AD 61-21-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| 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.
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Compliance Time
within the next 150 hours' time in service after the effective date of this AD
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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 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:
Document Text
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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
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