STC SA10841SC

FAA Form 8110-2 (5/14) Page 1 of This certificate issued to:

Part of the Original Product – Type Certificate Number: Make:

By Direction of the Administrator Signature Title A37CE Supervan Systems Ltd.

8955 CR 135 Celina, TX 75009 5 SA10841SC Federal Aviation Regulations 23 The modification consists of removal of the Pratt & Whittney PT6A-114/114A engine, propeller and associated components to install a Honeywell TPE331-12JR engine, Hartzell HC-B4TN-5QL/LT10890NK (de-ice) or HC-B4TN-5QL/LT10890NK (non de-ice) or HC-B4TN-5NL/LT10981N (de-ice) propeller and associated components in accordance with Supervan Master Data List SSL-MDL-208-4001, Rev. D, dated May 22, 2012, or later FAA approved revision.

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.

(Continuation on page 4 of 5 & 5 of 5)

Textron Aviation, Inc.

208 and 208B Caravan July 30, 2012; January 24, 2013;

June 15, 2009; July 8, 2010; December 15, 2010;

June 11, 2012; June 13, 2017 October 24, 2002 November 26, 2008 Jim Grigg Manager, Fort Worth Aircraft Certification Office Southwest Region

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

5 SA10841SC

FAA Form 8110-2 (5/14) Page 3 of 5 Description of Type Design Change (continued):

Installation of optional Air Conditioner in accordance with Master Drawing List Number Document Number SSL-MDL-208-AC, Rev. A, dated 5/25/17, or later FAA approved revision.

The following FAA Approved Manual Supplement at the indicated revision level, or later FAA approved revision, is required:

For 208B Model: Document SSL-FMS-208B-12JR Landplane Rev. 4, dated May 5, 2017 For 208 Model: Document SSL-FMS-208-12JR Floatplane Rev. 3, dated May 5, 2017 Document SSL-FMS-208-12JR Landplane Rev. 4, dated May 5, 2017

Flight Manual Supplements For Standby Electrical System installations performed prior to June 13, 2017:

If optional Standby Electrical System is installed on a model 208B, FAA approved Flight Manual Supplement S2 Document Number SSL-SES-208B-12JR, Rev.1, dated December 15, 2010, or later FAA approved revision is required.

If optional Standby Electrical System is installed on a model 208, then FAA approved Flight Manual Supplement S2 Document Number SSL-SES-208-12JR, Rev. 1, dated December 15, 2010, or later FAA approved revision is required.

Flight Manual Supplement for Standby Electrical System installations beginning with STC amendment dated June 13, 2017:

If optional Standby Electrical System is installed on model 208 or model 208B, then FAA approved Flight Manual Supplement S2, Document Number SSL-SES-208/208B-12JR, Rev. 0, dated May 15, 2017, or later FAA approved revision is required.

If optional air conditioner is installed on model 208 or model 208B, then FAA approved Flight Manual Supplement S3, Document Number SSL-ACS-208/208B-12JR, Rev. 0, dated May 5, 2017, or later FAA approved revision is required.

For 208B flight into known icing conditions, FAA approved Flight Manual Supplement S1 SSL-KIS-208B-12JR, Rev. 1, dated February 23, 2012, or later FAA approved revision is required.

For 208 flight into known icing conditions, FAA approved Flight Manual Supplement S1 SSL-KIS-208-12JR, Rev. 1, dated February 23, 2012, or later FAA approved revision is required.

The aircraft must be maintained in accordance with Instructions for Continued Airworthiness document 9004-21, Rev. C1, dated April 15, 2017, or later FAA accepted revision.

Gross weight increase changes per STCs SA00188SE and SA00392SE for model 208B are compatible with this STC.

Gross weight increase changes per STC SA270CH for model 208 are compatible with this STC.

Wipaire STC SA1311GL, Float modification is compatible with this STC. Wipaire Service Kit #25 must be installed on aircraft serial number 20800329 and earlier.

SA10841SC

FAA Form 8110-2 (5/14) Page 4 of 5 Limitations and Conditions (continued):

For Model 208: This STC is limited to Standard version (without cargo pod) to serial numbers 20800001 through 20800415 and 20800417 through 20800499.

For Model 208B: This STC is limited to serial numbers 208B0001 through 208B1189, 208B1191 through 208B1215 and 208B1217 through 208B1999.

Certification Basis: Based on 14 CFR §§ 21.101 and 21.115, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Cessna 208 and 208B modified in accordance with Supervan Master Data List, SSL-MDL-208-4001, Rev.

D, dated May 22, 2012, or later FAA approved revision is as follows:

a) The type certification basis for the Cessna 208 and 208B is shown on FAA TCDS A37CE and accordingly on EASA TCDS IM.A.388 for areas not changed or affected by the change.

b) The certification basis for parts changed or affected by the Supervan modification of the Cessna 208/208B (FAA STC SA10841SC, EASA STC 10033267) is based upon 14 CFR Part 23 as amended by Amendment 23-55. Based on 14 CFR §§ 21.101 and 21.115, and FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be the following regulations at the latest amendment 23-0 through 23-55:

For Cessna 208B:

23.1(b); 23.21; 23.23; 23.25; 23.29; 23.33(a)(d); 23.45(a)(b)(1)(3)(c)(d)(e)(f)(g); 23.49; 23.51 (a)(2)(b)(2); 23.53(a)(b); 23.63(a)(1)(2)(c);

23.65(b); 23.69(a); 23.71; 23.73(b); 23.75(a)(b)(c) (d)(e)(f); 23.77(b); 23.141; 23.143; 23.145(a)(1)(2)(3)(ii)(b)(c)(d)(e)(1); 23.147(c);

23.153; 23.155(a)(1)(b)(c); 23.157(a)(2)(b)(1)(3)(4)(c)(2)(d); 23.161(a)(b)(1)(c); 23.171; 23.173(a) (b)(1)(c); 23.175(a)(1)(3)(4)(b)(1)(i)(ii)

(c); 23.177(a); 23.177(b)(d); 23.181 (a)(b)(d); 23.201; 23.203; 23.207(a)-(e); 23.221(a); 23.231(a); 23.233(a)(b)(c); 23.235; 23.251;

23.253; 23.301(a)(b)(c); 23.303; 23.305; 23.307(a)(b); 23.321(a)(b); 23.333(a)(b)(c)(d); 23.337(a)(1)(b)(1); 23.341(a)(c); 23.345(d)(1)

(2); 23.361 (a)(b)(c)(1); 23.363(a)(b); 23.371 (a)(2); 23.391; 23.409; 23.423; 23.471; 23.473(a)(e)(f)(g); 23.477; 23.479(a)(2)(b)(c);

23.481; 23.499(a)(b)(c)(e); 23.509(a)(c)(2)(d); 23.561 (a)(b)(3)(e); 23.572(a)(1)(b)(3); 23.575; 23.601; 23.603(a)(b); 23.605(a); 23.607

(a)(b)(c); 23.609(a)(b); 23.611; 23.613(a)(b)(c)(d); 23.619(a); 23.625(a)(b)(c); 23.627; 23.629(a)(b)(c)(d)(e)(i); 23.671(a)(b); 23.685(a);

23.689(a)(1)(2); 23.745(a); 23.771(a); 23.777(a)(b); 23.779(b); 23.781(b); 23.831(a); 23.853; 23.863(a)(b)(c)(d); 23.865; 23.867(a)(b)

(c); 23.901(b)(1)(2)(c)(d)(1)(2)(e)(1)(2); 23.903(a)(1)(2)(iv)(b)(1)(2)(e)(1)(2)(3)(4)(f)(g); 23.905(a)(b) (c)(d); 23.907; 23.925(a)(d); 23.929;

23.933(b); 23.937; 23.939(a)(c); 23.943; 23.951(a)(d); 23.955(a)(1)(2)(4)(f)(1)(3); 23.959; 23.961; 23.963(d)(e); 23.991(a)(2)(i)(d);

23.993; 23.994; 23.995(a)(b)(2)(c)(d)(e); 23.997(a)(b)(c)(d); 23.1011(a)(b)(c)(d); 23.1013(a)(b)(c)(d)(1)(2)(e)(g); 23.1015(a)(c); 23.1017

(a); 23.1019(a)(1)(2)(3)(4); 23.1021; 23.1023; 23.1027; 23.1041; 23.1043(a)(1)(2)(3)(b)(c); 23.1045; 23.1091(a)(c)(1); 23.1093(b)(1)(2);

23.1103(a)(b); 23.1111(a)(b)(c); 23.1121(a)-(g); 23.1123(a)(b); 23.1141(a)(b)(c)(d)(e)(g)(1)(2); 23.1143(a)(c); 23.1145(a)(c); 23.1149(a)

(1); 23.1153; 23.1155; 23.1163(a)(1)(2)(3)(b)(c); 23.1165(a)(b)(c)(1)(2)(d)(e); 23.1181(b); 23.1182; 23.1183(a)(b); 23.1189(b); 23.1191

(Continuation on page 5 of 5) SA10841SC

FAA Form 8110-2 (5/14) Page 5 of 5 Limitations and Conditions (continued):

23.1193(a)(b)(c)(e); 23.1203(b)(c)(e); 23.1301(a)-(d); 23.1305(a)(2)(3)(5)(c)(1)(2)(3)(5)(6)(7) (10)(e)(1)(2); 23.1309(a)(1)(2)(b)(1)(2)(3)

(4)(c)(d)(e)(f); 23.1321(a)(c); 23.1322(a)(b)(c)(d)(e); 23.1323(a)(b); 23.1325(e); 23.1337(a)(1)(2)(i)(ii)(3)(b)(1)(c); 23.1351(a)(1)(2)(i)(b)

(1)(i)(ii)(iii) (2)(3)(c)(1)(2)(3)(4)(5)(d)(1)(f)(g)(1)(2); 23.1353(a)(b)(c)(d)(e)(h); 23.1357(a)(b)(c)(1)(2)(d); 23.1359(a)(c); 23.1365(a)(b)(c)

(d)(e)(f); 23.1367(a)(b)(c)(d); 23.1416(a)(b); 23.1431(a)(b)(e); 23.1438(b); 23.1501(a)(b); 23.1505(c); 23.1507; 23.1511(a)(1)(2);

23.1519; 23.1521 (a)(b)(1)(3)(4)(c)(1)(3)(4)(d)(e); 23.1525; 23.1527(a); 23.1529; 23.1541(a)(b); 23.1543(b)(c); 23.1549(a)(b)(c);

23.1551; 23.1555(a)(e)(2); 23.1557(c)(2)(e); 23.1581(a)(1)(2)(3)(b)(1)(3) (c)(d)(f); 23.1583(b)(1)(2)(3)(c)(1)(2)(3)(d)(f)(h)(m)(n);

23.1585(a)(d)(j); 23.1587(a)(c)(1)(2)(3)(6); 14 CFR Part 34; 14 CFR Part 36.

For Cessna 208:

All of the regulations above for the 208B with the following additions:

23.231 (b), 23.233(d), 23.237, 23.239, 23.521, 23.523, 23.525, 23.527, 23.529(a)(c).

The certification basis for the optional air conditioner installation includes the above as affected 14 CFR regulations at the latest amendment 23-0 through 23-62:

23.1; 21.3; 23.21; 23.23; 23.29; 23.63(a)(c); 23.65(b); 23.77(b); 23.141; 23.143(a); 23.251; 23.301(a); 23.303; 23.305; 23.307(a); 23.337

(a)(1)(b)(1); 23.341(a)(c); 23.603(a)(2)(3)(b); 23.605; 23.609; 23.611; 23.613(a)(b)(c)(d); 23.619(a); 23.625(a)(b)(c); 23.627; 23.629;

23.863; 23.867(a)(b)(c); 23.901(a)(2)(b)(1)(e)(1)(2); 23.1041; 23.1043(a)(1)(2)(3)(b)(c); 23.1045; 23.1163(a)(1)(2)(3)(b); 23.1181(b)(1);

23.1183(a); 23.1191(b)(c)(h); 23.1301(a)-(d); 23.1308; 23.1309(a)(1)(2)(b)(e); 23.1351(a)(b)(1)(i)(ii)(iii)(2)(3)(c)(1)(2)(4); 23.1357(a)(b)

(c); 23.1359(a)(c); 23.1361(a); 23.1365(a)(b)(d)(e); 23.1367; 24.1419(a); 23.1431(b); 23.1501; 23.1519; 23:1529; 23.1541(a)(b);

23.1581(a)(1)(b)(1)(3); 23.1585(j); 23.1589(b); and 14 CFR Part 36, at amendment 36-30.

---------------------------------------------------------------------------------END------------------------------------------------------------------------------------

SA10841SC