STC SA1098WE

SA1098WE TALCO Aviation 3015 E. New York St, STE A2-270 Aurora, IL 60504 Part 3 the Civil Air Regulations 3A21 Cessna 210, 210A, 210B, 210C, 210-5(205), & 210-5A (205A) Installation of Roto-Master (Rajay) turbocharged Continental IO-470-E or IO-470-S engine in accordance with FAA sealed Roto-Master (Rajay) Drawing List No. RJ1600, or later FAA approved revisions.

(See continuation sheet 3 of 5) February 25, 1965 January 14, 1969; February 10, 1982; October 30, 1987; September 22, 1995; November 14, 2003;

July 3, 2006; March 16, 2007; March 5, 2018; February 2, 2021; August 31, 2023 November 5, 1965 February 3, 1970; August 11, 1977; March 21, 1985 for Paul (Vu) Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 5

SA1098WE 5

SA1098WE Date of Issuance: November 5, 1965 Date Amended: March 21, 1985 Date of Reissuance: August 31, 2023

See STC SA1098WE Addendum which is a portion of this Supplemental Type Certificate.

Supplemental Type Certificate Addendum No. SA1098WE

The conditions and limitations of Type Certificate Data Sheet No. 3A21 apply except where superseded by the following:

This data sheet, which is a part of Supplemental Type Certificate No. SA1098WE, prescribes conditions and limitations under which the product for which the STC was issued meets the airworthiness requirements of the Federal Aviation Regulations.

Supplemental T.C. Holder TALCO Aviation Corp. dba RAJAY Turbo Products 3015 E. New York St, STE A2-270 Aurora, IL 60504

Models 210, 210A, 210B, 210C, 210-5(205) & 210-5A(205A) (Normal Category) as modified by STC No. SA1098WE

Engine Continental IO-470-E (Models 210, 210A only) or IO-470-S (Models 210B, 210C, 210-5(205), 210-5A(205A) only) modified to incorporate turbochargers in accordance with Supplemental Type Certificate No. SE96SO.

SA1098WE Date of Issuance: November 5, 1965 Date Amended: March 21, 1985 Date of Reissuance: August 31, 2023

Fuel 100/130 Min. Grade Aviation Gasoline

Engine Limits Unturbocharged - same as original Turbocharged - Take Off - 28.0 in. Hg at 2625 RPM (3 min.)

Max. Continuous - 27.0 in Hg at 2500 RPM

Propeller Same as original except - Propeller Limits High pitch setting

Hartzell HC-A2XF-1/8433-2-30 deg at 30 in station.

McCauley D2A34C49/90A-8 or D2A36C33/90M-8 27 deg at 36 in. station.

Airspeed Limits Same as original except - Reduce Vne5MPH per 1,000 ft. above 22,000 ft. MSL for Models 210 and 210A and above 17,000 ft. MSL for Models 210B, 210C, 210-5(205), and 2105A(205A).

Placards The following placards must be located as shown on Roto-Master (Rajay) Drawing No. RJ1601, Sheet 6:

• MIN. CONT. CLIMB SPEED TURBOCHARGED MAX. CONT. C.A.S. 115MPH"

• FOR EMERGENCY DESCENT IDLE POWER - GEAR DOWN - C.A.S. 160MPH" 4 5

SA1098WE Date of Issuance: November 5, 1965 Date Amended: March 21, 1985 Date of Reissuance: August 31, 2023

• TURBOCHARGER OPERATION POWER LIMITS TAKEOFF: 28.0" MAP AT 2625RPM (3 MIN.)

MAX. CON.: 27.0" MAP AT 2500 RPM"

• "REDUCE VNE 5 MPH PER 1,000 FT. ABOVE 22,500 FT. MSL"

• "REDUCE VNE 5 MPH PER 1,000 FT. ABOVE 17,000 FT MSL"

• THIS AIRPLANE HAS NOT BEEN FAA EVALUATED FOR FLIGHTS ABOVE 25,000 FT."

• "WIDE OPEN THROTTLE BEFORE ENGAGING TURBOCHARGER" "100/130 MIN. GRADE AVIATION GASOLINE"

• *Models 210 and 210A only **Models 210B, 210C, 210-5(205), and 210-5A(205A) only

Limitation of Applicability:

The approval of this change in type design applies to the basic Cessna 210, 210A, 210B, 210C, 210-5(205) & 210-5A(205A). The installer must determine whether this design change is compatible with previously approved modifications. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

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