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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR GLBA2014121700481Frame · crackedDURING A SCHEDULED INSPECTION, FOUND THREE CRACKS IN THE CARGO DOOR FUSELAGE FRAME AT BS 509.50 BETWEEN STRINGERS 4 - 5L IN THE BEND RADIUS OF THE FRAME, TWO INCHES IN TOTAL LENGTH. REPAIRED IAW EO 14-1900-53-057.SDR GLBA2014121700482Frame · crackedDURING A SCHEDULED INSPECTION FOUND A CRACK IN THE CARGO DOOR FUSELAGE FRAME AT BS 509.5 & STRINGER 11L, .75 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-057.SDR CA141218021Fastener · sheared(CAN) DURING ABC STRUCTURAL INSPECTION CHECK MAINTENANCE NOTICED A SHEARED FASTENER AT LH FRAME STA 288 FWD SPAR BOX SECTION. RECTIFICATION: REPAIRED IAW FR-CO-103576. REMAINDER OF SHEARED FASTENER REMOVED. NDT (EDDY CURRENT) CARRIED OUT TO ENSURE NO FURTHESDR GLBA2014121500478Bulkhead · crackedMAJOR REPAIR DURING A SCHEDULED INSPECTION MAINTENANCE FOUND CRACK IN THE CANT BULKHEAD FLANGE AT FS 588.10 & BETWEEN STRINGER 8R & 7R, 1.5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-055.SDR GLBA2014121500479Frame · crackedMAJOR REPAIR DURING A SCHEDULED INSPECTION MAINTENANCE FOUND CRACK IN THE FUSELAGE FRAME IN THE FLANGE BEND RADIUS AT FS 177.35 BETWEEN STRINGERS 12L & 13L, 1.1 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-SDR CA141215009Tire · damaged(CAN) DURING A ROUTINE INSPECTION MAINTENANCE NOTED A LARGE GASH/DISBOND ON THE NR 3 TIRE. THE REMAINING TIRES WERE INSPECTED WITH NO DEFECTS NOTED. THE TIRE WAS CHANGED AND THE AIRCRAFT RELEASED FOR SERVICE. THE SUBJECT TIRE IS A GOODYEAR FLIGHT CUSTOM III (8SDR CA141217011Circuit Board · faulty(CAN) ON APPROACH THE CREW SELECTED THE GEAR DOWN WITH NO NOSE GEAR DOWN INDICATION EVIDENT. THE LANDING WAS ABORTED AND A GO AROUND WAS EXECUTED. THE GEAR WAS SELECTED TO THE UP POSITION WITH THE RED IN-TRANSIT LIGHT FLASHING INTERMITTENTLY. THE CREW CARRIED SDR CA141212005Spar Cap · cracked(CAN) FINDING LEFT & RIGHT VERTICAL STABILIZER FORWARD SPAR CAP ANGLES FOUND CRACKED AT UPPER FASTENER AREA. RECTIFICATION: REPAIRED IAW FR-CO-103556. LEFT & RIGHT SPAR REPAIRS CARRIED OUT. UPPER PORTIONS OF SPAR CAPS CUT AWAY TO REMOVE DAMAGE. INSERTION RSDR CA150217009Spar · corroded(CAN) DURING INSPECTION MAINTENANCE FOUND CORROSION ON THE FWD FACE OF THE MAIN SPAR (STRINGER 15R & 16). MANUFACTURER WAS CONTACTED & CORROSION WAS REMOVED IAW APPROVED FIELD REPAIR.SDR CA141205001Bearing · broken(CAN) WHEN MAINTENANCE WAS PERFORMING TRAVEL CHECKS AFTER ELEVATOR TRIM TAB BEARING REPLACEMENT, THEY NOTICED ABNORMAL NOISE AND BINDING FELT IN TRIM CONTROL WHEEL, ALSO INCONSISTENT TRAVEL READINGS WERE NOTED. FURTHER INVESTIGATION REVEALED THAT THE ELEVATOR SDR GLBA2014110500477Stringer · corrodedDURING A SCHEDULED INSPECTION MAINTENANCE FOUND STRINGER 14L CORRODED BS 228.25, DAMAGED AREA APPROXIMATELY 2 INCHES BY 2 INCHES, DAMAGE FOUND UNDER FRONT EDGE OF PREVIOUS SKIN REPAIR. REPAIRED IAW EO 14-1900-53-052. MAJOR REPAIR .SDR GLBA2014110500476Stringer · corrodedDURING A SCHEDULED INSPECTION FOUND STRINGER 15L CORRODED BS 228.25, DAMAGED AREA APPROXIMATELY 2 INCHES BY 2 INCHES, DAMAGE FOUND ON FRONT EDGE OF PREVIOUS SKIN REPAIR. REPAIRED IAW EO 14-1900-53-051. MAJOR REPAIR.SDR GLBA2014110500475Stringer · corrodedDURING A SCHEDULED INSPECTION FOUND CORROSION ON STRINGER 16 BS 213.25 AREA APPROX 3 INCHES BY 2 INCHES, DAMAGE FOUND UNDER & BETWEEN TWO PREVIOUS SKIN REPAIRS. REPAIRED IAW EO 14-1900-53-050. MAJOR REPAIR.SDR CA141203003Fastener · sheared(CAN) DURING A SCHEDULED STRUCTURAL INSPECTION OF FUSELAGE BS 288, A CHECK WAS CARRIED OUT FOR STRESSED AND MISSING FASTENERS ON THE LOWER FUSELAGE BULKHEAD, PN 114-430094-13 OR -15. DURING THIS INSPECTION OF THE FUSELAGE, MAINTENANCE NOTICED A SHEARED HI-LOKSDR GLBA2014120100472Skin · corrodedDURING A SCHEDULED INSPECTION, FOUND BELLY SKIN CORROSION & A CRACK AT BS 228.25 BETWEEN STRINGER 15 - 16R, .3 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-048. MAJOR REPAIR.SDR GLBA2014120100471Skin · corrodedMAJOR REPAIR DURING A SCHEDULED INSPECTION FOUND A CORRODED AREA APPROX 4 INCHES BY 3 INCHES AT FS 213.25 & STRINGER 16. DURING A SCHEDULED INSPECTION MX FOUND A CORRODED AREA APPROX 4 INCHES BY 3 INCHES AT FS 213.25 & STRINGER 16. REPAIRED IAW EO 14-1900-53SDR GLBA2014120100473Brake · contaminatedPILOT REPORTED THAT THE RT BRAKE IS INOPERATIVE ON BOTH FIRST OFFICERS & CAPTAINS ARE FLAT. MAINTENANCE TAXIED ACFT & DRIED BRAKES WITH ALCOHOL, SYS OPERATIONS CHECKED GOOD.SDR GLBA2014120100474Cam Lock · lack of lubePILOT REPORTED THAT THE MAIN CABIN DOOR HANDLE IS VERY DIFFICULT TO MOVE WHEN THE DOOR IS BROUGHT TO THE CLOSED POSITION, HANDLE IN NORMAL FASHION WITH DOOR OPEN. LUBRICATED THE CAM LOCKS OPERATIONS CHECKED GOOD IAW BMM 12-20-00, OPERATIONS CHECKED GOOD.SDR GLBA2014112600470Skin · crackedMAJOR REPAIR DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE LT SIDE BELLY SKIN AT BL 29.06 & WING SPAR, .5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-047.SDR CA141204003Engine · flamed out(CAN) DURING TAXI THE LEFT ENGINE EXPERIENCED A FLAME OUT.SDR GLBA2014112400468Skin · dentedMAJOR REPAIR. DURING A SCHEDULED INSPECTION FOUND DENT IN THE RT HORIZONTAL STAB LE 3.25 INCHES BY 1.375 INCHES, DENT AT HSS 58.00, DENT LOCATED AT RIB AREA, SMALLER DENT OTBD OF DENT AT HSS 58.00, APPROX AT HSS 61.00, 2 INCHES BY 1.5 INCHES, DUE TO BIRD STRSDR GLBA2014112400469Printed Ckt Board · faultyPILOT REPORTED THAT ON CLIMB OUT AFX DISABLE LIGHT ILLUMINATED, N1 ABOVE 91% ON THE RT SIDE. REPLACED PCB A123, PN 129-364091-9, SN ON 993-F-94, SN OFF 799-C-93 IAW MI 34-01, SYS OPERATIONS CHECK GOOD.SDR CA150120012Fuel Divider · failed(CAN) THE AIRCRAFT WAS STARTED AND TAXIED TO THE RUNWAY, BOTH STARTS HAD NO ABNORMAL INDICATIONS. AT THE RUNWAY THRESHOLD WHILE HOLDING THE BRAKES, THE PILOT APPLIED APPROXIMATELY 80 PERCENT TAKEOFF POWER AND BEFORE THE BRAKES WERE RELEASED, NR 2 ENGINE LOST PSDR CA141202027Engine · power loss(CAN) THE CREW STARTED THEIR SHIFT WITH A WALK AROUND AND AN ENGINE RUN UP. THE AIRCRAFT WAS STARTED AND TAXIED TO THE RUNWAY, BOTH STARTS HAD NO ABNORMAL INDICATIONS. APPLIED APPROXIMATELY 80% OF TAKEOFF POWER OBSERVING THE ENGINE INSTRUMENTS, AND BEFORE TSDR GLBA2014112100467Unknown · malfunctionedPILOT REPORTED THAT DURING GEAR RETRACTION, LG HANDLE LIGHT REMAINED ON & LG HANDLE CB POPPED. WENT THROUGH CHECKLIST & MANUALLY EXTENDED GEAR, GOT THREE GREENS, LANDED UNEVENTFULLY. MAINTENANCE PERFORMED OPS CKS ON THE LANDING GEAR SYSTEM IAW MI 32.01, COULSDR CA141124011Frame · cracked(CAN) DURING ABC STRUCTURAL INSPECTION MAINTENANCE NOTICED A 0.500" CRACK FOUND ON LT FRAME BS 288 AT STRINGER 11L LOCATION. REFERENCE "A" CHECK ITEM #37, FIGURE 27. "A HIGH FREQUENCY CURRENT SURFACE SCAN (EDDY CURRENT) WAS CARRIED OUT ON REPAIR OF STATION 288SDR CA141120010Wire · chafed(CAN) THE CREW REPORTED THAT WHEN THEY SELECTED THE GEAR DOWN THE LANDING GEAR CONTROL CIRCUIT BREAKER (2AMP) POPPED. MAINTENANCE WAS DISPATCHED TO INSPECT THE AIRCRAFT. AFTER EVALUATION OF THE AIRCRAFT A FLIGHT PERMIT WAS DEEMED TO BE REQUIRED DUE TO THE FACTSDR GLBA2014111700466Frame · crackedMAJOR REPAIR DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE FRAME FLANGE AT FS 177.35 BETWEEN STRINGERS 13L & 14L IN THE FRAME FLANGE BEND RADIUS AT OTBD END OF FRAME, .75 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTSDR GLBA2014111700465Control Cable · brokenPILOT REPORTED THAT THE RUDDER AILERON INTERCONNECT CABLE BROKE. REPLACED THE AILERON RUDDER INTERCONNECT CABLE PN NAS323-13-0250 IAW MM 27-10-08.SDR GLBA2014111300464Skin · crackedMAJOR REPAIR DURING A SCHEDULED INSPECTION FOUND THE EMER EXIT 6A EXTERIOR BONDED SKIN CRACKED AT THE INTERIOR LOWER AFT CORNER, 1.2 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-52-006.ENGINEERING ORDESDR V0DR20141104004Cell · shortedA BATTERY CELL DURING THE MAIN CHARGE INTERNALLY SHORTED OUT. NOTED THERE WAS SOME DISCOLORATION TO THE TOP OF THE CELL, BUT ALSO NOTED CELL APPEARED TO BE DRY & THE VOLTAGE READ ON THE AFFECTED CELL BEFORE SHUTDOWN OF THE CHARGER WAS 0 VOLTS. VISUAL INSPECTSDR GLBA2014110400463Shimmy Dampener · faultyDURING TAXI OUT, THE CREW NOTED THAT THE ACFT WOULD NOT STEER TO THE RT WITH MAX DIFFERENTIAL BRAKING POWER & NOSE WHEEL STEERING. TOWED THE ACFT BACK TO THE GATE & REPLACED THE NOSE SHIMMY DAMPER IAW BMM 32-50-00. AFTER RELEASE, THE ACFT FLEW & WHILE TAXIINSDR CA141030005Arm · damaged(CAN) PILOT REPORTED AN ISSUE WITH THE RUDDER PEDAL TO MAINTENANCE. ACFT WAS REMOVED FROM SERVICE AND INSPECTED. MAINTENANCE FOUND THE LT OTBD ATTACH POINT FOR THE RUDDER PEDAL ITSELF HAD BEEN ELONGATED TO THE POINT WHERE IT GOT TOO WEAK AND FAILED. THE RUDDESDR CA141027009Wire · chafed(CAN) WHILE CHANGING A FLAP DRIVE CABLE DURING A SCHEDULED MAINTENANCE TASK, MAINTENANCE PERSONNEL NOTICED THE EXTERNAL POWER WIRES TOUCHING THE EDGE OF THE AFT SPAR. FURTHER INSPECTION REVEALED MINOR CHAFING ON THE WIRE CAUSING A SHINY SURFACE ON THE SPAR. SDR CA141024025Stringer · corroded(CAN) DURING AN UNDER CABIN FLOOR STRUCTURAL INSPECTION, MAINTENANCE FOUND CORROSION AT BONDED STRINGER 15, BS 423.25--438.25.SDR CA141024023Frame · cracked(CAN) DURING A STRUCTURAL INSPECTION, MAINTENANCE FOUND A CRACK AT BS 451. CRACK MEASURES APPROXIMATELY 2 INCHES IN LENGTH.SDR CA141024022Seat Track · corroded(CAN) DURING A STRUCTURAL INSPECTION, MAINTENANCE FOUND CORROSION ON LT SEAT TRACK BETWEEN BS 163.975-177.35.SDR GLBA2014101600456Skin · crackedDURING A SCHEDULED INSPECTION FOUND CRACK IN THE LT AFT FUSELAGE SKIN AT BS 549.25 BETWEEN STRINGERS 12 - 13L, 1.1 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-043. MAJOR REPAIR.SDR GLBA2014101600455Structure · damagedDURING A SCHEDULED INSPECTION FOUND MULTIPLE FASTENER HOLES ELONGATED BETWEEN BS 531 - 557.5. ELONGATION RANGING FROM .20 INCHES TO .30 INCHES, FASTENER HOLES ARE FOR THE LT FWD VENTRAL FIND, INBD & OTBD OF STRINGER 12L. REPAIRED IAW EO 14-1900-52-043. MASDR CA141017010Shaft · broken(CAN) THE PILOT REPORTED A FLAP SPLIT ASYMMETRY OCCURRED DURING FLIGHT. MAINTENANCE FOUND THAT THE RT INBD FLAP FLEX SHAFT WAS BROKEN. A HEAVY AMOUNT OF CORROSION WAS NOTICED AT THE BREAK LOCATION.SDR CA141016005Bolt · broken(CAN) DURING VISUAL INSPECTION, UPPER DRAG BRACE ATTACH BOLT FOUND SHEARED THROUGH AT PRE-DRILLED HOLE THAT ALLOWS GREASE INTO THE CENTER OF THE BOLT. BUSHING IN THE DRAG BRACE WAS ALSO FOUND TO HAVE BEEN DAMAGED WHERE BOLT SHEARED.SDR GLBA2014101400454Skin · crackedDURING A SCHEDULED INSPECTION FOUND A CRACK IN THE EMERGENCY EXIT DOOR 6C RT AFT INSIDE SKIN 0.875 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-52-005. MAJOR REPAIR.SDR V0DR20141014003Wheel · looseVENT BLOWER WHEEL MOUNTING BOSS INSIDE DIAMETER TOO LARGE CAUSING EXCESSIVE PLAY BETWEEN THE ARMATURE & WHEEL. THE TECHNICIAN NOTED DURING ASSEMBLY OF THE ARMATURE & BLOWER WHEEL, THAT THE WHEEL WOULD WOBBLE AFTER BEING SECURED WITH THE SET SCREW. THE MATINGSDR CA141014005Spar · corroded(CAN) SPAR CORROSION FOUND AT 2ND FASTENER OF RH WING ON FWD SPAR FLANGE. REPAIR CARRIED OUT IAW CAS ENGINEERING B1900-57-002, RDA#A-RA14-036/D. CORROSION REMOVED AT 2ND FASTENER. STRIPS MADE FROM 7075T6 PICKING UP 8 AND 4 RIVETS RESPECTIVELY EITHER SIDE OF SDR CA141018001Structure · cracked(CAN) DURING INSPECTION, A CRACK WAS DISCOVERED IN THE ENGINE AIR INLET ANTI-ICE LIP WHERE THE BLEED AIRHOSE ATTACHES TO THE LIP. THE COWLING WAS REMOVED AND DELIVERED TO AN APPROVED ACFT WELDING FACILITY WHERE THE LIP CRACK WAS REPAIRED WITH APPROVED METHODSSDR CA141014006Former · cracked(CAN) FORMER SUPPORT FLANGES CRACKED AT FS 164.415 BENEATH PASSENGER LOWER CENTER DOOR SILL. RECTIFICATION: DAMAGED FLANGE REMOVED ( PACKER MADE FROM 2024T3-0.063Ï¿½. REINFORCEMENT ANGLE MADE. ALL WORK CARRIED OUT IAW CAS ENGINEERING EA-B1900-53-001. ALL MADESDR GLBA2014101000453Skin · crackedDURING A SCHEDULED INSPECTION FOUND A CRACK IN THE FUSELAGE SKIN AT FS 249.25 & STRINGER 12L UNDER LT VORTEX GEN 1.75 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-042. MATERIALS UTILIZED ARE INCLUDEDSDR GLBA2014100900451Bulkhead · crackedDURING A SCHEDULED INSPECTION FOUND A CRACK IN THE CANTED BULKHEAD AT FS 588.10 & STRINGER 8L .65 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-041. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING SDR GLBA2014100900452Skin · crackedDURING A SCHEDULED INSPECTION FOUND A CRACK IN THE UPPER FWD CORNER OF A/S DOOR CUT OUT FS 150.6 PROTRUDING UPWARD .75 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-040. MATERIALS UTILIZED ARE INCLUDESDR GLBA2014100800450Spar · crackedDURING A SCHEDULED INSPECTION FOUND A CRACK IN THE AFT CTR HORIZONTAL STAB SPAR WEB, .125 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-55-011. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.
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