AD 75-04-06

final rule

BOEING Model 747 Airplanes

AD Number
75-04-06
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 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

Erroneous information being displayed on flight instruments due to inadequate vertical rise in pitot-static tubing inboard of each pitot-static probe.

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

Required Actions

Modify the pitot-static tubing to include a vertical rise just inboard of each pitot-static probe by following Work Package 1, 2, and 3 of Boeing Service Bulletin 747-34-2058 or later FAA approved revisions, or an approved alternative method.

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

Compliance Time

Within the next 3,500 hours time in service after the effective date of this AD

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

Affected Aircraft

All Model 747 airplanes certificated in all categories listed in Boeing Service Bulletin 747-34-2058 dated January 31, 1974, or later FAA approved revisions.

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

Federal Register Abstract

Flight Instruments

Applicability Source Text

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AD Final Rules - DRS_75-04-06.html
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AD Number:
75-04-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
BOEING Model 747 Airplanes
Subject:
Flight Instruments
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/10/1975
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: 75-04-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2086

AD NUMBER:   75-04-06

SUBJECT HEADING:   BOEING Model 747 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective March 10, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-04-06 BOEING: Amendment 39-2086. Applies to all Model 747 airplanes, certificated in all categories, listed in Boeing Service Bulletin 747-34-2058 dated January 31, 1974, or later FAA approved revisions. To prevent erroneous information from being displayed on flight instruments:
Within the next 3,500 hours time in service after the effective date of this AD, modify the pitot-static tubing to include a vertical rise just inboard of each pitot-static probe in accordance with Work Package 1, 2, and 3 of Boeing Service Bulletin 747-34-2058, dated January 31, 1974, or later FAA approved revisions, or in a manner approved by the Chief, Engineering and Manufacturing Branch, FAA Northwest Region.
The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1).
All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to the Boeing Commercial Airplane Company, P. O. Box 3707, Seattle, Washington 98124. The documents may be examined at FAA Northwest Region, 9010 East Marginal Way, Seattle, Washington 98108.
This amendment becomes effective March 10, 1975.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_75-04-06.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
75-04-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
BOEING Model 747 Airplanes
Subject:
Flight Instruments
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/10/1975
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: 75-04-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2086

AD NUMBER:   75-04-06

SUBJECT HEADING:   BOEING Model 747 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective March 10, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-04-06 BOEING: Amendment 39-2086. Applies to all Model 747 airplanes, certificated in all categories, listed in Boeing Service Bulletin 747-34-2058 dated January 31, 1974, or later FAA approved revisions. To prevent erroneous information from being displayed on flight instruments:
Within the next 3,500 hours time in service after the effective date of this AD, modify the pitot-static tubing to include a vertical rise just inboard of each pitot-static probe in accordance with Work Package 1, 2, and 3 of Boeing Service Bulletin 747-34-2058, dated January 31, 1974, or later FAA approved revisions, or in a manner approved by the Chief, Engineering and Manufacturing Branch, FAA Northwest Region.
The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1).
All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to the Boeing Commercial Airplane Company, P. O. Box 3707, Seattle, Washington 98124. The documents may be examined at FAA Northwest Region, 9010 East Marginal Way, Seattle, Washington 98108.
This amendment becomes effective March 10, 1975.

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.