AD 67-08-06

final rule

ROLLS-ROYCE Models Spey Mark 506-14, 510-14, and 511-14 Engines

AD Number
67-08-06
Status
final_rule
Effective Date
Product Category
engine
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
engine Rolls-Royce Deutschland Ltd & Co KG Spey 506-14 ROLLS-ROYCE Models Spey Mark 506-14, 510-14, and 511-14 Engines
engine Rolls-Royce Deutschland Ltd & Co KG Spey 511-14 ROLLS-ROYCE Models Spey Mark 506-14, 510-14, and 511-14 Engines

Unsafe Condition

Fuel loss due to clamp failure

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

Required Actions

Inspect Avica fuel tube clamps with specified part numbers to ensure wire locking is intact and tight. Use Rolls-Royce Service Bulletins SP 72-360 and SP 71-93. Repetitive inspections may stop after incorporating specified modifications.

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

Compliance Time

Within the next 25 hours' time in service after the effective date of this AD and thereafter at intervals not to exceed 25 hours' time in service

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

Affected Aircraft

Rolls-Royce Spey Mark 506-14, 510-14, and 511-14 Engines

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

Federal Register Abstract

Fuel Tube Clamps

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_67-08-06.html
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Details
AD Number:
67-08-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
ROLLS-ROYCE Models Spey Mark 506-14, 510-14, and 511-14 Engines
Subject:
Fuel Tube Clamps
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/01/1967
Make:
Rolls-Royce Deutschland Ltd & Co KG
Model:
Spey 506-14 | Spey 511-14
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Superseded AD: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Superseded By: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: 67-08-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-453

AD NUMBER:   67-08-06

SUBJECT HEADING:   ROLLS-ROYCE Models Spey Mark 506-14, 510-14, and 511-14 Engines

ACTION:  

SUMMARY:  

DATES:   Effective August 1, 1967.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
67-08-06 ROLLS-ROYCE: Amdt. 39-453 Part 39 Federal Register, August 1, 1967. Applies to Spey Mark 506-14, 510-14, and 511-14 Engines.

Compliance required as indicated.

To prevent fuel loss due to clamp failure accomplish the following:

(a) Within the next 25 hours' time in service after the effective date of this AD and thereafter at intervals not to exceed 25 hours' time in service, inspect in accordance with the Accomplishment Instructions of Rolls- Royce Service Bulletin SP 72-360 (Mod. 2689) and SP 71-93 (Mod. 2468 PP), Avica fuel tube clamps P/N's EU 34387A or 3405803, EU 34393A or 3405809, EU 34389A or 3405805, and EU 34388A or 3405804 to determine that the wire locking is intact and tight.

(b) The repetitive inspections may be discontinued when Part 1 or Part 2 of Rolls-Royce Modifications 2939 and 2512PP or a later ARB-approved equivalent has been incorporated.

(Rolls-Royce Alert Service Bulletin SP 72-A477 pertains to this subject.)

This directive effective upon publication in the Federal Register for all persons except those to whom it was made effective immediately by telegram dated February 27, 1967.

Revised August 1, 1967.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_67-08-06.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
67-08-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
ROLLS-ROYCE Models Spey Mark 506-14, 510-14, and 511-14 Engines
Subject:
Fuel Tube Clamps
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/01/1967
Make:
Rolls-Royce Deutschland Ltd & Co KG
Model:
Spey 506-14 | Spey 511-14
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: 67-08-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-453

AD NUMBER:   67-08-06

SUBJECT HEADING:   ROLLS-ROYCE Models Spey Mark 506-14, 510-14, and 511-14 Engines

ACTION:  

SUMMARY:  

DATES:   Effective August 1, 1967.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
67-08-06 ROLLS-ROYCE: Amdt. 39-453 Part 39 Federal Register, August 1, 1967. Applies to Spey Mark 506-14, 510-14, and 511-14 Engines.

Compliance required as indicated.

To prevent fuel loss due to clamp failure accomplish the following:

(a) Within the next 25 hours' time in service after the effective date of this AD and thereafter at intervals not to exceed 25 hours' time in service, inspect in accordance with the Accomplishment Instructions of Rolls- Royce Service Bulletin SP 72-360 (Mod. 2689) and SP 71-93 (Mod. 2468 PP), Avica fuel tube clamps P/N's EU 34387A or 3405803, EU 34393A or 3405809, EU 34389A or 3405805, and EU 34388A or 3405804 to determine that the wire locking is intact and tight.

(b) The repetitive inspections may be discontinued when Part 1 or Part 2 of Rolls-Royce Modifications 2939 and 2512PP or a later ARB-approved equivalent has been incorporated.

(Rolls-Royce Alert Service Bulletin SP 72-A477 pertains to this subject.)

This directive effective upon publication in the Federal Register for all persons except those to whom it was made effective immediately by telegram dated February 27, 1967.

Revised August 1, 1967.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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