AD 47-30-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna Aircraft Company | T-50 | Airworthiness Directives; CESSNA Model T-50 Airplanes |
Unsafe Condition
The absence of reinforcing doubler plates on the ends of brake pedal links, P/N 53046, could result in failure of the brake pedal links due to overstress at the fitting holes.
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Required Actions
Inspect the ends of brake pedal links, P/N 53046, for reinforcing doubler plates. If doubler plates are missing, remove the links and rivet two 0.040 inch x 1/2-inch x approximately 2-inch length 24ST aluminum alloy reinforcing doubler plates to each end using two 1/8-inch A17ST rivets through both doublers and the link.
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Compliance Time
no later than next 100 hour inspection
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Affected Aircraft
Cessna Model T-50 Aircraft
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Federal Register Abstract
Brake Pedal Links
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_47-30-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 47-30-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CESSNA Model T-50 Airplanes Subject: Brake Pedal Links Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: Make: Cessna Aircraft Company Model: T-50 Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 47-30-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 47-30-02 SUBJECT HEADING: Airworthiness Directives; CESSNA Model T-50 Airplanes ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 47-30-02 CESSNA: (Was Mandatory Note 12 of AD-722-5.) Applies to T-50 Aircraft. Compliance required no later than next 100 hour inspection. Inspect the ends of the brake pedal links, P/N 53046, for reinforcing doubler plates around the fitting holes. If the doubler is not in evidence, remove the links and rivet two 0.040 inch x 1/2-inch x approximately 2-inch length - 24ST aluminum alloy reinforcing doubler plates to each end of each link using two 1/8-inch A17ST rivets through both doublers and the link on the far side of the joggle from the fitting holes. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_47-30-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 47-30-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CESSNA Model T-50 Airplanes Subject: Brake Pedal Links Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: Make: Cessna Aircraft Company Model: T-50 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: AIRWORTHINESS DIRECTIVES FINAL RULES: 47-30-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 47-30-02 SUBJECT HEADING: Airworthiness Directives; CESSNA Model T-50 Airplanes ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 47-30-02 CESSNA: (Was Mandatory Note 12 of AD-722-5.) Applies to T-50 Aircraft. Compliance required no later than next 100 hour inspection. Inspect the ends of the brake pedal links, P/N 53046, for reinforcing doubler plates around the fitting holes. If the doubler is not in evidence, remove the links and rivet two 0.040 inch x 1/2-inch x approximately 2-inch length - 24ST aluminum alloy reinforcing doubler plates to each end of each link using two 1/8-inch A17ST rivets through both doublers and the link on the far side of the joggle from the fitting holes. 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.
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