# Service difficulty reports: Textron 208B

A list on [Textron 208B](https://openairdocs.org/model/textron-208b.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 34 · 1,667 reports

- [SDR 141A2026101200001](https://openairdocs.org/sdr/141A2026101200001.md): Warning Message · illuminated · Oct 11, 2026 · N750Z · Cessna 208B · Door Warning System
  > NORMAL PREFLIGHT DUTIES WERE ACCOMPLISHED AND THE DOORS WERE VERIFIED LATCHED INSIDE AND OUT, TAXIED OUT WITH NO INCIDENT. UPON TAKEOFF ROLL THE DOOR WARNING ANNUNCIATOR FLASHED MULTIPLE TIMES AND AN ABORT WAS CALLED. WE ADVISED ATC WE NEEDED A GATE RETURN AND
- [SDR 141A2026100600001](https://openairdocs.org/sdr/141A2026100600001.md): Shimmy Dampener · chattering · Oct 6, 2026 · N932SP · Cessna 208B · Landing Gear Steering System
  > DEPARTING OGG ON FLIGHT 512 WITH 9 PAX ONBOARD. ON ADDING POWER TO TAKE OFF OGG, FRONT END OF ACFT STARTED TO SHAKE VIOLENTLY. PROPELLER WAS AT 1900 RPM & TORQUE WAS APPROX 1700 LBS WITH INTENTION OF CONTINUING TO ADD POWER TO APPROX 2000 LBS FOR TAKE OFF.
- [SDR GAJA202610070223](https://openairdocs.org/sdr/GAJA202610070223.md): Engine · surges · Oct 1, 2026 · N984AC · Cessna 208B · Engine (Turbine/Turboprop)
  > DURING CRUISE AT 13,000FT, THE PILOT EXPERIENCED A TEMPORARY UNCOMMANDED POWER SURGE BUT THE AIRCRAFT SETTLED BACK INTO NORMAL CRUISE PERFORMANCE SETTING. WITHIN THE NEXT 2 MINUTES, THE UNCOMMANDED CONTROL COMMENCED AGAIN ONLY THIS TIME PROCEEDED TO REDLINE A
- [SDR UATA5120929265701](https://openairdocs.org/sdr/UATA5120929265701.md): Flap Track · cracked · Sep 21, 2026 · N707RA · Cessna 208B · Trailing Edge Flaps
  > FOUND CRACK IN OUTBOARD FLAP TRACK ON RH WING., TRACK WAS REMOVED AND REPLACED WITH NEW TRACK (PN: MC2622075-6, SN: J079924-020) AND BACK DRILLED TO PRE-EXISTING RIVET SIZES. TRACK WAS INSTALLED WITH MS20470AD RIVETS, AND HL18PB HI-LOKS OF VARYING LENGTHS. ALL
- [SDR 141A2026090600001](https://openairdocs.org/sdr/141A2026090600001.md): Power Lever · malfunctioned · Sep 6, 2026 · N839MA · Cessna 208B · Engine Controls
  > FLYING IFR, BUT SAW THE FIELD, GOT CLEARED FOR THE VISUAL APPROACH AT MIMLE. WHEN TURNING BASE TO FINAL AT AROUND 1100 FT FLYING AT 120 KNOTS, SUDDENLY THE NG STUCK. SAW THE POWER LEVER AT IDLE & NG WAS AT 88.2. COULDN’T SLOW DOWN. BUT CYCLED THE POWER LEVER,
- [SDR L87A2026083100266](https://openairdocs.org/sdr/L87A2026083100266.md): Elec Connector · contaminated · Aug 28, 2026 · N622TP · Cessna 208B · Fire Protection System Wiring
  > ENGINE FIRE WARNING IN FLIGHT, APPROX 5 MINS AFTER TAKEOFF EXPERIENCED AN ENGINE FIRE WARNING WHICH WAS DETERMINED TO BE AN INDICATION PROBLEM. DIVERSION TO TEB HAD ALREADY BEEN INITIATED WHERE A PRECAUTIONARY LANDING MADE. PILOT REPORTED AFTER APPROX 5 MINS,
- [SDR 2026FA0000673](https://openairdocs.org/sdr/2026FA0000673.md): Wheel Half · damaged · Aug 27, 2026 · N515PE · Cessna 208B · Wheel/Ski/Float
  > A POST MAINTENANCE RELEASE INSPECTION REVEALED A MISSING NUT AND SHEARED BOLT ON THE RIGHT MAIN WHEEL ASSEMBLY. REMOVAL AND DISASSEMBLY OF THE RIGHT WHEEL REVEALED FURTHER DAMAGE TO THE OUTER HALF OF THE WHEEL ASSEMBLY IN THE SHEARED BOLT LOCATION, IN THE FORM
- [SDR ENHA202608040197](https://openairdocs.org/sdr/ENHA202608040197.md): B-Nut · loose · Aug 25, 2026 · N502GV · Cessna 208B · Turbine Engine Oil System
  > SMOKE IN CABIN. MECHANICS FOUND LOOSE B-NUT AT LINE FROM THE AIR/ OIL SEPERATOR TO WET TORQUE INDICATING VENT (FWD FITTING), TIGHTENED FITTING, CLEANED ENGINE, PERFOMED LEAK CHECK @ FULL POWER AND CRUISE SETTINGS FOR 15 MIN.. NO LEAKS. ENGINE RUN PERFORMED IA
- [SDR 141A2026081500002](https://openairdocs.org/sdr/141A2026081500002.md): Wing · damaged · Aug 15, 2026 · N835MA · Cessna 208B · Wing Main, Frame Structure
  > LEFT WING SUFFERED MAJOR DAMAGE FROM WINDS. WILL REMOVE AND REPLACE WING
- [SDR 141A2026081500001](https://openairdocs.org/sdr/141A2026081500001.md): Tire · blown · Aug 15, 2026 · N881SA · Cessna 208B · Tire
  > WHILE LANDING IN JONESBORO, MADE A NORMAL TOUCHDOWN AT ABOUT 70 - 75 KNOTS WITH FULL FLAPS & STARTED TO PUT ACFT IN FULL REVERSE THRUST & STARTED GETTING ON BRAKES. TOUCHDOWN STRAIGHT & ON CENTER LINE. ACFT WAS NOT SIDE LOADED. RT SIDE, FELT WEIRD UPON TOUCHD
- [SDR COEA2026081703856](https://openairdocs.org/sdr/COEA2026081703856.md): Indicator · faulted · Aug 13, 2026 · N856FE · Cessna 208B · Attitude Gyro and Indicating System
  > FLIGHT 7675 ENROUTE LMT-PDX AIR TURNBACK/DISCREPANCY: STANDBY ATTITUDE INDICATOR UNRELIABLE DURING CLIMB. RETURNED TO LMT. LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY DECLARED. CORRECTIVE ACTION: REPLACED THE STANDBY ATTITUDE INDICATOR.
- [SDR 2026F00174](https://openairdocs.org/sdr/2026F00174.md): Indicator · overheated · Aug 13, 2026 · N12155 · Cessna 208B · Turn and Bank/Rate of Turn Indicator
  > AIRCRAFT WAS OPERATING A PART 135 FLIGHT FROM KABI TO KDFW. DURING CRUISE FLIGHT AT APPROX 7,000 FT MSL NEAR THE BOOVE WAYPOINT, THE PILOT DETECTED AN ODOR CONSISTENT WITH SOMETHING BURNING. PILOT CLOSED CABIN VENTS TO DETERMINE WHETHER THE ODOR ORIGINATED WIT
- [SDR 141A2026080400001](https://openairdocs.org/sdr/141A2026080400001.md): Circuit Breaker · tripped · Aug 4, 2026 · N1983X · Cessna 208B · Air Conditioning System
  > LEFT VENT BLOWER CIRCUIT BREAKER POPPED OUT. SMELL OF SMOKE IN COCKPIT. DID A GATE RETURN.
- [SDR 141A2026080300001](https://openairdocs.org/sdr/141A2026080300001.md): Generator · malfunctioned · Aug 2, 2026 · N932SP · Cessna 208B · DC Generator-Alternator
  > PHNY TO PHNL FLT 663, CREW NOTICED A STANDBY POWER INOP CASS MESSAGE ILLUMINATED. GETTING READY TO COMPLETE STANDBY POWER INOP CHKLIST, NOTICED THE STANDBY POWER INOP CASS MESSAGE DISAPPEARED & GENERATOR OFF CASS MESSAGE ILLUMINATED. CREW SAW A DISCHARGE WIT
- [SDR 141A2026073000001](https://openairdocs.org/sdr/141A2026073000001.md): Warning Message · illuminated · Jul 30, 2026 · N852MA · Cessna 208B · Fuel Boost Pump
  > DEPARTED ON FLIGHT 864 FROM HONOLULU TO MOLOKAI, SHORTLY AFTER ROTATION ON DEPARTURE, FUEL BOOST ON CAS MESSAGE BEGAN INTERMITTENTLY FLASHING ON PRIMARY FLIGHT DISPLAY (PFD). FUEL FLOW INDICATION ON MULTI-FUNCTION DISPLAY(MFD) APPEARED NORMAL, BUT CAS MESS
- [SDR 2026FA0000598](https://openairdocs.org/sdr/2026FA0000598.md): Tube · leaking · Jul 20, 2026 · N624MF · Cessna 208B · Aircraft Fuel Distribution System
  > DURING THE PILOT POST FLIGHT INSPECTION, A STRONG ODOR OF JET FUEL WAS PRESENT AFTER OPENING THE LEFT COWL. THE TOP OF THE AIR CONDITIONER CONDENSER HOUSING, LOCATED AT THE BOTTOM OF THE LEFT COWL, WAS WET ON THE TOP WITH FUEL. A LEAK WAS DISCOVERED DRIPPING F
- [SDR 55YR202607290001](https://openairdocs.org/sdr/55YR202607290001.md): Screw · mismanufactured · Jun 23, 2026 · Cessna 208B · Standard Practices/Structures
  > DURING AN INSPECTION ON A CESSNA CARAVAN 208B5228 THE AILERON AND ELEVATOR TRIM ACTUATOR LUBRICATION WAS DUE. THE ACTUATORS WERE DISASSEMBLED AND INSPECTED. FOUR EXTERNAL THREAD SCREWS IPC 27-30-02 FIGURE 4 ITEM 3 WERE MEASURED TO BE UNDER ALLOWABLE DIMENSIO
- [SDR 141A2026062200001](https://openairdocs.org/sdr/141A2026062200001.md): Display · faulted · Jun 22, 2026 · N957SP · Cessna 208B · Flight Management Computing Hardware System
  > A/C HAD PFD 1 MALFUNCTION DURING FLIGHT, ALONG WITH CHIP DETECT AND LOW FUEL TEMPERATURE CAS MESSAGE CAME ON. WE TOLD ATC WE ARE HAVING A MALFUNCTIONING SCREEN AND CHIP DETECT AND WE’D LIKE TO DECLARE AN EMERGENCY FOR IT. ONCE WE LANDED THE SCREEN HAD FIXED IT
- [SDR 141A2026060400001](https://openairdocs.org/sdr/141A2026060400001.md): Warning Message · illuminated · Jun 4, 2026 · N731LC · Cessna 208B · Central Warning
  > FIRST OFFICER WAS GETTING CLEARANCE. GOT INTO THE PLANE & REALIZED THAT THE VOLTAGE LOW CAS WAS ILLUMINATING. CHECKED THE VOLTS AND THE BATTERY WAS BELOW 24. SHUTDOWN THE AVIONICS AND TURNED THE BATTERY OFF FOR ABOUT 3/5 MINUTES. TURNED IT BACK ON AND THE CAS
- [SDR DEMA202605270001](https://openairdocs.org/sdr/DEMA202605270001.md): Fuel Control · uncontrollable · May 19, 2026 · N774FE · Cessna 208B · Fuel Control/Turbine Engines
  > LOSS OF ENGINE THROTTLE RESPONSE FOLLOWED BY AN UNCOMMANDED ENGINE SHUTDOWN ON THE TAXIWAY PRIOR TO TAKEOFF. THE AIRCRAFT FUEL SYSTEM WAS CHECK FOR CONTAMINATION WITH NO APPRECIABLE WATER OR DEBRIS FOUND IN WING TANKS OR RESERVOIR. FIREWALL FUEL FILTER ASSEM
- [SDR FXTA20260519001](https://openairdocs.org/sdr/FXTA20260519001.md): Transducer · false indication · May 19, 2026 · N248BA · Cessna 208B · Stall Warning System
  > STALL WARNING HORN GOES OFF INTERMITTENTLY AS HIGH AS 140 KTS
- [SDR 141A2026050800001](https://openairdocs.org/sdr/141A2026050800001.md): Unknown · smoke · May 8, 2026 · N823MA · Cessna 208B · Air Distribution System
  > WHILE ENROUTE TO LAX, SMELLED AND NOTICED SMOKE COMING FROM THE FRONT OF THE DASHBOARD, WE DID INHALE SMOKE. ANNOUNCED SMOKE IN THE COCKPIT. WE BEGAN RUNNING ELECTRICAL FIRE CHECKLIST BECAUSE DID NOT HAVE AN ENGINE FIRE CAS. HEARD A SOUND COMING FROM THE FRO
- [SDR 2026FA0000334](https://openairdocs.org/sdr/2026FA0000334.md): Bellows · faulted · May 4, 2026 · N347KA · Cessna 208B · Fuel Control/Turbine Engines
  > PILOT NOTICED AFTER DESCENT TO FLIGHT LEVEL 1500 FEET, LEVELING OFF AND ADDING POWER, TORQUE INDICATION DROPPED 200 AND RECOVERED ON ITS OWN WITH NO INPUT TO THE POWER LEVER. AFTER DISCUSSION WITH PRATT AND WHITTNEY, IT WAS DETERMINED THAT THE FUEL CONTROL DE
- [SDR 141A2026042300001](https://openairdocs.org/sdr/141A2026042300001.md): Indicator · failed · Apr 23, 2026 · N1983X · Cessna 208B · Attitude Gyro and Indicating System
  > ATTITUDE INDICATOR FAILURE PRIOR TO DEPARTURE AND PERFORMED GATE RETURN.
- [SDR MTNA2026040800001](https://openairdocs.org/sdr/MTNA2026040800001.md): Unknown · odor · Apr 8, 2026 · N831FE · Cessna 208B · Air Distribution System
  > NOXIOUS VAPOR IN CABIN. FLAP CIRCUIT BREAKER POPPED. THE PILOT NOTED AN UNKNOWN AIRBORNE IRRITANT IN THE COCKPIT WHICH RESULTED IN A BURNING SENSATION IN THE EYES, NOSE AND THROAT. THE PIC DECLARED AN EMERGENCY AND RETURNED TO EWR AND LANDED SAFELY. MX: 1) P
- [SDR 2026FA0000262](https://openairdocs.org/sdr/2026FA0000262.md): Attach Fitting · cracked · Apr 8, 2026 · N805TH · Cessna 208B · Fuselage Main, Attach Fittings
  > FOUND CRACK IN WEB OF WEB OF NOSE LANDING GEAR ATTACH FITTING LOCATED ON LOWER FIREWALL. REPLACED FITTING WITH NEW PART. THIS AIRCRAFT WAS INVOLVED IN A HARD LANDING CAUSING NOSE LANDING GEAR DAMAGE IN 2003 WHICH MAY HAVE CONTRIBUTED TO THIS FINDING.
- [SDR 141A2026032600001](https://openairdocs.org/sdr/141A2026032600001.md): Generator · faulted · Mar 26, 2026 · N852MA · Cessna 208B · DC Generating System
  > DURING CLIMB OUT OF HNL, GEN AMPS AND STBY POWER ON ANNUNCIATORS BOTH ILLUMINATED INTERMITTENTLY. GEN AND ALTERNATOR AMPS BOTH FLUCTUATED BETWEEN APPROXIMATELY 0-15 AMPS. WE REQUESTED TO RETURN TO HNL AND MADE A RECAUTIONARY LANDING. WHEN ASKED BY ATC IF WE R
- [SDR ENHA20260218002](https://openairdocs.org/sdr/ENHA20260218002.md): Trim System · locked · Feb 17, 2026 · N502GV · Cessna 208B · Elevator Tab Control System
  > DURING TAKEOFF THE ELEVATOR CONTROL WAS LOCKED IN A SLIGHT CLIMB POSITION. ALSO ON TAKEOFF, THE ELECTRIC ELEVATOR PITCH TRIM LOCKED IN A TAKEOFF POSITION AND WAS UNRESPONSIVE IN ELECTRIC OR MANUAL MODES UNTIL WELL AFTER LANDING. AIRCRAFT LANDED SAFELY AND IS
- [SDR MTNA2026021600001](https://openairdocs.org/sdr/MTNA2026021600001.md): Alternator · inoperative · Feb 12, 2026 · N985FX · Cessna 208B · AC Generator-Alternator
  > ALTERNATOR FAILURE AFTER START. STANDBY POWER ON CONTINUOUSLY. REMOVED AND REPLACED ATANDBY ALTERNATOR AND BELT.
- [SDR COEA2026021202946](https://openairdocs.org/sdr/COEA2026021202946.md): Bolt · broken · Feb 12, 2026 · N946FX · Cessna 208B · Wheel/Ski/Float
  > FLT 7692/PDX: LEFT BRAKE SEIZED UP ON TAXI OFF RUNWAY. MAINTENANCE DISCOVERED THE WHEEL HALF BOLT ON THE LT MAIN WHEEL BROKEN. REPLACED THE L/H MAIN WHEEL ASSY. AND L/H BRAKE ASSY. OPS CHECK GOOD.
- [SDR 141A2026013000001](https://openairdocs.org/sdr/141A2026013000001.md): Coordinator · faulted · Jan 30, 2026 · N803F · Cessna 208B · Navigation System
  > AFTER TAKING OFF FROM HRO TO FLY TO DFW MY SELF FO NOTICED THE PIC SIDE HEADING COORDINATOR WAS SWINGING ERRATICALLY AND THE RED HEADING FLAG WAS DISPLAYED. AFTER TALKING IT OVER WITH HIM WE MADE THE DECISION TO TURN AROUND TO GO BACK TO HRO SINCE WE WASN’T TO
- [SDR UATA5120205265301](https://openairdocs.org/sdr/UATA5120205265301.md): Attach Fitting · corroded · Jan 27, 2026 · N707RA · Cessna 208B · Fuselage Main, Attach Fittings
  > RIGHT FUSELAGE STRUT FITTINGS FAILED SID 53-20-07-250. LIFT STRUT FITTINGS. REMOVED FLOOR PANELS 2611127-18, 2611127-22 AND PULLY BRACKET 2612112-2 REMOVED FOR ACCESS. CAP ASSEMBLY 2611011-66 RIVETS REMOVED TO OUTBOARD SEAT RAIL FOR ACCESS. REMOVED LIFT STRUT
- [SDR 141A202601200001](https://openairdocs.org/sdr/141A202601200001.md): Comms Unit · faulted · Jan 20, 2026 · N852MA · Cessna 208B · Communications System
  > AIRCRAFT EXPERIENCED AN IN-FLIGHT COMMUNICATION MALFUNCTION. THE AIRCRAFT’S COMMUNICATION SYSTEM BECAME STUCK IN THE TRANSMITTING (TX) POSITION, PREVENTING THE CREW FROM RECEIVING ANY TRANSMISSIONS AND EFFECTIVELY BLOCKING THE ACTIVE FREQUENCY. TROUBLESHOOTING
- [SDR COEA2026011501956](https://openairdocs.org/sdr/COEA2026011501956.md): Trim Switch · faulted · Jan 14, 2026 · N956FE · Cessna 208B · Rudder Tab Control System
  > REPOSITION FLIGHT 201, PHX-SMF: AIR TURNBACK FULL RIGHT RUDDER TRIM AND ADDITIONAL RIGHT RUDDER REQUIRED TO MAINTAIN STRAIGHT FLIGHT. RETURNED AIRCRAFT TO PHX. NO EMERGENCY WAS DECLARED. CORRECTIVE ACTION: MAINTENANCE INSPECTED RUDDER TRIM RIGGING. FOUND TR
- [SDR 141A2026011200001](https://openairdocs.org/sdr/141A2026011200001.md): Transducer · failed · Jan 10, 2026 · N592SA · Cessna 208B · Engine Oil Pressure
  > THIS IS REPO FLIGHT FROM HNL TO OGG. ABOUT 5 MINUTE AFTER TAKEOFF FROM HNL, OIL PRESSURE INDICATION DROP DOWN YELLOW AND CONTINUE DOWN. I DECIDED TO TURN BACK TO HNL. DURING DECENT TO THE AIRPORT OIL PRESSURE COMPLETELY DOWN TO RED. ALL THE WAY OIL TEMP INDICA
- [SDR 141A202512140001](https://openairdocs.org/sdr/141A202512140001.md): Trim System · abnormal · Dec 14, 2025 · N208BK · Cessna 208B · Aileron Tab Control System
  > I TOOK FLIGHT CONTROLS TO TRY TRIMMING OUT THE AILERON TRIM MORE THOROUGHLY. HOWEVER, WHEN I ROLLED IT LEFT, IT PUSHED BACK AND WENT BACK TO THE RT. THIS TIME IT WAS FAR LEFT OF CENTER, AND HAD TO HOLD THE YOKE TO THE RT IN ORDER TO KEEP THE WINGS LEVEL. UPON
- [SDR COEA2025121206779](https://openairdocs.org/sdr/COEA2025121206779.md): Display · failed · Dec 12, 2025 · N779FE · Cessna 208B · Attitude and Direction Data System
  > FLIGHT 4701 ENROUTE: GEG-PSC DURING FLIGHT, THE PRIMARY FLIGHT DISPLAY (G600), LEFT SIDE, FAILED. THE AIRCRAFT LANDED WITHOUT INCIDENT AND NO EMERGENCY WAS DECLARED. MAINTENANCE REPLACED THE GDU 620 DISPLAY UNIT. OPS CHECK GOOD.
- [SDR ENHA20251101002](https://openairdocs.org/sdr/ENHA20251101002.md): Screw · loose · Nov 1, 2025 · N407GV · Cessna 208B · Electrical Power System Wiring
  > AFTER SECURING LOOSE SCREW ON BUS 2 STANDBY POWER CIRCUIT BREAKER (LOG PAGE 263019)AND SUCCESSFUL CHECK FLIGHT THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR ENHA20251103001](https://openairdocs.org/sdr/ENHA20251103001.md): Electrical Sys · malfunctioned · Nov 1, 2025 · N407GV · Cessna 208B · Electrical Power System
  > PILOT NOTE DISCREPANCY AS AN ELECTRICAL POWER LOSS/MULTIPLE BUS BREAKERS POP/PFD LOSS. MAINTENANCE INSPECTED ELECTRICAL SYSTEM AND COULD NOT DUPLICATE. AIRCRAFT IS SCHEDULED TO PERFORM AN OPERATIONAL CHECK FLIGHT FOR THE ELECTRICAL SYSTEM.
- [SDR MTNA20251030001](https://openairdocs.org/sdr/MTNA20251030001.md): Oxygen Bottle · leaking · Oct 29, 2025 · N869FE · Cessna 208B · Crew Oxygen System
  > O2 LEAK FOUND AT REGULATOR. MX: INSPECTED, FOUND LEVER INTERCONNECT ROD BENT 90 DEGREES. 2609090-5 ROD. REPLACED OXYGEN CYLINDER AND REGULATOR. RIGGED OXYGEN ON/OFF CONTROL SYSTEM. SERVICED OXYGEN BOTTLE. CHECKED FOR LEAKS. NO LEAKS NOTED. REMOVED P/N: 176412-
- [SDR FXGA202511120001](https://openairdocs.org/sdr/FXGA202511120001.md): Structure · damaged · Oct 22, 2025 · N208CE · Cessna 208B · Fuselage Main, Structure
  > AIRCRAFT HAD A STATIONARY TAIL STRIKE DAMAGING THE LOWER TAIL CONE AREA AND TAIL TIE DOWN FITTING. AIRCRAFT WAS PARKED ON A SLOPE AND WHEN THE PILOTS EXITED THE AIRCRAFT THE PLANE TILTED BACK AND THE TAIL STRUCK THE GROUND. CAUSED DAMAGE TO LOWER AFT TAIL CONE
- [SDR 141A2025100800237](https://openairdocs.org/sdr/141A2025100800237.md): Brake · overtemp · Oct 3, 2025 · N808MA · Cessna 208B · Landing Gear Brake System
  > PIC CONTACTED ACP SABRINI FOR BRIEFING & CLARIFICATION ABOUT PROCEDURE BEFORE BEGINNING. WHILE ON THE RAMP, PIC PERFORMED LOW-SPEED BRAKE TESTS AT 5–10 KNOTS GS TO VERIFY FUNCTIONALITY. BRAKES WERE ONLY SLOWING DOWN THE ACFT, BUT IT WASN’T FIRM BRAKING AS THE
- [SDR COEA2025091605856](https://openairdocs.org/sdr/COEA2025091605856.md): Oxygen Bottle · leaking · Sep 10, 2025 · N856FE · Cessna 208B · Crew Oxygen System
  > AN EMERGENCY DESCENT WAS PERFORMED DUE TO OXYGEN DEPLETION AT FL210. AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED IN HDN WITHOUT FURTHER ISSUES. O2 BOTTLE REPLACEMENT IAW C208 MM 35-01-00.
- [SDR 2025FA0000626](https://openairdocs.org/sdr/2025FA0000626.md): Tire · blown · Sep 2, 2025 · N881SA · Cessna 208B · Tire
  > AFTER LANDING INTO KBFD, AIRCRAFT STARTED DRIFTING LEFT, PILOT LOOKED OUT AND NOTICED THAT THE LEFT MAIN TIRE HAD BLOWN. PILOT CONTACTED TOWER TO PLEASE CLOSE THE RUNWAY UNTIL THEY COULD GET THE AIRCRAFT OFF SAFELY.
- [SDR 2025F00205](https://openairdocs.org/sdr/2025F00205.md): Tire · failed · Sep 1, 2025 · N881SA · Cessna 208B · Tire
  > UPON LANDING IN BFD THE LH MAIN TIRE BLEW
- [SDR 2025F00206](https://openairdocs.org/sdr/2025F00206.md): Propeller · damaged · Aug 31, 2025 · N847MA · Cessna 208B · Propeller System
  > BIRD FLEW UNDER PROP AFTERWARDS CREW HEARD TO PROP MAKING CONTACT TO BIRD. CONFIRMED BIRD STRIKE BY AIRPORT RAMP. MX ACCOMPLISHED A BIRD STRIKE INSPECTION.
- [SDR 2025FA0000571](https://openairdocs.org/sdr/2025FA0000571.md): Tire · blown · Aug 25, 2025 · N732LC · Cessna 208B · Tire
  > UPON LANDING IN LNY LEFT MAIN TIRE BLEW
- [SDR 2025FA0000617](https://openairdocs.org/sdr/2025FA0000617.md): Battery · failed · Aug 24, 2025 · N732LC · Cessna 208B · Battery/Charger System
  > A/C DEPARTED HNL ABOUT 1/2 WAY THRU FLIGHT CREW NOTICED ACRID BURNING ODOR. CREW FIGURED IT WAS A/C BELT SO CONTINUED ON WITHOUT RUNNING THE A/C, SMELL CAME BACK SO CREW TURNED OFF OVERHEAD AIR VENTS. TURNED BACK ON THE AIR VENTS AND SMELL CAME BACK SO CREW DI
- [SDR 2025FA0000616](https://openairdocs.org/sdr/2025FA0000616.md): Brake Assy · failed · Aug 24, 2025 · N592SA · Cessna 208B · Landing Gear Brake System
  > WHILE TAXING OUT, RH BRAKE FAILURE. A/C HAD TO BE TOWED OFF TAXIWAY, UPON SPINNING AIRCRAFT WITH TUG PROP STRUCK A GROUND TAXI LIGHT
- [SDR 2025FA0000572](https://openairdocs.org/sdr/2025FA0000572.md): Brake Assy · failed · Aug 24, 2025 · N592SA · Cessna 208B · Landing Gear Brake System
  > RIGHT BRAKE FAILURE ON TAXI OUT TO RUNWAY, CAUSING AIRCRAFT TO TURN LEFT. PROP STRUCK TAXI WAY LIGHT. AIRCRAFT HAD TO BE TOWED OFF TAXI WAY.

Next page: https://openairdocs.org/model/textron-208b/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 = '208B'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/textron-208b/reports

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