AD 53-09-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| engine | Pratt & Whitney Division | Military R-2000 Series | PRATT & WHITNEY Model R-2000 Series Engines |
Unsafe Condition
Failures of link (knuckle) pins in the engines due to improper overhaul, inspection, or assembly procedures, resulting in cracked pins even in engines with zero time since overhaul.
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Required Actions
Dissassemble the engines, magnetically inspect link pins to eliminate cracked ones, and reassemble in accordance with manufacturer's instructions.
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Compliance Time
prior to further carriage of passengers or cargo in aircraft with such engines installed
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Affected Aircraft
Pratt & Whitney Model R-2000 Series Engines overhauled by San Antonio Air Depot between July 1, 1952, and April 9, 1953.
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Federal Register Abstract
Link Pins
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_53-09-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 53-09-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: PRATT & WHITNEY Model R-2000 Series Engines Subject: Link Pins Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: Make: Pratt & Whitney Division Model: Military R-2000 Series Product Type: Engine Product Subtype: Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 53-09-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 53-09-01 SUBJECT HEADING: PRATT & WHITNEY Model R-2000 Series Engines ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 53-09-01 PRATT & WHITNEY: Applies to R-2000 Series Engines Overhauled by San Antonio Air Depot Between July 1, 1952, and April 9, 1953. Compliance required prior to further carriage of passengers or cargo in aircraft with such engines installed. Aircraft may be ferried to base where inspection is to be conducted. Several operators of C-54 aircraft utilizing military overhauled engines, have experienced failures of link (knuckle) pins in the subject engines due to improper overhaul, inspection, or assembly procedures. The failures have occurred in comparatively low-time engines, and cracked pins have been found in engines with zero TSO. To preclude the possibility of further failures of this nature, engines falling within the category as noted must be dissassembled and the link pins magnetically inspected, eliminating any found with cracks, then reassembled in accordance with manufacturer's instructions, prior to further flight. Date of overhaul and identification of overhaul base stamped on exterior surface of engine nose housings. FOOTER:
Document Text
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AD Final Rules - DRS_53-09-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 53-09-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: PRATT & WHITNEY Model R-2000 Series Engines Subject: Link Pins Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: Make: Pratt & Whitney Division Model: Military R-2000 Series 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: 53-09-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 53-09-01 SUBJECT HEADING: PRATT & WHITNEY Model R-2000 Series Engines ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 53-09-01 PRATT & WHITNEY: Applies to R-2000 Series Engines Overhauled by San Antonio Air Depot Between July 1, 1952, and April 9, 1953. Compliance required prior to further carriage of passengers or cargo in aircraft with such engines installed. Aircraft may be ferried to base where inspection is to be conducted. Several operators of C-54 aircraft utilizing military overhauled engines, have experienced failures of link (knuckle) pins in the subject engines due to improper overhaul, inspection, or assembly procedures. The failures have occurred in comparatively low-time engines, and cracked pins have been found in engines with zero TSO. To preclude the possibility of further failures of this nature, engines falling within the category as noted must be dissassembled and the link pins magnetically inspected, eliminating any found with cracks, then reassembled in accordance with manufacturer's instructions, prior to further flight. Date of overhaul and identification of overhaul base stamped on exterior surface of engine nose housings. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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