FAA-PMA holders · By make · Piper
FAA-PMA parts for Piper -161
9 approved part numbers from 8 holders carry the Piper -161 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
- Aviation Products Systems Inc. · 2 parts
- Continental Motors Inc. · 1 part
- Hartzell Engine Technologies LLC · 1 part
- Lord Corporation · 1 part
- PMA Products Inc. · 1 part
- Steinbach & Associates Inc. · 1 part
- Talco Aviation Corp. dba Rajay Turbo Products · 1 part
- Texas Aeroplastics · 1 part
Approved parts · in stock first
| PMA part | Replaces (OEM) | Name | Holder | Status | On PartsAndPlanes | DLA paid (OEM no.) |
|---|---|---|---|---|---|---|
| 10-357200-1 | 14314-02, 756115, 14314-002, 752-892, 688-178, 470-713, 470-652, 87329-003, 87329-03, 87329-04 | Switch, Ignition and Starter | Continental Motors Inc. | Current, Feb 2017 | — | — |
| 3920 | Modification Part | Inflatable Door Seal | Talco Aviation Corp. dba Rajay Turbo Products | Current, Jan 2020 | — | — |
| 60-79445-80A | 79445-00,79445-000 | Rear Bulkhead Door | Texas Aeroplastics | Current, Nov 2025 | — | — |
| 98030000 | Modification Part | Refrigerant Cooling Conversion Kit | Steinbach & Associates Inc. | Current, Jul 2010 | — | — |
| ALY-6522 | Electrosystems ALY-6522R | Alternator Assembly | Hartzell Engine Technologies LLC | Current, Feb 2022 | — | — |
| APS105-00200 | 105-00200 | Rivet | Aviation Products Systems Inc. | Current, Aug 2022 | — | — |
| APS66-10500 | 066-10500 | Brake Lining | Aviation Products Systems Inc. | Current, Aug 2022 | — | — |
| CA63530-100 | 63530-000 (Piper) | Trim Barrel | PMA Products Inc. | Current, Oct 2008 | — | — |
| SE- I 508-2 | Piper PIN 456-015 | Shimmy Damper | Lord Corporation | Current, Dec 2014 | — | — |
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.