Mooney M20C

1,122 parts applicable to this airframe — ga_single

Part Number	Description	Manufacturer	Airframe	ATA	Category	Status
01-0790623-10	LED PAR46 Landing Light	Whelen Engineering Co Inc	—	33	Electromechanical	PMA
01-0790623-20	LED PAR46 Landing Light	Whelen Engineering Co Inc	—	33	Electromechanical	PMA
08-18088	Acorn 637-30Awl Tail Pipe M20-A / B / C / D	—	—	78	Engine Accessories	PMA
08-18152	Acorn 6261Awl Tail Pipe Assembly M20 / M20-A / M20-B	—	—	78	Engine Accessories	PMA
08-18153	Acorn 630066-000Awl Tail Pipe Assembly M20-C / M20-G	—	—	78	Engine Accessories	PMA
1049-4000-03-001C	Roll Steering Converter	DAC International	C172 Skyhawk C182 Skylane+43	32	Landing Gear	PMA
1049-4200-50	Isolation Coupler Installation Kit	DAC International	C172 Skyhawk C182 Skylane+43	25	Interior / Furnishings	PMA
1049-4201-20	Annunciator Kit GDC31	DAC International	C172 Skyhawk C182 Skylane+43	25	Interior / Furnishings	PMA
1049-4801-01	Isolation Coupler	DAC International	C172 Skyhawk C182 Skylane+43	25	Interior / Furnishings	PMA
540004505	LEG ASSY	Mooney	M20C M20F	32	Landing Gear	OEM
560194000	LEVER	Mooney	M20C M20F	32	unknown	OEM
610153	Aux. Fuel Pump 14 Volt	—	—	28	—	OEM
610153-000	Aux. Fuel Pump 14 Volt	—	—	28	—	OEM
6400471	AIR BOX	Mooney	M20C M20E	71	Engine Accessories	OEM
9100-001-D	MaxDim Lamp Intensity Controller	Seaton Engineering Corporation	C172 Skyhawk C182 Skylane+52	25	Interior / Furnishings	PMA
9200-000-A	MaxPulse Landing Light Controller	Seaton Engineering Corporation	C172 Skyhawk C182 Skylane+52	33	Electromechanical	PMA
9200000B	SWITCH	—	C172 Skyhawk C182 Skylane+52	33	Electromechanical	OEM
ALE-1013AS-AC	Alternator Brush	Hartzell Engine Technologies LLC	PA-28 Cherokee C310+21	25	Interior / Furnishings	PMA
L025-914007-004-005AB	Oversize Bushing, NLG Pivot	LASAR Inc.	M20C M20E+3	32	Landing Gear	PMA
L540042501	TRUSS	Mooney	M20C M20F	32	Structures	OEM
MDL 02041301	CGR-30( ) and Accessories	Electronics International Inc	C172 Skyhawk C182 Skylane+35	77	Instruments	PMA
MDL B-800	Wing Fuel Cell Installation	Griggs Aircraft Refinishing LLC	M20C M20E	28	Fuel Systems	PMA
MDL B-800A	Auxiliary Bladder	Griggs Aircraft Refinishing LLC	M20C M20E	28	Fuel Systems	PMA
NAS660518	BOLT	Mooney	M20C	71	Consumables / Hardware	OEM
P130062-501	Cover, Hat Rack Strip	Premier Aerospace Services & Technology, Inc.	M20C M20E	25	Interior / Furnishings	PMA
P130079-55	Headliner, Hatrack	Premier Aerospace Services & Technology, Inc.	M20C M20E	25	Interior / Furnishings	PMA
P130090	Panel, Rear Bag Comp, Aft	Premier Aerospace Services & Technology, Inc.	M20C M20E+1	56	Structures	PMA
P130103	Cover Assy, Nose Wheelwell	Premier Aerospace Services & Technology, Inc.	M20C M20E	25	Interior / Furnishings	PMA
P130103-15	Cover, RH	Premier Aerospace Services & Technology, Inc.	M20C M20E	25	Interior / Furnishings	PMA
P130105-1	Moulding, Footwell LH	Premier Aerospace Services & Technology, Inc.	M20C M20E+1	50	Interior / Furnishings	PMA
P130117	Panel Assy, Hat Rack Aft	Premier Aerospace Services & Technology, Inc.	M20C M20E	25	Interior / Furnishings	PMA
P610035-03	Pan, Fuel Selector Valve	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
P640042-03	Cover, Vent Outlet	Premier Aerospace Services & Technology, Inc.	M20C M20E	25	Interior / Furnishings	PMA
PA-111114-821	Switch, Pressure Differential	Peregrine LLC	C172 Skyhawk C182 Skylane+6	—	Electromechanical	PMA
PA-111114-833	Insert Stabilizer, Nylon	Peregrine LLC	C172 Skyhawk C182 Skylane	20	Consumables / Hardware	PMA
SC-W/G-2536-250	Mooney Door Window - With Assembled Oversize Vent (.250 SC Gray)	Great Lakes Aero Products Inc	M20C M20E	56	Structures	PMA
SC-W/G-2537	Mooney Door Window - With Assembled Oversize Vent (SC Gray )	Great Lakes Aero Products Inc	M20C M20E+1	52	Structures	PMA
SC-W/G-2537-250	Mooney Door Window - With Assembled Oversize Vent (.250 SC Gray)	Great Lakes Aero Products Inc	M20C M20E+1	52	Structures	PMA
SC-W/G-2538	Mooney Door Window - With Assembled Oversize Vent (SC Gray )	Great Lakes Aero Products Inc	M20C M20E+3	52	Structures	PMA
SC-W/G-2538-250	Mooney Door Window - With Assembled Oversize Vent (.250 SC Gray)	Great Lakes Aero Products Inc	M20C M20E+3	52	Structures	PMA
SC-W/T-2537	Mooney Door Window - With Assembled Oversize Vent (SC Green )	Great Lakes Aero Products Inc	M20C M20E+1	52	Structures	PMA
SC-W/T-2537-250	Mooney Door Window - With Assembled Oversize Vent (.250 SC Green)	Great Lakes Aero Products Inc	M20C M20E+1	56	Structures	PMA
SC-W/T-2538	Mooney Door Window - With Assembled Oversize Vent (SC Green )	Great Lakes Aero Products Inc	M20C M20E+3	56	Structures	PMA
W-2536	Mooney Door Window - With Assembled Oversize Vent (Clear )	Great Lakes Aero Products Inc	M20C M20E	56	Structures	PMA
W-2536-250	Mooney Door Window - With Assembled Oversize Vent (.250 Clear)	Great Lakes Aero Products Inc	M20C M20E	56	Structures	PMA
W-2538-250	Mooney Door Window - With Assembled Oversize Vent (.250 Clear)	Great Lakes Aero Products Inc	M20C M20E+3	56	Structures	PMA
W/G-2536-250	Mooney Door Window - With Assembled Oversize Vent (.250 Gray)	Great Lakes Aero Products Inc	M20C M20E	56	Structures	PMA
W/G-2538	Mooney Door Window - With Assembled Oversize Vent (Gray )	Great Lakes Aero Products Inc	M20C M20E+3	52	Structures	PMA
W/T-2537	Mooney Door Window - With Assembled Oversize Vent (Green )	Great Lakes Aero Products Inc	M20C M20E+1	52	Structures	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.