# Service difficulty reports: Beech 1900C

A list on [Beech 1900C](https://openairdocs.org/model/beech-1900c.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 37 · 1,840 reports

- [SDR JIKA2026082101](https://openairdocs.org/sdr/JIKA2026082101.md): Connector · faulted · Aug 19, 2026 · N718AF · Beech 1900C · Landing Gear System Wiring
  > THE FLIGHT CREW REPORTED THAT WHEN THE LANDING GEAR DOWN WAS SELECTED THE LANDING GEAR CIRCUIT BREAKER POPPED. THE BREAKER WAS RESET AND A MANUAL LANDING GEAR EXTENSION WAS PERFORMED. THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THAT
- [SDR JIKA2026081701](https://openairdocs.org/sdr/JIKA2026081701.md): Pcb · faulted · Aug 14, 2026 · N31702 · Beech 1900C · Landing Gear System Wiring
  > THE FLIGHT CREW REPORTED THAT THE LANDING GEAR FAILED TO EXTEND NORMALLY AND A MANUAL LANDING GEAR EXTENSION WAS PERFORMED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT AND MAINTENANCE DETERMINED THAT THE CAUSE OF FAILURE WAS CORROSION AT PCB A123. THE CORRODE
- [SDR JIKA2026072402](https://openairdocs.org/sdr/JIKA2026072402.md): Warning Message · illuminated · Jul 18, 2026 · N31702 · Beech 1900C · Landing Gear Position and Warning
  > THE FLIGHT CREW REPORTED THAT THE LANDING GEAR IN TRANSIT LIGHT REMAINS ILLUMINATED WITH THE GEAR IN THE DOWN AND LOCKED POSITION. MAINTENANCE INSPECTED THE SYSTEM AND FOUND PIN 23 ON PCB A123 CONNECTOR P277 REVEALED CORROSION INTERRUPTING THE CIRCUITRY. THE S
- [SDR JIKA2026072401](https://openairdocs.org/sdr/JIKA2026072401.md): Hydraulic System · low · Jul 18, 2026 · N338AF · Beech 1900C · Hydraulic System, Main
  > DURING APPROACH, THE FLIGHT CREW REPORTED THAT THE LANDING GEAR HANDLE WAS SELECTED DOWN BUT EMERGENCY EXTENSION PROCEDURES WERE FOLLOWED TO ALLOW THE LANDING GEAR TO BE EXTENDED SAFELY. MAINTENANCE REPORTED THAT UPON INSPECTION IT WAS NOTED THAT THE HYDRAULIC
- [SDR JIKA2026051901](https://openairdocs.org/sdr/JIKA2026051901.md): Spar Angle · corroded · Apr 27, 2026 · N31703 · Beech 1900C · Vertical Stabilizer, Spar/Rib
  > DURING AN EVENT 6 SCHEDULED INSPECTION OF BEECHCRAFT MODEL 1900C AIRCRAFT N31703 (SERIAL NUMBER UB-10), PDX MAINTENANCE FOUND CORROSION ON THE VERTICAL STABILIZER REAR SPAR LH ANGLE THAT EXCEEDED THE REPAIR LIMITS IN TEXTRON 1900C SRM CHAPTERS 51-40-02 AND 51-
- [SDR JIKA2026041301](https://openairdocs.org/sdr/JIKA2026041301.md): Landing Gear · inoperative · Apr 7, 2026 · N7203C · Beech 1900C · Landing Gear Retraction/Extension System
  > THE LANDING GEAR DID NOT EXTEND NORMALLY WHEN SELECTED FOR LANDING BY THE FLIGHT CREW. THE LANDING GEAR WAS MANUALLY EXTENDED AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND THE LANDING GEAR CONTROL RELAY WAS STUCK AND WAS ABLE TO RESET THE RELAY. MULTIPLE R
- [SDR JIKA2026012301](https://openairdocs.org/sdr/JIKA2026012301.md): Trim System · out of alignment · Jan 6, 2026 · N31704 · Beech 1900C · Flight Control System
  > DURING CLIMB, THE FLIGHT CREW NOTED THAT THE AIRCRAFT ROLLED TO THE LEFT AND REQUIRED FULL INPUT TO LEVEL OFF THE WINGS. THE CREW CALLED IT IN, AND AIR RETURNED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT THE SYSTEM, CHECKED ALL FLIGHT CONTROL CABLES FOR
- [SDR YADA2025051001](https://openairdocs.org/sdr/YADA2025051001.md): Housing · eroded · May 10, 2025 · N126AX · Beech 1900C · Turbine Engine Oil System
  > FLIGHT CREW REPORTED THE #1 ENGINE LEAKING OIL - MAINTENANCE LOCATED A PINHOLE ON THE ENGINE OIL SCAVENGE PUMP HOUSING AND REPLACED THE HOUSING DUE CAVITATION EROSION THROUGH THE PUMP BODY.
- [SDR JIKA2025041501](https://openairdocs.org/sdr/JIKA2025041501.md): Wire · broken · Apr 14, 2025 · N7203C · Beech 1900C · Landing Gear System Wiring
  > THE FLIGHT CREW PERFORMED AN EMERGENCY LANDING GEAR EXTENSION. WHEN ATTEMPTING TO EXTEND THE LANDING GEAR THE LANDING GEAR HANDLE WAS UN-RESPONSIVE. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE TO THE LANDING GEAR HYDRAULIC POWER PACK PRESSURE SWITCH AND OPERA
- [SDR TIMA20250130001](https://openairdocs.org/sdr/TIMA20250130001.md): Instrument Panel · shorted · Jan 30, 2025 · N422AX · Beech 1900C · Instrument Panel
  > OVER FFU VOR THE INSTRUMENT INDIRECT LIGHTS STARTED FLICKERING INTENSELY. SHORTLY AFTER THERE WAS A STRONG BUT DISTINCT SMELL OF BURNING ELECTRONICS. THEN THE POTENTIOMETER FOR THE INSTRUMENT INDIRECT LIGHTS BECAME AN “ON/OFF” SWITCH, AND THE SMELL BEGAN TO FA
- [SDR YADA2025012701](https://openairdocs.org/sdr/YADA2025012701.md): Pump · eroded · Jan 27, 2025 · N125AX · Beech 1900C · Turbine Engine Oil System
  > MAINTENANCE DISCOVERED A LEAKING ENGINE OIL SCAVENGE PUMP - A PINHOLE WAS VERIFIED IN THE PUMP HOUSING OUTER WALL FROM INTERNAL EROSION - REPLACED SAME.
- [SDR YADA2025012201](https://openairdocs.org/sdr/YADA2025012201.md): Housing · eroded · Jan 22, 2025 · N117AX · Beech 1900C · Turbine Engine Oil System
  > MAINTENANCE NOTICED OIL LEAKING FROM #2 ENGINE COWLING. INSPECTION REVEALED OIL LEAKING FROM THE SCAVENGE OIL PUMP HOUSING PINHOLE AND REPLACED HOUSING. REMOVED UNIT WAS VERIFIED TO HAVE INTERNAL EROSION THROUGH BODY OF THE HOUSING. THIS HAS BECOME A COMMO
- [SDR TIMA20240920012](https://openairdocs.org/sdr/TIMA20240920012.md): Engine · power loss · Sep 20, 2024 · N131SF · Beech 1900C · Engine (Turbine/Turboprop)
  > ON DESCENT TO RWY 27, ON ABOUT AN 8 MILE FINAL I REDUCED POWER TO SLOW DOWN. WHEN I WENT TO ADD POWER ONCE AGAIN THE LH SIDE PRODUCED NO ADDITIONAL THRUST. UPON LOOKING AT THE ENGINE INDICATIONS I NOTICED N1 WAS AT 35%, AUTO IGNITION WAS ACTIVATED, AND AUTO FE
- [SDR TIMA20240917011](https://openairdocs.org/sdr/TIMA20240917011.md): Engine · low torque · Sep 17, 2024 · N422AX · Beech 1900C · Engine (Turbine/Turboprop)
  > TAXIED FROM THE RAMP INTO THE RUN UP AREA, DID RUN UPS AS NORMAL NOTHING ABNORMAL DETECTED. TOOK OFF 16L REACHED V1 AND ROTATED AS I NOTICED THE PLANE WAS A LITTLE SLUGGISH TO LEAVE THE GROUND AS I GOT AIRBORNE I NOTICED THE TORQUE FOR THE LEFT ENGINE STARTING
- [SDR TIMA20240823010](https://openairdocs.org/sdr/TIMA20240823010.md): None · none · Aug 23, 2024 · N120UC · Beech 1900C · Standard Practices/Structures
  > DEPARTED VFR FROM GPI, CLIMBED TO 14000 VFR. SAW WEATHER ON GPS, DEVIATED LEFT/NORTH OF COURSE TO STAY AWAY FROM THUNDERSTORM AND LIGHTNING. ENTERED IMC AROUND 14500 AND ENCOUNTERED UPDRAFTS GREATER THAN 2800FPM, MOD RIME ICE, HAIL, CLOUD TO CLOUD LIGHTNING.
- [SDR JIKA2024072301](https://openairdocs.org/sdr/JIKA2024072301.md): Hinge · corroded · Jul 23, 2024 · N3071A · Beech 1900C · Elevator Structure
  > CENTER ELEVATOR HINGE ASSEMBLY P/N 101-620013-1 FOUND WITH EXCESSIVE CORROSION / MISSING MATERIAL CREATING A 1.5 X 0.5 INCH HOLE. OUTBOARD ELEVATOR HINGE ASSEMBLY P/N 101-620011-1 ALSO FOUND WITH EXCESSIVE CORROSION / MISSING MATERIAL.
- [SDR JIKA2024060701](https://openairdocs.org/sdr/JIKA2024060701.md): Wire · broken · Jun 6, 2024 · N3071A · Beech 1900C · Landing Gear System Wiring
  > THE FLIGHT CREW REPORTED THAT THE LANDING GEAR DOWN AND LOCKED GREEN INDICATION LIGHT DID NOT ILLUMINATE WHEN THE GEAR WAS SELECTED TO THE DOWN POSITION. OUT OF PRECAUTION, THE CREW DECIDED TO REPORT TO ATC THE DISCREPANT ITEM AND OPTED TO MANUALLY EXTEND THE
- [SDR YADA202406040301](https://openairdocs.org/sdr/YADA202406040301.md): Actuator · failed insp · Jun 3, 2024 · N110AX · Beech 1900C · Landing Gear Actuator
  > WHILE PERFORMING AD 2009-23-01 (E)(3) NDT INSPECTION, INDICATION OF CRACKING WAS IDENTIFIED IN THE END CAP – SEE ATTACHED NDT REPORT. THIS INSPECTION WAS PERFORMED ON UC-93 AND THE ACTUATOR HAD 1015 CYCLES SINCE LAST INSPECTION. NO CRACKS WERE VISUALLY VISIB
- [SDR YADA2024060351101](https://openairdocs.org/sdr/YADA2024060351101.md): Housing · eroded · May 11, 2024 · N117AX · Beech 1900C · Turbine Engine Oil System
  > PILOT REPORTED OIL LEAK ON #1 ENGINE AFTER FLIGHT - MAINTENANCE LOCATED LEAK AT #1 ENGINE SCAVENGE PUMP HOUSING AND REPLACED SAME.
- [SDR YADA2024042401](https://openairdocs.org/sdr/YADA2024042401.md): Housing · eroded · Apr 24, 2024 · N244AX · Beech 1900C · Turbine Engine Oil System
  > MAINTENANCE DISCOVERED A LEAKING ENGINE OIL SCAVENGE PUMP - A PINHOLE WAS VERIFIED IN THE PUMP HOUSING OUTER WALL FROM INTERNAL EROSION - REPLACED SAME.
- [SDR TIMA20240105002](https://openairdocs.org/sdr/TIMA20240105002.md): Unknown · odor · Jan 5, 2024 · N198GA · Beech 1900C · Air Distribution System
  > ON ROTATION SMELL OF SMOKE IN COCKPIT AND I REQUESTED IMMEDIATE TURN BACK TO THE APPROACH. FLAP CIRCUIT BREAKER WAS POPPED.
- [SDR TIMA2024011103001](https://openairdocs.org/sdr/TIMA2024011103001.md): Unknown · unknown · Jan 3, 2024 · N150KJ · Beech 1900C · Indicating/Recording System
  > DURING CLIMB OUT OF SLC, PILOT NOTICED SMOKE COMING OUT FROM THE FUEL PANEL. DECLARED AND EMERGENCY AND REQUESTED RETURN TO SLC. SMOKE STOPPED ON ITS OWN AFTER ABOUT 5-10 SECONDS, STILL RETURNED TO SLC.
- [SDR JIKA20231113101](https://openairdocs.org/sdr/JIKA20231113101.md): Landing Gear · intermittent · Nov 11, 2023 · N34RZ · Beech 1900C · Landing Gear Retraction/Extension System
  > DURING TAKEOFF, THE LANDING GEAR CIRCUIT BREAKER TRIPPED WHEN THE FLIGHT CREW ATTEMPTED TO STOW THE LANDING GEAR. MAINTENANCE PERFORMED THREE SUCCESSFUL LANDING GEAR SWINGS, CONDUCTED AN INSPECTION ON ALL ASSOCIATED WIRING, CHECKED THE SERVICING VALVE AND MICR
- [SDR JIKA20231113901](https://openairdocs.org/sdr/JIKA20231113901.md): Cable · broken · Nov 9, 2023 · N31703 · Beech 1900C · Rudder Control System
  > PILOT REPORTED THAT HE HAD NO RIGHT-HAND RUDDER CONTROL ON APPROACH. THE LEFT-HAND RUDDER AND RUDDER TRIM WERE NORMAL. MAINTENANCE FOUND A SEPARATED FLIGHT CONTROL CABLE AND IS IN THE PROCESS OF REPLACING IT. BEFORE RETURNING THE AIRCRAFT TO SERVICE.
- [SDR JIKA202311090324](https://openairdocs.org/sdr/JIKA202311090324.md): Wire · broken · Nov 7, 2023 · N34RZ · Beech 1900C · Landing Gear System Wiring
  > THE LANDING GEAR CIRCUIT BREAKER TRIPPED WHILE EN ROUTE TO KGEG. THE PILOT PERFORMED EMERGENCY GEAR DOWN PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND TWO WIRES DAMAGED, G19H22 AND D41A22. WIRE REPAIRS WERE MADE AND FUNCTIONAL CHECKS OF THE LANDING
- [SDR YADA2023110401](https://openairdocs.org/sdr/YADA2023110401.md): Housing · eroded · Nov 4, 2023 · N113AX · Beech 1900C · Turbine Engine Oil System
  > PILOT REPORTED SEEING OIL ON RH WING DURING PREFLIGHT. MAINTENANCE IDENTIFIED A LEAK FROM A HOLE IN THE RH ENGINE OIL SCAVENGE PUMP HOUSING AND REPLACED SAME. THIS IS A COMON ISSUE WITH THESE PUMP HOUSINGS.
- [SDR TIMA20231031008](https://openairdocs.org/sdr/TIMA20231031008.md): Unknown · unknown · Oct 31, 2023 · N124GP · Beech 1900C · Engine Fuel and Control
  > NORMAL TAXI/RUN UP/TAKEOFF / CLIMB. AS I WAS LEVELING OFF FUEL PRESSURE LOW ON RH ENG ILLUMINATED, SWITCHED ON STANDBY PUMP AND LIGHT EXTINGUISHED LOOKED FOR AND FOUND NO SECONDARY INDICATIONS OF IMPENDING FAILURE. REDUCED POWER TO CRUISE SETTING AND SCANNED
- [SDR TIMA20230923007](https://openairdocs.org/sdr/TIMA20230923007.md): Unknown · unknown · Sep 23, 2023 · N194GA · Beech 1900C · Air Distribution System
  > ABOUT 15 MINUTES PRIOR TO LANDING DURING DESCENT INTO SLC, NOTICED A BAD SMELL. ABOUT A MINUTE AFTER I NOTICED THE SMELL THERE WAS SMOKING COMING UP FROM BEHIND THE DASH. DUMPED THE CABIN, THREW THE MASK ON, DECLARED AN EMERGENCY. I WAS OVER TVY AND ORIGINALLY
- [SDR YADA2023092101](https://openairdocs.org/sdr/YADA2023092101.md): Master Cylinder · failed · Sep 21, 2023 · N113AX · Beech 1900C · Master Cylinder/Brake Valve
  > PILOT REPORTED AFTER LANDING AND DURING TAXI "PILOT SIDE LEFT BRAKE GOES FLAT". MAINTENANCE PERFORMED TROUBLESHOOTING AND FOUND THAT THE PILOTS LEFT PEDAL BRAKE MASTER CYLINDER WAS FULLY COMPRESSING CAUSING PEDAL TO GO ALL THE WAY TO THE FLOOR. PILOTS LEFT PE
- [SDR JIKA2023090901](https://openairdocs.org/sdr/JIKA2023090901.md): Electrical Sys · shorted · Sep 9, 2023 · N331AF · Beech 1900C · Landing Gear System Wiring
  > AFTER TAKEOFF THE LANDING GEAR BECAME STUCK IN THE TRANSIT POSITION. THE PILOT PERFORMED A MANUAL LANDING GEAR EXTENSION AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND THAT THERE WAS AN ELECTRICAL SHORT FROM THE TIME DELAY CA
- [SDR JIKA2023080201](https://openairdocs.org/sdr/JIKA2023080201.md): Module · damaged · Aug 2, 2023 · N347AF · Beech 1900C · Engine (Turbine/Turboprop)
  > DURING APPROACH TO KSJU, THE FLIGHT CREW REPORTED LEFT ENGINE TORQUE DROP AND SLIGHT YAW TO THE LEFT. PILOT SHUTDOWN LH ENGINE IAW QRH. AN EMERGENCY WAS DECLARED, AND THE AIRCRAFT LANDED IN KSJU WITHOUT INCIDENT. MAINTENANCE INSPECTED ENGINE COMPRESSOR BLADES,
- [SDR TIMA2023081131005](https://openairdocs.org/sdr/TIMA2023081131005.md): Unknown · unknown · Jul 31, 2023 · N114AX · Beech 1900C · Engine Bleed Air System
  > THE LEFT BLEED AIR FAILURE WARNING LIGHT CAME ON IN CRUISE. THE SMELL OF SMOKE, POSSIBLY FROM ELECTRICAL INSULATION, WAS ALSO PRESENT IN THE COCKPIT. WE MOVED THE LEFT BLEED AIR SWITCH TO INSTRUMENT AND ENVIRO OFF. AFTER CONSULTING 21-1-3 IN THE MEL WE DETERM
- [SDR YADA2023071301](https://openairdocs.org/sdr/YADA2023071301.md): Housing · eroded · Jun 22, 2023 · N119AX · Beech 1900C · Engine Fuel Pump
  > PILOT REPORTED OIL LEAKING OUT OF RIGHT ENGINE. MAINTENANCE DISCOVER #2 ENGINE OIL SCAVENGE PUMP HAVING A PINHOLE LEAK AND THE HOUSING WAS REPLACED. INSPECTION DETERMINED THAT CAVITATION EROSION OF THE PUMP BODY IN A CORNER OF THE CAVITY HAD CREATED A HOLE.
- [SDR JIKA20230628201](https://openairdocs.org/sdr/JIKA20230628201.md): Yaw Damper · failed · Jun 22, 2023 · N31704 · Beech 1900C · Flight Control System
  > AFTER DEPARTING KMFR ENROUTE TO KPDX THE FLIGHT CREW REPORTED YAW DAMPER FAILURE FOLLOWED BY AN ELECTRICAL BURNING SMELL. PILOT DECLARED AN EMERGENCY. THE AIRCRAFT DIVERTED TO KSLE AND LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION NOTED THE YAW DAMPER CIRCUI
- [SDR JIKA2023060801](https://openairdocs.org/sdr/JIKA2023060801.md): Indicator · failed · Jun 8, 2023 · N31704 · Beech 1900C · Propeller System
  > AMF1908 – ENROUTE TO KMFR PILOT DIVERTED TO KEUG DUE TO RT PROPELLER RPM FAILURE. PILOT REPORTED THAT AT CRUISE, THE RIGHT PROPELLER RPM FAILED AND DROPPED TO AROUND 700 RPM. PILOT REDUCED TORQUE AND RPMS INDICATED NORMAL, AFTER RAISING TORQUE AGAIN RPM FAIL
- [SDR YADA20230603001](https://openairdocs.org/sdr/YADA20230603001.md): Unknown · unknown · Jun 1, 2023 · N242AX · Beech 1900C · Turbine Engine Oil System
  > DURING DESCENT THE RIGHT HAND ENGINE OIL PRESSURE WARNING INDICATOR ALERTED, PIC PERFORMED PRECAUTIONARY ENGINE SHUTDOWN AND LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONAL WAS SENT OUT TO THE LOCATION OF THE AIRCRAFT TO PERFORM TROUBLESHOOTING. U
- [SDR JIKA2023042801](https://openairdocs.org/sdr/JIKA2023042801.md): Unknown · unknown · Apr 28, 2023 · N39UB · Beech 1900C · Air Conditioning System
  > AFTER TAKEOFF FROM KDFW, THE FLIGHT CREW REPORTED AN ELECTRICAL BURNING SMELL WITH BLEED AIR SYSTEM ON. BLEED SYSTEM WAS TURNED OFF. THE AIRCRAFT RETURNED TO KDFW AND LANDED WITHOUT INCIDENT. DFW ATC DISPATCHED EMERGENCY RESPONDERS. MAINTENANCE TROUBLESHOT IS
- [SDR JIKA20230421701](https://openairdocs.org/sdr/JIKA20230421701.md): Unknown · unknown · Apr 17, 2023 · N39UB · Beech 1900C · Hydraulic System, Main
  > PILOT REPORTED THAT HYDRAULIC FLUID LOW LIGHT CAME ON IN FLIGHT. LANDING GEAR RELAY CIRCUIT BREAKER THEN POPPED. A MANUAL GEAR EXTENSION WAS PERFORMED, AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED IN KLBB WITHOUT INCIDENT. AIRCRAFT HYDRAULIC SYSTEM WAS
- [SDR YADA20230313009](https://openairdocs.org/sdr/YADA20230313009.md): Bellcrank · cracked · Mar 13, 2023 · N127AX · Beech 1900C · Elevator Control System
  > WHILE PERFORMING A COMPANY FLEET CAMPAIGN DISCOVERED FORWARD ELEVATOR BELLCRANK CRACKED WEB.
- [SDR YADA20230313001](https://openairdocs.org/sdr/YADA20230313001.md): Bellcrank · cracked · Mar 11, 2023 · N113AX · Beech 1900C · Elevator Control System
  > WHILE PERFORMING A COMPANY FLEET CAMPAIGN DISCOVERED FORWARD ELEVATOR BELLCRANK CRACKED WEB.
- [SDR YADA20230313003](https://openairdocs.org/sdr/YADA20230313003.md): Bellcrank · cracked · Mar 9, 2023 · N124AX · Beech 1900C · Elevator Control System
  > WHILE PERFORMING A COMPANY FLEET CAMPAIGN DISCOVERED FORWARD ELEVATOR BELLCRANK CRACKED WEB.
- [SDR YADA20230313005](https://openairdocs.org/sdr/YADA20230313005.md): Bellcrank · cracked · Mar 6, 2023 · N125AX · Beech 1900C · Elevator Control System
  > WHILE PERFORMING A COMPANY FLEET CAMPAIGN DISCOVERED FORWARD ELEVATOR BELLCRANK CRACKED WEB.
- [SDR YADA20230313008](https://openairdocs.org/sdr/YADA20230313008.md): Bellcrank · cracked · Mar 5, 2023 · N117AX · Beech 1900C · Elevator Control System
  > WHILE PERFORMING A COMPANY FLEET CAMPAIGN DISCOVERED FORWARD ELEVATOR BELLCRANK CRACKED WEB.
- [SDR YADA20230313002](https://openairdocs.org/sdr/YADA20230313002.md): Bellcrank · cracked · Mar 4, 2023 · N115AX · Beech 1900C · Elevator Control System
  > WHILE PERFORMING A COMPANY FLEET CAMPAIGN DISCOVERED FORWARD ELEVATOR BELLCRANK CRACKED WEB.
- [SDR YADA20230313006](https://openairdocs.org/sdr/YADA20230313006.md): Bellcrank · cracked · Mar 2, 2023 · N126AX · Beech 1900C · Elevator Control System
  > WHILE PERFORMING A COMPANY FLEET CAMPAIGN DISCOVERED FORWARD ELEVATOR BELLCRANK CRACKED WEB.
- [SDR YADA20230313004](https://openairdocs.org/sdr/YADA20230313004.md): Bellcrank · cracked · Mar 2, 2023 · N247AX · Beech 1900C · Elevator Control System
  > WHILE PERFORMING A COMPANY FLEET CAMPAIGN DISCOVERED FORWARD ELEVATOR BELLCRANK CRACKED WEB.
- [SDR YADA20230313007](https://openairdocs.org/sdr/YADA20230313007.md): Bellcrank · cracked · Feb 18, 2023 · N248AX · Beech 1900C · Elevator Control System
  > WHILE PERFORMING A COMPANY FLEET CAMPAIGN DISCOVERED FORWARD ELEVATOR BELLCRANK CRACKED WEB.
- [SDR JIKA20230116001](https://openairdocs.org/sdr/JIKA20230116001.md): Seal · leaking · Jan 10, 2023 · N7203C · Beech 1900C · Turbine Engine Oil System
  > PILOT REPORTED THAT UPON APPROACH TO KRDM THE RT ENGINE OIL PRESSURE ANNUNCIATOR ILLUMINATED. PILOT DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM TO A LEAK COMING FROM RH ENGINE OIL SCAVENGE PUMP. MAINTENANCE REMOVED AND RE
- [SDR YADA2023010327001](https://openairdocs.org/sdr/YADA2023010327001.md): Bellcrank · damaged · Dec 27, 2022 · N118AX · Beech 1900C · Elevator Control System
  > PILOT REPORT - FLIGHT CONTROLS, ELEVATOR FEEL LIGHT DURING PREFLIGHT CHECK. MAINTENANCE DISCOVERED ELEVATOR WEIGHT BROKEN OFF FROM ELEVATOR BELLCRANK ASSEMBLY. AIRCRAFT HAD BEEN SUBJECTED TO STRONG GROUND WIND VERY RECENTLY. FAILED BELLCRANK TO BE RETURNED
- [SDR TIMA20221223014](https://openairdocs.org/sdr/TIMA20221223014.md): Control Cable · broken · Dec 20, 2022 · N422AX · Beech 1900C · Rudder Control System
  > CONTROL CHECK PRIOR TO FLIGHT NORMAL. FLIGHT KBIL - KGPI. NOTHING NOTICED UNTIL ON LAST 1/4 OF APPROACH, NO RESPONSE FROM RUDDER PEDALS. LANDED THE PLANE UNEVENTFUL.ONCE WEIGHT ON WHEELS NOSE STEERING OPERATED NORMALLY. TAXIED, PARKED AND NOTIFIED MOC. GLAC

Next page: https://openairdocs.org/model/beech-1900c/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 = '1900C'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/beech-1900c/reports

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