FAA-PMA holders · By make · Beechcraft / Hawker
FAA-PMA parts for Beechcraft / Hawker 76
36 approved part numbers from 14 holders carry the Beechcraft / Hawker 76 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
- Hartzell Engine Technologies LLC · 11 parts
- S-Tec Corporation · 11 parts
- Knots 2U Ltd. · 3 parts
- Aerospace Turbine Rotables · 2 parts
- Hartzell Engine Technologies LLC · 2 parts
- Rosen Sunvisor Systems, LLC · 2 parts
- Aircraft Door Seals · 1 part
- Aviation Engineering Consultants Inc. (Aeci) · 1 part
- Continental Motors Inc. · 1 part
- Donaldson Company Inc. · 1 part
- LP Aero Plastics Inc. · 1 part
- Lamar Technologies LLC · 1 part
- Plane Power, Ltd. · 1 part
- Rnl Inc. · 1 part
Approved parts · in stock first
| PMA part | Replaces (OEM) | Name | Holder | Status | On PartsAndPlanes | DLA paid (OEM no.) |
|---|---|---|---|---|---|---|
| 10-357250-1 | 10-126660-1, 10-357250-1, 10-357220-1 | Switch, Ignition and Starter | Continental Motors Inc. | Current, Feb 2017 | — | — |
| 1160005-0 | Modification Part | Sunvisor System | Rosen Sunvisor Systems, LLC | Current, Feb 2010 | — | — |
| 1160007-0 | Modification Part | Sunvisor System | Rosen Sunvisor Systems, LLC | Current, Feb 2010 | — | — |
| 273, 273.187, 273.250 | BeechcraftP/N 169-420035-37 (169-420038-45 green tint) (169-420035-23, -35, -37, -43, -605) (169-420038-31, -45, -65, -67 green tint) | Windshield | LP Aero Plastics Inc. | Current, Dec 2007 | — | — |
| ADS-1200-7 | 105-420015-33, 115155X10ft., 35-400405-3, 35-400320-54 | Forward Cabin Entry Door Seal ( Continued) | Aircraft Door Seals | Current, Feb 2008 | — | — |
| ADS1200-17 | Aircraft Door Seals, LLC P/N ADS1200-17 | Seal (Storm Window) | Knots 2U Ltd. | Current, Jul 2017 | — | — |
| ADS1200-19 ADS1200-19 | Aircraft Door Seals, LLC P/N ADS1200-19 Aircraft Door Seals, LLC P/N ADS1200-19 | Seal (Storm Window) Seal (Storm Window) | Knots 2U Ltd. | Current, Jul 2017 | — | — |
| ADS1200-7 | Aircraft Door Seals, LLC P/N ADS1200-7 | Main Seal, (Front Entry Door | Knots 2U Ltd. | Current, Jul 2017 | — | — |
| AECI PN, 169-524050AEC | Raytheon P/N, 169-524050 | Bearing | Aviation Engineering Consultants Inc. (Aeci) | Current, Jun 2009 | — | — |
| AL12-P70 | Kelly Aerospace ALY-8420, ALY-8420R | Alternator Kit | Hartzell Engine Technologies LLC | Current, Nov 2014 | — | — |
| AL12-P70 | Kelly Aerospace ALY-8420, ALY-8420R | Alternator Kit | Plane Power, Ltd. | Current, Nov 2009 | — | — |
| AL24-P70 | Kelly Aerospace ALU-8421 | Alternator Kit | Hartzell Engine Technologies LLC | Current, Nov 2014 | — | — |
| CD14019 | 07E94-1(EL), 07E94-2(EL) | Heater | Hartzell Engine Technologies LLC | Current, Apr 2016 | — | — |
| CD14019-1 | 07E94-1(EL) | Heater | Hartzell Engine Technologies LLC | Current, Apr 2016 | — | — |
| CD14020 | 07E94-2 | Heater | Hartzell Engine Technologies LLC | Current, Apr 2016 | — | — |
| CD14020-1 | 07E94-2(EL) | Heater | Hartzell Engine Technologies LLC | Current, Apr 2016 | — | — |
| CD20004 | 87D13-1, 87D13-2, 87D13-3 | Tube, Universal Combustion | Hartzell Engine Technologies LLC | Current, Apr 2016 | — | — |
| CD21156 | D08D09, 4091, 3061 8-5 | Nozzle, Fuel | Hartzell Engine Technologies LLC | Current, Apr 2016 | — | — |
| CD21384 | 09E80-1, 27D48 | Fan, 4 Blade | Hartzell Engine Technologies LLC | Current, Jun 2016 | — | — |
| CD21412 | 6310040081, K271-38SSL | Bearing | Hartzell Engine Technologies LLC | Current, Jun 2016 | — | — |
| CD21502 | 07D45, 752107 | Number Plate | Hartzell Engine Technologies LLC | Current, Jun 2016 | — | — |
| CD60535 | MS35489-18, MS35489-8S | Spark Plug Grommet | Hartzell Engine Technologies LLC | Current, Jun 2016 | — | — |
| P13-6680 | Beech P/N 105-389000-3 | Filter | Donaldson Company Inc. | Current, Oct 2009 | — | — |
| RN35-825145-2 | Beech P/N: 35-825145 and 35-825145-2 | Shimmy Damper | Rnl Inc. | Current, Feb 2008 | — | — |
| ST-073 | Modification Part | System 60 Single Axis Flight Guidance System | S-Tec Corporation | Current, Jan 2010 | — | — |
| ST-074 | Modification Part | System 60 Two Axis Automatic Flight Guidance System | S-Tec Corporation | Current, Jan 2012 | — | — |
| ST-075 | Modification Part | System 60 Pitch Stabilization System | S-Tec Corporation | Current, Jan 2010 | — | — |
| ST-076 | Modification Part | Yaw Damper System | S-Tec Corporation | Current, Jan 2012 | — | — |
| ST-105 | Modification Part | System 60 Single Axis Automatic Flight Guidance System | S-Tec Corporation | Current, Jan 2010 | — | — |
| ST-107 | Modification Part | System 60 Pitch Stabilization System | S-Tec Corporation | Current, Jan 2010 | — | — |
| ST-108 | Modification Part | Yaw Damper System | S-Tec Corporation | Current, Jan 2012 | — | — |
| ST-218-40/50 | Modification Part | System 40/50 Single and Two Axis Automatic Flight Guidance Systems | S-Tec Corporation | Current, May 2012 | — | — |
| ST-219-40/50 | Modification Part | System 40/50 Single and Two Axis Automatic Flight Guidance Systems | S-Tec Corporation | Current, May 2012 | — | — |
| ST-253 | Modification Part | Manual Electric Trim System | S-Tec Corporation | Current, May 2012 | — | — |
| ST-373 | Modification Part | System 65 Two Axis Automatic Flight Guidance System | S-Tec Corporation | Current, Jan 2012 | — | — |
| TR- 55-0069-1 | Grimes 55-0069-1 | Motor | Aerospace Turbine Rotables | Current, Mar 2015 | — | — |
| TR-55-0295-1 | Grimes 55-0295-1 | Contact | Aerospace Turbine Rotables | Current, Jan 2016 | — | — |
| VR-286 | Lamar Inc. B-00306-1, B-00306-2, B-00306-3 | Voltage Regulator | Hartzell Engine Technologies LLC | Current, Oct 2010 | — | — |
| VR-286 | Lamar Inc. B-00306-1, B-00306-2, B-00306-3 | Voltage Regulator | Hartzell Engine Technologies LLC | Current, Feb 2013 | — | — |
| VR286 | Lamar Inc. B-00306-1 B-00306-2 | Voltage Regulator 28V | Lamar Technologies LLC | Current, May 2013 | — | — |
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.