AD 77-22-04

final rule

Airworthiness Directives; Societe Nationale Industrielle Aerospatiale (S.N.I.A.S.) Models SA341G "Gazelle" Helicopters

AD Number
77-22-04
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 (S.N.I.A.S.) Models SA341G "Gazelle" Helicopters

Unsafe Condition

Excessive corrosion in landing gear members could lead to structural failure of the landing gear.

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

Required Actions

Remove the landing gear, inspect for corrosion, replace or turn 180 degrees as necessary, and reinstall in accordance with Service Bulletin No. 01.10 and Repair Manual.

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

Compliance Time

within the next 500 hours time in service after the effective date of this AD, but not later than January 31, 1978

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

Affected Aircraft

Models SA341G 'Gazelle' helicopters equipped with specific landing gear part numbers and modifications: Low-skid P/Ns 341A.41.5200.00 to .04 without Mod. AMS 07.1349/S.371, P/Ns 341A.41.5200.05 to .11 with Mod. AMS 07.1349 but without Mod. AMS 07.1578/S.440; High-skid P/N 341A.41.5300.00 without Mod. AMS 07.1350, P/Ns 341A.41.5300.01 to .11 with Mod. AMS 07.1350 but without Mod. AMS 07.1579.

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

Federal Register Abstract

Landing Gear

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_77-22-04.html
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AD Number:
77-22-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Societe Nationale Industrielle Aerospatiale (S.N.I.A.S.) Models SA341G "Ga...Show more
Subject:
Landing Gear
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/28/1977
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Superseded AD: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Superseded By: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: 77-22-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3068

AD NUMBER:   77-22-04

SUBJECT HEADING:   Airworthiness Directives; Societe Nationale Industrielle Aerospatiale (S.N.I.A.S.) Models SA341G "Gazelle" Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective November 28, 1977.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
77-22-04 SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE (S.N.I.A.S.): Amendment 39-3068. Applies to Models SA341G "Gazelle" helicopters, certificated in all categories, equipped with any of the following landing gear:

Low-skid, low-frequency landing gear
P/Ns 341A.41.5200.00 to .04 not incorporating Mod. AMS 07.1349/S.371. P/Ns 341A.41.5200.05 to .11 incorporating Mod. AMS 07.1349 but not incorporating Mod. AMS 07.1578/S.440.

High-skid, low-frequency landing gear
P/N 341A.41.5300.00 not incorporating Mod. AMS 07.1350. P/Ns 341A.41.5300.01 to .11 incorporating Mod. AMS 07.1350 but not incorporating Mod. AMS 07.1579.

Compliance is required within the next 500 hours time in service after the effective date of this AD, but not later than January 31, 1978, unless already accomplished.

To prevent possible excessive corrosion remove the landing gear, inspect for corrosion, and if corrosion is found, replace, or turn 180 degrees and thereafter replace, the landing gear members, as necessary and reinstall all in accordance with Paragraph C of "Gazelle" Service Bulletin No. 01.10 dated September 12, 1975, revised December 13, 1976 and the Models SA341G "Gazelle" Repair Manual or an FAA approved equivalent.

This Amendment becomes effective November 28, 1977.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_77-22-04.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
77-22-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Societe Nationale Industrielle Aerospatiale (S.N.I.A.S.) Models SA341G "Ga...Show more
Subject:
Landing Gear
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/28/1977
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: 77-22-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3068

AD NUMBER:   77-22-04

SUBJECT HEADING:   Airworthiness Directives; Societe Nationale Industrielle Aerospatiale (S.N.I.A.S.) Models SA341G "Gazelle" Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective November 28, 1977.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
77-22-04 SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE (S.N.I.A.S.): Amendment 39-3068. Applies to Models SA341G "Gazelle" helicopters, certificated in all categories, equipped with any of the following landing gear:

Low-skid, low-frequency landing gear
P/Ns 341A.41.5200.00 to .04 not incorporating Mod. AMS 07.1349/S.371. P/Ns 341A.41.5200.05 to .11 incorporating Mod. AMS 07.1349 but not incorporating Mod. AMS 07.1578/S.440.

High-skid, low-frequency landing gear
P/N 341A.41.5300.00 not incorporating Mod. AMS 07.1350. P/Ns 341A.41.5300.01 to .11 incorporating Mod. AMS 07.1350 but not incorporating Mod. AMS 07.1579.

Compliance is required within the next 500 hours time in service after the effective date of this AD, but not later than January 31, 1978, unless already accomplished.

To prevent possible excessive corrosion remove the landing gear, inspect for corrosion, and if corrosion is found, replace, or turn 180 degrees and thereafter replace, the landing gear members, as necessary and reinstall all in accordance with Paragraph C of "Gazelle" Service Bulletin No. 01.10 dated September 12, 1975, revised December 13, 1976 and the Models SA341G "Gazelle" Repair Manual or an FAA approved equivalent.

This Amendment becomes effective November 28, 1977.

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.