Mooney M20E

1,122 parts applicable to this airframe — ga_single

Part Number	Description	Manufacturer	Airframe	ATA	Category	Status
11-7512-12	LIGHT-ASSY, Polaris 12V	AeroLEDs LLC	C172 Skyhawk C182 Skylane+32	25	Interior / Furnishings	PMA
115-00345-00	Tray, IFD5XX series	—	—	34	—	OEM
130062-501	Cover, Hat Rack Strip	—	—	25	—	OEM
130078-511	Deflector FWD	—	—	25	—	OEM
130079-29	Strip, Trim	—	—	25	—	OEM
130079-33	Panel, Armrest, RH	—	—	25	—	OEM
130079-35	Moulding, Window, Rear, RH	—	—	56	—	OEM
130079-55	Headliner, Hatrack	—	—	25	—	OEM
130103	Cover Assy, Nose Wheelwell	—	—	25	—	OEM
130103-15	Cover, RH	—	—	25	—	OEM
130103-9	Cover, Lower Front	—	—	25	—	OEM
130105-02	Moulding, Footwell RH	—	—	50	—	OEM
130105-1	Moulding, Footwell LH	—	—	50	—	OEM
130117	Panel Assy, Hat Rack Aft	—	—	25	—	OEM
340067-7	Window Moulding Door	—	—	25	—	OEM
610035-03	Pan, Fuel Selector Valve	—	—	25	—	OEM
610035-501	Pan, Fuel Selector Valve	—	—	25	—	OEM
6104-02	Forward Spar Mount, Left, Outboard	f atlee dodge aircraft services llc	—	57	Structures	PMA
640030-09	Cover Plate Instrument Light	—	—	20	—	OEM
640030-3	Cover Plate Dome Light	—	—	25	—	OEM
640042-03	Cover, Vent Outlet	—	—	25	—	OEM
810001-3	Cover Plate Speaker	—	—	25	—	OEM
820061-503	Cover Assy, Circuit Breaker	—	—	25	—	OEM
820061-509	Cover Assy, Circuit Breaker	—	—	25	—	OEM
9100-001-A	MaxDim Lamp Intensity Controller	Seaton Engineering Corporation	C172 Skyhawk C182 Skylane+52	25	Interior / Furnishings	PMA
9100-001-B	MaxDim Lamp Intensity Controller	Seaton Engineering Corporation	C172 Skyhawk C182 Skylane+52	33	Electromechanical	PMA
9100-001-C	MaxDim Lamp Intensity Controller	Seaton Engineering Corporation	C172 Skyhawk C182 Skylane+52	25	Interior / Furnishings	PMA
9100-001-E	MaxDim Lamp Intensity Controller	Seaton Engineering Corporation	C172 Skyhawk C182 Skylane+52	33	Electromechanical	PMA
9100-001-F	MaxDim Lamp Intensity Controller	Seaton Engineering Corporation	C172 Skyhawk C182 Skylane+52	25	Interior / Furnishings	PMA
9100-001-G	MaxDim Lamp Intensity Controller	Seaton Engineering Corporation	C172 Skyhawk C182 Skylane+52	33	Electromechanical	PMA
ALE-2008AA-AC	Stator	Hartzell Engine Technologies LLC	PA-28 Cherokee C310+21	25	Interior / Furnishings	PMA
ALE-2008ABS-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 063-01200	Pressure Plate	—	—	20	—	OEM
Cleveland Wheels & Brakes P/N 066-10500	Brake Lining	—	—	32	—	OEM
Cleveland Wheels & Brakes P/N 105-00200	Rivet	—	—	20	—	OEM
Cleveland Wheels and Brakes P/N 063-01200	Pressure Plate	—	—	32	—	OEM
Cleveland Wheels and Brakes P/N 064-01500	Back Plate	—	—	32	—	OEM
ELECTROAIR Part No EAREM37HE	Spark Plug	—	—	74	—	OEM
ELECTROAIR Part number EARHM38SE	Spark Plug	—	—	74	—	OEM
GNS430 Backplate	Tray, IFD4XX series	—	—	34	—	OEM
GNS430 Tray 011-00676-00	Tray, IFD4XX series	—	—	34	—	OEM
GNS530 Backplate	Tray, IFD5XX series	—	—	34	—	OEM
GNS530 Tray 011-00671-00	Tray, IFD5XX series	—	—	34	—	OEM
LLC P/N VWS-101	Seal (Vent Window)	—	—	56	—	OEM
P130079-29	Strip, Trim	Premier Aerospace Services & Technology, Inc.	M20C M20E	25	Interior / Furnishings	PMA
P610035-501	Pan, Fuel Selector Valve	Premier Aerospace Services & Technology, Inc.	M20C M20E	25	Interior / Furnishings	PMA
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.