Mooney M20F

1,122 parts applicable to this airframe — ga_single

Part Number	Description	Manufacturer	Airframe	ATA	Category	Status
264N04	Union Tee, Nylon, 1/4 Inch OD	Peregrine LLC	C172 Skyhawk C182 Skylane+6	—	Unknown	PMA
4200-002-1	Circuit Breaker	Labinal, LLC	M20C M20E+3	24	Electrical	PMA
4200-002-2	Circuit Breaker	Labinal, LLC	M20C M20E+3	24	Electrical	PMA
4200-002-3	Circuit Breaker	Labinal, LLC	M20C M20E+3	24	Electromechanical	PMA
4200-002-4	Circuit Breaker	Labinal, LLC	M20C M20E+3	24	Electromechanical	PMA
4200-002-705	Circuit Breaker	Labinal, LLC	M20C M20E+3	24	Electrical	PMA
44PN	Tubing, Poly-Flo, Clear, 1/4 Inch OD	Peregrine LLC	C172 Skyhawk C182 Skylane+6	—	Unknown	PMA
700-00188-( )	Tray, IFD5XX series	Avidyne Corporation	C172 Skyhawk C182 Skylane+37	34	Avionics / Electronics	PMA
9060-17000-02 (right angle RF)	L-3 Kit Installation NGT-9000 Panel Mount	Acron Aviation Inc.	C172 Skyhawk C182 Skylane+47	34	Avionics / Electronics	PMA
9060-17500-01 (straight RF)	L-3 Kit Installation NGT-9000R Panel Mount	Acron Aviation Inc.	C172 Skyhawk C182 Skylane+47	34	Avionics / Electronics	PMA
9060-17500-02 (right angle RF)	L-3 Kit Installation NGT-9000R Panel Mount	Acron Aviation Inc.	C172 Skyhawk C182 Skylane+47	56	Structures	PMA
9100-001-G	MaxDim Lamp Intensity Controller	Seaton Engineering Corporation	C172 Skyhawk C182 Skylane+52	33	Electromechanical	PMA
965300-00	Time Trac Computer	Shadin Avionics (name change from Shadin Company 2/28/06)	C172 Skyhawk C182 Skylane+47	31	Avionics / Electrical	PMA
K130078-511	deflector forward	vantage plane plastics	M20C M20E+2	25	Interior / Furnishings	PMA
LS03-02040 12vdc LS03-02041 24vdc	Avionics, Electronics (1) Port Blower	Lone Star Aviation Corp	C172 Skyhawk C182 Skylane+35	21	Pneumatics	PMA
PA-111114-121	GPS Sensor Tray	Peregrine LLC	C172 Skyhawk C182 Skylane+6	34	Avionics / Electronics	PMA
PA-130827-521	GPS Wire Harness Assembly	Peregrine LLC	C172 Skyhawk C182 Skylane+6	24	Avionics / Electronics	PMA
PA-130827-523	GPS Coax Cable Assembly	Peregrine LLC	C172 Skyhawk C182 Skylane+6	23	Avionics / Electronics	PMA
PSF100A-T1.0	Switch, Pressure Differential	Peregrine LLC	C172 Skyhawk C182 Skylane+6	—	Unknown	PMA
SC-W/G-2040-II-250-LH	MOONEY 2 PC WINDSHIELDS - RH or LH	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
SC-W/G-2040-II-250-RH	MOONEY 2 PC WINDSHIELDS - RH or LH	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
SC-W/G-2040-II-LH	MOONEY 2 PC WINDSHIELDS - RH or LH	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
SC-W/G-2040-II-RH	MOONEY 2 PC WINDSHIELDS - RH or LH	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
SC-W/G-2123	MOONEY LH FWD WINDOW - (PILOT'S)	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
SC-W/G-2123-250	MOONEY LH FWD WINDOW - (PILOT'S)	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
SC-W/T-2040-II-250-LH	MOONEY 2 PC WINDSHIELDS - RH or LH	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
SC-W/T-2040-II-250-RH	MOONEY 2 PC WINDSHIELDS - RH or LH	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
SC-W/T-2040-II-LH	MOONEY 2 PC WINDSHIELDS - RH or LH	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
SC-W/T-2040-II-RH	MOONEY 2 PC WINDSHIELDS - RH or LH	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
SC-W/T-2123-250	MOONEY LH FWD WINDOW - (PILOT'S)	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
ST-022	Manual Electric Trim System	S-TEC Corporation	M20F	22	Avionics / Electronics	PMA
ST-049	System 60 Pitch Stabilization System	S-TEC Corporation	M20F	22	Avionics / Electronics	PMA
ST-115	System 60 Single Axis Automatic Flight Guidance System	S-TEC Corporation	M20F M20J	22	Avionics / Electronics	PMA
W-2040-II-250-LH	MOONEY 2 PC WINDSHIELDS - RH or LH	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
W-2040-II-250-RH	MOONEY 2 PC WINDSHIELDS - RH or LH	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
W-2040-II-LH	MOONEY 2 PC WINDSHIELDS - RH or LH	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
W-2040-II-RH	MOONEY 2 PC WINDSHIELDS - RH or LH	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
W-2123	MOONEY LH FWD WINDOW - (PILOT'S)	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
W-2123-250	MOONEY LH FWD WINDOW - (PILOT'S)	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
W/G-2040-II-250-LH	MOONEY 2 PC WINDSHIELDS - RH or LH	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
W/G-2040-II-250-RH	MOONEY 2 PC WINDSHIELDS - RH or LH	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
W/G-2040-II-LH	MOONEY 2 PC WINDSHIELDS - RH or LH	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
W/G-2040-II-RH	MOONEY 2 PC WINDSHIELDS - RH or LH	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
W/G-2123	MOONEY LH FWD WINDOW - (PILOT'S)	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
W/G-2123-250	MOONEY LH FWD WINDOW - (PILOT'S)	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
W/T-2040-II-250-LH	MOONEY 2 PC WINDSHIELDS - RH or LH	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
W/T-2040-II-250-RH	MOONEY 2 PC WINDSHIELDS - RH or LH	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
W/T-2040-II-LH	MOONEY 2 PC WINDSHIELDS - RH or LH	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
W/T-2040-II-RH	MOONEY 2 PC WINDSHIELDS - RH or LH	Great Lakes Aero Products	M20C M20E+1	56	Structures	PMA
W/T-2123	MOONEY LH FWD WINDOW - (PILOT'S)	Great Lakes Aero Products	M20C M20E+1	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.