STC SA2628NM

FAA Form 8110-2 (7/19) Page 1 of 3

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA2628NM

Part 23* of the Federal Aviation Regulations.

*Certification Basis is set forth in Type Certificate Data Sheet A27CE*

Original Product – Type Certificate Number: A27CE Make:

Optional takeoff gross weight increase for airplanes conforming to Branson Aircraft Corporation Conformity Checklist 91891 or New Flight Corporation General Arrangement and Conformity Checklist 91891 and Branson Aircraft Corporation or New Flight Corporation FAA sealed Drawing List 91890, Rev N/C, dated February 25, 1987, or later FAA Approved revision.

1. FAA Approved Airplane Flight Manual Supplement dated December 04, 1984, or later FAA approved revision is required for each airplane.

2. The approval of this change in type design applies basically to the above model aircraft only. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane. A copy of this certificate and Addendum No. SA2628NM shall be maintained as part of the permanent records for the modified aircraft.

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. There is a mandatory prerequisite for this STC. Prior to its incorporation, the aircraft must have the optional zero fuel we ight of 9,500 pounds in accordance with Cessna ERC04139 or Cessna Service Bulletin SB-34-15 installed.

(See Continuation Page 3)

Date of Application: August 20, 1984 Date Reissued: February 25, 1985; May 03, 1994; March 06, 2020

Date of Issuance: January 08, 1985 Date Amended: 02/26/1987; 08/10/1988; 07/19/1994; 08/09/2013

Signature Title Todd Dixon, Manager, Denver ACO Branch Compliance and Airworthiness Division

Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design da ta nor to alter an aircraft, aircraft engine, or propeller.

Cessna 501 (Serial numbers 0001 and on) New Flight Corporation 334 Estancia Ln Boerne, TX 78006

FAA Form 8110-2 (7/19) Page 2 of 3 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate

To (Name and address of transferee)

From (Name and address of grantor)

The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the propert y of the STC holder.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA2628NM

SUPPLEMENTAL TYPE CERTIFICATE ADDENDUM NO. SA2628NM

The limitations listed in Type Certificate Data Sheet No. A27CE are applicable except as follows:

AIRSPEED LIMITS (CAS)

VMo (Maximum Operating) (Sea Level to 30,300 feet) 260 KCAS

MMo (Above 30,300 feet) .698 MACH

VA (Maneuvering Speed) 186 KCAS (S.L.)

VFE (Flaps Extended) 40° (landing) 174 KCAS 15° (Takeoff and Approach) 200 KCAS

VLo (Landing Gear Operation ) 174 KCAS

Autopilot Operation 260 KCAS

GROSS WEIGHT LIMIT (Lbs.)

Max. Taxi (MTW) 12,650 lbs.

Max. Takeoff (MGW) 12,500 lbs.

Max. Zero Fuel (MZFW) (Takeoff weight 11,851 to 12,500 lbs) 9,100 lbs.

(Takeoff weight 11,850 or below) 9,500 lbs.

Max. Landing (MLW) 11,350 lbs.

Ref. FAA Approved Flight Manual Supplement PKCIT016 or FMS-963 for additional limitations.

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Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engi ne, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is t he property of the STC holder.

FAA Form 8110-2 (7/19) Page 3 of 3