Beech 1900D

Service difficulty reports · 7,152

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duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR GLBA20061009Hinge Fitting · damagedCARGO DOOR HINGE HALF FORWARD AND AFT LUGS MISSING AND SEVERAL LOOSE RIVETS. MAINTENANCE REPLACED HINGE HALF ON CARGO DOOR IAW SRM 52-90. RII INSPECTION COMPLIED WITH IAW TASKCARD 8.2.1. IWO NR 94171, L/P NR 207464.Oct 8, 2007 · N261GL · Beech 1900D · Cargo/Baggage DoorsSDR BSAASDR0725Skin · tornRIGHT FLAP HUMP MISSING LARGE SECTION OF SHEET METAL. FLAP WAS REMOVED AND REPLACED.Oct 5, 2007 · N182YV · Beech 1900D · Trailing Edge FlapsSDR AMWA87824Hsi · odorELECTRICAL ODOR REPORTED IN COCKPIT ON CLIMBOUT. RETURNED TO FIELD AND MAINTENANCE VERIFIED THAT PROBLEM ORIGINATING IN CAPTAIN'S EHSI. REMOVED AND REPLACED UNIT, OPERATIONAL CHECK WAS SATISFACTORY.Oct 4, 2007 · N176YV · Beech 1900D · Directional Gyro and Indicating SystemSDR CA071010008Actuator · seized(CAN) DURING A 50 HOUR ROUTINE INSPECTION MAINTENANCE PERSONEL DISCOVERED THAT THE AILERON TRIM WAS NOT MOVING. UPON INSPECTION OF THE SYSTEM IT WAS DISCOVERED THAT THE AILERON TRIM ACTUATOR WAS SEIZED. THE ACTUATOR WAS REMOVED AND DISSASSEMBLED. THERE WAS INTOct 3, 2007 · Beech 1900D · Aileron Tab Control SystemSDR AMWA0828013Spar Cap · corrodedBIO CORROSION LT MAIN SPAR, LWR CAP FROM APPROX WS119.5 TO WS122. REPAIRED IAW REPORT NR 6872 REV IR.Oct 2, 2007 · N176YV · Beech 1900D · Wing SparSDR AMWA0828013BFrame · chafedREPAIRED LT AND RT FUSELAGE FRAME DAMAGED BY FRICTION CHAFING AT FS 213.25.Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, FrameSDR AMWA0828013JFrame · chafedREPAIRED FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT LT AND RT FS 408.25.Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, FrameSDR AMWA0828013DFrame · chafedREPAIRED FUSELAGE FRAME DAMAGED BY FRICTION CHAFING AT FS 243.25, RT.Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, FrameSDR AMWA0828013CFrame · chafedREPAIRED LT AND RT FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT FS 228.25.Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, FrameSDR AMWA0828013GFrame · chafedREPAIRED FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT LT AND RT FS 318.25.Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, FrameSDR AMWA0828013HFrame · chafedREPAIRED FUSELAGE FRAME DAMAGED BY FRICTION CHAFING AT RT FS 363.25.Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, FrameSDR AMWA0828013KFrame · chafedREPAIRED FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT LT AND RT FS 438.25.Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, FrameSDR AMWA0828013IFrame · chafedREPAIRED FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT LT AND RT FS 378.25.Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, FrameSDR AMWA0828013FFrame · chafedREPAIRED FUSELAGE FRAME DAMAGED BY FRICTION CHAFING AT RT FS 303.25.Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, FrameSDR AMWA0828013EFrame · chafedREPAIRED LT AND RT FUSELAGE FRAMES DAMAGED BY FRICTION CHAFFING AT FS 258.25.Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, FrameSDR AMWA0828013ASkin · damagedRT UPPER WING SKIN BETWEEN WS117.5 AND WS133 HAD NUMEROUS ELONGATED HOLES FROM OVERSIZED RIVETS. REPAIRED IAW REPORT NR 6878-1 REV IR.Oct 2, 2007 · N176YV · Beech 1900D · Wing, Plate/SkinSDR GLBA20061007Stringer Splice · corrodedBELLY CORROSION FOUND AT APPROXIMATELY FS 246 TO FS 250 ON STRINGER 15R. MAINTENANCE REPLACED DAMAGED STRINGER SECTION PER ENGINEERING ORDER 07-UE261-01. APPROXIMATE STRINGER REPLACEMENT 15" WITH 11" NEW STRINGER SPLICE. PART NUMBER 131686. RII INSPECTION COMOct 1, 2007 · N261GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA20061008Frame · crackedFRAME CRACKED AT STRINGER CUTOUT FS 177 AT STRINGER 9AR. REPAIRED FRAME AT STRINGER RELIEF HOLE FS 177 AND STRINGER 9AR IAW 1900D SRM 51-70. REPAIR DIMENSIONS 4.5 BY 2.5 . 2024 T-3 .080. RII COMPLIED WITH IAW TASKCARD 8.2.1.Oct 1, 2007 · N261GL · Beech 1900D · Fuselage Main, FrameSDR NSVA20070238Handle · malfunctionedLANDING GEAR FAILED TO EXTEND (NO INDICATION WITH GEAR HANDLE DOWN) RE-CYCLED GEAR. EXTENDED NORMALLY. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE.Sep 30, 2007 · N152MJ · Beech 1900D · Landing Gear SelectorSDR GUUA09280701Bolt · unknownAFTER TAKEOFF AT TNT LT MAIN LANDING GEAR GREEN ANNUNCIATOR BLANK OUT AND RED HANDLE ILLUMINATED. RECYCLED LANDING GEAR TWO TIMES WITH SAME RESULTS.CONTINUED TO FLL. MANUALLY EXTENDED LANDING GEAR LANDED WITHOUT INCIDENT. INSPECTED LANDING GEAR SYSTEM INSTALSep 28, 2007 · N87552 · Beech 1900D · Main Landing GearSDR GUUA09270703Hinge Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT IB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED RT IB ELEVATOR HINGE BRACKET.Sep 27, 2007 · N87555 · Beech 1900D · Horizontal Stabilizer StructureSDR GUUA09260701Skin · damagedAT SCHEDULED INSPECTION DISCOVERED LT FUSELAGE SKIN EXFOLIATED AT FS 213.250 BETWEEN STRINGERS 13L TO 14L. REMOVED DAMAGED SKIN AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER IAW SRM 51-70-06.Sep 26, 2007 · N87555 · Beech 1900D · Fuselage Main, Plate/SkinSDR AMWA87659BCBattery · dischargedBATTERY CHARGE ANNUNCIATOR ILLUMINATED DURING FLIGHT. AIRCRAFT CONTINUED TO DESTINATION WITHOUT INCIDENT. BATTERY WAS REPLACED. THIS TYPE ANNNUNCIATOR WRITEUP IS CONSIDERED A NUISANCE AND DISTRACTION TO THE CREW.Sep 25, 2007 · N166YV · Beech 1900D · Battery/Charger SystemSDR NSVA20070232Switch · looseDURING TAKEOFF ROLL AUTO FEATHER INITIALLY ARMED WITH SETTING OF TAKEOFF POWER. AT 55 KIAS AUTOFEATHER DISABLE LIGHT ILLUMINATED AND TAKEOFF WAS ABORTED. FOUND LT POWER LEVER AFX SWITCH LOOSE. TIGHTENED SWITCH AND OP CHECKED IAW AMM 61-21-00, OPS CHK GOOD.Sep 24, 2007 · N152MJ · Beech 1900D · Propeller Feathering/ReversingSDR NSVA20070233Landing Gear · malfunctionedLANDING GEAR FAILED TO EXTEND NORMALLY. GEAR HANDLE PLACED IN DOWN POSITION, GEAR DID NOT EXTEND. RED LOLLIPOP LIGHTS DID NOT ILLUMINATE, RECYCLED GEAR HANDLE AND GEAR EXTENDED NORMALLY. PERFORMED EXTENSION AND RETRACTION OF THE LANDING GEAR SYSTEM IAW BEECSep 24, 2007 · N152MJ · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GUUA09240702Skin · crackedAT SCHEDULED INSPECTION DISCOVERED AIRCRAFT BELLY RT SIDE HAS A FUSELAGE CRACK AT FS 288.0. STOP DRILLED CRACK AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER IAW STRUCTURAL REPAIR MANUAL 53-90-18.Sep 24, 2007 · N49543 · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA09240701Unknown · odorFLIGHT: 2043 TNT/FLL, DURING FLIGHT AIRCRAFT COCKPIT SMELLS LIKE FUEL THE ODOR WAS OVERWELMING. INSPECTED AIRCRAFT FOUND NO EVIDENCE OF FUEL LEAK. PERFORMED ENGINE RUNS AT VARIOUS POWER SETTINGS NO FUEL ODOR NOTED.Sep 24, 2007 · N53545 · Beech 1900D · Air Distribution SystemSDR GLBA20061006Frame · crackedFUSELAGE FRAME CRACKED APPROXIMATELY .8 INCH IN LENGTH AT FS 177 AT STRINGER 9AR. CRACKED AT STRINGER CUTOUT ON FRAME. REPAIRED FUSELAGE FRAME CRACK AT STRINGER RELIEF HOL AT F.S. 177 STRINGER 9AR. REPAIR APPROXIMATELY 4.4 INCH BY 2.5 INCH .080 2024 T-3.Sep 24, 2007 · N210GL · Beech 1900D · Fuselage Main, FrameSDR GUUA09220703Door · out of adjustDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT AFT EMERGENCY HATCH INNER HANDLE HARD TO OPEN. ADJUSTED RT AFT EMERGENCY HATCH HANDLE.Sep 22, 2007 · N69547 · Beech 1900D · Emergency ExitsSDR GUUA09220701Uplock Switch · inoperativeAFTER TAKEOFF LANDING GEAR UNSAFE LIGHTS ILLUMINATED WITH LANDING GEAR IN THE UP POSITION. REPLACED LANDING GEAR UPLOCK SWITCH. OPERATIONAL CHECK NORMAL.Sep 22, 2007 · N87554 · Beech 1900D · Landing Gear Position and WarningSDR GLBA20061005Frame · crackedFRAME CRACKED AT FS 164 AT STRINGER 9AL. CRACK LENGTH APPROXIMATELY 4 INCHES. 09-26-07 REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE FS 164 AT STRINGER 9AR IAW BEECH 1900D SRM 51-70. REAPIR APPROXIMATELY 2.5" BY 4.1" .080 2024 T-3.Sep 21, 2007 · N210GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20061004Angle · crackedLT HEAVY ANGLE CRACKED AT FS STA 288.0 FORWARD END IN BEND RADIUS. 09-26-07 CRACK APPROXIMATELY 1.75" IN LENGTH. MAINTENANCE INSTALLED REPAIR ANGLE I.A.W. BEECH SRM 53-90-23. REPAIR LENGTH 13.8 INCHES. .080 2024-0.Sep 21, 2007 · N210GL · Beech 1900D · Fuselage Main, StructureSDR AMWA87546Battery · corrodedAFTER ARRIVING, THE CREW CALLED MAINT CONTROL TO WRITEUP THE BATTERY CHARGE ANNUNCIATOR ILLUMINATED IN FLT. THIS BATTERY CHARGE ANNUNCIATOR WRITEUP IS A NUISANCE ALARM AND IS DISTRACTING TO THE FLIGHTCREW. MAINTENANCE CLEANED THE BATTERY SHUNT, OPS NORMAL.Sep 19, 2007 · N244YV · Beech 1900D · Battery/Charger SystemSDR GUUA09170701Actuator · malfunctionedDURING APPROACH "H" OF THE LT "H" LANDING GEAR POSITION INDICATING LIGHTS ONLY ILLUMINATED ON THE THIRD CYCLING OF THE LANDING GEAR. REPLACED LT MAIN LANDING GEAR ACTUATOR OPERATIONAL CHECK NORMAL.Sep 17, 2007 · N190YV · Beech 1900D · Landing Gear ActuatorSDR AMWA87499Brake Assy · weakAFTER LANDING, THE NIGHT CREW CALLED MAINT CONTROL TO REPORT CAPT'S BRAKES FELT SPONGY. MAINTENANCE BLED BRAKES AS NEEDED.Sep 17, 2007 · N143YV · Beech 1900D · Landing Gear Brake SystemSDR GLBA20061000Skin · crackedBELLY SKIN CRACKED AT WING SPAR FS 290.5 AT BL 29.06 CRACK LENGTH APPROXIMATELY 1.250 INCHES. MAINTENANCE REPAIRED SKIN CRACK AT LT WING SPAR AREA FS 290 AND BL 29.06 IAW SRM 53-90. REPAIR DIMENSION 7 INCH BY 5.8 INCHES. 2024 T3, .040 INCH. RII INSPECTION Sep 17, 2007 · N169GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA09160702Skin · corrodedAT SCHEDULED INSPECTION DISCOVERED SEVERAL SPOTS OF SURFACE CORROSION ON AIRCRAFT BELLY SKIN BETWEEN LBL 29.06 AND RBL 29.06 FS 290.50 AND 326.00. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED NEW SKIN PANEL FROM IAW FAA APPROVED DATA CONTAINED IN FIELD REPAISep 16, 2007 · N81536 · Beech 1900D · Fuselage Main, Plate/SkinSDR BSAASDR0724Shutoff Valve · inoperativeDURING CLIMB THE LEFT ENVIROMENTAL FAIL LIGHT ILLUMINATED AND WOULD NOT RESET. UPON RETURN TO BOSTON THE DISCREPANCY WAS INITIALLY DEFERRED. AFTER RETURN TO BOSTON THE RT PRESSURE REGULATING SHUT OFF VALVE WAS REMOVED AND REPLACED. GROUND CHECK GOOD.Sep 16, 2007 · N171ZV · Beech 1900D · Air Distribution SystemSDR GUUA09130701Wire · chafedDURING FLIGHT LANDING GEAR LIGHTS FLICKER WITH LIGHT INOPERATIVE IN FLIGHT. REPAIRED CHAFED WIRE UNDER AIRSTAIR DOOR. OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY.Sep 13, 2007 · N190YV · Beech 1900D · Landing Gear System WiringSDR GUUA09130702Handle · failedDURING APPROACH LANDING GEAR DID NOT EXTEND ON THE FIRST AND SECOND SELECTION OF THE GEAR SELECTOR KNOB TO THE DOWN POSITION. RETURNED TO FLL LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR HANDLE. OPERATIONAL CHECK NORMAL.Sep 13, 2007 · N69549 · Beech 1900D · Landing Gear SelectorSDR GUUA09120701Hinge Bracket · corrodedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT OB ELEVATOR HINGE BRACKET HAS CORROSION. REPLACED LT OB ELEVATOR HINGE BRACKET.Sep 12, 2007 · N87552 · Beech 1900D · Elevator StructureSDR GLBA20060994Keel · crackedLT WHEEL WELL KEEL CRACKED APPROXIMATELY .5 INCH FORWARD OF LT MAIN LANDING GEAR MOUNT. MAINTENANCE REPAIRED FLANGE CRACK ON L/H INBOARD KEEL RIB I.A.W. E.O. 07-UE251-01. REPAIR DIMENSION 4 3/4" BY 3 1/2". 7075-T7351. RII INSPECTION COMPLIED WITH PER TASKCARSep 11, 2007 · N251GL · Beech 1900D · Fuselage Main, KeelSDR GLBA20060999Skin · crackedROW 6A, CABIN WINDOW INNER SKIN CRACKED AT THE LOWER FORWARD CORNER. MAINTENANCE REMOVED AND REPLACED SKIN ON EMERGENCY EXIT WINDOW 6A IAW. SRM 51-40. P/N NR 129-430045-21. RII INSPECTION COMPLIED IAW TASKCARD 8.2.1.Sep 11, 2007 · N251GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20060998Angle · crackedLT HEAVY ANGLE CRACKED APPROXIMATELY 1.6 INCHES AT F.S. 288.0 TO 289.6. MAINTENANCE REPAIRED LT HEAVY ANGLE IAW SRM 53-90. REPAIR LENGTH 13.5 INCHES. PN 114-430002-7179. AT FS 288 TO FS 301.5. RII INSPECTION COMPLIED WITH IAW TASKCARD 8.2.1.Sep 11, 2007 · N251GL · Beech 1900D · Fuselage Main, StructureSDR GLBA20060997Door Frame · crackedAIRSTAIR DOOR FRAME ANGLE CRACKED AT FS 150.6.AND APPROXIMATELY 3 INCHES ABOVE STRINGER 10L. CRACK APPROXIMATELY 1.3 INCHES. MAINTENANCE INSTALLED REPAIR INSERT AND REINFORCED ANGLE IAW SRM 53-90-28. ANGLE PART NR 129-420034-3. INSERT 2 INCHES, ANGLE 10 INCSep 11, 2007 · N251GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA20060996Frame · crackedFUSELAGE FRAME CRACKED AT FS 163.9 AT STRINGER 9AR APPROXIMATELY 1.2 INCHES IN LENGTH. MAINTENANCE REPAIRED FUSELAGE FRAME AT STRINGER RELIEF HOLE AT FS 163.9 AT STRINGER 9R IAW SRM 51-70. REPAIR APPROXIMATELY 6.5 INCHES BY 2.5 INCHES. 2024 T-3. .080. RII INSep 11, 2007 · N251GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20060995Frame · crackedFUSELAGE FRAME CRACKED AT F.S. 177.3 AT STRINGER 9AR APPROXIMATELY 1.1 INCH IN LENGTH. MAINTENANCE REPAIRED FUSELAGE FRAME CRACK AT STRINGER RELIEF HOLE AT FS 177.3 STRINGER 9R IAW SRM 51-70. REPAIR DIMENSIONS APPROX 5 INCH BY 2.5 INCH, 2024 T-3 .080. RII INSPSep 11, 2007 · N251GL · Beech 1900D · Fuselage Main, FrameSDR GUUA09110702Relay · failedAFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. REPLACED MLG RELAY, COULD NOT DUPLICATE OPERATIONAL CHECK NORMAL.Sep 11, 2007 · N69549 · Beech 1900D · Landing Gear Position and WarningSDR GUUA09110701Actuator · malfunctionedDURING FLIGHT LANDING GEAR INTRANSIT LIGHT ILLUMINATED. REPLACED LT MLG ACTUATOR. OPERATIONAL CHECK NORMAL.Sep 11, 2007 · N81546 · Beech 1900D · Landing Gear ActuatorSDR AMWA87352Indication Sys · smokeON TAXI OUT CAPT NOTED SMOKE AND ELECTRICAL ODOR WHICH APPEARED TO BE COMING FROM CAPT'S EFIS SYSTEM. CREW DECIDED TO RETURN TO GATE WITH NO FURTHER INCIDENT. CND ON GROUND, SYSTEM OPS CHECKS NORMAL. REMOVED AND REPLACED CAPT EFIS SCREEN FOR PRECAUTIONARY MSep 11, 2007 · N155ZV · Beech 1900D · Flight Environment Data
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