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 GLBA2014022800388Actuator · faultyPILOT REPORTED THAT ON APPROACH TO LANDING WITH LG HANDLE IN THE DOWN POSITION, ONLY NOSE & RT MAIN GEAR GREEN LIGHTS ILLUMINATED. LG RELAY CB TRIPPED, RAN ALL APPROPRIATE CHECKLISTS & LANDING GEAR MANUALLY EXTENDED NORMALLY. MX R & R THE LT MAIN ACTUATOR IASDR GLBA2014021700385Frame · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE FUSELAGE FRAME AT FS 183.250, BETWEEN STRINGERS 2R & 3R WHERE THE DUCT PASSES THROUGH THE FRAME, .5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 14-1900SDR CA140218002Servo · faulted(CAN) THE RT SIDE ELECTRIC TRIM DID NOT RESPOND WHEN NOSE DOWN TRIM WAS SELECTED ON CLIMBOUT. ACFT RETURNED TO MAINTENANCE BASE & LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AFFECTED SYS IN DETAIL AND FOUND THE ELEVATOR TRIM SERVO PN: 622-5734-002 TO BSDR GLBA2014021300382Frame · crackedDURING A SCHEDULED INSPECTION MX FOUND 2 CRACKS IN THE RT SIDE OF FS 107 & STRINGER 8R, FRAME ANGLE & LONGERON, FRAME CRACKED AT UPPER END OF FRAME IN BEND RADIUS. LONGERON CRACKED FROM LOWER EDGE TO LONGERON UPWARD THROUGH BEND RADIUS, 1.5 INCHES IN LENGTH.SDR GLBA2014021300381Skin · corrodedDURING A SCHEDULED INSPECTION MX FOUND BELLY SKIN CORROSION AT FS 270 & STRINGER 16, 1.2 INCHES FWD & AFT DIRECTION BETWEEN STRINGER 16 FASTENERS. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-010.SDR GLBA2014021300380Frame · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE LT FUSELAGE AT FS 107 & STRINGER 8L FRAME AT THE UPPER END AT FRAME IN BEND RADIUS, .75 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-009.SDR GLBA2014021400384Frame · crackedDURING A SCHEDULED INSPECTION MAINTENANCE FOUND A CRACK AT FS 456 LT SIDE LOWER FRAME, 1.5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-011.SDR GLBA2014021300383Motor · faultyPILOT REPORTED THAT WHEN THEY WENT TO EXTEND THE FLAPS HAD A STRONG ELECTRICAL SMELL & THE FLAPS DID NOT EXTEND. MAINTENANCE R&R FLAP GEAR BOX MOTOR P/N 100-524073-1 S/N OFF 6137 S/N ON. 5693 OPS CHECK GOOD AT THIS TIME REF 1900DMM 27-50-03.SDR GLBA2014021200379Rib · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE RT WING INBD RIB FLANGE & DOUBLER AT JUNCTION WITH THE WING SPAR, RADIATES FROM THE OTBD EDGE OF THE FLANGE & DOUBLER INWARD TOWARD THE FLANGE BEND RADIUS, 1 INCH IN LENGTH. REPAIRED THE AFFECTED AREA AND SDR GLBA2014021000378Skin · crackedDURING A SCHEDULED INSPECTION MX FOUND 2 CRACKS IN THE FUSELAGE SKIN AT FS 150 & STRINGER 1, JUST TO THE RT OF STRINGER 1 LOCATION, CRACK RADIATES INBD & OTBD FROM FASTENER .55 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECSDR A8OA2014F00068Pressure Switch · defectiveLEFT ENGINE AFX, AUTOFEATHER, ANNUNCIATOR DOES NOT ILLUMINATE WITH POWER LEVERS ABOVE 89-91 PERCENT N1.SDR GLBA2014021000377Door Frame · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE CARGO DOOR AFT LOWER FRAME AT FS 509.50 AT THE INTERSECTION OF THE LOWER SILL, 1" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-006.SDR ERAA20140002Downlock Switch · failedNOSE GEAR FAILS TO INDICATE DOWN & LOCKED. R & R LG DOWN LOCK POSITION SWITCH & PERFORMED GEAR SWINGS. ALL GEAR INDICATION OPERATIONS CHECKED GOOD IAW B1900D MM 32-60-01, OK FOR SERVICE.SDR GLBA2014020400375Brake Sys · malfunctionedSIG EVENT PILOT REPORTED THAT THE RT BRAKE PEDAL GOES COMPLETELY TO THE FLOOR ON THE CAPTAIN`S & FIRST OFFICER'S SIDE, RIGHT BRAKE COMPLETELY INEFFECTIVE. SUPPLEMENT INFORMATION ION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORKSDR 29GA93652020214Cable · frayedDURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED AIRSTAIR DOOR FORWARD LOCK CABLE HAS BROKEN STRANDS. REPLACED AIRSTAIR DOOR, FORWARD LOCK CABLE, OPS CHECK GOOD.SDR CA140131003Handle · departed(CAN) DURING DEPARTURE, A BANG WAS HEARD ON THE LT SIDE OF THE CABIN, NEAR THE FRONT. THOUGHT IT WAS JUST THE CABIN DOOR SEAL. NO ABNORMAL INDICATION NOTED, ALTHOUGH AIR COULD BE HEARD LEAKING FROM THE CABIN DOOR, AND FLIGHT CONTINUED ON. THE PASSENGER DOOSDR CA140129004Boot · cracked(CAN) ON WALK AROUND OF THE ACFT AND PROPELLERS A CHORDWISE CRACK WITHIN 6" OF THE BOOT WAS FOUND ON THE EROSION SHIELD. THE PROP SHOWED NO SIGN OF IMPACT DAMAGE THAT MAY HAVE CONTRIBUTED TO THIS CRACKING. PROP WAS REPLACE. THIS IS THE THIRD INCIDENT WE HAVSDR GLBA2014012300373Spar · crackedDURING A SCHEDULED INSPECTION MX ACCOMPLISH PROACTIVE REPAIR TO THE RT VERTICAL SPAR CAP ANGLE IAW EO 14-1900-55-001. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.SDR CA140128012Rib · damaged(CAN) DURING A STRUCTURAL INSPECTION, MAINTENANCE NOTICED THERE WERE MISSING/SHEARED RIVETS ADJACENT TO WHERE THE RUDDER TORQUE TUBE ASSY ATTACHES TO THE RIB CLOSURE AND DOUBLER DUE TO THE NATURE OF THE DEFECT A FLEET WIDE INSPECTION WAS COMPLETED ON AN ADDITSDR GLBA2014011600371Skin · dentedDURING A SCHEDULED INSPECTION, MX FOUND THE LT AFT SKIN DENTED AT BS 446 BETWEEN STRINGERS 11-12L. REPAIREDS IAW EO 14-1900-53-005.SDR 8EKA20140120001Flap · crackedDURING ROUTINE INSPECTION A CRACK WAS FOUND ON THE RT WING FLAP. THE ACFT WAS REMOVED FROM SERVICE & REPAIRED.SDR 8EKA20140120002Flap · crackedDURING INSPECTION A CRACK WAS FOUND ON THE LT WING FLAP. THE ACFT WAS REMOVED FROM SERVICE & REPAIRED.SDR 8EKA20140120003Flap · crackedDURING INSPECTION A CRACK WAS FOUND ON THE RT WING FLAP. THE ACFT WAS REMOVED FROM SERVICE & REPAIRED.SDR 8EKA20140120004Flap · crackedDURING INSPECTION A CRACK WAS FOUND ON THE LT WING FLAP. THE ACFT WAS REMOVED FROM SERVICE & REPAIRED.SDR GLBA2014011300368Frame · crackedDURING A SCHEDULED INSPECTION FOUND A CRACK AT BS 183 & STRINGER 9R FRAME ANGLE, .375 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-003.SDR GLBA2014011300367Door Frame · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE PAX DOOR CUTOUT LOWER FRAME AT APPROXIMATELY FS 172 LOWER AFT CORNER, 1 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-002.SDR GLBA2014011300370Skin · crackedDURING A SCHEDULED INSPECTION, FOUND TWO CRACKS AT BS 150 & STRINGER 1 EXTERIOR FUSELAGE SKIN PROTRUDING OUT OF RIVETS ON EITHER SIDE OF STRINGER, .25 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-004.SDR GLBA2014011300369Door · crackedDURING A SCHEDULED INSPECTION, FOUND THE EMERGENCY DOOR CRACKED, 4C AT THE RT FWD ASSEMBLY, 1.125 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-52-001.SDR GLBA2014011300366Downlock Switch · faultyPILOT REPORTED THAT EN ROUTE TO DVL GOT A GPWS C/O & FLICKERING IN TRANSIT LIGHTS WITH 3 GREEN DOWN LOCK INDICATED. FOLLOWED CHECKLIST, HAD NO CHANGE, WAS REROUTED BACK TO MSP, DID NORM EXTENSION, CONF WITH ATC THAT GEAR WAS DOWN, STILL GOT C/O, BUT NO IN TRASDR 7C7A2016071700245Skin · dentedSHARP DENT IN FUSELAGE RT SIDE BEHIND ICE SHIELD. REPAIRED WITH INSERTION PATCH SRM 51-70-06.SDR CA140121006Float Valve · broken(CAN) FUELER HEARD KNOCKING NOISE WHILE FUELING LT WING. AFTER INVESTIGATING PROBLEM FOUND THE FLOAT HAD BROKEN OFF THE FLOAT VALVE ASSY AND WAS FLOATING AROUND IN THE FUEL CELL. REPLACED FLOAT VALVE ASSY WITH SERVICEABLE ASSY.SDR GLBA2014010800364Door Frame · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE LOWER AIRSTAIR DOOR FRAME AT BS 172.0, 1.4 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-001.SDR 29GA2014010595732Motor · failedLEFT MLG LIGHTS DID NOT ILLUMINATE AFTER GEAR EXTENSION. GEAR HANDLE REMAINED RED, FINALLY GOT DOWN AND 3 GREEN AFTER TURNING/YAWIMG THE ACFT. REPLACED LANDING GEAR POWER PACK MOTOR. OPS CHECKS GOOD.SDR GLBA2013122300363Latch · lack of lubePILOT REPORTED THAT THE EMERGENCY EXIT DOOR AT 6C, EXTERIOR LATCH IS NOT STOWED. R & R 6C EMERGENCY DOOR IAW AMM 52-20-00, OPS CHECKED GOOD. LUBRICATED LATCH IAW 52-20-01 STEPS 1B18 1B14 1B22.SDR CA131218014Window Frame · cracked(CAN) WHEN REPLACING THE LT EMERGENCY EXIT WINDOW A 7.25 INCHES LONG CRACK WAS FOUND IN THE OUTER RADIUS OF THE WINDOW PAN. THE CRACK WAS NOT VISIBLE WITHOUT REMOVING THE WINDOW.SDR GLBA2013121700361Structure · crackedDURING A SCHEDULED INSPECTION, FOUND EMERGENCY EXIT 4C LOWER AFT CORNER OF BONDED ASSEMBLY, CRACKED APPROXIMATELY 1 5/8 INCHES. REPAIRED IAW EO 13-1900-52-003.SDR GLBA2013121800362Skin · debondedDURING A SCHEDULED INSPECTION, FOUND BELLY SKIN BETWEEN STRINGER 15-16L BS 290 CORRODED & DEBONDED. REPAIRED IAW EO 13-1900-53-081.SDR 29GA2013121593627Elevator · out of rigON TAKEOFF, WITH FLIGHT TRIM SET, 1.5 HAD TO FIGHT ELEVATOR TO KEEP FROM PITCHING UP IN LEVEL CRUISE, FORWARD TRIM AT 2. COMPLIED WITH ELEVATOR CONTROL SYSTEM RIGGING AND ELEVATOR TRIM TAB CONTROL RIGGING.SDR GLBA2013121600360Unknown · odorPILOT REPORTED THAT THERE WAS A HOT ELEC SMELL COMING FROM THE FIRST OFFICER'S SIDE OF THE COCKPIT, POSSIBLE FROM THE CB PANEL. INSPECTED BEHIND THE CB PANEL, PULLED UP FLOORBOARDS, RAN ENG NO DISCREPANCIES OR ABNORMAL ODORS NOTED.SDR GLBA2013121300355Spar · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE LT INBD WING INBD RT FLANGE ANGLE AT FS 288.00 & WING SPAR, ONE INCH IN LENGTH. REPAIRED IAW EO 13-1900-57-020.SDR GLBA2013121300356Rib · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE RT INBD WING RIB & FLANGE ANGLE. REPAIRED IAW EO 13-1900-57-021.SDR GLBA2013121300357Stringer · crackedDURING A SCHEDULED INSPECTION FOUND TWO CRACKS IN STRINGER 9L AT BULKHEAD BS 588.1 THAT HAVE CONVERGED TO FORM A TRIANGLE SHAPED PIECE, 1.3 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-57-020.SDR GLBA2013121300358Stringer · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE STRINGER 9R AT BULKHEAD BS 588.1, ONE INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-079.SDR GLBA2013121300359Frame · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE FRAME FLANGE BS 107 STRINGER 8R. THE CRACK RADIATES TO THE END OF THE FRAME & DOWN APPROXIMATELY .3 INCHES FROM THE UPPER FASTENER, .9 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-080.SDR GLBA2013121300354Unknown · odorPILOT REPORTED FUEL LEAKING ON THE RT WING LOWER SURFACE AT THE WING ROOT AT THE MID CHORD, ALSO HAS A STRONG FUEL ODOR IN CABIN. MAINTENANCE INSPECTED AUX TANK, FOUND NO LEAKS.SDR 29GA94632121113Uplock Switch · shortedAFTER GEAR RETRACTION THE RED UNSAFE LIGHT REMAINED ILLUMINATED AND VISUAL INSPECTION INDICATED GEAR WAS NOT FULLY RETRACTED. REPLACED RT MLG UPLOCK SWITCH. OPS CHECKS GOOD.SDR ERAA20130069Hydraulic System · lowLANDING GEAR, RETRACT & EXTENSION SOUNDS DIFFICULT. IT'S TAKING EXTRA EFFORT, WHINING & GRINDING. SERVICED LG HYD SYS IAW B1900 MM 12-10-00. PERFORMED LG OPERATIONAL CHECKS IAW B1900 MM32-30-00. NO DEFECTS NOTED, LG OPERATIONS CHECKED GOOD, NO LEAKS NOTED.SDR CA131220003Drive Assy · damaged(CAN) NORMAL APPROACH, FLAP 17 SELECTED WITH NO INDICATION ERRORS OR ANY CONTROL ISSUES OUT OF THE ORDINARY. ON FINAL, FLAPS 35 WAS SELECTED, PF INSTANTLY FELT VERY STRONG YAW TO THE LT. ACFT CONTROL WAS REGAINED WITH THE USE OF RUDDER TO HELP MAINTAIN DIRECTSDR GLBA2013120500353Hydraulic System · contaminatedPILOT REPORTED THAT AFTER SELECTING GEAR DOWN, LANDING GEAR RELAY CIRCUIT BREAKER TRIPPED. RAN THROUGH CHECK LIST, MANUALLY EXTENDED GEAR, ALL INDICATIONS SHOWED GEAR WAS DOWN AND LANDED SAFELY. MAINTENANCE INSPECTED RETRACTION AND EXTENSION OF LANDING GEAR SDR CA131128006Bolt · loose(CAN) CREW REPORTED FLICKERING EADI & EHSI, ALTERNATING, ON BOTH THE CAPTAIN`S & CO-PILOT`S SIDE. IN CONJUNCTION WITH THIS A LOUD NOISE WAS ALSO EVIDENT OVER THE COCKPIT AND CABIN SPEAKERS AS WELL AS THE CREW HEADSETS. TROUBLESHOOTING WAS CARRIED OUT & THE N
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