Boeing 747-230B
Service difficulty reports · 618
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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 = '747230B' 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 = '747230B' 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 UIEA200600034Panel · erodedLEFT WING LEADING EDGE PANEL VCF NR 6 LOWER SIDE OF PANEL IS EROSION DAMAGE, AND LOWER SIDE CHANNEL IS DAMAGED. REPAIRED VCF NR 6 IAW OHM 57-55-22 AND SRM 51-40-14 PARA 4N AND FIG 16.SDR UIEA200600033Skin · delaminatedLT WING OUTBOARD T/E FORE-FLAP HAS DELAMINATION BETWEEN NR 1 AND NR 2 TRACKS. REPAIRED IAW SRM 51-40-15 PARA 4N.SDR UIEA200600032Skin · delaminatedLT WING INBOARD T/E FORE-FLAP HAS DELAMINATION ON LOWER SIDE OF L/E BETWEEN NR 3 AND NR 4 TRACKS. REPAIRED IAW SRM 51-40-12 PARA 4C AND 51-40-14 PARA 4D.SDR UIEA200600031Skin · delaminatedLT WING INBOARD T/E MID-FLAP HAS DELAMINATION BETWEEN FLAP TRACKS NR 3 AND NR 4. REPAIRED IAW OHM 57-52-35 BY REPLACEMENT OF MID-FLAP LEADING EDGE SECTION BETWEEN NR 3 AND NR 4 TRACKS.SDR UIEA200600030Skin · delaminatedRT WING INBOARD T/E MIDFLAP HAS A LARGE SPOT OF DELAMINATION. REPAIRED IAW SRM 51-40-14 FIG 9.SDR UIEA200600029Skin · delaminatedRT WING INBOARD AFT T/E FLAP HAS DELAMINATION APPROX 15 INCHES. FLAP REPAIRED IAW SRM 51-40-14 REPAIR 4D.SDR UIEA200600028Tee Fitting · corrodedRT WING TRAILING EDGE - LOWER T-CHORD HAS CORROSION AT REAR SPAR CAVITY WS 725. REPLACED LOWER T-CHORD IAW SRM 51-30-02.SDR UIEA200600027Rib · crackedRT WING DRY BAY - LOWER CHORD OF RIB AT WS 1516 IS CRACKED IN TWO PLACES. REPLACED LOWER CHORD OF RIB IAW SB 747-2221 FIG 5.SDR UIEA200600026Intercostal · crackedDURING HFEC TEST OF BS 1265 FRAME TO RT FLOORBEAM INTERSECTION, FOUND A CRACK INDICATION IN ONE FASTENER HOLE. AFTER INVESTIGATION IT HAS BEEN FOUND THAT THE CRACK IS IN THE FLOORBEAM INTERCOSTAL UPPER CHORD. REPAIRED BY FREEZE PLUG INSTALLATION IAW SRM 51-1SDR UIEA200600025Skin · corrodedFOUND CORROSION ON THE CENTER WING TANK UPPER SKIN UPPER SURFACE, AT BS 1140 LBL 120. REWORKED UPPER SKIN PANEL IAW SRM 51-10-01. FOUND MATERIAL LOSS WITHIN LIMITS PER SRM 57-10-01 FIG 1.SDR UIEA20060024Frame · crackedBS 1000 BULKHEAD LOWER CHORD HAS A CRACK BETWEEN STRINGERS 46R - 47R. REPAIRED BS 1000 BULKHEAD LOWER CHORD BY SPLICING A NEW LOWER CHORD SECTION BETWEEN STRINGERS 45L AND 45R PER EDF KLM-CC1-2006-034 R3 WITH 8100-9 APPROVAL. REPEAT INSPECTION REQUIREMENTS ASDR UIEA200600023Stiffener · corrodedCENTER WING TANK UPPER SURFACE STRINGER 27C BETWEEN LBL 96 AND LBL 127.5 HAS EXFOLIATION CORROSION. REPAIRED STRINGER SECTION IAW SRM 57-10-04 FIG 3 AND EDF KLM-747-CC1-2006-032-R4 WITH 8100-9 APPROVAL. FIRST STAGE APPROVAL IN DOCUMENTED ON EO 4757A252.SDR UIEA200600022Frame · crackedBS 800 LT FRAME INNER CHORD FOUND WITH CRACK INDICATION BY HFEC INSPECTION 1 FASTENER HOLE ABOVE STRINGER 17L. REPAIRED INNER CHORD IAW SRM 53-10-04 FIG 114. REPAIR DOCUMENTED ON ATLAS EO 4753A630.SDR UIEA200600021Frame · misdrilledBS 800 RT FRAME FOUND WITH A MISS DRILLED HOLE ON THE FRAME INNER CHORD AT STRINGER 16R. REPAIRED ACCORDING EDF KLM-747-CC1-2006-031-R2 WITH 8100-9 APPROVAL. REFERENCE ATLAS EO 4753A630 FOR DOCUMENTATION.SDR EIS2006033Anti-Ice Valve · failedSHORTLY AFTER TAKEOFF, NR 1 ENGINE NACELLE ANTI-ICE VALVE OPEN LIGHT WOULD NOT ILLUMINATE. REPLACE ANTI-ICE VALVE PER MM30-21-05, OPS CHK GOOD.SDR EIA2006052Bottle · lowLT UPPER DECK SLIDE PRESSURE BOTTLE BELOW LIMITS. REMOVED AND REPLACED BOTTLE PER 25-68-04.SDR P5CA0601446Circuit Breaker · trippedGENERATORS NR 3 AND NR 4 SHOW NO GENERATOR LOAD AND NO VOLTS OF FREQ'S GENERATOR TEST SHOWS CSD RPM AND PMG FOR BOTH 3 AND 4. FOUND CIRCUIT BREAKERS FOR NR 3 AND NR 4 DISTRIBUTION METER POPPED, RESET BREAKERS AND RAN ENGINES PER MM 71-00-00. OPS CHECK NORMALSDR P5CA0601445Starter · failedABORTED START ON NR 1 ENGINE, DUE TO SLOW ACCELERATION AND SPARKS FROM STARTER EXHAUST. REMOVED AND REPLACED NR 1 ENGINE STARTER PER MM 80-40-07. FUNCTION CHECKS NORMAL.SDR P5CA0601436Pressure Switch · failedNR 4 MAIN AFT BOOST PUMP FAILED. ITEM DEFERRED PER MEL 28-01-C. CHANGED NR 4 FUEL AFT BOOST PUMP PRESSURE SWITCH IAW MM 28-42-01. TEST OK.SDR P5CA0601433Trim System · malfunctionedAUTOPILOT A DID NOT TRIM STABILIZER AND DID NOT CAPTURE ALTITUDE. REPLACED THE AUTOMATIC STABILIZER TRIM UNIT PER MM 22-14-01. TEST OK.SDR P5CA0601427Proximity Switch · failedFLIGHT CREW REPORTED AFTER TAKEOFF, GROUND SAFE RELAY LIGHT CAME ON. ALTERNATE PROCEDURE ACCOMPLISHED. AUTO PRESS CONTROLLER NOT OPERATING NORMALLY, AURAL WARNING COULD NOT BE SILENCED. REPLACED LT BODY GEAR SWITCH AND TARGET. REPLACED LT WING GEAR ALT TILSDR P5CA0601426Warning System · activatedFLIGHT CREW REPORTED AFTER T/O, GEAR AND FLAPS UP, GOT T/O WARNING HORN THAT COULD NOT BE SILENCED. WARNING HORN C/B ON P-6 PULLED TO SILENCE. INDICATION WERE LEFT WING TILT LIGHT ON IN ALT. RIGHT HAND BODY GEAR TILT LIGHT ON IN ALT. LOW SPEED BRAKE RELEASESDR EIA2006006Battery · malfunctionedFWD LAVATORY SMOKE DETECTOR LOW BATTERY ALTER TONE SOUNDING. REMOVED AND REPLACED SMOKE DETECTOR BATTERY, OPERATIONAL CK OK.SDR P5CA0601425Warning Horn · activatedDURING CLIMB, AURAL WARNING SOUNDED AT 1000 FT - GEAR UP FLAPS AT 5 DEGREES ON F/E PANEL GEAR SAFE LIGHT ON. LEFT WING TILT LIGHT ON, RIGHT BODY TILT LIGHT ON, LOW SPEED BK REL LIGHT ON. T/O PROT OFF LT ON. LATER ALL LIGHTS EXCEPT RT BODY TILT EXTINGUISHED SDR P5CA0501422Drive Assy · damagedADP CHUGGING, REPORTING NO PRESSURE. OPENED MEL 29-2BSDR P5CA0501416Metering Tube · leakingNR1 ENGINE FUEL LEAK AT FUEL METERING UNIT VBV ROD END TUBE. VBV ACTUATOR FUEL TUBE REPLACED AT FUEL CONTROL AND PERFORMED ENGINE RUN AND LEAK CHECK IAW MM 73-21-01.SDR P5CA0501414Coupler · defectiveFO'S HEADING, FLIGHT DIRECTOR, AND BOTH VOR FLAGS IN RMI CAME INTO VIEW WITH HEADING FLAG IN HSI. REMOVED AND REPLACED NR 2 COMPASS COUPLER IAW AMM 34-21-00.SDR P5CA0501410Rudder · out of positionCREW REPORTED LOWER RUDDER OFF TO LEFT 3 DEGREES WITH UPPER RUDDER NEUTRAL. CLEANED PLUG ON SURFACE POSITION INDICATOR, CYCLED RUDDER, ALL OPS AND INDICATIONS NORMAL IAW MM.SDR P5CA0501398Check Valve · failedAT FL 37.0 NR 3 ENGINE COMPRESSOR STALLED, ALL PARAMETERS NORMAL. OPS OK AT LOWER ALTITUDE. BORESCOPE PER MM 72-00-00 PG 680P, NO FINDINGS. FOUND 8TH STAGE CHECK VALVE FAILED. REPLACED SAME, OPS NORMAL PER 36-11-02.SDR EIA2005151Slide · unsecureUPPER DECK ESCAPE SLIDE NEEDS TO BE REPACKED. SLIDE REMOVED IAW EO 25-747-1780-05 REV B.SDR EIA2005148Light · inoperative5 EA EMERGENCY LIGHTS INOP. REMOVED AND REPLACED 5 EA EMERGENCY LIGHT ASSY PER B747 MM 33-51-07. OPS CHECKED GOOD PER B747 MM 33-51-0.SDR EIA2005147Access Panel · crackedA CRACK WAS FOUND ON NR 3 ENG, RT CORE COWL AT LOCATION OF ACCESS PANEL 473AR. REMOVED PREVIOUS REPAIRS, FAF0581021BBED NEW REPAIR PARTS AND INSTALLED PER ECRA 487-54-016-2.BSDR EIA2005144Skin · corrodedAFT LOWER CARGO DOOR INNER LOWER SKIN CORRODED SEVERAL PLACES. REMOVED CORROSION FROM FT LOWER C/D INNER SKIN PER B747 SRM 51-10-01 AND REPAIRED INNER LWR SKIN PER ECRA 487-52-002-2.SDR EIA2005142Stiffener · crackedTOP ON NLG BOX HAS CRACKED LONGITUDINAL STIFFENER AT LBL 26 STA 280-300. REPLACED STIFFENER PER B747 SRM 51-30-02 PGS 8-9 AND 51-30-05 PAGES 6-9.SDR EIA2005141Web · puncturedSTA 455 WL 247 STR 20R R1 DOOR INTERIOR WEB PUNCTURED. REPAIRED R1 DOOR INTERIOR WEB STA 455 WL 247 STR 20R PER ECRA 487-52-008-2.SDR EIA2005140Frame · crackedSTA 803 WL 215 1.5" BELOW STR 24R DOOR FRAME WEB HAS A CRACK. REMOVED DAMAGE AND REPAIRED DOOR FRAME STA 803 WL 215 STR 24R AREA PER ECRA 487-53-025-2.SDR EIA2005139Floorbeam · damagedFLOORBEAM WEB REPAIR BUCKLED AT STA 280 RBL 45. REPAIRED FLOORBEAM WEB STA 280 RBL 45 PER ECRA 487-53-010-2.SDR EIA2005138Frame · crackedFRAME STA 2231 STR 24L CRACK IN WEB INNER STRAP. REPAIRED CRACK AT STA 2231 WEB CUT OUT BETWEEN STR 24L AND 25L PER B747 SRM 53-10-01 FIG 1 DETAIL 1 AND ECRA 487-53-018-2.SDR EIA2005137Fitting · crackedCRACKED STR 38L AT BS 990 UNDER BATHTUB FITTING. REMOVED DAMAGE, NDT AREA, FABBED AND INSTALLED PARTS PER SRM B747 53-10-03 FIG 1, 51-10-02 AND SOPM 20-41-02.SDR P5CA0501372Skin · crackedCRACK AT NR 4 NACELLE STRUT TOP FORWARD CORNER OF PRECOOLER EXHAUST CUTOUT. PRECOOLER EXHAUST CUTOUT REPAIRED PER BOEING INSTRUCTIONS 1-1MNS9D AND FAA FORM 8100-9.SDR P5CA0501371Skin · wornWORN/CHAFING NR 3 NACELLE STRUT SKIN AROUND CUTOUT NR 12. NR 3 NACELLE STRUT SKIN AROUND CUTOUT REPAIRED PER BOEING INSTRUCTIONS 1-1MNB95 AND FAA FORM 8100-9.SDR P5CA0501370Vertical Beam · crackedFOUND 2 CRACKS AT VERTICAL WEB BEAM BS 280 AND ONE CRACK AT BS 320. VERTICAL WEB BEAM REPAIR ACCOMPLISHED PER BOEING MESSAGE 1-1MEI6G AND FAA FORM 8100-9.SDR P5CA0501369Structure · crackedRIGHT O/B ELEVATOR FOUND CRACKED AT LEADING EDGE AREA I/B OF ELEVATOR STATION 256.811 AND BRACKET CRACKED AT ELEVATOR STATION 256.811. RIGHT O/B ELEVATOR REPAIRED PER BOEING INSTRUCTIONS 1-1N575W AND FAA FORM 8100-9.SDR P5CA0501368Pressure Panel · crackedNOSE WHEEL WELL WEB AT STATION BS 400 STR 47R FOUND CRACKED AT RETRACT ACTUATOR CUTOUT. NOSE WHEEL WELL WEB REPAIRED AS PER BOEING MESSAGE 1-1MCB8E AND FAA FORM 8100-9.SDR P5CA0501373Engine · failedAFTER TAKEOFF NR 1 ENGINE FAILED. SHUT DOWN ENGINE AND JETTISON FUEL IAW CHECK LIST. AFTER SHUT DOWN OIL PRESSURE ZERO. NR 1 ENGINE REPLACED PER ENGINE CHANGE FORM 00-AA-45. RUN UP OK PER MM 71-00-00 TEST NR 3, 8 AND 9.SDR P5CA0501365Torque Tube · damagedNR 22 LEADING EDGE PANEL BROKEN. REPLACED NR 22 LEADING EDGE PANEL, 2 ROTARY ACTUATORS AND TORQUE TUBE. RIGGED AND OPS CHECK PER MM 27-81-00.SDR P5CA0501364Panel · brokenNR 22 LEADING EDGE PANEL BROKEN. REPLACED NR 22 LEADING EDGE PANEL, 2 ROTARY ACTUATORS AND TORQUE TUBE. RIGGED AND OPS CHECK PER MM 27-81-00.SDR P5CA0501363Actuator · failedNR 22 LEADING EDGE PANEL BROKEN. REPLACED NR 22 LEADING EDGE PANEL, 2 ROTARY ACTUATORS AND TORQUE TUBE. RIGGED AND OPS CHECK IAW MM 27-81-00.SDR P5CA0501350Wheel · failedCREW REPORTED HEARING TWO LOUD BANGS AFTER TAKEOFF. FOUND NR 8 TIRE BLOWN AND PANEL 193E MISSING. REPLACED NR 7 & 8 WHEEL ASSY'S.SDR P5CA0501358Structure · crackedNOSE GEAR WHEEL BOX STRUCTURE FOUND SEVERAL CRACKS AT STATION 320L BETWEEN WL 140 AND 150, AT STATION 300R BETWEEN WL 170 AND 180, AT STATION 300L AT WL 175. ACCOMPLISHED INTERIM REPAIR PER BOEING INSTRUCTIONS SEP-SIN-05-00574C AND 1-1HZQME AND FAA FORM 8100-
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