Cirrus SR22

811 parts applicable to this airframe — ga_single

Part Number	Description	Manufacturer	Airframe	ATA	Category	Status
10332002	HINGE FITTING	Cirrus	SR22	57	Structures
10357586	DISTRIBUTOR GEAR	Bendix	C172 Skyhawk SR22+5	74	Engine Accessories	OEM
10382584	BREAKER POINTS	CONT	C206 Stationair SR22+5	74	Engine Accessories	OEM
10712-003	Cirrus Door Window RH or LH	—	SR22 SR20	56	window/transparency	OEM
10712-004	Cirrus Door Window RH or LH	—	SR22 SR20	56	window/transparency	OEM
10714-003	Cirrus Passenger Window RH or LH	—	SR22 SR20	56	Structures	OEM
10714-004	Cirrus Passenger Window RH or LH	—	SR22 SR20	56	Structures	OEM
10714-005	Cirrus Passenger Window RH or LH	—	SR22 SR20	56	window/transparency	OEM
10714-006	Cirrus Passenger Window RH or LH	—	SR22 SR20	56	window/transparency	OEM
10714-007	Cirrus Passenger Window RH or LH	—	SR22 SR20	56	window/transparency	OEM
10714-008	Cirrus Passenger Window RH or LH	—	SR22 SR20	56	window/transparency	OEM
10716-002	Cirrus Rear Back Window	—	SR22 SR20	56	Structures	OEM
10716-003	Cirrus Rear Back Window	—	SR22 SR20	56	Structures	OEM
10716-004	Cirrus Rear Back Window	—	SR22 SR20	56	Structures	OEM
11799001	BRACKET	—	SR22 SR20	32	unknown	OEM
12212-003	Trim Upper Windshield	—	SR22 SR20	25	—	OEM
12216-002	Mid Console Interior Trim LH	—	SR22 SR20	20	—	OEM
12217-002	Mid Console Interior Trim RH	—	SR22 SR20	25	—	OEM
12221-004	Aft Console Side Panel RH	—	SR22 SR20	25	—	OEM
12228-005	Trim B Pillar LH	—	SR22 SR20	25	—	OEM
12228-006	Trim B Pillar RH	—	SR22 SR20	25	—	OEM
12235-005	Trim Passenger Light Access Panel LH	—	SR22 SR20	25	—	OEM
12235-006	Trim Passenger Light Access Panel RH	—	SR22 SR20	25	—	OEM
12258-002	Aft Console Rear Cover	—	SR22 SR20	25	—	OEM
12412-001	Cirrus Windshield	—	SR22 SR20	56	Structures	OEM
12414-001	Cirrus Passenger Window LH or RH	—	SR22 SR20	56	Structures	OEM
12414-002	Cirrus Passenger Window LH or RH	—	SR22 SR20	56	Structures	OEM
12414-003	Cirrus Passenger Window LH or RH	—	SR22 SR20	56	Structures	OEM
12414-004	Cirrus Passenger Window LH or RH	—	SR22 SR20	56	Structures	OEM
13099-001	A Pillar Bottom LH	—	SR22 SR20	25	—	OEM
13099-002	A Pillar Bottom RH	—	SR22 SR20	25	—	OEM
13104-002	Center Bolster Cover	—	SR22 SR20	25	—	OEM
13105-002	LH Bolster W/PFD	—	SR22 SR20	25	—	OEM
16402504	BRAKE DISC	CLEVELAND	SR22 SR22T+1	32	Wheels & Brakes	OEM
537750	SCREW	CONT	SR22 C404 Titan+2	85	Consumables / Hardware	OEM
630046	PISTON PIN	CONT	C206 Stationair SR22+6	85	Engine Accessories	OEM
646843	ALTERNATOR	CONT	SR22 C210 Centurion	24	Electromechanical	OEM
AN37A	STOP-BOLT	Cirrus	SR22 PA-31 Navajo+2	32	Consumables / Hardware	OEM
BA111	SUPPORT	Airbus	C172 Skyhawk SR22+1	71	Structures	unknown
Cleveland Wheels & Brakes P/N 066-10500 Rapco	Brake Lining	—	C172 Skyhawk C182 Skylane+25	20	—	OEM
Cleveland Wheels & Brakes P/N 105-00200 Rapco	Rivet	—	C172 Skyhawk C182 Skylane+29	20	—	OEM
G243	BATTERY	GILLBATT	C172 Skyhawk PA-28 Cherokee+3	24	Electromechanical	OEM
Inc. P/N RA105-002 Aviation Products Systems Inc. P/N APS105-00200	Rivet	—	C172 Skyhawk C182 Skylane+29	20	—	OEM
Inc. P/N RA66-105 Aviation Products Systems Inc. P/N APS66-10500	Brake Lining	—	C172 Skyhawk C182 Skylane+25	20	—	OEM
Inc. P/N RA66-105-8K	Brake Lining Kit	—	C182 Skylane C206 Stationair+12	20	—	OEM
MS178268	NUT	—	SR22	62	Consumables / Hardware	OEM
MS25237327	LIGHT	GE	737-900 Dash 8-400+6	33	Interior / Furnishings	OEM
RHB32E	SPARK PLUG	CHAMPION	C206 Stationair SR22+5	74	Engine Accessories	OEM
RHB32S	SPARK PLUG	CHAMPION	C182 Skylane SR22+3	74	Engine Accessories	OEM
SA630046	PISTON PIN	—	SR22	85	Consumables / Hardware	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 2024-24-11effective Dec 23, 2024Mixed actions
The FAA is adopting a new airworthiness directive (AD) for certain Cirrus Design Corporation (Cirrus) Model SR20, SR22, and SR22T airplanes. This AD was prompted by a report of failure of the upper power lever. This AD requires repetitively inspecting (visual) the upper power lever for any crack(s) and depending on the results of any visual inspection, either inspecting (fluorescent penetrant) or replacing the upper power lever. This AD also requires reporting all inspection results to the FAA. 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.