AD 73-19-03

final rule

Airworthiness Directives; Mitsubishi Model MU-2B, MU-2B-10, MU-2B-15, MU-2B-20, and MU-2B-25 Airplanes

AD Number
73-19-03
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 Mitsubishi Heavy Industries, Ltd. MU-2B Airworthiness Directives; Mitsubishi Model MU-2B, MU-2B-10, MU-2B-15, MU-2B-20, and MU-2B-25 Airplanes
aircraft Mitsubishi Heavy Industries, Ltd. MU-2B-10 Airworthiness Directives; Mitsubishi Model MU-2B, MU-2B-10, MU-2B-15, MU-2B-20, and MU-2B-25 Airplanes
aircraft Mitsubishi Heavy Industries, Ltd. MU-2B-15 Airworthiness Directives; Mitsubishi Model MU-2B, MU-2B-10, MU-2B-15, MU-2B-20, and MU-2B-25 Airplanes
aircraft Mitsubishi Heavy Industries, Ltd. MU-2B-20 Airworthiness Directives; Mitsubishi Model MU-2B, MU-2B-10, MU-2B-15, MU-2B-20, and MU-2B-25 Airplanes
aircraft Mitsubishi Heavy Industries, Ltd. MU-2B-25 Airworthiness Directives; Mitsubishi Model MU-2B, MU-2B-10, MU-2B-15, MU-2B-20, and MU-2B-25 Airplanes

Unsafe Condition

Failure of the nose gear actuating system.

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

Required Actions

Modify the nose gear actuating assembly and its supporting structure in accordance with Mitsubishi MU-2 Service Bulletin No. 155, dated June 26, 1972, or an equivalent method approved by the Chief, Engineering and Manufacturing Branch, FAA, Pacific-Asia Region.

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

Compliance Time

Within the next 100 hours' time in service after the effective date of this AD

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

Affected Aircraft

Mitsubishi Model MU-2B airplanes (S/N 004, and 006 through 038); MU-2B-10, and -15 airplanes (S/N 101, and 103 through 120); MU-2B-20, and -25 airplanes (S/N 005, 102, and 121 through 271)

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

Federal Register Abstract

Nose Gear Actuating System Failure

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_73-19-03.html
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AD Number:
73-19-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Mitsubishi Model MU-2B, MU-2B-10, MU-2B-15, MU-2B-20, and MU-2B-25 Airplanes
Subject:
Nose Gear Actuating System Failure
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/08/1973
Make:
Mitsubishi Heavy Industries, Ltd.
Model:
MU-2B | MU-2B-10 | MU-2B-15 | MU-2B-20 | MU-2B-25
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: 73-19-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1716

AD NUMBER:   73-19-03

SUBJECT HEADING:   Airworthiness Directives; Mitsubishi Model MU-2B, MU-2B-10, MU-2B-15, MU-2B-20, and MU-2B-25 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective October 8, 1973.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   73-19-03 MITSUBISHI HEAVY INDUSTRIES, LTD: Amdt. 39-1716. Applies to Mitsubishi Model MU-2B airplanes (S/N 004, and 006 through 038); MU-2B-10, and -15 airplanes (S/N 101, and 103 through 120); MU-2B-20, and -25 airplanes (S/N 005, 102, and 121 through 271).
Compliance is required as indicated.
To prevent the failure of the nose gear actuating system, accomplish the following:
Within the next 100 hours' time in service after the effective date of this AD, unless already accomplished, modify the nose gear actuating assembly and its supporting structure in accordance with Mitsubishi MU-2 Service Bulletin No. 155, dated June 26, 1972, or an equivalent method approved by the Chief, Engineering and Manufacturing Branch, FAA, Pacific- Asia Region.
This amendment becomes effective October 8, 1973.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_73-19-03.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
73-19-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Mitsubishi Model MU-2B, MU-2B-10, MU-2B-15, MU-2B-20, and MU-2B-25 Airplanes
Subject:
Nose Gear Actuating System Failure
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/08/1973
Make:
Mitsubishi Heavy Industries, Ltd.
Model:
MU-2B | MU-2B-10 | MU-2B-15 | MU-2B-20 | MU-2B-25
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: 73-19-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1716

AD NUMBER:   73-19-03

SUBJECT HEADING:   Airworthiness Directives; Mitsubishi Model MU-2B, MU-2B-10, MU-2B-15, MU-2B-20, and MU-2B-25 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective October 8, 1973.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   73-19-03 MITSUBISHI HEAVY INDUSTRIES, LTD: Amdt. 39-1716. Applies to Mitsubishi Model MU-2B airplanes (S/N 004, and 006 through 038); MU-2B-10, and -15 airplanes (S/N 101, and 103 through 120); MU-2B-20, and -25 airplanes (S/N 005, 102, and 121 through 271).
Compliance is required as indicated.
To prevent the failure of the nose gear actuating system, accomplish the following:
Within the next 100 hours' time in service after the effective date of this AD, unless already accomplished, modify the nose gear actuating assembly and its supporting structure in accordance with Mitsubishi MU-2 Service Bulletin No. 155, dated June 26, 1972, or an equivalent method approved by the Chief, Engineering and Manufacturing Branch, FAA, Pacific- Asia Region.
This amendment becomes effective October 8, 1973.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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