AD 50-20-01

Airworthiness directive · Crankcase · Continental Motors C145-2 and C145-2H

Models
C145-2, C145-2H
Data sheet
TCDSE-253
Registered aircraft
1,840 matched by model
Product
Engine

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

50-20-01 CONTINENTAL: Applies to All Model C145 Engines, Serially Numbered 3000 to 5031 Inclusive, Except: Nos. 3612, 4650, 4652, 4654, 4671, 4676, 4679, 4683, 4690, 4710, 4855, 4889, 4904, 4996, 4997, 5002 Through 5021, 5023 Through 5029. Compliance required by June 1, 1950, and each 25-hour period of operation thereafter. To minimize possible engine operation difficulty due to crankcase and/or cylinder barrel failures, the following inspection procedure should be accomplished as indicated. (1) Visually inspect crankcase for cracks giving special attention to those areas around each cylinder base. This portion of the inspection need not be accomplished or new type crankcases (P/N 530836 and 530837) which are incorporated on all serially numbered engines above No. 4383, and on all engines overhauled by the manufacturer after September 1, 1949. This new type crankcase can be identified by throughbolts (extending through both halves of crankcase) located ahead of the frontcylinder and adjacent to nose oil seal. The old style crankcase (P/N 6642 and 6643) requiring inspection has studs at this location extending through one crankcase half only. (2) Visually inspect cylinder barrels for cracks at the base flange fillet. New flanged-typed cylinder base nuts, P/N 531001 and 531003 have been made available for service operation. This portion of the inspection may be discontinued upon accomplishing one additional 25-hour inspection including a torque check after installation of these new flanged nuts. During installation of new cylinder base nuts, special attention should be given to the removal of paint and burrs from the cylinder flange nut seat and to compliance with the engine manufacturer's torque limits of 500 plus or minus 10 inch-pounds for the 7/16 studs and through bolts, and 420 plus or minus 10 inch-pounds for 3/8 studs. Improperly torqued nuts are a major contributing factor to cylinder barrel, cylinder base studs, and crankcase failures. The engines exempted from this inspection, as indicated above, have had the new flanged nuts installed at the manufacturer's plant. Since small cracks are more easily detectable by oil leaks, it is recommended that each inspection include a run-up with a clean engine. (Continental Motors Corp. Service Bulletin No. M50-2 covers this same subject.) This supersedes AD 50-18-04.

Affected TCDS · 1

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

Registered aircraft · 1,840

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
  • Cessna1,562 aircraft
  • Aeronca146 aircraft
  • Globe60 aircraft
  • Temco25 aircraft
  • Universal11 aircraft
  • Other makers1536 aircraft
By year built
19402026
Registered aircraft by year built: 1,566 aircraft
19402
19413
194659
19473
1948266
1949148
1950189
1951119
1952370
1953227
1954133
195518
195612
19572
19592
19602
19651
19681
19751
19761
19801
19831
19861
19891
20041
20051
20261

274 with no year recorded

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