Piedmont Propulsion Systems LLC
PMA PQ04267CE · 10 approved parts replacing 10 OEM numbers · Hamilton Sundstrand, Dowty, Hamilton Sundstrand Corporation
| PMA part | Replaces | Name | Make / model | Status | On PartsAndPlanes | DLA paid (OEM no.) |
|---|---|---|---|---|---|---|
| PPS-1007556-3 | 1007556-3 | Blade Sheath | Hamilton Sundstrand Corporation 14SF-17 | 14SF-19 | Current, Jun 2024 | — | — |
| PPS-599036-12 | 599036-12 | Outer Bearing Race | Hamilton Sundstrand 14SF-5 | and -7 per P7NE | Current, Feb 2021 | — | — |
| PPS-750350302 | 750350302 | O-Ring | Dowty R354 per P12NER375 per P17NER389 per P30NER390 per P31NE | Current, Jun 2022 | — | — |
| PPS-750350507 | 750350507 | O-Ring | Dowty R354 per P12NER375 per P17NER389 per P30NER390 per P31NE | Current, May 2022 | — | — |
| PPS-772536-7 | 772536-7 | Blade Bearing | Hamilton Sundstrand -7 | -11 | -11E | -15 and -23 per P7NE14RF-9 | -19 | -21 | -23 | -35 | 14SF-5 | and -37 per P11NE | Current, Feb 2021 | — | — |
| PPS-782290-1 | 782290-1 | Wear Plate | Hamilton Sundstrand 14SF-5, -7, -11, -11E, -15, -23 per P7NE | Current, Mar 2019 | — | — |
| PPS-782290-1 | 782290-1 | Wear Plate | Hamilton Sundstrand 14SF -19 per P7NE | Current, Apr 2022 | — | — |
| PPS-782669-1 | 782669-1 | Hex Head Bolt | Hamilton Sundstrand -19 | -21 | -23 | -35 | 14SF-19 per A14EA and P7NE14RF-9 | and -37 per P11NE | Current, Apr 2022 | — | — |
| PPS-820436-1 | 820436-1 | Taper Bore Cone | Hamilton Sundstrand 14SF-19 per A14EA | Current, Apr 2022 | — | — |
| PPS-820566-1 | 820566-1 | Inner Sleeve | Hamilton Sundstrand -7 | -11 | -11E | -15 and -23 per P7NE14RF-9 | -19 | -21 | -23 | -35 | 14SF-5 | and -37 per P11NE | Current, Feb 2021 | — | — |
| PPS-R817405-2 | R817405-2 | Bolt | Hamilton Sundstrand Corporation 568F-1 | 568F-5 | 568F-7 | Current, Sep 2024 | — | — |
Sell any of these? List it free and this table names you, as does the page of every OEM number it replaces.
Source: the FAA PMA database, refreshed weekly. A PMA part is approved for the specific eligibility on its FAA record; whether it may be installed on a particular aircraft, engine or component is the installer's determination.