# Service difficulty reports: Cessna R172K

A list on [Cessna R172K](https://openairdocs.org/model/cessna-r172k.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 71 reports

- [SDR 2026FA0000165](https://openairdocs.org/sdr/2026FA0000165.md): Alternator · failed · Feb 16, 2026 · N6149K · Cessna R172K · AC Generator-Alternator
  > PILOT HAD AN ALTERNATOR FAILURE IN CRUISE.
- [SDR NI6R201409110020](https://openairdocs.org/sdr/NI6R201409110020.md): Fairing · wrong part · Sep 9, 2014 · N758HS · Cessna R172K · Aerodynamic Fairings
  > FOUND LT MLG FAIRING CHAFING FUSELAGE. DETERMINED THAT AFTERMARKET FAIRING PRODUCED BY UNDER PMA SA-1741005-239 TO BE MADE OF FIBERGLASS, AND AFTER APPROXIMATELY 800 FLIGHT HOURS, IT CHAFED THROUGH THE.051 SHEET METAL FUSELAGE SKIN IN SEVERAL CONTACTING AREA
- [SDR CA130808002](https://openairdocs.org/sdr/CA130808002.md): Line · broken · Aug 7, 2013 · Cessna R172K · Engine Fuel Distribution
  > (CAN) DURING THE CRUISE PORTION OF AN FLOAT INSTRUCTION FLIGHT, THE INSTRUCTOR NOTICED AN ODOR OF FUEL AND A REDUCTION IN ENGINE POWER. THE CREW DECIDED TO MAKE A PRECAUTINARY LANDING AT A NEAR-BY FLOAT BASE. THE LANDING WAS EXECUTED WITHOUT FURTHER ISSUE. M
- [SDR 2011FA0000458](https://openairdocs.org/sdr/2011FA0000458.md): Gear · worn · Jul 14, 2011 · N8186V · Cessna R172K · Engine (Reciprocating)
  > WHILE PERFORMING AN ANNUAL INSP OF THE ENGINE, NOTICED ALTERNATOR HSG LOOSE. 500HR ALTERNATOR INSP WAS DUE. SO UPON REMOVAL OF ALTERNATOR FOR INSP IT WAS DISCOVERED THAT ALL OF THE TEETH ON THE CRANKSHAFT GEAR FACE WERE EITHER MISSING OF SEVERLY WORN. THERE
- [SDR 2011FA0000317](https://openairdocs.org/sdr/2011FA0000317.md): Engine · misoverhauled · May 16, 2011 · N736VG · Cessna R172K · Engine (Reciprocating)
  > REMOVED ENGINE OIL PUMP SUCTION SCREEN AS PART OF 100 HR INSP. FOUND OLD STYLE SUCTION SCREEN WITH FOD IN IT CONSISTING OF 1EA,.2500" AN FLAT WASHER, 2 EA SPRINGS SUCH AS USED IN GARLOCK SEALS (THESE HAD PARTIALLY PENETRATED THE SUCTION SCREEN BY ABOUT.7500
- [SDR CA110209030](https://openairdocs.org/sdr/CA110209030.md): Alternator · inoperative · Feb 8, 2011 · Cessna R172K · DC Generator-Alternator
  > DURING FLIGHT, THE GPS THEN THE RADIOS CUT OUT. THE PILOT LANDED SAFELY FOLLOWING PROCEDURES. MX DISCOVERED THAT THE ALTERNATOR OUTER CASE HAD SEPERATED FROM THE ALTERNATOR BODY CAUSING THE CHARGING SYS TO BE INOPERATIVE THUS THE BATTERY WAS DEPLETED AND THE
- [SDR CA110112006](https://openairdocs.org/sdr/CA110112006.md): Bearing · wrong part · Jan 12, 2011 · Cessna R172K · Propeller Blade Section
  > BLADE RETENTION BEARINGS ARE MANUFACTURED AS MATCHED SETS WITH CORRESPONDING SERIAL NUMBERS. UPON INSPECTION, IT WAS FOUND THAT 2 OF THE BEARING HALVES SERIAL NUMBERS DID NOT MATCH REQUIRING REPLACEMENT YAW MANUAL #MPC200.
- [SDR 2010FA0000031](https://openairdocs.org/sdr/2010FA0000031.md): Switch · cracked · Dec 17, 2009 · N1437V · Cessna R172K · Trailing Edge Flap Control System
  > OWNER COMPLAINT - WHEN FLAPS "DOWN" WAS SELECTED, SPARKS CAME OUT AROUND HANDLE. FOUND MICROSWITCH PN S1906-1, BROKEN IN HALF, AND SHORTING OUT ON MOUNTING BRACKET. SWITCH BELIEVED TO BE ORIGINAL. REPLACED SWITCH, ALL OPS NORMAL.
- [SDR CA090514006](https://openairdocs.org/sdr/CA090514006.md): Retainer · cracked · May 14, 2009 · Cessna R172K · Reciprocating Engine Cylinder Section
  > (CAN) NR 1 CYLINDER INTAKE ROCKER RETAINER WAS FOUND CRACKED.
- [SDR CA081125004](https://openairdocs.org/sdr/CA081125004.md): Engine · making metal · Nov 12, 2008 · Cessna R172K · Engine (Reciprocating)
  > (CAN) LOSS OF OIL PRESSURE DURING FLIGHT. PRECAUTIONARY LANDING ON NEARBY LAKE. INSP REVEALED HEAVY METAL CONTAMINATION IN OIL SCREEN, POSSIBLY CRANKSHAFT BEARING.
- [SDR 2008FA0000560](https://openairdocs.org/sdr/2008FA0000560.md): Valve · damaged · Aug 8, 2008 · N9927V · Cessna R172K · Nose/Tail Landing Gear Strut/Axle
  > A NEW VALVE WAS ORDERED AND INSTALLED TO CURE A SUSPECTED LEAK IN THE VALVE CORE. THE NEW VALVE ARRIVED WITH A BRIGHT APPEARANCE, EITHER CHROME OR NICKEL PLATED. WITH THE NEW VALVE INSTALLED, THE STRUT LEAK WORSENED. AN EXTERNAL INSP REVEALED THAT THE COSME
- [SDR 2008FA0000186](https://openairdocs.org/sdr/2008FA0000186.md): Mount Bracket · cracked · Mar 6, 2008 · N758PX · Cessna R172K · Engine Mount Section
  > FOUND UPPER LT ENGINE MOUNT BRACKET CRACKED WHILE INSPECTING FOR CESSNA SEB07-2 REV 2. THIS SERVICE BULLETIN DOES NOT APPLY TO THIS SERIAL NUMBER, ALTHOUGH A CRACK WAS FOUND. RECOMMEND INCREASING THE SERIAL NUMBER RANGE OF AFFECTED AIRCRAFT. THIS SHOP HAS A
- [SDR 2007FA0000643](https://openairdocs.org/sdr/2007FA0000643.md): Wheel · misrepaired · Jun 13, 2007 · N736MV · Cessna R172K · Wheel/Ski/Float
  > DURING TAKEOFF FROM A GRASS STRIP AS THE AIRCRAFT APPROACHED 30 TO 40 KNOTS, BOTH NOSE WHEELS INSTALLED ON THE FLOATS FAILED, CAUSING THE AIRCRAFT TO FLIP ON TO ITS BACK. UPON EXAMINATION OF THE FLOAT NOSE WHEEL STRUTS THE FAILURE OCCURRED AT THE WELD JOINT O
- [SDR 2007FA0000112](https://openairdocs.org/sdr/2007FA0000112.md): Air Filter · twisted · Jan 8, 2007 · N758EJ · Cessna R172K · Engine Air Intake System
  > DURING REMOVAL OF THE AIR FILTER THE CENTER WIRE MESH SCREEN WAS FOUND TWISTED AND BENT. SOME OF THE WELDS WERE BROKEN. SCREEN DEFORMATION CAN LEAD TO UNFILTERED AIR AND FOD ENTERING THE ENGINE. APPARENT CAUSE IS EITHER OVERTORQUEING WING NUT AND/OR INSUFFI
- [SDR CA060209003](https://openairdocs.org/sdr/CA060209003.md): Governor · damaged · Feb 2, 2006 · Cessna R172K · Propeller Governor
  > (CAN) ENGINE OVERSPEED ON A TOUCH AND GO LANDING AT AIRPORT, ON TAKEOFF. ENGINE WAS REPORTED ROUGH ON THE RETURN FLIGHT. THE INSTRUCTOR AND THE OWNER ONBOARD DECIDED TO DECLARE AN EMERGENCY AND LAND BACK WHERE THE AIRCRAFT IS BASED AT THIS TIME. MAINTENANCE
- [SDR 2006FA0000045](https://openairdocs.org/sdr/2006FA0000045.md): Distributor Gear · failed · Jan 18, 2006 · N4718K · Cessna R172K · Magneto/Distributor
  > ELEVEN GEAR TEETH FAILED ON NYLON DISTRIBUTOR GEAR.
- [SDR EY2R77637](https://openairdocs.org/sdr/EY2R77637.md): Hub · corroded · Oct 11, 2005 · Cessna R172K · Propeller Hub Section
  > PITTING CORROSION ON INTERNAL SURFACES OF PROPELLER HUB.
- [SDR CA050416001](https://openairdocs.org/sdr/CA050416001.md): Spar · cracked · Apr 15, 2005 · Cessna R172K · Horizontal Stabilizer, Spar/Rib
  > (CAN) FRONT SPAR CRACKED CENTER SECTION AT LIGHTNING HOLE.
- [SDR 2004FA0000785](https://openairdocs.org/sdr/2004FA0000785.md): Pcu · frozen · Aug 27, 2004 · N218H · Cessna R172K · Propeller Controlling System
  > NEW PROP CONTROL INSTALLED IAW SRM, CONTROL OPERATED FINE, AIRCRAFT WAS FLOWN ONCE AFTER COOL DOWN. PROP CONTROL WAS FROZEN, WAS ABLE TO BREAK FREE, INSTALLATION AND RIGGING CHECKED, PROP GOVERNOR CHECKED, AIRCRAFT FLOWN AGAIN, PROP CONTROL FROZEN AGAIN AFTER
- [SDR AUS20040499](https://openairdocs.org/sdr/AUS20040499.md): Piston · failed · Apr 18, 2004 · Cessna R172K · Reciprocating Engine Power Section
  > (AUS) PISTON FAILED. SUSPECT FAULTY INJECTOR. LIMITED INFORMATION PROVIDED.
- [SDR 2004FA0000340](https://openairdocs.org/sdr/2004FA0000340.md): Rocker · broken · Mar 31, 2004 · N736DU · Cessna R172K · Reciprocating Engine Cylinder Section
  > FOUND HOLE IN ROCKER COVER CAUSED BY ROCKER ARM ON EXHAUST SIDE. FOUND FWD STUD ASSY BROKEN OFF FLUSH WITH CYLINDER HEAD. STUD (PN 401852). ROCKER RETAINER (PN 631996) WAS BROKEN AND HALF MISSING (GONE OUT OF HOLE IN COVER) IB STUD HOLD DOWN NUT WAS 4 TO 5
- [SDR CA031216003](https://openairdocs.org/sdr/CA031216003.md): Bracket · cracked · Nov 17, 2003 · Cessna R172K · Engine Mount Section
  > (CAN) ENGINE MOUNT TO FIREWALL 1/B LT LOWER CHANNEL BRACKET FOUND CRACKED. REPLACED WITH NEW.
- [SDR CA020611004](https://openairdocs.org/sdr/CA020611004.md): Bearing · seized · May 26, 2002 · Cessna R172K · Alternator-Generator Drive
  > (CAN) ALTERNATOR FAILURE. REAR ROLLER BEARING SEIZED SHAFT CAUSING SHAFT TO SHEAR IMMEDIATELY AFT OF THE DRIVE ASSEMBLY.NO EVIDENCE OF OR ADEQUATE LUBRICANT IN AFFECTED BEARING. OTHER PARTS OF THE ALTERNATOR APPEARED IN GOOD CONDITION EXCEPT FOR THE BRUSHES WH
- [SDR 2002FA0000683](https://openairdocs.org/sdr/2002FA0000683.md): Bushing · worn · May 23, 2002 · N3712V · Cessna R172K · DC Generator-Alternator
  > ENGINE DRIVEN ALTENATOR DRIVE FOUND WORN.
- [SDR AUS20011382](https://openairdocs.org/sdr/AUS20011382.md): Exhaust Valve · worn · Oct 10, 2001 · Cessna R172K · Reciprocating Engine Cylinder Section
  > (AUS) EXHAUST VALVE GUIDE WORN EXCESSIVELY. INVESTIGATION FOUND SPRINGCAP RIDING UP ON VALVE AND CONTACTING ROCKER ARM DUE TO WORNCOLLETS.
- [SDR AUS20010938](https://openairdocs.org/sdr/AUS20010938.md): Piston · damaged · Feb 14, 2001 · Cessna R172K · Reciprocating Engine Cylinder Section
  > (AUS) NR 2 CYLINDER PISTON HOLED IN AREA OF RING GROOVES. EXCESSIVE CRANKCASE PRESSURE VENTED OIL THROUGH THE BREATHER. LOSS OF OIL PRESSURE CAUSED NR 1 CYLINDER CONNECTING ROD BIGEND FAILURE. INVESTIGATION FOUND A PIECE OF BROKEN PISTON RING HAD BEEN WORKING
- [SDR AU010008](https://openairdocs.org/sdr/AU010008.md): Retainer · cracked · Jan 3, 2001 · Cessna R172K · Reciprocating Engine Cylinder Section
  > (AUS) NR 3 CYLINDER ROCKER HAT REMOVED TO REPAIR OIL LEAK. THE ROCKER PIN RETAINER WAS FOUND TO CRACKED. ON FURTHER INSPECTION OTHER ROCKER PIN RETAINERS SHOWED SIGNS OF INCIPIENT FAILURE.
- [SDR CA000606007](https://openairdocs.org/sdr/CA000606007.md): Support Bracket · worn · May 20, 2000 · Cessna R172K · Trailing Edge Flaps
  > (CAN) WEAR WAS FOUND WHERE ROLLER IS ATTACHED TO THE FLAP SUPPORT RIB. BEARING MUST BE REMOVED TO INSPECT. FOUND WORN OVER 1/3 THROUGH FLAP SUPPORT RIB, IN NICE CIRCLES CAUSED BY BEARING/ROLLER ITSELF. THIS THE 2ND CASE SUBMITTER HAS SEEN.
- [SDR AU990038](https://openairdocs.org/sdr/AU990038.md): Line · fractured · Jan 16, 1999 · Cessna R172K · Engine Fuel Distribution
  > (AUS) NR 2 CYLINDER INJECTOR LINE FRACTURED AT THE FERRULE ON THE DISTRIBUTOR END.
- [SDR 98ZZZX4825](https://openairdocs.org/sdr/98ZZZX4825.md): Skin · cracked · Nov 30, 1998 · N758HC · Cessna R172K · Nacelle/Pylon, Bulkhead/Firewall
  > SEVERE CRACKING OF LOWER COWL AT CORNERS OF COWL FLAP CUT-OUT. CRACKS EXTEND THROUGH DOUBLER P/N 0552145-1.
- [SDR 98ZZZX4824](https://openairdocs.org/sdr/98ZZZX4824.md): Skin · cracked · Nov 30, 1998 · N736FC · Cessna R172K · Nacelle/Pylon, Bulkhead/Firewall
  > SEVERE CRACKING OF LOWER COWL AT BOTH CORNERS OF THE COWL FLAP CUT-OUT. CRACKS EXTEND THROUGH DOUBLER P/N 0552145-1.
- [SDR 99ZZZX491](https://openairdocs.org/sdr/99ZZZX491.md): Cylinder · cracked · Oct 25, 1998 · N5453V · Cessna R172K · Reciprocating Engine Cylinder Section
  > DURING INSPECTION FOR AN OIL LEAK, FOUND THE ENGINE CYLINDER HEAD CRACKED BEHIND THE ROCKER COVER AREA AND EXTENDING BEHIND THE INTAKE VALVE SPRAY. ONE DAY LATER, FOUND SIMILAR CRACK ON A DIFFERENT AIRPLANE WITH THE SAME MODEL ENGINE. AFTER CLOSE INSPECTION,
- [SDR 98ZZZX4476](https://openairdocs.org/sdr/98ZZZX4476.md): Piston Pin · broken · Oct 15, 1998 · N736VN · Cessna R172K · Reciprocating Engine Cylinder Section
  > ENGINE DISASSEMBLED PER AD 98-19-02. FOUND NR 4 PISTON PIN BROKEN INTO TWO PIECES. REBUSHED NR 4 CONNECTING ROD, INSTALLED NEW PISTON AND RINGS. REPLACED ALL PISTON PINS WITH NEW.
- [SDR CA980825007](https://openairdocs.org/sdr/CA980825007.md): Blade · corroded · Aug 21, 1998 · Cessna R172K · Propeller Blade Section
  > (CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. PAINT WAS REMOVED FROM THE BLADES AND CORROSION WAS FOUND ON THE CAMBER AND THE THRUST FACE OF THE PROPELLER BLADES. THE CORROSION WAS REMOVED BY GRINDING IN ACCORDANCE WITH MCCAULEY SERVICE MANUAL 780630 AN
- [SDR 98ZZZX3427](https://openairdocs.org/sdr/98ZZZX3427.md): Magnet · cracked · Aug 17, 1998 · N758SZ · Cessna R172K · Magneto/Distributor
  > MAGNETO WAS DISASSEMBLED DUE TO BAD POINTS. INSPECTION OF ROTATING MAGNET SHOWED CRACKS ON THE BACK FACE. MAGNTO WAS REPLACED WITH NEW.
- [SDR CA980330011](https://openairdocs.org/sdr/CA980330011.md): Seal · scored · Mar 20, 1998 · Cessna R172K · Propeller Hub Section
  > (CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. THE CYLINDER WAS FOUND SCORED IN THE SEAL AREA.
- [SDR 98ZZZX1176](https://openairdocs.org/sdr/98ZZZX1176.md): Fuel Pump · defective · Mar 1, 1998 · N736XB · Cessna R172K · Engine Fuel Pump
  > IN-FLIGHT MIXTURE CONTROL WOULD STICK AND WOULD NOT GO BACK TO FULL RICH MIXTURE. PREVIOUSLY, MOISTURE STIFF BUT WOULD MOVE, AND INSPECTION FOUND NO PROBLEMS. AFTER LAST 'STICK', INSPECTION FOUND THAT IDLE CUT-OFF STOP PIN WAS LOOSE IN ITS HOLE AND FREE TO M
- [SDR CA980309007](https://openairdocs.org/sdr/CA980309007.md): Bearing · corroded · Feb 24, 1998 · Cessna R172K · Propeller Assembly
  > (CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. THE FOLLOWING PARTS WERE FOUND CORRODED: 2 BEARING SETS; 2 ACTUATING PINS; 2 PISTON PINS; 1 CYLINDER; 80 BALL BEARINGS AND ALL PROPELLER INTERNAL PARTS. THE SUBMITTER SUGGESTS THIS CORROSION WOULD HAVE CAUSED
- [SDR AU980210](https://openairdocs.org/sdr/AU980210.md): Cylinder · separated · Feb 22, 1998 · Cessna R172K · Reciprocating Engine Cylinder Section
  > (AUS) RT REAR CYLINDER HEAD SEPARATED.
- [SDR AU980209](https://openairdocs.org/sdr/AU980209.md): Cylinder · failed · Feb 18, 1998 · Cessna R172K · Reciprocating Engine Cylinder Section
  > (AUS) RT FRONT CYLINDER HEAD SEPARATED AT ROCKER BOLT DOWN PAD.
- [SDR CA971128005](https://openairdocs.org/sdr/CA971128005.md): Control Cable · misinstalled · Nov 4, 1997 · Cessna R172K · Autopilot System
  > (CAN) AUTOPILOT NOT FUNCTIONING PROPERLY. AILERON SERVO CABLES INSTALLED IN REVERSE, REPAIRED.
- [SDR 97ZZZX4744](https://openairdocs.org/sdr/97ZZZX4744.md): Spring Assy · corroded · Oct 27, 1997 · N1092V · Cessna R172K · Main Landing Gear Strut/Axle/Truck
  > FOUND DURING A SCHEDULED INSPECTION. MAIN LANDING GEAR AND SPRING ASSEMBLY CORRODED AND RUSTY. AIRCRAFT TOTAL TIME 2,283.2 HOURS. THE SUSPECT CAUSE WAS FAILURE OF NOT REMOVING GEAR FAIRINGS DURING INSPECTIONS. SUBMITTER RECOMMENDATION IS TO REMOVE FAIRINGS
- [SDR 97ZZZX4743](https://openairdocs.org/sdr/97ZZZX4743.md): Spring Assy · corroded · Oct 27, 1997 · N1092V · Cessna R172K · Main Landing Gear Strut/Axle/Truck
  > FOUND DURING A SCHEDULED INSPECTION. MAIN LANDING GEAR AND SPRING ASSEMBLY CORRODED AND RUSTY. AIRCRAFT TOTAL TIME 2,283.2 HOURS. THE SUSPECT CAUSE WAS FAILURE OF NOT REMOVING GEAR FAIRINGS DURING INSPECTIONS. SUBMITTER RECOMMENDATION IS TO REMOVE FAIRINGS
- [SDR AU971338](https://openairdocs.org/sdr/AU971338.md): Plug · loose · Oct 26, 1997 · Cessna R172K · Reciprocating Engine Oil System
  > (AUS) ENGINE OIL DRAIN PLUG NOT TIGHTENED OR LOCKWIRED FOLLOWING AN OIL CHANGE. PERSONNEL/MAINTENANCE ERROR.
- [SDR 97ZZZX4625](https://openairdocs.org/sdr/97ZZZX4625.md): Crankcase · fractured · Oct 2, 1997 · N7342K · Cessna R172K · Reciprocating Engine Power Section
  > LT CRANKCASE BROKE OFF AT THE TOP SIDE AT THE PERIMETER OF NR 2 CYLINDER BASE. SUSPECT CAUSE, FAILURE OF FWD THROUGH-BOLT NUT OR THREADS OR POSSIBLE INTERNAL FLAW IN CRANKCASE HALF.
- [SDR CA970930002](https://openairdocs.org/sdr/CA970930002.md): Fuel Inject Line · broken · Sep 24, 1997 · Cessna R172K · Engine Fuel Distribution
  > (CAN) DURING FLIGHT THE ENGINE WAS RUNNING ROUGH WITH A LOSS OF POWER. THERE WAS ALSO THE SMELL OF FUEL. POST FLIGHT INSPECTION FOUND THE NR6 FUEL INJECTOR LINE BROKEN AT THE DISTRIBUTOR CENTRE OF THE ENGINE. THE CAUSE OF THE FAILURE WAS THE THROTTLE CONTROL C
- [SDR CA970930012](https://openairdocs.org/sdr/CA970930012.md): Blade · damage · Sep 19, 1997 · Cessna R172K · Propeller Blade Section
  > (CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. PROPELLER BLADE FOUND WITH STONE DAMAGE. PROPELLER BLADE WAS TRIMMED.
- [SDR 97ZZZX3421](https://openairdocs.org/sdr/97ZZZX3421.md): Alternator · cracked · Jul 21, 1997 · N758BZ · Cessna R172K · DC Generator-Alternator
  > TOTAL AIRCRAFT TIME 3,176.9 HOURS. DURING AN ANNUAL INSPECTION, THE ALTERNATOR FORWARD HOUSING WAS FOUND CRACKED AT THE WEB SUPPORTS. SUBMITTER SUGGESTS ALTERNATOR BE INSPECTED IN MORE DETAIL.
- [SDR CA970702021](https://openairdocs.org/sdr/CA970702021.md): Spinner Prop · cracked · Jun 18, 1997 · Cessna R172K · Propeller Spinner Section
  > (CAN) THE PROP SPINNER WAS CHANGED DUE TO CRACKING AT 21.7 HOURS. AT 62.5 HOURS THE NEW SPINNER TORE AT THE SCREW ATTACH HOLES. SUBMITTER INSTALLED AN OLDER SPINNER AND SUGGESTS A MANUFACTURING FAULT.
- [SDR CA970612006](https://openairdocs.org/sdr/CA970612006.md): Pin Base Assembl · worn · Jun 5, 1997 · Cessna R172K · Propeller Hub Section
  > (CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. PIN BASE ASSEMBLY REPLACED DUE TO WE

Next page: https://openairdocs.org/model/cessna-r172k/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 = 'R172K'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/cessna-r172k/reports

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