# STC SR03280NY - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Leonardo Helicopters US Corporation, United States - Description: Installation of a Garmin G1000H PFD/MFD Display System - Applied: September 24, 2012 - Status date: June 16, 2026 - Product: Aircraft, Rotorcraft - Certification basis: Part 27 - Data sheets: [TCDS H7EU](https://openairdocs.org/tcds/H7EU) - Certificate PDF: https://openairdocs.org/files/sha256/b6/69/b669766e554ec5f5217ee21092a8fcc6fdfc6d6ab896a099d1303e41fd6bedbf - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121419545220260717132248.0001 - DRS record last changed: July 17, 2026 - Page: https://openairdocs.org/stc/SR03280NY ## ADs that name it (1) - [AD 2025-09-06](https://openairdocs.org/ad/2025-09-06): Battery/charger system · Leonardo A119 and AW119 MKII. Effective Jun 16, 2025. Cited in the text ## Approved models (1) - Leonardo S.p.A. AW119 MKII ([TCDS H7EU](https://openairdocs.org/tcds/H7EU)) ## 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. SR03280NY Leonardo Helicopters US Corporation 3050 Red Lion Road Philadelphia, PA 19114 Part 27 Title 14 Code of Federal Regulations H7EU Leonardo S.p.A AW119 MKII Configuration A: 1. Garmin G1000H Loader Card P/N 010-12065-03 is required with this installation. (Limitations and Conditions continued on page (5 of 7) 09/24/2012 06/16/2026 05/23/2013 05/30/2013 08/28/2014 06/08/2015 ✔ Michael Linegang Manager, East Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 7 Configuration A (Core G1000H): 1. Installation of a Garmin G1000H PFD/MFD Display System P/N AWPC-ENG-12-052-A in accordance with AgustaWestland Philadelphia Corporation Installation Master Data List, AWPC-ENG-12-052, Revision AC, dated July 19, 2024 or later FAA approved revision. (Description of Type Design Changed continued on page 3 of 7) SR03280NY 06/16/2026 7 SR03280NY 06/16/2026 Date Amended continued: June 20, 2016, March 27, 2017, October 07, 2024 Configuration A (Core G1000H): 2. Aircraft is to be operated in accordance with the AgustaWestland Philadelphia Corporation Rotorcraft Flight Manual Supplement No. AWPC-ENG-12-065 Revision 6, FAA approved September 26, 2024, or later approved revision. Configuration B (Core G1000H with EMS): 1. Installation of an EMS Medical Kit P/N AWPC-ENG-12-052-B in accordance with Agusta Westland Philadelphia Corporation Installation Master Data List, AWPC-ENG-12-052, Revision AC, dated July 19, 2024 or later FAA approved revision. 2. Aircraft is to be operated in accordance with the AgustaWestland Philadelphia Corporation Rotorcraft Flight Manual Supplement No. AWPC-ENG-12-144, Revision -, FAA approved May 23, 2013, or later approved revision. Configuration C (Core G1000H with NVIS): 1. Installation of an NVIS/NVG Compatible Lighting System, P/N AWPC-12-052-C in accordance with AgustaWestland Philadelphia Corporation Installation Master Data List, AWPC-ENG-12-052, Revision AC, dated July 19, 2024 or later FAA approved revision. 2. Aircraft is to be operated in accordance with the AgustaWestland Philadelphia Corporation Rotorcraft Flight Manual Supplement No. AWPC-ENG-12-145, Revision B, FAA approved March 22, 2017, or later approved revision. Configuration E (Core G1000H with Utility): 1. Installation of a Utility Cabin Interior Configuration, P/N AWPC-12-052-E in accordance with AgustaWestland Philadelphia Corporation Installation Master Data List, AWPC-ENG-12-052, Revision AC, dated July 19, 2024 , or later FAA approved revision. Configuration F (Core G1000H with -35 Deg C Operation): 1. Installation of a -35 degree Celsius Configuration kit, P/N AWPC-ENG-12-052-F in accordance with AgustaWestland Philadelphia Corporation Installation Master Data List, AWPC-ENG-12-052, Revision AC, dated July 19, 2024 , or later FAA approved revision. (Continued to Page 4 of 6) 3 7 Add Page SR03280NY 06/16/2026 2. Aircraft is to be operated in accordance with the AgustaWestland Philadelphia Corporation Rotorcraft Flight Manual Supplement No. AWPC-ENG-15-033, Revision -, approved May 27, 2015, or later approved revision. Configuration G1 (EMS2 with Minimum Cabin Liners with TC G1000H): 1. Installation of an Emergency Medical Services (EMS) cabin interior P/N AWPC-ENG-12-052-G1 with a TC Garmin G1000H PFD/MFD Display System in accordance with AgustaWestland Philadelphia Corporation Installation Master Data List AWPC-ENG-12-052, Revision AC, dated July 19, 2024 , or later FAA approved revision. 2. Aircraft is to be operated in accordance with the AgustaWestland Philadelphia Corporation Rotorcraft Flight Manual Supplement No. AWPC-ENG-16-019 Revision A, FAA approved March 22, 2017, or later FAA approved revision. Configuration G2 (EMS2 with Standard Cabin Liners with TC G1000H): 1. Installation of an Emergency Medical Services (EMS) cabin interior P/N AWPC-ENG-12-052-G2 with a TC Garmin G1000H PFD/MFD Display System in accordance with AgustaWestland Philadelphia Corporation Installation Master Data List, AWPC-ENG-12-052, Revision AC, dated July 19, 2024 , or later FAA approved revision. 2. Aircraft is to be operated in accordance with the AgustaWestland Philadelphia Corporation Rotorcraft Flight Manual Supplement No. AWPC-ENG-16-019 Revision A, FAA approved March 22, 2017, or later FAA approved revision. Configuration H1 (EMS3 with Minimum Cabin Liners with TC G1000H): 1. Installation of an Emergency Medical Services (EMS) cabin interior P/N AWPC-ENG-12-052-H1 with a TC Garmin G1000H PFD/MFD Display System in accordance with AgustaWestland Philadelphia Corporation Installation Master Data List, AWPC-ENG-12-052, Revision AC, dated July 19, 2024, or later FAA approved revision. 2. Aircraft is to be operated in accordance with the AgustaWestland Philadelphia Corporation Rotorcraft Flight Manual Supplement No. AWPC-ENG-16-076 Revision -, FAA approved March 22, 2017, or later FAA approved revision. Configuration H2 (EMS3 with Standard Cabin Liners with TC G1000H): 1. Installation of an Emergency Medical Services (EMS) cabin interior P/N AWPC-ENG-12-052-H2 with a TC Garmin G1000H PFD/MFD Display System in accordance with AgustaWestland Philadelphia Corporation Installation Master Data List, AWPC-ENG-12-052, Revision AC, dated July 19, 2024, or later FAA approved revision. (Continued to Page 5 of 6) 4 7 Add Page SR03280NY 06/16/2026 2. Aircraft is to be operated in accordance with the AgustaWestland Philadelphia Corporation Rotorcraft Flight Manual Supplement No. AWPC-ENG-16-076 Revision -, FAA approved March 22, 2017, or later FAA approved revision. Configuration J (NVIS with TC G1000H): 1. Installation of a NVIS/NVG Compatible Lighting System P/N AWPC-ENG-12-052-J in accordance with AgustaWestland Philadelphia Corporation Installation Master Data List, AWPC-ENG-12-052, Revision AC, dated July 19, 2024 , or later FAA approved revision.. 2. Aircraft is to be operated in accordance with the AgustaWestland Philadelphia Corporation Rotorcraft Flight Manual Supplement No. AWPC-ENG-12-145, Revision B, FAA approved March 22, 2017, or later approved revision. Configuration K (-35 Deg C Operation with TC G1000H): 1. Installation of a -35 degree Celsius Configuration kit P/N AWPC-ENG-12-052-K in accordance with AgustaWestland Philadelphia Corporation Installation Master Data List AWPC-ENG-12-052, Revision AC, dated July 19, 2024 or later FAA approved revision. 2. Aircraft is to be operated in accordance with the AgustaWestland Philadelphia Corporation Rotorcraft Flight Manual Supplement No. AWPC-ENG-17-007, Revision -, approved March 22, 2017, or later approved revision. Configurations G1, G1, H1, H2, J and K 1. Aircraft equipped with OPT 14.3 (Pulse Light System) are to be operated in accordance with the AgustaWestland Philadelphia Corporation Rotorcraft Flight Manual Supplement No. AWPC-ENG-17-008 Revision -, FAA approved March 22, 2017, or later approved revision. Configuration X 1. Installation of Battery Discharge Detector (P/N 109-0900-19-101) on AW119MKII rotorcraft with Garmin G1000H Integrated Flight Deck in accordance with Installation Master Data List AWPC-ENG-12-052, Revision AC, dated July 19, 2024 or later FAA approved revision. All Configurations: 1. Maintenance is to be preformed in accordance with the AgustaWestland Philadelphia Corporation Instructions for Continued Airworthiness, AWPC-ENG-12-066, Revision T, dated May 15, 2024, or later FAA accepted revision. Configurations A, B, C, E and F: (Continued on page 6 of 6) 5 7 Add Page SR03280NY 06/16/2026 Limitations and Conditions continued: 1. This modification is applicable to the AW119MKII serial numbers 14900 and below. 2. The installation of configurations B, C, E or F requires the installation of configuration A as a prerequisite. 3. Configurations A, B, C, and F can be combined. 4. Configurations A, E, F can be combined. 5. Configuration E cannot be combined with either configuration B or C. Configurations G1, G2, H1, H2, J and K: 1. This modification is applicable to the AW119MKII serial numbers 14901 and above. 2. Configurations G1, G2, and K can be combined. 3. Configurations H1, H2, J, and K can be combined. 4. Configuration J cannot be combined with either configuration G1 or G2. Configuration X: 1. This modification is applicable to AW119MKII serial numbers up to and including 14900. Configuration C: 1. The aircraft must be operated in accordance with the "Limitations" section of AgustaWestland Philadelphia Corporation Flight Manual Supplement, AWPC-ENG-12-145, Revision B, FAA approved March 22, 2017, or later approved revision. 2. Aircraft cockpit and external lighting must be in accordance with AgustaWestland Philadelphia Corporation Certification Equipment List, Report No. AWPC-ENG-12-054, Revision F, dated January 6, 2017, or later FAA approved revision. Configuration J: 1. The aircraft must be operated in accordance with the "Limitations" section of AgustaWestland Philadelphia Corporation Flight Manual Supplement, AWPC-ENG-12-145, Revision B, FAA approved March 22, 2017, or later approved revision. 2. Aircraft cockpit and external lighting must be in accordance with AgustaWestland Philadelphia Corporation Certification Equipment List, Report No. AWPC-ENG-17-001, Revision A, dated February 1, 2017, or later FAA approved revision. All Configurations: 1. The installer must determine whether this design change is compatible with previously approved modifications. 2. If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission. SR03280NY 06/16/2026 Certification Basis: Based on 14 CFR 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the FAA certification basis for the Leonardo S.p.A Model AW119 MKII series aircraft modification is as follows: (a) The type certification basis for the series Leonardo S.p.A AW119 MKII aircraft is shown on TCDS H7EU for parts not changed or not affected by the change. (b) The certification basis for parts changed or affected by the change since the reference date of application September 24, 2012, is based upon part 27 as amended by Amendment 27-26. Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be: 27.301 Amdt. [27-0], 27.303 Amdt. [27-0], 27.305(a) Amdt. [27-0], 27.307(a) Amdt. [27-26], 27.321 (a) Amdt. [27-11], 27.337 Amdt. [27-26], 27.601(a) Amdt. [27-0], 27.603 Amdt. [27-16], 27.605(a) Amdt. [27-16], 27.607 Amdt. [27-4], 27.609(a) Amdt. [27-0], 27.613 Amdt. [27-26], 27.1301(a)(b)(c)(d) Amdt. [27-0], 27.1307(e) Amdt. [27-0], 27.1309(a) Amdt. [27-21], 27.1322(a)(b)(c) Amdt. [27-11], 27.1351(a) Amdt. [27-13], 27.1365(a)(b)(c) Amdt. [27-0], 27.1501(b) Amdt. [27-14], 27.1529 Amdt. [27-18], 27.1581 (a)(b)(d) Amdt. [27-14], 27.1583(b) Amdt. [27-16], 27.1585(a) Amdt. [27-21]. ------------------------------------------------------END-------------------------------------------------- 7 7 Add Page ## Every issue (5) - June 16, 2026: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/b6/69/b669766e554ec5f5217ee21092a8fcc6fdfc6d6ab896a099d1303e41fd6bedbf) - October 7, 2024: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/c2/42/c2425193a887922bb61abe2d501074ae33274500877c794a29a1a47d10d279ad) - March 27, 2017: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/ad/57/ad574bd7c3df93090fa1b50d492c178c88c5e3bb6481cabdfc17be4756c9063a) - August 28, 2014: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/e2/b4/e2b4af1f3b3526586fb84e9b3b19c2f1127a0e0d165c4ea940166fd51e708d0d) - May 30, 2013: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/86/2c/862c9732c074e138935bfe68dd62c8e7cb7a4bea5fed49639ddfc39e00553e94) --- 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.