AD 91-03-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| 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
Show captured applicability text from the source AD
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Make: The Boeing Company Model: 747-400 Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: Updated RGL applicability to match AD applicability; CAR C-11-185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:
Document Text
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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:
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