AD 76-02-03

final rule

Airworthiness Directives; Societe Nationale Industrielle Aerospatiale Model SA341G Helicopters

AD Number
76-02-03
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 Airbus Helicopters SA341G Airworthiness Directives; Societe Nationale Industrielle Aerospatiale Model SA341G Helicopters

Unsafe Condition

Abnormal wear of main gear box oil pump hydraulic unit drive gear splines

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

Required Actions

Inspect the main gear box oil pump hydraulic unit drive gear splines in accordance with Service Bulletin No. 05.09a, replace the drive gear, oil pump or both as necessary, or return to service per the criteria in the service bulletin. Additionally, lubricate the splines as per the same service bulletin.

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

Compliance Time

Prior to the accumulation of 600 hours' total time in service or within the next 10 hours' time in service after the effective date of this AD, whichever occurs later, unless already accomplished within the last 590 hours' time in service, and thereafter at intervals not to exceed 600 hours' time in service from the last inspection for inspections. For lubrication, compliance is required prior to the accumulation of 600 hours' time in service or within the next 10 hours' time in service after the effective date, whichever occurs later, unless already accomplished within the last 190 hours' time in service, and thereafter at intervals not to exceed 200 hours' time in service from the last lubrication.

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

Affected Aircraft

Societe Nationale Industrielle Aerospatiale Model SA341G 'Gazelle' helicopters, certificated in all categories.

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

Federal Register Abstract

Hydraulic Unit Drive

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_76-02-03.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
76-02-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Societe Nationale Industrielle Aerospatiale Model SA341G Helicopters
Subject:
Hydraulic Unit Drive
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
01/30/1976
Make:
Airbus Helicopters
Model:
SA341G
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: 76-02-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2496

AD NUMBER:   76-02-03

SUBJECT HEADING:   Airworthiness Directives; Societe Nationale Industrielle Aerospatiale Model SA341G Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective January 30, 1976

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
76-02-03 SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE: Amendment 39- 2496. Applies to Model SA341G "Gazelle" helicopters, certificated in all categories.

Compliance is required as indicated.

To prevent abnormal wear of main gear box oil pump hydraulic unit drive gear splines, accomplish the following:

(a) Prior to the accumulation of 600 hours' total time in service or within the next 10 hours' time in service after the effective date of this AD, whichever occurs later, unless already accomplished within the last 590 hours' time in service, and thereafter at intervals not to exceed 600 hours' time in service from the last inspection, comply with paragraph (b) of this AD.

(b) Inspect the main gear box (MGB) oil pump hydraulic unit drive gear splines in accordance with subparagraphs 1C(1) and 1C(2), and replace the drive gear, oil pump or both, as necessary, or return to service in accordance with the criteria set forth in subparagraph 1C(3), of Gazelle Service Bulletin No. 05.09a, dated March 10, 1975, or an equivalent approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa, and Middle East Region, c/o American Embassy, APO New York, N.Y. 09667.

(c) Prior to the accumulation of 600 hours' time in service or within the next 10 hours' time in service after the effective date of this AD, whichever occurs later, unless already accomplished within the last 190 hours' time in service, and thereafter at intervals not to exceed 200 hours' time in service from the last lubrication, comply with paragraph (d) of this AD.

(d) Lubricate the splines in accordance with subparagraph 1C(4) of Gazelle Service Bulletin No. 05.09a, dated March 10, 1975, or an equivalent approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa, and Middle East Region, c/o American Embassy, APO New York, N.Y. 09667.

This amendment becomes effective January 30, 1976.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_76-02-03.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
76-02-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Societe Nationale Industrielle Aerospatiale Model SA341G Helicopters
Subject:
Hydraulic Unit Drive
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
01/30/1976
Make:
Airbus Helicopters
Model:
SA341G
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: 76-02-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2496

AD NUMBER:   76-02-03

SUBJECT HEADING:   Airworthiness Directives; Societe Nationale Industrielle Aerospatiale Model SA341G Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective January 30, 1976

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
76-02-03 SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE: Amendment 39- 2496. Applies to Model SA341G "Gazelle" helicopters, certificated in all categories.

Compliance is required as indicated.

To prevent abnormal wear of main gear box oil pump hydraulic unit drive gear splines, accomplish the following:

(a) Prior to the accumulation of 600 hours' total time in service or within the next 10 hours' time in service after the effective date of this AD, whichever occurs later, unless already accomplished within the last 590 hours' time in service, and thereafter at intervals not to exceed 600 hours' time in service from the last inspection, comply with paragraph (b) of this AD.

(b) Inspect the main gear box (MGB) oil pump hydraulic unit drive gear splines in accordance with subparagraphs 1C(1) and 1C(2), and replace the drive gear, oil pump or both, as necessary, or return to service in accordance with the criteria set forth in subparagraph 1C(3), of Gazelle Service Bulletin No. 05.09a, dated March 10, 1975, or an equivalent approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa, and Middle East Region, c/o American Embassy, APO New York, N.Y. 09667.

(c) Prior to the accumulation of 600 hours' time in service or within the next 10 hours' time in service after the effective date of this AD, whichever occurs later, unless already accomplished within the last 190 hours' time in service, and thereafter at intervals not to exceed 200 hours' time in service from the last lubrication, comply with paragraph (d) of this AD.

(d) Lubricate the splines in accordance with subparagraph 1C(4) of Gazelle Service Bulletin No. 05.09a, dated March 10, 1975, or an equivalent approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa, and Middle East Region, c/o American Embassy, APO New York, N.Y. 09667.

This amendment becomes effective January 30, 1976.

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.