AD 58-09-02

final rule

HARTZELL Models HC-82XF-1 and -1A Propellers

AD Number
58-09-02
Status
final_rule
Effective Date
Product Category
propeller
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Hartzell Propeller, Inc. HC-82XF-1 HARTZELL Models HC-82XF-1 and -1A Propellers
propeller Hartzell Propeller, Inc. HC-82XF-1 HARTZELL Models HC-82XF-1 and -1A Propellers

Unsafe Condition

Failure of the piston guide rod P/N A-811 used in jack assembly B-804 breaking at the point where it is pinned to the A-96A fork, which could allow a blade to become uncontrollable.

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

Required Actions

Inspect the exposed rod for cracks within 25 flight hours if replacement is not done. Replace jack assembly B-804 with B-828 prior to September 1, 1958.

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

Compliance Time

Within 25 flight hours for inspection if replacement is not done; replacement must be completed prior to September 1, 1958.

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

Affected Aircraft

Hartzell Propeller, Inc. models HC-82XF-1 and -1A propellers installed on Cessna 180 aircraft.

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

Federal Register Abstract

Piston Guide Rod

Applicability Source Text

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AD Final Rules - DRS_58-09-02.html
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AD Number:
58-09-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
HARTZELL Models HC-82XF-1 and -1A Propellers
Subject:
Piston Guide Rod
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Hartzell Propeller, Inc.
Model:
HC-82XF-1
Product Type:
Propeller
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Superseded AD: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Superseded By: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: 58-09-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   58-09-02

SUBJECT HEADING:   HARTZELL Models HC-82XF-1 and -1A Propellers

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
58-09-02 HARTZELL: Applies to HC-82XF-1 and -1A Propellers Installed on Cessna 180 Aircraft.

Compliance required as outlined.

There have been several reported instances of the piston guide rod P/N A-811 used in jack assembly B-804 breaking at the point where it is pinned to the A-96A fork. Failure of a guide rod will allow the particular blade to become uncontrollable. In view of the possible serious consequences resulting from vibration and the loss of control of the propeller, the following steps must be taken:

1. Inspection within 25 hours.

If item 2 will not be complied with within 25 hours of operation, remove fork pin P/N A- 522 and slide the pitch change fork P/N A-96 sufficiently to completely expose the hole in push rod P/N A-811 used in jack assembly B-804. Visually inspect the exposed rod for cracks. If a crack is found, the rod should be removed from the propeller and replaced.

2. Replacement.

Prior to September 1, 1958, replace jack assembly B-804 with jack assembly B-828.

(Hartzell Service Bulletin No. 39 dated January 16, 1957, covers this same subject, and Hartzell Service Bulletin No. 47 also applies.)

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_58-09-02.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
58-09-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
HARTZELL Models HC-82XF-1 and -1A Propellers
Subject:
Piston Guide Rod
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Hartzell Propeller, Inc.
Model:
HC-82XF-1
Product Type:
Propeller
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: 58-09-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   58-09-02

SUBJECT HEADING:   HARTZELL Models HC-82XF-1 and -1A Propellers

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
58-09-02 HARTZELL: Applies to HC-82XF-1 and -1A Propellers Installed on Cessna 180 Aircraft.

Compliance required as outlined.

There have been several reported instances of the piston guide rod P/N A-811 used in jack assembly B-804 breaking at the point where it is pinned to the A-96A fork. Failure of a guide rod will allow the particular blade to become uncontrollable. In view of the possible serious consequences resulting from vibration and the loss of control of the propeller, the following steps must be taken:

1. Inspection within 25 hours.

If item 2 will not be complied with within 25 hours of operation, remove fork pin P/N A- 522 and slide the pitch change fork P/N A-96 sufficiently to completely expose the hole in push rod P/N A-811 used in jack assembly B-804. Visually inspect the exposed rod for cracks. If a crack is found, the rod should be removed from the propeller and replaced.

2. Replacement.

Prior to September 1, 1958, replace jack assembly B-804 with jack assembly B-828.

(Hartzell Service Bulletin No. 39 dated January 16, 1957, covers this same subject, and Hartzell Service Bulletin No. 47 also applies.)

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.