STC SA1032WE

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA1032WE This certificate issued to: Texas Skyways, Inc 308 Boerne Stage Airfield Boerne, TX 78006 Part 3 of the Civil Air Regulations.

Original Product Type Berlificate Number: ЗА 13 Make: Cessna Model: 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182N, 182P Description of Type Design Change:

Installation of Roto-Master (Rajay) turbocharged Continental O-470L or 0-470R engine in accordance with FAA sealed Drawing List No. RJ1500, or later FAA approved revision.

Limitations and Conditions: See STC SA1032 Addendum which is part of this Supplemental Type Certificate.

suspended reecked or a termination date is otherwise estublished by the Administrater of the Federal Aviation Administretion Date of Application: February 02, 1965 Sale rested: Jan. 14, 1969; Feb. 10, 1982; Oct. 23, 1987;

Sept: 22, 1995; May 19. 2000 Date of Issuance: , August 18, 1965 Lute unvended. Aug.30, 1965; Sept. 12, 1967; Apr. 9, 1968;

Oct. L, 1975: Mar. 21, 1985 FEDERAL AVIATION Ву пін свість ту Не Аватитя Dange aler (Signature) TOMINSTRATO Paule. Sconvers Associate Manager, ACE-117A Atlanta Aircraft Certification Office (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1032WE Date of Issuance: August 18, 1965 Date Reissued: May 19, 2000 Supplemental Type Certificate Addendum No. SA 1032WE The conditions and limitations of Type Certificate Data Sheet No. 3A13 apply where superseded by the following:

This data sheet, which is part of Supplemental Type Certificate No. SA1032WE, prescribes conditions and limitations under which the product for which the STC was issues meets the airworthiness requirements of the Federal Aviation Regulations.

Supplemental T.C. Holder: Texas Skyways, Inc.

308 Boerne Stage Airfield Boerne, Texas 78006

1. - Models 182, 182A, 182B, 182C, 182D, 182D, 182E, 182F, 182G, 182H, and 182J (Normal Category) as modified by this STC Engine Continental 0-470-L (Models 182, 182A through 182G) or O-470-R (Models 182E through 182L) modified to incorporate turbochargers in accordance with Supplemental Type Certificate No SE25WE.

Fuel 100/130 Min. Grade Aviation Gasoline Engine Limits Unturbocharged - same as original Turbocharged - Take Off - 29.5 in. Hg at 2600 RPM (3 min.)

Max. Continuous - 27.0 in. Hg at 2500RPM Propeller and Same as original except - Propeller Limits High pitch setting:

Hartzell HC-82XF-1, HC-A2XF-1 or BHC-A2XF-1/8433-3 30° at 30 in. station.

Hartzell BHC-C2YF-1/8466-2 30° at 30 in. station.

McCauley 2A36C/90M-8 27° at 36 in. station.

McCauley 2A34C/90A-8 or 90AT-8 27° at 36 in. station.

Airspeed Limits Same as original except - Reduce VNE 5 MPH per 1, 000 ft. above 22,000 ft. MSL

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United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1032WE Date of Issuance: August 18, 1965 Date Reissued: May 19, 2000 Limitations and Conditions: (Continued):

Placards The following placards must be located as shown on Roto-Master (Rayjay) Drawing No. RJ1501, Sheet 2:

"MIN. CONT. CLIMB SPEED TURBOCHARGED METO POWER - C.A.S. 110 MPH" "FOR EMERGENCY DESCENT IDLE POWER - C.A.S. 160 MPH" "TURBOCHARGER OPERATION POWER LIMITS TAKEOFF: 29.5" MAP AT 2600 RPM (3 MIN.)

MAX. CONT.: 27.0" MAP AT 2500 RPM" "REDUCE VNE 5 MPH PER 1,000 FT. ABOVE 22,000 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" Limitation of Applicability The approval of this change in type design applies to the basic Cessna 182 Series as noted above. This approval should not be extended to other aircraft of these models on which other modifications are incorporated unless it is determined that the interrelationship between this change and any previously approved modification will introduce no adverse effect on the airworthiness of these aircraft.

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