AD 90-02-15

final rule

Airworthiness Directives; Airbus Industrie Model A320 Series Airplanes

AD Number
90-02-15
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Airbus A320-111 Airworthiness Directives; Airbus Industrie Model A320 Series Airplanes
aircraft Airbus A320-211 Airworthiness Directives; Airbus Industrie Model A320 Series Airplanes
aircraft Airbus A320-212 Airworthiness Directives; Airbus Industrie Model A320 Series Airplanes
aircraft Airbus A320-214 Airworthiness Directives; Airbus Industrie Model A320 Series Airplanes
aircraft Airbus A320-231 Airworthiness Directives; Airbus Industrie Model A320 Series Airplanes
aircraft Airbus A320-232 Airworthiness Directives; Airbus Industrie Model A320 Series Airplanes
aircraft Airbus A320-233 Airworthiness Directives; Airbus Industrie Model A320 Series Airplanes

Unsafe Condition

Possible false electronic centralized aircraft monitor (ECAM) messages on Auxiliary Power Unit (APU) shutdown due to standby transformer/rectifier (TR) not being identical to the main TR and located in a position with insufficient ventilation.

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

Required Actions

Replace the standby transformer/rectifier (TR) with one identical to the main TR and relocate it to a position with improved ventilation per Airbus Service Bulletin A320-24-1028. Alternate compliance may be approved by the FAA Manager, Standardization Branch, ANM-113.

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

Compliance Time

within 60 days after the effective date of this AD, unless previously accomplished

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

Affected Aircraft

Airbus Model A320 series airplanes, Serial Numbers 005 through 039, and 042 through 049, certificated in any category.

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

Federal Register Abstract

Auxiliary Power Unit

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_90-02-15.html
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AD Number:
90-02-15
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Airbus Industrie Model A320 Series Airplanes
Subject:
Auxiliary Power Unit
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
02/20/1990
Make:
Airbus
Model:
A320-111 | A320-211 | A320-212 | A320-214 | A320-231 | A320-232 | A320-233
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: 90-02-15
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-6477

AD NUMBER:   90-02-15

SUBJECT HEADING:   Airworthiness Directives; Airbus Industrie Model A320 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective on February 20, 1990.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
90-02-15 AIRBUS INDUSTRIE: Amendment 39-6477.

Applicability: Model A320 series airplanes, Serial Numbers 005 through 039, and 042 through 049, certificated in any category.

Compliance: Required within 60 days after the effective date of this AD, unless previously accomplished.

To prevent possible false electronic centralized aircraft monitor (ECAM) messages on Auxiliary Power Unit (APU) shutdown, accomplish the following:

A. Replace the standby transformer/rectifier (TR) with one identical to the main TR, and relocate it to a position with improved ventilation, in accordance with Airbus Industrie Service Bulletin No. A320-24-1028, dated July 7, 1989.

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.

NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who will either concur or comment and then send it to the Manager, Standardization Branch, ANM-113.

C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of 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, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or the Standardization Branch, 9010 East Marginal Way South, Seattle, Washington.

This amendment (39-6477, AD 90-02-15) becomes effective on February 20, 1990.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_90-02-15.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
90-02-15
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Airbus Industrie Model A320 Series Airplanes
Subject:
Auxiliary Power Unit
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
02/20/1990
Make:
Airbus
Model:
A320-111 | A320-211 | A320-212 | A320-214 | A320-231 | A320-232 | A320-233
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: 90-02-15
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-6477

AD NUMBER:   90-02-15

SUBJECT HEADING:   Airworthiness Directives; Airbus Industrie Model A320 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective on February 20, 1990.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
90-02-15 AIRBUS INDUSTRIE: Amendment 39-6477.

Applicability: Model A320 series airplanes, Serial Numbers 005 through 039, and 042 through 049, certificated in any category.

Compliance: Required within 60 days after the effective date of this AD, unless previously accomplished.

To prevent possible false electronic centralized aircraft monitor (ECAM) messages on Auxiliary Power Unit (APU) shutdown, accomplish the following:

A. Replace the standby transformer/rectifier (TR) with one identical to the main TR, and relocate it to a position with improved ventilation, in accordance with Airbus Industrie Service Bulletin No. A320-24-1028, dated July 7, 1989.

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.

NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who will either concur or comment and then send it to the Manager, Standardization Branch, ANM-113.

C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of 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, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or the Standardization Branch, 9010 East Marginal Way South, Seattle, Washington.

This amendment (39-6477, AD 90-02-15) becomes effective on February 20, 1990.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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