Mooney M20C

1,122 parts applicable to this airframe — ga_single

Part Number	Description	Manufacturer	Airframe	ATA	Category	Status
0713130-1	Starting Vibrator, S-200 Series, 12 Volts DC	—	C185 Skywagon C210 Centurion+4	74	—	OEM
10-87998-121	Starting Vibrator, S-200 Series, 12 Volts DC	—	C185 Skywagon C210 Centurion+4	74	—	OEM
1049-4200-20	Connector Kit GDC31	DAC International	C172 Skyhawk C182 Skylane+43	25	Interior / Furnishings	PMA
115-00345-00	Tray, IFD5XX series	—	C172 Skyhawk C182 Skylane+37	34	—	OEM
130062-501	Cover, Hat Rack Strip	—	M20C M20E	25	—	OEM
130078-511	Deflector FWD	—	M20C M20E+2	25	—	OEM
130079-29	Strip, Trim	—	M20C M20E	25	—	OEM
130079-33	Panel, Armrest, RH	—	M20C M20E	25	—	OEM
130079-35	Moulding, Window, Rear, RH	—	M20C M20E	56	—	OEM
130079-55	Headliner, Hatrack	—	M20C M20E	25	—	OEM
130103	Cover Assy, Nose Wheelwell	—	M20C M20E	25	—	OEM
130103-15	Cover, RH	—	M20C M20E	25	—	OEM
130103-9	Cover, Lower Front	—	M20C M20E	25	—	OEM
130105-02	Moulding, Footwell RH	—	M20C M20E+1	50	—	OEM
130105-1	Moulding, Footwell LH	—	M20C M20E+1	50	—	OEM
130117	Panel Assy, Hat Rack Aft	—	M20C M20E	25	—	OEM
31-324	Starting Vibrator, S-200 Series, 12 Volts DC	—	C185 Skywagon C210 Centurion+4	74	—	OEM
340067-7	Window Moulding Door	—	M20C M20E	25	—	OEM
492 643	Starting Vibrator, S-200 Series, 12 Volts DC	—	C185 Skywagon C210 Centurion+4	74	—	OEM
492 674	Starting Vibrator, S-200 Series, 12 Volts DC	—	C185 Skywagon C210 Centurion+4	74	—	OEM
6078-1	REAR RH BAFFLE ASSEMBLY	—	M20C	71	—	OEM
6083	ROCKER COVER BAFFLE ASSEMBLY	—	M20C	71	—	OEM
6088	FWD RH BAFFLE ASSEMBLY	—	M20C	28	—	OEM
6092	FWD LH BAFFLE ASSEMBLY	—	M20C	71	—	OEM
610035-501	Pan, Fuel Selector Valve	—	M20C M20E	25	—	OEM
6104-03	Forward Spar Mount, Center	f atlee dodge aircraft services llc	M20C M20E+3	57	Structures	PMA
6104-1	TOP BAFFLE ASSEMBLY	—	M20C	71	—	OEM
6105	FWD BAFFLE ASSEMBLY	—	M20C 747+1	32	—	OEM
6242	ROCKER COVER BAFFLE ASSEMBLY	—	M20C	28	—	OEM
6246-1	ROCKER COVER BAFFLE ASSEMBLY	—	M20C 727+2	29	—	OEM
640030-09	Cover Plate Instrument Light	—	M20C M20E	20	—	OEM
640030-3	Cover Plate Dome Light	—	M20C M20E	25	—	OEM
640042-03	Cover, Vent Outlet	—	M20C M20E	25	—	OEM
6415	RH ACCESS PANEL	—	M20C	28	—	OEM
6416	RH ACCESS PANEL	—	M20C	28	—	OEM
810001-3	Cover Plate Speaker	—	M20C M20E	25	—	OEM
ALE-2008AA-AC	Stator	Hartzell Engine Technologies LLC	PA-28 Cherokee C310+21	25	Interior / Furnishings	PMA
ALE-2008AE-AC	Stator	Hartzell Engine Technologies LLC	PA-28 Cherokee C310+21	25	Interior / Furnishings	PMA
ALU-3045BS-AC	Brush Assembly	Hartzell Engine Technologies LLC	PA-28 Cherokee C310+21	24	Electromechanical	PMA
Cleveland Wheels and Brakes P/N 063-01200	Pressure Plate	—	C172 Skyhawk C182 Skylane+10	32	—	OEM
Dukes Inc. P/N 4140-00-21A	Pump-Motor Assembly	—	M20C	28	—	OEM
ELECTROAIR Part No EAREM37HE	Spark Plug	—	C172 Skyhawk PA-28 Cherokee+12	74	—	OEM
ELECTROAIR Part number EARHM38SE	Spark Plug	—	C172 Skyhawk PA-28 Cherokee+1	74	—	OEM
GNS430 Backplate	Tray, IFD4XX series	—	C172 Skyhawk C182 Skylane+49	34	—	OEM
GNS430 Tray 011-00676-00	Tray, IFD4XX series	—	C172 Skyhawk C182 Skylane+49	34	—	OEM
GNS530 Backplate	Tray, IFD5XX series	—	C172 Skyhawk C182 Skylane+37	34	—	OEM
GNS530 Tray 011-00671-00	Tray, IFD5XX series	—	C172 Skyhawk C182 Skylane+37	34	—	OEM
Weldon P/N 8164-A	Pump-Motor Assembly	—	M20C	28	—	OEM
XA-943FS-AC	Pos. Diode	Hartzell Engine Technologies LLC	PA-28 Cherokee C310+21	25	Interior / Furnishings	PMA
XA-944JS-AC	Neg. Diode	Hartzell Engine Technologies LLC	PA-28 Cherokee C310+21	25	Interior / Furnishings	PMA

Airworthiness Directive activity

FAA / EASA public regulatory data

1airworthiness directives affecting this fleet — recurring compliance demand for the parts and shops that serve it

Most recent

FAA AD 2023-02-04effective Feb 13, 2023Prohibition
The FAA is adopting a new airworthiness directive (AD) for certain Mooney International Corporation Model M20C, M20D, M20E, M20F, and M20G airplanes. This AD was prompted by reports of the hybrid material elevator balance weight cracking. This AD requires inspecting to determine whether a certain elevator balance weight is installed. If installed, this AD requires inspecting each affected elevator balance weight for corrosion and cracking, and depending on the findings, either replacing each affected elevator balance weight with a non- hybrid (lead) elevator balance weight or repetitively inspecting each affected elevator balance weight. This AD also prohibits the installation of an affected elevator balance weight on any airplane. The FAA is issuing this AD to address the unsafe condition on these products.

Directives linked to this airframe family in the FAA / EASA regulatory corpus we have processed — not a complete historical AD list. An AD is a compliance requirement that drives scheduled work (inspections, replacements, modifications) across the fleet; inspection directives are not replacement directives, and none of this is a prediction that any part will fail.