# Service difficulty reports: Hanger 9 SR-22T

A list on [Hanger 9 SR-22T](https://openairdocs.org/model/hanger-9-sr-22t.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 70 reports

- [SDR 2026FA0000822](https://openairdocs.org/sdr/2026FA0000822.md): Cylinder · cracked · Oct 2, 2026 · N1096W · Cirrus SR22T · Reciprocating Engine Cylinder Section
  > DISCOVERED CRACKED CYLINDER #3 FOLLOWING A ROUTINE INSPECTION FOR SB25-04.
- [SDR 2026FA0000808](https://openairdocs.org/sdr/2026FA0000808.md): Skin · corroded · Oct 2, 2026 · N504TK · Cirrus SR22T · Elevator, Plate/Skin
  > THIS PLANE HAS CONTINUED REPETITIVE CORROSION OF THE ALUMINUM PARTS OF THE ELEVATOR. IT IS SEEN AT EMANATING FROM THE BONDED PARTS WHERE THE PIECES ARE RIVETED TOGETHER. IT WAS REPAINTED ONCE WHEN THE AIRFRAME WAS ONLY 2 YEARS OLD. IT THEN AGAIN OCCURRED NE
- [SDR 2026FA0000807](https://openairdocs.org/sdr/2026FA0000807.md): Drive Gear · spalled · Oct 1, 2026 · Cirrus SR22T · Reciprocating Engine Power Section
  > FACE GEAR DAMAGED, ENGINE HAS EXHIBITED DAMAGE TO THE ALTERNATOR DRIVE FACE GEAR (P/N 657984), WHICH DRIVES THE NO. 1 ALTERNATOR. THE DAMAGE HAS INCLUDED VARYING DEGREES OF SPALLING, GALLING, AND CHIPPING OF THE GEAR TEETH.
- [SDR 2026FA0000804](https://openairdocs.org/sdr/2026FA0000804.md): Flt Controls · corroded · Oct 1, 2026 · N37CL · Cirrus SR22T · Flight Control System
  > ALL FLIGHT CONTROLS BORESCOPED. ALL FLIGHT CONTROLS EXHIBIT CORRISION THROUGHOUT, FLAPS, AILERON, & RUDDER. CORROSION FOUND THROUGHOUT ALONG THE SEAM LINES FROM INADEQUATE SURFACE PREP AND THROUGHOUT THE FLIGHT CONTROL STRUCTURE AND RIVET JOININGS. EXAMINED A
- [SDR 2026FA0000803](https://openairdocs.org/sdr/2026FA0000803.md): Torque Tube · mismanufactured · Sep 30, 2026 · N131DX · Cirrus SR22T · Landing Gear Brake System
  > AIRCRAFT WAS BROUGHT INTO ACE AVIATION FOR ANNUAL INSPECTION. 14857-002, 14857-001 ARE THE TWO PARTS FOR RH AND LH TORQUE TUBE WELDMENTS. THESE ARE ATTACHED TO THE BRAKE PEDALS ON BOTH LEFT AND RIGHT SIDE OF THE CABIN FLOOR AND WERE DISCOVERED TO HAVE EXCESSI
- [SDR 2026FA0000587](https://openairdocs.org/sdr/2026FA0000587.md): Drive Shaft · broken · Jul 16, 2026 · N127TS · Cirrus SR22T · Cabin Cooling System
  > ALL BOLTS OF DRIVE SHAFT HUB ASSY. SHEARED FROM THE DRIVE ASSY. OF THE AIR CONDITIONING SYSTEM.
- [SDR 2026FA0000817](https://openairdocs.org/sdr/2026FA0000817.md): Drive Gear · spalled · Jul 15, 2026 · Cirrus SR22T · Reciprocating Engine Power Section
  > FACE GEAR DAMAGED, ENGINE HAS EXHIBITED DAMAGE TO THE ALTERNATOR DRIVE FACE GEAR (P/N 657984), WHICH DRIVES THE NO. 1 ALTERNATOR. THE DAMAGE HAS INCLUDED VARYING DEGREES OF SPALLING AND GALLING OF THE GEAR TEETH.
- [SDR 2026FA0000553](https://openairdocs.org/sdr/2026FA0000553.md): Fuel Line · cracked · Jul 1, 2026 · N451JS · Cirrus SR22T · Aircraft Fuel Distribution System
  > WHILE PERFORMING FUEL SET UP FOUND FUEL LINE FROM THROTTLE BODY TO FUEL DISTRIBUTION MANIFOLD B-NUT FERRULE TO BE CRACKED.
- [SDR 2026FA0000547](https://openairdocs.org/sdr/2026FA0000547.md): Tube · cracked · Jun 29, 2026 · N233FD · Cirrus SR22T · Aircraft Fuel Distribution System
  > DURING THE ANNUAL INSPECTION ON A SEPARATE AIRCRAFT (N90CF), IT WAS IDENTIFIED THAT THE FUEL SUPPLY LINE FROM THE ENGINE THROTTLE BODY TO THE FUEL DISTRIBUTION MANIFOLD HAD A CRACK IN THE FERULE. OUT OF PRECAUTION, THIS AIRCRAFT WAS INSPECTED FOR THE SAME DEFE
- [SDR 2026FA0000546](https://openairdocs.org/sdr/2026FA0000546.md): Tube · cracked · Jun 29, 2026 · N90CF · Cirrus SR22T · Aircraft Fuel Distribution System
  > DURING THE ANNUAL INSPECTION, IT WAS IDENTIFIED THAT THE FUEL SUPPLY LINE FROM THE ENGINE THROTTLE BODY TO THE FUEL DISTRIBUTION MANIFOLD HAD A CRACK IN THE FERULE. OUT OF PRECAUTION, FOUR OTHER SR22TS ALSO UNDERGOING MAINTENANCE AT THE TIME WERE CHECKED FOR T
- [SDR 2026FA0000404](https://openairdocs.org/sdr/2026FA0000404.md): Cylinder Head · separated · May 18, 2026 · N444AN · Cirrus SR22T · Reciprocating Engine Cylinder Section
  > SEPARATION OF CYLINDER HEAD, EXHAUST SIDE FROM NR 5 CYLINDER DURING CRUISE/LEVEL FLIGHT. APPROXIMATELY 30 MINUTES INTO FLIGHT.
- [SDR 2026FA0000819](https://openairdocs.org/sdr/2026FA0000819.md): Drive Gear · spalled · Apr 29, 2026 · Cirrus SR22T · Reciprocating Engine Power Section
  > FACE GEAR DAMAGED, ENGINE HAS EXHIBITED DAMAGE TO THE ALTERNATOR DRIVE FACE GEAR (P/N 657984), WHICH DRIVES THE NO. 1 ALTERNATOR. THE DAMAGE HAS INCLUDED VARYING DEGREES OF SPALLING AND GALLING OF THE GEAR TEETH.
- [SDR 2026FA0000258](https://openairdocs.org/sdr/2026FA0000258.md): Brake Disc · cracked · Apr 2, 2026 · N356SC · Cirrus SR22T · Landing Gear Brake System
  > LEFT MAIN BRAKE DISC FAILED/BROKE IN HALF WHEN AIRCRAFT WAS TAXIING.
- [SDR 2026FA0000211](https://openairdocs.org/sdr/2026FA0000211.md): Brush Block · exploded · Mar 24, 2026 · Cirrus SR22T · DC Generator-Alternator
  > ALTERNATOR WOULD INTERMITTENTLY FAIL DURING FLIGHT. LANDED. ALT CHECKED FINE. PULLED BRUSH BLOCK ASSEMBLY. AND IT FELL INTO A MILLION PIECES. SEE VIDEO LINK WHILE ITS ACTIVE. SUSPECT CHINESE COMPONENTS FROM HET. FURTHER INVESTIGATION WARRANTED.
- [SDR 2026FA0000191](https://openairdocs.org/sdr/2026FA0000191.md): Manifold · erratic · Mar 18, 2026 · N788BM · Cirrus SR22T · Manifold Pressure (MP) Indicating
  > IN CRUISE PILOT REPORTED THAT THE ENGINE BEGAN SURGING, RECEIVED A FLASHING CAS MESSAGE (UNCERTAIN WHAT THE MESSAGE WAS). PILOT REDUCED POWER TO 40% TO GET IT TO RUN SMOOTHLY AND MADE AN EMERGENCY LANDING IN BAKERSFIELD CA.
- [SDR 2026FA0000549](https://openairdocs.org/sdr/2026FA0000549.md): Coupling · cracked · Feb 26, 2026 · N233FD · Cirrus SR22T · Exhaust Turbocharger
  > DURING THE ANNUAL INSPECTION, BOTH TURBO V-BAND CLAMPS WERE REMOVED FOR INSPECTION AND BOTH WERE FOUND TO HAVE CRACKS IN THE CORNER RADII OF CLAMP INNER SEGMENTS.
- [SDR 2026FA0000142](https://openairdocs.org/sdr/2026FA0000142.md): Cylinder · cracked · Feb 25, 2026 · N267HH · Cirrus SR22T · Reciprocating Engine Cylinder Section
  > DURING ANNUAL INSPECTION, I WAS BORESCOPING TCM TSIO 550 K ENGINE AND FOUND NUMBER 2 CYLINDER INTAKE VALVE CRACKED AND THE EDGES WERE CHIPPED AWAY. THE CYLINDER ONLY HAD 220 HOURS SINCE OVERHAUL. I REMOVED THE CYLINDER ASSEMBLY AND SENT TO CONTINENTAL ENGINES
- [SDR 2025FA0000709](https://openairdocs.org/sdr/2025FA0000709.md): B-Nut · loose · Oct 13, 2025 · N90CF · Cirrus SR22T · Aircraft Fuel Distribution System
  > DOWNLOAD THE FLIGHT INFORMATION FROM THE DATA CARD. UPON OPENING THE CABIN DOOR, WAS IMMEDIATELY MET WITH A STRONG ODOR OF FUEL. THE COCKPIT SEATS WERE REMOVED FOR INSPECTION. UPON OPENING AN INSPECTION PANEL ON THE RT WING SPAR PASSTHROUGH, NOTED THAT THE
- [SDR 2025FA0000513](https://openairdocs.org/sdr/2025FA0000513.md): Magneto · failed · Jul 23, 2025 · N822R · Cirrus SR22T · Magneto/Distributor
  > PILOT OBSERVED #4 CYLINDER INDICATING IN THE RED. PERFORMED UNSCHEDULED LANDING AT KBOI. LOCAL FBO PERFORMED TROUBLESHOOTING. TESTED PROBES WITH GOOD RESULTS. PERFORMED ENG RUN. FOUND LT MAG WITH EXCESSIVE DROP (OVER 900 RPM) & CAUSE ENG TO DIE. VERIFIED ENG
- [SDR 2025FA0000512](https://openairdocs.org/sdr/2025FA0000512.md): Wire Harness · failed insp · Jul 23, 2025 · N822R · Cirrus SR22T · Ignition System Wiring
  > PILOT OBSERVED #4 CYLINDER TEMPERATURE INDICATING IN THE RED. MADE AN UNSCHEDULED LANDING AT KBOI. LOCAL FBO PERFORMED TROUBLESHOOTING. LOGBOOK ENTRY; "TESTED PROBES WITH SATISFACTORY RESULTS. PERFORMED ENGINE RUN. FOUND LH MAG TO HAVE EXCESSIVE DROP (OVER 900
- [SDR 2025FA0000529](https://openairdocs.org/sdr/2025FA0000529.md): Filter · melted · Jul 18, 2025 · Cirrus SR22T · Magneto/Distributor
  > PRESSURIZED MAGNETO AIR SOURCE FILTER MELTED/DEFORMED AFTER ONLY 79H AFTER INSTALLATION. BLOCKAGE OF AIR TO MAGNETO CAUSED LEFT MAGNETO FAILURE, WHICH WAS ALSO JUST 79H AFTER REPLACEMENT. PROBLEM SEEMS TO OCCUR FREQUENTLY WITH THAT FILTER INSTALLATION IN SR22
- [SDR 2025FA0000415](https://openairdocs.org/sdr/2025FA0000415.md): Cylinder Head · cracked · Jun 12, 2025 · N891DM · Cirrus SR22T · Reciprocating Engine Cylinder Section
  > AD2020-16-11 PREVIOUSLY COMPLIED WITH ON 11/12/24 AT 2158.7 FLIGHT TIME (536.5 SFRM) TO PREVENT CYLINDER CRACKS. SEVEN MONTHS AND 64.5 HOURS LATER, CYLINDER #5 CRACKED AND BROKE FREE WHILE AIRBORNE AT 12,000 FEET APPROXIMATELY 18.5 MILES WEST-NORTHWEST OF MGW
- [SDR 2025FA0000501](https://openairdocs.org/sdr/2025FA0000501.md): Turbocharger · defective · Jun 9, 2025 · N385BL · Cirrus SR22T · Exhaust Turbocharger
  > PILOT REPORTED SEVERE POWER LOSS WAS NOT ABLE TO MAINTAIN 100KTS. UNSCHEDULED LANDING AT THE CHALLIS AIRPORT, IDAHO (C53) MECHANICS INVESTED GATED ISSUE FOUND THE TURBO WAS LEAKING INTERNALLY, AND TURBO IMPELLOR WAS RUBBING INTO HOUSING. TT AIRFRAME 73.1 HOURS
- [SDR 2025FA0000383](https://openairdocs.org/sdr/2025FA0000383.md): Camshaft · gouged · Jun 3, 2025 · N486W · Cirrus SR22T · Reciprocating Engine Power Section
  > AN UNACCEPTABLE OIL SAMPLE LEAD TO A RECOMMENDATION BY AN OUTSIDE COMPANY TO HAVE AN INSPECTION OF THE CAMSHAFT AND LIFTERS PERFORMED. WE PERFORMED THESE INSPECTIONS AND FOUND A GOUGE ON THE #6 INTAKE LOBE ON THE CAMSHAFT. A PICK CAN BE CAUGHT IN THIS GOUGE TH
- [SDR 2025FA0000317](https://openairdocs.org/sdr/2025FA0000317.md): Sensor · erratic · Apr 25, 2025 · N321LL · Cirrus SR22T · Engine Oil Indicating System
  > PILOT REPORTED LOW OIL PRESSURE CAS ANNUNCIATION OBSERVED IN FLIGHT AND RETURNED FOR LANDING. PERFORMED POST FLIGHT INSPECTION, OIL QUANTITY WAS 6-7 QUARTS INDICATED (READ DIRECTLY AFTER SHUT DOWN). INSPECTED THE ENGINE FOR OIL LEAKS, NONE FOUND. INSPECTED OIL
- [SDR 2025FA0000150](https://openairdocs.org/sdr/2025FA0000150.md): Strut · broken · Mar 5, 2025 · N575TV · Cirrus SR22T · Nose/Tail Landing Gear Strut/Axle
  > NOSE LANDING GEAR STRUT COLLAPSED WHILE LANDING. INSPECTION OF THE AIRCRAFT DISCOVERED THAT THE NOSE LANDING GEAR STRUT HAD BROKEN CAUSING THE GEAR TO COLLAPSE.
- [SDR 2025FA0000112](https://openairdocs.org/sdr/2025FA0000112.md): Cylinder · cracked · Feb 13, 2025 · N828PW · Cirrus SR22T · Reciprocating Engine Cylinder Section
  > CYLINDER #3 WAS LEAKING OIL. UPON FURTHER INVESTIGATION, IT WAS DISCOVERED THAT THE CYLINDER WAS CRACKED. THE CRACK WAS DISCOVERED IN THE CROSSFLOW AREA THAT WAS BLENDED AS PER AD 2020-16-11. AD 2020-16-11 WAS ACCOMPLISHED ON THIS ENGINE ON 9/25/2020.
- [SDR 2025FA0000085](https://openairdocs.org/sdr/2025FA0000085.md): Exhaust Header · cracked · Feb 4, 2025 · N78DS · Cirrus SR22T · Engine Collector/Tailpipe/Nozzle
  > CRACKED EXHAUST HEADER ATTACHED TO THE FIFTH CYLINDER.
- [SDR 2025FA0000140](https://openairdocs.org/sdr/2025FA0000140.md): Magneto · faulted · Jan 24, 2025 · N81DX · Cirrus SR22T · Magneto/Distributor
  > THE COMMERCIAL STUDENT ON BOARD WAS PERFORMING THE DUTIES OF PILOT IN COMMAND (PIC) WHILE A CERTIFIED FLIGHT INSTRUCTOR ACTED AS THE PIC INSTRUCTOR. THE OUTBOUND FLIGHT WAS UNEVENTFUL; HOWEVER, DURING THE RETURN AND WHILE ON CRUISE FLIGHT ON V21 NEAR MLD, THER
- [SDR 2024FA0000942](https://openairdocs.org/sdr/2024FA0000942.md): Cylinder · cracked · Dec 6, 2024 · N365HG · Cirrus SR22T · Reciprocating Engine Cylinder Section
  > THIS REPORT PERTAINS TO AD 20-16-11. THE CURRENTLY INSTALLED #5 CYLINDER, PN: 658595 SN: AC18DA103 WAS AFFECTED BY AD 20-16-11. THE CORRECTIVE ACTION, RADIUS THE TARGET AREA TO RELIEVE STRESS AND PREVENT CRACKING, HAD PREVIOUSLY BEEN COMPLIED WITH. HOWEVER,
- [SDR 2024FA0000821](https://openairdocs.org/sdr/2024FA0000821.md): Cylinder · seized · Oct 22, 2024 · N512HW · Cirrus SR22T · Reciprocating Engine Cylinder Section
  > #4 TOP SPARK PLUG (TEMPEST) WAS SEIZED IN THE CYLINDER HEAD. SPARK PLUG APPEARS TO BE TORQUING AGAINST THE BASE OF THE HELICOIL RATHER THAN AT THE SPARK PLUG FLANGE AND THE GASKET. THE SPARK PLUG COULD NOT BE REMOVED WITH HEAT OR PENETRATING OIL, EVEN WITH MAX
- [SDR 2025FA0000421](https://openairdocs.org/sdr/2025FA0000421.md): Cylinder Head · cracked · Oct 12, 2024 · N891DM · Cirrus SR22T · Reciprocating Engine Cylinder Section
  > WHILE APPROACHING INTENDED DESTINATION OF SSI, LEVEL AT 5,000 FEET, THE PLANE STARTED VIBRATING/SHAKING WITH A LOSS OF PERCENT POWER AND MANIFOLD PRESSURE, AMONG OTHER INDICATIONS. CYLINDER #6 EGT WENT OFFLINE, INDICATING A PROBLEM WITH THAT CYLINDER. TURNED
- [SDR 2024FA0000838](https://openairdocs.org/sdr/2024FA0000838.md): Cylinder Head · separated · Aug 1, 2024 · N811SB · Cirrus SR22T · Reciprocating Engine Cylinder Section
  > WHILE IN NORMAL CRUISE FLIGHT, THE PILOT/OWNER REPORTED THE ENGINE BEGAN RUNNING ROUGH WITH ASSOCIATED LOSS OF POWER. EXECUTED AN UNSCHEDULED LANDING AT PWM AIRPORT AND WE TOOK IN SUBJECT AIRPLANE FOR REPAIRS AND RETURN TO SERVICE. INSPECTION REVEALED THE #2 C
- [SDR 2024FA0000504](https://openairdocs.org/sdr/2024FA0000504.md): Cylinder · cracked · Jul 17, 2024 · N12ZZ · Cirrus SR22T · Reciprocating Engine Cylinder Section
  > THE EXHAUST ROCKER ARM AND CYLINDER CASTING SEPARATED FROM CYLINDER IN CRUISE FLIGHT. POWER WAS REDUCED AND AIRCRAFT LANDED AT AN ALTERNATE AIRPORT.
- [SDR 2024FA0000424](https://openairdocs.org/sdr/2024FA0000424.md): Filter · melted · Jun 5, 2024 · N991SG · Cirrus SR22T · Magneto/Distributor
  > PRESSURIZED MAGNETO AIR SOURCE FILTER MELTED/DEFORMED. IF CONTINUED COULD CAUSE BLOCKAGE OF AIR TO MAGNETO CAUSING PREMATURE MAGNETO FAILURE. PROBLEM SEEMS TO COINCIDE WITH RELOCATION OF FILTER CLOSER TO CYLINDERS WITH NEWER MANUFACTURED AIRCRAFT
- [SDR 2024FA0000422](https://openairdocs.org/sdr/2024FA0000422.md): Connecting Rod · failed · Jun 4, 2024 · N522RK · Cirrus SR22T · Reciprocating Engine Power Section
  > ENGINE WAS DISASSEMBLED FOR INSPECTION DUE TO PROPELLER STRIKE. UPON DISASSEMBLY IT WAS NOTED THAT THE CONNECTING ROD BUSHING HAS MIGRATED PARTLY OUT OF THE BORE ON THE SMALL END OF CONNECTING ROD #2, #3, & #5. THIS IS THE THIRD TIME THAT WE HAVE SEEN THIS P
- [SDR 2024FA0000326](https://openairdocs.org/sdr/2024FA0000326.md): Landing Gear · broken · Apr 13, 2024 · N522RK · Cirrus SR22T · Nose/Tail Landing Gear
  > ON LANDING AT SCOTTSDALE AIRPORT KSDL, AIRCRAFT EXPERIENCED A NOSE GEAR FAILURE. NOSE GEAR BROKE AFT OF THE ACTUATOR ATTACH POINT, FOLDED UNDER THE ENGINE TO THE LEFT SIDE, THE PROP STRUCK THE GROUND AND THE AIRCRAFT SLIDE FOR A SHORT DISTANCE. NO INJURIES OR
- [SDR 2024FA0000074](https://openairdocs.org/sdr/2024FA0000074.md): Magneto · broken · Jan 13, 2024 · N114DB · Cirrus SR22T · Magneto/Distributor
  > ON APPROACH INTO KCPR FROM U68 THE PILOT OBSERVED ENGINE BEGAN TO RUN ROUGH FOLLOWED BY EGT AND CHT TEMPERATURES DRASTICALLY INCREASE. THE PILOT LANDED AT KCPR WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH MAGNETOS AND OPS CHECK GOOD. UPON TEARDOWN OF MAGNETOS,
- [SDR 2023FA0000764](https://openairdocs.org/sdr/2023FA0000764.md): Magneto · defective · Nov 20, 2023 · N398JT · Cirrus SR22T · Magneto/Distributor
  > ON TAKEOFF ENGINE RAN ROUGH AND PIC RETURNED TO FIELD. THE RIGHT MAGNETO IMPULSE WAS FOUND TO BE INOPERATIVE ALONG WITH A FAILED #4 IGNITION PLUG. BOTH UNITS WERE REPLACED, AND AIRCRAFT RUN-UP TEST PERFORMED AND FOUND SATISFACTORY.
- [SDR 2023FA0000762](https://openairdocs.org/sdr/2023FA0000762.md): Spring · destroyed · Nov 16, 2023 · N305MS · Cirrus SR22T · Propeller Assembly
  > PROPELLER EXHIBITED SEVERAL LOOSE BLADES IN THE HUB UPON INSPECTION AFTER PICKUP FROM THE FACTORY SERVICE CENTER IN KNOXVILLE TN POST ANNUAL. THIS WAS TOLD TO BE A DESIGN FEATURE AND NOT A CAUSE FOR CONCERN. THE SERVICE CENTER HAD SERVICED PROP WITH GREASE DUR
- [SDR 2023FA0000564](https://openairdocs.org/sdr/2023FA0000564.md): Cylinder Head · cracked · Sep 21, 2023 · N748CM · Cirrus SR22T · Cylinder Head Temperature (CHT) Indicating System
  > CRACKED #5 CYLINDER HEAD
- [SDR 2023FA0000149](https://openairdocs.org/sdr/2023FA0000149.md): Drive Unit · stripped · Mar 21, 2023 · N118EB · Cirrus SR22T · Air Conditioning System
  > AFTER AN UNSCHEDULED LANDING BECAUSE OF A LEFT MAGNETO PROBLEM, MAINTENANCE FOUND THE A/C DRIVE PULLEY TO SPLINE SHAFT MISSING 3 OF 4 MOUNTING BOLTS. FOUND THREADS IN PULLEY STRIPPED OUT.
- [SDR 2023FA0000044](https://openairdocs.org/sdr/2023FA0000044.md): Gear · broken · Jan 10, 2023 · N773GP · Cirrus SR22T · Magneto/Distributor
  > ENGINE SUFFERED LOSS OF POWER, ENGINE OUT DURING CRUISE AT 23K. TURBOCHARGED ENGINE RUNNING LEAN OF PEAK PER POH. PILOT REPORTED CHECKING MAGNETOS DURING DESCENT, SWITCHED KEY FROM BOTH TO LEFT AND THE MOTOR INSTANTLY QUIT MAKING MEANINGFUL POWER, IMMEDIAT
- [SDR 2022FA0000571](https://openairdocs.org/sdr/2022FA0000571.md): Lug · sheared · Oct 6, 2022 · N59WV · Cirrus SR22T · Landing Gear Brake System
  > LEFT HAND BRAKE ROTOR MOUNT LANGE SHEARED CAUSING THE BRAKE TO FAIL.
- [SDR 2022FA0000565](https://openairdocs.org/sdr/2022FA0000565.md): Brake Disc · failed · Aug 31, 2022 · N59WV · Cirrus SR22T · Landing Gear Brake System
  > RIGHT HAND BRAKE ROTOR MOUNT LUG SHEAVED CAUSING BRAKE TO FAIL
- [SDR 2022FA0000462](https://openairdocs.org/sdr/2022FA0000462.md): None · none · Aug 18, 2022 · N191JB · Cirrus SR22T · Propeller Assembly
  > FLIGHT WALK AROUND NOTICED PROP WAS DAMAGED. SHOP WILL TAKE ACTIONS TO REPAIR PLANE IN COMING WEEKS. NO DEFECT IN ANY PARTS ON PLANE UNTIL AFTER ATTEMPTING LANDING.
- [SDR VPEA20224213153](https://openairdocs.org/sdr/VPEA20224213153.md): Cylinder Head · broken · Apr 19, 2022 · N703TP · Cirrus SR22T · Reciprocating Engine Cylinder Section
  > DURING FLIGHT BACK TO COD. ENGINE STARTED RUNNING ROUGH WITH POWER LOSS OIL PRESSURE DROPPED TO 9 PSI. ONCE IN MX IT WAS DISCOVERED THE #2 CYLINDER EXHAUST SIDE HAD BROKEN OFF WITH THE ROCKER ARM INSIDE.
- [SDR 2022FA0000095](https://openairdocs.org/sdr/2022FA0000095.md): None · none · Feb 22, 2022 · N428AN · Cirrus SR22T · Engine (Turbine/Turboprop)
  > N428AN JUST CAME OUT OF SERVICE AT EDWARDS JET CENTER FOR A CHECK VALVE NOT CLOSING ALL THE WAY AFTER SHUT-DOWN. IT WAS DISCOVERED THAT A VERY SMALL PIECE OF FILTER AND SOME "GUNK" WAS PREVENTING THE CHECK VALVE FROM CLOSING ALL THE WAY. AFTER DISASSEMBLING,
- [SDR 2022FA0000046](https://openairdocs.org/sdr/2022FA0000046.md): Magneto · malfunctioned · Jan 26, 2022 · N717DM · Cirrus SR22T · Magneto/Distributor
  > AIRCRAFT SUFFERED ENGINE POWER LOSS DUE TO A MALFUNCTIONING LEFT HAND MAGNETO.
- [SDR 2021FA0000299](https://openairdocs.org/sdr/2021FA0000299.md): None · melted · Oct 1, 2021 · N888VE · Cirrus SR22T · Stall Warning System
  > INVESTIGATION OF PITOT HEAT/STALL VANE HEAT ELECTRICAL SYSTEM FOUND RELAY BASE CIRRUS WDM ID "P1383" MFG TE 27E487 AND RELAY K1383" MFG P/N K10P-11D15-24 SUPPLING STALL VANE LIFT TRANSDUCER AND PITOT PROBE TO BE MELTED AT BASE AND RELAY TO HAVE OVERHEAT DAMAGE

Next page: https://openairdocs.org/model/hanger-9-sr-22t/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = 'SR22T'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/hanger-9-sr-22t/reports

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