AD 68-08-01

final rule

MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models

AD Number
68-08-01
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 McCauley Propeller Systems 2A34C MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
aircraft McCauley Propeller Systems 2A36C23 MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
aircraft McCauley Propeller Systems 2A36C29 MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
aircraft McCauley Propeller Systems 2A36C82 MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
aircraft McCauley Propeller Systems 2D34C MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
aircraft McCauley Propeller Systems 3A32C76 MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
aircraft McCauley Propeller Systems B2A36C31 MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
aircraft McCauley Propeller Systems C2A36C32 MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
aircraft McCauley Propeller Systems D2A34C MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
aircraft McCauley Propeller Systems D2A36C31 MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
propeller McCauley Propeller Systems 2A34C MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
propeller McCauley Propeller Systems 2A36C23 MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
propeller McCauley Propeller Systems 2A36C29 MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
propeller McCauley Propeller Systems 2A36C82 MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
propeller McCauley Propeller Systems 2D34C MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
propeller McCauley Propeller Systems 3A32C76 MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
propeller McCauley Propeller Systems B2A36C31 MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
propeller McCauley Propeller Systems C2A36C32 MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
propeller McCauley Propeller Systems D2A34C MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
propeller McCauley Propeller Systems D2A36C31 MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
propeller McCauley Propeller Systems D2A36C33 MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
propeller McCauley Propeller Systems D2A36C45 MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
propeller McCauley Propeller Systems D3A32C77 MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
propeller McCauley Propeller Systems D3A32C79 MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
propeller McCauley Propeller Systems D3A32C88 MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
propeller McCauley Propeller Systems D3A32C90 MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
propeller McCauley Propeller Systems E2A34C MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models

Unsafe Condition

Failure of the propeller cylinder attach screws

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

Required Actions

Modify propeller cylinder attachment in accordance with McCauley Service Bulletin No. 92 (or later FAA-approved revision) unless used on Bellanca Aircraft Models 17-30 and 17-30A, which require Service Bulletin No. 94. Equivalent methods must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.

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

Compliance Time

within the next 100 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

McCauley Propeller Systems models 2D34C8, C2A36C32, D2A34C58-B, 3A32C76-S, D2A34C78-K and others listed, with hub serial numbers 59000 up to and including 712778 except specific excluded numbers

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

Federal Register Abstract

Cylinder Attach Screws

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_68-08-01.html
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AD Number:
68-08-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
Subject:
Cylinder Attach Screws
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
01/21/1972
Make:
McCauley Propeller Systems
Model:
2A34C | 2A36C23 | 2A36C29 | 2A36C82 | 2D34C | 3A32C76 | B2A36C31 | C2A36C32 | D2A34C | D2A36C31 | D2...Show more
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: 68-08-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1377

AD NUMBER:   68-08-01

SUBJECT HEADING:   MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models


ACTION:  

SUMMARY:  

DATES:   Effective January 21, 1972.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   68-08-01 MCCAULEY AIRCRAFT PROPELLERS: Amdt. 39-581 as amended by Amendment 39-1314 is further amended by Amendment 39-1377. Applies to the following two- and three-bladed constant speed propeller models with hub serial numbers indicated below:

PROPELLER MODELS
2D34C8	C2A36C32	D2A34C58-B	3A32C76-S	D2A34C78-K
2D34C8-A	C2A36C32-A	D2A34C58-J	3A32C76-T	D2A34C78-L
2D34C8-J	C2A36C32-D	D2A34C58-K	3A32C76-AD	D2A34C78-M
2D34C8-K	D2A36C33	D2A34C58-L	3A32C76-AS	D3A32C79
2D34C8-M	D2A36C33-D	D2A34C58-M	3A32C76-AT	D3A32C79-A
2A36C23-C	D2A36C45	2A34C66	3A32C76-FD	D3A32C79-B
2A36C23-CD	D2A36C45-D	2A34C66-A	3A32C76-FS	D3A32C79-F
2A36C23-CH	D2A34C49	2A34C66-B	3A32C76-FT	D3A32C79-J
2A36C23-CJ	D2A34C49-A	2A34C66-C	3A32C76-JD	D3A32C79-K
2A36C23-CP	D2A34C49-B	2A34C66-J	3A32C76-JS	2A36C82-T
2A36C23-CS	D2A34C49-J	2A34C66-K	3A32C76-JT	2A36C82-DT
2A36C23-DD	D2A34C49-K	2A34C66-L	3A32C76-KD	D3A32C88
2A36C23-DH	D2A34C49-L	2A34C66-M	3A32C76-KS	D3A32C88-A
2A36C23-DJ	D2A34C49-M	E2A34C70	3A32C76-KT	D3A32C88-F
2A36C23-DP	2A34C50	E2A34C70-A	D3A32C77	D3A32C88-J
2A36C29	2A34C50-A	E2A34C70-J	D3A32C77-A	D3A32C88-K
2A36C29-A	2A34C50-B	E2A34C70-K	D3A32C77-F	D3A32C90
2A36C29-D	2A34C50-J	E2A34C70-M	D2A32C77-J	D3A32C90-A
B2A36C31	2A34C50-K	E2A34C73	D3A32C77-K	D3A32C90-B
B2A36C31-A	2A34C50-L	E2A34C73-A	D2A34C78	D3A32C90-C
B2A36C31-D	2A34C50-M	E2A34C73-J	D2A34C78-A	D3A32C90-F
D2A36C31-A	D2A34C58	E2A34C73-K	D2A34C78-B	D3A32C90-J
D2A36C31-D	D2A34C58-A	E2A34C73-M	D2A34C78-J	D3A32C90-K
		3A32C76-D		
HUB SERIAL NUMBERS
59000 up to and including 712778 except 700492, 700500 thru 700558; 700561 thru 700568; 700570 thru 700594; 700596 thru 701050 and 701053

Compliance required within the next 100 hours' time in service after the effective date of this AD, unless already accomplished. To prevent failure of the propeller cylinder attach screws, accomplish the following:

Modify propeller cylinder attachment in accordance with McCauley Service Bulletin No. 92, dated April 21, 1971, or later FAA-approved revision. However, for propellers used on Bellanca Aircraft Models 17-30 and 17-30A modify propeller cylinder attachment in accordance with McCauley Service Bulletin No. 94, dated July 28, 1971, or later FAA-approved revision instead of Service Bulletin No. 92. Equivalent methods of compliance with this AD must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.

Amendment 39-581 was effective April 11, 1968.

Amendment 39-1314 was effective October 14, 1971.

This Amendment 39-1377 is effective January 21, 1972.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_68-08-01.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
68-08-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models
Subject:
Cylinder Attach Screws
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
01/21/1972
Make:
McCauley Propeller Systems
Model:
2A34C | 2A36C23 | 2A36C29 | 2A36C82 | 2D34C | 3A32C76 | B2A36C31 | C2A36C32 | D2A34C | D2A36C31 | D2...Show more
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: 68-08-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1377

AD NUMBER:   68-08-01

SUBJECT HEADING:   MCCAULEY AIRCRAFT PROPELLERS two- and three-bladed constant speed propeller models


ACTION:  

SUMMARY:  

DATES:   Effective January 21, 1972.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   68-08-01 MCCAULEY AIRCRAFT PROPELLERS: Amdt. 39-581 as amended by Amendment 39-1314 is further amended by Amendment 39-1377. Applies to the following two- and three-bladed constant speed propeller models with hub serial numbers indicated below:

PROPELLER MODELS
2D34C8	C2A36C32	D2A34C58-B	3A32C76-S	D2A34C78-K
2D34C8-A	C2A36C32-A	D2A34C58-J	3A32C76-T	D2A34C78-L
2D34C8-J	C2A36C32-D	D2A34C58-K	3A32C76-AD	D2A34C78-M
2D34C8-K	D2A36C33	D2A34C58-L	3A32C76-AS	D3A32C79
2D34C8-M	D2A36C33-D	D2A34C58-M	3A32C76-AT	D3A32C79-A
2A36C23-C	D2A36C45	2A34C66	3A32C76-FD	D3A32C79-B
2A36C23-CD	D2A36C45-D	2A34C66-A	3A32C76-FS	D3A32C79-F
2A36C23-CH	D2A34C49	2A34C66-B	3A32C76-FT	D3A32C79-J
2A36C23-CJ	D2A34C49-A	2A34C66-C	3A32C76-JD	D3A32C79-K
2A36C23-CP	D2A34C49-B	2A34C66-J	3A32C76-JS	2A36C82-T
2A36C23-CS	D2A34C49-J	2A34C66-K	3A32C76-JT	2A36C82-DT
2A36C23-DD	D2A34C49-K	2A34C66-L	3A32C76-KD	D3A32C88
2A36C23-DH	D2A34C49-L	2A34C66-M	3A32C76-KS	D3A32C88-A
2A36C23-DJ	D2A34C49-M	E2A34C70	3A32C76-KT	D3A32C88-F
2A36C23-DP	2A34C50	E2A34C70-A	D3A32C77	D3A32C88-J
2A36C29	2A34C50-A	E2A34C70-J	D3A32C77-A	D3A32C88-K
2A36C29-A	2A34C50-B	E2A34C70-K	D3A32C77-F	D3A32C90
2A36C29-D	2A34C50-J	E2A34C70-M	D2A32C77-J	D3A32C90-A
B2A36C31	2A34C50-K	E2A34C73	D3A32C77-K	D3A32C90-B
B2A36C31-A	2A34C50-L	E2A34C73-A	D2A34C78	D3A32C90-C
B2A36C31-D	2A34C50-M	E2A34C73-J	D2A34C78-A	D3A32C90-F
D2A36C31-A	D2A34C58	E2A34C73-K	D2A34C78-B	D3A32C90-J
D2A36C31-D	D2A34C58-A	E2A34C73-M	D2A34C78-J	D3A32C90-K
		3A32C76-D		
HUB SERIAL NUMBERS
59000 up to and including 712778 except 700492, 700500 thru 700558; 700561 thru 700568; 700570 thru 700594; 700596 thru 701050 and 701053

Compliance required within the next 100 hours' time in service after the effective date of this AD, unless already accomplished. To prevent failure of the propeller cylinder attach screws, accomplish the following:

Modify propeller cylinder attachment in accordance with McCauley Service Bulletin No. 92, dated April 21, 1971, or later FAA-approved revision. However, for propellers used on Bellanca Aircraft Models 17-30 and 17-30A modify propeller cylinder attachment in accordance with McCauley Service Bulletin No. 94, dated July 28, 1971, or later FAA-approved revision instead of Service Bulletin No. 92. Equivalent methods of compliance with this AD must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.

Amendment 39-581 was effective April 11, 1968.

Amendment 39-1314 was effective October 14, 1971.

This Amendment 39-1377 is effective January 21, 1972.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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