# Service difficulty reports: Raytheon 390

A list on [Raytheon 390](https://openairdocs.org/model/raytheon-390.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 141 reports

- [SDR HBKA202605260587](https://openairdocs.org/sdr/HBKA202605260587.md): Fire Detector · false activation · May 22, 2026 · N189K · Raythn 390 · Fire Detection
  > WHILE CRUISING AT 38,000 FEET IN AND OUT OF CLOUDS NO PRECIPITATION OR TURBULENCE. RIGHT ENGINE FIRE INDICATION PUSH BUTTON ILLUMINATED AND "FIRE" ANNUNCIATOR IN THE N1 INDICATION CAME ON. THE FLIGHT CREW PERFORMED MEMORY ITEMS OF: THROTTLE TO IDLE AND WAIT FO
- [SDR HBKA202604160001](https://openairdocs.org/sdr/HBKA202604160001.md): Compressor · failed insp · Apr 11, 2026 · N189K · Raythn 390 · Turbine Engine Compressor Section
  > SHORTLY AFTER TAKE OFF, CREW WITNESSED THE LT ENGINE INDICATIONS STARTING TO ROLL BACK. THIS INDICATION HAPPENED BETWEEN 500 & 1000 FOR AGL. FELT THE DECELERATION OF THE ACFT. THE FLIGHT CREW REPORTED THERE WERE NO CAUTION OR WARNING LIGHTS PRESENT DURING THI
- [SDR 2025F00145](https://openairdocs.org/sdr/2025F00145.md): Warning Light · multiple fail · Jun 20, 2025 · N145J · Raythn 390 · Aircraft Fuel System
  > THROUGHOUT THE FLIGHT, OBSERVED THAT THE FUEL KEPT MOVING AROUND WITHOUT US MOVING THE FUEL TRANSFER SWITCH. WE WOULD EVENTUALLY TRY TO EVEN BOTH FUEL GAUGES OUT BUT THEY NEVER SEEMED TO BALANCE. THEY WOULD BALANCE FOR A SECOND, SO WE'D TURN THE FUEL SWITCH OF
- [SDR 2025FA0000006](https://openairdocs.org/sdr/2025FA0000006.md): Landing Gear · malfunctioned · Jan 3, 2025 · N415HD · Raythn 390 · Landing Gear Position and Warning
  > AFTER TAKEOFF WHEN RETRACTING THE LANDING GEAR THE GEAR UNSAFE LIGHT DID NOT EXTINGUISH AND THERE WAS A DISTINCT SOUND OF RUSHING AIR UNDER THE AIRCRAFT. MAIN LANDING GEAR DOORS DID NOT RETRACT.
- [SDR ZKFA202408190193](https://openairdocs.org/sdr/ZKFA202408190193.md): Pitot Line · contaminated · Aug 15, 2024 · N46CK · Raythn 390 · Pitot/Static System
  > WHILE AT FL40 NOTED YELLOW IAS LIGHT ON BOTH PFD'S. DURING DESCENT NOTED A 60 KT SPLIT (BETWEEN PILOT AND COPILOT PFD). SWITCHED TO ADC2 AND A/S WERE NORMAL. PITCH TRIM ALSO WOULD NOT RESET, FLEW AIRCRAFT IN SBY TRIM. TECHNICIANS AT NASHVILLE, TN, KBNA WERE DI
- [SDR 2024FA0000412](https://openairdocs.org/sdr/2024FA0000412.md): Rod End · broken · May 30, 2024 · N720MH · Raythn 390 · Landing Gear Doors
  > PREMIER 1A N720MH (S/N: RB-176) JUST AFTER TAKEOFF FROM SAN ANTONIO (KSAT) THE PILOT RETRACTED THE GEAR AND HEARD AN UNUSUAL NOISE. THEY INFORMED ACT THEY HEARD A NOISE AND NEEDED TO RETURN TO THE AIRPORT. THEY RETURNED BACK TO SAN ANTONIO SAFELY. AFTER THEY L
- [SDR 2024F00023](https://openairdocs.org/sdr/2024F00023.md): Shimmy Dampener · failed · Jan 4, 2024 · N390DP · Raythn 390 · Wheel/Ski/Float
  > ON TAKEOFF FROM LAS VEGAS, NV (KLAS) AT ABOUT 50 KNOTS, THE AIRCRAFT BEGAN TO VIBRATE. ACCOMPANIED BY A RATTLING NOISE. TAKEOFF WAS ABORTED AND TOWER WAS NOTIFIED. MAINTENANCE WAS CONTACTED CREW WAS DISPATCHED TO TROUBLESHOOT AND REPAIR. INITIALLY THE SHIMMY D
- [SDR 2023F00102](https://openairdocs.org/sdr/2023F00102.md): Control Valve · failed · Mar 14, 2023 · N390DP · Raythn 390 · Cabin Temperature Control System
  > ON TAKEOFF FROM SCOTTSDALE, AZ (KSDL) A LOUD RUSH OF HOT BLEED AIR ENTERED THE COCKPIT. THE TEMPERATURE INCREASED IN A MATTER OF SECONDS. AS A PRECAUTION THE TAKEOFF WAS ABORTED. MAINTENANCE TROUBLESHOT THE SYSTEM AND DETERMINED THAT THE LEFT BI-LEVEL CONTROL
- [SDR 2023F00073](https://openairdocs.org/sdr/2023F00073.md): Firewall · cracked · Mar 3, 2023 · N972PF · Raythn 390 · Nacelle/Pylon Structure
  > WHILE CHANGING #1 ENGINE MOUNTS A CRACK WAS FOUND IN THE PYLON FIREWALL.
- [SDR 2023FA0000062](https://openairdocs.org/sdr/2023FA0000062.md): Firewall · cracked · Jan 18, 2023 · N330AC · Raythn 390 · Nacelle/Pylon Miscellaneous Structure
  > LEFT ENGINE FIREWALL FOUND CRACKED DURING ENGINE CHANGE.
- [SDR 2022F00523](https://openairdocs.org/sdr/2022F00523.md): Actuator · leaking · Dec 15, 2022 · N145JS · Raythn 390 · Landing Gear Actuator
  > AFTER TAKEOFF THE NOSE GEAR RETRACTED BUT THE MAIN GEAR DID NOT RETRACT. SELECTED GEAR DOWN AND GOT 3 GREEN GEAR DOWN INDICATIONS. RETURNED TO POINT OF DEPARTURE, SCOTTSDALE, AZ (KSDL). MAINTENANCE TROUBLESHOT THE PROBLEM TO A LEFT/HAND MAIN LANDING GEAR ACTUA
- [SDR 2022FA0000036](https://openairdocs.org/sdr/2022FA0000036.md): Engine · cracked · Oct 30, 2021 · N330AC · Raythn 390 · Powerplant System
  > ON OCT 30,2021, #1 ENGINE HAD AN UN COMMANDED ENGINE SHUT DOWN. THE PILOTS LANDED AT THE SCHEDULED AIRPORT (KBKL) UNEVENTFUL. MAINTENANCE CONTACTED TEXTRON WHO CAME TO KBKL AND INVESTIGATED THE ISSUE. THEY DISCOVERED THE LP SWITCH TRIPPED. AFTER FURTHER INVEST
- [SDR SVGA20210806002](https://openairdocs.org/sdr/SVGA20210806002.md): Link · cracked · Sep 20, 2021 · N19KM · Raythn 390 · Service Doors
  > DURING A SCHEDULED INSPECTION THE RH FLAP LINK ASSEMBLY CONNECTING THE INBOARD FLAP TO THE FUSELAGE FAIRING WAS DISCONNECTED AND CRACKED. SEE THE ATTACHED PICTURE. NO DAMAGE TO THE FAIRING WAS FOUND.
- [SDR SVGA20210806001](https://openairdocs.org/sdr/SVGA20210806001.md): Connector · corroded · Aug 3, 2021 · N19KM · Raythn 390 · Fire Protection System Wiring
  > THIS IS THE 2ND EVENT OF A FALSE FIRE WARNING MESSAGE, 9.5 HOURS & 16 CYCLES SINCE PRIOR EVENT. DURING CRUISE FLIGHT AT 41,000 FT. RH ENGINE FIRE WARNING. CREW DIVERTED TO KBUR AND LANDED. ENGINE WAS SHUTDOWN PRIOR TO LANDING AND THE SINGLE FIRE EXTINGUISHE
- [SDR 2021F00101](https://openairdocs.org/sdr/2021F00101.md): Seal · leaking · Jul 31, 2021 · N19KM · Raythn 390 · Engine Bleed Air System
  > RIGHT FIRE LIGHT ON MFD AND RIGHT FIRE PUSH ANNUNCIATOR ILLUMINATED IN FLIGHT AND DID NOT EXTINGUISH. THE DESCENT 100 MILES OUT FROM APA WAS WITH RIGHT ENGINE AT IDLE, WHICH HAD NO EFFECT. ALL ENGINE INDICATORS SUCH AS OIL READINGS REMAINED NORMAL, SHOWING A
- [SDR QZJA20210308004](https://openairdocs.org/sdr/QZJA20210308004.md): Valve · stuck · Mar 8, 2021 · N1SH · Raythn 390 · Engine Bleed Air System
  > UPON DEPARTURE, THE CREW NOTICED THE FOLLOWING MECHANICAL IRREGULARITY: “UNSCHEDULED BLEED AIR AS AIRCRAFT ROTATED OFF RUNWAY. PRESSURIZATION CONTROLLER INDICATED -1,400 FPM. ATTEMPTED TO STOP HOT AIR BY TURNING OFF PRESSURIZATION AND BLEED AIR. DID NOT SOLVE
- [SDR 2021FA0000039](https://openairdocs.org/sdr/2021FA0000039.md): Lead · arced · Jan 26, 2021 · N46JM · Raythn 390 · Fuselage Main, Bulkhead Fuselage wiring
  > DURING MAINTENANCE, THE COMPRESSOR MOTOR LEADS CAME INTO CONTACT WITH THE FUSELAGE, BELOW THE RH AFT AVIONICS BAY, WITH AIRCRAFT POWER ON CAUSING THE LEADS TO ARC ON THE FUSELAGE DAMAGING THE FUSELAGE INSIDE OF THE AVIONICS BAY. THE DAMAGE WAS FIXED IAW TEXTRO
- [SDR WI5R2020111900001](https://openairdocs.org/sdr/WI5R2020111900001.md): Rotor · damaged · Nov 19, 2020 · Raythn 390 · Turbine Engine Compressor Section
  > DURING DISASSEMBLY OF ENGINE SERIAL NUMBER 105163 FOR AN UNRELATED ISSUE, A LIBERATED 1ST-STAGE INTERMEDIATE PRESSURE COMPRESSOR (IPC) ROTOR BLADE WAS DISCOVERED. NO OPERATIONAL ISSUES RELATED TO THE IPC ROTOR BLADE ANOMALY WERE REPORTED BY THE FLIGHT-CREW.
- [SDR QZJA20201119002](https://openairdocs.org/sdr/QZJA20201119002.md): Bleed Valve · intermittent · Nov 17, 2020 · N1SH · Raythn 390 · Compressor Bleed Valve
  > ON NOVEMBER 17, 2020 THE PILOT REPORTED: ABORTED THE TAKEOFF AT KABQ AT APPROXIMATELY 1712Z IN N1SH DUE TO A LOUD RUSHING OF AIR NOISE IN THE COCKPIT, FOLLOWED BY A LOT OF HOT AIR ENTERING THE COCKPIT. THIS HAPPENED AS THE THROTTLES WERE BROUGHT TO THEIR T/O
- [SDR WI5R2020091190001](https://openairdocs.org/sdr/WI5R2020091190001.md): Turbine · damaged · Sep 9, 2020 · Raythn 390 · Turbine Section
  > FLIGHT CREW REPORTED THAT DURING TAKEOFF, AT APPROXIMATELY 3000 FT AGL, LT ENGINE EXHIBITED AN UNUSUAL NOISE ACCOMPANIED BY AN INCREASE IN INDICATED INTER-TURBINE TEMPERATURE (ITT) AND FOLLOWED BY UNCOMMANDED IN-FLIGHT SHUTDOWN OF THE ENGINE. AIRCRAFT LANDED
- [SDR SVGA20200527001](https://openairdocs.org/sdr/SVGA20200527001.md): Tire · blown · May 22, 2020 · N33PJ · Raythn 390 · Tire
  > WE TOOK OFF FROM 30C AT KIWA TO KSTS, WHERE OUR RT MAIN LANDING GEAR TIRE BLEW AFTER PASSING V1 AND CROSSED FROM THE CONCRETE PORTION OF THE RUNWAY TO THE ASPHALT. OUR TAKEOFF WEIGHT WAS 12,500LBS, THE WEATHER WAS VFR AND WE HAD FOUR PASSENGERS ON BOARD. ON
- [SDR WI5R20191218002](https://openairdocs.org/sdr/WI5R20191218002.md): Rotor · fractured · Dec 17, 2019 · Raythn 390 · Turbine Engine Compressor Section
  > DURING A PRE-BUY BORESCOPE INSPECTION A MISSING IP BLADE AND HPC DAMAGE WAS NOTED. DISASSEMBLY OF THE ENGINE CONFIRMED THAT ONE OF THE 3RD STAGE IPC ROTOR BLADES WAS MISSING.
- [SDR WI5R2019090400001](https://openairdocs.org/sdr/WI5R2019090400001.md): Blade · fractured · Sep 4, 2019 · N952SP · Raythn 390 · Turbine Section
  > ENGINE RETURNED TO REPAIR STATION AFTER FIELD REPORT OF "AFTER TAKE OFF ROLL, LOUD GRINDING NOISE FROM ENGINE AND ENGINE SHUTDOWN. ENGINE N1 WILL NOT ROTATE BY HAND." DISASSEMBLY IN THE REPAIR STATION FOUND SEVERAL COMPONENTS DAMAGED AND AN INVESTIGATION CONT
- [SDR ODAR20190405001](https://openairdocs.org/sdr/ODAR20190405001.md): Bellows · ruptured · Apr 5, 2019 · N668Z · Raythn 390 · Pneumatic Distribution System
  > RETURN FLIGHT KCHO TO KFCI, PILOT ENCOUNTERED RIGHT ENGINE FIRE ANNUNCIATION. SHUT RIGHT ENGINE DOWN AND DEPLOYED FIRE EXTINGUISHER PER AIRCRAFT ENGINE FIRE EMERGENCY CHECKLIST. PILOT DECLARED INFLIGHT EMERGENCY AND LANDED WITHOUT INCIDENT AT KFCI. MAINTENA
- [SDR E81R2018041825105](https://openairdocs.org/sdr/E81R2018041825105.md): Clamp · broken · Apr 2, 2018 · N18RF · Raythn 390 · Engine Bleed Air System
  > PILOT NOTED THE RT ENGINE ITT INCREASING TO RED LINE. NOTED THE RT ENGINE FUEL FLOW INDICATION GOING TO DASHES ACROSS DISPLAY. NO ENGINE FIRE INDICATION NOTED. PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN. MAINTENANCE PERSONNEL NOTED DIFFICULTY IN OPENING THE
- [SDR 5RJR12167](https://openairdocs.org/sdr/5RJR12167.md): Pressure Switch · shorted · Dec 8, 2017 · N972PF · Raythn 390 · Engine Oil Indicating System
  > LEFT ENGINE LOW OIL PRESSURE LIGHT WOULD INTERMITTENTLY ILLUMINATE BUT OIL PRESSURE INDICATION INDICATED IN THE GREEN. FOUND PRESSURE SWITCH P/N 680S53 "A" WIRE INSIDE PRESSURE SWITCH CHAFED AND GROUNDING ON SWITCH CASE. REPLACED PRESSURE SWITCH. OPERATIONAL
- [SDR 5RJR2018012212155](https://openairdocs.org/sdr/5RJR2018012212155.md): Actuator · leaking · Nov 10, 2017 · N777JF · Raythn 390 · Drag Control Actuator
  > AIRCRAFT HAD NO LIFT DUMP OR SPOILER ACTUATION. FOUND LEFT BLOW DOWN ACTUATOR END SEAL BLOWN OUT.
- [SDR 2016FA0000386](https://openairdocs.org/sdr/2016FA0000386.md): Adapter · cracked · Aug 2, 2016 · N99BC · Raythn 390 · Aircraft Fuel Distribution System
  > THE AIRCRAFT ARRIVED FOR UNRELATED MAINTENANCE WHEN IT WAS NOTED THAT A LARGE AMOUNT OF FUEL WAS EMANATING FROM THE BELLY AREA BETWEEN THE WHEEL WELLS. ACCESS WAS GAINED TO THE AREA BETWEEN THE WHEEL WELLS CONTAINING THE MAIN FUEL SHUTOFF VALVES. WITH BOOST
- [SDR F2PA2016041100104](https://openairdocs.org/sdr/F2PA2016041100104.md): Door · binding · Apr 11, 2016 · N1XH · Raythn 390 · Landing Gear Door Retract Section
  > UPON EXTENDING THE LANDING GEAR FOR LANDING, ONCE THE MAIN GEARS WERE DOWN AND LOCKED INDICATING GREEN/SAFE, THE INBD GEAR DOORS FAILED TO SEQUENCE TO THE CLOSED POSITION. THE INBD GEAR DOORS SUBSEQUENTLY STAYED OPEN DURING THE LANDING AND TAXI IN, SCRAPPING
- [SDR F2PA20160411001](https://openairdocs.org/sdr/F2PA20160411001.md): Door · open · Apr 10, 2016 · N1XH · Raythn 390 · Landing Gear Door Retract Section
  > UPON EXTENDING THE GEAR FOR LANDING, AFTER THE MAIN GEAR WERE DOWN & LOCKED, THE INBD MAIN GEAR DOORS FAILED TO STOW AND REMAINED OPEN DURING THE LANDING & TAXI, SCRAPING THE PAVEMENT & CAUSING DAMAGE TO THE LE CORNERS OF THE MAIN INBD GEAR DOORS. CAUSE OF TH
- [SDR YCOA20160113001](https://openairdocs.org/sdr/YCOA20160113001.md): Circuit Breaker · faulty · Jan 10, 2016 · N401PP · Raythn 390 · Cabin Temperature Control System
  > APPROXIMATELY 1300 LOCAL TIME, DEPARTED ON A POSITIONING FLIGHT FROM KPDK. CLIMBING THROUGH ~1000 FT AGL, CREW NOTED "R BLEED OVHT" ANNUNCIATION INDICATING A DUCT OVER HEAT CONDITION. CREW PERFORMED THE APPROPRIATE CHECKLIST WITH NO IMMEDIATE CHANGE IN CONDI
- [SDR 9JLA201512108841](https://openairdocs.org/sdr/9JLA201512108841.md): Modulating Valve · defective · Dec 7, 2015 · N42EL · Raythn 390 · Cabin Temperature Control System
  > THE FLIGHT CREW HAD SEVERAL REPORTS OF AN INTERMITTENT ISSUE CONTROLLING THE COCKPIT TEMPERATURE. THEY DESCRIBED THIS ISSUE, SAYING THE COCKPIT TEMP WOULD GET EXTREMELY HOT. THERE WERE ATTEMPTS TO CORRECT THE PROBLEM AFTER EACH REPORT WITH TECH SUPPORT ASSIS
- [SDR 9JLA201512098832](https://openairdocs.org/sdr/9JLA201512098832.md): Support Bracket · broken · Oct 22, 2015 · N42EL · Raythn 390 · Passenger/Crew Doors
  > THE CREW INDICATED THAT WHEN A PAX WAS EXITING THE ACFT, THE MAIN CABIN DOOR SNUBBER LOWER ATTACHMENT BRACKET BROKE. THIS BRACKET IS NOT MADE VERY STRONG TO BEGIN WITH, IT IS ONLY A MATTER OF TIME BEFORE IT CRACKS UNDER NORMAL CONDITIONS. THE CABIN DOOR BRAC
- [SDR 9JLA201512098828](https://openairdocs.org/sdr/9JLA201512098828.md): Wire · pinched · Sep 11, 2015 · N42EL · Raythn 390 · Navigation System Wiring
  > THE CREW HAD REPORTED SEVERAL TIMES REGARDING AN INTERMITTENT OR COMPLETE FAILURE OF THE NR 1 AHRS SYS. AFTER EACH REPORT MX TROUBLE SHOT BUT COULD NOT VERIFY THE ACTUAL CAUSE OF THE FAULT OR FAILURE OF THE SYS. AFTER A FEW MORE REPORTS FAILURES OF THE NR 1
- [SDR CA150908019](https://openairdocs.org/sdr/CA150908019.md): Valve · malfunctioned · Sep 4, 2015 · Raythn 390 · Air Distribution System
  > (CAN) ON CLIMBOUT, THE PILOT NOTICED AN UNUSUAL NOISE COMING FROM THE REAR OF THE ACFT. RECOGNIZING THE NOISE WAS COMING FROM THE RT ENGINE AND HEAT WAS COMING INTO THE ACFT FROM THE CABIN AIR-CONDITIONING SYS HE QUICKLY CONCLUDED THE PROBLEM WAS ORIGINATING
- [SDR CA150629010](https://openairdocs.org/sdr/CA150629010.md): Compressor · corroded · Jun 26, 2015 · Raythn 390 · Turbine Engine Compressor Section
  > (CAN) ON RT ENG START, N1 DID NOT TURN, PILOT SHUTDOWN THE ENG. HE WENT TO TURN THE FAN BY HAND & HE FIGURED THAT N1 FAN WAS STUCK IN PLACE. AFTER INSPECTION BY MX DEPT, N1 FAN IS STUCK IN CORROSION. ENG NEEDS TO BE REPAIRED. LT ENG INSPECTION DONE & FOUND
- [SDR CA150415001](https://openairdocs.org/sdr/CA150415001.md): Actuator · malfunctioned · Mar 23, 2015 · Raythn 390 · Trailing Edge Flap Actuator
  > (CAN) "FLAP FAIL" ANNUNCIATOR ILLUMINATES IN FLIGHT SYSTEM CHECKS SERVICEABLE ON THE GROUND FLIGHT CONDITIONS: AFTER TAKEOFF AND ACFT AT CRUISE ALTITUDE AND SPEED WITH NO FLAP MOVEMENTS AND ABOUT 30 MINS INTO THE FLIGHT, FAULT RE-APPEARS, BUT ONCE THE ACFT LA
- [SDR E81R2015012324345](https://openairdocs.org/sdr/E81R2015012324345.md): Connector · burned · Jan 23, 2015 · N23HD · Raythn 390 · Electrical Power System Wiring
  > OPERATOR REPORTED EXTERNAL POWER CONNECTOR AT FBO WAS FITTING LOOSE AND REQUESTED FURTHER INSPECTION. UPON VISUAL INSPECTION NOTED GROUND CABLE WIRING HARNESS W103 CONNECTIONS AT THE 24J2 EXTERNAL POWER CONNECTOR, MS3506-1, NEGATIVE STUD WAS LOOSE AND THE NEGA
- [SDR CA141124004](https://openairdocs.org/sdr/CA141124004.md): Valve · defective · Nov 16, 2014 · Raythn 390 · Pneumatic Distribution System
  > (CAN) RT BLEED OVERHEAT LIGHT ON DURING TAKEOFF.
- [SDR 2014FA0000555](https://openairdocs.org/sdr/2014FA0000555.md): Wheel · failed · Sep 25, 2014 · N801BP · Raythn 390 · Wheel/Ski/Float
  > THE BEAD ON THE RT HALF OF THE NOSE WHEEL SEPARATED CAUSING EXTENSIVE DAMAGE TO FUSELAGE BELLY. THE WHEEL DID NOT DEFLATE.
- [SDR ZP7A20130807001](https://openairdocs.org/sdr/ZP7A20130807001.md): Pitot System · frozen · Aug 7, 2013 · N998PA · Raythn 390 · Pitot/Static System
  > AFTER APPROX 30 MINUTES IN CRUISE, RECEIVED AN AIRSPEED DISAGREEMENT BETWEEN NR 1 & 2 PFDS, WITH AN INDICATION OF 10 KNOTS OR GREATER. DETERMINED THE NR 2 PFD FAULTY AND COUPLED NR 2 PFD TO NR 1 ADC. AFTER DESCENT AT ABOUT FL 37,000 THE AUTOPILOT DISENGAGED.
- [SDR J5XA20130723001](https://openairdocs.org/sdr/J5XA20130723001.md): Actuator · faulty · Jun 28, 2013 · N535CD · Raythn 390 · Trailing Edge Flap Actuator
  > FLAP FAIL TO RETRACT. FOUND ACTUATOR FAULTY.
- [SDR E81R2013060423721](https://openairdocs.org/sdr/E81R2013060423721.md): Hinge · loose · Jun 4, 2013 · N527PM · Raythn 390 · Landing Gear Doors
  > FOUND LT MLG OTBD DOOR ASSY CRACKED ACROSS MAJORITY OF BONDED DOOR PANEL NEAR HINGE ATTACHMENT POINT. REQUIRED DOOR ASSY REPLACEMENT. NOTED HINGE AREA LOOSE ON RT MLG OTBD DOOR AT SIMILAR LOCATION. SUSPECT HINGE MOUNTING BECAME LOOSE ALLOWING AERODYNAMIC FO
- [SDR E81R2013052923713](https://openairdocs.org/sdr/E81R2013052923713.md): Spring · disengaged · May 29, 2013 · N112CM · Raythn 390 · Starter-Generator
  > PILOT REPORTED LT ENGINE DC GENERATOR FAIL INDICATION DEPARTING AIRPORT. INVESTIGATED LT ENGINE STARTER/GENERATOR CONDITION UPON ARRIVAL AT DESTINATION. SUSPECTED INTERNAL ELECTRICAL FAILURE OF STARTER/GENERATOR DUE TO COMMUTATOR CONDITION AND AREA RESIDUE/ODO
- [SDR 2013FA0000070](https://openairdocs.org/sdr/2013FA0000070.md): Current Limiter · open · Dec 20, 2012 · N855RM · Raythn 390 · Electrical Power System Wiring
  > AT APPROX 18:00, AFTER TAKEOFF AND CLIMBOUT, THE RT SIDE OF THE COCKPIT WENT DARK. THE PILOT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. HAD MFG TECH TROUBLESHOOT THE PROBLEM TO AN OPEN, PN ANL-325 (325 AMP) RT BUS CURRENT LIMITER WITH NO EXPLANATION
- [SDR E81R2012102300001](https://openairdocs.org/sdr/E81R2012102300001.md): Actuator · failed · Oct 23, 2012 · N285EB · Raythn 390 · Aileron Tab Control System
  > PILOT REPORTED THE RT AILERON TRIM ACTUATOR NOT RESPONDING TO CONTROL SWITCH INPUTS AND TRIPPING AFFECTED CIRCUIT BREAKERS. TROUBLESHOT TO INTERNALLY FAILED RT AILERON ROLL TRIM ACTUATOR. REPLACED THE ACTUATOR WITH A NEW ACTUATOR, ROLL TRIM SYS FUNCTIONAL CHE
- [SDR CA121017006](https://openairdocs.org/sdr/CA121017006.md): Skin · unknown · Sep 27, 2012 · Raythn 390 · Nacelle/Pylon, Plate/Skin
  > (CAN) MAINTENANCE WHEN TROUBLESHOOTING A RECURRING PROBLEM WITH THE RUDDER BOOST, FOUND WATER LEAKING INTO THE PYLON THROUGH A VENT HOLE THAT IS THERE TO PREVENT OVERHEATING OF THE PYLON.
- [SDR 2012FA0000284](https://openairdocs.org/sdr/2012FA0000284.md): Hinge Fitting · cracked · May 7, 2012 · N527PM · Raythn 390 · Wing, Control Surface Attach Fittings
  > DURING THE INSPECTION OF THE WING FLAP ACTUATOR ATTACHMENTS, FOUND THAT BOTH THE LT WING INBD FLAP FAIRING HINGE FITTING ASSY AND THE RT WING INBD FLAP FAIRING HINGE FITTING ASSY WERE CRACKED.
- [SDR E81R2012021600001](https://openairdocs.org/sdr/E81R2012021600001.md): Clamp · corroded · Feb 16, 2012 · N1XT · Raythn 390 · Flight Compartment Windows
  > DURING REPLACEMENT OF THE LT WINDSHIELD FOR HEATER ELEMENT AREA DAMAGE, NOTED EXTENSIVE CORROSION ON INTERIOR OF THE THE EXTERIOR WINDSHIELD CLAMP THAT ATTACHES THE WINDSHIELD ASSY TO THE FUSELAGE WINDSHIELD OPENING STRUCTURE. CORROSION DAMAGE REQUIRED REPLACE
- [SDR E81R2012011700001](https://openairdocs.org/sdr/E81R2012011700001.md): Keelbeam · corroded · Jan 17, 2012 · N713AZ · Raythn 390 · Fuselage Main, Keel
  > DURING SCHEDULED "A" AND "B" INSPECTIONS, VISUAL INSPECTION OF COCKPIT UNDERFLOOR AREA SHOWED FLUID SPILLAGE. FURTHER INVESTIGATION FOUND SURFACE CORROSION AND DEEP CORROSION PITS ON LBL 8.10 KEEL BEAM CAP FROM FS 121.2 TO FS 148.4 AREA. AFFECTED STRUCTURAL M

Next page: https://openairdocs.org/model/raytheon-390/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 = '390'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/raytheon-390/reports

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