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 GUUA10130801Dampener · crackedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED AIRSTAIR DOOR COUNTER BALANCE SUPPORT ASSEMBLY DAMPENER CRACK. REPLACED AIRSTAIR DOOR COUNTER BALANCE UPPER SUPPORT ASSEMBLY DAMPENER.Oct 13, 2008 · N69549 · Beech 1900D · Passenger/Crew DoorsSDR GUUA10100803Lock · lack of lubeAT SCHEDULED ROUTINE MAINT, DISCOVERED RT AFT EMERGENCY EXIT FROZEN AND WILL NOT OPEN, APPLIED LUBRICANT TO RT AFT EMERGENCY EXIT LOCKING ASSY. OPERATIONAL CHECK NORMAL.Oct 10, 2008 · N69549 · Beech 1900D · Emergency ExitsSDR GUUA10100802Lock · lack of lubeAT SCHEDULED ROUTINE MAINT DISCOVERED LT AFT EMERGENCY EXIT FROZEN AND WILL NOT OPEN. APPLIED LUBRICANT TO LT AFT EMERGENCY EXIT LOCKING ASSY. OPS CHECK NORMAL.Oct 10, 2008 · N69549 · Beech 1900D · Emergency ExitsSDR GUUA10100801Door · stiffPILOT REPORTED CABIN DOOR HARD TO CLOSE. CLEANED AND LUBRICATED AIRSTAIR DOOR LOCKING CAMS AND ADJUSTED DOOR SUPPORT CABLES. OPS CHECK GOOD.Oct 10, 2008 · N81556 · Beech 1900D · Entrance StairsSDR CA081016011Torque Tube · broken(CAN) RUDDER PEDALS LINKAGE (UNDER FLOOR) - LT TORQUE TUBE BROKEN JUST INBD OF THE LT RUDDER PEDAL BLOCK. RUDDER TORQUE TUBE FAILURE STARTED AT TAPER PIN HOLE USED TO SECURE THE RUDDER PEDAL ASSY BLOCK TO THE SHAFT. FAILURE APPEARS TO BE FROM AN OVERLOAD CONDIOct 10, 2008 · Beech 1900D · Rudder Control SystemSDR GUUA10090801R1Actuator · crackedFLIGHT 9159 TPA/VPS - PILOT REPORTED POST FLIGHT FOUND HYD LEAK NOSE GEAR ACTUATOR AREA. REPLACED NOSE GEAR ACTUATOR.Oct 9, 2008 · N81536 · Beech 1900D · Landing Gear ActuatorSDR GUUA10090801Actuator · crackedFLIGHT 9159 TPA/VPS - PILOT REPORTED POST FLIGHT INSPECTION FOUND HYD LEAK NOSE GEAR ACTUATOR AREA. REPLACED NOSE GEAR ACTUATOR.Oct 9, 2008 · N81536 · Beech 1900D · Landing Gear ActuatorSDR NSVA2008036Powerpack · faultyON ILS TO 22L (BOS) PUT THE LANDING GEAR DOWN AND GOT A WARNING INDICATION HAD TO INITIATE A GO-AROUND AND PERFORM ABNORMAL GEAR EXT. INSTALLED HYD POWER PACK LANDING GEAR MOTOR RELAY AND NEW LANDING GEAR POWER CB AND REINSTALLED CB IAW BEECH 1900D 24-00-00. Oct 9, 2008 · N171CJ · Beech 1900D · Hydraulic Pump (Electric/Engine), MainSDR GUUA10050801Socket · dirtyFLIGHT 9166 - NAS/FLL - PILOT REPORTED LANDING GEAR ANNUNCIATOR GREEN "L" DOESN'T ILLUMINATE WITH GEAR DOWN. CLEANED ANNUNCIATOR LIGHT SOCKET.Oct 5, 2008 · N81536 · Beech 1900D · Landing Gear Position and WarningSDR GUUA10040802Motor · sluggishFLIGHT 9126 - NAS/FLL - PILOT REPORTED GEAR RETRACTION TOOK 14 SECONDS. REMOVED AND REPLACED HYDRAULIC MOTOR.Oct 4, 2008 · N87557 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GUUA10040801Motor · malfunctionedFLIGHT 9126 - NAS/FLL - AFTER TAKEOFF LANDING GEAR RETRACTION TOOK 14 SECONDS. REPLACED HYDRAULIC MOTOR. OPERATIONAL CHECK NORMAL.Oct 4, 2008 · N87557 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GUU2008F00056Cable Assy · brokenFLIGHT 9146 - TPA/MIA - PILOT REPORTED FORWARD DOOR CAMLOCKS STUCK. DOOR WOULD NOT OPEN FROM INSIDE OR OUTSIDE. REPLACED FORWARD AIRSTAIR DOOR UPPER FORWARD CABLE ASSEMBLY.Oct 4, 2008 · N49543 · Beech 1900D · Passenger/Crew DoorsSDR GUUA10030802Structure · crackedAT SCHEDULED INSPECTION DISCOVERED A .5 INCH CRACK LEFT AIRCRAFT FUSELAGE BELLY LBL 29.06. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER BEECH STRUCTURAL REPAIR MANUAL 53-90-18.Oct 3, 2008 · N81546 · Beech 1900D · Fuselage Miscellaneous StructureSDR GUUA10030801Structure · crackedAT SCHEDULED INSPECTION DISCOVERED A .5 INCH CRACK RIGHT AIRCRAFT FUSELAGE BELLY RBL 29.06. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER BEECH STRUCTURAL REPAIR MANUAL 53-90-18.Oct 3, 2008 · N81546 · Beech 1900D · Fuselage Miscellaneous StructureSDR CA081022010Drive Assy · sheared(CAN) ON APPROACH THE FLAPS WERE SELECTED TO 17 DEG BUT FAILED TO EXTEND PAST 10 DEG. THE FLIGHT CREW INITIATED AN OVERSHOOT TO TROUBLESHOOT THE PROBLEM, THEY WERE UNABLE TO FIX THE BROKEN FLAPS AND RETURNED TO BASE. MX REPLACED THE FLAP DRIVE AND NO FURTHER FOct 2, 2008 · Beech 1900D · Trailing Edge Flap ActuatorSDR GUUA10020801Annunciator · looseFLIGHT - 9236 - EYW/TPA - PILOT REPORTED "H H" LANDING GEAR POSITION INDICATORS INTERMITTENT. RESET AND RE-SECURED H H ANNUNCIATOR SOCKET ASSEMBLIES.Oct 2, 2008 · N82539 · Beech 1900D · Landing Gear Position and WarningSDR CA081021001Bolt · loose(CAN) BOLT WAS FOUND LOOSE ON RT SIDE OF NLG. THE COTTER PIN AND NUT WERE MISSING.Oct 1, 2008 · Beech 1900D · Nose/Tail Landing GearSDR CA081014007Bearing · failed(CAN) LT MLG OTBD MAIN WHEEL ASSY BECAME DETACHED FROM THE AXLE ASSY, ONLY BEING HELD ON BY THE OUTER MAIN WHEEL AXLE NUT AND BRG CONE. INITIAL INVESTIGATION CONFIRMED THAT THIS WAS THE RESULT OF AN EXTREME BEARING FAILURE. FAILURE WAS TO SUCH EXTENT THAT IT Oct 1, 2008 · Beech 1900D · Wheel/Ski/FloatSDR GUUA09300802Keelbeam · crackedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT NACELLE INBOARD KEEL HAS .75 INCH CRACK FORWARD AND ABOVE LANDING GEAR BOLT. REMOVED AND REPLACED INBOARD KEEL.Sep 30, 2008 · N81546 · Beech 1900D · Nacelle/Pylon, Main FrameSDR GUU2008F00058Hinge Bracket · corrodedDURING SCHEDULED ROUTINE MX DISCOVERED LT ELEVATOR OTBD HINGE BRACKET CORRODED. REPLACED LT OTBD ELEVATOR HINGE BRACKET.Sep 30, 2008 · N87557 · Beech 1900D · Elevator StructureSDR GUUA93653092908ASkin · corrodedDURING SCHEDULED ROUTINE MX DISCOVERED EXFOLIATION AT THE LOWER FUSELAGE SKIN AT FS 438.250 STRINGER 16. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED AN EXTERNAL REPAIR DOUBLER.Sep 29, 2008 · N81536 · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA09270801Skin · corrodedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT OUTBOARD WING UPPER SKIN TRAILING EDGE HAD CORROSION AND DEBOND BETWEEN WS 121 THROUGH 194.85. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED AN EXTERNAL REPAIR DOUBLER.Sep 27, 2008 · N81546 · Beech 1900D · Wing, Plate/SkinSDR GUU2008F00054Cable Assy · defectiveFLIGHT 9208 TPA/PNS PILOT DISCREPANCY. PILOT REPORTED UNABLE TO OPEN MAIN CABIN DOOR. C/A REPLACED UPPER AFT AIRSTAIR DOOR CABLE. OPS CHECK GOOD.Sep 27, 2008 · N87552 · Beech 1900D · Passenger/Crew DoorsSDR GUU2008F00055Relay · failedFLIGHT 9132 MIA/TPA PILOT DISCREPANCY. DURING APPROACH WHEN LANDING GEAR CONTROL SELECTED DOWN CIRCUIT BREAKER POPPED. HAD TO RESET SEVERAL TIMES BEFORE ALL GEAR CAME DOWN AND LOCKED 3 GREEN. C/A REPLACED LANDING GEAR RELAY. OPS CHECK NORMAL. TEST FLIGHT Sep 24, 2008 · N69549 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GUU2008F00053Warning System · malfunctionedFLIGHT 99184 FLL/EYW PILOT DISCREPANCY. DURING APPROACH FLAPS AT 35 DEGREE SELECTION, LANDING GEAR UNSAFE LIGHT ILLUMINATED WITH 3 GREEN DOWN AND LOCKED LIGHT. CONTINUED TO EYW AND LANDED WITHOUT INCIDENT. C/A CHECKED SECURITY OF LANDING GEARS AND SWITCHES Sep 24, 2008 · N87552 · Beech 1900D · Landing Gear Position and WarningSDR GLB2008F00028Skin · crackedMAJOR REPAIR CONFORMITY CHECK OF REPAIR ABOVE AIRSTAIR DOOR PERFORMED. MX FOUND STOP DRILLED CRACKS AROUND 2 RIVETS BOTH 1.25 FROM LT AND RT CENTERLINE OF STRINGER 1 AT 163.975. MX REMOVED OLD PATCH, REMOVED DAMAGED AREAS BY CUTTING OUT .75" SKIN IN BOTH ARESep 24, 2008 · N100UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GUU2008F00052Circuit Breaker · poppedFLIGHT 9130 FPO/FLL PILOT DISCREPANCY DURING APPROACH, WHEN LANDING GEAR HANDLE SELECTED DOWN THE LANDING GEAR CIRCUIT BREAKER POPPED. RESET THE CIRCUIT BREAKER AND THE LANDING GEAR EXTENDED NORMALLY. C/A TROUBLE SHOT LANDING GEAR SYSTEM. NO DEFECTS NOTED. Sep 21, 2008 · N69549 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLB2008F00030Spar · damagedMAJOR REPAIR FOR CONFORMITY REPLACEMENT REQUESTED OF HORIZONTAL STABILIZER MAIN SPAR CENTER WEB REPAIR. PRIOR REPAIR DOES NOT CONFORM TO SRM DATA. MX REPLACED THE MAIN SPAR CENTER WEB REPAIR IAW BEECH 1900D SRM 55-91. REPAIR APPROXIMATELY 5.75" BY 4.75" OUTSep 19, 2008 · N122UX · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLB2008F00029Stabilizer · damagedMAJOR REPAIR ACFT 122UX WHILE TAXIING THE ACFT TO THE GATE THE PILOTS STRUCK A JETWAY WITH THE TAIL OF THE ACFT DAMAGING THE VERTICAL AND HORIZONTAL STABILIZERS. THE STABILIZER WAS DAMAGED AND TWISTED TO THE LT FROM VERTICAL STABILIZER POSITION CSS 39.289 TO Sep 19, 2008 · N122UX · Beech 1900D · Horizontal Stabilizer StructureSDR GLB2008F00027Stabilizer · damagedMAJOR REPAIR ACFT N122UX WHILE TAXIING THE ACFT TO THE GATE THE PILOTS STRUCK A JETWAY WITH THE TAIL OF THE ACFT DAMAGING THE VERTICAL AND HORIZONTAL STABILIZERS. THE VERTICAL STABILIZER WAS DAMAGED AND TWISTED TO THE LT FROM VERTICAL STABILIZER POSITION CSS Sep 19, 2008 · N122UX · Beech 1900D · Vertical StabilizerSDR GUU2008F00057Handle · out of adjustFLIGHT PBI ASD DURING PREFLIGHT PILOT REPORTED RT EMERGENCY EXIT EXTERIOR HANDLE SUNK IN. PROPERLY ADJUSTED RT REAR EMERGENCY EXIT INTERNAL MECHANISM.Sep 15, 2008 · N45AR · Beech 1900D · Entrance StairsSDR GUU2008F00065Wire · out of positionAFTER TAKEOFF UPON TURNING BOTH LANDING LIGHTS SWITCHES OFF THERE WAS A SPARK COMING OUT OF THE SWITCH. SPLICED AND REPOSITIONED WIRE AT LT LANDING LIGHT SWITCH. OPS CHECK GOOD. (K)Sep 14, 2008 · N87551 · Beech 1900D · Light System WiringSDR GUU2008F00062Door · lack of lubeDURING SCHEDULED ROUTINE MAINT DISCOVERED SEAT 6F EMERGENCY EXIT HARD TO OPEN. LUBED EMERGENCY EXIT. OPS CHECK GOOD. (K)Sep 14, 2008 · N87551 · Beech 1900D · Emergency ExitsSDR GUU2008F00064Unknown · odorDURING APPROACH VERY STRONG ODOR COMING FROM CABIN VENTS REGARDLESS OF MODE CONTROL SETTING. RAN ENGINES FOR 30 MINUTES AT ALL POWER SETTINGS AND MODE CONTROL SETTINGS NO ODOR NOTED. (K)Sep 10, 2008 · N87550 · Beech 1900D · Air Distribution SystemSDR GUU2008F00049Door · out of adjustDURING SCHEDULED ROUTINE MAINT, DISCOVERED LT EMERGENCY EXIT DOOR DOES NOT CLOSE PROPERLY. READJUSTED LT EMERGENCY EXIT DOOR. (K)Sep 10, 2008 · N53545 · Beech 1900D · Emergency ExitsSDR GUU2008F00048Unknown · odorDURING FINAL APPROACH BOTH PILOTS OBSERVED BURNING ODOR. INSPECTED COCKPIT INSTRUMENTS NO DEFECTS NOTED, PERFORMED OPERATIONAL CHECK OF ENVIRONMENTAL SYSTEM COULD NOT DUPLICATE. (K)Sep 9, 2008 · N87550 · Beech 1900D · Air Distribution SystemSDR GLB2008F00023B-Nut · loosePILOTS REPORTED IN CRUISE AND DESCENT A STRONG FUEL ODOR IN THE COCKPIT AND CABIN AREA. MAINTENANCE TIGHTENED A LOOSE "B" NUT IN THE FUEL PURGE AREA ON THE NR (1) ENGINE IAW MM 28-20. CLEANED CHECK VALVES ON THE FUEL PURGE SYSTEMS FOR THE RT ENGINE AND LT ENGSep 4, 2008 · N219GL · Beech 1900D · Engine Fuel DistributionSDR NSV2008F00024Seal · brokenACFT OVER SCUPP AT 12,000 FEET THE PAX DOOR SEAL BROKE. THE CREW DECLARED AN EMERGENCY AND DESCENDED BELOW 10,000 FEET. THE ACFT LANDED WITHOUT INCIDENT IN BOSTONSep 4, 2008 · N191CJ · Beech 1900D · Passenger/Crew DoorsSDR GLB2008F00026Stiffener · crackedDURING STRUCTURAL CHECK MAINT DISCOVERED A CRACK ON THE RT WHEEL WELL OB KEEL TAB TO OB FENDER STIFFENER 1" AT THE BOTTOM END OF STIFFENERS TO KEEL AREA. " SUPPLEMENTAL INFORMATION WILL BE PROVIDED UPON COMPLETION OF THE REPAIR". (K)Sep 3, 2008 · N211GL · Beech 1900D · Fuselage Miscellaneous StructureSDR GLB2008F00031Motor · burnedPILOTS REPORTED A STRONG ODOR OF SMOKE WITH EYE IRRITATION PRESENT ON TAXI. TURNING OFF BLEEDS TO ENVIRO OFF AS WELL AS TURNING OFF MODE CONTROL, DID NOT CHANGE ODOR . THERE WAS NO VISIBLE SMOKE. MAINT TROUBLESHOT AND FOUND THE SMOKE ODOR TO BE A FLAP MOTOR THSep 2, 2008 · N100UX · Beech 1900D · Trailing Edge Flap Control SystemSDR GLB2008F00025Frame · crackedDURING STRUCTURAL INSPECTION MAINT FOUND FRAME CRACKED AT STRINGER CUTOUT AT FS 164.4 STRINGER 9AR. LENGTH OF CRACK APPROXIMATELY .5". MAINT REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE IAW SRM 51-70 AT FS 164.4 REPAIR APPROXIMATELY 5 INCH BY 2.5 INCH. 2024-T3Sep 2, 2008 · N211GL · Beech 1900D · Fuselage Main, FrameSDR GLB2008F00024Frame · crackedDURING STRUCTURAL INSPECTION MAINTENANCE FOUND FRAME CRACKED AT STRINGER CUTOUT FS 177.3 AT STRINGER 9AR. LENGTH OF CRACK APPROXIMATELY .750". MAINTENANCE REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE IAW SRM 51-70 AT FS 177.3 AT STRINGER 9AR. REPAIR APPROXIMASep 2, 2008 · N211GL · Beech 1900D · Fuselage Main, FrameSDR GLB2008F00020Frame · crackedDURING STRUCTURAL INSP MAINT FOUND FRAME CRACKED AT STRINGER CUTOUT FS 177.3 AT STRINGER 9AR. LENGTH OF CRACK APPROXIMATELY .750. (K)Sep 2, 2008 · N211GL · Beech 1900D · Fuselage Main, FrameSDR GLB2008F00019Frame · crackedDURING STRUCTURAL INSPECTION MAINT FOUND FRAME CRACKED AT STRINGER CUTOUT AT FS 164.4 STRINGER 9AR. LENGTH OF CRACK APPROXIMATELY .5 INCH. OPEN (K)Sep 2, 2008 · N211GL · Beech 1900D · Fuselage Main, FrameSDR GUU2008F00051Brake Assy · malfunctionedPILOT REPORTED NO BRAKES AND NO STEERING AT THE END OF LANDING ROLL. PERFORMED PRESSURE POT BLEEDING OF BRAKE SYSTEM. OPERATIONAL CHECK OF BRAKES AND STEERING NORMAL. (K)Aug 31, 2008 · N81533 · Beech 1900D · Landing Gear Brake SystemSDR GLB2008F00018Switch · out of adjustSUSPECTED AUTOFEATHER EVENT. DURING CRUISE, THE PILOTS REPORTED THAT THE LT AUTOFEATHER DISARMED IN FLIGHT AND NEVER REARMED AT ANY POWER SETTING. MAIT ADJUSTED THE LT POWER LEVER SWITCH. OPS CHECK OF THE AUTOFEATHER SYS GOOD IAW MM 61-20-00. (K)Aug 28, 2008 · N881SK · Beech 1900D · Propeller Feathering/ReversingSDR GLB2008F00021Connector · looseSUSPECTED AUTOFEATHER EVENT, UPON APPROACH, PILOTS REPORTED THAT RT AUTOFEATHER ACTUATED (AS IT NORMALLY DOES DURING TESTING) ON APPROACH AFTER A MINOR POWER INCREASE. MAINT REMOVED AND REPLACED THE OVERSPEED GOVERNOR IAW MM 61-20. OPS CHECK WAS GOOD, HOWEVERAug 26, 2008 · N211GL · Beech 1900D · Propeller GovernorSDR GUU2008F00047Cable · brokenPILOT REPORTED UNABLE TO OPEN CABIN DOOR, FOUND UPPER FWD DOOR CABLE BROKEN. REPLACED UPPER FWD DOOR CABLE. (K)Aug 26, 2008 · N87554 · Beech 1900D · Passenger/Crew DoorsSDR GUU2008F00045Cable · brokenPILOT REPORTED UNABLE TO OPEN CABIN DOOR, FOUND UPPER FWD DOOR CABLE BROKEN. REPLACED UPPER FWD DOOR CABLE. (K)Aug 26, 2008 · N87554 · Beech 1900D · Passenger/Crew DoorsSDR GUU2008F00046Cam · obstructedCABIN DOOR RT SIDE SECOND CAM FROM TOP IS RUBBING ON CAM LOCK MAKING DOOR HARD TO OPEN AND CLOSE. CLEANED EXCESSIVE GREASE AND GUM OUT OF CAM. (K)Aug 25, 2008 · N87557 · Beech 1900D · Passenger/Crew Doors
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