Mooney M20C

1,122 parts applicable to this airframe — ga_single

Part Number	Description	Manufacturer	Airframe	ATA	Category	Status
01-0771833-10	LED Landing Light	Whelen Aerospace Technologies	C172 Skyhawk C182 Skylane+37	33	Electromechanical	PMA
01-0771833-15	LED Landing Light	Whelen Aerospace Technologies	C172 Skyhawk C182 Skylane+18	33	Electromechanical	PMA
10176487121	VIBRATOR	—	C185 Skywagon C210 Centurion+5	74	unknown
11-7512-12	LIGHT-ASSY, Polaris 12V	AeroLEDs LLC	C172 Skyhawk C182 Skylane+32	25	Interior / Furnishings	PMA
1499-00-21	Pump, Fuel Electric & Shutoff	Aero Fluid Products	—	25	Interior / Furnishings	PMA
1499-00-21A	Pump, Fuel Electric & Shutoff	Aero Fluid Products	—	25	Interior / Furnishings	PMA
18024-A	18024 a new weldon fuel boost pump	WELDON	M20C	28	Fuel Systems	OEM
8164-A	weldon fuel pump 8164 a	WELDON	M20C	28	Fuel Systems	OEM
87-05207-002	Assembly, Light, PAR 36 Taxi	Astronics Luminescent Systems Inc.	—	44	Electromechanical	PMA
9060-17000-01 (straight RF)	L-3 Kit Installation NGT-9000 Panel Mount	Acron Aviation Inc.	—	34	Avionics / Electronics	PMA
9060-17500-01 (straight RF)	L-3 Kit Installation NGT-9000R Panel Mount	Acron Aviation Inc.	—	34	Avionics / Electronics	PMA
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
A630066-000	Tailpipe	Aerospace Welding Minneapolis, Inc.	—	25	Interior / Furnishings	PMA
AF6108	REAR LH ACCESS PANEL	Airforms, Inc.	—	71	Engine Systems	PMA
AL-004-001	Auto-Lean Universal Vernier Disable Cap	Flight Enhancements, LLC	—	73	unknown	PMA
AL-007-001	Auto-Lean Actuator Assembly	Flight Enhancements, LLC	—	20	unknown	PMA
ALE-2008ABS-AC	Stator	Hartzell Engine Technologies LLC	PA-28 Cherokee C310+21	25	Interior / Furnishings	PMA
AS-KIT-001	Auto-Step Actuator	Flight Enhancements, LLC	—	25	Interior / Furnishings	PMA
AS-KIT-002	Auto-Step Actuator	Flight Enhancements, LLC	—	25	Interior / Furnishings	PMA
EA13000	IGNITION SWITCH	—	C172 Skyhawk C182 Skylane+36	74	Engine Accessories	OEM
K7336-201	INFLATABLE KIT ASSEMBLY	AmSafe	—	25	Safety / Emergency	PMA
MDL-T-1530501	Interior Panel	Triumph Airborne Structures LLC	—	56	Structures	PMA
P130079-29	Strip, Trim	Premier Aerospace Services & Technology, Inc.	M20C M20E	25	Interior / Furnishings	PMA
P130079-33	Panel, Armrest, RH	Premier Aerospace Services & Technology, Inc.	M20C M20E	25	Interior / Furnishings	PMA
P130079-35	Moulding, Window, Rear, RH	Premier Aerospace Services & Technology, Inc.	M20C M20E	56	Structures	PMA
P130087	Cover Assy, Hat Rack	Premier Aerospace Services & Technology, Inc.	M20C M20E	25	Interior / Furnishings	PMA
P130103-9	Cover, Lower Front	Premier Aerospace Services & Technology, Inc.	M20C M20E	25	Interior / Furnishings	PMA
P130105-02	Moulding, Footwell RH	Premier Aerospace Services & Technology, Inc.	M20C M20E+1	50	Interior / Furnishings	PMA
SC-W/G-2536	Mooney Door Window - With Assembled Oversize Vent (SC Gray )	Great Lakes Aero Products Inc	—	52	Structures	PMA
SC-W/T-2536	Mooney Door Window - With Assembled Oversize Vent (SC Green )	Great Lakes Aero Products Inc	—	56	Structures	PMA
SC-W/T-2536-250	Mooney Door Window - With Assembled Oversize Vent (.250 SC Green)	Great Lakes Aero Products Inc	—	56	Structures	PMA
SC-W/T-2538-250	Mooney Door Window - With Assembled Oversize Vent (.250 SC Green)	Great Lakes Aero Products Inc	—	56	Structures	PMA
V674UL91	UL91 (minimum) grade aviation fuel per ASTM D7547 Unleaded Aviation Gasoline	Petersen Aviation Inc	—	20	unknown	PMA
W-2537	Mooney Door Window - With Assembled Oversize Vent (Clear )	Great Lakes Aero Products Inc	—	52	Structures	PMA
W-2537-250	Mooney Door Window - With Assembled Oversize Vent (.250 Clear)	Great Lakes Aero Products Inc	—	56	Structures	PMA
W-2538	Mooney Door Window - With Assembled Oversize Vent (Clear )	Great Lakes Aero Products Inc	—	56	Structures	PMA
W/G-2536	Mooney Door Window - With Assembled Oversize Vent (Gray )	Great Lakes Aero Products Inc	—	52	Structures	PMA
W/G-2537	Mooney Door Window - With Assembled Oversize Vent (Gray )	Great Lakes Aero Products Inc	—	56	Structures	PMA
W/G-2537-250	Mooney Door Window - With Assembled Oversize Vent (.250 Gray)	Great Lakes Aero Products Inc	—	56	Structures	PMA
W/G-2538-250	Mooney Door Window - With Assembled Oversize Vent (.250 Gray)	Great Lakes Aero Products Inc	—	52	Structures	PMA
W/T-2536	Mooney Door Window - With Assembled Oversize Vent (Green )	Great Lakes Aero Products Inc	—	56	Structures	PMA
W/T-2536-250	Mooney Door Window - With Assembled Oversize Vent (.250 Green)	Great Lakes Aero Products Inc	—	52	Structures	PMA
W/T-2537-250	Mooney Door Window - With Assembled Oversize Vent (.250 Green)	Great Lakes Aero Products Inc	—	56	Structures	PMA
W/T-2538	Mooney Door Window - With Assembled Oversize Vent (Green )	Great Lakes Aero Products Inc	—	52	Structures	PMA
W/T-2538-250	Mooney Door Window - With Assembled Oversize Vent (.250 Green)	Great Lakes Aero Products Inc	—	56	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.