AD/COOL/2 - Stewart Warner Oil Coolers - Inspection and Replacement

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B08659 In force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 107 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Coolers

 

AD/COOL/2 Stewart Warner Oil Coolers - Inspection NK

and Replacement

Applicability: Stewart Warner Oil Coolers:

 

Stewart-Warner Model Numbers

Begining Serial Numbers

Ending Serial Numbers

8406J

12558

16212

8406L

1496

1763

8432K

514

541

8432L

631

964

10568C

1105

1141

10578B

2212

2316

10599A

7369

9013

10610A

815

1956

10614A

732

947

10622A

334

394

10634D

105

907

8446C

575

629

8437C

422

472

10641B

143

162

8493B

1269

1603

 

Which do not have a date ink stamped next to the nameplate.

 

Note: Oil coolers of the above model and S/Nos. that do have a date ink stamped next to the nameplate have been inspected and found satisfactory for continued use.

 

Requirement: 1. Inspect the engine oil cooler for applicability within the affected model and serial number range.

 

2.    If the oil cooler has accumulated 10 hours or less time in service since new, replace with a serviceable cooler not of the above serial numbered range unless the serial number has a date ink stamped next the oil cooler nameplate.

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 107 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 

3.    If the oil cooler has accumulated more than 10 hours time in service since new, inspect the cooler for oil leakage.

 

4.    If leakage is evident, replace cooler as in paragraph 2.

 

5.    If no leakage is evident, fabricate and install the following placard on the aircraft instrument panel:

 

"Visually inspect oil cooler for leakage prior to each flight".

 

Note 1: FAA AD 80-25-07 refers.

 

Note 2: This inspection may be performed by the pilot.

 

These oil coolers may be installed on, but not limited to, the following aircraft:

 

Bellanca Models :

7GCAA, 7GCBC, 7KCAB, 8GCBC and 8KCAB.

Cessna Models:

152, A152, F152, FA152, 172I, 172K, 172L, 172M,

(including Reims Aviation)

172N, 172P, 172RG, F172L, F172M, F172P, 177,

 

177A, 177B, 177RG, F177RG, R182, FR182, TR182,

 

T182, A188B, T188C, 210N, T210N and P210N.

Piper Models:

PA-38-112 and PA-44.

Mooney Models:

M20C, M20E, M20F, M20G and M20J.

Great Lakes Models:

2T-1A-1 and 2T-1A-2.

Beech Models:

76, 77 and C-23.

Compliance: For Para. 2 - Inspect before further flight. Replace within 10 hours time in service.

 

For Para. 3 - Inspect before further flight.

 

Background: Improper heat treatment during manufacture has resulted in several failures of oil coolers overseas. In flight failure of an oil cooler may be a fire hazard.

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.