2) Amdt. 27-13; 27.1365 (a)(b)(c) Amdt. 27-0; 27.1529 Amdt. 27-18. ---------------------------------------------------------------------------END-------------------------------------------------------------------------- ## Every issue (4) - December 14, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/26/70/26708955ba36e2b2a3072a4b791be04ec8a936066380cce4c8c43454c60ef1a4) - March 24, 2020: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/38/60/386051200d8f360e8da24d3144988b5a6be9e61bbe33025878a00527e383d3cb) - October 26, 2010: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/f0/ca/f0ca573ba49533c2e14efe36c9b5716ee28a8e24a1befe08947cc38274a1d3b1) - May 10, 2006: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/90/3c/903cb661b0a05af37e5bcb83ad0595bbf8f0b39589a977b41b50f139f840c080) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.