AD 50-17-02

final rule

Airworthiness Directive; Stinson Model All 108 Series Aircraft

AD Number
50-17-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

Applicability

TypeManufacturerModelDetails
aircraft Univair Aircraft Corporation 108 Airworthiness Directive; Stinson Model All 108 Series Aircraft
aircraft Univair Aircraft Corporation 108-1 Airworthiness Directive; Stinson Model All 108 Series Aircraft
aircraft Univair Aircraft Corporation 108-2 Airworthiness Directive; Stinson Model All 108 Series Aircraft
aircraft Univair Aircraft Corporation 108-3 Airworthiness Directive; Stinson Model All 108 Series Aircraft

Unsafe Condition

Broken core strands in the rudder cables where they pass over the pulley at fuselage Station 18.75.

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

Required Actions

Inspect rudder cables within next 25 hours and every 100 hours thereafter by removing them from pulleys, bending into a tight 'U', and visually or tactile inspection. Replace cables showing breakage. Alternatively, remove AN 210-3A pulleys, modify brackets, install P/N 41001-2 pulleys and P/N SK253-2 cable guards per Piper SB No. 114 or equivalent.

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

Compliance Time

Within the next 25 hours and at every 100 hours thereafter

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

Affected Aircraft

Stinson Model All 108 Series Aircraft (108, 108-1, 108-2, 108-3) manufactured by Univair Aircraft Corporation.

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

Federal Register Abstract

Rudder cable inspection

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_50-17-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
50-17-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directive; Stinson Model All 108 Series Aircraft
Subject:
Rudder cable inspection
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Univair Aircraft Corporation
Model:
108 | 108-1 | 108-2 | 108-3
Product Type:
Aircraft
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
Updated RGL applicability to match AD applicability; CAR C-11-185
AIRWORTHINESS DIRECTIVES FINAL RULES: 50-17-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   50-17-02

SUBJECT HEADING:   Airworthiness Directive; Stinson Model All 108 Series Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   50-17-02 STINSON: Applies to All Model 108 Series Aircraft.
Compliance required as indicated.
A number of cases have been reported of broken core strands in the rudder cables where they pass over the pulley at fuselage Station 18.75 (first pulley aft of rudded pedals). To preclude failures, the following is therefore required:
1. Within the next 25 hours and at every 100 hours thereafter the following should be accomplished. Remove the rudder cables from the pulleys, bend the cables in a tight "U" where they pass over the pulley, being careful that permanent kinks are not formed, and inspect either visually or by touch. Replace all cables showing signs of breakage.
2. The above inspection may be discontinued and the normal inspections resumed if the following is done: Remove the AN 210-3A pulleys at fuselage Station 18.75; modify the pulley brackets and install larger pulleys, P/N 41001-2, and two cable guards, P/N SK253-2, in accordance with detailed instructions in Piper Service Bulletin No. 114 or an equivalent modification.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_50-17-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
50-17-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directive; Stinson Model All 108 Series Aircraft
Subject:
Rudder cable inspection
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Univair Aircraft Corporation
Model:
108 | 108-1 | 108-2 | 108-3
Product Type:
Aircraft
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
Updated RGL applicability to match AD applicability; CAR C-11-185
AIRWORTHINESS DIRECTIVES FINAL RULES: 50-17-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   50-17-02

SUBJECT HEADING:   Airworthiness Directive; Stinson Model All 108 Series Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   50-17-02 STINSON: Applies to All Model 108 Series Aircraft.
Compliance required as indicated.
A number of cases have been reported of broken core strands in the rudder cables where they pass over the pulley at fuselage Station 18.75 (first pulley aft of rudded pedals). To preclude failures, the following is therefore required:
1. Within the next 25 hours and at every 100 hours thereafter the following should be accomplished. Remove the rudder cables from the pulleys, bend the cables in a tight "U" where they pass over the pulley, being careful that permanent kinks are not formed, and inspect either visually or by touch. Replace all cables showing signs of breakage.
2. The above inspection may be discontinued and the normal inspections resumed if the following is done: Remove the AN 210-3A pulleys at fuselage Station 18.75; modify the pulley brackets and install larger pulleys, P/N 41001-2, and two cable guards, P/N SK253-2, in accordance with detailed instructions in Piper Service Bulletin No. 114 or an equivalent modification.

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.