What it approves
Installation of McCauley Propeller Model B3DF36C526/80HJA-0 and B3DF36C527/L80HJA-0, spinner assembly and optional de-icer.
What the certificate saysOCR
This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA0085TCH This certificate issued to: McCauley Propeller Systems 7751 East Pawnee Wichita, KS 67207 Purt 23 of the Federal Aviation
•Pegufulions. See Aircraft Specification No. A20SO for complete certification basis.
Original Product • Type Certificate Number: A2050 Abuke : Piper Model: PA-31, PA-31-325, PA-31-350 Description of Type Design Change:
Installation of McCauley Propeller Model B3DF36C526/80HJA-0 and B3DF36C527/L80HJA-0, spinner assembly and optional deice in accordance with McCauley Technical Report No. 790, no revision, dated February 16, 1998, and McCauley Drawing No. D- 60105, no revision, dated March 24, 1998, or Inter FAA approved revisions.
1. Compatibility of this design change with previously approved modifications must be determined by the installer.
(See continuation sheet 3 of 3) hull remain in effect until surrendered, suspended, reecked or u terminatien dute is etherwise estublished by the Administruter of the Federal Aviation Administration .
Date of Application: February 27, 1998 Lude reissued: September 23,2005 Late of issu * April 14, 1998 Lute unendert EDERA AVIATI By direction of the Sadn Hats (Signature) Thaddeus D. Krolicki, Jr.
SOMINISTRA Manager, Propulsion Branch Chicago Aircraft Certification Office (Title) or imprisonment not exceeding 3 years, or both This certificate may be transferred in accordance wich FAR 21.17.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA00357CH Date of Issuance: April 14, 1998 Reissued: September 23, 2005 Limitations and Conditions: (Continued):
2. FAA Approved Airplane Flight Manual Supplement for the Piper Aircraft Model PA-31, Technical Report Number 784, dated April 14, 1998, or later FAA approved revisions, is required.
3. FAA Approved Airplane Flight Manual Supplement for the Piper Aircraft Model PA-31-325 and PA-31-350, Technical Report Number 785, dated April 14, 1998, or later FAA approved revisions, is required.
4. The Lycoming engine models and Piper aircraft models eligible with the McCauley propeller models are as shown:
Aircraft Model Propeller Model Engine Model Maximum Continuous
EP RPM PA-31 B3DF36C526/80HJA-0 TIO-540-A1A, -A1B, 310 2575 -A2A, -A2B, -A2C PA-31-325 B3DF36C526/80HJA-0 (left) TIO-540-F2BD (left) 325 2575 B3DF36C527/L80HJA-0 (right) LTIO-540-F2BD (right) 325 2575 PA-31-350 B3DF36C526/80HJA-0 (left) TIO-540-J2B, -J2BD (left) 350 2575 B3DF36C527/L8OHJA-0 (right) LTIO-540-J2B, -J2BD (right) 350 2575
5. Aircraft specification limits are the same as listed on Aircraft Specification No. A20SO except as listed in McCauley Technical Report Numbers 784 and 785.
6. 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...
or boch.
FAA FORM 9110-3-1(10-69) PAGE 3 of 3 PAGES
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