# Service difficulty reports: Cessna R182

A list on [Cessna R182](https://openairdocs.org/model/cessna-r182.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 5 · 219 reports

- [SDR 2026FA0000311](https://openairdocs.org/sdr/2026FA0000311.md): Tube · melted · May 1, 2026 · N736ZG · Cessna R182 · Pitot/Static System
  > OWNER ADVISED TECHNICIAN THAT NEITHER OF THE TWO AIRSPEED INDICATORS WERE READING. WHEN TECHNICIAN OPENED INSPECTION PANELS NEAR THE PITOT PROBE, THE PLASTIC TUBING WAS FOUND TO BE MELTED THROUGH BY WHAT APPEARED TO BE A WIRE. TECHNICIAN FOUND THAT THE WIRES C
- [SDR 2024FA0000741](https://openairdocs.org/sdr/2024FA0000741.md): Magneto · making metal · Sep 25, 2024 · N756MN · Cessna R182 · Magneto/Distributor
  > RECENTLY INSTALLED ELECTROAIR ELECTRONIC IGNITION SYSTEM EIS-61000-5M AND EIS-61000-5C. WHILE TROUBLE SHOOTING ERRONEOUS RPM INDICATIONS WE OPENED THE COVER OF THE MAGNETO TIMING HOUSING (MTH) AND FOUND SIGNIFICANT SHAVINGS IN THE CASE. BORESCOPE INSPECTION SH
- [SDR 2022FA0000697](https://openairdocs.org/sdr/2022FA0000697.md): Starter · fire · Nov 14, 2022 · N414FH · Cessna R182 · Engine Starter
  > A/C CAME IN FOR A 50HR OIL CHANGE AND ELECTRICAL ISSUES. FOUND THAT UPON INSTALL OF NEW ENGINE, REPAIR STATION REMOVED A JUMPER WIRE FROM A 12V STARTER AGAINST THE INSTRUCTIONS LISTED ON PART AND SL, WHICH ALLOWED IT TO RECEIVE 24V FOR WHICH THE A/C WAS RATED
- [SDR 2022FA0000149](https://openairdocs.org/sdr/2022FA0000149.md): Propeller · worn · Mar 11, 2022 · N271RG · Cessna R182 · Propeller Hub Section
  > PROPELLER WAS LEAKING OIL. HAD OUR SHOP PULL THE PROPELLER AND SEND IT OFF TO BE RE-SEALED. PROP SHOP DISCOVERED THAT THE PISTON HAD WORN OUT OF SPEC. SCORING WAS FOUND ON THE INSIDE OF THE PISTON WHERE IT RIDES ON THE GUIDE. WEAR MARS ARE 180 DEGREES APART ON
- [SDR 2022FA0000003](https://openairdocs.org/sdr/2022FA0000003.md): Spinner · fractured · Jan 5, 2022 · N4696T · Cessna R182 · Propeller Spinner Section
  > ON RUNUP AFTER AN OIL CHANGE, DETECTED A NOTICEABLE WOBBLE ON THE PROPELLER SPINNER. AFTER ENGINE SHUTDOWN FOUND THAT THE SPINNER WAS EASILY DEFLECTED AN INCH OR SO. REMOVED SPINNER,AND FOUND THAT THE INNER FLANGE ON THE SPINNER FORWARD BULKHEAD WAS FRACTURED
- [SDR 2020FA0000488](https://openairdocs.org/sdr/2020FA0000488.md): Sleeve · worn · Sep 12, 2020 · N4893T · Cessna R182 · Landing Gear Door Retract Section
  > PILOT REPORTED THAT HE WAS ABOUT TO LAND AT PVD WHEN HE DIDN'T HAVE 3 IN THE GREEN. THE MAINS WERE DOWN AND LOCKED. HE FLEW BY THE TOWER TWICE AND THEY CONFIRMED THAT THE NOSE WHEEL DOORS WEREN'T EVEN OPEN. HE CYCLED THE GEAR A NUMBER OF TIMES, TO NO AVAIL.
- [SDR CA190621004](https://openairdocs.org/sdr/CA190621004.md): Circuit Breaker · defective · Jun 20, 2019 · Cessna R182 · Electrical Power System Wiring
  > (CAN) ALTERNATOR 60 AMP.BREAKER WITH INTERNAL RESISTANCE (IN 28V OUT 8V) THIS WILL MAKE THE ALTERNATOR STOP CHARGING.... (TC# 20190621004)
- [SDR CA190621006](https://openairdocs.org/sdr/CA190621006.md): Float · failed · Jun 13, 2019 · Cessna R182 · Fuel Control/Reciprocating Engines
  > (CAN) CARBURATOR FLOAT FILLED WITH AVGAS THIS IS THE SECOND TIME IT HAPPEN ON ARE FLEET WITH THIS PART (REF SDR#20170503018) (TC# 20190621006)
- [SDR 2016FA0000403](https://openairdocs.org/sdr/2016FA0000403.md): Bracket · cracked · Aug 31, 2016 · N9076C · Cessna R182 · Trailing Edge Flaps
  > THE INBOARD FLAP SUPPORT ARM CAME IN CONTACT WITH A SUPPORT BRACKET THAT ATTACHES THE LOWER WING SKIN TO THE FLAP TRACK IN AN EFFORT TO STIFFEN THE SKIN. THE SUPPORT BRACKET HAD A LONGITUDINAL CRACK ALONG THE INSIDE OF A NINETY DEGREE RADIUS. BECAUSE OF THE
- [SDR YN8R201605180001](https://openairdocs.org/sdr/YN8R201605180001.md): Seat Track · cracked · May 18, 2016 · N182JF · Cessna R182 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ANNUAL INSPECTION, WHILE INSPECTING IAW AD2011-10-09, CRACKS WERE FOUND LIKE FIGURE 5 OF AD, ITEM 1 WITH VERTICAL CRACK SHOWN AS ITEM 2 COMING OUT OF SAME CRACKED HOLE. R & R SEAT TRACK.
- [SDR PAIR201604133229](https://openairdocs.org/sdr/PAIR201604133229.md): Pivot Assy · cracked · Apr 13, 2016 · N4728T · Cessna R182 · Main Landing Gear Attach Section
  > DURING ANNUAL INSPECTION FOUND RT MLG PIVOT, PN 2241102-7 WITH A CRACK APPROXIMATELY 3" LONG WHERE GEAR LEG ATTACHES.
- [SDR PAIR2016041303229](https://openairdocs.org/sdr/PAIR2016041303229.md): Support Bracket · cracked · Apr 13, 2016 · N4728T · Cessna R182 · Fuselage, Landing Gear Attach Fittings
  > DURING ANNUAL INSPECTION, FOUND NOSE GEAR ACTUATOR AFT SUPPORT WITH MULTIPLE CRACKS.
- [SDR 2015FA0000591](https://openairdocs.org/sdr/2015FA0000591.md): Cylinder Head · cracked · Nov 19, 2015 · N5897E · Cessna R182 · Reciprocating Engine Cylinder Section
  > PILOT REPORTED A LOSS OF 300-400, RPM SHORTLY AFTER TAKEOFF AND RETURNED TO AIRPORT. PERFORMED COMPRESSION CHECK AND FOUND 3 CYLINDERS CRACKED FROM THE INTAKE VALVE TO THE SPARK PLUG HOLE, CYLINDERS 1, 2 & 5. CYLINDER NR 3 WAS ALSO FOUND TO HAVE LOW COMPRESSI
- [SDR CA151030019](https://openairdocs.org/sdr/CA151030019.md): Pin · sheared · Oct 28, 2015 · Cessna R182 · Propeller Governor
  > (CAN) GOVERNOR CONTROL ARM STOP PIN SHEARED OFF.
- [SDR CA151026005](https://openairdocs.org/sdr/CA151026005.md): Pin · broken · Oct 17, 2015 · Cessna R182 · Propeller Governor
  > (CAN) STOP PIN WAS NOTICED MISSING. THE PIN HAD BROKEN OFF FLUSH OF THE PROP GOVERNOR CONTROL LEVER ASSY. THE PILOT FIRST NOTICED AND REPORTED THAT THE ENGINE RPM WAS REACHING AND EXCEEDING THE RED LINE. THE STOP PIN ALLOWS THE CONTROL LEVER ASSY TO CONTACT
- [SDR J4YR201509151245](https://openairdocs.org/sdr/J4YR201509151245.md): Pivot · cracked · Sep 15, 2015 · N1702R · Cessna R182 · Hydraulic System, Main
  > CUSTOMER REPORTED THAT BRAKE HYDRAULIC FLUID WAS LEAKING FROM THE ACFT BELLY. ACCESSED BELLY TO DETERMINE WHERE LEAKAGE ORIGINATED FROM. DISCOVERED FLUID IN THE AREA OF THE LT LANDING GEAR ACTUATOR. UPON CLOSER EXAMINATION OF THE LT LANDING GEAR COMPONENTS
- [SDR LJ8S2015FA0000425](https://openairdocs.org/sdr/LJ8S2015FA0000425.md): Actuator · failed · Aug 25, 2015 · N2696C · Cessna R182 · Landing Gear Actuator
  > SELECTED GEAR DOWN PRIOR TO LANDING. GREEN DOWN LIGHT DID NOT ILLUMINATE AND GEAR WARNING HORN ACTIVATED. THE MAIN WHEELS COULD BE SEEN AND FELT IN THE DOWN LOCKED POSITION. A MIRROR ON THE RT WING SHOWED THAT THE NOSE GEAR WAS DOWN, BUT IT COULD NOT BE DE
- [SDR CGFR2015FA0000140](https://openairdocs.org/sdr/CGFR2015FA0000140.md): Piston · broken · Mar 19, 2015 · N977LA · Cessna R182 · Landing Gear Actuator
  > ON 02/03/2015 ACFT WAS CONDUCTING A TRAINING FLIGHT AND ON THE FINAL LANDING GEAR CYCLE, THE GEAR FAILED TO GIVE A POSITIVE DOWN AND LOCKED INDICATION. THE GEAR WAS TRANSITIONING FROM UP TO DOWN AND BEFORE IT REACHED THE DOWN POSITION, THE CREW HEARD A "POP"
- [SDR 2015FA0000076](https://openairdocs.org/sdr/2015FA0000076.md): Cam · damaged · Jan 21, 2015 · N1668R · Cessna R182 · Landing Gear System
  > LOW MANIFOLD PRESSURE. THROTTLE ARM LOOSE ON CARBURETOR SHAFT. CAM FOR LANDING GEAR WARNING SWITCH BOTTOMS OUT ON SHAFT STEP PREVENTING PROPER ENGAGEMENT OF THROTTLE ARM AND SHAFT. DRILLED CAM TO ALLOW IT TO FIT OVER STEP ON THROTTLE SHAFT.
- [SDR 2014FA0000487](https://openairdocs.org/sdr/2014FA0000487.md): Fitting · fractured · Aug 17, 2014 · N292LC · Cessna R182 · Fuel Controlling System
  > DURING A PART 91 FLIGHT, THE PILOT NOTICED ABNORMAL FUEL FLOW AND PRESSURE READINGS AND DECIDED TO RETURN TO THE AIRPORT. DURING THE DESCENT TO FINAL APPROACH, THE PILOT AND 1 PASSENGER NOTICED SMOKE AND FLAMES COMING FROM CO-PILOT RUDDER PEDAL AREA. AN EMERG
- [SDR 2014FA0000584](https://openairdocs.org/sdr/2014FA0000584.md): Pivot Assy · sheared · Jul 17, 2014 · N7571T · Cessna R182 · Main Landing Gear
  > RIGHT MLG DID NOT EXTEND INTO THE DOWN AND LOCKED POSITION. RT GEAR LEG WAS IN TRAIL WHEN ACFT LANDED WITH THE NOSE GEAR AND LT MAIN DOWN AND LOCKED. CAUSED ACFT TO VEER TO THE RT ON LANDING, CAUSING DAMAGE TO THE RT WINGTIP AND HORIZONTAL STABILIZER AND RT
- [SDR 2014FA0000022](https://openairdocs.org/sdr/2014FA0000022.md): Float · failed · Jan 14, 2014 · N517MS · Cessna R182 · Fuel Control/Reciprocating Engines
  > THE ENGINE HAD A VERY ROUGH IDLE, SHUTDOWN ATTEMPT WITH IDLE CUTOFF FAILED TO ACHIEVE SHUTDOWN. ENGINE SHUTOFF WITH IGNITION AND AS EXITING THE ACFT, NOTED FUEL DRAINING FROM CARBURETOR AIR BOX. REMOVED CARBURETOR AND FOUND FLOAT FULL OF FUEL AND NO LONGER FU
- [SDR P39R20131107001](https://openairdocs.org/sdr/P39R20131107001.md): Pin · broken · Oct 21, 2013 · N756EB · Cessna R182 · Landing Gear Retraction/Extension System
  > NOSE GEAR FAILURE RESULTING IN A PROP STRIKE AND LOWER SKIN AND RIB DAMAGE. ACFT PLACED ON JACKS TO INSPECT NOSE GEAR ACTUATOR. OBSERVED THE NOSE GEAR ACTUATOR HAD NOT FULLY RETRACTED TO POSITION THE DOWN LOCKS OVER THE LOCKING PINS. 1 OF THE PINS, LT SIDE,
- [SDR 2013FA0000649](https://openairdocs.org/sdr/2013FA0000649.md): Bulkhead · cracked · Oct 4, 2013 · N2487S · Cessna R182 · Fuselage Main, Bulkhead
  > WIRING HARNESS CUTOUTS IN STA. 110 AND 124 BULKHEADS ON THE RT SIDE OF THE FUSELAGE IS CRACKED IN THE EXTREME CORNER DUE TO IMPROPER REINFORCEMENT OF BULKHEADS AND FUSELAGE FLEXING IN FLIGHT. REMANFACTURE OF BULKHEAD WITH THICKER MATERIAL TO WITHSTAND IN FLIG
- [SDR 2013FA0000648](https://openairdocs.org/sdr/2013FA0000648.md): Bulkhead · cracked · Oct 4, 2013 · N756MN · Cessna R182 · Fuselage Main, Bulkhead
  > CRACK IN WIRING HARNESS CUTOUT IN BULKHEAD AT STA 124, DUE TO IMPROPER REINFORCEMENT OF BULKHEAD AND FUSELAGE FLEXING IN FLIGHT. RECOMMEND REMANFACTURE OF BULKHEAD WITH THICKER MATERIAL TO WITHSTAND IN-FLIGHT STRESS OR ENSURE THAT BULKHEAD IS PROPERLY SUPPORT
- [SDR 2013FA0000458](https://openairdocs.org/sdr/2013FA0000458.md): Strut · damaged · May 12, 2013 · N6096T · Cessna R182 · Wing Main, Frame Structure
  > ON INSPECTION OF WING UPPER LIFT STRUT ATTACHMENT POINTS, A BLACK RING WAS NOTED AROUND THE MOST FWD RIVET IN A CLUSTER OF FOUR. EXAMINATION SHOWED THAT THERE WAS MOVEMENT BETWEEN THE RIVET AND THE SURROUNDING STRUT ATTACHMENT. FURTHER EXAMINATION OF THE LT
- [SDR 2013FA0000137](https://openairdocs.org/sdr/2013FA0000137.md): Distributor Gear · broken · Feb 28, 2013 · N2114S · Cessna R182 · Magneto/Distributor
  > DURING INSPECTION, DISCOVERED MAGNETO DISTRIBUTOR GEAR, MISSING TEETH ON BOTH GEARS.
- [SDR 2013FA0000023](https://openairdocs.org/sdr/2013FA0000023.md): Wire · burned · Jan 11, 2013 · N2744C · Cessna R182 · Instrument System Wiring
  > THE ALTERNATOR REGULATOR AND FUEL PUMP CIRCUT BREAKERS WOULD POP AND NOT RESET. FOUND THE BUSS BAR TO BE HOT TO THE TOUCH BEHIND THOSE BREAKERS. THE BUSS BAR WAS HOT ENOUGH THAT THE BREAKERS WHERE TRIPPING FROM THE HEAT. FOUND WIRE NR PA4 FROM THE ALTERNATO
- [SDR 2012FA0000763](https://openairdocs.org/sdr/2012FA0000763.md): Bolt · backed out · Nov 10, 2012 · N2623C · Cessna R182 · Landing Gear Brake System
  > PILOT REPORTED LT LANDING GEAR WOULD NOT EXTEND. ACFT LANDED GEAR UP. FOUND 1 TIE BOLT ON LT BRAKE CALIPER HAD BACKED OUT AND WEDGED BETWEEN THE CALIPER AND GEAR WELL NOT ALLOWING LANDING GEAR TO EXTEND.
- [SDR CA120522015](https://openairdocs.org/sdr/CA120522015.md): Diode · failed · May 21, 2012 · Cessna R182 · Landing Gear System Wiring
  > (CAN) LANDING GEAR POWER PACK DIODE BURNED, DIODE REPLACE. LANDING GEAR SYS TESTED.
- [SDR 2011FA0000494](https://openairdocs.org/sdr/2011FA0000494.md): Baffle · loose · Jul 5, 2011 · N7392X · Cessna R182 · Engine Noise Suppressor
  > CONE SHAPED BAFFLE IN MUFFLER CAME LOOSE AND COMPLETELY BLOCKED EXHAUST STACK.
- [SDR 2010FA0001192](https://openairdocs.org/sdr/2010FA0001192.md): Tappet · making metal · Nov 22, 2010 · N1806R · Cessna R182 · Reciprocating Engine Power Section
  > THESE TAPPETS WERE SOME OF THE FIRST PRODUCED, UNDER THIS NEW PN. FOUND 8 OF 12 IN THE ENGINE IN DISTRESSED CONDITION AND MAKING METAL. PN 15B26064
- [SDR 2010FA0001092](https://openairdocs.org/sdr/2010FA0001092.md): Bushing · damaged · Sep 17, 2010 · N2487S · Cessna R182 · Fuel Control/Reciprocating Engines
  > REPORT CAME BACK FROM PILOT THAT THEY HAD AN ENGINE FAILURE IN THE PATTERN AT U30. THE ACFT LANDED WITH NO POWER AVAILABLE. PUMPING THE ACFT THROTTLE WOULD KEEP THE ENGINE RUNNING. PROBLEM WAS DETERMINED TO BE CARBURETOR. MFG SERVICE DEPARTMENT WAS CONSULT
- [SDR CA100723008](https://openairdocs.org/sdr/CA100723008.md): Drive Gear · worn · Jul 21, 2010 · Cessna R182 · Engine Starter
  > A WHISTLING NOISE WAS NOTED BY GROUND PERSONNEL DURING TAXI. AFTER SHUTDOWN, A VISUAL CHECK REVEALED THAT THE STARTER DRIVE HAD NOT FULLY RETRACTED AND THE DRIVE GEAR`S TEETH HAD BEEN WORN BY THE ENGINE RING GEAR. DISASSEMBLY OF THE STARTER FOUND GREASE ON DR
- [SDR CA100525017](https://openairdocs.org/sdr/CA100525017.md): Transponder · odor · May 22, 2010 · Cessna R182 · Communications System
  > WHILE IN FLIGHT THE PILOT SAW SOME SMOKE COMING OUT FROM UNDER THE DASH NEARBY THE TRANSPONDER. THE PILOT RETURN TO THE BASE WITHOUT ANY PROBLEM. AFTER INVESTIGATION THE TRANSPONDER WAS SMELLING LIKE SMOKE, LIKE SOMETHING THAT BURNED INSIDE. SERVICEABLE TRA
- [SDR 2010FA0000133](https://openairdocs.org/sdr/2010FA0000133.md): Pivot · cracked · Feb 7, 2010 · Cessna R182 · Standard Practices/Structures
  > PIVOT CRACKED AT INBD END OF SHAFT.
- [SDR CA090506011](https://openairdocs.org/sdr/CA090506011.md): Line · clogged · May 6, 2009 · Cessna R182 · Manifold Pressure (MP) Indicating
  > (CAN) MANIFOLD PRESSURE STOCK AT 23 INC WHILE REDUCING FOR CRUISE SETTING, PILOT RETURN TO BASE. INSPECTION REVEAL DIRT IN MANIFOLD PRESSURE LINE AND INSTRUMENT ORIFICE. INSTRUMENT SENT TO APPROVED SHOP FOR REPAIR.
- [SDR 2009FA0000156](https://openairdocs.org/sdr/2009FA0000156.md): Pivot · sheared · Mar 2, 2009 · N2253T · Cessna R182 · Main Landing Gear Strut/Axle/Truck
  > DURING SLOW FLIGHT MANEUVERS THE INSTRUCTOR NOTICED THE GREEN GEAR SAFE LIGHT WAS OUT. THE STUDENT OBSERVED THE LEFT GEAR WAS HANGING OUT AND SWINGING. THE GEAR WAS CYCLED BUT THE GEAR REMAINED HANGING. AFTER CONTACTING DISPATCH THE INSTRUCTOR ELECTED TO RE
- [SDR CA090206005](https://openairdocs.org/sdr/CA090206005.md): Carburetor · malfunctioned · Feb 5, 2009 · Cessna R182 · Fuel Control/Reciprocating Engines
  > DURING START AND RUNUP, NR 3 CYLINDER WAS RELUCTANT TO FIRE UNLESS THE MIXTURE WAS LEANED ALMOST TO IDLE CUTOFF. ONCE THE ENGINE WAS WARM IT WOULD RUN NORMALLY. IN FLIGHT THE EGTS WERE UNEVEN, WITH NR 3 AND NR 6 MUCH COOLER THAN THE REST. BOTH OF THESE CYLI
- [SDR 2008FA0000592](https://openairdocs.org/sdr/2008FA0000592.md): Swivel Fitting · failed · Aug 21, 2008 · N4652T · Cessna R182 · Landing Gear Retraction/Extension System
  > BRAKE SWIVEL JOINT FAILED LEADING TO FAILURE OF LT BRAKE WHEN EXITING RUNWAY. (K)
- [SDR 2008FA0000235](https://openairdocs.org/sdr/2008FA0000235.md): Screw · improper part · Mar 1, 2008 · N757XU · Cessna R182 · Flight Compartment Equipment
  > MFG SB NR SEB07-3 TO CHECK THE LENGTH OF THE SCREWS IN ACCESS PLATE UNDER REAR SEAT. THE PLATE MAY HAVE HAD TOO LONG A SCREW INSTALLED WHICH COULD CAUSE A FAILURE OF THE LANDING GEAR TO OPERATE DOWN. THE SB LISTED THE PROPER SCREWS TO USE IN EACH HOLE IN THE
- [SDR 2008FA0000319](https://openairdocs.org/sdr/2008FA0000319.md): Unknown · unknown · Dec 25, 2007 · N6079C · Cessna R182 · Standard Practices/Structures
  > INFLIGHT FAILURE OF PART OR PARTS UNKNOWN WITH NO SYMPTOMS FROM WITHIN COCKPIT, IE: OIL PRESSURE, OIL TEMPERATURE, AND CYLINDER HEAD TEMPERATURES WERE ALL INDICATING WITHIN NORMAL RANGES. OUTWARD MANIFESTATIONS WERE EXCESSIVE BLOW-BY OIL ON BELLY OF THE AIRPL
- [SDR 2007FA0000583](https://openairdocs.org/sdr/2007FA0000583.md): Starter · defective · May 24, 2007 · N182MS · Cessna R182 · Engine Starter
  > REMOVED THIS STARTER FROM SAME AIRCRAFT FOR THE 4TH TIME WITH 11.3 HOURS SINCE OVERHAUL. STARTER BENDIX WOULD NOT ENGAGE ANYMORE DURING STARTUP. NO PROBLEM COULD BE FOUND WITH AIRCRAFT ELECTRICAL SYSTEM. INSTALLED ON ANOTHER AIRCRAFT TO VERIFY PROBLEM AND F
- [SDR 2007FA0000581](https://openairdocs.org/sdr/2007FA0000581.md): Starter · malfunctioned · May 18, 2007 · N182MS · Cessna R182 · Engine Starter
  > REMOVED THIS STARTER FROM SAME AIRCRAFT FOR THE 3RD TIME WITH 62.3 HRS SINCE OVERHAUL. STARTER BENDIX WOULD NOT ENGAGE ANYMORE DURING START UP. NO PROBLEM COULD BE FOUND WITH AIRCRAFT ELECTRICAL SYSTEM. (K)
- [SDR 2007FA0000372](https://openairdocs.org/sdr/2007FA0000372.md): Battery · leaking · May 2, 2007 · Cessna R182 · Emergency Locator Beacon
  > BATTERIES LEAKED INSIDE ELT UNIT PREVENTING ELT OPERATION AND DESTROYING CONTACTS INSIDE UNIT. THIS IS ONE OF SEVERAL TIMES THIS PROBLEM HAS BEEN SEEN IN THE NEWER OR MORE RECENTLY MANUFACTURED BATTERIES THIS PARTICULAR SET HAD AN EXPIRATION OF 2012 AND HAD ON
- [SDR 2007FA0000582](https://openairdocs.org/sdr/2007FA0000582.md): Starter · failed · Apr 30, 2007 · N182MS · Cessna R182 · Engine Starter
  > REMOVED THIS STARTER WITH 3.3 HOURS SINCE OVERHAUL. STARTER BENDIX STAYED ENGAGED DURING START UP. NO PROBLEM COULD BE FOUND WITH AIRCRAFT ELECTRICAL SYSTEM. (K)
- [SDR 2007FA0000580](https://openairdocs.org/sdr/2007FA0000580.md): Starter · failed · Apr 27, 2007 · N182MS · Cessna R182 · Engine Starter
  > REMOVED THIS STARTER FROM AIRCRAFT DUE TO BENDIX FAILURE. TIME ON THIS STARTER IS UNKNOWN. (K)
- [SDR 2006FA0001056](https://openairdocs.org/sdr/2006FA0001056.md): Pin · broken · Oct 22, 2006 · N5274S · Cessna R182 · Standard Practices/Structures
  > LOCKDOWN PINS BROKE AT GROOVE FOR ROLL PINS. THIS ALLOWED THE PINS TO MOVE OUT OF ACTUATOR BEARING END AND JAM THE ACTUATOR. IN THE UNLOCKED POSITION, SEB95-20 ACTUATOR DOWNLOCK PIN. INSPECTION SAYS TO CHECK FOR LOOSE PINS. THESE PINS WERE NOT LOOSE IN THE
- [SDR 2006FA0000770](https://openairdocs.org/sdr/2006FA0000770.md): Hose · leaking · Mar 20, 2006 · N3648C · Cessna R182 · Engine Fuel Distribution
  > DURING AN ANNUAL INSPECTION THE HOSE ASSEMBLY FROM THE TEE FITTING AT CARBURETOR TO THE FIREWALL FITTING FOR FUEL PSI WAS FOUND TO BE LEAKING. HOSE WAS INSTALLED 5-12-03.
- [SDR 2006FA0000769](https://openairdocs.org/sdr/2006FA0000769.md): Hose · leaking · Mar 20, 2006 · N3648C · Cessna R182 · Engine Fuel Distribution
  > DURING AN ANNUAL INSPECTION THE HOSE ASSEMBLY FROM THE ELECTRIC PUMP TO THE ENGINE DRIVEN FUEL PUMP WAS FOUND TO BE LEAKING. HOSE WAS INSTALLED 5-12-03 AND REMOVED 3-20-06.

Next page: https://openairdocs.org/model/cessna-r182/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 = 'R182'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/cessna-r182/reports

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