STC SA04589CH

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number 

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HARTZELL PROPELLER LLC

ONE PROPELLER PLACE PIQUA, OHIO 45356-2634 Part 23 the Federal Aviation Regulations Daher Aircraft Design, LLC Kodiak 100 A00007SE

- Installation of Hartzell Propeller model 5D3-NK366A1(Y)( )/91D17(B) in accordance with Hartzell STC Installation Instructions INST-030822 (Revision B) dated 05/12/2025 or later FAA-approved revisions.

- Airplane Flight Manual Supplement AFMS-030822 (Initial Revision) dated 02/22/2023 or later FAA-approved revision is required.

- Instructions for Continued Airworthiness ICA-030822 (Initial Revision) dated 03/15/2023 or later FAA-accepted revision are applicable.

- Propeller RPM tachometer update using Hartzell STC Installation Instructions INST-030822 (Revision B) dated 05/12/2025 or later FAA-approved revisions is required.

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 shall give the other person written evidence of that permission.

(See Continuation Sheet 3 of 3 pages) 10/12/22 11/27/24 3/24/23 11/27/24 5/14/25 Bo R. Landess STC ODA administrator Hartzell Propeller ODA-100082-CE 3

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3. This STC is applicable only to the Models listed with the following serial numbers:

- 100-0001 and greater

4. Revised Type Certificate Data Sheet information:

Propeller and Propeller Limits:

Propeller Manufacturer: Hartzell Propeller LLC Number of Propellers: One (1) Propeller TC Number: P00015CH Propeller Model Designation: 5D3-NK366A1(Y)( )/91D17(B) Diameter Limits: 96.0" minimum, 96.0" maximum; no further tolerance permitted.

High Pitch Angle: 88.3° ± 0.5° Low Pitch Angle: 18.3° ± 0.1° Reverse Pitch Angle: -8.0° ± 0.5° Static RPM Limits: Stabilized ground operation is prohibited between 450 and 1050 RPM. The propeller may be operated when feathered at or below 450 RPM.

5. This STC is limited to Kodiak 100 aircraft that have wing and flap vortex generators. The wing and flap vortex generators can be installed via Field Service Instruction FSI-007 or Service Notice SN-025 for Kodiak 100 airplane serial numbers 100-0001 to 100-0034. The wing and flap vortex generators are included as part of type design standard equipment on Kodiak 100 airplane serial numbers 100-0035 and greater.

6. The original certification basis (14 CFR Part 23 Amendment 23-55) was used for this STC with the following exceptions:

14 CFR 23.907 Amendment 23-59 14 CFR Part 36 Amendment 36-31 -------------------------------------------------------- END ---------------------------------------------------- 33 05/14/25