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 = '7478' 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 = '7478' 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 2026F00033Connector · burnedDURING ROUTINE MAINTENANCE, REMOVAL OF A RACK AND ITS ELECTRICAL COMPONENTS, IT WAS NOTICED THAT A ELECTRICLA CONNECTOR (PLUG/RECEPTACLE) STABILIZER FUEL PUMP WIRING, HAD NOT BEEN PROPERLY CONNECTED. WHEN THE DISCONNECTING THE PLUG, IT WAS FOUND THAT TWO PINSSDR 2025FA0000632Stringer · multiple failPERFORMED GENERAL VISUAL INSPECTIONS OF STINGER SPLICE JOINTS ON AIRCRAFT. THESE LOCATIONS FALL OUTSIDE OF THOSE CURRENTLY IDENTIFIED BY AD’S AND SB’S FOR INSPECTION. IDENTIFIED THE FOLLOWING STRINGER CRACKS: STA 1000: S-2L, S-2AL, S-13R STA 1480: S-14R, S-19LSDR 2025FA0000631Stringer · multiple failPERFORMED INSPECTIONS IAW BOEING SERVICE BULLETIN 747-53-2908. IDENTIFIED CRACKS IN STRINGERS AT THE FOLLOWING LOCATIONS: STA 740: S-3AL, S-17L, S-18L, S-19L, S-22AL, S-23L, S-25L, S-40L, S-41L, S-43L, S-44L, S-46L, S-47L, S-1R, S-2AR, S-4R, S-5R, S-17R, S-18SDR 2025FA0000621Stringer · crackedPERFORMED INSPECTIONS PER AD-2023-12-18 IAW BOEING REQUIREMENTS BULLETIN 747-53A2907. IDENTIFIED CRACKS IN STRINGERS AT THE FOLLOWING LOCATIONS: STA 1740: S-13L, S-14L, S-14R, S-15R STA 1960: S-1L, S-2L, S-3L, S-4L, S-6L, S-8L, S-9L, S-10L, S-11L, S-12L, S-SDR 2025FA0000620Stringer · crackedPERFORMED INSPECTIONS PER AD-2023-14-03 IAW BOEING REQUIREMENTS BULLETIN 747-53A2911. IDENTIFIED CRACKS IN STRINGERS AT THE FOLLOWING LOCATIONS: STA 2598: S-4R, S-5R, S-25R, S-4L, S-5L, S-8L, S-10LSDR B72R202507220001Stringer · crackedOPERATOR OF A 747-8 REPORTED THAT WHILE INSPECTING THE CROWN SKIN, STRINGERS, AND FRAME FOR CORROSION INHIBITING COMPOUND (CIC) AND FOREIGN OBJECT DEBRIS (FOD), MULTIPLE TRANSVERSE STRINGER CRACKS WERE FOUND COMMON TO S-1L, S-3L, S-5L, S-12L, AND S-12R BETWEESDR 2025FA0000281Link · looseAXIAL LINK FAN COWL TO AGB AFT BEARING LOOSE BOTH SIDES --- SN F1A0RHFT AND F1A0RHFKSDR 2025FA0000255Panel · crackedLH WING UPPER SKIN PANEL FOUND CRACKED, DELAMINATED, FOUND DURING INSPECTION PER B223914; EXTERNAL - GV: WING UPPER SKIN PANELS. TO INCLUDE: FORWARD OF LEADING EDGE SPAR, FRONT SPAR TO REAR SPAR, & AFT OF REAR SPAR. ACCESS NOTE: UPPER WING SKIN LOWER SURFACE -SDR IPXA2024102107037Lens · inoperativeTHE LENS OF€?CAUTION RAILS UP€? LIGHT AT STA 400 IN MAIN DECK MISSING. REMOVED AND REPLACED €ŒCAUTION RAILS UP€? LENS IAW AMM 33-34-02. OPS CHECK GOOD.SDR IPXA2024102197331Stringer · crackedMAJOR REPAIR, STRINGER CRACK, FWD SIDE OF STA 740 S-44L (REPAIR) ACCOMPLISHED REPAIR I.A.W UPS EO-91707-REQ1 REV.1 AND 747-8F SRM53-20-03-2R-5 REV.44 EGAT WORK SHEET NO.40902.SDR IPXA2024101997273Stringer · crackedSTRINGER CRACK, FWD SIDE OF STA 740 S-46L (REPAIR) ACCOMPLISHED REPAIR I.A.W UPS EO-91709-REQ1 REV.1 AND SRM 53-20-03-2R-5 REV.44 AND EGAT WORK SHEET NO.40904.SDR IPXA2024101997254Stringer · crackedSTRINGER CRACK, FWD SIDE OF STA 740 S-47R (REPAIR) ACCOMPLISHED REPAIR I.A.W UPS EO-91711-REQ1 REV.1 AND 747-8F SRM 53-20-03-2R-5 REV.44 AND EGAT WORK SHEET NO.40906. REVIEWED TASK PER GMM-MTX 09.05.01.09.SDR UIEA2024100600966A/C Pack · warning messageIN FLIGHT AT FL 360 RECEIVED A PACK 3 CAUTION MSG. RESET PACK PER CHECKLIST AFTER 90 SECONDS RECEIVED PACK 3 MSG AGAIN.(<P>CMC MSG - 21962 33 PACK INOP. RESET PACK 2 IAW AMM 21-51-00-740-802, OPS CHECK GOOD. TRANSFER PACK 3 TO DMI 218252 IAW MEL 21-51-01-01-SDR IPXA2024102154916Stringer · crackedSTRINGER CRACK, FWD AND AFT SIDE OF STA 2180 S-10R. (REPAIR) ACCOMPLISHED REPAIR I.A.W. UPS EO-91748-REQ1 REV.1 AND 747-8F SRM 53-60-03-2R-3 REV.44 AND EGAT WORK SHEET NO.40868. REVIEWED TASK PER GMM-MTX 09.05.01.09.SDR IPXA2024101953788Stringer · crackedMAJOR REPAIR, STRINGER CRACK, FWD SIDE OF STA 2180 S-17L. (REPAIR) PERFORM REPAIR I.A.W EGAT WORK SHEET NO.40871(SRM 53-60-03-2R-3 REV.43) AND EI NO.F2024A53M-2560 REV.1 AND EO-91745-REQ1 REV.1. JOB COMPLETED.SDR IPXA2024101954940Stringer · crackedMAJOR REPAIR, STRINGER CRACK, AFT SIDE OF STA 2180 S-9R. (REPAIR) REPAIR DAMAGE AREA I.A.W. UPS EO-91747-REQ1 REV.1 AND SRM 53-60-03-2R-3 REV.44 AND EGAT WORK SHEET NO.40874. JOB COMPLETED AND ATTACHMENTS ARE UPLOADED.SDR IPXA2024102154622Stringer · crackedMAJOR REPAIR, STRINGER CRACK, FWD SIDE OF STA 1740 S-20R. (REPAIR) PERFORM REPAIR I.A.W EGAT WORK SHEET NO.40860(SRM 53-60-03-2R-5 REV.44) AND EI NO.F2024A53M-2697 REV.1 AND EO-91715-REQ1 REV.1. JOB COMPLETED.SDR IPXA2023095663531Unknown · unknown*** SDR FILED OPEN *** LIGHTNING STRIKE DAMAGE FOUND ON LEFT SIDE OF FUSELAGE @STA 880, BWL 118. DAMAGE CENTERED AROUND 4 RIVETS APPROXIMATELY 1INCH APART. ACCOMPLISHED LIGHTNING STRIKE INSPECTION IAW AMM 5-51-13. NO OTHER FAULTS FOUND.SDR UIEA2023082200781Unknown · unknownCRACK - STRINGER OF FUSELAGE STA 880 S9L(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-6 REV 40 AND DWG 142U3312 SH 8 REV C. 2) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)SDR UIEA2023082200782Unknown · unknownCRACK - STRINGER OF FUSELAGE STA 880 TO STA 900 S10R(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-6 REV 40 AND DWG 142U3725 SH 19 REV -. 2) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)SDR UIEA2023082200783Unknown · unknown1) CRACK - STRINGER OF FUSELAGE STA 820 S12L(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-1 REV 40 AND DWG 142U3312 SH 8 REV C AND EI T2023A53M-2151 REV 0. 2) ACCOMPLISHED EI T2023A53M-2151 REV 1 AND EI ATTACHED TO W/OO 8538401 (066). 3) CONDITION CHECK NORMSDR UIEA2023082200784Unknown · unknownCRACK - STRINGER OF FUSELAGE STA 880 S12L(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-1 REV 40 AND DWG 142U3312 SH 8 REV C AND EI T2023A53M-2151 REV 0. 2) ACCOMPLISHED EI T2023A53M-2151 REV 1. 3) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)SDR UIEA2023082200785Unknown · unknownCRACK - STRINGER OF FUSELAGE STA 820 S12R(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-1 REV 40, DWG 142U3312 SH 8 REV C AND EI T2023A53M-2152 REV 0. 2) ACCOMPLISHED EI T2023A53M-2152 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL. 4) ORIGINAL EI ATTACHESDR UIEA2023082200786Unknown · unknownCRACK - FOUND MAIN DECK STRINGER CRACK STA 760 S12R(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-1 REV 40, DWG 142U3312 SH 8 REV C AND EI T2023A53M-2152 REV 0. 2) ACCOMPLISHED EI T2023A53M-2152 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL. 4) ORIGINAL SDR UIEA2023082200787Unknown · unknownCRACK - STRINGER OF FUSELAGE STA 980 - 1120 S12L(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-1 REV 40 AND DWG 142U3312 SH 8 REV C. 2) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)SDR UIEA2023082200788Unknown · unknownCRACK - FOUND MAIN DECK STRINGER CRACK STA 780 S12R(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-1 REV 40, DWG 142U3312 SH 8 REV C AND EI T2023A53M-2152 REV 0. 2) ACCOMPLISHED EI T2023A53M-2152 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2023082200789Unknown · unknownCRACK - STRINGER OF FUSELAGE STA 860 S12R(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-1 REV 40, DWG 142U3312 SH 8 REV C AND EI T2023A53M-2152 REV 0. 2) ACCOMPLISHED EI T2023A53M-2152 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL. 4) ORIGINAL EI ATTACHESDR UIEA2023082200790Unknown · unknownCRACK - FOUND MAIN DECK STRINGER CRACK STA 840 S12R(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-1 REV 40, DWG 142U3312 SH 8 REV C AND EI T2023A53M-2152 REV 0. ACCOMPLISHED EI T2023A53M-2152 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL. 4) ORIGINAL EI SDR UIEA2023082200791Unknown · unknownCRACK - STRINGER OF FUSELAGE STA 980 + 160 S12L(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-1 REV 40 AND DWG 142U3312 SH 8 REV C. 2) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)SDR UIEA2023082200792Unknown · unknownCORROSION - SEAT TRACK STA 1980 LBL 98.58(<P>1) REMOVED THE AFFECTED FASTENER IAW SRM 51-40-02-0G-0 REV 40. 2) PERFORM EI T2023A53M-2031 REV 0 SEQ A AND DWG 146U5234 SH 40 REV - & 146U5406 SH 42 REV -. 3) ACCOMPLISHED EI T2023A53M-2031 REV 1. 4) JOB COMPLETED SDR UIEA2023082200793Unknown · unknownCORROSION - FITTING AT STA 2360 RBL 35(<P>1) IAW AMM 53-44-00-200-801 REV 42 REMOVED M/D CGO FITTING AT STA 2360 RBL 35. 2) ACCOMPLISHED EI T2023A53M-2131 SEQUENCE A REV 0. 3) IAW AMM 53-44-00-200-801 REV 42 INSTALL M/D CGO FITTING AT STA 2360 RBL 35. 4) CONDISDR UIEA2023082200794Power Supply · unknownFOUND EMERGENCY LIGHT INOP (EQUIPMENT NUMBER L6690, L1533, L5735, L1853 & L1854) TOTAL 5(<P>IAW AMM 33-51-10-962-001, 33-51-09-960-901, 33-51-04-000-803 & 33-51-04-400-803 REV 41 R/R SLIDE LIGHT AND INERTIA REEL LIGHT LAMPS, M5170 POWER SUPPLY AND PERFORMED EMSDR IPXA2023020769915Light · inoperativeEMERGENCY LIGHTS INOP RNRD SUPPLY BATTERY, AMM 33 51 04SDR IPXA2022103121417Smoke Detector · false activationCARGO DET FWD 1 STATUS MESSAGE APPEARED INTERMITTENTLY THROUGHOUT FLIGHT AND AFTER LANDING BUT NOT PRESENT AFTER SHUTDOWN. SMOKE DEDECTOR FWD CARGO FWD 1 REPLACED IAW AMM 26-16-014-401 REV 39.04. SATISSDR IPXA2022080832914Structure · damagedFOUND A HOLE AT AFT FUESLAGE STA 1980 WL 120 AMC SHOWS REPAIR COMPLETE PER EO-84363-REQ1 .SDR IPXA2022033180699Rod · inoperativeINSPECTION TYPE:N/ACREW ENTRY DOOR LWR VENT FLAP ROD BENT REF AIPC 52 11 19 01 ITEM 340R&R'D CREW ENTRY DOOR LWR VENT FLAP ROD REF MM CHPTR 52 11 19 OP CK GOODSDR IPXA2021122477225None · noneINSPECTION TYPE:N/A** ATB ** NO EMERG DEC'D** A/C LANDED WITHOUT INCIDENT**MEMO MESSAGE - "VMO GEAR DOWN" VMO SPEED LIMITS WITH GEAR DOWN MESSAGE.REF TO IFIM 31-50-00-810-808 REPOSITIONED VMO GEAR DOWN DISPATCH SW TO NORMAL & MSG ERASED. A/C OK FOR SERVICE.SDR 2021FA0000374Skin · crackedSUBJECT OUTBOARD ELEVATOR ASSEMBLY WAS RECEIVED IN FOR REPAIRS. THE ELEVATOR'S UPPER SKIN PANEL FASTENERS HAD WORKED LOOSE, AND THE FIBERGLASS SKIN PANEL'S ATTACHMENT HOLES HAD BECOME ELONGATED. FURTHER VISUAL INSPECTION OF THE ELEVATOR ASSEMBLY LOCATED CRACSDR 2021F00398Skin · crackedSUBJECT OUTBOARD ELEVATOR ASSEMBLY WAS RECEIVED IN FOR REPAIRS. THE ELEVATOR'S UPPER SKIN PANEL FASTENERS HAD WORKED LOOSE, AND THE FIBERGLASS SKIN PANEL'S ATTACHMENT HOLES HAD BECOME ELONGATED. FURTHER VISUAL INSPECTION OF THE ELEVATOR ASSEMBLY LOCATED CRACSDR IPXA2021110375573None · brokenINSPECTION TYPE:N/AGROUNDED SWITCH FOR EMERGENCY LIGHT BROKENREPLACED GROUND PER AMM 20-51-00 OPS TEST GOOD.SDR IPXA2020030552831Warning System · activatedINSPECTION TYPE:NA**ATB - SDR FILED OPEN** FUEL X FEED 4 EICAS ON TAKE OFF CLIMBING THRU 2000 FT NO VALVE LOGIC FLOW BARS ON FUEL SYNOPTIC PAGE AIR TURN BACK. NO EMERGENCY DECLARED. NO FUEL DUMPED. PLACED ON DEFERRAL M700858 PER MEL 28-22-3-1-1 DMP COMPLISDR IPXA2020022865516Warning Switch · inoperativeL1 DOOR IND INOP. TRANSFERRED TO DI LOG IAW MEL 52-71-1-1 DMP C/WREPLACED L1 DOOR WARNING SWITCH IN REF TO MM 52-71-01, TEST NORMAL. THIS CLEARS ESR 52-71-01-03-025.SDR IPXA2020022645439Switch · dirtyINSPECTION TYPE:N/AENTRY 1 DOOR LIGHT WILL NOT EXTINGUISH WHEN DOOR CLOSEDT/S PER FIM 52-71-00-810-801. NO EXISTING FAULT FOUND, CLEAN AND ADJUST 1L WARNING SW S29 PER AMM 52-71-01-400-805. A/C OK FOR SVC. THIS CLEARS M699885SDR IPXA2020022645437Indication Sys · malfunctionedINSPECTION TYPE:N/AL1 ENTRY DOOR OPEN DOOR DOES NOT INDICATE OPEN ON SYNOPTIC DISPLAY OR EICAS.PERFORMED OPERATIONAL TEST OF DOOR WARNING SYSTEM FOR MAIN ENTRY L1 DOOR IAW AMM 52-71-00-700-801. OPS CK GOOD. NO DEFAULT NOTED AT THIS TIME. THIS CLEARS M699840.SDR B72R2020027000183Stringer Splice · crackedAFTER REMOVAL OF INSULATION BLANKETS IN PREPARATION FOR AIRFRAME MAJOR ALTERATION AT AIRCRAFT COMPLETION CENTER, A CRACK 1.80 LONG WAS DISCOVERED AT STATION 1960 STRINGER SPLICE ON STRINGER S-10L. FURTHER INSPECTION OF OTHER STRINGERS DETECTED CRACKS IN MULTISDR B72R20200270182Stringer Splice · crackedAFTER REMOVAL OF INSULATION BLANKETS IN PREPARATION FOR AIRFRAME MAJOR ALTERATION OF AIRCRAFT COMPLETION CENTER, A CRACK 1.80 LONG WAS DISCOVERED AT STATION 1960 STRINGER SPLICE ON STRINGER S-10L. FURTHER INSPECTION OF OTHER STRINGERS DETECTED CRACKS IN MULTISDR IPXA2019112749474Switch · failedBLEED DUCT LEAK MESSAGE IN CRUISE. MESSAGE REMAINED. EMERGENCY DECLARED AND DIVERTED TO DEPARTURE. BLEED DUCT LEAK MESSAGE IN CRUISE. MESSAGE REMAINED. TROUBLESHOT TO BAD TEMP SWITCH S877. RT WING LE SWAPPED WITH S876. SYSTEM OPS NORMAL IAW AMM 26-11-00-501SDR IPXA2019111869048Status Message · activatedINSPECTION TYPE:N/AIN FLIGHT GOT "GEAR MONITOR" STATUS MESSAGE.PSEU GND TEST I.A.W. AMM 32-61-00 REV. 30.10 "PASS", NEVERTHELESS CLEANED R/H WING GEAR UPLOCK SENSORS. A/C O.K. FOR FLIGHT.SDR IPXA201910047489Panel · corrodedINSPECTION TYPE: C1, CORROSION ON THE INBD LWR PANEL (P/N: 313U8740-1) OF PYLON #3.REPAIR I.A.W. SRID: 4-4594220677 AND EO B747-5450-74170-A.SDR IPXA201910047488Panel · corrodedINSPECTION TYPE: C1, CORROSION ON THE INBD LWR PANEL (P/N: 323U8704-2) OF PYLON #1.REPAIR I.A.W. SRID: 4-4594281148 AND UPS EO B747-5450-74169-A.
Back to Boeing 747-8