AD 59-16-05

final rule

BOEING 707-100 series aircraft

AD Number
59-16-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company 707-100 Long Body BOEING 707-100 series aircraft
aircraft The Boeing Company 707-100B Long Body BOEING 707-100 series aircraft
aircraft The Boeing Company 707-100B Short Body BOEING 707-100 series aircraft

Unsafe Condition

Complete loss of fluid during service operation of the utility hydraulic system, primarily due to failure of engine driven hydraulic pump.

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

Required Actions

Install new pump Vickers No. AS-61689-L-2E in place of AS-61689-L-2B or -2C, or install pump external by-pass valve No. A-90073-Y6 with the -2B or -2C pump and replace shaft seal on each hydraulic pump. Install return line filter.

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

Compliance Time

not later than August 21, 1959

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

Affected Aircraft

Boeing 707-100 series aircraft with serial numbers: Model 707-121 (17586-17591), Model 707-124 (17609), Model 707-123 (17628-17643), Model 707-131 (17659-17672), Model VC-137A (17925-17927)

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

Federal Register Abstract

Utility Hydraulic System

Applicability Source Text

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AD Final Rules - DRS_59-16-05.html
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Details
AD Number:
59-16-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
BOEING 707-100 series aircraft
Subject:
Utility Hydraulic System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
The Boeing Company
Model:
707-100 Long Body | 707-100B Long Body | 707-100B Short Body
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Superseded AD: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Superseded By: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: 59-16-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   59-16-05

SUBJECT HEADING:   BOEING 707-100 series aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   59-16-05 BOEING: Applies to 707-100 series aircraft with the following serial numbers: Model 707-121 serial numbers 17586 through 17591, Model 707-124 serial number 17609, Model 707-123 serial numbers 17628 through 17643, Model 707-131 serial numbers 17659 through 17672, Model VC-137A serial numbers 17925 through 17927.
Compliance required not later than August 21, 1959.
As a result of complete loss of fluid during service operation of the utility hydraulic system, primarily due to failure of engine driven hydraulic pump the following must be accomplished:
(a) Install new pump, Vickers No. AS-61689-L-2E, in place of the AS-61689-L-2B or - 2C, or install pump external by-pass valve No. A-90073-Y6 with the -2B or -2C pump. If the pump external by-pass valve is installed the shaft seal on each hydraulic pump must be replaced at the same time.
(b) Install return line filter.
Boeing Service Bulletin No. 379 and Vickers Service Letter dated June 17, 1959, pertain to item (a). Boeing Service Bulletins Nos. 69 and 213 pertain to item (b).



FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_59-16-05.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
59-16-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
BOEING 707-100 series aircraft
Subject:
Utility Hydraulic System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
The Boeing Company
Model:
707-100 Long Body | 707-100B Long Body | 707-100B Short Body
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: 59-16-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   59-16-05

SUBJECT HEADING:   BOEING 707-100 series aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   59-16-05 BOEING: Applies to 707-100 series aircraft with the following serial numbers: Model 707-121 serial numbers 17586 through 17591, Model 707-124 serial number 17609, Model 707-123 serial numbers 17628 through 17643, Model 707-131 serial numbers 17659 through 17672, Model VC-137A serial numbers 17925 through 17927.
Compliance required not later than August 21, 1959.
As a result of complete loss of fluid during service operation of the utility hydraulic system, primarily due to failure of engine driven hydraulic pump the following must be accomplished:
(a) Install new pump, Vickers No. AS-61689-L-2E, in place of the AS-61689-L-2B or - 2C, or install pump external by-pass valve No. A-90073-Y6 with the -2B or -2C pump. If the pump external by-pass valve is installed the shaft seal on each hydraulic pump must be replaced at the same time.
(b) Install return line filter.
Boeing Service Bulletin No. 379 and Vickers Service Letter dated June 17, 1959, pertain to item (a). Boeing Service Bulletins Nos. 69 and 213 pertain to item (b).



FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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