AD 75-22-03

final rule

Airworthiness Directives; Hughes Model 369, 369A, 369H, 369HS, 369HE, 369HM

AD Number
75-22-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system

Applicability

TypeManufacturerModelDetails
aircraft MD Helicopters, Inc. 369 Airworthiness Directives; Hughes Model 369, 369A, 369H, 369HS, 369HE, 369HM
aircraft MD Helicopters, Inc. 369A Airworthiness Directives; Hughes Model 369, 369A, 369H, 369HS, 369HE, 369HM
aircraft MD Helicopters, Inc. 369H Airworthiness Directives; Hughes Model 369, 369A, 369H, 369HS, 369HE, 369HM
aircraft MD Helicopters, Inc. 369HE Airworthiness Directives; Hughes Model 369, 369A, 369H, 369HS, 369HE, 369HM
aircraft MD Helicopters, Inc. 369HM Airworthiness Directives; Hughes Model 369, 369A, 369H, 369HS, 369HE, 369HM
aircraft MD Helicopters, Inc. 369HS Airworthiness Directives; Hughes Model 369, 369A, 369H, 369HS, 369HE, 369HM

Unsafe Condition

Failure of the tail rotor drive shaft (Part Number 369A5518) could result in emergency flight situations.

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

Required Actions

Replace drive shaft P/N 369A5518 with P/N 369A5518-601 following Hughes Service Information Notice No. HN-86, Part I, B.3., or equivalent FAA-approved procedures.

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

Compliance Time

within the next 50 hours time in service after the effective date of this AD unless already accomplished

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

Affected Aircraft

Hughes Model 369, 369A, 369H, 369HS, 369HE, 369HM, and military OH-6A and YOH-6A helicopters with tail rotor blades P/N 369A1613 or -3 and tail rotor drive shaft P/N 369A5518.

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

Federal Register Abstract

Tail Rotor Drive Shaft

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_75-22-03.html
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AD Number:
75-22-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Hughes Model 369, 369A, 369H, 369HS, 369HE, 369HM
Subject:
Tail Rotor Drive Shaft
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/24/1975
Make:
MD Helicopters, Inc.
Model:
369 | 369A | 369H | 369HE | 369HM | 369HS
Product Type:
Aircraft
Product Subtype:
Rotorcraft
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 75-22-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2387

AD NUMBER:   75-22-03

SUBJECT HEADING:   Airworthiness Directives; Hughes Model 369, 369A, 369H, 369HS, 369HE, 369HM

ACTION:  

SUMMARY:  

DATES:   Effective October 24, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-22-03 HUGHES HELICOPTERS: Amendment 39-2387. Applies to all Hughes Model 369, 369A, 369H, 369HS, 369HE, 369HM, certificated in all categories and military OH- 6A and YOH-6A helicopters incorporating metal tail rotor blades Part Number 369A1613, or -3, in combination with tail rotor drive shaft, Part Number 369A5518.

Compliance required within the next 50 hours time in service, after the effective date of this AD unless already accomplished.

(a) To prevent possible emergency flight situations resulting from failure of the tail rotor drive shaft, replace drive shaft P/N 369A5518 with drive shaft P/N 369A5518-601 in accordance with Part I, B.3. of Hughes Service Information Notice No. HN-86, dated April 28, 1975, or later FAA-approved revisions.

(b) Aircraft may be flown in accordance with FAR 21.197 to a base for the performance of the maintenance described herein.

(c) Equivalent modification procedures may be approved by the Chief, Aircraft Engineering Division, FAA Western Region.

NOTE: Assure that the record to reflect compliance with this AD is made in aircraft records in accordance with FAR's 91.165 and 91.173.

This amendment becomes effective October 24, 1975.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_75-22-03.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
75-22-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Hughes Model 369, 369A, 369H, 369HS, 369HE, 369HM
Subject:
Tail Rotor Drive Shaft
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/24/1975
Make:
MD Helicopters, Inc.
Model:
369 | 369A | 369H | 369HE | 369HM | 369HS
Product Type:
Aircraft
Product Subtype:
Rotorcraft
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 75-22-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2387

AD NUMBER:   75-22-03

SUBJECT HEADING:   Airworthiness Directives; Hughes Model 369, 369A, 369H, 369HS, 369HE, 369HM

ACTION:  

SUMMARY:  

DATES:   Effective October 24, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-22-03 HUGHES HELICOPTERS: Amendment 39-2387. Applies to all Hughes Model 369, 369A, 369H, 369HS, 369HE, 369HM, certificated in all categories and military OH- 6A and YOH-6A helicopters incorporating metal tail rotor blades Part Number 369A1613, or -3, in combination with tail rotor drive shaft, Part Number 369A5518.

Compliance required within the next 50 hours time in service, after the effective date of this AD unless already accomplished.

(a) To prevent possible emergency flight situations resulting from failure of the tail rotor drive shaft, replace drive shaft P/N 369A5518 with drive shaft P/N 369A5518-601 in accordance with Part I, B.3. of Hughes Service Information Notice No. HN-86, dated April 28, 1975, or later FAA-approved revisions.

(b) Aircraft may be flown in accordance with FAR 21.197 to a base for the performance of the maintenance described herein.

(c) Equivalent modification procedures may be approved by the Chief, Aircraft Engineering Division, FAA Western Region.

NOTE: Assure that the record to reflect compliance with this AD is made in aircraft records in accordance with FAR's 91.165 and 91.173.

This amendment becomes effective October 24, 1975.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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