FAA-PMA holders · By make · Piper
FAA-PMA parts for Piper -310
10 approved part numbers from 7 holders carry the Piper -310 on their FAA eligibility record. Search any OEM number from this aircraft and the approved replacements are on its part page, in stock first.
Holders
- Knots 2U Ltd. · 4 parts
- Aerospace Welding Minneapolis, Inc. · 1 part
- Aircraft Components Inc. · 1 part
- Continental Motors Inc. · 1 part
- Hartzell Engine Technologies LLC · 1 part
- Pacific Southwest Instruments · 1 part
- Rapco Inc. · 1 part
Approved parts · in stock first
| PMA part | Replaces (OEM) | Name | Holder | Status | On PartsAndPlanes | DLA paid (OEM no.) |
|---|---|---|---|---|---|---|
| 10-357487-242 | 10-176487-242, 492 687 | Starting Vibrator, S-1200 Series, 24 Volts Dc | Continental Motors Inc. | Current, Feb 2017 | — | — |
| 2037 | Modification Part | Gear Alert System | Aircraft Components Inc. | Current, Jun 2016 | — | — |
| A40263-00 | 40263-00 | Stud, Nose Gear Door Pick-Up | Aerospace Welding Minneapolis, Inc. | Current, Nov 2013 | — | — |
| ES66-33FM | Cleveland 066-03300 | Brake Lining | Hartzell Engine Technologies LLC | Current, Oct 2010 | — | — |
| ES66-33FM | Cleveland 066-03300 | Brake Lining | Hartzell Engine Technologies LLC | Current, Feb 2013 | — | — |
| GF40364-02 | 40364-02 | Tip - Stabilizer | Knots 2U Ltd. | Current, Jan 2012 | — | — |
| GF43741-00 | 43741-00 | Tip - Elevator Left | Knots 2U Ltd. | Current, Jan 2012 | — | — |
| GF43741-01 | 43741-01 | Tip - Elevator Right | Knots 2U Ltd. | Current, Jan 2012 | — | — |
| GF43786-00 | 43786-00 | Tip - Elevator Leading Edge | Knots 2U Ltd. | Current, Jan 2012 | — | — |
| P628-6938-001 | 628-6938-001 | Front Panel Assembly | Pacific Southwest Instruments | Current, Jul 2010 | — | — |
| RA177-01600 | Cleveland Wheels & Brakes P/N 177-01600 | Brake Pin | Rapco Inc. | Current, Jul 2010 | — | — |
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.