AD 70-22-07

final rule

ROLLS-ROYCE Models Dart 506, 510, and 526 Engines

AD Number
70-22-07
Status
final_rule
Effective Date
Product Category
engine
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft propeller assembly
Problem area Propeller

Applicability

TypeManufacturerModelDetails
engine Rolls-Royce Deutschland Ltd & Co KG Dart 506 ROLLS-ROYCE Models Dart 506, 510, and 526 Engines
engine Rolls-Royce Deutschland Ltd & Co KG Dart 510 ROLLS-ROYCE Models Dart 506, 510, and 526 Engines
engine Rolls-Royce Deutschland Ltd & Co KG Dart 526 ROLLS-ROYCE Models Dart 506, 510, and 526 Engines

Unsafe Condition

Annulus gear failure could lead to loss of propeller control.

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

Required Actions

Incorporate Rolls-Royce Modifications 1431 (for Model 506) and 1550 (for Models 510 and 526) per specified service bulletins or FAA-approved equivalents.

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

Compliance Time

within the next 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

Rolls-Royce Models Dart 506, 510, and 526 engines installed on British Aircraft Corporation Viscount 744 and 745D; and Armstrong Whitworth Argosy 650 Series 101 airplanes.

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

Federal Register Abstract

Annulus Gear Failure

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_70-22-07.html
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AD Number:
70-22-07
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
ROLLS-ROYCE Models Dart 506, 510, and 526 Engines
Subject:
Annulus Gear Failure
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/23/1970
Make:
Rolls-Royce Deutschland Ltd & Co KG
Model:
Dart 506 | Dart 510 | Dart 526
Product Type:
Engine
Product Subtype:
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 70-22-07
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1098

AD NUMBER:   70-22-07

SUBJECT HEADING:   ROLLS-ROYCE Models Dart 506, 510, and 526 Engines

ACTION:  

SUMMARY:  

DATES:   Effective November 23, 1970.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
70-22-07 ROLLS-ROYCE: Amdt. 39-1098. Applies to Rolls-Royce Dart engines Models 506, 510, and 526, installed on, but not necessarily limited to, British Aircraft Corporation Viscount 744 and 745D; and Armstrong Whitworth Argosy 650 Series 101 airplanes.

Compliance is required within the next 500 hours' time in service after the effective date of this AD, unless already accomplished.

To prevent the loss of propeller control in the event of an annulus gear failure, accomplish the following:

(a) For Rolls-Royce Dart Model 506 engines, incorporate Rolls-Royce Dart Modification 1431 in accordance with Rolls-Royce Dart Aero Engine Service Bulletin Number Da72-297, Revision 7, dated February 20, 1970, or later ARB-approved revision, or an FAA-approved equivalent.

(b) For Rolls-Royce Dart Models 510 and 526, incorporate Rolls-Royce Dart Modification 1550 in accordance with Rolls-Royce Dart Aero Engine Service Bulletin Number Da72-348, Revision 9, dated November 28, 1969, or later ARB-approved revision or an FAA-approved equivalent.

This amendment becomes effective November 23, 1970.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_70-22-07.html
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Details
AD Number:
70-22-07
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
ROLLS-ROYCE Models Dart 506, 510, and 526 Engines
Subject:
Annulus Gear Failure
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/23/1970
Make:
Rolls-Royce Deutschland Ltd & Co KG
Model:
Dart 506 | Dart 510 | Dart 526
Product Type:
Engine
Product Subtype:
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 70-22-07
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1098

AD NUMBER:   70-22-07

SUBJECT HEADING:   ROLLS-ROYCE Models Dart 506, 510, and 526 Engines

ACTION:  

SUMMARY:  

DATES:   Effective November 23, 1970.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
70-22-07 ROLLS-ROYCE: Amdt. 39-1098. Applies to Rolls-Royce Dart engines Models 506, 510, and 526, installed on, but not necessarily limited to, British Aircraft Corporation Viscount 744 and 745D; and Armstrong Whitworth Argosy 650 Series 101 airplanes.

Compliance is required within the next 500 hours' time in service after the effective date of this AD, unless already accomplished.

To prevent the loss of propeller control in the event of an annulus gear failure, accomplish the following:

(a) For Rolls-Royce Dart Model 506 engines, incorporate Rolls-Royce Dart Modification 1431 in accordance with Rolls-Royce Dart Aero Engine Service Bulletin Number Da72-297, Revision 7, dated February 20, 1970, or later ARB-approved revision, or an FAA-approved equivalent.

(b) For Rolls-Royce Dart Models 510 and 526, incorporate Rolls-Royce Dart Modification 1550 in accordance with Rolls-Royce Dart Aero Engine Service Bulletin Number Da72-348, Revision 9, dated November 28, 1969, or later ARB-approved revision or an FAA-approved equivalent.

This amendment becomes effective November 23, 1970.

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.