AD 88-03-04

final rule

Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 Series Airplanes

AD Number
88-03-04
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 A300 B2-1A Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 Series Airplanes
aircraft Airbus A300 B2-1C Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 Series Airplanes
aircraft Airbus A300 B2-203 Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 Series Airplanes
aircraft Airbus A300 B2K-3C Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 Series Airplanes

Unsafe Condition

Collapse of the main landing gear (MLG) due to potential defects in the lower tie rods.

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

Required Actions

Perform an ultrasonic inspection of the MLG lower tie rods in accordance with AI Service Bulletin A300-32-369. Replace defective lower tie rods before further flight. An alternate means of compliance may be used if approved by the FAA.

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

Compliance Time

Prior to each lower tie rod accumulating 7,000 landings or within the next 500 landings, whichever occurs later, and thereafter at intervals not to exceed 1,500 landings.

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

Affected Aircraft

AIRBUS INDUSTRIE Model A300 B2-1A, A300 B2-1C, A300 B2-203, A300 B2K-3C airplanes as listed in AI Service Bulletin A300-32-369 dated December 12, 1986.

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

Federal Register Abstract

Main Landing Gear

Applicability Source Text

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AD Final Rules - DRS_88-03-04.html
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AD Number:
88-03-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 Series Airplanes
Subject:
Main Landing Gear
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
02/28/1988
Make:
Airbus
Model:
A300 B2-1A | A300 B2-1C | A300 B2-203 | A300 B2K-3C
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: 88-03-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5833

AD NUMBER:   88-03-04

SUBJECT HEADING:   Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective February 28, 1988.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
88-03-04 AIRBUS INDUSTRIE: Amendment 39-5833. Applies to Model A300 B2 series airplanes, as listed in Airbus Industrie (AI) Service Bulletin A300-32-369, dated December 12, 1986, certificated in any category. Compliance required as indicated, unless previously accomplished.

To prevent collapse of the main landing gear (MLG), accomplish the following:

A. Prior to each lower tie rod accumulating 7,000 landings or within the next 500 landings, whichever occurs later, and thereafter at intervals not to exceed 1,500 landings, perform an ultrasonic inspection of the MLG lower tie rods, in accordance with AI Service Bulletin A300- 32-369, dated December 12, 1986. Replace defective lower tie rods before further flight.

B. An alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Standardization Branch, ANM-113, FAA, Northwest Mountain Region.

C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD.

All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to Airbus Industrie, Airbus Support Division, Avenue Didier Daurat, 31700 Blagnac, France. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or at the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington.

This amendment becomes effective February 28, 1988.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_88-03-04.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
88-03-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 Series Airplanes
Subject:
Main Landing Gear
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
02/28/1988
Make:
Airbus
Model:
A300 B2-1A | A300 B2-1C | A300 B2-203 | A300 B2K-3C
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: 88-03-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5833

AD NUMBER:   88-03-04

SUBJECT HEADING:   Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective February 28, 1988.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
88-03-04 AIRBUS INDUSTRIE: Amendment 39-5833. Applies to Model A300 B2 series airplanes, as listed in Airbus Industrie (AI) Service Bulletin A300-32-369, dated December 12, 1986, certificated in any category. Compliance required as indicated, unless previously accomplished.

To prevent collapse of the main landing gear (MLG), accomplish the following:

A. Prior to each lower tie rod accumulating 7,000 landings or within the next 500 landings, whichever occurs later, and thereafter at intervals not to exceed 1,500 landings, perform an ultrasonic inspection of the MLG lower tie rods, in accordance with AI Service Bulletin A300- 32-369, dated December 12, 1986. Replace defective lower tie rods before further flight.

B. An alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Standardization Branch, ANM-113, FAA, Northwest Mountain Region.

C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD.

All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to Airbus Industrie, Airbus Support Division, Avenue Didier Daurat, 31700 Blagnac, France. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or at the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington.

This amendment becomes effective February 28, 1988.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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