STC SR00805SE

Number SR00805SE

This certificate, issued to Cert Works 5150 Front Range Parkway Watkins, CO 80137

Part 21.29 of the Federal Aviation Regulations.

Original ProductType Certificate Number: H9EU Make: Airbus Helicopters Model: AS350BA

Description of the Type Design Change: Modifications completed prior to January 31, 2007: Installation of Honeywell engine Model LTS 101-600A-3A, in accordance with Soloy Document EHDA-199-B, Revision 1, dated February 16, 2005, and maintained in accordance with Maintenance Manual Supplement EHDA -197-B Revision 2, dated February 18, 2005, or later FAA approved revision.

Modifications completed after January 31, 2007: Installation of Honeywell LTS101 -600A-3A engine, in accordance with Soloy Master Drawing List 920-100, Revision N/C, dated February 28, 2007, or later FAA approved revisions, and maintained in accordance with Maintenance Manual Supplement S2042H, Revision 0, dated December 4, 2006, or later FAA approved revisions.

Limitations and Conditions: Approval of this change in type design applies to the above model rotorcraft only.

This approval should not be extended to other rotorcraft of these models on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previous modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that rotorcraft. Compatibility of this modification with previously approved modifi cations must be determined by the installer.

If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

Date of application: February 11, 2000 Date reissued 12/22/04; 2/28/07; 8/26/20 Date of issuance: June 5, 2000 Date amended 12/22/04; 6/15/05; 2/28/07; 4/5/11

FAA FORM 8110-2 (5/14) PAGE 1 OF 5 PAGES By direction of the Administrator

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U.S. GPO: 1987-763-289

Number SR00805DE

Cert Works Date of issuance: June 5, 2000 Reissued: 12/22/04; 2/28/07; 8/26/20 Amended: 12/22/04; 6/15/05; 2/28/07; 4/5/11 Limitations and Conditions: (cont’d)

A copy of this Certificate and the FAA-approved Rotorcraft Flight Manual Supplement listed in Soloy Master Drawing List 920-100 must be maintained as part of the permanent records for the modified rotorcraft.

Certain limitations and conditions shown on the Type Certificate Data Sheet No. H9EU for Model AS 350 BA remain applicable. The following list contains those limitations and conditions which are modified, and certain unmodified ones which are listed for clarity.

Model: AS350BA Engine: Honeywell LTS101-600A-3A Engine Limits: Power Ratings (Sea Level, ISA)

Takeoff (five minutes) 650 s.h.p.

Max. Continuous 625 s.h.p.

Gas Generator Speed, NG (100% = 47,870 RPM) Transient 50,787 RPM (106.2%) Takeoff Rating 49,830 RPM (104.1%) Max. Continuous Rating and Below 49,255 RPM (102.9%) Output Shaft Speed, Npt (100% = 5966 RPM = 37,000 Power Turbine RPM) Transient 7200 RPM (120.6%) Takeoff Rating 6780 RPM (113.6%) Max. Continuous Rating and Below 6780 RPM (113.6%)

Note: The takeoff output shaft speed must not be exceeded for more than 30 seconds.

Measured Gas Temperature Limit, MGT: ˚F (˚C)

Starting 1650 (899) Transient 1557 (847) Takeoff Rating 1447 (786) Max. Continuous Rating and Below 1409 (765)

Note: Transient MGT must not exceed the takeoff MGT for more than 22 seconds.

FAA FORM 8110-2 (5/14) PAGE 3 OF 5 PAGES

Number SR00805DE

Cert Works Date of issuance: June 5, 2000 Reissued: 12/22/04; 2/28/07; 8/26/20 Amended: 12/22/04; 6/15/05; 2/28/07; 4/5/11 Limitations and Conditions: (cont’d)

Transmission Limits: Airspeed Lower than 40 Kt Maximum Torque 107% (421 Kw) Airspeed Equal to or Higher Than 40 Kt Maximum Torque 101% (396 Kw) Note: Power corresponding to 390 rotor RPM Helicopter Limits: Same as Transmission Limits Except that the Maximum Continuous T4 limit is 735˚C.

Fuel: Refer to Eurocopter Rotorcraft Flight Manual approved fuels and additives and Soloy Rotorcraft Flight Manual Supplement for approved emergency fuels.

Engine Lubricating Oil: MIL-L-7808G or MIL-L-23699 and subsequent revisions (Mixing of these oils is prohibited).

Certification Basis: Title 14 Code of Federal Regulations (CFR) sections (§§) 21.29 and 14 CFR Part 27 dated February 1, 1965, with Amendments 1 Through 10, plus FAA Special Conditions No. 27-29-EU-23, dated August 13, 1977.

Eqivalent safety, in lieu of direct compliance, found with respect to 14 CFR §§

27.1189, Shutoff Means.

14 CFR part 36 dated July 2, 2004, with Amendments 1 through 25.

Equipment: The basic required equipment as prescribe in the applicable airworthiness regulations (See Certification Basis) must be installed in the helicopter for certification. The equipment must be include the DGAC Approved Eurocopter Rotorcraft Flight Manual AS-350BA, dated December 14, 1994, and the FAA Approved Soloy Rotorcraft Flight Manual Supplement, Revision 3, dated March 27, 2006, or later FAA approved revisions or the FAA Approved Soloy Rotorcraft Flight Manual Supplement listed in Soloy Master Drawing List 920-100, Revision N/C, dated February 28, 2007 or later FAA approved revisions.

Note 1: The rotorcraft must be maintained in accordance with the AS-350BA Master Servicing Recommendations (MSR), Soloy AS350 series Maintenance and Overhaul Manual Supplement, S2042H, dated December 4, 2006 or later revisions and Airworthiness Limitations. Life limited components and the associated retirement times are presented in the manuals and components must be replaced in accordance therewith.

(See Continuation Sheet Page 5 of 5 Pages) FAA FORM 8110-2 (5/14) PAGE 4 OF 5 PAGES

Number SR00805DE

Cert Works Date of issuance: June 5, 2000 Reissued: 12/22/04; 2/28/07; 8/26/20 Amended: 12/22/04; 6/15/05; 2/28/07; 4/5/11 Limitations and Conditions: (cont’d)

Note 2: If optional AFS 112000-101 Inlet Air Filter Kit is installed, Rotorcraft Flight Manual Supplement S2043H, Revision 0, dated February 28, 2007, or later FAA approved revision must be included with basic required equipment for the helicopter.

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FAA FORM 8110-2 (5/14) PAGE 5 OF 5 PAGES