Mooney M20F

1,122 parts applicable to this airframe — ga_single

Part Number	Description	Manufacturer	Airframe	ATA	Category	Status
064-01500-OAA	Back Plate	Omega Aircraft Articles LLC	C172 Skyhawk C182 Skylane+20	32	Landing Gear	PMA
130099-501	Moulding, Windshield, Right	—	—	56	—	OEM
130099-501	Moulding, Windshield, Right	—	—	56	—	OEM
130105-02	Moulding, Footwell RH	—	—	50	—	OEM
130105-1	Moulding, Footwell LH	—	—	50	—	OEM
130105-1	Moulding, Footwell LH	—	—	50	—	OEM
130158-17	Panel Assy, Left Rear	—	—	25	—	OEM
130158-17	Panel Assy, Left Rear	—	—	25	—	OEM
130158-21	Panel Assy, Right Rear	—	—	25	—	OEM
130158-21	Panel Assy, Right Rear	—	—	25	—	OEM
130158-25	Panel Assy, Left Front	—	—	25	—	OEM
130160	Console Assy, Headliner	—	—	25	—	OEM
130165	Panel Assy, Bag Comp RH	—	—	25	—	OEM
130165	Panel Assy, Bag Comp RH	—	—	25	—	OEM
130187	Headliner, Hatrack	—	—	25	—	OEM
340121-11	Mooney Door Window - With Assembled Oversize Vent (.250 SC Gray)	—	—	56	Structures	OEM
340121-21	Mooney Door Window - With Assembled Oversize Vent (.250 SC Gray)	—	—	56	Structures	OEM
340285-039	Mooney Door Window - With Assembled Oversize Vent (.250 SC Green)	—	—	56	Structures	OEM
340285-063	Mooney Door Window - With Assembled Oversize Vent (.250 SC Green)	—	—	56	Structures	OEM
620019	Engine Oil Cooler Assembly	—	—	25	—	OEM
620052	Engine Oil Cooler Assembly	—	—	25	—	OEM
820024-17	Door Assy	—	—	25	—	OEM
820024-17	Door Assy	—	—	25	—	OEM
820061-509	Cover Assy, Circuit Breaker	—	—	25	—	OEM
820061-509	Cover Assy, Circuit Breaker	—	—	25	—	OEM
ALE-2008AA	Stator	—	PA-28 Cherokee C310+21	25	—	OEM
ALE-2008ABS	Stator	—	PA-28 Cherokee C310+21	25	—	OEM
ALE-2008AE	Stator	—	PA-28 Cherokee C310+21	25	—	OEM
ALT series	Brush Assembly	—	PA-28 Cherokee C310+21	24	—	OEM
ALU series	Brush Assembly	—	PA-28 Cherokee C310+21	24	—	OEM
ALX series	Brush Assembly	—	PA-28 Cherokee C310+21	24	—	OEM
ALY series	Brush Assembly	—	PA-28 Cherokee C310+21	24	—	OEM
ALZ series	Brush Assembly	—	PA-28 Cherokee C310+21	24	—	OEM
as used in alternators ALE series	Brush Assembly	—	PA-28 Cherokee C310+21	24	—	OEM
as used in alternators ALT series	Stator	—	PA-28 Cherokee C310+21	25	—	OEM
as used in alternators ALU series	Stator	—	PA-28 Cherokee C310+21	25	—	OEM
as used in alternators ALY series	Stator	—	PA-28 Cherokee C310+21	25	—	OEM
CMA7512-12	LIGHT-ASSY, Polaris 12V	—	C172 Skyhawk C182 Skylane+32	25	—	OEM
LLC P/N VWS-101	Seal (Vent Window)	—	—	56	—	OEM
ML7512-12	LIGHT-ASSY, Polaris 12V	—	C172 Skyhawk C182 Skylane+32	25	—	OEM
MO2-1-1	Starter Cable Conversion Leads	Bogert Aviation, Bogert International	M20F	24	Electromechanical	PMA
MO2-1-2	Starter Cable Conversion Leads	Bogert Aviation, Bogert International	M20F	24	Electromechanical	PMA
MO2-1-4	Starter Cable Conversion Leads	Bogert Aviation, Bogert International	M20F	24	Electromechanical	PMA
MO2-1-6	Starter Cable Conversion Leads	Bogert Aviation, Bogert International	M20F	24	Electromechanical	PMA
SC-W/T-2123	MOONEY LH FWD WINDOW - (PILOT'S)	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
T7512-12	LIGHT-ASSY, Polaris 12V	—	C172 Skyhawk C182 Skylane+32	25	—	OEM
UA-7512-12	LIGHT-ASSY, Polaris 12V	—	C172 Skyhawk C182 Skylane+11	25	—	OEM
W1290-14	LIGHT-ASSY, Polaris 12V	—	C172 Skyhawk C182 Skylane+32	25	—	OEM
XA-943FS	Pos. Diode	—	PA-28 Cherokee C310+21	25	—	OEM
XA-944JS	Neg. Diode	—	PA-28 Cherokee C310+21	25	—	OEM

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.