# Service difficulty reports: Beech C90

A list on [Beech C90](https://openairdocs.org/model/beech-c90.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 6 · 278 reports

- [SDR 2026F00118](https://openairdocs.org/sdr/2026F00118.md): Compressor · faulted · Jun 3, 2026 · N284PM · Beech C90 · Turbine Engine Compressor Section
  > LOSS OF TORQUE AND RPM TO THE PROP, CURRENTLY UNSURE IF PGB CAUSED ENGINE FAILURE OR IF THE ENGINE FAILED. AFTER SPINNING THE COMPRESSOR BY HAND IT WAS NOTED THAT THERE WAS DRAG AND A RASPY SOUND COMING FROM THE COMPRESSOR. ENGINE WILL GO OUT FOR SHOP VISIT
- [SDR G1IA20251106099](https://openairdocs.org/sdr/G1IA20251106099.md): Downlock Switch · faulted · Nov 6, 2025 · N400EM · Beech C90 · Landing Gear Position and Warning
  > DESCRIPTION OF SERVICE DIFFICULTY: RETURNING TO OUR BASE (ABQ), WE WERE ON A VISUAL APPROACH TO RUNWAY 3 IN CLEAR & CALM CONDITIONS. LANDING GEAR WAS SELECTED DOWN AND L GEAR INDICATOR FAILED TO ILLUMINATE AND PUMP CONTINUED TO RUN. I INFORMED MY CREW AND LET
- [SDR 454A250906075836](https://openairdocs.org/sdr/454A250906075836.md): Heater · dirty · Sep 6, 2025 · N500EQ · Beech C90 · Heating System
  > CREW OBSERVED SMOKE IN CABIN WITH HEATER ON CLIMB-OUT. THE PIC DECIDED TO ABORT THE FLIGHT AND RETURN TO STARTING POINT. UPON INVESTIGATION, IT WAS DISCOVERED THAT THIS WAS THE FIRST TIME THAT HEATER HAS BEEN TURNED ON SINCE THE SPRING MONTHS. LINT AND DUST WI
- [SDR G1IA202505302591](https://openairdocs.org/sdr/G1IA202505302591.md): Safety Switch · unserviceable · May 25, 2025 · N147LJ · Beech C90 · Landing Gear Position and Warning
  > AFTER TAKING OFF OUT OF KRQE, THA LANDING GEAR DID NOT RETRACT AFTER BRINGING THE LANDING GEAR HANDLE UP. I STILL HAD 3 GREENS. AFTER SPEAKING WITH OUR PILOT MANAGER ON CALL (PMOC) AND MAINTENANCE MANAGER ON CALL (MMOC) BY SAT PHONE I DECLARED AN EMERGENCY. PR
- [SDR 2025FA0000368](https://openairdocs.org/sdr/2025FA0000368.md): Clamp · loose · May 20, 2025 · N28KP · Beech C90 · Landing Gear Position and Warning
  > MAIN LANDING GEAR DOWNLOCK SWITCH WIRE HARNESS CLAMP THAT ATTACHES TO DOWNLOCK HOOK WAS INSTALLED ON OUTSIDE OF HOOK/DOWNLOCK OVER CENTER ASSEMBLY. DISASSMBLED DOWNLOCK OVER CENTER HOOKS AND REROUTED HARNESSES AND CLAMPS TO THE CENTER OF EACH ASSEMBLY, REASSEM
- [SDR G1IA202505110090](https://openairdocs.org/sdr/G1IA202505110090.md): Motor · inoperative · May 11, 2025 · N299RP · Beech C90 · Cabin Cooling System
  > AIR CONDITIONING STOPPED WORKING EN ROUTE TO HNL. REPLACED MOTOR WITH NEW MOTOR.
- [SDR G1IA202503240088](https://openairdocs.org/sdr/G1IA202503240088.md): Autopilot Sys · malfunctioned · Mar 24, 2025 · N400EM · Beech C90 · Autopilot System
  > DISCREPANCY: ON CLIMB OUT AP DISCONNECTED ON IT'S OWN WITH AFCS FAIL AND AP FAIL MESSAGES. FOR THE REMAINING 25 MINUTES OF THE FLIGHT THE FAIL MESSAGES EXTINGUISHED AND CAME BACK ~ 15 TIMES. NO CIRCUIT BREAKERS WERE PULLED. PERFORMED PRE-FLIGHT TEST (PFT)
- [SDR YQSA20250205001](https://openairdocs.org/sdr/YQSA20250205001.md): Warning Message · activated · Feb 4, 2025 · N590SH · Beech C90 · Engine Temperature Indicating System
  > CRUISING AT FL230 WHEN ITT ON RIGHT SPIKED TO 900-1000 DEGREES C. TORQUE FELL SHORTLY AFTER DROPPING TO "0". RPM WAS 200RPM FROM PROP WINDMILLING. IDENTIFIED RIGHT ENGINE AS FAILED AND SECURED ENGINE PER THE MEMORY ITEMS FROM THE CHECKLIST. ANNOUNCED EMERGENC
- [SDR G1IA202501310083](https://openairdocs.org/sdr/G1IA202501310083.md): Wire · damaged · Jan 31, 2025 · N60VP · Beech C90 · Landing Gear System Wiring
  > LANDING GEAR WOULD NOT EXTEND, LANDING GEAR C/B TRIPPED PUMPED GEAR DOWN AND RETURNED TO HNL, ( ACTION TAKEN) PUMPED HANDLE BEFORE LANDING TO INSURE GEAR WAS DOWN
- [SDR 454A202501303217](https://openairdocs.org/sdr/454A202501303217.md): Vent · blocked · Jan 29, 2025 · N500EQ · Beech C90 · Air Distribution System
  > SMOKE IN THE CABIN AFTER 5 MINUTES OF FLIGHT, SIGNIFICANT SMELL. THE SMOKE DID DIMINISH AFTER HEAT WAS TURNED OFF AND AC TURNED ON. CORRECTIVE ACTION: INSPECTED AND CLEANED AREA AROUND HEATER VENTS. PERFORMED GROUND RUNS WITH NO DEFECTS NOTED. UNABLE TO DUPLIC
- [SDR 1LXA2025012800062](https://openairdocs.org/sdr/1LXA2025012800062.md): Unknown · smoke · Dec 30, 2024 · N711BN · Beech C90 · Air Distribution System
  > SMOKE IN CABIN
- [SDR MDGA202501060002](https://openairdocs.org/sdr/MDGA202501060002.md): Brake Caliper · leaking · Dec 13, 2024 · Beech C90 · Landing Gear Brake System
  > PILOT REPORTED LEFT BRAKE LOSS ON TAXI IN TO RAMP. BRAKE CALIPER DEVELOPED A SEVERE LEAK AND WAS REPLACED.
- [SDR G1IA20231207053](https://openairdocs.org/sdr/G1IA20231207053.md): Unknown · unknown · Dec 7, 2023 · N98KS · Beech C90 · Engine (Turbine/Turboprop)
  > DURING OUR TRAINING FLIGHT WE NOTICED THE R OIL PRESSURE ANNUNCIATOR FLICKERING. THE RIGHT OIL PRESSURE GAUGE CONFIRMED LOW OIL PRESSURE WITH A READING HOVERING AROUND 40 PSI. EVERY OTHER ENGINE INSTRUMENT WERE IN NORMAL PARAMETERS. PER THE CHECKLIST, WE PER
- [SDR G1IA202312107053](https://openairdocs.org/sdr/G1IA202312107053.md): Unknown · unknown · Dec 7, 2023 · N98KS · Beech C90 · Engine (Turbine/Turboprop)
  > DURING OUR TRAINING FLIGHT WE NOTICED THE R OIL PRESSURE ANNUNCIATOR FLICKERING. THE RIGHT OIL PRESSURE GAUGE CONFIRMED LOW OIL PRESSURE WITH A READING HOVERING AROUND 40 PSI. EVERY OTHER ENGINE INSTRUMENT WERE IN NORMAL PARAMETERS. PER THE CHECKLIST, WE PER
- [SDR 2023F00340](https://openairdocs.org/sdr/2023F00340.md): Motor · arced · Nov 29, 2023 · N149CF · Beech C90 · Air Conditioning System
  > DURING A SCHEDULED INSPECTION THE ELECTRICAL CONNECTION ON AIR CONDITIONING COMPRESSOR DRIVE MOTOR WAS FOUND TO BE LOOSE AND SHOWED SIGNS OF ARCING.
- [SDR 2023FA0000396](https://openairdocs.org/sdr/2023FA0000396.md): Unknown · unknown · Aug 1, 2023 · N387AS · Beech C90 · Brake
  > RH BRAKE FAIL ON TOUCHDOWN. PILOT SIDE RH PEDAL WOULD PRESS TO FLOOR. CO PILOT RH SIDE SPONGY. BLED BRAKE SYSTEM. OPERATIONAL GROUND CHECKS SATISFACTORY.
- [SDR GCSA202307030001](https://openairdocs.org/sdr/GCSA202307030001.md): Windshield · shorted · Jun 29, 2023 · N117MF · Beech C90 · Flight Compartment Windows
  > IN FLIGHT FIRE REPORTED AT LOWER PILOT WINDSHIELD/ INSTRUMENT PANNEL AREA. REPORTING REQUIRED PURSUANT FAR 135.415 (A)(2) & (5). AIRCRAFT LANDED WITHOUT INCIDENT AT CRESCENT CITY,CA (CEC). POST INCIDENT INVESTIGATION REVEALED LEFT HAND WINDSHIELD HEAT TERMINAL
- [SDR G1IA2023051109046](https://openairdocs.org/sdr/G1IA2023051109046.md): Display · intermittent · May 9, 2023 · N902TS · Beech C90 · Flight Management Computing Hardware System
  > EADI FLASHED OFF AND ON IN FLIGHT
- [SDR G1IA20230318037](https://openairdocs.org/sdr/G1IA20230318037.md): Actuator · inoperative · Mar 18, 2023 · N1079D · Beech C90 · Landing Gear System
  > DISCREPANCY: THE RED GEAR HANDLE UNSAFE LIGHTS REMAINED ILLUMINATED AND THE RIGHT MAIN GEAR SAFE LIGHT REMAINED DARK WITH THE GEAR HANDLE IN THE DOWN POSITION. THE J HOOK WAS ALSO NOT VISIBLE. CYCLED THE LANDING GEAR ONE TIME AND THE SAME CONDITION CONTINUED U
- [SDR MDGALJ1356021223](https://openairdocs.org/sdr/MDGALJ1356021223.md): Downlock Switch · false indication · Feb 12, 2023 · N8287E · Beech C90 · Landing Gear Position and Warning
  > ON APPROACH TO LAND THE LEFT MAIN LANDING GEAR DOWNLOCK INDICATION FAILED TO ILLUMINATE. DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT.
- [SDR 2022FA0000491](https://openairdocs.org/sdr/2022FA0000491.md): Frame · bent · Sep 1, 2022 · N149CF · Beech C90 · Fuselage Main, Frame
  > TAIL STAND WAS NOT REMOVED PRIOR TO AIRCRAFT BEING LOWER OFF OF JACKS, SUBSEQUENTLY DAMAGING FUSELAGE FRAME LOCATED AT AIRFRAME STATION 319.0.
- [SDR QMLA2022082620057](https://openairdocs.org/sdr/QMLA2022082620057.md): Relay · failed · Aug 24, 2022 · N771PA · Beech C90 · Trailing Edge Flap Control System
  > ON APPROACH TO KGCK WHEN IT WAS TIME TO PUT FLAPS TO APPROACH SETTING THE FLAPS DID NOT COME DOWN OR INDICATE IN THE DOWN POSITION. DECIDED TO RETURN TO KAAO AND PERFORMED A NO FLAP LANDING. REPLACED FLAP MOTOR RELAY.
- [SDR MDGALJ14485242022](https://openairdocs.org/sdr/MDGALJ14485242022.md): Brake Caliper · leaking · May 24, 2022 · N1068K · Beech C90 · Landing Gear Brake System
  > ON ARRIVAL AT THE RAMP THE PILOT RIGHT BRAKE PEDAL WENT TO THE FLOOR AND WAS INEFFECTIVE. AIRCRAFT STOPPED USING LEFT BRAKE. BRAKE CALIPER WAS REMOVED AND SEALS REPLACED AND AIRCRAFT RETURNED TO SERVICE.
- [SDR 2022FA0000078](https://openairdocs.org/sdr/2022FA0000078.md): Blower Motor · overheated · Feb 4, 2022 · N431BG · Beech C90 · Cabin Cooling System
  > ON CLIMB OUT IT APPEARS THAT THE VENT BLOWER MOTOR BELOW THE PILOT'S FEET SEIZED UP AND THEN THE MOTOR ITSELF STARTED TO SMOKE. THE BREAKER FOR THE MOTOR TRIPPED AT THIS TIME.
- [SDR G1IA20211001021](https://openairdocs.org/sdr/G1IA20211001021.md): None · none · Oct 1, 2021 · N35HD · Beech C90 · Heating System
  > SHORTLY AFTER DEPARTURE FROM KAPA EN ROUTE TO KRCV AT FL200 MEDICAL CREW ALERTED PILOT TO SMOKE IN THE CABIN. MEDICAL CREW ALSO ADVISED THE RIGHT SIDE CABIN AIR OUTLET AND WALL NEAR THE RIGHT REAR FACING SEAT WAS ABNORMALLY HOT. CREW DONNED OXYGEN MASKS IAW TH
- [SDR G1IA20210513009](https://openairdocs.org/sdr/G1IA20210513009.md): Switch · shorted · May 17, 2021 · N948AM · Beech C90 · Landing Gear System Wiring
  > WHILE ON APPROACH INTO WAIMEA, I HAD THE AC CONFIGURED WITH APPROACH FLAPS AND GEAR. I THEN DECIDED TO PUT FULL FLAPS BECAUSE I WAS HIGH AND NEEDED TO LOSE ALTITUDE. SO WHEN I ADDED FULL FLAPS, THE GEAR WARNING HORN AND LIGHT CAME ON. I DECIDED TO RECYCLE THE
- [SDR G1IA20210507006](https://openairdocs.org/sdr/G1IA20210507006.md): Engine · surges · May 7, 2021 · N785JP · Beech C90 · Engine (Turbine/Turboprop)
  > 7-10 MILES FROM KFLG THE LEFT ENGINE BEGAN TO SURGE 50-100 FT/LBS ON THE TORQUE. NO OTHER FLUCTUATIONS ON THE LEFT ENGINE GAUGES WERE OBSERVED. THIS FLUCTUATION WAS FIRST NOTICES AUDIBLY. THIS OCCURRED UPON REDUCING THE THROTTLES TO 400 FT/LBS. AT APPROXIM
- [SDR YEWA20200910002](https://openairdocs.org/sdr/YEWA20200910002.md): Exhaust Duct · torn · Aug 31, 2020 · N813JB · Beech C90 · Engine Collector/Tailpipe/Nozzle
  > PILOT REPORTED HEARING A POP UPON ADVANCING PROP LEVERS ON MID-FINAL APPROACH INTO KAAO. PILOT NOTICED NR 1 ENGINE TORQUE INDICATION EXTREMELY LOW, LANDING WAS COMPLETED PER NORMAL PROCEDURES WITHOUT INCIDENT. VISUAL INSPECTION OF THE NR 1 ENGINE FOUND THE P
- [SDR YEWA20200806001](https://openairdocs.org/sdr/YEWA20200806001.md): Bracket · chafed · Mar 25, 2020 · N771PA · Beech C90 · Trailing Edge Flap Control System
  > MULTIPLE FLAP ROLLER BRACKETS INSIDE FLAPS CHAFED BY FLAP ROLLERS REQUIRING REPLACEMENT. (L/H OTBD FLAP, OTBD TRACK, INBD BRACKET P/N 35-165050-35)(L/H OTBD FLAP, INBD TRACK, INBD AND OTBD BRACKETS P/N 35-165050-31, P/N 35-165050-30)(L/H INBD FLAP, INBD TRACK,
- [SDR YEWA20200806003](https://openairdocs.org/sdr/YEWA20200806003.md): Bracket · chafed · Feb 19, 2020 · N813JB · Beech C90 · Trailing Edge Flap Control System
  > MULTIPLE FLAP ROLLER BRACKETS INSIDE FLAPS CHAFED BY FLAP ROLLERS REQUIRING REPLACEMENT. (R/H INBD FLAP,INBD TRACK, OTBD BRACKET P/N 50-160003-5)(L/H OTBD FLAP, OTBD TRACK, INBD AND OTBD BRACKETS P/N 35-165050-30 P/N 35-165050-35)
- [SDR 2020FA0000042](https://openairdocs.org/sdr/2020FA0000042.md): Wheel Half · cracked · Jun 20, 2019 · N100KB · Beech C90 · Wheel/Ski/Float
  > CRACK-LIKE INDICATION WAS LOCATED STARTING IN BEAD ARE GOING ACROSS FACE FOR 1-1/2 INCH LONG. LIQUID PENETRANT INSPECTION WAS THE METHOD SPECIFIED AND USED FOR THE NOT EXAMINATION.
- [SDR 2020FA0000089](https://openairdocs.org/sdr/2020FA0000089.md): Plate · damaged · Feb 14, 2019 · N46CV · Beech C90 · Main Landing Gear
  > UPPER FORWARD HOLE FOR THE UPPER ANCHOR BOLT FOR THE FORWARD BRAKE CALIPER BROKE OUT JAMMING THE FORWARD CALIPER ON THE BRAKE DISK ROTATING WITH THE TIRE AND BREAKING THE AFTER CALIPER OFF THE TORQUE PLATE FROM THE LH MAIN GEAR. INCIDENT WAS DURING TAXI, WHEN
- [SDR 2020FA0000110](https://openairdocs.org/sdr/2020FA0000110.md): Torque Knee · cracked · Aug 8, 2018 · N46CV · Beech C90 · Main Landing Gear
  > A CRACK LIKE INDICATION WAS INDICATED ON THE MLG TORQUE KNEE ATTACHMENT HOLE. THE CRACK INDICATION IS ON THE LEFT ALUMINUM MLG TORQUE KNEE. LOCATED ON THE INSIDE OF THE ATTACHMENT HOLE. CAN BE VISUALLY CONFIRM INDICATION. CRACK WAS FOUND WITH FLORESCENT LI
- [SDR 2020FA0000022](https://openairdocs.org/sdr/2020FA0000022.md): Torque Knee · cracked · Aug 8, 2018 · N46CV · Beech C90 · Landing Gear Retraction/Extension System
  > A CRACK LIKE INDICATION WAS INDICATED ON THE MAIN LANDING GEAR TORQUE KNEE ATTACHMENT HOLE. THE CRACK INDICATION IS ON THE LEFT ALUMINUM MAIN LANDING GEAR TORQUE KNEE. LOCATED ON THE INSIDE OF THE ATTACHMENT HOLE. CAN BE VISUALLY CONFIRM INDICATION. CRACK
- [SDR YBB2018F00000](https://openairdocs.org/sdr/YBB2018F00000.md): Window · cracked · Jan 15, 2018 · N790A · Beech C90 · Passenger Compartment Windows
  > PILOT REPORTED THAT DURING FLIGHT, HEARD A NOISE FROM AFT OF THE ACFT. NOTICE AFT PAX NR 1 LT CABIN WINDOW CRACKED, DIVERTED NEAREST AIRPORT. UPON LANDING FOUND NR 1 LT PAX WINDOW CRACKED. SUSPECTED THAT FATIGUE, STRESS CRAZE WERE CONTRIBUTING FACTORS IN
- [SDR HJ2R2018071600225](https://openairdocs.org/sdr/HJ2R2018071600225.md): Wheel · cracked · Oct 5, 2017 · N431BG · Beech C90 · Wheel/Ski/Float
  > CRACK LIKE INDICATION LOCATED ON THE BEAD AREA OF WHEEL ON BOTH HALVES. CRACK INDICATION WERE FOUND BY THE EDDY CURRENT EXAMINATION METHOD.
- [SDR 2017FA0000274](https://openairdocs.org/sdr/2017FA0000274.md): Bumper Block · detached · Jun 2, 2017 · Beech C90 · Main Landing Gear
  > A PROPERTY OWNER REPORTED THAT AN AIRCRAFT PART HAD FALLEN THROUGH HIS BARN ROOF. THE PART WAS CONSTRUCTED OF ALUMINUM AND MARKED WITH THE PART NUMBER 50-980091-2. THE IPC SHOWED IT AS A RT MAIN LANDING GEAR BLOCK-BUMPER.
- [SDR EBTR20170523015](https://openairdocs.org/sdr/EBTR20170523015.md): Engine · shutdown · May 20, 2017 · N4447W · Beech C90 · Engine (Turbine/Turboprop)
  > ON DESCENT FROM UGN TO ARB HEARD POP, AIRCRAFT YAWED, NOTICED RIGHT ENGINE FUEL FLOW AND ITT DIMINISHING TO 0. VISUAL OF ENGINE COWL NO DEFECTS NOTED. FOLLOWED FLIGHT MANUAL PROCEDURES FOR ENGINE RESTART USING ISOLATION SWITCH NO FUEL FLOW OR ITT REGISTERED AN
- [SDR 2017FA0000232](https://openairdocs.org/sdr/2017FA0000232.md): Fitting · cracked · Apr 20, 2017 · N249CP · Beech C90 · Wing, Attach Fittings
  > DURING A SCHEDULED WING STRUCTURE INSPECTION, A CRACK WAS DISCOVERED BY EDDY CURRENT INSPECTION IN THE LEFT LOWER FORWARD INBOARD WING BOLT ATTACH FITTING. REPLACED THE FITTING. MAJOR REPAIR.
- [SDR U9FR20170124001](https://openairdocs.org/sdr/U9FR20170124001.md): Light · arced · Jan 20, 2017 · N519A · Beech C90 · Passenger Compartment Lighting
  > DURING TAXI THE ODOR OF BURNED WIRING WAS NOTED BY A CREW MEMBER. DURING FURTHER INVESTIGATION, A WHISP OF SMOKE WAS NOTED IN THE CABIN AREA. TAXI OPERATION WAS ABORTED AT THIS TIME. AIRCRAFT WAS BROUGHT TO MAINTENANCE WHERE IT WAS DISCOVERED THAT THE "+" TERM
- [SDR EBTR201610150001](https://openairdocs.org/sdr/EBTR201610150001.md): Pump · inoperative · Oct 12, 2016 · N4447W · Beech C90 · Fuel Boost Pump
  > ENROUTE FROM APN TO MKG, DURING CRUISE AT 8,000 FT APPROXIMATELY 20 MINUTES FROM MKG, FUEL SYSTEM AUTOMATICALLY SWITCHED TO CROSSFEED TO SUPPLY FUEL TO RT ENGINE, INDICATING THAT THE RT ENGINE HAD A FUEL PRESSURE DROP. THIS IS NORMAL SEQUENCE OF EVENTS FOR AI
- [SDR 2016F00197](https://openairdocs.org/sdr/2016F00197.md): Engine · flamed out · Oct 1, 2016 · N20WP · Beech C90 · Engine (Turbine/Turboprop)
  > PILOT REPORTED RT ENGINE FLAMEOUT AFTER LEVELING OFF FOR CRUISE AT 11,000 FT. FAILED RESTART. SUCCESSFUL LANDING.
- [SDR CTY2016F00001](https://openairdocs.org/sdr/CTY2016F00001.md): Engine · overheated · Aug 22, 2016 · N46CV · Beech C90 · Engine (Turbine/Turboprop)
  > ENGINE OVERHEATED AT 6000 FT ON CLIMBOUT. FEATHERED PROP AND RETURNED TO DEPARTURE. WILL BE DOING A TEARDOWN REPORT. WE ARE SENDING THE FUEL CONTROL UNIT OUT FOR TESTING. UNTIL THAT TIME, WE ARE NOT DRAWING ANY CONCLUSIONS.
- [SDR 2016FA0000199](https://openairdocs.org/sdr/2016FA0000199.md): Wire Harness · mismanufactured · Apr 30, 2016 · N402EM · Beech C90 · Flight Control System Wiring
  > FLIGHT CREW REPORTED THAT THE PITCH TRIM SYSTEM OPERATED IN REVERSE DURING AUTOPILOT USE. TROUBLESHOOTING REVEALED THAT PINS C & D WERE SWAPPED ON THE HARNESS CONNECTING THE ELECTRONIC PITCH TRIM AMP AND THE TRIM SERVO.
- [SDR CTYA2016040100000](https://openairdocs.org/sdr/CTYA2016040100000.md): Engine · power loss · Apr 1, 2016 · N46CV · Beech C90 · Engine (Turbine/Turboprop)
  > PILOT REPORTED ENGINE RUNNING HOTTER THAN NORMAL, LACK OF POWER.
- [SDR 2015FA0000512](https://openairdocs.org/sdr/2015FA0000512.md): Wire · sparks · Oct 28, 2015 · N24GJ · Beech C90 · Light System Wiring
  > AFTER DEPARTURE, CREW REPORTED SEEING SPARKS FROM THE FUEL CONTROL PANEL ON THE PILOTS SIDEWALL. CREW RETURNED TO DEPARTURE AIRPORT AND AN UNEVENTFUL LANDING WAS MADE. EXPOSED AREA OF FIRE ON THE BACKLIGHTING PANEL WAS SHORTING TO THE PANEL AND EMITTING SPAR
- [SDR CA151019010](https://openairdocs.org/sdr/CA151019010.md): Stator · unserviceable · Oct 16, 2015 · Beech C90 · Turbine Engine Compressor Section
  > (CAN) THE SUBJECT ENGINE WAS RECEIVED FOR O/H. UPON REVIEW, 1 VANE AIRFOIL FROM THE 3RD STAGE COMPRESSOR STATOR WAS FOUND LIBERATED. SECONDARY DAMAGE WAS CAUSED TO MULTIPLE OTHER 3RD STAGE COMPRESSOR VANES AS WELL AS DAMAGE TO MULTIPLE IMPELLER VANES. NO FO
- [SDR 3PSR20150918004](https://openairdocs.org/sdr/3PSR20150918004.md): Spring · cracked · Sep 18, 2015 · Beech C90 · Propeller Assembly
  > DURING THE NDT INSPECTION, REQUIRED DURING THE O/H OF THE PROPELLER, A CRACK WAS FOUND ON THE FEATHERING SPRING,
- [SDR 2015F00101](https://openairdocs.org/sdr/2015F00101.md): Fire Detector · defective · Aug 27, 2015 · N16 · Beech C90 · Fire Detection
  > RIGHT SIDE FIRE LIGHT ILLUMINATED, SHUTDOWN ENGINE, DISCHARGED FIRE EXTINGUISHER AND COMPLETED SAFE LANDING. EMERGENCY FIRE & RESCUE DEPLOYED.
- [SDR CA160120006](https://openairdocs.org/sdr/CA160120006.md): Engine · power loss · Aug 1, 2015 · Beech C90 · Engine (Turbine/Turboprop)
  > (CAN) THE ACFT IMPACTED AIRPORT TERRAIN DURING AN EMERGENCY LANDING ATTEMPT. THE AIRPLANE SUSTAINED SUBSTANTIAL DAMAGE AND 3 OF THE 4 INJURED OCCUPANTS ONBOARD RECEIVED SERIOUS INJURIES, 1 RECEIVED MINOR INJURIES. CONTACT WITH THE NTSB HAS BEEN ESTABLISHED A

Next page: https://openairdocs.org/model/beech-c90/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 = 'C90'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/beech-c90/reports

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