AD 80-22-05

Airworthiness directive · Crankshaft Front Oil Seal · Continental Motors TSIO-520-M, TSIO-520-P and TSIO-520-R

Effective
October 24, 1980
Models
TSIO-520-M, TSIO-520-P, TSIO-520-R
Data sheet
TCDSE8CE
Registered aircraft
4,207 matched by model
Product
Engine
Amendment
39-3948

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

80-22-05 TELEDYNE CONTINENTAL MOTORS: Amendment 39-3948. Applies to engine models as follows: TSIO-520-M, serial numbers 511000 through 520187, 230126R through 230129R, 230131R through 230142R, and 230144R through 230146R, installed in, but not limited to, certain Cessna Models TU206G and T207A airplanes certificated in all categories; TSIO-520-P, serial numbers 513000 through 513620, and 236401R, installed in, but not limited to, certain Cessna Model P210N airplanes certificated in all categories; TSIO-520-R, serial numbers 512000 through 517961, 230226R, 230228R, 230230R through 230233R, 230235R through 230246R, and 230248R, installed in, but not limited to, certain Cessna Models T210M and T210N airplanes certificated in all categories. Compliance is required within the next 25 hours time in service after effective date of this AD, unless already accomplished. To prevent the crankshaft front oil seal being dislodged from the engine crankcase, accomplish the following: (a) Remove engine top cowl panel and left and right nose cowl sections. (b) Inspect the crankshaft front oil seal which is located on the crankshaft where it passes through the front engine case. If the seal is displaced or there is evidence of oil leakage, replace the oil seal in accordance with the appropriate maintenance manual. (c) Install two (2) seal half plates, TCM Part No. 641361, on the forward face of the crankcase with four (4) TCM Part No. 628321-.38 bolts. Torque bolts to 21-25 in-lbs. (d) Reinstall left and right nose cowl sections and engine top cowl panel, ensuring that baffle seals are fitted and turned in the correct direction. (e) Run the engine until normal operating temperature is reached and inspect crankshaft front oil seal for leaks. (f) Make an appropriate maintenance record entry. NOTE: Teledyne Continental Service Bulletin No. M80-20, dated September 12, 1980, pertains to this subject. An equivalent method of compliance may be approvedby the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Southern Region. This amendment is effective October 24, 1980.

Affected TCDS · 1

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

Registered aircraft · 4,207

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
  • Cessna3,273 aircraft
  • Beech672 aircraft
  • Piper173 aircraft
  • Raytheon61 aircraft
  • Mooney11 aircraft
  • Other makers1417 aircraft
By year built
19182003
Registered aircraft by year built: 3,742 aircraft
19181
19471
19482
19491
19561
19571
19622
19631
19642
19657
196615
196715
196813
196926
197016
197127
197297
1973141
1974138
1975174
1976238
1977288
1978481
1979589
1980438
1981364
1982158
198370
1984123
198586
198656
198725
198822
19893
19909
19919
19928
199311
199410
19957
19965
19976
199811
199913
200012
200115
20022
20032

465 with no year recorded

By model

Aircraft

See all 4,207 aircraft