AD 84-25-04

final rule

BOEING Model 747 Airplanes

AD Number
84-25-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company 747-100 Series BOEING Model 747 Airplanes
aircraft The Boeing Company 747-100B Series BOEING Model 747 Airplanes
aircraft The Boeing Company 747-100B SUD Series BOEING Model 747 Airplanes
aircraft The Boeing Company 747-200B Series BOEING Model 747 Airplanes
aircraft The Boeing Company 747-200C Series BOEING Model 747 Airplanes
aircraft The Boeing Company 747-200F Series BOEING Model 747 Airplanes
aircraft The Boeing Company 747-300 Series BOEING Model 747 Airplanes
aircraft The Boeing Company 747-400 Series BOEING Model 747 Airplanes
aircraft The Boeing Company 747-400D Series BOEING Model 747 Airplanes
aircraft The Boeing Company 747-400F Series BOEING Model 747 Airplanes
aircraft The Boeing Company 747SP Series BOEING Model 747 Airplanes
aircraft The Boeing Company 747SR Series BOEING Model 747 Airplanes

Unsafe Condition

Loss of autopilot battery power due to the absence of a placard on the autopilot P10 mode select panel preventing use of the land mode.

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

Required Actions

Install a placard on the autopilot P10 mode select panel reading 'DO NOT USE THE LAND MODE' within 30 days after the effective date. The placard may be removed after modifying airplane wiring per Boeing Service Bulletin 747-22A2152 or approved alternate means.

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

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

Affected Aircraft

Boeing Model 747 airplanes equipped with Landing Rollout Control Unit automatic landing systems, Boeing P/N 60B00013-757 or 60B00013-759

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

Federal Register Abstract

Autopilot Battery Power

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_84-25-04.html
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AD Number:
84-25-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
BOEING Model 747 Airplanes
Subject:
Autopilot Battery Power
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
01/02/1985
Make:
The Boeing Company
Model:
747-100 Series | 747-100B Series | 747-100B SUD Series | 747-200B Series | 747-200C Series | 747-200...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: 84-25-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4968

AD NUMBER:   84-25-04

SUBJECT HEADING:   BOEING Model 747 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective January 2, 1985.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
84-25-04 BOEING: Amendment 39-4968. Applies to all Boeing Model 747 airplanes equipped with Landing Rollout Control Unit automatic landing systems, Boeing P/N 60B00013-757 or 60B00013-759.

To prevent a hazardous condition due to loss of the autopilot battery power, within 30 days after the effective date of this AD install a placard on the autopilot P10 mode select panel which reads as follows: "DO NOT USE THE LAND MODE," unless already accomplished. The placard may be removed when the airplane wiring has been modified in accordance with Boeing Service Bulletin 747-22A2152, dated November 16, 1984, or later FAA approved revision; or any alternate means of compliance which provides an equivalent level of safety approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region.

All persons affected by this proposal who have not already received the Service Bulletin may obtain copies upon request to Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98168. These documents may also be examined at the FAA, Northwest Mountain Region, 9010 East Marginal Way South, Seattle, Washington.

This amendment becomes effective January 2, 1985.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_84-25-04.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
84-25-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
BOEING Model 747 Airplanes
Subject:
Autopilot Battery Power
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
01/02/1985
Make:
The Boeing Company
Model:
747-100 Series | 747-100B Series | 747-100B SUD Series | 747-200B Series | 747-200C Series | 747-200...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: 84-25-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4968

AD NUMBER:   84-25-04

SUBJECT HEADING:   BOEING Model 747 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective January 2, 1985.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
84-25-04 BOEING: Amendment 39-4968. Applies to all Boeing Model 747 airplanes equipped with Landing Rollout Control Unit automatic landing systems, Boeing P/N 60B00013-757 or 60B00013-759.

To prevent a hazardous condition due to loss of the autopilot battery power, within 30 days after the effective date of this AD install a placard on the autopilot P10 mode select panel which reads as follows: "DO NOT USE THE LAND MODE," unless already accomplished. The placard may be removed when the airplane wiring has been modified in accordance with Boeing Service Bulletin 747-22A2152, dated November 16, 1984, or later FAA approved revision; or any alternate means of compliance which provides an equivalent level of safety approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region.

All persons affected by this proposal who have not already received the Service Bulletin may obtain copies upon request to Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98168. These documents may also be examined at the FAA, Northwest Mountain Region, 9010 East Marginal Way South, Seattle, Washington.

This amendment becomes effective January 2, 1985.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.