AD 56-17-03

final rule

HARTZELL Model HC-12X20 Reversing Propellers

AD Number
56-17-03
Status
final_rule
Effective Date
Product Category
engine
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft propeller assembly
Problem area Propeller

Applicability

TypeManufacturerModelDetails
engine Hartzell Propeller, Inc. HC-12X20-1 HARTZELL Model HC-12X20 Reversing Propellers
engine Hartzell Propeller, Inc. HC-12X20-2 HARTZELL Model HC-12X20 Reversing Propellers
engine Hartzell Propeller, Inc. HC-12X20-3 HARTZELL Model HC-12X20 Reversing Propellers
engine Hartzell Propeller, Inc. HC-12X20-4 HARTZELL Model HC-12X20 Reversing Propellers
engine Hartzell Propeller, Inc. HC-12X20-5 HARTZELL Model HC-12X20 Reversing Propellers
engine Hartzell Propeller, Inc. HC-12X20-6 HARTZELL Model HC-12X20 Reversing Propellers
engine Hartzell Propeller, Inc. HC-12X20-7 HARTZELL Model HC-12X20 Reversing Propellers
engine Hartzell Propeller, Inc. HC-12X20-8 HARTZELL Model HC-12X20 Reversing Propellers
engine Hartzell Propeller, Inc. HC-12X20-9 HARTZELL Model HC-12X20 Reversing Propellers

Unsafe Condition

Failure of the valve tube A-57 due to vibration and weakening effect of the valve porthole, which could allow the propeller to go into reverse under certain conditions, forcing the airplane to land.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Disassemble the valve assembly and inspect the A-57 valve tube around the valve port with a magnifying glass or magnetic inspection equipment. If no cracks are found, round the sharp edges at the sides of the porthole using a fine round file.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

as soon as possible but not later than next 25 hours of operation and each 100 hours flight time thereafter

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Hartzell Propeller, Inc. Model HC-12X20 Reversing Propellers installed on Downer (Republic) RC-3 Aircraft with B-55 Valve Assembly

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

Valve Tube

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_56-17-03.html
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AD Number:
56-17-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
HARTZELL Model HC-12X20 Reversing Propellers
Subject:
Valve Tube
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Hartzell Propeller, Inc.
Model:
HC-12X20-1 | HC-12X20-2 | HC-12X20-3 | HC-12X20-4 | HC-12X20-5 | HC-12X20-6 | HC-12X20-7 | HC-12X20-...Show more
Product Type:
Engine
Product Subtype:
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 56-17-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   56-17-03

SUBJECT HEADING:   HARTZELL Model HC-12X20 Reversing Propellers

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
56-17-03 HARTZELL: Applies to All Model HC-12X20 Reversing Propellers Installed on Downer (Republic) RC-3 Aircraft Having B-55 Valve Assembly.

Compliance required as soon as possible but not later than next 25 hours of operation and each 100 hours flight time thereafter.

There have been two reported instances of broken valve tube A-57. These failures were due to vibration of the valve assembly and the weakening effect of the valve porthole. Failure of this part will allow the propeller to go into reverse under certain conditions, forcing the airplane to land. In view of the possible serious consequences resulting from inadvertent reversal of the propeller, disassemble the valve and inspect the A-57 valve tube around the valve port with a magnifying glass or with magnetic inspection equipment. If no cracks are found, the sharp edges at the sides of the porthole should be rounded slightly, using a fine round file.

This inspection is not required for valve assembly B-299.

(Hartzell Service Bulletin No. 38 dated June 16, 1956, covers the same subject.)

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_56-17-03.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
56-17-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
HARTZELL Model HC-12X20 Reversing Propellers
Subject:
Valve Tube
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Hartzell Propeller, Inc.
Model:
HC-12X20-1 | HC-12X20-2 | HC-12X20-3 | HC-12X20-4 | HC-12X20-5 | HC-12X20-6 | HC-12X20-7 | HC-12X20-...Show more
Product Type:
Engine
Product Subtype:
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 56-17-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   56-17-03

SUBJECT HEADING:   HARTZELL Model HC-12X20 Reversing Propellers

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
56-17-03 HARTZELL: Applies to All Model HC-12X20 Reversing Propellers Installed on Downer (Republic) RC-3 Aircraft Having B-55 Valve Assembly.

Compliance required as soon as possible but not later than next 25 hours of operation and each 100 hours flight time thereafter.

There have been two reported instances of broken valve tube A-57. These failures were due to vibration of the valve assembly and the weakening effect of the valve porthole. Failure of this part will allow the propeller to go into reverse under certain conditions, forcing the airplane to land. In view of the possible serious consequences resulting from inadvertent reversal of the propeller, disassemble the valve and inspect the A-57 valve tube around the valve port with a magnifying glass or with magnetic inspection equipment. If no cracks are found, the sharp edges at the sides of the porthole should be rounded slightly, using a fine round file.

This inspection is not required for valve assembly B-299.

(Hartzell Service Bulletin No. 38 dated June 16, 1956, covers the same subject.)

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.