AD 87-12-04

final rule

Airworthiness Directives; BOEING Model 747 Series Airplanes

AD Number
87-12-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

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

Unsafe Condition

Loss of all four hydraulic systems in the event of severe damage to or loss of the vertical stabilizer.

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

Required Actions

Install a hydraulic fuse in the number 4 hydraulic system in accordance with Boeing Service Bulletin 747-29-2063 or later FAA-approved revision. An alternate means of compliance or adjustment of compliance time may be approved by the Manager, Seattle Aircraft Certification Office. Special flight permits may be issued under FAR 21.197 and 21.199 to operate to a base for modification.

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

Compliance Time

Within the next 24 months after the effective date of this AD

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

Affected Aircraft

Model 747 series airplanes listed in Boeing Service Bulletin 747-29-2063, dated December 23, 1986, certificated in any category.

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

Federal Register Abstract

Hydraulic System

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_87-12-04.html
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AD Number:
87-12-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BOEING Model 747 Series Airplanes
Subject:
Hydraulic System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/13/1987
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: 87-12-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5635

AD NUMBER:   87-12-04

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 747 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective July 13, 1987.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
87-12-04 BOEING: Amendment 39-5635. Applies to Model 747 series airplanes, listed in Boeing Service Bulletin 747-29-2063, dated December 23, 1986, certificated in any category. Compliance required as indicated, unless previously accomplished.

To prevent the loss of all four hydraulic systems in the event of severe damage to or loss of the vertical stabilizer, accomplish the following:

A. Within the next 24 months after the effective date of this AD, modify the number 4 hydraulic system by installing a hydraulic fuse in accordance with Boeing Service Bulletin 747- 29-2063, dated December 23, 1986, or later FAA-approved revision.

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, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region.

C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for accomplishment of the modification required by 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 the Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124-2207. These documents may be examined at FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington.

This amendment becomes effective July 13, 1987.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_87-12-04.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
87-12-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BOEING Model 747 Series Airplanes
Subject:
Hydraulic System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/13/1987
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: 87-12-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5635

AD NUMBER:   87-12-04

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 747 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective July 13, 1987.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
87-12-04 BOEING: Amendment 39-5635. Applies to Model 747 series airplanes, listed in Boeing Service Bulletin 747-29-2063, dated December 23, 1986, certificated in any category. Compliance required as indicated, unless previously accomplished.

To prevent the loss of all four hydraulic systems in the event of severe damage to or loss of the vertical stabilizer, accomplish the following:

A. Within the next 24 months after the effective date of this AD, modify the number 4 hydraulic system by installing a hydraulic fuse in accordance with Boeing Service Bulletin 747- 29-2063, dated December 23, 1986, or later FAA-approved revision.

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, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region.

C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for accomplishment of the modification required by 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 the Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124-2207. These documents may be examined at FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington.

This amendment becomes effective July 13, 1987.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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