AD 78-06-02

final rule

MCCAULEY PROPELLERS Model 3FF32C501 Propellers

AD Number
78-06-02
Status
final_rule
Effective Date
Product Category
propeller
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

Applicability

TypeManufacturerModelDetails
aircraft McCauley Propeller Systems 3FF32C501 MCCAULEY PROPELLERS Model 3FF32C501 Propellers
propeller McCauley Propeller Systems 3FF32C501 MCCAULEY PROPELLERS Model 3FF32C501 Propellers

Unsafe Condition

Blade actuating pin screws (P/N A-1635-104) may fail, leading to possible blade pitch control failures.

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

Required Actions

Replace blade actuating pin screws P/N A-1635-104 with new screws P/N A-1635-108 per McCauley Service Bulletin No. 131 and Service Manual No. 751201. The replacement must be done by an FAA Certificated Propeller Repair Station.

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

Compliance Time

before further flight

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

Affected Aircraft

McCauley Propeller Systems Model 3FF32C501 propellers with specified serial numbers listed in the AD, installed on but not limited to Cessna Model 421C and 404 aircraft.

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

Federal Register Abstract

Blade Actuating Pin Screws

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_78-06-02.html
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AD Number:
78-06-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
MCCAULEY PROPELLERS Model 3FF32C501 Propellers
Subject:
Blade Actuating Pin Screws
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
06/07/1978
Make:
McCauley Propeller Systems
Model:
3FF32C501
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Superseded AD: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Superseded By: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: 78-06-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3233

AD NUMBER:   78-06-02

SUBJECT HEADING:   MCCAULEY PROPELLERS Model 3FF32C501 Propellers

ACTION:  

SUMMARY:  

DATES:   Effective June 7, 1978.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
78-06-02 MCCAULEY PROPELLERS: Amendment 39-3159 as amended by Amendment 39-3233. Applies to the following three bladed full feathering constant speed Model 3FF32C501 propellers installed on but not limited to the Cessna Model 421C and 404 aircraft:

Affected Propeller Serial Numbers

769303	769304	769571	769572	769573	769574	769575
769576	769577	769578	769579	769580	769581	769582
769583	769584	769585	769586	769587	769588	769589
769590	770176	770177	770178	770179	770601	770602
770603	770604	770605	770606	770607	770643	770644
770645	770646	770647	770648	770649	770650	770651
770652	770653	770654	771239	771291	771318	771319
771320	771321	771322	771323	771324	771325	771326
771327	771328	771329	771330	771331	771332	771333
771334	771335	771491	771492	771493	771495	771496
771497	771498	771499	771500	771534	771535	771536
771537	771538	771539	771540	771734	771735	771736
771737	771738	771739	771740	771741	771742	771743
771744	771745	771746	771747	771748	771839	771840
771841	771843	771848	772212	772213	772335	772336
772337	772338	772339	772340	772341	772342	772343
772344	772345	772346	772347	772348	772349	772396
772397	772398	772399	772400	772401	772429	772430
772432	772433	772434	772435	772436	772437	772438
772439	772440	772952	772953	772958	772959	772960
772961	772994	772995	772996	772997	772998	772999
773000	773047	773048	773049	773050	773051	773052
773053	773054	773055	773056	773057	773058	773059
773060	773061	773062	773066	773184	773185	773186
773187	773188	773189	773190	773191	773348	773349
773350	773351	773352	773353	773356	773358	773359
773360	773361	773573	773574	773575	773896	773897
773898	773899	773903	773966	773969	773970	773971
773973	773974	774113	774116	774122	774124	774175
774178	774180	774181				

NOTE: Serial numbers are stamped on the side of the propeller hub. These propellers are equipped with Model 90UMB-0 blades.

Compliance required before further flight, except that the airplane may be flown in accordance with FAR 21.197 to a Federal Aviation Administration Certificate Propeller Repair Station.

To prevent possible blade pitch control failures, accomplish the following:

(a) Replace blade actuating pin screws, P/N A-1635-104 (cadmium plated), with new screws, P/N A-1635-108 (black oxide) in accordance with McCauley Service Bulletin No. 131 dated January 20, 1978, and Service Manual No. 751201 or later Federal Aviation Administration approved revisions.

(b) Replacement of the above parts must be accomplished by a Federal Aviation Administration Certificated Propeller Repair Station, since it is considered a major repair.

(c) When the affected propellers are approved for return to service, compliance with this airworthiness directive shall be noted in the Aircraft's Records.

The manufacturer's specifications and procedures identified in this directive are incorporated herein and made part hereof pursuant to 5 U.S.C. 552(a)(1). All persons affected by the directive who have not already received these documents from the manufacturer, may obtain copies upon request to McCauley Accessory Division, Cessna Aircraft Company, Box 7, Roosevelt Station, Dayton, Ohio 45417. These documents may also be examined at the Great Lakes Regional Office, 2300 East Devon Avenue, Des Plaines, Illinois 60018, and at FAA Headquarters, 800 Independence Avenue, S.W., Washington, D.C. 20591. A historical file on this airworthiness directive which includes incorporated material in full is maintained by the FAA at its headquarters in Washington, D.C., and the Great Lakes Region.

Amendment 39-3101 became effective March 22, 1978.

This amendment 39-3233 becomes effective on June 7, 1978.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_78-06-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
78-06-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
MCCAULEY PROPELLERS Model 3FF32C501 Propellers
Subject:
Blade Actuating Pin Screws
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
06/07/1978
Make:
McCauley Propeller Systems
Model:
3FF32C501
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: 78-06-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3233

AD NUMBER:   78-06-02

SUBJECT HEADING:   MCCAULEY PROPELLERS Model 3FF32C501 Propellers

ACTION:  

SUMMARY:  

DATES:   Effective June 7, 1978.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
78-06-02 MCCAULEY PROPELLERS: Amendment 39-3159 as amended by Amendment 39-3233. Applies to the following three bladed full feathering constant speed Model 3FF32C501 propellers installed on but not limited to the Cessna Model 421C and 404 aircraft:

Affected Propeller Serial Numbers

769303	769304	769571	769572	769573	769574	769575
769576	769577	769578	769579	769580	769581	769582
769583	769584	769585	769586	769587	769588	769589
769590	770176	770177	770178	770179	770601	770602
770603	770604	770605	770606	770607	770643	770644
770645	770646	770647	770648	770649	770650	770651
770652	770653	770654	771239	771291	771318	771319
771320	771321	771322	771323	771324	771325	771326
771327	771328	771329	771330	771331	771332	771333
771334	771335	771491	771492	771493	771495	771496
771497	771498	771499	771500	771534	771535	771536
771537	771538	771539	771540	771734	771735	771736
771737	771738	771739	771740	771741	771742	771743
771744	771745	771746	771747	771748	771839	771840
771841	771843	771848	772212	772213	772335	772336
772337	772338	772339	772340	772341	772342	772343
772344	772345	772346	772347	772348	772349	772396
772397	772398	772399	772400	772401	772429	772430
772432	772433	772434	772435	772436	772437	772438
772439	772440	772952	772953	772958	772959	772960
772961	772994	772995	772996	772997	772998	772999
773000	773047	773048	773049	773050	773051	773052
773053	773054	773055	773056	773057	773058	773059
773060	773061	773062	773066	773184	773185	773186
773187	773188	773189	773190	773191	773348	773349
773350	773351	773352	773353	773356	773358	773359
773360	773361	773573	773574	773575	773896	773897
773898	773899	773903	773966	773969	773970	773971
773973	773974	774113	774116	774122	774124	774175
774178	774180	774181				

NOTE: Serial numbers are stamped on the side of the propeller hub. These propellers are equipped with Model 90UMB-0 blades.

Compliance required before further flight, except that the airplane may be flown in accordance with FAR 21.197 to a Federal Aviation Administration Certificate Propeller Repair Station.

To prevent possible blade pitch control failures, accomplish the following:

(a) Replace blade actuating pin screws, P/N A-1635-104 (cadmium plated), with new screws, P/N A-1635-108 (black oxide) in accordance with McCauley Service Bulletin No. 131 dated January 20, 1978, and Service Manual No. 751201 or later Federal Aviation Administration approved revisions.

(b) Replacement of the above parts must be accomplished by a Federal Aviation Administration Certificated Propeller Repair Station, since it is considered a major repair.

(c) When the affected propellers are approved for return to service, compliance with this airworthiness directive shall be noted in the Aircraft's Records.

The manufacturer's specifications and procedures identified in this directive are incorporated herein and made part hereof pursuant to 5 U.S.C. 552(a)(1). All persons affected by the directive who have not already received these documents from the manufacturer, may obtain copies upon request to McCauley Accessory Division, Cessna Aircraft Company, Box 7, Roosevelt Station, Dayton, Ohio 45417. These documents may also be examined at the Great Lakes Regional Office, 2300 East Devon Avenue, Des Plaines, Illinois 60018, and at FAA Headquarters, 800 Independence Avenue, S.W., Washington, D.C. 20591. A historical file on this airworthiness directive which includes incorporated material in full is maintained by the FAA at its headquarters in Washington, D.C., and the Great Lakes Region.

Amendment 39-3101 became effective March 22, 1978.

This amendment 39-3233 becomes effective on June 7, 1978.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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