AD 61-21-03

final rule

Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft

AD Number
61-21-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
(Federal Register: October 13, 1961)

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company DC-8-11 Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8-12 Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8-21 Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8-31 Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8-32 Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8-33 Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8-41 Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8-42 Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8-43 Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8-51 Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8-52 Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8-53 Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8-55 Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8-61 Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8-61F Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8-62 Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8-62F Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8-63 Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8-63F Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8-71 Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8-71F Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8-72 Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8-72F Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8-73 Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8-73F Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8F-54 Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
aircraft The Boeing Company DC-8F-55 Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft

Unsafe Condition

Failure to provide an accurate indication of reserve hydraulic fluid quantity in the system reservoir could result in insufficient hydraulic fluid leading to system failure.

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

Required Actions

Replace or modify the cockpit hydraulic quantity gage and reservoir quantity transmitter per Douglas Service Bulletin DC-8 A29-40 (Reissue No. 1 or later) or FAA-approved equivalent to indicate reserve fluid down to approximately one gallon with ≤10% error. Mark the gage dial into three segments (NORMAL, AUX., EMER.) corresponding to fluid levels.

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

Compliance Time

within the next 150 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

DOUGLAS All DC-8 Series Aircraft including models DC-8-11, DC-8-12, DC-8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, DC-8-43, DC-8-51, and others as listed

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

Federal Register Abstract

Hydraulic Fluid Gage

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_61-21-03.html
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Details
AD Number:
61-21-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
Subject:
Hydraulic Fluid Gage
Status:
Current
Citation:
(Federal Register: October 13, 1961)
Citation Publish Date:
10/13/1961
Effective Date:
10/13/1961
Make:
The Boeing Company
Model:
DC-8-11 | DC-8-12 | DC-8-21 | DC-8-31 | DC-8-32 | DC-8-33 | DC-8-41 | DC-8-42 | DC-8-43 | DC-8-51 | ...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: 61-21-03
CITATION:   [Federal Register: October 13, 1961]

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   61-21-03

SUBJECT HEADING:   Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft

ACTION:  

SUMMARY:  

DATES:   Effective October 13, 1961.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
61-21-03 DOUGLAS: Amdt. 346 Part 507 Federal Register October 13, 1961. Applies to All DC-8 Series Aircraft.

Compliance required within the next 150 hours' time in service after the effective date of this AD.

As a result of recent incidents which have shown the need for effective quantity indication of "reserve" hydraulic fluid in the system reservoir, the following must be accomplished:

Unless already accomplished in accordance with FAA approved technical data, replace or modify in accordance with Douglas Service Bulletin No. DC-8 A29-40 (Reissue No. 1 or later) or FAA approved equivalent, the existing hydraulic quantity gage in the cockpit and the quantity transmitter in the fluid reservoir, to provide a system which will indicate the quantity of reserve hydraulic fluid in the reservoir down to approximately one gallon. The system indication error shall not exceed 10 percent. The dial on the quantity gage shall be marked in a manner which divides the total indicator range into three segments and identifies the three segments, as follows:

Segment	Reserve Fluid Quantity in Reservoir
NORMAL	Full (11.5 gal.) to 4.9 gal.
AUX.	4.9 gal. to 1.5 gal.
EMER.	1.5 gal. to approx. 1.0 gal.

The exact quantities in gallons need not be marked on the quality indicator. "EMER." need not be shown provided that this segment is otherwise marked in a manner distinctly different from the other segments.

(Douglas Service Bulletin No. DC-8 A29-40 (Reissue No. 1 or later) pertains to this same subject.)

This directive effective October 13, 1961.


FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_61-21-03.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
61-21-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft
Subject:
Hydraulic Fluid Gage
Status:
Current
Citation:
(Federal Register: October 13, 1961)
Citation Publish Date:
10/13/1961
Effective Date:
10/13/1961
Make:
The Boeing Company
Model:
DC-8-11 | DC-8-12 | DC-8-21 | DC-8-31 | DC-8-32 | DC-8-33 | DC-8-41 | DC-8-42 | DC-8-43 | DC-8-51 | ...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: 61-21-03
CITATION:   [Federal Register: October 13, 1961]

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   61-21-03

SUBJECT HEADING:   Airworthiness Directives; DOUGLAS All DC-8 Series Aircraft

ACTION:  

SUMMARY:  

DATES:   Effective October 13, 1961.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
61-21-03 DOUGLAS: Amdt. 346 Part 507 Federal Register October 13, 1961. Applies to All DC-8 Series Aircraft.

Compliance required within the next 150 hours' time in service after the effective date of this AD.

As a result of recent incidents which have shown the need for effective quantity indication of "reserve" hydraulic fluid in the system reservoir, the following must be accomplished:

Unless already accomplished in accordance with FAA approved technical data, replace or modify in accordance with Douglas Service Bulletin No. DC-8 A29-40 (Reissue No. 1 or later) or FAA approved equivalent, the existing hydraulic quantity gage in the cockpit and the quantity transmitter in the fluid reservoir, to provide a system which will indicate the quantity of reserve hydraulic fluid in the reservoir down to approximately one gallon. The system indication error shall not exceed 10 percent. The dial on the quantity gage shall be marked in a manner which divides the total indicator range into three segments and identifies the three segments, as follows:

Segment	Reserve Fluid Quantity in Reservoir
NORMAL	Full (11.5 gal.) to 4.9 gal.
AUX.	4.9 gal. to 1.5 gal.
EMER.	1.5 gal. to approx. 1.0 gal.

The exact quantities in gallons need not be marked on the quality indicator. "EMER." need not be shown provided that this segment is otherwise marked in a manner distinctly different from the other segments.

(Douglas Service Bulletin No. DC-8 A29-40 (Reissue No. 1 or later) pertains to this same subject.)

This directive effective October 13, 1961.


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.