AD 90-03-12

final rule

Airworthiness Directives; BOEING Model 747 Series Airplanes

AD Number
90-03-12
Status
final_rule
Effective Date
Product Category
aircraft
Docket
89-NM-180-AD
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

Empennage control cables may snag on the cable shroud brackets above the Door 5 crew rest area.

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

Required Actions

Install control cable block plates in accordance with Boeing Service Bulletin 747-25-2776. Alternate means of compliance or adjustments may be approved by the Manager, Seattle Aircraft Certification Office.

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

Compliance Time

within the next 12 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

Boeing Model 747 series airplanes with a door 5 crew rest area listed in Boeing Service Bulletin 747-25-2776 dated June 8, 1989

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

Federal Register Abstract

Control Cable Block Plates

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_90-03-12.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
90-03-12
Document Type:
AD Final Rules
Docket Number:
89-NM-180-AD
Subject Heading:
Airworthiness Directives; BOEING Model 747 Series Airplanes
Subject:
Control Cable Block Plates
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/05/1990
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: 90-03-12
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   89-NM-180-AD

AMENDMENT:   39-6495

AD NUMBER:   90-03-12

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 747 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective March 5, 1990.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
90-03-12 BOEING: Amendment 39-6495. Docket No. 89-NM-180-AD.

Applicability: Model 747 series airplanes with a door 5 crew rest area, listed in Boeing Service Bulletin 747-25-2776, dated June 8, 1989, certificated in any category.

Compliance: Required within the next 12 months after the effective date of this AD, unless previously accomplished.

To prevent empennage control cables from snagging on the cable shroud brackets above the Door 5 crew rest area, accomplish the following:

A. Install control cable block plates in accordance with Boeing Service Bulletin 747-25- 2776, dated June 8, 1989.

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. NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who will either concur or comment and then send it to the Manager, Seattle Aircraft Certification Office.

C. 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. All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington.

This amendment (39-6495, AD 90-03-12) becomes effective on March 5, 1990.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_90-03-12.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
90-03-12
Document Type:
AD Final Rules
Docket Number:
89-NM-180-AD
Subject Heading:
Airworthiness Directives; BOEING Model 747 Series Airplanes
Subject:
Control Cable Block Plates
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/05/1990
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: 90-03-12
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   89-NM-180-AD

AMENDMENT:   39-6495

AD NUMBER:   90-03-12

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 747 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective March 5, 1990.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
90-03-12 BOEING: Amendment 39-6495. Docket No. 89-NM-180-AD.

Applicability: Model 747 series airplanes with a door 5 crew rest area, listed in Boeing Service Bulletin 747-25-2776, dated June 8, 1989, certificated in any category.

Compliance: Required within the next 12 months after the effective date of this AD, unless previously accomplished.

To prevent empennage control cables from snagging on the cable shroud brackets above the Door 5 crew rest area, accomplish the following:

A. Install control cable block plates in accordance with Boeing Service Bulletin 747-25- 2776, dated June 8, 1989.

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. NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who will either concur or comment and then send it to the Manager, Seattle Aircraft Certification Office.

C. 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. All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington.

This amendment (39-6495, AD 90-03-12) becomes effective on March 5, 1990.

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.