# Service difficulty reports: Cessna 182R

A list on [Cessna 182R](https://openairdocs.org/model/cessna-182r.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 67 reports

- [SDR 2026FA0000672](https://openairdocs.org/sdr/2026FA0000672.md): Cylinder · separated · Aug 27, 2026 · N9772H · Cessna 182R · Reciprocating Engine Cylinder Section
  > CYLINDER NR 3 HEAD SEPARATED FROM BARREL. THE OPERATOR HAD PREVIOUSLY INSPECTED AN OIL LEAK ON OR AROUND CYLINDER NR 3. PRESENTATION OF OIL LEAK AND SEPARATION OF HEAD FROM BARREL IS THE SAME AS DESCRIBED IN AD 86-13-04 R3. THIS CYLINDER PN STAMPED ON THE FLAN
- [SDR 2023FA0000376](https://openairdocs.org/sdr/2023FA0000376.md): Camshaft · distressed · Dec 7, 2021 · N9953H · Cessna 182R · Reciprocating Engine Power Section
  > DURING ROUTINE MAINTENANCE SEVERE DISTRESS OF CAMSHAFT LOBE AND LIFTERS WAS IDENTIFIED. THE MAINTENANCE WAS CARRIED OUT DURING INTERNATIONAL TRAVEL, IN AUSTRALIA. PLEASE CONTACT ME FOR PHOTOGRAPHS/ENGINE INSPECTION REPORT.
- [SDR 2021FA0000365](https://openairdocs.org/sdr/2021FA0000365.md): None · none · Dec 7, 2021 · N81MP · Cessna 182R · Autopilot System
  > ELECTRIC TRIM ACTIVATION WAS KEYING RADIO AND PRESSING PTT SWITCH WAS DISCONNECTING AUTOPILOT. THE YOKE COIL CORD INSULATION WAS FALLING OFF OF 2 ADJACENT WIRES ALLOWING THE 2 CONDUCTORS TO TOUCH AND SHORT CIRCUIT. THE COIL CORD IS A CYGNET CA3934-24 INSTALLED
- [SDR 2021FA0000256](https://openairdocs.org/sdr/2021FA0000256.md): Wire · arced · Sep 8, 2021 · N9930E · Cessna 182R · Electrical Power System Wiring
  > DURING INITIAL TAKEOFF ROLL AFTER APPLICATION OF FULL POWER. PILOT NOTICED SPARKS COMING FROM BELOW PILOT'S INSTRUMENT PANEL. POWER WAS REDUCED TO IDLE AND TAKEOFF ROLL WAS ABORTED. SPARKS STOPPED ONCE POWER WAS PULLED TO IDLE. AFTER TAXI TO RAMP AND ENGINE SH
- [SDR Q532018F00001](https://openairdocs.org/sdr/Q532018F00001.md): Gear · chipped · Sep 5, 2018 · N1262S · Cessna 182R · Reciprocating Engine Power Section
  > CRANKSHAFT GEAR CHIPPED ONE TOOTH OFF. PROB DUE TO STARTER KICKBACK (ENERGIZER STARTER). AROUND 05/20/2018 AT TACK 3175 OWNER REPORTED TICKING NOSE ON GROUND. SOUND WENT AWAY WITH INCREASE RPM. ABOUT 1500. EVENTUALLY FOUND ONE TOOTH MISSING FROM CRANKSHAF
- [SDR 2018FA0000015](https://openairdocs.org/sdr/2018FA0000015.md): Cylinder Head · separated · Dec 19, 2017 · N9851H · Cessna 182R · Reciprocating Engine Cylinder Section
  > ENGINE VIBRATION. DISCOVERED NR 3 CYLINDER LOW PRESSURE, AT 20 PSI DURING TEST. FOUND THE CYLINDER HEAD AND BARREL SEPARATING AFTER REMOVAL.
- [SDR 2017FA0000549](https://openairdocs.org/sdr/2017FA0000549.md): Cylinder · cracked · Aug 7, 2017 · N2366E · Cessna 182R · Reciprocating Engine Cylinder Section
  > CRACKED CYLINDER INSTALLED. THE ENGINE HAS APPROXIMATELY 850 HOURS ON IT SINCE OVERHAUL. DURING OVERHAUL, SIX NEW CYLINDERS WERE INSTALLED. THE ACFT RECENTLY CAME IN FOR A 50 HOUR INSPECTION AT WHICH TIME A COMPRESSION TEST WAS CONDUCTED. DURING THE COMPRE
- [SDR 2016FA0000231](https://openairdocs.org/sdr/2016FA0000231.md): Heat Exchanger · failed · Apr 15, 2016 · N619MW · Cessna 182R · Heating System
  > HEAT EXCHANGER FAILED IN FLIGHT, CAUSED MELTING OF PLASTIC, RUBBER COMPONENTS IN ENGINE COMPARTMENT. RESULTING IN SMOKE IN THE COCKPIT AND A INFLIGHT EMERGENCY DECLARED. LANDED WITHOUT INCIDENT.
- [SDR 6NAR2015FA0000566](https://openairdocs.org/sdr/6NAR2015FA0000566.md): Gasket · leaking · Oct 12, 2015 · N101SP · Cessna 182R · Reciprocating Engine Cylinder Section
  > ALL VALVE COVERS FOUND LEAKING. REMOVED ALL VALVE COVERS AND FOUND THE UPPER SECTION OF THE VALVE COVER GASKET NEAR THE EXHAUST VALVE HAD SHRUNK, PULLING IN TOWARD EXHAUST VALVE SPRING. WE HAVE FOUND THIS ISSUE ON NUMEROUS ENGINES WITH THE SUPERIOR VALVE COV
- [SDR 2011FA0000591](https://openairdocs.org/sdr/2011FA0000591.md): Cylinder Head · separated · Sep 14, 2011 · N9870E · Cessna 182R · Reciprocating Engine Cylinder Section
  > CYLINDER HEAD SEPARATION.
- [SDR 2009FA0000367](https://openairdocs.org/sdr/2009FA0000367.md): Cable · frayed · May 5, 2009 · N5481E · Cessna 182R · Propeller Governor
  > UPON APPLYING FULL THROTTLE FOR TAKEOFF, THE PILOT NOTED THAT THE ENGINE ONLY REACHED 2000 RPM. TAKEOFF WAS ABORTED AND A VISUAL CHECK OF THE PROPELLER GOVERNOR WAS MADE. THE MX RATED PILOT DETERMINED THAT THE CONTROL WAS STICKING BEFORE REACHING THE HIGH RPM
- [SDR 2009FA0000467](https://openairdocs.org/sdr/2009FA0000467.md): Tube · separated · May 1, 2009 · N5481N · Cessna 182R · Vacuum Distribution System
  > A SIGNIFICANT PROBLEM OCCURRED IN THE FUEL INDUCTION SYSTEM, WHERE A RUBBER INTAKE TUBE CONNECTS THE INTAKE MANIFOLD TO THE FUEL INDUCTION RAIL. SHORTLY AFTER A FLIGHT WHERE ENTIRELY NORMAL OPERATION WAS EXPERIENCED, ENGINE RESTART COULD NOT BE ACCOMPLISHED.
- [SDR 2009FA0000480](https://openairdocs.org/sdr/2009FA0000480.md): Piston · failed · Apr 17, 2009 · N149T · Cessna 182R · Reciprocating Engine Power Section
  > CYLINDER NR 2 PISTON SKIRT BROKE FROM THE PISTON AND CREATED A METAL CONTAMINATION IN THE ENGINE. (K)
- [SDR 2007FA0000728](https://openairdocs.org/sdr/2007FA0000728.md): Alternator · shorted · Jul 31, 2007 · N9628X · Cessna 182R · AC Generation System
  > ALTERNATOR SHORTED, THIS UNIT IS (1) OF (3) REPLACED IN THE LAST MONTHS. (K)
- [SDR 2007FA0000664](https://openairdocs.org/sdr/2007FA0000664.md): Spring Assy · cracked · Jun 28, 2007 · N5544N · Cessna 182R · Main Landing Gear Strut/Axle/Truck
  > DURING NDI OF MAIN LANDING GEAR SPRING ASSY, THE RT FITTING WAS FOUND CRACKED. DURING WFPT FOR ASTM E1417. PART WAS REPLACED WITH A SERVICEABLE UNIT. SUSPECT CRACK WAS DUE TO CORROSION BETWEEN THE SPRING AND ALUMINUM FITTING. (K)
- [SDR 2006FA0000783](https://openairdocs.org/sdr/2006FA0000783.md): Seat · broken · Jul 25, 2006 · N9983H · Cessna 182R · Flight Compartment Equipment
  > INSPECTED SEATS IAW AD. FOUND PILOTS SEAT BOTTOM ASSY BROKEN AT LT FWD ATTACH POINT AND RT FWD CRACKED. (K)
- [SDR LAT2006F00000](https://openairdocs.org/sdr/LAT2006F00000.md): Elt · inoperative · Apr 17, 2006 · N9802H · Cessna 182R · Emergency Locator Beacon
  > G-SWITCH INOPERATIVE, TOGGLE SWITCH BENT, PART NO LONGER AVAILABLE. INSTALL NEW UNIT. (K)
- [SDR 2004FA0000379](https://openairdocs.org/sdr/2004FA0000379.md): Control Cable · frayed · Apr 15, 2004 · N9873E · Cessna 182R · Rudder Control System
  > WHILE INSTALLING THE BATTERY AFTER SERVING, IT WAS NOTICED THAT THE FORWARD RT RUDDER CABLE WAS FRAYED IN TWO SPOTS. IT WAS DETERMINED THAT, AT SOMETIME, DURING BATTERY REMOVAL OR REINSTALLATION THE RUDDER CABLE ARCED ON BOTH POSITIVE AND NEGATIVE POSTS. THE
- [SDR N736ZX](https://openairdocs.org/sdr/N736ZX.md): Torque Tube · detached · Mar 11, 2004 · N736Z · Cessna 182R · Rudder Structure
  > LT RUDDER BAR TORQUE TUBE ASSEMBLY, PN 2260114-5 FAILURE. FAILURE OCCURRED IN FLIGHT RESULTING IN LT SIDE PILOT'S TOTAL LOSS OF LT RUDDER AND STEERING CONTROL. NATURE OF FAILURE; LT OB RUDDER PEDAL SOCKET ON TORQUE TUBE BROKE AWAY FROM THE TORQUE TUBE. THERE I
- [SDR 2004FA0000002](https://openairdocs.org/sdr/2004FA0000002.md): Pushrod · worn · Nov 8, 2003 · N5497N · Cessna 182R · Reciprocating Engine Cylinder Section
  > ON ROUTINE FLIGHT PILOT HEARD A BANG AND ENGINE LOST POWER BUT CONTINUED TO RUN. UNABLE TO MAINTAIN ALTITUDE, PILOT MADE AN OFF AIRPORT LANDING. FOUND NR 1 EXHAUST PUSHROD BENT, WORN AND BROKEN. REMOVED ALL CYLINDERS AND FOUND NR 1 CYLINDER INTAKE PUSHROD B
- [SDR 2003FA0001267](https://openairdocs.org/sdr/2003FA0001267.md): Pushrod · failed · Nov 8, 2003 · N5497N · Cessna 182R · Reciprocating Engine Cylinder Section
  > ON ROUTINE FLT PILOT HEARD A BANG AND ENGINE LOST POWER BUT CONTINUED TO RUN. UNABLE TO MAINTAIN ALTITUDE PILOT MADE AN OFF AIRPORT LANDING. FOUND EXHAUST PUSHROD BENT, WORN AND BROKEN. REMOVED ALL CYLINDERS AND FOUND NR 1 CYLINDER INTAKE PUSHROD BENT SLIGH
- [SDR 2004FA0000091](https://openairdocs.org/sdr/2004FA0000091.md): Piston · failed · Aug 25, 2003 · N9815H · Cessna 182R · Reciprocating Engine Power Section
  > THE PISTON WAS INSTALLED NEW AT TIME OF MAJOR OVERHAUL. ONE SIDE OF PISTON SKIRT, AT LOWER SCRAPER RING BROKE AWAY AND BECAME SMALL CHUNKS OF ALUMINUM, AND RING PIECES IN THE OIL PAN. THE PROBLEM WAS DETECTED BY APPROX 5 EACH..020 X.040 PIECES OF CAST ALU
- [SDR 2002FA0001363](https://openairdocs.org/sdr/2002FA0001363.md): Skin · cracked · Nov 1, 2002 · N9669X · Cessna 182R · Fuselage Main, Plate/Skin
  > DURING A 100 HOUR INSPECTION, A CRACK WAS FOUND IN THE FUSELAGE SKIN JUST BEHIND THE STEP THAT IS ATTACHED TO THE FUSELAGE TO AID THE PILOT FOR FUEL CAP INSPECTION OR REFUELING. THIS STEP IS LOCATED ON BOTH SIDES OF THE AIRCRAFT AT STATION 17.0 AND IS ATTACHE
- [SDR 2001FA0000229](https://openairdocs.org/sdr/2001FA0000229.md): Detector · inoperative · Jul 16, 2001 · N35VA · Cessna 182R · Stall Warning System
  > UPON INSTALLING NEW LIFT DETECTION, NOTED THAT WHEN WIRED AS ORIGINALLY REMOVED FROM AIRCRAFT, WITH HEAT TURNED ON, DETECTION WAS INOPERATIVE. GROUND FOR HEATER WAS INSTALLED ON COMMON FOR DETECTION; CAUSING A NO POTENTIAL WHEN HEATER TURNED ON.
- [SDR 2001F00248](https://openairdocs.org/sdr/2001F00248.md): Detector · inoperative · Jul 16, 2001 · N35VA · Cessna 182R · Stall Warning System
  > UPON INSTALLING NEW LIFT DETECTION NOTED THAT WHEN WIRED AS ORIGINALLY REMOVED FROM AIRCRAFT, WITH HEAT TURNED ON, DETECTION WAS INOPERATIVE. GROUND FOR HEATER WAS INSTALLED ON COMMON FOR DETECTION; CAUSING A NO POTENTIAL WHEN HEATER TURNED ON.
- [SDR 2001FA0000108](https://openairdocs.org/sdr/2001FA0000108.md): Hose · disintegrated · Jun 27, 2001 · N9953H · Cessna 182R · Vacuum Distribution System
  > CUSTOMER REPORTED LOW VACUUM INDICATION BUT GYROS RUNNING OK. INITIAL INVESTIGATION ALL HOSES LOOKED OK, HOWEVER WHEN HOSES WERE TOUCHED, FELL APART. THE ABOVE REFERENCED PN IS FOR ONE OF THE VACUUM GAUGE HOSES, HOWEVER ALL INSTRUMENT HOSE WERE OF THE SAME T
- [SDR 20010206CW003](https://openairdocs.org/sdr/20010206CW003.md): Indicator · reads low · Jan 8, 2001 · N4776T · Cessna 182R · Vacuum Indicating System
  > WHILE COMPLYING WITH AD, 3.5 MINIMUM VACUUM COULD NOT BE OBTAINED, EVEN AT SEA LEVEL. TROUBLESHOOTING REVEALED VACUUM INDICATOR WAS 2-2 1/2 IN HG LOW AND REGULATOR HAD BEEN MIS-ADJUSTED. INSTALLED NEW GAGE, WHICH WAS CALIBRATED, AND RESET REGULATOR DOWN. ST
- [SDR 20000925SH008](https://openairdocs.org/sdr/20000925SH008.md): Line · deteriorated · Sep 25, 2000 · N6545E · Cessna 182R · Vacuum Distribution System
  > WHILE CERTIFYING THE STATIC SYSTEM, DISCOVERED THE VACUUM LINES WERE DETERIORATING. AFTER FURTHER INVESTIGATION, FOUND THE VACUUM LINES WERE THE LINES THAT HAD AD ISSUED AGAINST THEM. REMOVED ALL VACUUM LINES AND REPLACED WITH NEW HOSES. POSSIBLE CAUSE FOR
- [SDR 20000925SH012](https://openairdocs.org/sdr/20000925SH012.md): Transponder · inoperative · Sep 7, 2000 · N9910H · Cessna 182R · ATC Transponder System
  > TRANSPONDER REPORTED INOPERATIVE. BENCH TEST REVEALED CAVITY TRANSMITTING AT 2,012 MEGAHERTZ AND IT COULD NOT BE ADJUSTED INTO TOLERANCE. FOUND TUBE INSTALLED WAS PC2080A, DATE CODE 99-13. INSTALLED BY FAA CRS AJVR135C, PRESENT MANUFACTURER (SIGMA-TEK) DOES
- [SDR 20000920SH016](https://openairdocs.org/sdr/20000920SH016.md): Support Bracket · cracked · Sep 1, 2000 · N9386X · Cessna 182R · Battery Box Structure
  > ON INSPECTION OF AIRCRAFT, FOUND LEFT AND RIGHT BATTERY BOX SUPPORTS CRACKED IN BEND RADIUS, P/N 0712059-1. 24V BATTERY LOCATED IN TAIL SECTION OF AIRCRAFT. NOTE: THIS PROBLEM HAS BEEN FOUND IN OTHER 182R''S. (X)
- [SDR 20000920SH015](https://openairdocs.org/sdr/20000920SH015.md): Hose · deteriorated · Aug 30, 2000 · N9386X · Cessna 182R · Vacuum Distribution System
  > FOUND HOSE MADE BY IMPERIAL EASTMAN HYTYON YP006 250 PSI W.P. FOUND OUTSIDE OF HOSE CRACKED AND COMING APART. FOUND INSIDE OF HOSE RED IN COLOR VERY BRITTLE, CRACKING. HOSE USED FOR INSTRUMENT VACUUM SERVICE. HOSE ROUTED FROM INSTRUMENT AIR FILTER TO ARTIF
- [SDR CA000606033](https://openairdocs.org/sdr/CA000606033.md): Blade · damaged · May 31, 2000 · Cessna 182R · Propeller Blade Section
  > (CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. BLADES TRIMMED, ALODINED, PAINTED.
- [SDR AU991070](https://openairdocs.org/sdr/AU991070.md): Exhaust Valve · worn · Sep 8, 1999 · Cessna 182R · Reciprocating Engine Cylinder Section
  > (AUS) NR 1 CYLINDER EXHAUST VALVE P/N 652956 AND EXHAUST VALVE GUIDE P/N 643767 WORN BEYOND LIMITS.
- [SDR 99ZZZX3655](https://openairdocs.org/sdr/99ZZZX3655.md): Hose · cracking · Sep 8, 1999 · N9476X · Cessna 182R · Vacuum Distribution System
  > AIRCRAFT BEGAN TO LOSE VACUUM ON INSTRUMENT AIR SYSTEM. FOUND A POSSIBLE LINE CRACK ON THE OUTSIDE FROM AGE. AFTER REMOVING THAT LINE AND OTHER LINES ALSO CONNECTED TO THE INSTRUMENTS, FOUND THAT NOT ONLY THE OUTSIDE OF THE LINE WAS CRACKED, BUT THE INSIDE L
- [SDR 99ZZZX3593](https://openairdocs.org/sdr/99ZZZX3593.md): Support · cracked · Aug 30, 1999 · N182MT · Cessna 182R · Fuselage Miscellaneous Structure
  > BATTERY BOX SUPPORT ANGLES WERE FOUND CRACKED DURING ANNUAL INSPECTION. IF UNDETECTED, BATTERY CAN BECOME LOOSE IN TAIL. IT IS VERY COMMON IN THIS TYPE OF DESIGN, USING THESE ANGLES. SUBMITTER STATED SHOULD HAVE A STRONGER RE-DESIGN FOX.
- [SDR 99ZZZX2594](https://openairdocs.org/sdr/99ZZZX2594.md): Hose · deteriorated · Jun 21, 1999 · N6453H · Cessna 182R · Vacuum Distribution System
  > ALL VACUUM HOSES INSTALLED IN THIS AIRCRAFT HAVE HEAVY DETERIORATION BOTH INSIDE AND OUTSIDE OF THE HOSE. THE ONLY INDICATION OF A PROBLEM WAS A DROP IN THE VACUUM GAUGE PRESSURE WITH THE AIRCRAFT IN-FLIGHT. THIS AIRCRAFT HAS HAD TWO PREVIOUS VACUUM PUMPS INS
- [SDR 99ZZZX2037](https://openairdocs.org/sdr/99ZZZX2037.md): Impulse Coupling · corroded · Mar 29, 1999 · N6594E · Cessna 182R · Magneto/Distributor
  > IMPULSE COUPLING CORRODED ON MAGNETO.
- [SDR 99ZZZX1080](https://openairdocs.org/sdr/99ZZZX1080.md): Prop Governor · failed · Feb 26, 1999 · Cessna 182R · Propeller Controlling System
  > GOVERNOR WAS REMOVED DUE TO FAILURE TO CONTROL THE PROPELLER. WHEN IT WAS RECEIVED FOR OVERHAUL, DISASSEMBLED FOR INSPECTION, AND FOUND THE FLYWEIGHT ASSY COMPLETELY DESTROYED DUE TO CATASTROPHIC FAILURE. THERE WERE SHAVINGS OF METAL IN THE PUMP BODY. OWNER
- [SDR 99ZZZX651](https://openairdocs.org/sdr/99ZZZX651.md): Bolt · failed · Aug 24, 1998 · N5080Y · Cessna 182R · Reciprocating Engine Power Section
  > NR 2 MAIN JOURNAL THROUGH-BOLT WAS BROKEN AT TOP OF NR 2 CYLINDER. NO OTHER DEFECT NOTED. PILOT DID NOT STATE ABOUT ANYTHING TO CAUSE THIS, ALL OTHER ASSOCIATED ATTACH POINTS INSPECTED OK. ENGINE ONLY HAS 146.6 TSMOH AT FACTORY. PER SB 97-6, THROUGH-BOLTS
- [SDR 98ZZZX2180](https://openairdocs.org/sdr/98ZZZX2180.md): Support · failed · May 21, 1998 · N9921H · Cessna 182R · Battery Box Structure
  > BOTH BATTERY SUPPORT BRACKETS WERE FOUND BROKEN DURING AN ANNUAL INSPECTION. THESE SUPPORT BRACKETS ARE ONLY INSTALLED WITH THE MANIFOLD BATTERY INSTALLATION. ITEM 12 OF PART'S LIST.
- [SDR 98ZZZX999](https://openairdocs.org/sdr/98ZZZX999.md): Line · failed · Feb 3, 1998 · N2939E · Cessna 182R · Landing Gear Brake System
  > LEFT BRAKE FAILED ON TAKEOFF ROLL AND TAKEOFF ABORTED. FOUND SMALL HOLE WORN THROUGH ALUMINUM BRAKE LINE WHERE LINE CHAFED ON AFT SIDE OF ENTRY STEP CASTING. INSTALLED NEW 0700099-93 BRAKE LINE. SUGGEST REMOVING LANDING GEAR STRUT FAIRINGS FOR INSPECTION AT
- [SDR 98ZZZX803](https://openairdocs.org/sdr/98ZZZX803.md): Fuel Cap · mismarked · Jan 14, 1998 · N9815H · Cessna 182R · Fuel Storage
  > C/W CESSNA SI TO REMOVE FLUSH-TYPE LARGE OPENING FUEL CAPS AND INSTALLING ABOVE WING CAPS WITH SMALL FILL OPENINGS SUPPLIED IN KIT SK182-86C. INSPECTED FILL ADAPTER PLATES PRIOR TO INSTALLATION AND FOUND FUEL CAPS OPEN IN A REVERSE/NON-STANDARD DIRECTION. OR
- [SDR 98ZZZX1558](https://openairdocs.org/sdr/98ZZZX1558.md): Skin · cracked · Nov 25, 1997 · N9557X · Cessna 182R · Fuselage Main, Plate/Skin
  > THE (FUEL CHECK) STEPS ARE MOUNTED WITH AN3 BOLTS ATTACHED TO THE ACFT'S SKIN, P/N 0713334-3, AND P/N 0713334-4, LEFT AND RIGHT FORWARD SKINS. THE UPPER BACK BOLT WAS THROUGH THE SKIN AND THE BULKHEAD AT STA 1700. THE USE OF THE STEP CAUSED THE BOLT TO BREAK
- [SDR 98ZZZX1557](https://openairdocs.org/sdr/98ZZZX1557.md): Skin · cracked · Nov 25, 1997 · N9557X · Cessna 182R · Fuselage Main, Plate/Skin
  > THE (FUEL CHECK) STEPS ARE MOUNTED WITH AN3 BOLTS ATTACHED TO THE ACFT'S SKIN, P/N 0713334-3, AND P/N 0713334-4, LEFT AND RIGHT FORWARD SKINS. THE UPPER BACK BOLT WAS THROUGH THE SKIN AND THE BULKHEAD AT STA 1700. THE USE OF THE STEP CAUSED THE BOLT TO BREAK
- [SDR 97ZZZX3671](https://openairdocs.org/sdr/97ZZZX3671.md): Nut · broken · Jul 31, 1997 · N4804 · Cessna 182R · Reciprocating Engine Power Section
  > NUT WAS BROKEN THROUGH COMPLETELY. ALL TORQUE WAS RELEASED. THIS NUT WAS INSTALLED AT ENGINE OVERHAUL IAW CONT SB M92-9.
- [SDR 97ZZZX3327](https://openairdocs.org/sdr/97ZZZX3327.md): Bulkhead · failed · Jul 10, 1997 · N5535N · Cessna 182R · Propeller Spinner Section
  > SPINNER BULKHEAD CRACKED BEWEEN BOLT HOLES AND SEPARATED CAUSING SPINNER TO WOBBLE. ACTION OF SPINNER CAUSED DAMAGE TO BOTH PROPELLER BLADES AT THE ROOTS, AND DAMAGE TO PROPELLER HUB, SPINNER AND BULKHEAD. SUBMITTER STATED CLOSE INSPECTION OF SPINNER BULKHEA
- [SDR 97ZZZX464](https://openairdocs.org/sdr/97ZZZX464.md): Control Arm · misdrilled · Jan 6, 1997 · Cessna 182R · Exhaust Turbocharger
  > WASTEGATE CONTROL ARM (NEW PART) WAS MIS-DRILLED. SUBMITTER HAD TO ORDER 4 UNITS BEFORE RECEIVING A USEABLE PART.
- [SDR 97ZZZX6215](https://openairdocs.org/sdr/97ZZZX6215.md): Bulkhead · cracked · Nov 5, 1996 · Cessna 182R · Propeller Spinner Section
  > INSPECTION FOUND PROPELLER SPINNER BULKHEAD CRACKED.
- [SDR 97ZZZX6214](https://openairdocs.org/sdr/97ZZZX6214.md): Piston Rod · corroded · Nov 5, 1996 · Cessna 182R · Propeller Assembly
  > PROPELLER INSPECTION FOUND PISTON ROD CORRODED.
- [SDR 97ZZZX152](https://openairdocs.org/sdr/97ZZZX152.md): Dowel Pin · corroded · Nov 5, 1996 · Cessna 182R · Propeller Assembly
  > INSPECTION FOUND PROPELLER ASSY DOWEL PIN CORRODED.

Next page: https://openairdocs.org/model/cessna-182r/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 = '182R'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/cessna-182r/reports

---
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