Supplemental Type Certificate Number: STC SVA554
Cessna 208B Grand Caravan · Type Certificate
Overview
This document is a Supplemental Type Certificate (STC) issued by the Australian Government's Civil Aviation Safety Authority for modifications made to the Cessna 208 aircraft. The STC certifies that the modified type design meets the applicable airworthiness requirements for single-engine aeroplanes. The modifications primarily involve the replacement of the original Pratt and Whitney PT6A-114(A) engine with a PT6A-42A engine, along with the installation of new propellers and associated equipment. The document outlines the conditions and limitations for these modifications, ensuring that they do not adversely affect the airworthiness of the aircraft. It also specifies the necessary compliance with FAA regulations and provides references to the required documentation for installation and continued airworthiness.
- The Cessna 208 can be modified with a PT6A-42A engine and specific Hartzell propellers.
- Modifications must comply with FAA Approved Master Drawing Lists and specific revisions.
- The STC does not apply to Cessna 208 aircraft with serial numbers 2080500 and greater.
- Installations must follow the instructions for continued airworthiness provided by Blackhawk Modifications Inc.
- The certification is based on compliance with 14 CFR Part 23 regulations.
Document
Source
Originally published by www.casa.gov.au. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Type Certificate
- Year
- 2022
- Pages
- 2
- File size
- 449 KB
- Publisher
- www.casa.gov.au
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- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Modification Options
The STC details two options for modifying the Cessna 208. Option One involves replacing the original Pratt and Whitney PT6A-114(A) engine with a PT6A-42A engine and installing either a 4-blade Hartzell Propeller HC-E4N-3P/D9900(K) or a 3-blade Hartzell Propeller HC-B3TN-3AE(Y)/T10290N(K)+2. Option Two outlines a similar replacement with the addition of an ADAS+ Engine Trend Monitor system.
Installation Requirements
All installations must comply with the FAA Approved Master Drawing List and the Pilot's Operating Handbook, including specific revisions dated February 15, 2013, and June 21, 2013. The document emphasizes that modifications must be performed according to the approved instructions to ensure continued airworthiness.
Limitations and Conditions
The STC specifies that the modifications are not compatible with Cessna Model 208 aircraft with serial numbers 2080500 and greater, those equipped with Garmin 1000 installations, or TKS installations. It also states that the approval should not extend to other aircraft unless the installer confirms no adverse effects on airworthiness.
Certification Basis
The certification for the modifications is based on compliance with 14 CFR Part 23 of the Federal Aviation Regulations, which includes numerous amendments ensuring the aircraft meets safety and performance standards.
Safety notes
- Modifications must not adversely affect the airworthiness of the aircraft.
- Ensure compliance with all specified FAA regulations and documentation.
Full document text
i Australian Government Civil Aviation Safety Authority Supplemental Type Certificate Number: STC SVA554 This certificate issued to: Blackhawk Modifications Inc 7601 Karl May Drive Waco, Texas 76708 certifies that the type design for the following changed product with the limitations and conditions as specified herein meets the applicable airworthiness requirements for eligibility as a prescribed single-engine aeroplane (PSEA). A320 (previously A123) | FAA A37CE Cessna 208 Original Product: Type Acceptance Certificate Number: Referenced TC Number: Make/Model: Description of Type Design Change: Option One: Replacement of the original Pratt and Whitney PT6A-114(A) engine and propellerwith a Pratt and Whitney PT6A-42A and 4-blade Hartzell Propeller HC-E4N-3P/D9900(K) propeller or 3- blade Hartzell Propeller HC-B3TN-3AE(Y)/T10290N(K)+2, and associated equipment in accordance with FAA STC SA02467LA, inclusive of Flight Systems Checkpoint Engine Trend Monitor System. Installations done in accordance with FAA Approved Master Drawing List 201201-000, Rev A, dated Feb. 15, 2013, or later FAA approved revisions. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplements, AFMS 201201-1, Rev IR, dated June 21, 2013 and AFMS 201201-2, Rev IR, dated June 21,201 3 or later FAA approved revisions. Blackhawk Modifications Inc. Instructions for Continued Airworthiness document ICA 201201-30, Rev IR, dated June 14, 2013, or later revisions. Option Two: Replacement of the original Pratt and Whitney PT6A-114(A) engine and propeller with a Pratt and Whitney PT6A-42A and 4-blade Hartzell Propeller HC-E4N-3P/D9900(K) propeller or 3- blade Hartzell Propeller HC-B3TN-3AE(Y)/T10290N(K)+2, and associated equipment in accordance with FAA STC SA02467LA, inclusive of ADAS+ Engine Trend Monitor system. fsee continuation sheet) Date of application: 01/03/2013 Date of issuance: Date Amended: 24/11/2014 07/09/2022 This certificate is issued pursuant to Part 21.113A of the Civil Aviation Regulations 199K^^>.. VU£'!'k£Wv- Klh'^^p^^t^er a^'ttief^uthori uthority This certificate^ ransferred in accordance with CASR (1998) 21.47 Paae 1 of 2 CAS401 Prinieciia'2609 Supplemental Type Certificate- SVA554 (Continuation Sheet) Option Two: (continued) Installations done in accordance with FAA Approved Master Drawing List 201201-000, Rev A, dated Feb. 15, 2013, or later FAA approved revisions. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplements, AFMS 201201-1, Rev IR, dated June 21, 2013 and AFMS 201201-2, Rev IR, dated June 21, 2013 or later FAA approved revisions. ADAS+ installed IAW installation manual ADAS-G-010-1/A revision K, ADAS+ Addendum A, or later approved revisions, including additional drawings (x2) 201318-100+ Modifications for XP- 42A.BIackhawk Modifications Inc. Instructions for Continued Airworthiness document ICA 201201-30, Rev IR, dated June 14, 2013, or later revisions. Limitations and Conditions: This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those previously approved modifications will produce no adverse effect upon the airworthiness of that aircraft. 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. This certificate and the supporting data which is the basis for approval shall remain in effect until suspended, cancelled or a termination date is otherwise established by the Civil Aviation Safety Authority. Conditions: The aircraft must meet the requirements of CAO 100.5 for PSEA. These modifications are not compatible with Cessna Model 208 Serial Number 2080500 and greater, aircraft equipped with Garmin 1000 installations, and aircraft equipped with TKS installation. Certification Basis: 14 CFR Part 23 of the Federal Aviation Regulations effective February 1, 1965, as amended by Amendments 23-1 through 23-62 for 23.1, 23.21, 23.23, 23.25, 23.33, 23.45, 23.49, 23.51, 23.53, 23.63, 23.65, 23.69, 23.73, 23.75, 23.77, 23.141, 23.143, 23.145, 23.147, 23.153, 23.155, 23.157, 23.161, 23.171, 23.173, 23.175, 23.177, 23.179, 23.181, 23.201, 23.203, 23.221, 23.231, 23.233, 23.251, 23.253, 23.301, 23.303, 23.305, 23.307, 23.321, 23.331, 23.333. 23.335, 23.337, 23.341, 23.361, 23.363, 23.371, 23.421, 23.471, 23.473, 23.479, 23.481, 23.483, 23.485, 23.493, 23.499, 23.507, 23.509, 23.561, 23.572, 23.601, 23.603, 23.605, 23.607, 23.609, 23.611, 23.613, 23.619, 23.623, 23.625, 23.627, 23.629, 23.735, 23.771, 23.831, 23.863, 23.865, 23.867, 23.901, 23.903, 23.905, 23.907, 23.925, 23.929, 23.933, 23.939, 23.955, 23.959, 23.961, 23.991, 23.993, 23.994, 23.999, 23.1011, 23.1017, 23.1019, 23.1021, 23.1023, 23.1027, 23.1041, 23.1043, 23.1045, 23.1121, 23.1123, 23.1141, 23.1163, 23.1165, 23.1181, 23.1305, 23.1308, 23.1309, 23.1321, 23.1322, 23.1327, 23.1357, 23.1359, 23.1365, 23.1381, 23.1416, 23.1431, 23.1091 23.1183 23.1329 23.1501 23.1093, 23.1103, 23.1111, 23.1193, 23.1203, 23.1301, 23,1331, 23.1337, 23.1351, 23.1507, 23.1519, 23.1521, 23.1525, 23.1527, 23.1529, 23.1541, 23.1543, 23.1547, 23.1549, 23.1551, 23.1555, 23.1557, 23.1581, 23.1583, 23.1585, 23.1587, 23.1589, except 23.1419 as amended by 23-1 through 23-14. 1. Special Condition 23-ACE-3, Dynamic Evaluation, Engine Installation. Factors from this special condition were incorporated into the whirl mode flutter analysis per 14 CFR 23.629(e)(1) and (2) Amendment 23-54, Flutter. 2. 14 CFR 34, effective January 1, 1994, as amended by Amendments 34-1 thru 34-4. 3. 14 CFR 36, effective December 1, 1969, as amended by Amendments 36-1 thru 36-28. This certificate may be transferred in accordance with CASR (1998) 21.47 Page 2 of 2 "^•A^" ftX/ CAS402 Printed 03/2019 CIVIL AVIATION SAFETY AUTHORITY
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