STC SA755EA

the Civil Air Regulations.

SA755EA PC6-AU23 Spares, LLC 37 Styles Way Lagrangeville, NY 12540 Part 3

7A15 Pilatus

PC-6/B-H2, PC-6/B1-H2, PC-6/C-H2

1. Operation under the provisions of this Supplemental Type Certificate may be conducted only if the fuel valve placard denotes that the usable fuel is reduced from 128 US-GAL. to 123 US-GAL for 130 gallon capacity fuel systems or the usable fuel is reduced from 170 US-GAL to 164 US-GAL for 170 gallon capacity fuel system.

(Limitations and Conditions continued on page 3 of 3) 02/05/1969 10/18/1988 06/27/2003 05/06/1969 11/09/1973 ✔ Christina M. Underwood Manager, East Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 3 Installation of polyurethane Reticulated Foam in the aircraft's integral and collector fuel tanks in addition to check valves in the fuel lines between the integral tanks and the collector and sediment tanks in accordance with drawings noted in either Fairchild Hiller addition to check valves in the fuel lines between the integral tanks and the collector and sediment tanks in accordance with drawings noted in either Fairchild Hiller November 7. 1973, for 170 gallon capacity fuel systems.

06/30/1994

SA755EA 10/25/2023 3

SA755EA 10/25/2023 Date Reissued Continued: 10/25/2023

Limitations and Conditions continued

2. The following Fairchild flight Manual Supplements to the Pilatus Turboporter approved Flight Manual are required:

3. 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.

4. Compatibility of this design change with previously approved modifications must be determined by the installer.

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