AD 51-03-02

final rule

Martin Models 202 and 202A Aircraft

AD Number
51-03-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

Applicability

TypeManufacturerModelDetails
aircraft Martin-Marietta Corporation 202 Martin Models 202 and 202A Aircraft
aircraft Martin-Marietta Corporation 202A Martin Models 202 and 202A Aircraft

Unsafe Condition

Cracks in main landing gear crankshafts (P/N 202SD82019 and 202SD82021) due to reported occurrences.

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

Required Actions

Replace main landing gear crankshafts with new ones bearing the same part numbers and having a ground radius around the periphery of the hole for the retract pin.

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

Compliance Time

By April 1, 1951, for aircraft with main landing gears having 4,000 hours service or more, and thereafter every 4,360 cycles of landing gear operation.

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

Affected Aircraft

Martin-Marietta Corporation Models 202 and 202A Aircraft with main landing gears having 4,000 hours service or more.

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

Federal Register Abstract

Landing Gear Crankshafts

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_51-03-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
51-03-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Martin Models 202 and 202A Aircraft
Subject:
Landing Gear Crankshafts
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Martin-Marietta Corporation
Model:
202 | 202A
Product Type:
Aircraft
Product Subtype:
Large 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Superseded AD: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Superseded By: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: 51-03-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   51-03-02

SUBJECT HEADING:   Martin Models 202 and 202A Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
51-03-02 MARTIN: Applies to All Models 202 and 202A Aircraft.

Compliance required by April 1, 1951, on all aircraft having main landing gears with 4,000 hours service or more, and thereafter every 4,360 cycles of landing gear operation.

Due to reported occurrences of cracks, the main landing gear crankshafts (P/N 202SD82019 and 202SD82021) should be replaced with new crankshafts bearing the same part numbers and having a ground radius around the periphery of the hole for the retract pin.

(Martin Service Bulletin No. 128, dated October 4, 1950, covers this same subject.)

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_51-03-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
51-03-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Martin Models 202 and 202A Aircraft
Subject:
Landing Gear Crankshafts
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Martin-Marietta Corporation
Model:
202 | 202A
Product Type:
Aircraft
Product Subtype:
Large 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: 51-03-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   51-03-02

SUBJECT HEADING:   Martin Models 202 and 202A Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
51-03-02 MARTIN: Applies to All Models 202 and 202A Aircraft.

Compliance required by April 1, 1951, on all aircraft having main landing gears with 4,000 hours service or more, and thereafter every 4,360 cycles of landing gear operation.

Due to reported occurrences of cracks, the main landing gear crankshafts (P/N 202SD82019 and 202SD82021) should be replaced with new crankshafts bearing the same part numbers and having a ground radius around the periphery of the hole for the retract pin.

(Martin Service Bulletin No. 128, dated October 4, 1950, covers this same subject.)

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.