AD 91-03-04

final rule

Airworthiness Directives; BOEING Model 747-400 Series Airplanes

AD Number
91-03-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
90-NM-281-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company 747-400 Series Airworthiness Directives; BOEING Model 747-400 Series Airplanes

Unsafe Condition

Inadvertent reversal of direction of flight due to the flight management system commanding an unanticipated turn to intercept an out-of-sequence waypoint.

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

Required Actions

Install placards on or adjacent to both left and right Control Display Units (CDU) stating 'Use of ABEAM PTS FMC Function Prohibited'. Revise the AFM's Limitations Section, Electronics Subsection, to add 'Do not use the FMC ABEAM PTS Function'.

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, unless previously accomplished

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

Affected Aircraft

All Model 747-400 series airplanes, certificated in any category.

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

Federal Register Abstract

AFM Change

Applicability Source Text

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AD Number:
91-03-04
Document Type:
AD Final Rules
Docket Number:
90-NM-281-AD
Subject Heading:
Airworthiness Directives; BOEING Model 747-400 Series Airplanes
Subject:
AFM Change
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
02/04/1991
Make:
The Boeing Company
Model:
747-400 Series
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Superseded AD: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Superseded By: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:
Updated RGL applicability to match AD applicability; CAR C-11-185
AIRWORTHINESS DIRECTIVES FINAL RULES: 91-03-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   90-NM-281-AD

AMENDMENT:   39-6864

AD NUMBER:   91-03-04

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 747-400 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective February 4, 1991.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
91-03-04 BOEING: Amendment 39-6864. Docket No. 90-NM-281-AD.

Applicability: All Model 747-400 series airplanes, certificated in any category.

Compliance: Required within 30 days after the effective date of this AD, unless previously accomplished.

To prevent inadvertently reversing the direction of flight due to the flight management system commanding an unanticipated turn to intercept an out-of-sequence waypoint, accomplish the following:

A. Install placards on or directly adjacent to both the left and right Control Display Units (CDU), in positions clearly visible to the flight crew, stating: Use of "ABEAM PTS" FMC Function Prohibited.

B. Revise the Limitations Section, Electronics Subsection, of the FAA-approved Airplane Flight Manual (AFM), to add the following statement: "Do not use the FMC ABEAM PTS Function." This may be accomplished by inserting a copy of this AD in the AFM.

C. 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, Seattle Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate.

NOTE: The request should be submitted directly to the Manager, Seattle ACO, and a copy sent to the cognizant FAA Principal Inspector (PI). The PI will then forward comments or concurrence to the Seattle ACO.

D. 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.

This amendment (39-6864, AD 91-03-04) becomes effective on February 4, 1991.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_91-03-04.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
91-03-04
Document Type:
AD Final Rules
Docket Number:
90-NM-281-AD
Subject Heading:
Airworthiness Directives; BOEING Model 747-400 Series Airplanes
Subject:
AFM Change
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
02/04/1991
Make:
The Boeing Company
Model:
747-400 Series
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:
Updated RGL applicability to match AD applicability; CAR C-11-185
AIRWORTHINESS DIRECTIVES FINAL RULES: 91-03-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   90-NM-281-AD

AMENDMENT:   39-6864

AD NUMBER:   91-03-04

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 747-400 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective February 4, 1991.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
91-03-04 BOEING: Amendment 39-6864. Docket No. 90-NM-281-AD.

Applicability: All Model 747-400 series airplanes, certificated in any category.

Compliance: Required within 30 days after the effective date of this AD, unless previously accomplished.

To prevent inadvertently reversing the direction of flight due to the flight management system commanding an unanticipated turn to intercept an out-of-sequence waypoint, accomplish the following:

A. Install placards on or directly adjacent to both the left and right Control Display Units (CDU), in positions clearly visible to the flight crew, stating: Use of "ABEAM PTS" FMC Function Prohibited.

B. Revise the Limitations Section, Electronics Subsection, of the FAA-approved Airplane Flight Manual (AFM), to add the following statement: "Do not use the FMC ABEAM PTS Function." This may be accomplished by inserting a copy of this AD in the AFM.

C. 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, Seattle Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate.

NOTE: The request should be submitted directly to the Manager, Seattle ACO, and a copy sent to the cognizant FAA Principal Inspector (PI). The PI will then forward comments or concurrence to the Seattle ACO.

D. 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.

This amendment (39-6864, AD 91-03-04) becomes effective on February 4, 1991.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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