AD 72-24-03

Airworthiness directive · Oil Filter Adapter · Continental Motors IO-360-A, IO-520-B, IO-520-C and 3 more

Effective
November 15, 1972
Models
IO-360-A, IO-520-B, IO-520-C, TSIO-520-B, TSIO-520-E, TSIO-520-J
Registered aircraft
15,585 matched by model
Product
Engine
Amendment
39-1554

Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.

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The airworthiness directive

72-24-03 TELEDYNE CONTINENTAL: Amendment 39-1554. Applies to Models IO-346-A, IO-520-B and -C and TSIO 520-B, -E, and -J engines having Teledyne Continental Part Number 631645 oil filter adapter installed, used with AC OF-9-A oil filter assembly. Compliance required as indicated, unless already accomplished. To prevent loss of oil accomplish the following or an equivalent procedure approved by the Chief, Engineering and Manufacturing Branch, Southern Region, Atlanta, Georgia: (A) Not later than next engine overhaul, replace Teledyne Continental Part Number 631645 oil filter adapter with strengthened Teledyne Continental Part Number 632881 (Kit Part Number 637584A1) in accordance with Teledyne Continental Service Bulletin M70-16 or AC Part Number 5579663 (Package No. 6437861) in accordance with AC instruction sheet 6439067. NOTE: The correct AC part may be identified by a cast-in insignia "A" (raised letter A with a raised bar over the letter A). All other AC adapters areineligible, including those identified by a plain raised letter "A" and a raised letter "A" and a raised dot (A) directly above. The Teledyne Continental adapter is identified by part number only. (B) Within 25 hours' time in service from the effective date of the amendment, unless already accomplished under AD 71-11-04, paragraph (B) inspect the base plate to determine whether the gasket retaining seat is wedge-shaped or rectangular. If the gasket seat is wedge-shaped, replace this part with improved Teledyne Continental Part Number 633750 or AC Part Number 6437508 (Package No. 6436627) base plate having a rectangular shaped gasket retaining seat. NOTE: The required base plate can be identified by the presence of a thin sheet metal square shouldered retaining ring spot welded around the gasket groove to hold the gasket in place. (C) Unless already accomplished within the last 50 hours' of service prior to date of this amendment, accomplish the following within the next 25hours' time in service and at every oil filter element change thereafter: (1) Visually inspect the upper surface of the oil filter adapter face using a light and mirror for indications of radial cracks inward from the outer edge. Replace any cracked adapters with serviceable parts prescribed in paragraph (A). (2) After placing filter element in housing in accordance with oil filter element manufacturers' instructions, install assembled housing and base plate to adapter as follows: a. Clean all gasket and seal surfaces. b. Lubricate new gasket well on both sides using engine oil. c. Install assembly on adapter and turn center stud to a light seal contact by hand. d. Visually inspect base plate to adapter seal for proper positioning and seating. e. Torque center studs to 15 - 18 lb. ft. If torque wrench is not available or center stud is inaccessible to torque wrench, tighten center stud 1 3/4 turns beyond point of initial seal contact. f. Re-attach upper bracket and resafety. g. Operate engine for approximately 5 minutes at 1000-2000 RPM. Check for oil leaks and proper assembly using a light and mirror if necessary. If a leak appears between top of housing and stud, remove stud and check for nicks or visual damage at sealing surface. Correct any damage and re-install using a new copper gasket. DO NOT INCREASE TORQUE TO STOP LEAKS. Continental Service Bulletin M66-6, dated April 28, 1966, refers to this subject. (D) The requirements of Paragraph (C) are no longer applicable when Paragraph (A) has been complied with. This airworthiness directive supersedes Amendment 39-1215, (36 F.R. 9241, 9242), A.D. 71-11-04, as amended by Amendments 39-1256, (39 F.R. 14127) and 39-1289, (39 F.R. 18373). This amendment becomes effective November 15, 1972.

Affected TCDS · 3

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 15,585

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Cessna8,074 aircraft
  • Beech5,960 aircraft
  • Bellanca461 aircraft
  • Cirrus Design303 aircraft
  • Piper212 aircraft
  • Other makers184575 aircraft
By year built
19182025
Registered aircraft by year built: 13,871 aircraft
19181
19441
194617
19477
19488
19494
19508
19512
19524
19532
19549
19558
195614
19574
19582
19594
19607
196110
196220
196364
1964441
1965389
1966633
1967546
1968537
1969441
1970300
1971249
1972441
1973662
1974667
1975836
1976941
19771,130
19781,120
19791,161
1980733
1981664
1982294
1983150
1984163
1985128
198685
198785
198892
198964
199081
199164
199239
199346
199428
199512
199612
199712
199817
199920
200048
200139
200267
200350
200460
200558
20067
20077
20088
20094
20109
201114
20124
20132
20141
20153
20162
20171
20193
20201
20221
20231
20252

1,714 with no year recorded

By model

Aircraft

See all 15,585 aircraft