AD 76-21-06

final rule

Airworthiness Directives; CESSNA Models 172M, 172N. 177B and 177RG Airplanes

AD Number
76-21-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Applicability

TypeManufacturerModelDetails
aircraft Cessna Aircraft Company 172M Airworthiness Directives; CESSNA Models 172M, 172N. 177B and 177RG Airplanes
aircraft Cessna Aircraft Company 172N Airworthiness Directives; CESSNA Models 172M, 172N. 177B and 177RG Airplanes
aircraft Cessna Aircraft Company 177B Airworthiness Directives; CESSNA Models 172M, 172N. 177B and 177RG Airplanes
aircraft Cessna Aircraft Company 177RG Airworthiness Directives; CESSNA Models 172M, 172N. 177B and 177RG Airplanes

Unsafe Condition

Loss of engine oil due to Model 8406J (S/N 101 thru 1500) or Model 10599A (S/N 101 thru 700) engine oil cooler fluid fitting side.

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

Required Actions

Before next flight, inspect the engine oil cooler fluid fitting side to determine if it is Model 8406J (S/N 101-1500) or Model 10599A (S/N 101-700). If not, record the inspection and return to service. If it is, replace the cooler with a serviceable one not of those models/serials before further flight.

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

Compliance Time

Before next flight (inspection) and prior to further flight (replacement if required).

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

Affected Aircraft

CESSNA Models 172M (Serial Numbers 17266981-17267584); 172N (specific serial ranges listed); 177B (Serial Numbers 17702450-17702536, 17702538-17702544); 177RG (Serial Numbers 177RG0875-177RG0990, 177RG0992-177RG0995, 0997-1000, 1002, 1004)

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

Federal Register Abstract

Loss of Engine Oil

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_76-21-06.html
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AD Number:
76-21-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; CESSNA Models 172M, 172N. 177B and 177RG Airplanes
Subject:
Loss of Engine Oil
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/26/1976
Make:
Cessna Aircraft Company
Model:
172M | 172N | 177B | 177RG
Product Type:
Aircraft
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 76-21-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2750

AD NUMBER:   76-21-06

SUBJECT HEADING:   Airworthiness Directives; CESSNA Models 172M, 172N. 177B and 177RG Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective October 26, 1976.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
76-21-06 CESSNA: Amendment 39-2750. Applies to Models 172M (Serial Numbers 17266981 thru 17267584); 172N (Serial Numbers 17267585 thru 67610, 612 thru 621, 623 thru 626, 628 thru 634, 636, 638 thru 648, 651 thru 655, 657, 658, 660 thru 666, 669, 670, 673 thru 679, 681, 682, 684 thru 687, 689, 691 thru 698, 700, 701, 703 thru 706, 708 thru 713, 715, 718, 722 thru 724, 727 thru 729, 732, 736, 738, 739, 74l thru 744, 746 thru 749, 752, 754, 756, 757, 759, 760, 763, 764, 770, 772, 776, 785, 791 and 800); 177B (Serial Numbers 17702450 thru 17702536, 17702538 thru 17702544); and 177RG (Serial Numbers 177RG0875 thru 177RG0990, 177RG0992 thru 177RG0995, 0997 thru 1000, 1002 and 1004) airplanes.

Compliance: Required as indicated, unless already accomplished.

To prevent loss of engine oil, accomplish the following:

A) Before next flight of the affected airplanes, remove the lower engine cowl and visually inspect the engine oil cooler fluid fitting side to determine whether it is a Model 8406J (S/N 101 thru 1500) or Model 10599A (S/N 101 thru 700).

1. If the oil cooler is not of the model and serial number listed above, make an entry in the aircraft maintenance records indicating that this AD has been accomplished and the airplane may be returned to service.

2. If the oil cooler is of a model and serial number listed above, prior to further flight, replace this cooler with a serviceable oil cooler not of the above model and serial numbers.

B. The inspection and maintenance record entry required by Paragraph A(l) may be accomplished by holder of a pilot's certificate issued under Part 61 of the Federal Aviation Regulations on any aircraft owned or operated by him.

C. Any equivalent method of compliance with this AD must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.

Cessna Service Letter SE76-17 pertains to this subject.

NOTE: A ferry permit to accomplish a needed oil cooler replacement may be issued under the provisions of FAR 21.197 by FAA District Offices, with appropriate limitations, in coordination with the Chief, Engineering and Manufacturing Branch, FAA. Central Region.

This amendment becomes effective October 26, 1976, to all persons except those to whom it was made effective earlier by air mail letters issued September 21, 1976, and October 1, 1976, respectively.


FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_76-21-06.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
76-21-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; CESSNA Models 172M, 172N. 177B and 177RG Airplanes
Subject:
Loss of Engine Oil
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/26/1976
Make:
Cessna Aircraft Company
Model:
172M | 172N | 177B | 177RG
Product Type:
Aircraft
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 76-21-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2750

AD NUMBER:   76-21-06

SUBJECT HEADING:   Airworthiness Directives; CESSNA Models 172M, 172N. 177B and 177RG Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective October 26, 1976.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
76-21-06 CESSNA: Amendment 39-2750. Applies to Models 172M (Serial Numbers 17266981 thru 17267584); 172N (Serial Numbers 17267585 thru 67610, 612 thru 621, 623 thru 626, 628 thru 634, 636, 638 thru 648, 651 thru 655, 657, 658, 660 thru 666, 669, 670, 673 thru 679, 681, 682, 684 thru 687, 689, 691 thru 698, 700, 701, 703 thru 706, 708 thru 713, 715, 718, 722 thru 724, 727 thru 729, 732, 736, 738, 739, 74l thru 744, 746 thru 749, 752, 754, 756, 757, 759, 760, 763, 764, 770, 772, 776, 785, 791 and 800); 177B (Serial Numbers 17702450 thru 17702536, 17702538 thru 17702544); and 177RG (Serial Numbers 177RG0875 thru 177RG0990, 177RG0992 thru 177RG0995, 0997 thru 1000, 1002 and 1004) airplanes.

Compliance: Required as indicated, unless already accomplished.

To prevent loss of engine oil, accomplish the following:

A) Before next flight of the affected airplanes, remove the lower engine cowl and visually inspect the engine oil cooler fluid fitting side to determine whether it is a Model 8406J (S/N 101 thru 1500) or Model 10599A (S/N 101 thru 700).

1. If the oil cooler is not of the model and serial number listed above, make an entry in the aircraft maintenance records indicating that this AD has been accomplished and the airplane may be returned to service.

2. If the oil cooler is of a model and serial number listed above, prior to further flight, replace this cooler with a serviceable oil cooler not of the above model and serial numbers.

B. The inspection and maintenance record entry required by Paragraph A(l) may be accomplished by holder of a pilot's certificate issued under Part 61 of the Federal Aviation Regulations on any aircraft owned or operated by him.

C. Any equivalent method of compliance with this AD must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.

Cessna Service Letter SE76-17 pertains to this subject.

NOTE: A ferry permit to accomplish a needed oil cooler replacement may be issued under the provisions of FAR 21.197 by FAA District Offices, with appropriate limitations, in coordination with the Chief, Engineering and Manufacturing Branch, FAA. Central Region.

This amendment becomes effective October 26, 1976, to all persons except those to whom it was made effective earlier by air mail letters issued September 21, 1976, and October 1, 1976, respectively.


FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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