AD 76-18-03

final rule

DOWTY ROTOL Models (c)R193/4-30-4/50, (c)R257/4-30-4/60, and (c)R184/4-30-4/50 Propellers

AD Number
76-18-03
Status
final_rule
Effective Date
Product Category
propeller
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Dowty Propellers (c) R184/4-30-4/ DOWTY ROTOL Models (c)R193/4-30-4/50, (c)R257/4-30-4/60, and (c)R184/4-30-4/50 Propellers
aircraft Dowty Propellers (c) R193/4-30-4/ DOWTY ROTOL Models (c)R193/4-30-4/50, (c)R257/4-30-4/60, and (c)R184/4-30-4/50 Propellers
aircraft Dowty Propellers (c) R257/4-30-4/ DOWTY ROTOL Models (c)R193/4-30-4/50, (c)R257/4-30-4/60, and (c)R184/4-30-4/50 Propellers
propeller Dowty Propellers (c) R184/4-30-4/ DOWTY ROTOL Models (c)R193/4-30-4/50, (c)R257/4-30-4/60, and (c)R184/4-30-4/50 Propellers
propeller Dowty Propellers (c) R193/4-30-4/ DOWTY ROTOL Models (c)R193/4-30-4/50, (c)R257/4-30-4/60, and (c)R184/4-30-4/50 Propellers
propeller Dowty Propellers (c) R257/4-30-4/ DOWTY ROTOL Models (c)R193/4-30-4/50, (c)R257/4-30-4/60, and (c)R184/4-30-4/50 Propellers

Unsafe Condition

Cracking and possible failure of the hub driving center due to improper machining.

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

Required Actions

Re-work the hub driving center to salvage scheme No. 640144000 for listed serial numbers. Inspect and rework if incorrectly machined for unlisted serial numbers, following Service Bulletin 61-858 or approved equivalent.

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

Compliance Time

At the next propeller overhaul or within the next 4700 hours propeller time in service after the effective date of this AD, whichever occurs first.

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

Affected Aircraft

Dowty Propellers models (c)R193/4-30-4/50, (c)R257/4-30-4/60, and (c)R184/4-30-4/50 with Hub Driving Centers P/N 601026638 modified to Mod. No. (c)VP2486.

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

Federal Register Abstract

Hub and Driving Center Assemblies

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_76-18-03.html
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AD Number:
76-18-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
DOWTY ROTOL Models (c)R193/4-30-4/50, (c)R257/4-30-4/60, and (c)R184/4-30-4/50 Propellers
Subject:
Hub and Driving Center Assemblies
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/01/1976
Make:
Dowty Propellers
Model:
(c) R184/4-30-4/ | (c) R193/4-30-4/ | (c) R257/4-30-4/
Product Type:
Propeller
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: 76-18-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2711

AD NUMBER:   76-18-03

SUBJECT HEADING:   DOWTY ROTOL Models (c)R193/4-30-4/50, (c)R257/4-30-4/60, and (c)R184/4-30-4/50 Propellers

ACTION:  

SUMMARY:  

DATES:   Effective October 1, 1976.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
76-18-03 DOWTY ROTOL: Amendment 39-2711. Applies to Dowty Rotol Type (c)R193/4-30-4/50, (c)R257/4-30-4/60, and (c)R184/4-30-4/50 propellers having Hub Driving Centers, P/N 601026638, modified to Dowty Rotol Mod. No. (c)VP2486. These propellers are installed on, but not necessarily limited to, Fokker Model F-27, Fairchild Model FH-227, and Grumman Model G-159 Series airplanes.

NOTE: Dowty Rotol Mod. No. (c)VP2486 is covered in Dowty Rotol Service Bulletin 61-573A, dated June 1968, and the incorporation of the modification is required by AD 68-20-7.

Compliance is required at the next propeller overhaul or within the next 4700 hours propeller time in service after the effective date of this AD, whichever occurs first, unless already accomplished.

To prevent cracking and possible failure of the hub driving center due to improper machining, accomplish the following:
(a) For propellers that incorporate hub and driving center assemblies having the following serial numbers, rework the hub driving center to salvage scheme No. 640144000, in accordance with Dowty Rotol Service Bulletin 61-858, dated February 4, 1975, or an equivalent approved in accordance with paragraph (c) of this AD:

Hub and Driving Center Assembly Serial Numbers

Serial No.	Propeller Type	Serial No.	Propeller Type
184/59/47	R184/4-30-4/50	DRG/31/62	R184/4-30-4/50
184/59/60	"	DRG/288/64	"
184/59/62	"	DRG/290/64	"
184/59/64	"	DRG/56/65	"
184/59/65	"	DRG/116/65	"
184/60/79	"	DRG/122/65	"
184/60/86	"	DRG/223/65	"
184/60/89	"	DRG/223/65	"
184/60/94	"	DRG/224/65	"
184/60/95	"	DRG/42/66	"
184/60/96	"	DRG/122/66	"
184/60/99	"	193/58/11	R193/4-30-4/50
184/60/103	"	193/58/17	"
184/60/126	"	193/58/27	"
184/60/146	"	193/58/38	"
184/60/147	"	193/59/116	"
184/60/159	"	193/59/119	"
184/60/160	"	193/60/150	"
DRG/10/61	"	193/60/151	"
DRG/12/61	"	DRG/32/62	"
DRG/14/61	"	DRG/119/66	"
DRG/17/61	"	DRG/442/66	"
DRG/20/61	"	DRG/131/66	R257/4-30-4/60
DRG/24/61	"	DRG/407/66	"
DRG/25/61	"	DRG/408/66	"
DRG/31/61	"	DRG/454/66	"
DRG/38/61	"	DRG/28/67	"
DRG/41/61	"	DRG/30/67	"
DRG/43/61	"	DRG/86/67	"
DRG/44/61	"	DRG/93/67	"
DRG/48/61	"	DRG/95/67	"
DRG/49/61	"	DRG/189/67	"
DRG/58/61	"	DRG/194/67	"
DRG/2/62	"	DRG/231/67	"
DRG/9/62	"	DRG/233/67	"
DRG/10/62	"	DRG/344/67	"
DRG/11/62	"	DRG/345/67	"
DRG/19/62	"	DRG/348/67	"

(b) For propellers that incorporate hub and driving center assemblies having serial numbers not listed in paragraph (a) of this AD, accomplish the following in accordance with Dowty Rotol Service Bulletin 61-858, dated February 4, 1975, or an equivalent approved in accordance with paragraph (c) of this AD:
(1) Inspect the hub driving center to verify correct machining.
(2) If the hub driving center is found to be incorrectly machined, rework the hub driving center to salvage scheme No. 640144000.

(c) The equivalent means of compliance specified in paragraphs (a) and (b) of this AD must be approved by the Chief, Aircraft Certification Staff, FAA Europe, Africa and Middle East Region, c/o American Embassy, APO New York, N.Y. 09667.

This amendment becomes effective on October 1, 1976.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_76-18-03.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
76-18-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
DOWTY ROTOL Models (c)R193/4-30-4/50, (c)R257/4-30-4/60, and (c)R184/4-30-4/50 Propellers
Subject:
Hub and Driving Center Assemblies
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/01/1976
Make:
Dowty Propellers
Model:
(c) R184/4-30-4/ | (c) R193/4-30-4/ | (c) R257/4-30-4/
Product Type:
Propeller
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: 76-18-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2711

AD NUMBER:   76-18-03

SUBJECT HEADING:   DOWTY ROTOL Models (c)R193/4-30-4/50, (c)R257/4-30-4/60, and (c)R184/4-30-4/50 Propellers

ACTION:  

SUMMARY:  

DATES:   Effective October 1, 1976.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
76-18-03 DOWTY ROTOL: Amendment 39-2711. Applies to Dowty Rotol Type (c)R193/4-30-4/50, (c)R257/4-30-4/60, and (c)R184/4-30-4/50 propellers having Hub Driving Centers, P/N 601026638, modified to Dowty Rotol Mod. No. (c)VP2486. These propellers are installed on, but not necessarily limited to, Fokker Model F-27, Fairchild Model FH-227, and Grumman Model G-159 Series airplanes.

NOTE: Dowty Rotol Mod. No. (c)VP2486 is covered in Dowty Rotol Service Bulletin 61-573A, dated June 1968, and the incorporation of the modification is required by AD 68-20-7.

Compliance is required at the next propeller overhaul or within the next 4700 hours propeller time in service after the effective date of this AD, whichever occurs first, unless already accomplished.

To prevent cracking and possible failure of the hub driving center due to improper machining, accomplish the following:
(a) For propellers that incorporate hub and driving center assemblies having the following serial numbers, rework the hub driving center to salvage scheme No. 640144000, in accordance with Dowty Rotol Service Bulletin 61-858, dated February 4, 1975, or an equivalent approved in accordance with paragraph (c) of this AD:

Hub and Driving Center Assembly Serial Numbers

Serial No.	Propeller Type	Serial No.	Propeller Type
184/59/47	R184/4-30-4/50	DRG/31/62	R184/4-30-4/50
184/59/60	"	DRG/288/64	"
184/59/62	"	DRG/290/64	"
184/59/64	"	DRG/56/65	"
184/59/65	"	DRG/116/65	"
184/60/79	"	DRG/122/65	"
184/60/86	"	DRG/223/65	"
184/60/89	"	DRG/223/65	"
184/60/94	"	DRG/224/65	"
184/60/95	"	DRG/42/66	"
184/60/96	"	DRG/122/66	"
184/60/99	"	193/58/11	R193/4-30-4/50
184/60/103	"	193/58/17	"
184/60/126	"	193/58/27	"
184/60/146	"	193/58/38	"
184/60/147	"	193/59/116	"
184/60/159	"	193/59/119	"
184/60/160	"	193/60/150	"
DRG/10/61	"	193/60/151	"
DRG/12/61	"	DRG/32/62	"
DRG/14/61	"	DRG/119/66	"
DRG/17/61	"	DRG/442/66	"
DRG/20/61	"	DRG/131/66	R257/4-30-4/60
DRG/24/61	"	DRG/407/66	"
DRG/25/61	"	DRG/408/66	"
DRG/31/61	"	DRG/454/66	"
DRG/38/61	"	DRG/28/67	"
DRG/41/61	"	DRG/30/67	"
DRG/43/61	"	DRG/86/67	"
DRG/44/61	"	DRG/93/67	"
DRG/48/61	"	DRG/95/67	"
DRG/49/61	"	DRG/189/67	"
DRG/58/61	"	DRG/194/67	"
DRG/2/62	"	DRG/231/67	"
DRG/9/62	"	DRG/233/67	"
DRG/10/62	"	DRG/344/67	"
DRG/11/62	"	DRG/345/67	"
DRG/19/62	"	DRG/348/67	"

(b) For propellers that incorporate hub and driving center assemblies having serial numbers not listed in paragraph (a) of this AD, accomplish the following in accordance with Dowty Rotol Service Bulletin 61-858, dated February 4, 1975, or an equivalent approved in accordance with paragraph (c) of this AD:
(1) Inspect the hub driving center to verify correct machining.
(2) If the hub driving center is found to be incorrectly machined, rework the hub driving center to salvage scheme No. 640144000.

(c) The equivalent means of compliance specified in paragraphs (a) and (b) of this AD must be approved by the Chief, Aircraft Certification Staff, FAA Europe, Africa and Middle East Region, c/o American Embassy, APO New York, N.Y. 09667.

This amendment becomes effective on October 1, 1976.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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