Airworthiness Directive · Amendment 39-15986 · Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating Engines With Superior Air Parts, Inc. (SAP) Cylinder Assemblies Installed
Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating Engines With Superior Air Parts, Inc. (SAP) Cylinder Assemblies Installed
Superseded. A later AD replaced this one: AD 2014-05-29. Comply with the one in force.
This AD applies to Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 series reciprocating engines with SAP investment cast cylinder assemblies, part numbers (P/Ns) SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P, installed. These engines are installed on, but not limited to, the airplanes listed in Table 1 of this AD.
| Engine model | Aircraft manufacturer | Aircraft model designation |
|---|---|---|
| IO-520-A | Cessna | 210 D, E, F, G, & H. |
| IO-520-A | Cessna | 206. |
| IO-520-A | Cessna | P206. |
| IO-520-A | Rockwell | 200 D. |
| IO-520-B | Beechcraft | 36 Bonanza. |
| IO-520-B | Beechcraft | A36. |
| IO-520-B | Navion | Range Master. |
| IO-520-BA | Beechcraft | A36. |
| IO-520-BA | Beechcraft | S & V35, V35A, V35B. |
| IO-520-BA | Beechcraft | C33 A. |
| IO-520-BA | Beechcraft | E33 A & C. |
| IO-520-BA | Beechcraft | F33 A & C. |
| IO-520-BA | Navion | Range Master. |
| IO-520-BB | Beechcraft | A36. |
| IO-520-BB | Beechcraft | V35B. |
| IO-520-BB | Beechcraft | F33 A. |
| IO-520-C & CB | Beechcraft | C55-E55 Baron. |
| IO-520-D | Bellanca | 17-30 Viking. |
| IO-520-D | Cessna | A188-300 AG Truck. |
| IO-520-D | Cessna | 185. |
| IO-520-E | (Cessna 310) | Exec 600. |
| IO-520-E | (Beech Baron) | Pres 600. |
| IO-520-F | Cessna | 207. |
| IO-520-F | Cessna | U206. |
| IO-520-K | Bellanca | 17-30A. |
| IO-520-L | Cessna | 210 K, L, M, N & R. |
| IO-520-L | Cessna | 210N II. |
| IO-520-L | Cessna | 210R. |
| IO-520-M | Cessna | 310R. |
| IO-520-MB | Cessna | 310R. |
| IO-550-A | Cessna | 310 Conversion. |
| IO-550-B | Beechcraft | A36. |
| IO-550-B | (Beech Bonanza) | Foxstar. |
| IO-550-C | Beechcraft | 58 Baron. |
| IO-550-D | Cessna | 185/188 Conversion. |
| IO-550-E | Cessna | 310 Conversion. |
| IO-550-F | Cessna | 206/207 Conversion. |
| IO-550-L | Cessna | 210 Conversion. |
The FAA is adopting a new airworthiness directive (AD) for certain TCM IO-520, TSIO-520, and IO-550 series reciprocating engines, with certain SAP investment cast cylinder assemblies installed. This AD requires initial and repetitive inspections and compression tests to detect cracks in those cylinders with more than 750 flight hours (FH) time-in-service (TIS). This AD results from reports of cracks in the area of the exhaust valve and separation of cylinder heads from the barrels of SAP cylinder assemblies with certain part numbers. We are issuing this AD to prevent the separation of the cylinder head, which could result in immediate loss of engine power, possible structural damage to the engine, and possible fire in the engine compartment.
You are responsible for having the actions required by this AD performed within the compliance times specified unless the actions have already been done.
If the engine records don't contain the P/N of the cylinder heads, do the following:
(1) Remove the valve cover from the cylinder assembly.
(2) Look at the cylinder head for the P/N SAC 52001 I or SAC 55001 I and the word “AMCAST.”
(g) For TCM IO-520, TSIO-520, and IO-550 series reciprocating engines with SAP investment cast cylinder assemblies, P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P, installed, with over 750 flight hours (FH) time-in-service (TIS), do the following within 25 FH TIS after the effective date of this AD:
(1) Inspect each cylinder head around the exhaust valve side for visual cracks or any signs of black combustion leakage.
(2) Replace any cracked or leaking cylinders before further flight.
(3) Perform a standard cylinder compression test. Guidance on standard cylinder compression tests can be found in Teledyne Continental Aircraft Engine Service Bulletin SB03-3, Differential Pressure Test and Borescope Inspection Procedures for Cylinders, dated March 28, 2003.
(i) If the cylinder pressure gauge reads below 60 pounds per-square inch, determine if the unacceptable pressure is due to a cracked cylinder.
(ii) To check the cylinder, apply a 2 percent soapy water solution to the side of the leaking cylinder.
(iii) If you see air bubbles, indicating air leakage, on the side of the cylinder head, or near the head-to-cylinder interface, replace the cylinder assembly before further flight.
(h) Thereafter, repeat the cylinder visual inspections and compression tests within 50 FH time-since-last inspection (TSLI) until the cylinders reach their time-between-overhaul (TBO) limits specified in Teledyne Continental Aircraft Engine Service Information Letter SIL98-9A, Revision A, dated March 28, 2003.
(i) For TCM IO-520, TSIO-520, and IO-550 series reciprocating engines with SAP investment cast cylinder assemblies, P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P, replace the SAP cylinder head assembly at the first TBO after the effective date of this AD. Engines that were already overhauled may continue in service until the first TBO after the effective date of this AD.
After the effective date of this AD, do not install any SAP investment cast cylinder assembly, P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P, in any engine.
The aircraft, engines and makers this AD names, by the model designations in its text. A model listed here may still be outside the AD's serial ranges.