AD 50-17-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| 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.
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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.
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Compliance Time
Within the next 25 hours and at every 100 hours thereafter
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Affected Aircraft
Stinson Model All 108 Series Aircraft (108, 108-1, 108-2, 108-3) manufactured by Univair Aircraft Corporation.
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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Corporation Model: 108 | 108-1 | 108-2 | 108-3 Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: Updated RGL applicability to match AD applicability; CAR C-11-185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
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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
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