Boeing 747-123
Service difficulty reports · 2,292
Newest first. General aviation reporting is voluntary.
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 = '747123' 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 = '747123' 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 06017Battery Pack · dischargedEMERGENCY EXIT LIGHT AT STATION 460 INOP. FAILED TEST DURING A-CHECK. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY.SDR 06016Fuse · blownEMERGENCY EXIT SLIDE LIGHTS INOP. FAILED TEST DURING A-CHECK. REPLACED 2 FUSES IN THE EXIT LIGHT POWER SUPPLY MODULE.SDR P5CA0601435Wire · failedFLIGHT CREW REPORTED OUTBOARD AILERON LOCKOUT CIRCUIT BREAKER TRIPPING. REPLACED ACTUATOR, NO HELP. REPAIRED WIRE SPLICE AT S216 PER WDM 27-11-21. UNLOCKED AILERON LOCKOUTS AND RELEASED PER MEL 27-28.SDR UPS05445843Battery · dischargedEMERGENCY LIGHT OVER THE FLT DECK STAIRS INOP (LOW BATTERY). REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW MM 33-51-00, OPS NORMAL.SDR UPS05445732Link · crackedNR 4 NACELLE REAR ENGINE MOUNT THRUST LINK, CRACK INDICATION REVEALED AT FWD END LUG UPPER EXIT LIMIT. NR 4 ENG REAR MOUNT THRUST LINK REPLACED PER EO B747-7120-22596-A WORK CARRIED OUT ON TASK CARD APPENDIX-I NR 4 ENG REMOVED AND INSTALLED (FOR ACCESS) AS PESDR UPS05445731Link · crackedNR 3 NACELLE REAR ENGINE MOUNT THRUST LINK, CRACK INDICATION REVEALED AT AFT END LUG LOWER EXIT LIMIT. NR 3 ENG REAR MOUNT THRUST LINK REPLACED PER EO B747-7120-22596-A WORK CARRIED OUT ON TASK CARD APPENDIX-H. NR 3 ENG REMOVED AND INSTALLED (FOR ACCESS) AS SDR UPS05445720Link · crackedINSPECTION TYPE:AD NR 1 NACELLE REAR ENGINE MOUNT THRUST LINK, CRACK INDICATION REVEALED AT AFT END LUG EXCEEDED LIMIT. NR 1 ENG REAR MOUNT THRUST LINK REPLACED AS PER EO B747-7120-22596-A ON APPENDIX-F. ENG REMOVED AND REINSTALLED AS PER UPS TASK CARD TC 50SDR P5CA0501411Tire · failedON TAXI INTO BLOCKS NR 10 AND 12 THERMALED. REPLACED NR 9, 10, 11 AND 12 TIRES IAW MM 32-45-01.SDR UPS05445664Cowling · openN/A RTO BTB NR 4 ENG OB CORE COWL OPEN ON TAKE-OFF ROLL. REPLACED OB NR 4 ENG CORE COWLS PER MM 71-10-00.SDR UPS05445460Lamp · inoperativeUPPER DECK SERVICE DOOR EMERGENCY LIGHT INOP. RELAMPED PER MM 33-51-05 OPS CK OK.SDR UPS05445374Light · inoperativeEMERGENCY EXIT LIGHTS WILL NOT ARM WITH SAFETY SWITCH CLOSED. REPOSITIONED SWITCH ENGAGE HOOP. CHECKS OK.SDR P5CA0501397Actuator · malfunctionedAFTER ENGINE START, NR 1 ENGINE RAN FOR APPROX 3 MINUTES THEN SHUT DOWN. REPLACED NR 1 ENGINE SPAR VALVE ACTUATOR, MM 28-22-01.SDR P5CA0501390Valve · leakingFUEL LEAKING OUT OF LEFT WING OUTBOARD FRONT SPAR. RESEATED POPPED VALVE ON LEFT SPAR. INSPECTED OK NO LEAKS, OPS OK PER MM 28-11-04.SDR P5CA0501391Connector · looseNR 2 ENGINE SQUIB TEST FAILED ON FLIGHT ENGINEER PREFLIGHT. CLEANED AND RESEATED NR 2 ENGINE RT FIRE EXTINGUISHER BOTTLE SQUIB PLUG PER MM 26-11-00.SDR P5CA0501379Bolt · shearedRIGHT WING LANDING GEAR SUPPORT BEAM GATE BEARING ATTACHMENT SUPPORT UPPER VERTICAL BOLT SHEARED AND MIGRATED. REF IPC 57-15-05-0 ITEM 290. SHEARED BOLT REMOVED AND NEW BOLT /WASHERS/ NUT INSTALLED AND TORQUED IAW SRM 51-30-04 FIG 1 SHT 2 TABLE AND MM 57-15-SDR P5CA0501375Line · leakingNR 2 ENGINE FUEL LEAK. REPLACED NR 2 ENGINE FUEL LINE (DRY BAY AREA). LEAK CHECK OK PER MM 28-22-00.SDR UPS05444870Spar · crackedINSPECTION TYPE: C, LT WING REAR SPAR UPPER CHORD HORIZONTAL FLANGE FWD FASTENER HOLE AT WS 392 CRACK RUNNING AFT APPROX 0.080 INCH. LEFT WING REAR SPAR UPPER CHORD HORIZONTAL FLANGE FWD FASTENER HOLE REPAIRED AT WS 392 AREA AS PER HX RS R57-25-35337 & UPS EOSDR UPS05444869Skin · corrodedINSPECTION TYPE: C, AFT T/E PANEL REMOVED FOR RECTIFICATION WING UPPER SKIN LWR SURFACE FOUND CORRODED AT WS 390. CORROSION BLEND OUT 0.131 X 1.25 X 2.5 INCHES EXCEED SRM 57-30-01 FIG 1 LIMITS, LEFT WING UPPER SKIN LOWER SURFACE REPAIRED AT WS 390 AREA AS PERSDR UPS05444863Spar · crackedINSPECTION TYPE: C, RT SIDE OF BS 1241 UPPER REAR SPAR SIDE OF BODY SPLICE PLATE AREA NR 5 HOLE FOUND CORRODED CRACKED AT SPAR CHORD HORIZONTAL FLANGE LWR SURFACE WITH DEPTH 0.060 INCH & LENGTH 0.050 INCH APPROX. RIGHT BS 1241 UPPER CHORD BOLT HOLE NR 5 REPAISDR UPS05444864Fitting · crackedINSPECTION TYPE: C, RIGHT WING UPPER REAR SPAR SIDE OF BODY SPLICE PLATE AREA NR 5 FASTENER HOLE FOUND CRACK AT INTERNAL SPLICE FITTING (CRACK LENGTH .25 INCH). RIGHT WING INTERNAL SPLICE FITTING BOLT HOLE NR 5 REPAIRED AS PER HX RS R57-18-35333 & UPS EO B747SDR P5CA0501376Engine · failedAFTER TAKEOFF, NR 1 ENGINE FELT LARGE BANG ALONG WITH EGT OFF SCALE HIGH. SHUT DOWN ENGINE. REMOVED AND REPLACED NR 1 ENGINE MM 71-00-02.SDR UPS05444878Fitting · crackedINSPECTION TYPE:C RIGHT WING STA 1241 UPPER REAR SPAR SIDE OF BODY SPLICE FITTING NR 4 HOLE FOUND CRACK & COR AT INTERNAL SPLICE FITTING. RIGHT WING BS 1241 BOLT HOLE NR 4 HOLE REPAIRED AS PER SB B747-5740-17032.SDR UPS05444742Frame · crackedCARGO BAY, STA 2180 RBL 58 FRAME UPPER CHORD LWR SURFACE FOUND CRACKED. CRACK LENGTH 1.25 IN . CORROSION BLEND OUT N/A. CARGO BAY STA 2180 RBL 58 IN FRAME REPAIRED AS PER SRM 53-10-04 FIG 66.SDR UPS05444868Fitting · corrodedINSPECTION TYPE:C FX - LT STA 1241 FORGING TO KICK FITTING BOLT HOLES FOUND CORRODED (FINAL HOLE SIZE: 1.173 INCH). FORGING BOLT HOLE REPAIRED AS PER HX RS R53-43-35324 & UPS ENGINEERING FILE 747-53-20264.SDR UPS05444798Flange · crackedBS 910 RBL 11-33 LATERAL HAT SECTION FWD FLANGE FOUND CRACKED. CORROSION BLEND OUT 0.020 BY 1.0 BY 1.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, LATERAL HAT SECTION REPLACED AS PER SRM 51-10-01 PG 9.SDR UPS05444877Bracket · corrodedINSPECTION TYPE: C, FX KEELBEAM BOX INTERIOR SUPPORT ROD ATTACH BRACKET FOUND CORROSION AT STA 1240 LBL 3 BOX TOP AREA. CORROSION BLEND OUT 0.051 X .5 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. BRACKET REPLACED AS PER SRM 51-10-01 PG 9 AT BS 1240 LBL 3 AREA.SDR UPS05444800Seat Track · corrodedSTA 783 LBL 11 SEAT TRACK RT FLANGE CORROSION. CORROSION BLEND OUT 0.019 BY 0.75 BY 1.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14 AT BS 723- BS 857 LBL 11 AREA WORK DETAIL REF NRC NR 6006.SDR UPS05444799Seat Track · corrodedBS 800 TO 840 LBL 11 SEAT TRACK NECK FOUND CORRODED. CORROSION BLEND OUT 0.052 BY 1.0 BY 2.0 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14 AT BS 723 TO BS 857 LBL 11 AREA.SDR UPS05444747Frame · crackedBS 900 LT FRAME O/B FLANGE FOUND CRACKED BTN S-12L AND S-13L. CRACK LENGTH 0.4375 IN. CORROSION BLEND OUT N/A. BS 900 LT FRAME O/B FLANGE BETWEEN STR 12L AND 13L AREA REPAIRED AS PER SRM 53-10-04 FIG 4.SDR UPS05444802Stringer · crackedFX LT TUNNEL STR 41 AFT END CRACKED BETWEEN STA 260-280, CRACK LENGTH 0.75 IN. FX BS 260-280 STR 41L STRINGER REPLACED AS PER SRM 51-10-01 PG 9.SDR UPS05444797Seat Track · corrodedTIE DOWN TRACK BS 1483 RBL 97 CORRODED. CORROSION BLEND OUT 0.080 BY 0.75 BY 1.25 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.SDR UPS05444715Pressure Panel · crackedAD LT NLG WW SIDE PANEL WEB FOUND 2 LOCATIONS CRACKED BETWEEN STA 265 AND 280, WL 160 AND 170. CRACK LENGTH APPROX 1 INCH. LT NLG WW SIDE PANEL WEB REPAIRED AT BETWEEN BS 265 AND 280 WL 160 AND 170 AREA AS PER SRM 53-10-04 FIG 116. SUBSEQUENT INSP NECESSARYSDR UPS05444801Floorbeam · crackedAFT CARGO BAY BS 1800 BL 0 AND FLOORBEAM UPPER FLANGE CRACKED. CRACK LENGTH 2.5 IN. AFT CARGO BAY BS 1800 LBL 22 TO RBL 40 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2.SDR UPS05444468Floorbeam · damagedFLOORBEAM AT STA 1800 HAS ELONGATED HOLES. A/C OOS AND WILL REQUIRE MX FERRY (9127) TO SAT. INSTALLED FREEZE PLUG AT STA 1800 LBL 99 IN FLOORBEAM IAW SA SK 675-800542.SDR P5CA0501346Warning System · inoperativeON PRE-FLIGHT, FOUND NO T/O WARNING ALTITUDE SELECT OR AUTOPILOT DISCONNECT WARNINGS. REPLACED AURAL WARNING DEVICE. OPS CHECK NORMAL IAW 31-26-02.SDR 05024Fire Detector · malfunctionedLOWER AFT CARGO COMPARTMENT FIRE WARNING LIGHT ILLUMINATED AND BELL SOUNDED (WITH CARGO HEAT ON). INSPECTED LOWER AFT CARGO COMPT FOR SIGNS OF FIRE. NO INDICATION OF FIRE FOUND. CANNOT DUPLICATE ON GROUND. INSPECTED THE CARGO HEATING SYSTEM. NO DEFECTS FOSDR UPS05444027Control Module · intermittentINSPECTION TYPE:N/A EMERGENCY LIGHT CONTROL SWITCH INTERMITTENT FOR EMERGENCY LIGHTS. REMOVED AND REPLACED EMERGENCY LIGHTS CONTROL MODULE AS PER MM 33-51-09, OPS CHECKS OK.SDR UPS05444007Rib · crackedINSPECTION TYPE:C RIGHT W ILES 1057.55, 21 V/C FLAP I/B ARM O/B RIB MULTI CRACKS FOUND DURING RIB INSTALLATION WITH RIVET (CRACK LENGTH 1 TO 3 INCH). RIGHT WING 21 VC FLAP I/B ARM O/B RIB TOP FLANGE REPAIRED AS PER HX RS R-57-41-35262 AND UPS EO B747-5740-218SDR UPS05444004Support Fitting · crackedINSPECTION TYPE:C M/D BS 1960 RBL 60 FLOOR TRACK SUPPORT FITTING 2EA FOUND CRACKED. SUPPORT FITTINGS REPLACED PER SRM 51-10-01 PG 9.SDR UPS05443996Skin · damagedINSPECTION TYPE:C FX LAP JOINT AT BS 1867 TO 1877 STR 46L FOUND LOSS OF SKIN THICKNESS DUE PREVIOUSLY BLENDED 0.013 X .5 X 4 INCH. LAP JOINT OPENED UP FOR INSPECTION FOR DEFECTS FREE, LAP JOINT REINSTALLED PER HX RS R-53-60-35259 AND UPS EO B747-5330-21779-ASDR UPS05443992Floorbeam · corrodedBS 1700 LBL 58 - 76 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.045 X 2 X 2 INCH, M/D BS 1700 BL 0 TO LBL 69 FLOORBEAM REPAIRED AS PER SRM 53-10-07 FIG 12.SDR UPS05443971Floorbeam · corrodedINSPECTION TYPE: C, BS 1700, RBL 11 - 33 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.050 X 2 X 2 EXCEED SRM 53-10-01 FIG 1, LIMIT FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 1.SDR UPS05443945Attach Fitting · corrodedINSPECTION TYPE:C - BS 2100 RBL 90 - 98 FLOORBEAM ATTACH SPLICE CORROSION FOUND CORROSION BLEND OUT 0.035 X 1 X 2.5 EXCEED SRM 53-10-01 FIG 1, LIMIT. SPLICE REPLACED AS PER SRM 51-10-01 PG 9.SDR UPS05443944Seat Track · corrodedINSPECTION TYPE: C - BS 2060 - 2140 RBL 98 SEAT TRACK CORROSION FOUND. CORROSION BLEND OUT 0.042 X 1 X 3 EXCEED SRM 53-10-01 FIG 1, LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9.SDR UPS05443943Seat Track · corrodedINSPECTION TYPE: C, BS 2060 LBL 70 INCH SEAT TRACK CORROSION FOUND. CORROSION BLEND OUT 0.045 X 1 X 2 EXCEED SRM 53-10-01 FIG 1, LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9.SDR UPS05443942Cargo Track · crackedINSPECTION TYPE: C, BS 2060 - 2140, RBL 90, TIE DOWN TRACK FLANGE FOUND CORROSION CRACK (CRACK LENGTH 1 INCH). TIE DOWN TRACK REPLACED AS PER SRM 51-10-01 PG 9.SDR UPS05443980Attach Angle · crackedINSPECTION TYPE:C, BS 440 RBL 55 INTERCOSTAL WEB ATTACH ANGLE CRACKED (CRACK LENGTH .75 INCH). ANGLE REPLACED AS PER SRM 51-10-01 PG 9.SDR UPS05443979Attach Angle · crackedINSPECTION TYPE: C, BS 420 RBL 55 INTERCOSTAL WEB ATTACH ANGLE CRACKED (CRACK LENGTH 1 INCH). ANGLE REPLACED AS PER SRM 51-10-01 PG 9.SDR UPS05443977Cargo Track · corrodedINSPECTION TYPE:C M/D- BS 480-500 LBL 68 TIE DOWN TRACK O/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.039 X 1 X 2 EXCEED SRM 53-10-01 FIG 1, LIMIT TIE DOWN TRACK REPLACED AS PER SRM 51-10-01 PG 9.SDR UPS05443976Cargo Track · corrodedINSPECTION TYPE: C, BS 480-510 LBL 66 TIE DOWN TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.041 X 1 X 3 EXCEED SRM 53-10-01 FIG 1, LIMIT TIE DOWN TRACK REPLACED AS PER SRM 51-10-01 PG 9.
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