STC SR00798DE

Thrita Shades of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SR00798DE This certificate issued to: Erickson Incorporated 5550 S.W. Macadam Ave, Ste. 200 Portland, OR 97239 Part 29* of the Federal Aviation Poegulations.

See Page 3 Original Product Type Certificate Number: H6SW Make: Bell Model: 214B, 214B-1 Description of Type Design Change:

Installation of Torque Meter Junction Box Relocation in accordance with Erickson Incorporated Document EAC 2365, Master Drawing List, Torque Meter Junction Box Relocation, Revision IR dated 6/8/2015, FAA approved December 7, 2015 or later FAA approved Revision. Instructions for Continued Airworthiness, Erickson Incorporated Document EAC 2364, Revision IR dated 9/4/2015, FAA accepted 11/3/2015, or later FAA accepted revision is required for this installation.

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 a product, the holder must give the other person written evidence of that permission.

Limitations and Conditions: continued on page 3 of 3)

suspended, revoked, or a ternination date is otheruise established by the Administrator of the Federal Aviation Administratica Date of Application: 6/3/2015 Date Reissued:

Date of Issuance: 12/9/2015 Date Amended:

FEDERA AVIATION By Direction of the Administrator Kreg R. Voorhies (Signature) TOMINIST RATION ODA No. ODA(AIR)-833887-NM ODA Lead administrator, Cert Works, LLC. ODA (Title)

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and ZIP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and ZIP code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SR00798DE Limitations and Conditions: Continued:

3. A copy of this certificate must be maintained as part of the permanent records for the modified rotorcraft.

Certification Basis:

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 the Bell 214B/214B-1 Torque Meter Junction Box Relocation is as follows:

a. The type certification basis for Bell 214B/214B-1 series rotorcraft is shown on TCDS H6SW 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, 6/3/2015, is also shown on TCDS H6SW Regulations at amendment level shown on TCDS H6SW for Bell 214B/214B-1

29.301 (a), 29.303, 29.305, 29.307 (a), 29.337, 29.341, 29.601(a), 29.603, 29.605, 29.607, 29.609,

29.611, 29.613, 29.625(a), 29.901(a), 29.1163(a), 29.1181, 29.1191(c),(d), 29.1301,

29.1305(a) (15), 29.1309(a), 29.1353(a), 29.1359(a), 29.1529.

Regulations at an intermediate amendment level None Note:

It has been determined that this modification is a No Acoustical Change per 14 CFR 21.93(b).

- END Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both