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 = '7372T5' 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 = '7372T5' 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 CA030417011Pcu · inoperative(CAN) AFTER PUSHBACK AND START, FLAP 2 SELECTED AND HYDRAULIC SYSTEM A LOW PRESSURE ILLUMINATED AND HYD QTY GUAGE DECREASED TO ZERO. MAINTENANCE FOUND THE A SYSTEM AILERON POWER CONTROL UNIT (PCU) FILTER BOWL HAD FRACTURED RESULTING IN LOSS OF HYD PRESS/FLUID.SDR CA030225003Oxygen Mask · misinstalled(CAN) A/C EXPERIENCED RAPID DEPRESSURIZATION. CLIMBED TO 15,000 FT IN APPROX 5-10 SECONDS. O2 SYS DEPLOYED AUTOMATIC. STANDBY MODE DID NOT OPERATE NORMALLY BUT CABIN PRESSURE WAS RECAPTURED. DURING EMER DESCENT WITH MANUAL MODE MAINT REPLACED CABIN PRESSURSDR CA030121007Bearing(CAN) LOG SNAG - ON FLAP SELECTION TO ONE UNIT, LE FLAP TRANSIT LIGHT REMAINED ON. NO. 4 SLAT REMAINED AMBER. ALL OTHERS GREEN. ON SELECTION OF FLAP 10, NO. 4 WENT GREEN FULL EXTEND WITH OTHER LE DEVICES.THE MAINTENANCE MECHANICS DISCOVERED THE NO. 4 LE SLAT OSDR CA030106004Connector · burned(CAN) ON OVERNIGHT CHECK OF AUTO PILOT STAB TRIM, C/B FOUND TRIPPED AND UNABLE TO RESET. SMOKE NOTED IN STAB COMPARTMENT AND UPON INVESTIGATION FOUND CONNECTOR AND 3 INCHES OF ASSOCIATED WIRING DAMAGED ATA/P STAB TRIM MOTOR CONNECTION. WIRING REPAIRED, CONNSDR CA030103020Connector · burned(CAN) DURING OVERNIGHT CHECK IN THE HANGER, AVIONICS FOUND THE A/P STAB TRIM MOTOR C/B WAS POPPED. TRIED A RESET BUT NO JOY AND C/B FELT ODD. TURNED A/C POWER OFF AND C/B WOULD NOT RESET. C/B REPLACED. C/B RESET BUT POPPED A FRACTION OF A SECOND LATER. AVIONSDR CA030121003Bearing · loose(CAN) ON 9 JAN 2003 IT WAS FOUND THAT THE ROLLER BEARING ON THE NR 5 SLAT OUTBOARD TRACK HAD BECOME DETACHED AND THE CONTROL ARM HAD WORN THROUGH THE TOP WING SKIN FORWARD OF THE FRONT SPAR. UPON REMOVAL OF THE ACCESS PANEL ALL THE PARTS WERE FOUND INSIDE INCLSDR P2EA2001M0004ComputerAuto Pilot twitches in pitch on VG1. Auto Pilot pulls back on controls continuiously when operated on system "A". Corrective action: Removed and replaced Pitch Computer IAW MM 22-11-151A, operatoinal check normal. See A/C 120 Log pages 92743 and 92744. This reSDR P2EA2001M0006Control PanelHeading Hold will not hold heading with Auto Pilot in B channnel. Corrective action: Deffered Heading Hold per MEL 22-1, CI#M120076 per MX CNTL Mic. Replaced Mode Control Panel, operational check normal IAW MM 22-11-191, This clears CI#M120079. See A/C 120 LogSDR P2EA2001M0003Gyro · faultyAUTO PILOT ON HDG2 HOLD WILL NOT MAINTAIN BANK AND ROLL LEVEL AND OCCASIONALLY JERKS ABRUPTLY. REPLACED NR 1 VERTICAL GYRO PER MM 34-22-11, OPERATIONAL CHECK OKAY.SDR P2EA01167Skin · crackedSJO - DURING Q-CHECK, RIGHT WING OUTBOARD MID FLAP WBL 304.5, SKIN WITH CRACK. RIGHT WING OUTBOARD MID FLAP L/E OF CENTER TRACK CAVITY SKIN SECTION REPAIRED IAW COOPESA EO NR COO-3-57-452-01. (M)SDR P2EA01162Skin · dentedSJO - DURING Q-CHECK, FOUND EXTERNAL FUSELAGE SKIN WITH DENT AT BS 500A PLUS 12, BETWEEN STRINGER 1 AND STRINGER 2L. REPAIRED FUSELAGE SKIN SECTION FROM BS 500A PLUS 7 INCHES TO 500B, BETWEEN STRINGER 2 LEFT AND STRINGER 2 RIGHT DUE TO DENT IAW SRM 53-30-3 FISDR P2EA01163Cargo Track · corrodedDURING Q-CHECK, FOUND FORWARD CARGO COMPARTMENT FROM BS 380 TO BS 520 LBL 18.5, CARGO TRACK WITH CORROSION. (M)SDR P2EA01164Floor Support · corrodedDURING Q-CHECK, AFT CARGO COMPARTMENT BETWEEN BS 767 AND BS 847 AT STRINGER 25 RIGHT FLOOR SUPPORT WITH CORROSION. (M)SDR P2EA01156Doubler · crackedSJO - DURING Q-CHECK, EXTERNAL FUSELAGE DOUBLER WITH CRACK AT BS 1138, WL 266 LEFT SIDE. (M)SDR P2EA01159Skin · canningDURING Q-CHECK, FOUND EXTERNAL FUSELAGE WITH OIL CAN AT BS 901, BETWEEN STRINGER 21 AND 22 RIGHT. REPAIRED FUSELAGE SKIN SECTION FROM BS 898.5 TO BS 902.5 BETWEEN STRINGER 21 AND 22 RT DUE TO OIL CAN IAW SRM 53-30-3, FIG 05. (M)SDR P2EA01158Stringer · dentedSJO - DURING Q-CHECK, LOWER FUSELAGE TAIL CONE STRINGER 27 LEFT WITH DENT AT BS 1035. REPAIRED STRINGER 27 LEFT FROM BS 1032 TO BS 1045 DUE TO DENT IAW SRM 53-10-3, FIG 01. (M)SDR P2EA01157Bulkhead · crackedDURING Q-CHECK INSPECTION PER S/B 737-53A1173, FOUND PRESSURE BULKHEAD BS 178, WEB CRACKED AT RBL 11.5-WL 213, PRESSURE BULKHEAD BS 178 FLOOR WEB SECTION CRACKED AT SL 207, PRESSURE BULKHEAD BS 178 LEFT SIDE LATERAL CHORD CRACKED AT WL 207, PRESSURE BULKHEAD BSDR P2EA01151Frame · crackedDURING Q-CHECK, FUSELAGE AFT CARGO COMPARTMENT AT FRAME BS 807, BETWEEN STRINGER 27 LEFT AND 27 RIGHT, LOWER SECTION WITH CRACK. S/D - REPAIRED FRAME SECTION AT BS 807 BETWEEN STRINGER 27 RIGHT AND STRINGER LEFT DUE TO CRACK IAW SRM 53-10-4, FIG 06. (M)SDR P2EA01154Skin · dentedDURING Q-CHECK, FOUND EXTERNAL SKIN WITH DENT AT BS 500A PLUS 12 INCHES, BETWEEN STRINGER 1 AND 2 LEFT. (M)SDR P2EA01153Skin · dentedDURING Q-CHECK, FOUND EXTERNAL FUSELAGE SKIN WITH DENT AT BS 590, STRINGER 1. S/D - REPAIRED FUSELAGE SKIN SECTION FROM BS 590 TO BS 599 BETWEEN STRINGER 2 LEFT AND 2 RIGHT DUE TO DENT IAW SRM 53-30-3, FIG 7. (M)SDR P2EA01150Skin · dentedDURING Q-CHECK, FOUND EXTERNAL FUSELAGE SKIN WITH DENT AT BS 1040, BETWEEN STRINGER 27 LEFT AND 27 RIGHT. S/D - REPAIRED FUSELAGE SKIN SECTION FROM BS 1030 TO BS 1057 BETWEEN STRINGER 27 RIGHT AND STRINGER 24 LEFT DUE TO DENT IAW SRM 53-30-3, FIG 06. (M)SDR P2EA01145Skin · dentedDURING Q-CHECK, FOUND TWO DENTS RIGHT SIDE OF AFT OUT FLOW VALVE. REPAIRED FUSELAGE SKIN SECTION FROM BS 907 TO BS 922 BETWEEN STRINGER 21 RIGHT AND 23 RIGHT DUE TO DENTS IAW SRM 53-30-3, FIG 28. (M)SDR P2EA01146Skin · dentedDURING Q-CHECK, EXTERNAL FUSELAGE SKIN WITH DENT AT BS 1051, BETWEEN STRINGER 16 LEFT AND 17 LEFT. REPAIRED FUSELAGE SKIN SECTION FROM BS 1047.5 TO BS 1055.5 BETWEEN STRINGER 16 LEFT AND 17 LEFT DUE TO DENT IAW SRM 53-30-3, FIG 19. (M)SDR P2EA01152Floorbeam · corrodedSJO - DURING Q-CHECK, FOUND PAX CABIN AT BS 294, BETWEEN BL 0 AND RBL 40 INCHES, WL 208, UPPER SECTION AND BS 294.5 BETWEEN BL 0 AND LBL 30, FLOORBEAM WITH CORROSION. (M)SDR P2EA01149Stringer · corrodedDURING Q-CHECK, FOUND LOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 968, STRINGER 27 RIGHT WITH CORROSION. S/D - REPAIRED STRINGER 27 RIGHT FROM BS 958.5 TO BS 976 DUE TO CORROSION IAW SRM 53-10-3, FIG 01. (M)SDR P2EA01148Skin · dentedSJO - DURING Q-CHECK, EXTERNAL FUSELAGE SKIN WITH DENT AT BS 807, BETWEEN STRINGER 26 LEFT AND 27 RIGHT. REPAIRED FUSELAGE SKIN SECTION FROM BS 789.5 TO BS 815 BETWEEN STRINGER 25 LEFT TO STRINGER 26 RT DUE TO DENT IAW SRM 53-30-3, FIG 06. (M)SDR P2EA01122Indicator · inoperativeMCI - FLT 350 - DURING CRUISE AT 33,000 FEET CABIN RATE OF CHANGE WAS PLUS 250 FEET PER MINUTE AND CABIN PRESSURE WAS AT 9,500 FEET AND SHOULD BE AT 800 FEET FOR NORMAL. STANDBY WAS SELECTED WITH NO IMPROVEMENT. DURING DESCENT WITH THROTTLES AT IDLE, CABIN RSDR CA010522007Csd · unreliable(CAN) AT FL 230, NR 1 CONSTANT SPEED DRIVE LOW OIL PRESSURE LIGHT ILLUMINATED. FLIGHT ELECTED TO RETURN DUE APU ELECTRICS WERE UNRELIABLE. REPLACED NR 1 CSD AS PER WORK CARD 1182-1. APU AND NR 1 CSD CHECKED SERVICEABLE DURING GROUND RUN.SDR CA010404008Windshield · leaking(CAN) CLIMBING THROUGH 13,000 FEET, APPROXIMATELY 4 PSI CABIN PRESSURE, CAPTS WINDSHIELD POPPED WITH A NOTICEABLE PRESSURIZATION LEAK. RETURNED. WINDOW INSPECTED, NO DEFECTS NOTED. WINDOW ATTACHED BOLTS WERE RETORQUED. AIRCRAFT PRESSURIZED TO 3 PSI, NO PRESSURSDR P2EA00221Gasper Fan · malfunctionedFLT 307 - MYR - SMOKE AND FUMES NOTED IN COCKPIT. EMERGENCY DECLARED AND AIRCRAFT RETURNED TO MYR LANDING UNEVENTFUL. FOUND FAULTY GASPER FAN, DEFERRED PER MEL 21-24, CONTROL M120626 PER MX CONTROL. REMOVED AND REPLACED GASPER FAN PER MM 21-24-21, OPERATINOSDR P2EA00212Control Cable · looseMCI - FLT 589 - EMERGENCY DECLARED, NR 1 ENGINE SHUT DOWN 5 MINUTES BEFORE LANDING, AIRCRAFT RETURNED TO MCI, LANDING UNEVENTFUL. LOST THROTTLE CONTROL NR 1 ENGINE: EPR 2.09, N1 91 PERCENT, EGT 450, N2 91 PERCENT, AND FUEL FLOW NORMAL. FOUND LOOSE HARDWARE SDR P2EA00202Skin · delaminatedYYC - DURING C-CHECK, RIGHT OUTBOARD FOREFLAP, REPAIR DELAMINATED ON UPPER SURFACE 87 INCHES OUTBOARD OF INBOARD END. REPAIRED FOREFLAP IAW SRM 51-40-6, PAGE 8 PARAGRAPH 11. (M)SDR P2EA00203Skin · dentedYYC - DURING C-CHECK, FOUND DENT WITH SHARP CREASE AT BS 860, BETWEEN STRINGERS 15L AND 16L. REPAIRED DENT AT BS 860 BETWEEN STRINGERS 15L AND 16L IAW SRM 53-30-3, FIG 1. (M)SDR CA000209003Bolt · broken(CAN) NR 4 SLAT BOLT BROKEN THROUGH GREASE PASSAGE DUE TO LACK OF LUBRICATION, BOLT WORN. REPLACED.SDR P2EA99275Engine · bird strikeMDW - FLT 815 - ABORTED TAKEOFF, NO EMERGENCY DECLARED, RETURNED TO BLOCKS. AT APPROXIMATELY 100 KNOTS DURING TAKEOFF ROLL, INGESTED BIRD IN NR 1 ENGINE. (X)SDR CA981125024Sensor · malfunctioned(CAN) AT TOP OF DESCENT, RT RED GEAR WARNING LIGHT FLICKERED WITH GEAR SELECTED UP. REPLACED RT MLG UPLOCK SENSOR.SDR CA970904013Rod End Bearing · broken(CAN) ROD END BEARING SHEARED AT NECK. DETACHED FROM MAIN LANDING GEAR PANEL. REPLACED.SDR CA970327007Line · failed(CAN) ONE HOUR OUT 'B' SYSTEM QTY LOSS, AIRCRAFT RETURNED. FOUND 'B' PUMP PRESSURE LINE FAILED. REPLACED.SDR CA970318002Bearing · failed(CAN) ON LANDING CREW REPORTED NOSE WHEEL SHIMMY. INBOARD BEARING OF THE L/H WHEEL WAS FOUND TO HAVE FAILED. THE ROLLER AND CAGE ASSEMBLY DEPARTED THE AIRCRAFT AND THE SECTION IN CONTACT WITH THE AXEL WELDED ITSELF TO THE AXLE. SEVERAL PIECES OF THE BEARING
Back to Boeing 737-2T5