# Service difficulty reports: Beech 1900D

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

Newest first. General aviation reporting is voluntary.

Page 1 of 144 · 7,152 reports

- [SDR TIMA20260425001](https://openairdocs.org/sdr/TIMA20260425001.md): Blower Motor · inoperative · Apr 25, 2026 · N169GL · Beech 1900D · Air Distribution Fan
  > WAS IN CRUISE FROM MKG TO IND FOR ABOUT 5 MINUTES. BEGAN TO SMELL ODOR. GOT SLIGHTLY STRONGER WITHIN ABOUT 2 MINUTES. CHOSE TO DIVERT TO SBN. ON APPROACH/FINAL RADIOS CUT IN AND OUT.
- [SDR TIMA20250603003](https://openairdocs.org/sdr/TIMA20250603003.md): Engine · power loss · Jun 3, 2025 · N247GL · Beech 1900D · Engine (Turbine/Turboprop)
  > AFTER LEVELING OFF AT 14000' LEFT FUEL PRESSURE ANNUNCIATION CAME ON, STNADBY PUMP TURNED ON, FUEL PRESSURE ANNUMC REMAINED ON, FLOW DROPPED, ENGINE ROLLED BACK. PUSHED PROPS/POWER UP, LEFT ENGINE REMINED ROLLED BACK (11%) N1. SHUTDOWN ENGINE CUTOFF, FEATHERED
- [SDR TIMA20250215002](https://openairdocs.org/sdr/TIMA20250215002.md): Unknown · odor · Feb 15, 2025 · N210GL · Beech 1900D · Air Distribution System
  > WHILE IN CRUISE FLIGHT AT 10,000FT PILOT BEGAN TO SMELL SOMETHING SUSPICIOUS. MOMENTS LATER THE PILOT EXPERIENCED A LEFT AC BUS FAILURE AND BEGAN TO SEE SMOKE COMING FROM UNDERNEATH THE CO-PILOTS SIDE OF THE AVIONICS PANEL. IMMEDIATELY PROCEEDED WITH THE MEMO
- [SDR FXTA20231124001](https://openairdocs.org/sdr/FXTA20231124001.md): Relay · failed · Nov 24, 2024 · N171CJ · Beech 1900D · Central Warning
  > BATT TIE OPEN ANNUNCIATOR ILLUMINATED DURING FLIGHT.
- [SDR TIMA20240724009](https://openairdocs.org/sdr/TIMA20240724009.md): Landing Gear · faulted · Jul 24, 2024 · N169GL · Beech 1900D · Landing Gear System
  > DURING FLINAL APPROACH, ALL THREE BUSS TIE ANNUCIATOR LIGHTS ILLUMINATED INDICATING A FAILURE OF THE CENTER BUS. I VERIFIED THE STATUS OF THE ELECTRICAL SYSTEM AND CONFIRMED NO VOLTAGE ON THE CENTER BUS. I REFERRED TO THE QRH DUE TO THE LOSS OF THE CENTER BUSS
- [SDR TIMA20240705007](https://openairdocs.org/sdr/TIMA20240705007.md): Engine · low torque · Jul 5, 2024 · N169GL · Beech 1900D · Engine (Turbine/Turboprop)
  > AFTER DESCENDING AND LEVELING OFF LEFT ENGINE TORQUE NOT RISING PROPERLY AND INCORRECT ENGINE CONTROL / FEEL, PILOT NOTICED IMPROPER POWER OUT OF LEFT ENGINE AND DECLARED EMERGENCY DUE TO PARITIAL POWER ON LEFT ENGINE. PILOT WAS CLEARD TO LAND. LANDED SAFELY A
- [SDR TIMA2024071105007](https://openairdocs.org/sdr/TIMA2024071105007.md): Engine · power loss · Jul 5, 2024 · N184UX · Beech 1900D · Engine (Turbine/Turboprop)
  > AFTER DESCENDING AND LEVELING OFF LEFT ENGINE TORQUE NOT RISISNG PROPERLY AND INCORRECT ENGINE CONTROL/FEEL, PILOT NOTICED IMPROPER PWOER OUT OF LEFT ENGINE AND DECLARED EMERGENCY DUE TO PARITAL POWER ON LEFT ENGINE. PILOT WAS CLEARED TO LAND. LANDED SAFELY AN
- [SDR 2024FA0000039](https://openairdocs.org/sdr/2024FA0000039.md): Landing Gear · malfunctioned · Jan 4, 2024 · N3199Q · Beech 1900D · Landing Gear Retraction/Extension System
  > JUST BEFORE LANDING WE GOT LANDING GEAR RELAY MESSAGE, TURNO AROUND PERFORMED. NEXT LANDING TRY WAS SUCESSFUL. CORRECTIVE ACTION: CB RESET AND NLG LUBRICATED. ELECTRICAL CONECTRO WAS CLEANED IAW WIRING MANUAL 32-31-01-01.
- [SDR 2022F00509](https://openairdocs.org/sdr/2022F00509.md): Rib · cracked · Dec 9, 2022 · N254GL · Beech 1900D · Wing, Rib/Bulkhead
  > CRACKS IN LEFT HAND CENTER WING MAIN RIB, AT LEFT BUTTOCK LINE 29, RADIATING FROM FASTENER HOLES OF U-SHAPED STIFFENER CHANNEL FLANGES AT THE FOLLOWING LOCATIONS; BS 303 AFT FLANGE RADIATING BOTH INBOARD AND OUTBOARD FROM FASTENER HOLE AT LEFT BUTTOCK LINE 28.
- [SDR 2022FA0000756](https://openairdocs.org/sdr/2022FA0000756.md): Rib · cracked · Dec 9, 2022 · N201GL · Beech 1900D · Wing, Rib/Bulkhead
  > CRACKS IN LEFT HAND CENTER WING MAIN RIB, AT LEFT BUTTOCK LINE 29, RADIATING FROM FASTENER HOLES OF U-SHAPED STIFFENER CHANNEL FLANGES AT BS 303 AFT FLANGE RADIATING BOTH INBOARD AND OUTBOARD FROM FASTENER HOLE AT LEFT BUTTOCK LINE 28.3, WATER LINE 80.5. BS 30
- [SDR 2022F00440](https://openairdocs.org/sdr/2022F00440.md): Adapter · cracked · Nov 1, 2022 · N148SK · Beech 1900D · Elevator Control System
  > DURING ROUTINE INSPECTION WHILE PERFORMING INSPECTION "I" CHECK PROCEDURE (5-00-I0) TABLE 1 ITEM 30. IT WAS DISCOVERED THAT THE ELEVATOR HORN TO ELEVATOR ATTACH BRACKET P/N:101-610017-1 WAS CRACKED 85% AROUND THE CIRCUMFERENCE OF THE BRACKET WITH THE CRACK TRA
- [SDR GRTA20220801001](https://openairdocs.org/sdr/GRTA20220801001.md): Skin · damaged · Aug 1, 2022 · N195AW · Beech 1900D · Elevator, Plate/Skin
  > LH ELEVATOR LIGHTNING STRIKE ON TRAILING EDGE APPROX 1.1" FROM ELEVATOR TRIM TAB AT DRAIN GROMMET. DAMAGE 0.7" X 0.6" THROUGH TOP AND BOTTOM SKIN. REPAIRED IAW TEXTRON REPAIR FR-UE-128-10858
- [SDR 2022FA0000426](https://openairdocs.org/sdr/2022FA0000426.md): Wire · out of position · Jul 4, 2022 · N49543 · Beech 1900D · Engine Indicating System Wiring
  > LH ENGINE TORQUE INDICATION QITH CONTINUOUS OSCILATION. QRF TO SLLP. CORRECTIVE ACTION: REPOSITIONES ELECTRICAL LINE IAW WDM 77-12-01. IN OPERATIONAL TEST OK IAW AMM 72-00-00.
- [SDR 2022FA0000289](https://openairdocs.org/sdr/2022FA0000289.md): None · none · Jun 8, 2022 · Beech 1900D · Door Warning System
  > FORWARD DOOR WARNING INDICATOR LIGHT TUNED ON DURING CLIMB. CORRECTIVE ACTION: DOOR POSITION SWITCH WAS ADJUSTED/REGULATED. IN TEST OK
- [SDR 2022FA0000757](https://openairdocs.org/sdr/2022FA0000757.md): Rib · cracked · May 17, 2022 · N245GL · Beech 1900D · Wing, Rib/Bulkhead
  > CRACKS IN LEFT HAND CENTER WING MAIN RIB, AT LEFT BUTTOCK LINE 29, RADIATING FROM FASTENER HOLES OF U-SHAPED STIFFENER CHANNEL FORWARD AND AFT FLANGES AT FUSELAGE STATION 303 BOTH INBOARD AND OUTBOARD FROM FASTENER HOLE AT LEFT BUTTOCK LINE 28.3, WATER LINE 80
- [SDR TIMA20220314003](https://openairdocs.org/sdr/TIMA20220314003.md): None · none · Mar 10, 2022 · N716MJ · Beech 1900D · Landing Gear System
  > EXITING RUNWAY ONTO TAXIWAY AIRCRAFT ENCOUNTERED A PATCH OF ICE NEAR THE EDGE OF THE PAVEMENT SURFACE DURING LEFT HAND TURN. AS TURNING REQUIRED BRAKING ACTION TO COMPLETE, LEFT BRAKE WAS INEFFECTIVE. PLACED POWER LEVERS IN REVERSE AND DEPRESSED RIGHT BRAKE TO
- [SDR 2021FA0000410](https://openairdocs.org/sdr/2021FA0000410.md): Bleed Air Sys · dirty · Dec 14, 2021 · Beech 1900D · Engine Bleed Air System
  > ENGINE #2 LOW POWER DURING TAKEOFF (TORQUE INDICATOR 600PSI). ABORTED TAKEOFF. CORRRECTIVE ACTION: BLEED AIR CLEANED IAW AMM 75-00-00. ENGINE RUNNUP OK.
- [SDR GRTA20210420001](https://openairdocs.org/sdr/GRTA20210420001.md): Spar Cap · cracked · Apr 20, 2021 · N195AW · Beech 1900D · Fuselage Main, Frame
  > AFT SPAR UPPER SPAR CAP CRACKED (FS 327.630) AT LBL 1.0 THRU LBL 5.0. JUST OB OF FLAP MOTOR/GEAR BOX.
- [SDR GRTA20210414004](https://openairdocs.org/sdr/GRTA20210414004.md): Stringer · cracked · Apr 12, 2021 · N195AW · Beech 1900D · Fuselage Main, Longeron/Stringer
  > STRINGER 9R CRACKED AT LAST RIVET JUST AFT OF AFT PRESSURE BULKHEAD (APPROX FS 557.500)
- [SDR GRTA20210414001](https://openairdocs.org/sdr/GRTA20210414001.md): Stringer · debonded · Apr 11, 2021 · N195AW · Beech 1900D · Fuselage Main, Longeron/Stringer
  > STRINGER 15R DISBONDED FROM SKIN BETWEEN FS 378.250 AND 393.250.
- [SDR GRTA20210414003](https://openairdocs.org/sdr/GRTA20210414003.md): Pan · cracked · Apr 7, 2021 · N195AW · Beech 1900D · Emergency Exits
  > EMERGENCY EXIT 4C WINDOW PAN CRACKED PART NUMBER 129-430043-3.
- [SDR GRTA20210414002](https://openairdocs.org/sdr/GRTA20210414002.md): Pan · cracked · Apr 7, 2021 · N195AW · Beech 1900D · Emergency Exits
  > EMERGENCY EXIT 6A WINDOW PAN CRACKED PART NUMBER 129-430043-3.
- [SDR GRTA20201210002](https://openairdocs.org/sdr/GRTA20201210002.md): Skin · cracked · Jan 6, 2021 · N195AW · Beech 1900D · Fuselage Main, Plate/Skin
  > BELLY SKIN CRACKED AT FS 288.25 JUST OUTBOARD OF STRINGER 15L APPROXIMATELY 1" AND 1.5". AFTER FURTHER INVESTIGATION, FOUND FRAME SHIM CORRODED. REPAIRED IAW BEECHCRAFT 1900 SRM 51-70-06.
- [SDR TIMA2020090982003](https://openairdocs.org/sdr/TIMA2020090982003.md): Governor · leaking · Aug 29, 2020 · N170GL · Beech 1900D · Engine Oil Indicating System
  > LEVELED OFF IN CRUISE AT 14000' STARTED CRUISE CHECKS AND NOTICED OIL PRESS ON NR 2 ENGINE AT 60 PSI. PRESSURE EVENTUALLY DROPPED BELOW 60, SHUT DOWN ENGINE, MADE EMERGENCY LANDING IN BIL.
- [SDR TIMA20200609002](https://openairdocs.org/sdr/TIMA20200609002.md): Control Rod · broken · Jun 9, 2020 · N60MJ · Beech 1900D · Rudder Control System
  > DURING FLIGHT, PILOT EXPERIENCED LOSS OF RUDDER INPUT. LANDED SAFELY IN MOT. MAINTENANCE FOUND THE RUDDER CROSSOVER SHAFT WHICH CONNECTS PILOT WITH CO-PILOT PEDAL CONTROLS BROKEN.
- [SDR CA190806006](https://openairdocs.org/sdr/CA190806006.md): Bearing · damaged · Aug 6, 2019 · Beech 1900D · Trailing Edge Flap Control System
  > (CAN) DURING THE MANUFACTURERS SCHEDULED 5000HR/5 YEAR FLAP INSPECTION IT WAS FOUND THAT THE AIRCRAFT WAS NOT IN COMPLIANCE WITH AN AD THAT WAS SHOWING AS PREVIOUSLY COMPLIED WITH IN THE AIRCRAFT RECORDS. AD99-01-03 WAS SHOWING AS BEING PREVIOUSLY COMPLIED WIT
- [SDR CA190726009](https://openairdocs.org/sdr/CA190726009.md): Control Head · failed · Jul 9, 2019 · Beech 1900D · VHF Communications System
  > (CAN) AT TOP OF CLIMB THE #2 COMM FAILED. THE CREW HAD CARRIED OUT SOME BASIC TROUBLESHOOTING AND DETERMINED THAT THE RADIO WAS, INDEED, U/S. THEY HAD INFORMED AIR TRAFFIC CONTROL AND DID A RETURN BACK TO AIRPORT OF ORIGIN WHERE THEY HAD LANDED SAFELY. MAINTEN
- [SDR CA190621007](https://openairdocs.org/sdr/CA190621007.md): Torque Tube · cracked · Jun 20, 2019 · Beech 1900D · Rudder Control System
  > (CAN) DURING HEAVY CHECK 3RD PARTY MRO IDENTIFED RUDDER TORQUE SHAFT LOOSE AND A CIRCUMFERENTIAL CRACK.
- [SDR CA190521005](https://openairdocs.org/sdr/CA190521005.md): Diode · overheated · May 16, 2019 · Beech 1900D · Landing Gear Retraction/Extension System
  > (CAN) DURING LANDING CHECKS, UPON FINAL INTO XXXX, THE LANDING GEAR WAS SELECTED DOWN BY THE CREW, BUT DID NOT EXTEND. CREW HAD CARRIED OUT A `GO AROUND` AND REQUESTED A HOLD WITH CENTER. CREW HAD CARRIED OUT REQUIREMENTS OF THE APPLICABLE CHECKLIST WHERE THE
- [SDR CA190513002](https://openairdocs.org/sdr/CA190513002.md): Pressure Switch · leaking · May 11, 2019 · Beech 1900D · Engine Oil Pressure
  > (CAN) AFTER DEPARTING OUT OF XXX WE HAD THE #2 ENGINE BOUNCING BETWEEN 4000-2500 TORQUE, AT 400 FEET WE BROUGHT POWER BACK TO CLIMB POWER AND THE TORQUE WAS STEADY, SO WE THOUGHT IT WAS JUST THE GAUGE. WHEN WE WERE CRUISING TO XXX AT 4500 FEET WE HAD A LOW OIL
- [SDR CA190501023](https://openairdocs.org/sdr/CA190501023.md): Screw · damaged · May 1, 2019 · Beech 1900D · Main Landing Gear
  > (CAN) UPON APPROCH INTO XXXX, FLIGHT CREW OF C-XXXX ATTEMPTED TO SELECT GEAR DOWN. `LANDING GEAR CONTROL` CIRCUIT BREAKER FOUND TO BE `POPPED`. BREAKER RESET & DOWN SELECTION RE-SELECTED. POSITIVE DOWN LOCK INDICATION FOR BOTH MAINS ACHIEVED, NEGATIVE INDICATI
- [SDR CA190501015](https://openairdocs.org/sdr/CA190501015.md): Altimeter · failed · Apr 30, 2019 · Beech 1900D · Altimeter, Barometric/Encoder
  > (CAN) JUST AFTER TAKE OFF THE CAPTAIN`S ALTIMETER FAILED. THIS EVENT, IN TURN, CAUSED DISRUPTION OF OTHER ASSOCIATED EQUIPMENT SUCH AS THE ALTITUDE ALERTER, TCAS AND TRANSPONDER. (TC# 20190501015)
- [SDR CA190514017](https://openairdocs.org/sdr/CA190514017.md): Uplock Switch · faulty · Apr 16, 2019 · Beech 1900D · Landing Gear Retraction/Extension System
  > (CAN) GEAR FAILED TO RETRACT AFTER TAKE-OFF. FOUND RH MLG UPLOCK SWITCH TO BE AT FAULT. RH MLG UPLOCK SWITCH REPLACED AND RIGGED. (TC# 20190514017)
- [SDR CA190415001](https://openairdocs.org/sdr/CA190415001.md): Governor · weak · Apr 13, 2019 · Beech 1900D · Propeller Governor
  > (CAN) LEFT ENGINE AUTO FEATHER ENGAGED ON APPROACH PILOT REPORTED PROP FEATHERED FOR ABOUT 3 SEC WHEN POWER WAS REDUCED BEFORE SELECTING FLAP 35. IT CAUSED THE PLANE TO YAW QUITE A BIT CORRECTION P/N OS GOVERNOR 210961C (TC# 20190415001)
- [SDR CA190417007](https://openairdocs.org/sdr/CA190417007.md): Safety Switch · unserviceable · Apr 12, 2019 · Beech 1900D · Landing Gear Position and Warning
  > (CAN) THIS GEAR SAFETY SWITCH (SQUAT SWITCH) HAS MULTIPLE SWITCH THROWS THAT CONTROL MULTIPLE SYSTEMS. ONE SWITCH THROW THAT CONTROLS THE OPERATION OF THE GROUND FINE SOLENOIDS SHORTED INTERNALLY WHICH MAKE THE GROUND FINE SOLENOID SYSTEM ALWAYS BEHAVE LIKE IT
- [SDR CA190410015](https://openairdocs.org/sdr/CA190410015.md): Actuator · malfunctioned · Apr 8, 2019 · Beech 1900D · Landing Gear Actuator
  > (CAN) MAIN LANDING GEAR ACTUATOR 114-380041-15 S/N 0606A WAS INSTALLED ON 14 DEC 2018 AT 14,026.9HRS. THE ACTUATOR HAD A FORM ONE FOR THE OVERHAUL WHICH ALSO STATED AD2009-23-01 (ULTRASONIC INSPECTION) WAS CARRIED OUT AT THE OVERHAUL. WE RECEIVED AN EMAIL FROM
- [SDR CA190403020](https://openairdocs.org/sdr/CA190403020.md): Pushrod · worn · Apr 3, 2019 · Beech 1900D · Power Lever
  > (CAN) DURING INSPECTION IT WAS DISCOVERED THAT THERE WAS WEAR ON THE RH POWER LEVER PEDESTAL PUSH ROD. IT WAS DETERMINED TO ORIGINATE FROM INTERFERENCE WITH THE LH PROPELLER CONTROL. AFTER CONSULTATION WITH BEECHCRAFT IT WAS FOUND THAT THE DIAGRAM SHOWING INST
- [SDR CA190319008](https://openairdocs.org/sdr/CA190319008.md): Connector · loose · Mar 18, 2019 · Beech 1900D · Landing Gear System Wiring
  > (CAN) AIRCRAFT LANDING GEAR WOULD NOT EXTEND. APPROACH WAS ABORTED AND FLIGHT CREW COMPLETED AN EMERGENCY EXTENSION. FOUND ELECTRICAL CONNECTOR ON THE LANDING GEAR CONTROL ASSEMBLY TO BE LOOSE. AFTER CONNECTOR TIGHTENED THE LANDING GEAR SYSTEM TESTED SERVICEAB
- [SDR CA190221008](https://openairdocs.org/sdr/CA190221008.md): Shaft · deformed · Feb 18, 2019 · Beech 1900D · Trailing Edge Flap Control System
  > (CAN) DURING MAINTENANCE TO RECTIFY A FLAP MEL, IT WAS DISCOVERED THAT THE #4 FLAP SHAFT ASSEMBLY HAD BEEN TWISTED AND DEFORMED. THE SHAFT ASSEMBLY WAS ULTIMATELY REPLACED IAW MANUFACTURER`S INSTRUCTIONS AND SYSTEM OPERATION WAS CARRIED OUT WITH NO OTHER FAULT
- [SDR CA190305016](https://openairdocs.org/sdr/CA190305016.md): Relay · failed · Feb 4, 2019 · Beech 1900D · Electrical Power System
  > (CAN) JUST AFTER GROUND POWER WAS PUGGED IN, I OPENED THE DOOR TO COMMUNICATE THE FUEL LOAD TO THE FUELLER. I NOTICED THE PROP SMOKING NEAR THE SPINNER, JUST AFTER TALKING TO THE FUELLER. I CALL TO XXX TO TURN OFF THE PROP HEAT. HE SAID IT WAS OFF. I CALLED FO
- [SDR CA181015014](https://openairdocs.org/sdr/CA181015014.md): Buss Bar · corroded · Oct 12, 2018 · Beech 1900D · Electrical Power System Wiring
  > (CAN) DURING TROUBLE SHOOTING FOUND OUT THAT BUS BAR WAS CORRODED AND NOT MAKING PROPER CONTACTS WHEN GPU IS ATTACHED. BUS BAR WAS REPLACED ALONG WITH RECEPTACLE FOR FIX. SYSTEM CHECKED SERVICEABLE AND AIRCRAFT WAS RELEASED FOR SERVICE. (TC# 20181015014)
- [SDR CA180707001](https://openairdocs.org/sdr/CA180707001.md): Transducer · disconnected · Jul 4, 2018 · Beech 1900D · Brake Anti-Skid Section
  > (CAN) ATTACH SCREWS P/N MS24693-S24 BECAME FREE OF WHEEL SPEED TRANSDUCER P/N 140-04715. TRANSDUCER WAS ABLE TO SHIFT INSIDE THE AXLE ALLOWING FOR THE TRANSDUCER TO LOOSE WHEEL SPEED INPUT, DUE TO SEPARATION FROM DRIVE HUBCAP P/N 114-810055-3. ONLY INDICATIO
- [SDR GLBA2018032100704](https://openairdocs.org/sdr/GLBA2018032100704.md): Cable · broken · Mar 20, 2018 · N251GL · Beech 1900D · Passenger/Crew Doors
  > MAINTENANCE REPORTED THAT THE FORWARD LOWER PASSENGER DOOR CABLE WAS BROKEN. MAINTENANCE REPLACED THE CABLE IAW MM 52-10-02 3A & B.
- [SDR GLBA2018030800702](https://openairdocs.org/sdr/GLBA2018030800702.md): Cable · frayed · Mar 6, 2018 · N195GL · Beech 1900D · Passenger/Crew Doors
  > MAINTENANCE REPORTED THAT THE AIRSTAIR DOOR LOWER FORWARD HANDRAIL CABLE IS FRAYED. MAINTENANCE REMOVED AND REPLACED AIRSTAIR DOOR LOWER FORWARD HANDRAIL CABLE IAW MM 52-10-02.
- [SDR CA180222015](https://openairdocs.org/sdr/CA180222015.md): Landing Gear · damaged · Feb 16, 2018 · Beech 1900D · Nose/Tail Landing Gear
  > (CAN) DURING PUSH BACK IN YUL, DUE TO ICY CONDITION NOSE STEERING EXCEEDED NOSE GEAR STEERING LIMIT AND DAMAGE TO STEERING BUNGEE, SHIMMY DAMPER, GUIDE AND ALIGNMENT BRACKET. ALL THE DAMAGED PARTS HAVE BEEN REPLACED INCLUDING NOSE GEAR ASSEMBLY FOR FIX. (TC
- [SDR GLBA2018020700701](https://openairdocs.org/sdr/GLBA2018020700701.md): Mount · worn · Feb 6, 2018 · N192GL · Beech 1900D · Trailing Edge Flaps
  > MAJOR REPAIR - RT INBD FLAP ACTUATOR FORWARD MOUNT WORN AT RT WS 53.94. ** SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR AND RETENTION OF THE PAPERWORK. **
- [SDR GLBA2018020700700](https://openairdocs.org/sdr/GLBA2018020700700.md): Mount · worn · Feb 6, 2018 · N192GL · Beech 1900D · Trailing Edge Flaps
  > MAJOR REPAIR - RT INBD FLAP ACTUATOR FORWARD MOUNT WORN AT RT WS 56.06. ** SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR AND RETENTION OF THE PAPERWORK. **
- [SDR 2018FA0000051](https://openairdocs.org/sdr/2018FA0000051.md): Duct · damaged · Feb 5, 2018 · N15GA · Beech 1900D · Pneumatic Distribution System
  > LEFT TEMPERATURE CONTROLLER SENSOR MOUNT BASE BROKE AT THE BLEED AIR DUCT ASSEMBLY CREATING A HOLE LARGE ENOUGH TO PROHIBIT CABIN PRESSURIZATION AND PROMPTING A LT ENVIR OFF LIGHT. PHOTOS AND DRAWING PROVIDED.
- [SDR GLBA2018011100699](https://openairdocs.org/sdr/GLBA2018011100699.md): Rudder Pedal · sheared · Jan 9, 2018 · N169GL · Beech 1900D · Rudder Control System
  > PILOTS REPORTED THAT WHILE TAXING OFF THE RUNWAY, WHEN RIGHT RUDDER PRESSURE WAS APPLIED, THE CAPTAIN'S RIGHT RUDDER PEDAL ASSEMBLY SHEARED OFF, FLOPS LOOSE ON THE ASSEMBLY. R & R THE CAPTAIN'S RT RUDDER PEDAL AND ARM ASSEMBLY IAW MM 27-20-03-201. OPS CHECK
- [SDR GLBA2017121800698](https://openairdocs.org/sdr/GLBA2017121800698.md): Coupling · leaking · Dec 15, 2017 · N261GL · Beech 1900D · Fuel Storage
  > CREW REPORTED THAT THERE WAS A HYDRAULIC LEAK IN THE RIGHT FRONT PART OF THE RIGHT WHEEL [WELL]. 6-7 INCH PUDDLE BUT COULD SEE NO ACTUAL DRIPS. MAINTENANCE TROUBLESHOT AND FOUND FUEL LEAKAGE AT THE RIGHT OUTBOARD WING VENT BOX TRANSFERRING TO WHEEL WELL THROUG

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

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

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