STC SR03948NY

SR03948NY Helifab East, LLC 602 Sevier St. Unit 300 Johnson City, TN 37604-7561 Part 6&27 CAR & Federal Aviation Regs H2SW Bell Textron Canada Limited 206, 206A, 206A-1(OH-58A), 206B, 206B-1, 206L, 206L-1, 206L-3, 206L-4, 407 Installation of Frameless Crew Seat Cushion in accordance with FAA approved Helifab East, LLC Master Document List MDL-RH407-1014, Revision F, dated October 27, 2022; or later FAA approved revision.

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 upon the airworthiness of the aircraft. (Limitations and Conditions continued on page 3 of 4) June 22, 2017 May 4, 2021 August 30, 2017 January 3, 2023 Robert P. Capezzuto Acting Manager, Atlanta ACO Branch 4

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Limitations and Conditions: (continued)

The installer must determine whether this design change is compatible with previously approved modifications.

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.

A copy of this STC must be included in the permanent record of the modified aircraft.

The Helifab East, LLC Instructions for Continued Airworthiness, ICA-RH407-1014, Revision 5, dated October 27, 2022, or later FAA accepted revision, must be made available to the operator at the time of installation.

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48A, the certification basis for the Bell Textron Canada Limited model rotorcraft listed on page 1 of this certificate is as follows:

a. The type certification basis for parts not changed or not affected by the change, for the Bell Textron Canada Limited models shown on page 1, is shown on TCDS H2SW.

b. The certification basis for parts changed or affected by the change since the reference date of application, June 22, 2017, is based upon part 27 as amended by Amendment 27-48. Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for non-significant changes in FAA Order 8110.48A, the certification basis for this modification was determined to be: (Certification Basis Continued on Page 4 of 4) 3 4

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(Certification Basis Continued)

Regulations at the latest amendment 27-1 through 27-50:

None

Regulations at an intermediate amendment:

None

Regulations at the amendment level in TCDS H2SW for the Model 407*:

27.1, 27.21(a), 27.25(a)(b), 27.27, 27.29(a), 27.301(a), 27.397(a), 27.561(a)(b)(c),

27.601(a), 27.603, 27.605, 27.607, 27.609(a), 27.611, 27.785(a)(b)(c)(f)(g)(h),

27.853(a)(b), 27.1301, 27.1501(a), 27.1529, 27.1581(a).

* For all models, other than the model 407 listed on page 1 of this certificate, some of these regulations constitute a later amendment level than those listed on the applicable TCDS (H2SW).

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