FAA-PMA parts for Saberliner
5 approved part numbers from 2 holders on the FAA's Parts Manufacturer Approval list for Saberliner (FAA records under Saberliner, Saberliner). Pick a model for its own page, or search any OEM number: the approved replacements are on its part page.
Models
- NA-265-40 4
- NA265-60 4
- NA-265-65 2
- NA-265-65) BOEING (717-200 2
- -30 1
- -40 1
- -60 1
- -65 1
- -70 1
- -80 1
- CORP. MODELS NA-265-20 1
Holders with the most Saberliner approvals
- Timken Corporation · 4 parts
- Aero Fluid Products · 1 part
Approved parts · in stock first
| PMA part | Replaces (OEM) | Name | Holder | Model | Status | On PartsAndPlanes | DLA paid (OEM no.) |
|---|---|---|---|---|---|---|---|
| 7000-911521 | Saberliner P/N 370-870008-3 | Check Valve | Aero Fluid Products | Corp. Models NA-265-20, -30, -40, -60, -65, -70, -80 | Current, Jul 2013 | — | — |
| L305610 | L305610 | Cup | Timken Corporation | NA-265-40, NA265-60, NA-265-65 | Current, May 2016 | — | — |
| L305610 | L305610 | Cup | Timken Corporation | NA-265-40, NA265-60, NA-265-65 | Current, Jun 2014 | — | — |
| L305649 | L305649 | Cone | Timken Corporation | NA-265-40, NA265-60, NA-265-65 | Current, May 2016 | — | — |
| L305649 | L305649 | Cone | Timken Corporation | NA-265-40, NA265-60, NA-265-65 | Current, Jun 2014 | — | — |
| L610510 | L610510 | Cup | Timken Corporation | NA-265-40, NA265-60, NA-265-65)
BOEING (717-200 | Current, May 2016 | — | — |
| L610510 | L610510 | Cup | Timken Corporation | NA-265-40, NA265-60, NA-265-65)
BOEING (717-200 | Current, Jun 2014 | — | — |
| L610549 | L610549 | Cone | Timken Corporation | NA-265-40, NA265-60, NA-265-65)
BOEING (717-200 | Current, May 2016 | — | — |
| L610549 | L610549 | Cone | Timken Corporation | NA-265-40, NA265-60, NA-265-65)
BOEING (717-200 | Current, Jun 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.