STC SA02476CH-D

United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Number: SA02476CH-D This certificate issued to Hartzell Propeller Inc.

One Propeller Place Piqua, OH 45356-2634 Part 23 of the Federal AviationRegulations.

(See Type Certificate Data Sheet A47CE for the complete certification basis).

Original Product -Type Certificate Number: A47CE Make: Diamond Aircraft Industries GmbH Model: DA 40 Description of Type Design Change:

Installation of a Hartzell HC-C2YR-1BFP/F7497 propeller or Hartzell HC-C2YR-IN/N7605 propeller in accordance with Installation Instructions INST_102706 dated October 27, 2006, or later FAA Approved revisions.

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

2. FAA Approved Airplane Flight Manual Supplement, AFMS_ 102706, dated October 27, 2006, or later FAA approved revision is required.

(See continuation sheet 3 of 3) Meyer TOMINSTRATOT DAS administrator Hartzell DAS-100082-CE (rule) or imprisoment not exceeding 3 years, or boch PAA Рови 8110-2 (10-68) PACE 1 Of 3 PAGES This certificate may be transferred in accordance with PAR 21.41

United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) STC SA02476CH-D Date of Issuance: October 31, 2007 Limitations and Conditions: continued...

3. The following spinner is approved: Hartzell A-2295(P).

4. The following goverors are approved: Hartzell model S-1-6 and Woodward/Ontic goveror model C210776 (C210776 is already approved on the aircraft TC A47CE).

5. 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.

6. This STC is compatible with FAA STC SA03281AT (Power Flow exhaust system and early cowling).

7. This STC is compatible with STC SA02292NY (Power Flow exhaust system and later cowling).

8. This STC is compatible with FAA STC SA01254WI (Garmin G1000 integrated avionics system).

9. This STC is compatible with the original MAM-066 WCC Exhaust Manifold (exhaust system) originally typecertificated by Diamond.

10. This STC is compatible with a 2646 pound (1200 kg) maximum takeoff weight.

11. ICA_ 102706, dated October 27, 2006 or later FAA accepted revision is applicable to this STC.

...END...

or imprisonment not exceeding 3 years. or both.

PAA PORN 8110-2-1 (10-69) PAGE 3 of 3 This certificate may be transferred in accordance with FAR 2) 47.