AD 75-16-18

final rule

DOWTY ROTOL Models R245/4-40-4.5/13, R259/4-40-4.5/17 and R209/4-40-4.5/2 Propellers

AD Number
75-16-18
Status
final_rule
Effective Date
Product Category
propeller
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft propeller assembly
Problem area Propeller

Applicability

TypeManufacturerModelDetails
aircraft Dowty Propellers (c) R.209/4-40-4.5 DOWTY ROTOL Models R245/4-40-4.5/13, R259/4-40-4.5/17 and R209/4-40-4.5/2 Propellers
aircraft Dowty Propellers (c) R.245/4-40-4.5 DOWTY ROTOL Models R245/4-40-4.5/13, R259/4-40-4.5/17 and R209/4-40-4.5/2 Propellers
aircraft Dowty Propellers (c) R.259/4-40-4.5 DOWTY ROTOL Models R245/4-40-4.5/13, R259/4-40-4.5/17 and R209/4-40-4.5/2 Propellers
propeller Dowty Propellers (c) R.209/4-40-4.5 DOWTY ROTOL Models R245/4-40-4.5/13, R259/4-40-4.5/17 and R209/4-40-4.5/2 Propellers
propeller Dowty Propellers (c) R.245/4-40-4.5 DOWTY ROTOL Models R245/4-40-4.5/13, R259/4-40-4.5/17 and R209/4-40-4.5/2 Propellers
propeller Dowty Propellers (c) R.259/4-40-4.5 DOWTY ROTOL Models R245/4-40-4.5/13, R259/4-40-4.5/17 and R209/4-40-4.5/2 Propellers

Unsafe Condition

Propeller blade failures from cracks or forging defects in flight.

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

Required Actions

Inspect and test specified blade serial numbers for cracks or forging defects. Repair blades in accordance with Dowty Rotol Bulletin 61-A862 or remove from service if repair is not possible. Return blades to service only if free of defects or repaired as required.

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

Compliance Time

within the next 300 hours propeller time in service after the effective date of this AD or before the accumulation of 5300 hours propeller time in service, whichever occurs later

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

Affected Aircraft

Dowty Propellers models R245/4-40-4.5/13, R259/4-40-4.5/17, and R209/4-40-4.5/2 propellers with specified blade serial numbers listed in the AD, used on Convair 600 series and YS-11 series airplanes.

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

Federal Register Abstract

Blades

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_75-16-18.html
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AD Number:
75-16-18
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
DOWTY ROTOL Models R245/4-40-4.5/13, R259/4-40-4.5/17 and R209/4-40-4.5/2 Propellers
Subject:
Blades
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/29/1975
Make:
Dowty Propellers
Model:
(c) R.209/4-40-4.5 | (c) R.245/4-40-4.5 | (c) R.259/4-40-4.5
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: 75-16-18
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2292

AD NUMBER:   75-16-18

SUBJECT HEADING:   DOWTY ROTOL Models R245/4-40-4.5/13, R259/4-40-4.5/17 and R209/4-40-4.5/2 Propellers

ACTION:  

SUMMARY:  

DATES:   Effective July 29, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-16-18 DOWTY ROTOL: Amendment 39-2292. Applies to Dowty Rotol Propellers R245/4-40-4.5/13, R259/4-40-4.5/17 and R209/4-40-4.5/2 used on Convair 600 series and YS-11 series airplanes.

Compliance required as indicated within the next 300 hours propeller time in service after the effective date of this AD or before the accumulation of 5300 hours propeller time in service, whichever occurs later, unless already accomplished.

To prevent propeller blade failures from occurring in flight:

(a) Inspect and test the following serial number blades for cracks or forging defects in accordance with Appendix B of Dowty Rotol Alert Service Bulletin 61-A862, Revision 1, dated May 22, 1975, (hereafter Dowty Rotol Bulletin 61-A862) or later FAA-approved revision, or an equivalent approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa and Middle East Region, c/o American Embassy, APO New York, N.Y. 09667.

YS11 & 11A propeller blades with blade serial numbers:
A124879	A125027	A125113	A125242	A125292	A12556	A125720
A124882	A125028	A125115	A125243	A125293	A125570	A125762
A124884	A125035	A125116	A125244	A125294	A125583	A125780
A124890	A125036	A125121	A125245	A125296	A125585	A125822
A124892	A125037	A125122	A125246	A125298	A125587	A125824
A124893	A125038	A125123	A125299	A125247	A125589	A125833
A124894	A125039	A125141	A125248	A125302	A125590	A125834
A124906	A125040	A125142	A125249	A125304	A125611	A125835
A124907	A125047	A125143	A125251	A125316	A125612	A125842
A124908	A125048	A125149	A125252	A125317	A125613	A125843
A124909	A125049	A125151	A125262	A125318	A125614	A125900
A124910	A125050	A125152	A125263	A125527	A125628	A125908
A124928	A125051	A125159	A125264	A125528	A125629	A125911
A124929	A125057	A125160	A125272	A125538	A125642	A125930
A125008	A125058	A125275	A125540	A125654	A125654	A125956
A125009	A125059	A125165	A125276	A125547	A12565	A125982
A125010	A125061	A125166	A125283	A125549	A125674	A125984
A125016	A125062	A125167	A125285	A125556	A125676	A125985
A125017	A125090	A125169	A125287	A125557	A125677	A125989
A125018	A125091	A125171	A125288	A125565	A125708	A126089
A125019	A125093	A125290	A125290	A125566	A125709	A126090
A125025	A125112	A125239	A125291	A125567	A125718	A126122

Convair propeller blades with blade serial numbers:


A125447	A125661
A125448	A125662
A125458	A125699
A125462	A125844

(b) If cracks or forging defects are found, comply with (1) or (2) as appropriate:

(1) Repair the blade in accordance with Appendix B of Dowty Rotol Bulletin 61-A862 or later FAA-approved revision or an FAA equivalent approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa and Middle East Region, c/o American Embassy, APO New York, N.Y. 09667.

(2) Remove the blade from service if repair cannot be made in accordance with paragraph (b)(1).

(c) Blades may be returned to service following inspection and test if found free of cracks or forging defects or have been repaired in accordance with paragraph (b)(1) of this AD.
This amendment becomes effective July 29, 1975.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_75-16-18.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
75-16-18
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
DOWTY ROTOL Models R245/4-40-4.5/13, R259/4-40-4.5/17 and R209/4-40-4.5/2 Propellers
Subject:
Blades
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/29/1975
Make:
Dowty Propellers
Model:
(c) R.209/4-40-4.5 | (c) R.245/4-40-4.5 | (c) R.259/4-40-4.5
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: 75-16-18
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2292

AD NUMBER:   75-16-18

SUBJECT HEADING:   DOWTY ROTOL Models R245/4-40-4.5/13, R259/4-40-4.5/17 and R209/4-40-4.5/2 Propellers

ACTION:  

SUMMARY:  

DATES:   Effective July 29, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-16-18 DOWTY ROTOL: Amendment 39-2292. Applies to Dowty Rotol Propellers R245/4-40-4.5/13, R259/4-40-4.5/17 and R209/4-40-4.5/2 used on Convair 600 series and YS-11 series airplanes.

Compliance required as indicated within the next 300 hours propeller time in service after the effective date of this AD or before the accumulation of 5300 hours propeller time in service, whichever occurs later, unless already accomplished.

To prevent propeller blade failures from occurring in flight:

(a) Inspect and test the following serial number blades for cracks or forging defects in accordance with Appendix B of Dowty Rotol Alert Service Bulletin 61-A862, Revision 1, dated May 22, 1975, (hereafter Dowty Rotol Bulletin 61-A862) or later FAA-approved revision, or an equivalent approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa and Middle East Region, c/o American Embassy, APO New York, N.Y. 09667.

YS11 & 11A propeller blades with blade serial numbers:
A124879	A125027	A125113	A125242	A125292	A12556	A125720
A124882	A125028	A125115	A125243	A125293	A125570	A125762
A124884	A125035	A125116	A125244	A125294	A125583	A125780
A124890	A125036	A125121	A125245	A125296	A125585	A125822
A124892	A125037	A125122	A125246	A125298	A125587	A125824
A124893	A125038	A125123	A125299	A125247	A125589	A125833
A124894	A125039	A125141	A125248	A125302	A125590	A125834
A124906	A125040	A125142	A125249	A125304	A125611	A125835
A124907	A125047	A125143	A125251	A125316	A125612	A125842
A124908	A125048	A125149	A125252	A125317	A125613	A125843
A124909	A125049	A125151	A125262	A125318	A125614	A125900
A124910	A125050	A125152	A125263	A125527	A125628	A125908
A124928	A125051	A125159	A125264	A125528	A125629	A125911
A124929	A125057	A125160	A125272	A125538	A125642	A125930
A125008	A125058	A125275	A125540	A125654	A125654	A125956
A125009	A125059	A125165	A125276	A125547	A12565	A125982
A125010	A125061	A125166	A125283	A125549	A125674	A125984
A125016	A125062	A125167	A125285	A125556	A125676	A125985
A125017	A125090	A125169	A125287	A125557	A125677	A125989
A125018	A125091	A125171	A125288	A125565	A125708	A126089
A125019	A125093	A125290	A125290	A125566	A125709	A126090
A125025	A125112	A125239	A125291	A125567	A125718	A126122

Convair propeller blades with blade serial numbers:


A125447	A125661
A125448	A125662
A125458	A125699
A125462	A125844

(b) If cracks or forging defects are found, comply with (1) or (2) as appropriate:

(1) Repair the blade in accordance with Appendix B of Dowty Rotol Bulletin 61-A862 or later FAA-approved revision or an FAA equivalent approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa and Middle East Region, c/o American Embassy, APO New York, N.Y. 09667.

(2) Remove the blade from service if repair cannot be made in accordance with paragraph (b)(1).

(c) Blades may be returned to service following inspection and test if found free of cracks or forging defects or have been repaired in accordance with paragraph (b)(1) of this AD.
This amendment becomes effective July 29, 1975.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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