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Teledyne Continental (TCM Engineering Report No. AER 9101),Textron Lycoming (O-290-D1A, D1B, D1D, D2A, D2G, D2H, D2J, D3G, E1A, E2A, E2D, E2G, E2H, E3D, E3H, IO-320-B1A, B1B, B1C, B2A, C1A, C1B, E1A, E1B, E2A, E2B, F1A, AEIO-320-E1A, E1B, E2A, E2B, O-340-A1A, A2A, B1A, O-360-A1A, A1A, A1H, A2A, A2H, A3A, A4A, A4D, A4J, A4K, A4M, A4N, B1A, B2A, C1A, C1E, C1G, C2A, C2B, C2E, D1A, D2A, F1A6, G1A6, IO-360-B4A, AEIO-360-B4A, VO-360-A1A engines, O-235-C1, C1A, C1C, C2A, C2C, E1, E2A, F1, F2A, G1, G2A, H2C, J2A, M2C, M3C, N2C, P2C, P3C, O-290-D, D2, D2A, D2B,O-320-A1A, A1B, A2A, A2B, A2D, A3A, A3B, B1A, B1B, B2A, B3A, B3B, C1A, C1B, C2A, C2B, C3A, C3B,)
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