AD/ELECT/40 - Slick Magneto Coil
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 107 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
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Electrical Equipment
AD/ELECT/40 Slick Magneto Coil 11/81
Applicability: SLICK magnetos model No. 4201, 4201R, 4216, 4216R, 4230, 4230R, 4250, 4250R,
4251, 4251R, 4252, 4252R, 4281, 4281R, 6210, 6210R, 6214 and 6214R.
The Serial Number range of these magnetos includes:
| 8100000-8109999 | October, 1978 |
|---|---|
| 8110000-8119999 | November, 1978 |
| 8120000-8129999 | December, 1978 |
| 9010000-9019999 | January, 1979 |
| 9020000-9029999 | February, 1979 |
| 9030000-9039999 | March, 1979 |
| 9040000-9049999 | April, 1979 |
| 9050000-9059999 | May, 1979 |
| 9060000-9069999 | June, 1979 |
| 9070000-9079999 | July, 1979 |
| 9080000-9089999 | August, 1979 |
| 9090000-9099999 | September, 1979 |
| 9100000-9109999 | October, 1979 |
| 9110000-9119999 | November, 1979 |
| 9120000-9129999 | December, 1979 |
| 0010000-0019999 | January, 1980 |
| 0020000-0029999 | February, 1980 |
| 0030000-0039999 | March, 1980 |
| 0040000-0049999 | April, 1980 |
The above magneto models are installed on, but not limited to the following engines:
| Teledyne Continental | ||
|---|---|---|
| A-65 | C-90 | O-470 |
| A-75 | O-200 | IO-470 |
| C-75 | IO-360 | IO-520 |
| C-85 | TSIO-360 | TSIO-520 |
Lycoming
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 107 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
| 0-235-H2C | 0-320-E1J | 0-360-C1E |
|---|---|---|
| 0-235-K2C | 0-320-E2D | 0-360-C1F |
| 0-235-L2C | 0-320-E2G | 0-360-C2E |
| 0-320-A2D | 0-320-E3D | 0-360-F1A6 |
| 0-320-D1D | AEI0-320-E1B | AEI0-360-B1G6 |
| 0-320-D2G | AEI0-320-E2B | AEI0-360-H1A |
| 0-320-D2J | 0-360-A4K | |
| 0-320-D3G | 0-360-A4M |
Document: Slick SB1-81. Lycoming SB457A, Cessna SIL SE81-30 and FAA AD 81-16-05 also refer.
Compliance: Within the next 100 hours time in service after 30 November 1981.
Background: The manufacturer has indicated that a situation exists in a certain group of coils that could facilitate cracking of the coil potting compound and a subsequent shorting failure. The above group include coils which have already failed in service both in Australia and overseas.