AD 92-25-12

final rule

Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes

AD Number
92-25-12
Status
final_rule
Effective Date
Product Category
aircraft
Docket
92-NM-150-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Airbus A300 B2-1A Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B2-1C Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B2-203 Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B2K-3C Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B4-103 Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B4-203 Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B4-2C Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B4-601 Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B4-603 Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B4-605R Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B4-620 Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B4-622R Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes
aircraft Airbus A300 F4-605R Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes
aircraft Airbus A300 F4-622R Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes
aircraft Airbus A310-203 Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes
aircraft Airbus A310-221 Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes
aircraft Airbus A310-222 Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes
aircraft Airbus A310-304 Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes
aircraft Airbus A310-322 Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes
aircraft Airbus A310-324 Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes
aircraft Airbus A310-325 Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes

Unsafe Condition

Overrunning the available runway length during a rejected takeoff (RTO) due to inadequate accelerate stop distance data in the Airplane Flight Manual (AFM).

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

Required Actions

Revise the Limitations Section of the FAA-approved AFM to update accelerate stop distance data using specified temporary revisions. Submit requests for alternative compliance methods through an FAA Principal Maintenance Inspector.

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

Compliance Time

Within 30 days after the effective date of this AD (January 12, 1993).

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

Affected Aircraft

Airbus Model A300 B2, A300 B4, A310, and A300-600 series airplanes equipped with Messier Bugatti carbon brakes.

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

Federal Register Abstract

AFM Revision-Carbon Brakes

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_92-25-12.html
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AD Number:
92-25-12
Document Type:
AD Final Rules
Docket Number:
92-NM-150-AD
Subject Heading:
Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes
Subject:
AFM Revision-Carbon Brakes
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
01/12/1993
Make:
Airbus
Model:
A300 B2-1A | A300 B2-1C | A300 B2-203 | A300 B2K-3C | A300 B4-103 | A300 B4-203 | A300 B4-2C | A300 ...Show more
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: 92-25-12
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   92-NM-150-AD

AMENDMENT:   39-8426

AD NUMBER:   92-25-12

SUBJECT HEADING:   Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective January 12, 1993.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
92-25-12 AIRBUS INDUSTRIE: Amendment 39-8426. Docket No. 92-NM-150-AD.

Applicability: Model A300 B2, A300 B4, A310, and A300-600 series airplanes; equipped with Messier Bugatti carbon brakes; certificated in any category.

Compliance: Required as indicated, unless accomplished previously.

To prevent overrunning the available runway length during a rejected takeoff (RTO), accomplish the following:

(a) Within 30 days after the effective date of this AD, revise the Limitations Section of the FAA-approved Airplane Flight Manual (AFM) to change the data concerning the accelerate stop distance to be used during a RTO, in accordance with either Model A300 AFM Temporary Revision 5.02.00/1, dated December 4, 1991; Model A310 AFM Temporary Revision 5.04.00/3, dated February 13, 1992; Model A310 AFM Temporary Revision 5.04.00/1, dated October 22, 1991; Model A310 AFM Temporary Revision 5.04.00/4, dated March 6, 1992; Model A300-600 AFM Temporary Revision 5.04.00/1, dated November 4, 1991; or Model A300-600 AFM Temporary Revision 5.04.00/2, dated December 4, 1991; as applicable.

(b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Standardization Branch, ANM-113, FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Standardization Branch, ANM-113.

NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Standardization Branch, ANM-113.

(c) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished.

(d) The AFM revision shall be done in accordance with Model A300 AFM Temporary Revision 5.02.00/1, dated December 4, 1991; Model A310 AFM Temporary Revision 5.04.00/3, dated February 13, 1992; Model A310 AFM Temporary Revision 5.04.00/1, dated October 22, 1991; Model A310 AFM Temporary Revision 5.04.00/4, dated March 6, 1992; Model A300-600 AFM Temporary Revision 5.04.00/1, dated November 4, 1991; or Model A300-600 AFM Temporary Revision 5.04.00/2, dated December 4, 1991; as applicable. (NOTE: The issue date of the AFM Temporary Revisions are indicated only on "page 1"; no other pages of these documents are dated.) This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from Airbus Industrie, Airbus Support Division, Avenue Didier Daurat, 31700, Blagnac, France. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC.

(e) This amendment becomes effective on January 12, 1993.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_92-25-12.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
92-25-12
Document Type:
AD Final Rules
Docket Number:
92-NM-150-AD
Subject Heading:
Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes
Subject:
AFM Revision-Carbon Brakes
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
01/12/1993
Make:
Airbus
Model:
A300 B2-1A | A300 B2-1C | A300 B2-203 | A300 B2K-3C | A300 B4-103 | A300 B4-203 | A300 B4-2C | A300 ...Show more
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: 92-25-12
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   92-NM-150-AD

AMENDMENT:   39-8426

AD NUMBER:   92-25-12

SUBJECT HEADING:   Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2, A300 B4, A310, and A300-600 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective January 12, 1993.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
92-25-12 AIRBUS INDUSTRIE: Amendment 39-8426. Docket No. 92-NM-150-AD.

Applicability: Model A300 B2, A300 B4, A310, and A300-600 series airplanes; equipped with Messier Bugatti carbon brakes; certificated in any category.

Compliance: Required as indicated, unless accomplished previously.

To prevent overrunning the available runway length during a rejected takeoff (RTO), accomplish the following:

(a) Within 30 days after the effective date of this AD, revise the Limitations Section of the FAA-approved Airplane Flight Manual (AFM) to change the data concerning the accelerate stop distance to be used during a RTO, in accordance with either Model A300 AFM Temporary Revision 5.02.00/1, dated December 4, 1991; Model A310 AFM Temporary Revision 5.04.00/3, dated February 13, 1992; Model A310 AFM Temporary Revision 5.04.00/1, dated October 22, 1991; Model A310 AFM Temporary Revision 5.04.00/4, dated March 6, 1992; Model A300-600 AFM Temporary Revision 5.04.00/1, dated November 4, 1991; or Model A300-600 AFM Temporary Revision 5.04.00/2, dated December 4, 1991; as applicable.

(b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Standardization Branch, ANM-113, FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Standardization Branch, ANM-113.

NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Standardization Branch, ANM-113.

(c) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished.

(d) The AFM revision shall be done in accordance with Model A300 AFM Temporary Revision 5.02.00/1, dated December 4, 1991; Model A310 AFM Temporary Revision 5.04.00/3, dated February 13, 1992; Model A310 AFM Temporary Revision 5.04.00/1, dated October 22, 1991; Model A310 AFM Temporary Revision 5.04.00/4, dated March 6, 1992; Model A300-600 AFM Temporary Revision 5.04.00/1, dated November 4, 1991; or Model A300-600 AFM Temporary Revision 5.04.00/2, dated December 4, 1991; as applicable. (NOTE: The issue date of the AFM Temporary Revisions are indicated only on "page 1"; no other pages of these documents are dated.) This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from Airbus Industrie, Airbus Support Division, Avenue Didier Daurat, 31700, Blagnac, France. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC.

(e) This amendment becomes effective on January 12, 1993.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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