Mooney M20C

1,122 parts applicable to this airframe — ga_single

Part Number	Description	Manufacturer	Airframe	ATA	Category	Status
SA00024NY	—	Airwolf Filter Corporation	—	—	unknown	OEM
SA00149BO	—	Aircraft Components Inc	—	—	unknown	OEM
SA00151WI-D	—	Honeywell	M20C	—	unknown	OEM
SA00243WI-D	—	Honeywell	M20C	—	unknown	OEM
SA00244WI-D	—	Honeywell	M20C	—	unknown	OEM
SA00343BO (page 1)	—	Avidyne Corporation	—	34	Avionics / Electronics	STC
SA00344BO PAGE 1	—	Whelen Aerospace Technologies	C172 Skyhawk C182 Skylane+35	33	Electromechanical	STC
SA00352BO Page 1	—	Avidyne Corporation	—	34	Avionics / Electronics	STC
SA00353BO	—	Flight Enhancements, LLC	—	—	unknown	OEM
SA00382BO (page 1)	—	Avidyne Corporation	—	34	Avionics / Electronics	STC
SA00744DE	—	Peregrine	C172 Skyhawk C182 Skylane+42	—	unknown	OEM
SA00765DE	—	Peregrine	C172 Skyhawk C182 Skylane+50	—	unknown	OEM
SA00780SE (PAGE 3)	—	True Lock LLC	—	—	unknown	OEM
SA01049DE	—	William Patrick Rourke	M20C	—	unknown	OEM
SA01114CH	—	P2 Incorporated	—	—	unknown	OEM
SA01240SE (1 OF 5)	—	Visual Instruments, LLC	—	—	unknown	OEM
SA01435SE	—	J P Instruments	C172 Skyhawk C182 Skylane+27	—	unknown	OEM
SA01439SE	—	Micro Aerodynamics Inc	—	—	unknown	OEM
SA01560WI-D	—	Honeywell	C172 Skyhawk C182 Skylane+26	—	unknown	OEM
SA01714WI (1 OF 2)	—	Garmin	PA-28 Cherokee SR22+25	34	Avionics / Electronics	STC
SA01714WI (Page 1)	—	Garmin	—	34	Avionics / Electronics	STC
SA01734SE (PG 3)	—	Andrew D. Humphrey	—	—	unknown	OEM
SA01800SE (PG 2)	—	Seaton Engineering Corp.	SR22 C340+15	—	unknown	OEM
SA01816WI	—	Trego Dugan Aviation	—	—	unknown	OEM
SA01835WI	—	Peregrine	—	—	unknown	OEM
SA01838WI	—	Trego Dugan Aviation	—	—	unknown	OEM
SA01861SE (PAGE 3)	—	Seaton Engineering Corp.	PA-28 Cherokee King Air 200+16	—	unknown	OEM
SA01933LA-D (2 OF 2)	—	Garmin	—	34	Avionics / Electronics	STC
SA02013CH	—	Avidyne Corporation	—	34	Avionics / Electronics	STC
SA02019SE-D (2 OF 2)	—	Garmin	PA-28 Cherokee PA-34 Seneca+19	34	Avionics / Electronics	STC
SA02019SE-D (2 OF 3)	—	Garmin	PA-28 Cherokee PA-34 Seneca+19	34	Avionics / Electronics	STC
SA02153LA-D Page 1	—	Garmin	—	34	Avionics / Electronics	STC
SA02212AK (PG 1)	—	Seaplanes North LLC	—	—	unknown	OEM
SA02428SE (Page 1)	—	Henry F Rogers/David E Polley	—	—	unknown	OEM
SA02503AK (Page 1)	—	AmSafe	C172 Skyhawk C182 Skylane+3	—	unknown	OEM
SA02573SE	—	Garmin	—	34	Avionics / Electronics	STC
SA02636SE	—	Garmin	C172 Skyhawk C182 Skylane+37	34	Avionics / Electronics	STC
SA04032CH	—	Electroair Acquisition Corporation	C172 Skyhawk C182 Skylane+39	—	unknown	OEM
SA04112CH	—	Appareo Systems LLC	C172 Skyhawk C182 Skylane+23	—	unknown	OEM
SA04165NY (Page 1)	—	Latitude Technologies Corporation	C172 Skyhawk C182 Skylane+32	—	unknown	OEM
SA04362CH	—	uAvionix Corporation	C172 Skyhawk C182 Skylane+20	—	unknown	OEM
SA11172SC	—	NavWorx Inc	—	—	unknown	OEM
SA2350CE	—	Griggs Aircraft Refinishing LLC	—	—	unknown	OEM
SA2586NM	—	J P Instruments	—	—	unknown	OEM
SA3859WE	—	Airwolf Filter Corporation	—	—	unknown	OEM
SA4-1426	—	Brittain Industries Inc	—	22	Avionics / Electronics	STC
SA406WE	—	Brittain Industries Inc	—	22	Avionics / Electronics	STC
SA4553SW	—	Brittain Industries Inc	—	22	Avionics / Electronics	STC
SA4606SW	—	Brittain Industries Inc	—	22	Avionics / Electronics	STC
SA800EA	—	Whelen Aerospace Technologies	C172 Skyhawk C182 Skylane+34	33	Electromechanical	STC

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.