Beech 1900D

Service difficulty reports · 7,152

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Query with SQL
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 GLBA2012080800029Elevator · damagedDURING A SCHEDULED ROUTINE INSPECTION FOUND THE LT ELEVATOR HAS DAMAGE ON THE T/E, .37" BY .15". REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-27-001. MATERIALS UTILIZED ARE INCLUDED IN THE EO.Aug 8, 2012 · N100UX · Beech 1900D · Elevator Tab Control SystemSDR GLBA2012080700028Spar Cap · crackedDURING A SCHEDULED INSPECTION, FOUND TWO CRACKS IN THE RT SIDE OF THE VERTICAL STAB, RT FWD SPAR CAP ANGLE AT APPROX AREA VSS 84.10, 20 PERCENT. REPAIRED AFFECTED AREA IAW EO 12-1900-55-022. MAJOR REPAIR.Aug 7, 2012 · N100UX · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR 2012FA0000620Resistor · malfunctionedACFT FWD VENT BLOWER ASSY REMOVED BEFORE SCHEDULED MAINTENANCE PERIOD. INTERNAL RESISTORS HAD MALFUNCTIONED CAUSING COMPONENT FAILURE. THE REMOVED AND REPLACEDE BLOWER ASSY.Aug 6, 2012 · N535M · Beech 1900D · Air Conditioning System WiringSDR GLBA2012080600027Spar Cap · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE LT VERTICAL STAB, LT FWD SPAR CAP ANGLE AT APPROX FSS 84.10, 20 PERCENT CHORD VISIBLE, 1.25" IN LENGTH. REPAIRED AFFECTED AREA IAW EO 12-1900-55-021. MAJOR REPAIR.Aug 6, 2012 · N100UX · Beech 1900D · Vertical Stabilizer, Spar/RibSDR NOZR20120807001Ground Wire · chafedRED GPWS ANNUCIATOR FLICKERED INTERMITTENTLY DURING FLIGHT. FOUND THE GROUND WIRE FOR THE ANNUCIATOR LIGHT CHAFE ON A STRINGER ON THE RIGHT SIDE OF THE CABIN AT FLIGHT STATION 330 BELT LINE 0 FLOORBOARD 172AT.Aug 4, 2012 · N29NG · Beech 1900D · Navigation System WiringSDR GLBA2012080300025Stringer · corrodedDURING A SCHEDULED ROUTINE INSPECTION FOUND CORROSION BETWEEN STRINGER 16 AT FS 243.25 AND 258.25, IN A 2.25" AREA. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-042. MATERIALS UTILIZED ARE INCLUDED IN THE EO.Aug 3, 2012 · N100UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2012080300026Rib · crackedDURING A SCHEDULED ROUTINE INSP FOUND A CRACK ON THE LT WING INBD AUX RIB FLANGE & ANGLE AT JUNCTION WITH LT WING FWD WING SPAR AT FS 288, 1.3" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-57-008. MATERIALSAug 3, 2012 · N100UX · Beech 1900D · Wing, Rib/BulkheadSDR 29GA95471080312Truss · crackedDURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS MOUNT WELD AREA CRACKS AND TRUSS TUBE CHAFE. PERFORMED WELD REPAIR TO ENGINE MOUNT ATTACH POINTS WELD AREAS AND ENGINE TRUSS TUBE IN ACCORDANCE WITH FAA APPROVED DATA.Aug 3, 2012 · N87554 · Beech 1900D · Engine Mount SectionSDR GLBA201208030024Skin · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND THE CENTER BELLY SKIN AT FS 303, 2" IB FROM RT EDGE, SKIN CRACKED, 1.25" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-041. MATERIALS UTILIZED ARE INCLUDED IN THAug 2, 2012 · N100UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA201208020023Bulkhead · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND 9 CRACKS IN THE LT LOWER PRESSURE BULKHEAD RADIATING FROM THE DOUBLE ROW OF FASTENERS AT THE INBD EDGE OF THE BULKHEAD, 3" IN LENGTH. REPAIRED AFFECTED AREA IAW EO 12-1900-53-040. MAJOR REPAIR.Aug 2, 2012 · N100UX · Beech 1900D · Fuselage Main, BulkheadSDR GLBA201208020022Bulkhead · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND CRACKS IN THE RT LOWER PRESSURE BULKHEAD RADIATING FROM FASTENERS AT THE INBD EDGE OF THE BULKHEAD, 8 CRACKS, 3.1" IN TOTAL LENGTH. REPAIRED AFFECTED AREA IAW EO 12-1900-53-040. MAJOR REPAIR.Aug 2, 2012 · N100UX · Beech 1900D · Fuselage Main, BulkheadSDR 29GA95757080112Skin · corrodedREPROT: DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RIGHT WING TRAILING EDGE SKIN HAD CORROSION AT WS 159.51. REMOVED CORROSION DAMAGE AND INSTALLED FILLER AND EXTERNAL DOUBLER REPAIR.Aug 1, 2012 · N87557 · Beech 1900D · Wing, Plate/SkinSDR GLBA2012080100021Skin · corrodedDURING A SCHEDULED ROUTINE INSPECTION, FOUND BELLY SKIN CORROSION AT FS 243.25, AT JUNCTION OF FRAME & STRINGER 16, AND AT FS 243.25, AT JUNCTION OF FRAME & STRINGER 15L. REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-039.Aug 1, 2012 · N100UX · Beech 1900D · Fuselage Main, Plate/SkinSDR EHAA20120729005Brake Assy · failedRIGHT BRAKE FAILED ON LANDING. NO PEDAL PRESSURE ON EITHER PILOT'S OR CO-PILOT'S BRAKE PEDAL.Jul 29, 2012 · N171CJ · Beech 1900D · Landing Gear Brake SystemSDR GLBA2012073000020Web · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACKS ON THE HORIZONTAL STAB WEB AT HS 0.00, .125" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW FR-CO-02476. MAJOR REPAIR.Jul 27, 2012 · N192GL · Beech 1900D · Horizontal Stabilizer StructureSDR 29GA95779072512Line · looseFLIGHT:3989 MCO/PNS RIGHT ENGINE WAS LOSING OIL PRESSURE IN FLIGHT SECURED RIGHT ENGINE WITH 50 PSI STILL SHOWING ON THE GAUGE. DIVERTED TO GNV LANDED WITHOUT INCIDENT. SECURED OIL PRESSURE LINE TO TORQUE TRANSMITTER OPERATIONAL CHECK GOOD. NO LEAKS NOTED.Jul 25, 2012 · N87557 · Beech 1900D · Engine Oil Distribution (Airframe Furnished)SDR GLBA2012072500019Fuse · inoperativePILOT REPORTED THAT THE INSTRUMENT EMERGENCY LIGHT IS INOPERATIVE. MX REPLACED THE SYS FUSE, OPS CHECKED GOOD.Jul 24, 2012 · N178YV · Beech 1900D · Emergency LightingSDR 29GA32954072312Warning Horn · inoperativeFLIGHT: 3577 LWT/BIL GEAR WARNING HORN INOPERATIVE DURING DESCENT INTO BIL. GEAR HYDRAULIC PUMP ACTIVATING FREQUENTLY IN FLIGHT. REPLACED AURAL TONE, OPERATIONAL CHECK GOOD.Jul 23, 2012 · N87554 · Beech 1900D · Landing Gear Position and WarningSDR 29GA93952072112Handle · lack of lubeREPORT: DURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT EMERGENCY EXIT OUTER HANDLE DOES NOT SPRING OPEN. LUBRICATED LEFT EMERGENCY EXIT OPERATIONAL CHECK OK.Jul 21, 2012 · N82539 · Beech 1900D · Emergency ExitsSDR 29GA94252072112Cable · inoperativeFLIGHT: 4066 EYW/GNV PILOT REPORTED AIRSTAIR IS NOT CLOSING, INOPERATIVE. REPLACED AIRSTAIR DOOR LOWER FORWARD DOOR CABLE OPERATIONAL CHECK GOOD.Jul 21, 2012 · N47542 · Beech 1900D · Passenger/Crew DoorsSDR GLBA2012072300017Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 4 CRACKS AROUND THE HORZ STAB AFT SPAR WEB AT HSS 0.00, 1.625" IN LENGTH. REPAIRED IAW EO 12-1900-55-019. MAJOR REPAIRJul 21, 2012 · N240GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR 29GA95652071912Link · malfunctionedFLIGHT: 4066 DUJ/FKL PILOT REPORTED AIRSTAIR DOOR HANDLE INOPERATIVE. REPLACED AIRSTAIR DOOR INTERIOR HANDLE LINK ASSEMBLY OPERATIONAL CHECK GOOD.Jul 19, 2012 · N81556 · Beech 1900D · Passenger/Crew DoorsSDR 29GA95352071912Link · malfunctionedFLIGHT: 4066 DUJ/FKL PILOT REPORTED AIRSTAIR DOOR HANDLE INOPERATIVE. REPLACED AIRSTAIR DOOR INTERIOR HANDLE LINK ASSEMBLY OPERATIONAL CHECK GOOD.Jul 19, 2012 · N81556 · Beech 1900D · Passenger/Crew DoorsSDR GLBA2012071900016Pressure Blkhd · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 4 CRACKS IN THE LT LWR FWD PRESSURE BULKHEAD AT THE INBD EDGE DOUBLER ROW OF FASTENERS, 1.1" IN LENGTH. REPAIRED IAW EO 12-1900-53-038. MAJOR REPAIR.Jul 19, 2012 · N169GL · Beech 1900D · Fuselage Main, BulkheadSDR 29GA94153071412Skin · corrodedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED SEVERE CORROSION AT FS 363.25 STRINGER 16. REMOVED DAMAGED SKIN AREA AND STRINGER 16 DAMAGE AND INSTALLED FUSELAGE SKIN DOUBLER REPAIR AND STRINGER 16 REPAIR ANGLE.Jul 14, 2012 · N17541 · Beech 1900D · Fuselage Main, Plate/SkinSDR CA120723006Oil System · low pressure(CAN) DURING FLIGHT, THE NR 2 ENGINE LOST OIL PRESSURE PILOTS SHUTDOWN AND SECURED ENGINE. UNEVENTFUL LANDING. ON GROUND INSPECTION SHOWED LITTLE OR NO OIL IN ENGINE, OIL FILLER CAP IN PLACE, NO SIGNS OF EXTERNAL LEAK AND PROPELLER EXTREMELY DIFFICULT TO TURNJul 12, 2012 · Beech 1900D · Engine Oil Indicating SystemSDR CA120717007Oil System · low pressure(CAN) WHILE CRUISING AT FL 200 WE OBSERVED A MASTER WARNING LIGHT DUE TO THE R OIL PRESS LOW ANNUNCIATOR FLICKERING. THE R OIL PRESSURE GAUGE WAS BOUNCING AROUND FROM 55-70PSI AND AT THIS POINT ALL OTHER ENGINE INDICATIONS WERE NORMAL. WE WERE NOT ABLE TO CANCJul 12, 2012 · Beech 1900D · Engine Oil Indicating SystemSDR 29GA94032070712APowerpack · defectiveFLIGHT: 3979 PNS/PNS AFTER TAKEOFF LANDING GEAR DID NOT RETRACT. REPLACED HYDRAULIC POWER PACK, OPERATIONAL CHECK SATISFACTORY.Jul 7, 2012 · N16540 · Beech 1900D · Hydraulic Pump (Electric/Engine), MainSDR GLBA2012070900013Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 4 .125" CRACK ON THE HORIZONTAL STAB AFT SPAR WEB BETWEEN LT HSS 5.000 AND RT HSS 5.000. REPAIRED IAW EO 12-1900-55-018.Jul 7, 2012 · N219GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA2012070500011Rib · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE RIB ON LT INBD WING, INBD RT AT BL 29.06 AND FS 288.00, 2" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-57-005.Jul 5, 2012 · N220GL · Beech 1900D · Wing, Rib/BulkheadSDR GLBA2012070500010Rib · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE LT INBD WING AUX RIB AT WS 29.00 AND FS 288, 1.1" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-57-006.Jul 5, 2012 · N153GL · Beech 1900D · Wing, Rib/BulkheadSDR GLBA2012070500009Spar · chafedDURING A SCHEDULED ROUTINE INSPECTION, FOUND THE SPAR CHAFED AT LT INBD WING LWR FWD AREA, .02380 DEEP. REPAIRED THE AFFECTED AREA IAW EO 12-1900-57-007.Jul 5, 2012 · N220GL · Beech 1900D · Wing SparSDR A8OA201207100001Pcb · failedNR 1 PROPELLER ATTEMPTED TO FEATHER IN FLIGHT WITH AUTOFEATHER ARMED. TROUBLESHOT AND FOUND 2 BAD DIODES ON PCBA123. REPLACED DEFECTIVE PC BOARD WITH INSPECTED UNIT. OPS CHECKED GOOD. NO FURTHER OCCURRENCES.Jul 3, 2012 · N60MJ · Beech 1900D · Propeller Feathering/ReversingSDR 29GA94153062912Skin · wrinkledDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED BELLY SKIN WRINKLE AT BEACON LOCATION.Jun 29, 2012 · N17541 · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA201206271Bulb · inoperativeEMERGENCY LIGHT BULB INOPERATIVE. REPLACED BULB, IAW AIM 12-22-0, OPS CHECKED GOOD.Jun 27, 2012 · N192GL · Beech 1900D · Emergency LightingSDR 29GA93732062712Indication Sys · intermittentFLIGHT 3574 BIL/MLS NOSE WHEEL DID NOT GIVE DOWN AND LOCKED INDICATION UPON NORMAL EXTENSION ATTEMPTED EXTENSION A SECOND TIME AND WAS SUCCESSFUL. CYCLED GEAR FIVE TIMES NO FAILURES. REMOVED AND REPLACED GREEN GEAR INDICATION BLOCK CYCLED GEAR FIVE MORE TIMEJun 27, 2012 · N38537 · Beech 1900D · Landing Gear Position and WarningSDR GLBA2012062700007Skin · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND THE SKIN CRACKED IN THE UPPER CABIN FUSELAGE AT FS 273.25, BETWEEN STRINGER 1 AND 2R, CRACK IS ALONG A ROW OF FASTENERS, 3.65" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO12-1900-53-037.Jun 27, 2012 · N153GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2012062600006Skin · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND THE SKIN CRACKED AT THE EMERGENCY EXIT DOOR 6C SKIN AT THE LWR AFT CORNER, 2" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-52-001.Jun 26, 2012 · N153GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2012062600005Skin · crackedDURING A SCHEDULED ROUTINE INSP, FOUND A CRACK IN THE BELLY SKIN AT FS 303, IB 2.5" FROM SKIN EDGE, 4.25" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-036.Jun 26, 2012 · N153GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2012062500002Door Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE UPPER CARGO DOOR FRAME ON THE FWD SIDE AT APPROX FS 459, 3" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-033. MATERIALS UTILIZED ARE INCLUDED INJun 25, 2012 · N153GL · Beech 1900D · Fuselage Main, StructureSDR GLBA201206261Door · unlatchedEMERGENCY EXIT AT SEAT 6A UNLATCHED. MX REMOVED, INSPECTED AND RESECURED EXIT DOOR IAW BMM 52-20-00, OK FOR SERVICE.Jun 25, 2012 · N253GL · Beech 1900D · Emergency ExitsSDR GLBA201206250004Pressure Blkhd · crackedDURING A SCHEDULED ROUTINE INSP, FOUND A CRACK IN THE FWD LWR LT PRESSURE BULKHEAD AT FS 84, 2" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-034.Jun 25, 2012 · N153GL · Beech 1900D · Fuselage Main, BulkheadSDR GLBA2012062500003Bulkhead · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FWD LWR RT PRESSURE BULKHEAD AT FS 84, 1" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-035.Jun 25, 2012 · N153GL · Beech 1900D · Fuselage Main, BulkheadSDR GLBA2012062500001Door Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE UPPER CARGO DOOR FRAME ON THE FWD SIDE AT APPROX FS 459, 3" IN LENGTH.Jun 25, 2012 · N153GL · Beech 1900D · Fuselage Main, StructureSDR 29GA93932062212Control Handle · faultyFLIGHT: 4037 FLL/FLL AFTER TAKEOFF AND WITH LANDING GEAR UP THE THREE GREEN LIGHTS WERE ILLUMINATED. RETURNED TO FLL LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR HANDLE, OPERATIONAL CHECK NORMAL.Jun 22, 2012 · N82539 · Beech 1900D · Landing Gear SelectorSDR GLBA2012061900001Web · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE HORIZONTAL STAB AFT WEB AT HSS 0.00, 2" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-017.Jun 19, 2012 · N154GL · Beech 1900D · Horizontal Stabilizer StructureSDR GLBA2012061801Web · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE HORIZONTAL STAB AFT WEB AT HSS 0.00 IN THE LIGHTNING HOLE AT 2 O'CLOCK POSITION LOOKING FWD, .125" IN LENGTH. REPAIRED AFFECTED AREA IAW EO 12-1900-55-016. MAJOR REPAIR.Jun 16, 2012 · N100UX · Beech 1900D · Horizontal Stabilizer StructureSDR 29GA94953061512Skin · corrodedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED FUSELAGE SKIN CORROSION AT STRINGER 15L AND 15R FS 408.25 TO FS 456.00. REMOVED DAMAGED AREA BETWEEN STRINGER 15R AND STRINGER 16 AT FS 423.25 AND INSTALLED REPAIR FILLER AND EXTERNAL DOUBLER REPAIR.Jun 15, 2012 · N69549 · Beech 1900D · Fuselage Main, Plate/SkinSDR 29GA95132061512AAnnunciator · defectiveFLIGHT: 3983 TPA/PNS NOSE GEAR ANNUNCIATOR FLICKERS WITH THE LANDING GEAR IN THE DOWN POSITION. REPLACED THE LANDING GEAR ANNUNCIATOR ASSEMBLY OPERATIONAL CHECK GOOD.Jun 15, 2012 · N87551 · Beech 1900D · Landing Gear Position and WarningSDR 2012FA0000618Resistor · failedACFT FWD VENT BLOWER ASSY WAS REPLACED BEFORE SCHEDULED MAINT PERIOD. INTERNAL MALFUNCTION OF THE VENT BLOWER ASEMBLIES RESISTORS FOUND TO BE PROBLEM OF COMPONENT FAILURE. REMOVAL AND REPLACEDMENT OF VENT BLOWER ASSY WAS THE COURSE OF ACTION TO BE TAKEN DUE Jun 14, 2012 · N535M · Beech 1900D · Air Distribution Fan
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