# Service difficulty reports: Cessna P206B A list on [Cessna P206B](https://openairdocs.org/model/cessna-p206b.md). Newest first. General aviation reporting is voluntary. - [SDR CA140226001](https://openairdocs.org/sdr/CA140226001.md): Axle · corroded · Feb 19, 2014 · Cessna P206B · Main Landing Gear Strut/Axle/Truck > (CAN) DURING CPCP INSPECTION, WHILE ACCOMPLISHING SID 32-13-01, CORROSION WAS FOUND IN INNER BORE OF AXLE. AXLE WAS REPLACED. - [SDR CA140212006](https://openairdocs.org/sdr/CA140212006.md): Bracket · cracked · Feb 6, 2014 · Cessna P206B · Ailerons > (CAN) DURING CPCP INSPECTION OF ACFT. SUPPLEMENTAL INSPECTION NR 57-51-01, AILERON SUPPORT STRUCTURE INSPECTION. RT WING INBD AILERON BRACKET ASSY WAS FOUND TO HAVE MULTIPLE CRACKS IN BEND RADIUS WHERE IT ATTACHES TO REAR SPAR. PART WAS REPLACED WITH NEW ASS - [SDR 2008FA0000364](https://openairdocs.org/sdr/2008FA0000364.md): Trim Switch · inoperative · May 9, 2008 · N4711F · Cessna P206B · Elevator Tab Control System > PILOT REPORTED IN FLIGHT WHEN AUTOPILOT/ELECTRIC TRIM ENABLE, TRIM SERVO "RAN ON", WHEN ELECTRIC TRIM TURNED OFF MANUAL TRIM WHEEL OPERABLE AND NO MALFUNCTION OF SYSTEM NOTED, UPON INSPECTION NOTICED SOLDERED CONNECTION ON BASE OF SWITCH BENT AND JUMPED BETWEE - [SDR AU990732](https://openairdocs.org/sdr/AU990732.md): Bulkhead · cracked · Jul 12, 1999 · Cessna P206B · Fuselage Main, Bulkhead > (AUS) FUSELAGE AFT BULKHEAD LOCATED AT STN 209.0 CRACKED IN THE UPPER RT CORNER ADJACENT TO THE RT HORIZONTAL STABILIZER ATTACHMENT FITTING. - [SDR AU990731](https://openairdocs.org/sdr/AU990731.md): Frame · cracked · Jul 12, 1999 · Cessna P206B · Fuselage Main, Frame > (AUS) LEFT DOORPOST FRAME CRACKED. FUSELAGE SKIN RIVETS LOOSE IN AREA ADJACENT TO THE WING STRUT. - [SDR 99ZZZX96](https://openairdocs.org/sdr/99ZZZX96.md): Support · cracked · Sep 21, 1998 · N4790F · Cessna P206B · DC Generator-Alternator > DURING AN ENGINE CHANGE, THE ALTERNATOR SUPPORT BRACKET WAS FOUND CRACKED. THE CRACK WAS ABOUT 1.25 INCHES LONG AND SEEMS TO HAVE STARTED AT THE MANUFACTURER'S WELD. CESSNA SIL SE 79-5 CALLS FOR REPLACEMENT OF THIS PART WITH AN INTEGRAL ENGINE MOUNT LEG/ALTE - [SDR CA980623021](https://openairdocs.org/sdr/CA980623021.md): Cylinder · separated · Jun 15, 1998 · Cessna P206B · Reciprocating Engine Cylinder Section > (CAN) NR 5 CYLINDER WAS FOUND TO HAVE A CYLINDER SEPARATION. - [SDR CA970909007](https://openairdocs.org/sdr/CA970909007.md): Collar · broken · Aug 18, 1997 · Cessna P206B · Main Landing Gear Strut/Axle/Truck > (CAN) THE AIRCRAFT IS USED FOR TRANSPORTING SKY DIVERS AND IS SUBJECT TO LONG TAKEOFF RUNS AND CROSSWINDS. THIS CONDITION SUBJECTS THE LANDING GEAR STRUT TO HIGH STRESS LOADS WHICH CONTRIBUTED TO THE STRUT COLLAR FAILURE. - [SDR AU970418](https://openairdocs.org/sdr/AU970418.md): Crankshaft · failed · Apr 10, 1997 · Cessna P206B · Reciprocating Engine Power Section > (AUS) ENGINE CRANKSHAFT FAILED FROM CRACKING AT THE REAR FILLET RADIUS OF NO2 MAIN BEARING JOURNAL DUE TO FRICTION FROM CONTACT WITH THE BEARING SHELLS - [SDR EY2R9601557](https://openairdocs.org/sdr/EY2R9601557.md): Blade · stripped · Jun 1, 1996 · Cessna P206B · Propeller Blade Section > BLADE SN EJ247YS, THREADS CHIPPED - [SDR EY2R9601556](https://openairdocs.org/sdr/EY2R9601556.md): Blade · damaged · Jun 1, 1996 · Cessna P206B · Propeller Blade Section > BLADE SN EJ299YS, THREADS CHIPPED. - [SDR CA960620009](https://openairdocs.org/sdr/CA960620009.md): Gasket · leaking · May 31, 1996 · Cessna P206B · Engine Fuel Pump > (CAN) SLIGHT LEAK AT FUEL PUMP BODY GASKET REPLACED - [SDR EY2R9600279](https://openairdocs.org/sdr/EY2R9600279.md): Cylinder · corroded · Jan 1, 1996 · Cessna P206B · Propeller Assembly > PROP ASSY CYLINDER IS CORRODED - [SDR 95ZZZX6028](https://openairdocs.org/sdr/95ZZZX6028.md): Door · departed · Aug 3, 1995 · N4794F · Cessna P206B · Passenger/Crew Doors > RT CABIN DOOR WAS HEAVILY MODIFIED FOR SKY DIVING APPLICATIONS. FORWARD LATCH PIN WAS WORN AND ALLOWED DOOR TO UNLATCH IN-FLIGHT. DUE TO THE HIGH SPEEDS INVOLVED, THE DOOR BROKE IN HALF AND DEPARTED THE AIRCRAFT. - [SDR 96ZZZX2148](https://openairdocs.org/sdr/96ZZZX2148.md): Channel · rivets sheared · May 2, 1995 · N4778F · Cessna P206B · Engine Mount Section > DURING ROUTINE PROPELLER REMOVAL FOR OVERHAUL, DETERMINED 6 AN470 4-4 RIVETS COMPLETELY SHEARED OFF AND MISSING FROM RIGHT FRONT ENGINE SUPPORT AND CHANNEL ASSY, PN 1213433-14, AND SUPPORT, PN 1213433-17. FURTHER INSPECTION REVEALED NO OTHER DAMAGE OR SHEARED - [SDR 96ZZZX2147](https://openairdocs.org/sdr/96ZZZX2147.md): Support · rivets sheared · May 2, 1995 · N4778F · Cessna P206B · Engine Mount Section > DURING ROUTINE PROPELLER REMOVAL FOR OVERHAUL, DETERMINED 6 AN470 4-4 RIVETS COMPLETELY SHEARED OFF AND MISSING FROM RIGHT FRONT ENGINE SUPPORT AND CHANNEL ASSY, PN 1213433-14, AND SUPPORT, PN 1213433-17. FURTHER INSPECTION REVEALED NO OTHER DAMAGE OR SHEARED ## 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 = 'P206B' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/cessna-p206b/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.