| P/N | LIMITATIONS | CMM ref | ELIGIBILITY |
|---|---|---|---|
| 2-1474-52-1474-7 | Up to and including heat sink change, except conversion of the piston housing assembly, threaded hole repair in the torque plate, bleeder port thread repair, nickel plating | 32-40-30
32-40-61 |
Boeing 737-200/300/400/500 |
| 2-16052-1605-1
2-1605-2 |
Up to and including heat sink change, except nickel plating | 32-48-33 | Bombardier DHC-8-400 |
| 2-16242-1624 OPT2 | Up to and including heat sink change, except nickel plating | 32-49-03 | Embraer ERJ145LR |
| 2-1457
2-1457-1 2-1457-2 |
Up to and including heat sink change, except installation of Lee plugs, nickel and chrome plating | 32-40-26
32-40-62 |
Boeing 757 |
| 2-1549-22-1549-3 | Up to and including heat sink change | 32-46-86 | ATR 42 |
| 2-1608-2 | Up to and including heat sink change, except nickel plating | 32-48-21 | Bombardier BD-700 Series (Global Express) |
| 2-1684 | Up to and including heat sink change, except chrome plating | 32-41-87 | A318, A319, A320 |
| 2-1587-1 | Up to and including heat sink change, except installation of Lee plugs and cadmium plating | 32-40-4832-40-63 | Boeing 737-600/700/800/900/BBJ |
| 2-17402-1740-1 | Up to and including heat sink change, except installation of Lee plugs and application of the SermeTel Process 2F-1 coating system | 32-42-27 | Boeing 737 NG
Boeing 737 MAX |
|
2-1577-1OPT1 2-1577-1OPT2 2-1577-2 2-1577-3 2-1577-4 2-1577-5 2-1577-6 2-1577-7 2-1577-8 2-1577-9 |
No limitations | 32-41-81 | A330 / A340 |
