STC SA02092SE

(See TCDS No. 3A13 for complete certification basis) Original Product—Type Certificate Number :

Installation of Continental/NorthPoint XP470 engine and a McCauley D2A34C58/90AT-8, or 2A34C66/90AT-8, or D3A32C90/82NC-2, D3A34C401/90DFA-8, or D2A37C230/90REB-8 propeller in accordance with NorthPoint Aviation Number NPA-10182, Revision A, dated June 15, 2020 or later FAA approved revision.

Approval of this change in design applied to the above model aircraft only. A Continental engine modified under STC SE4985NM or SE4988NM to a NorthPoint XP470 engine is required. This approval should not be extended to other aircraft of this model on which other previously approved modifications have been incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design will introduce no adverse effect upon the airworthiness of that aircraft. (See Continuation Sheet on Page 3) A c opy of this certificate and its continuation sheet must be maintained as part of the permanent records for the modified aircraft. The modified aircraft must be maintained with Instructions for Continued Airworthiness Report NAS2010-3, Revision A, dated June 15, 2020 or later FAA accepted revision.

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.

NorthPoint Aviation 16384 Airport Road, Suite #8 Brainerd, MN 56401 3A13 Make : Cessna Model: 182, A, B, C, D, E, F, and G Date reissued: March 21, 2019; August 24, 2020 Date amended: February 9, 1996, December 2, 2005, June 15, 2020 By direction of the Administrator __

(Signature) Roy E. Boffo III Manager, Propulsion and Project Management Section Chicago Aircraft Certification Office Branch Compliance and Airworthiness Division, FAA

(Title)

Date of application: May 12, 1991 Date of issuance: January 15, 1992

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):

FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES Number SA02092SE

Date of issuance: January 15, 1992 Date Amended: February 9, 1996; December 2, 2005; June 15, 2020 Date Reissued: March 21, 2019; August 24, 2020

Engine: NorthPoint XP470 per STC SE4985NM or SE4988NM

Fuel: 100/100-L minimum grade aviation gasoline

Engine Limits : Takeoff (5 min.); 2700 RPM for 2 or 3 blade propeller Maximum Continuous Power:

With 2 blade propeller – 2600 RPM With 3 blade propeller – 2700 RPM

Propeller and Propeller Limits

1. McCauley D2A34C58/90AT- Diameter Limits: Max-82”; Min-80.5” Pitch Stop Settings @ 36” Station High – 25.8 deg; Low – 9.5 deg

2. McCauley 2A34C66/90AT-8 Diameter Limits: Max-82”; Min-80.5” Pitch Stop Settings @ 36” Station High – 25.8 deg; Low – 9.5 deg

3. McCauley D3A32C90/82NC-2 Diameter Limits: Max-80”; Min-74” Pitch Stop Settings @ 30” Station High – 28 deg; Low – 10.4 deg

4. McCauley D3A34C401/90DFA-8 Diameter Limits: Max-82”; Min-74” Pitch Stop Settings @ 30” Station High – 28.5; Low – 10.4 deg

5. McCauley D2A37C230/90REB-8 Diameter Limits: Max-82”; Min-80” Pitch Stop Settings @ 30” Station High – 28.3 deg; Low – 12.0 deg

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