What it approves
Installation of Walter a.s. turboprop engine model M601E-l l or M601D-l l with the AVIA Propeller Ltd. model V510AG, V508E-AG/99 or V508E-AG/106 in accordance with Turbine Conversions Drawing List, Report 3100, Revision C, dated August I, 2005, or later FAA approved revision.
What the certificate saysOCR
This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.
nepors United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA01353CH This certificate issued to: Turbine Conversions, Ltd.
18155 120h Ave Nunica, MI 49448 Purt 08 of the Civil Air Regulations.
(See Type Certificate Data Sheet No. 1A16 for complete certification basis) Original Product - Type Cerlificate Number: 1A16 Make: Ag Cat Corp.
Model: G-164A, G-164B Description of Type Design Change:
Installation of Walter a.s. turboprop engine model M601E-11 or M601D-11 with the AVIA Propeller Ltd.
model V510AG, V508E-AG/99 or V508E-AG/106 in accordance with Turbine Conversions Drawing List, Report 3100, Revision C, dated August 1, 2005, or later FAA approved revision.
1. FAA Approved Airplane Flight Manual Supplement for FAT-CAT (Ag Cat, G-164A and G-164B models with STC SA3645SW installed) modified in accordance with STC SA01353CH, Revision A, dated January 26, 2005, or later FAA Approved Revision, is required.
(See Continuation Sheet Page 3 for additional Limitations and Conditions.)
Date of Application: September 6, 2000 Date Reissued:
Date of Issuance: January 23, 2001 Date Amended: August 30, 2005
FEDERAL AVIATION 'Thaddeus D. Krolicki Jr.
TOMINSTRATO Manager, Propulsion Branch Chicago Aircraft Certification Office (Title)
TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) _ (Address of transferee) (Number and street) (City, State, and ZIP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) ( Citr. State, and KIP code) Extent of Authority (if licensing agreement):.
Signature of grantor (In ink):
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01353CH Date of Issuance: January 23, 2001 Amended August 30, 2005 Limitations and Conditions: (Continued)
2. Aircraft Specification limits are the same as listed on Type Certificate Data Sheet No. 1A16 except as listed in the FAA Approved Flight Manual Supplement for FAT CAT (Ag Cat, G-164A and G-164B models with STC SA3645SW installed) modified in accordance with this STC.
Limits for Walter a.s. turboprop engine model M601E-11 and M601D-11 and AVIA Propeller Ltd.
models V510AG, V508E-AG/99 and V508E-AG/106 are published in the FAA Approved Flight Manual Supplement for FAT CAT (Ag Cat, G-164A and G-164B models with STC SA3645SW installed) modified in accordance with this SIC.
The life limits for the AVIA Propeller Ltd. models V510AG, V508E-AG/99 and V508E-AG/106 in accordance with Type Certificate Data Sheet Numbers P2BO and P21BO, and as referenced in the AVIA Maintenance Manual, is 6,000 flight hours.
Power lever below flight idle (Beta Range) when the aircraft is in flight can result in severe over speeding and/or loss of aircraft control and must be avoided.
6. STC SA3645SW modifications must be incorporated.
7. The engine manufacturer's Beta, Torque, and Temperature Limiting indicating systems are installed in accordance with this STC.
8. Compatibility of this design change with previously approved modifications must be determined by the installer.
9. 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.
....End....
FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES
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