Boeing 737-752
Service difficulty reports · 2,590
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 = '737752' 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 = '737752' 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 SWAA2015073042368Seat Track · crackedFORWARD SEAT TRACK FASTENER HOLES CRACKED AT BS 727B, LBL 24.75, OUTBOARD FORWARD, OUTBOARD AFT, INBOARD FORWARD & INBOARD AFT. REPAIRED SEAT TRACK PER ER & EA.SDR SWAA2015073042367Seat Track · crackedFORWARD SEAT TRACK FASTENER HOLES CRACKED AT BS 727B, LBL 45.5, OUTBOARD FORWARD, OUTBOARD AFT, INBOARD FORWARD & INBOARD AFT. REPAIRED SEAT TRACK IAW ER & EA.SDR SWAA2015070841566Rib · crackedLEFT HORIZONTAL STABILIZER INTERIOR CRACKED RIB AT STATION 92.70, 20" AFT FROM THE FWD LOWER SPAR CHORD, AT THE LOWER RADIUS INBD SIDE OF RIB. REPAIRED RIB IAW SRM.SDR ASMF201507015Window · crackedCAPTAIN REPORTED THAT AT 39,000 FEET, THE LT WINDOW NR 1 CRACKED. ACCOMPLISHED THE QRH 1.14 PROCEDURE, CONFIRMING THE FAILURE & CONTINUING TO DESTINATION. REPLACED THE LT WINDOW NR 1 & WINDOW HEAT CONTROLLER MODULE IAW AMM 56-12-11 & AMM 30-41-11, TESTED CORSDR ASMF201507013Hydraulic Line · leakingDURING TRANSIT CHECK, A HYD LEAK WAS DETECTED IN THE HYD SYS B OF THE ENG DRIVEN PUMP. PERFORMED REVISION DETECTING HYD LEAK AT HYD SYS B OF THE ENG DRIVEN PUMP HYD PRESS LINE. THE HYD PRESS LINE WAS CLEANED & TIGHTENED IAW AMM 29-11-11. AS PRECAUTIONARY ACSDR SWAA2015082443151Skin · crackedFUSELAGE SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW EA & ER.SDR SWAA2015081442841Window Frame · crackedRIGHT NR 3 FLIGHT DECK WINDOW FRAME CRACKED IN 2ND FASTENER HOLE FROM BOTTOM OF E - F POST. REPAIRED FRAME IAW SAM.SDR SWAA2015071041746Frame · crackedFUSELAGE FRAME CRACKED AT BS 500C, STRINGER 8L. REPAIRED FRAME IAW EA.SDR SWAA2015071041745Frame · crackedFUSELAGE FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.SDR SWAA2015071041744Frame · crackedFUSELAGE FRAME CRACKED AT BS 727B, STRINGER 8R. REPAIRED FRAME IAW EA.SDR SWAA2015071041743Frame · crackedFUSELAGE FRAME CRACKED AT BS 500C, STRINGER 8R. REPAIRED FRAME IAW EA.SDR SWAA2015071041742Frame · crackedFRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED FRAME IAW EA.SDR SWAA2015071041741Frame · crackedFRAME CRACKED AT BS 747, STRINGER 8R. REPAIRED FRAME IAW EA.SDR SWAA2015071041740Frame · crackedFRAME CRACKED AT BS 440, STRINGER 8R. REPAIRED FRAME IAW EA.SDR SWAA2015071041739Frame · crackedFRAME CRACKED AT BS 440, STRINGER 8L. REPAIRED FRAME IAW EA.SDR ASMF201507011Sensor · out of alignmentAIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF THE AUTO SLATS FAIL LIGHT TURNED ON. PERFORMED FIM 27-32 TASKS 801 & 809 PROCEDURES, SHOWING FAILURE CODE 27-31004 & DETECTING THE ANGLE OF ATTACK SENSOR OUT OF ALIGNMENT. THE ANGLE OF ATTACK SENSOR WAS ALIGNMESDR SCNA20150526114Lamp · inoperativeEMERGENCY LIGHT AT DOOR R2 IS OUT. REPLACED THE LAMP.SDR SWAA2015051339634Window · arcedL2 WINDOW ARCED IN RT CORNER. R & R L2 WINDOW IAW AMM.SDR ASMF201506005Actuator · leakingDURING TRANSIT CHECK, IT WAS DETECTED A HYD LEAK IN THE LT MLG RETRACT ACTUATOR. ACFT WAS SENT TO THE HANGAR. REPLACED THE LT MLG RETRACT ACTUATOR IAW MM 32-32-11, TESTED CORRECT.SDR ASMF201506002Gcu · failedAIRCRAFT PERFORMED AN UNSCHEDULED LANDING DUE TO SOURCE OFF, GEN OFF & BUS ON LIGHTS TURNED ON. THE FLIGHT CREW ACCOMPLISHED THE QRH 6.4 PROCEDURE & APU WAS NOT STARTED, CONFIRMING THE FAILURE. PERSONNEL REVISION DETECTING LT IDG FAILED, SO THE LT IDG WAS DESDR ASMF201503025Winglet · damagedCAPTAIN INFORMED THAT DURING FLIGHT ACFT RECEIVED A LIGHTNING STRIKE. ACFT WAS SENT TO THE HANGAR & LIGHTNING STRIKE INSPECTION WAS PERFORMED IAW MM05-51-19. DETECTED DAMAGED OUT OF LIMITS ON RT WINGLET. NON-ROUTINE CARD A022497 WAS GENERATED FOR REPLACING SDR SCNA20150310049Lamp · inoperativeEMERGENCY EXTERIOR LIGHT AT DOOR R2 BURNED OUT. R & R LAMP.SDR ASMF201503019Actuator · failedAIRCRAFT RETURNED TO PLATFORM DUE TO TAKEOFF CONFIGURATION ALARM WAS ACTIVE. PERFORMED BITE TO FSEU IAW FIM 31-51 TASK 801, NO CONFIRMING FAILURE, TESTED CORRECT. THE ACFT WAS SENT TO THE HANGAR & AS PRECAUTIONARY ACTIONS, THE AUTO SPEED BRAKE ACTUATOR WAS RSDR SWAA2015022636924Light · inoperativeR2 DOOR EMER EXIT LIGHT INOPERATIVE. R & R BULB IAW AMM.SDR SWAA2015022636923Light · inoperativeL2 DOOR EMER EXIT LIGHT INOPERATIVE. R & R LIGHT IAW AMM.SDR ASMF201503016Pump · leakingAIRCRAFT RETURNED TO PLATFORM DUE TO DURING RT ENG START, A FUEL LEAK WAS DETECTED. THE PLATFORM WAS CLEANED BY FIREMEN & MX PERFORMED REVISION, DETECTING FUEL LEAK IN THE MAIN FUEL PUMP DRAIN PORT. THE RT ENG WAS MOTORING, AFTER IT WAS STARTED & ENG OPERATISDR ASMF201503015Static Inverter · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE ELEC LIGHT TURNED ON. PERFORMED ELEC SYS AUTO TEST IAW FIM 34-31 TASK 801, DETECTING THE STATIC INVERTER WITH FAILURE. THE STATIC INVERTER WAS REPLACED IAW AMM 24-34-21, TESTED CORRECT.SDR SWAA2015022436851Light · inoperativeL2 DOOR EXTERIOR EMER LIGHT INOPERATIVE. REPAIRED LIGHT IAW MM.SDR SWAA2015021936725Connector · disconnectedL2 DOOR EMER EXIT LIGHT INOPERATIVE. CONNECTED CONNECTOR IAW SWPM & AMM.SDR SWAA2015021936724Lens · dirtyEXTERIOR EMER EXIT LIGHT LENS DIRTY. CLEANED LENS IAW AMM.SDR SWAA2015021836700Slide · out of adjustR2 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM.SDR SWAA2015021836699Slide · out of adjustL2 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM.SDR ASMF201503011Generator · failedAIRCRAFT RETURNED TO PLATFORM DUE TO AFTER LT ENG START, THE LT ALTER ENG & ENG CONTROL LIGHTS TURNED ON. PERFORMED BITE TO LT EEC IAW FIM 73-21 TASK 804 & 73-27 TASK 805 PROCEDURES, SHOWING FAILURE CODES 73-21-271, 73-11281 & 73-20211. THE GEN & EEC WERE RESDR ASMF201503007Blade · vibrationDURING CLIMB, THE LT ENG VIBRATION REACHED 3.8 UNITS. PERFORMED A BORESCOPE INSPECTIONS IAW AMM 72-00-00-200-808-F00, AMM 72-00-28-00-200-808-F00, AMM 72-00-00-200-804-F00, AMM 72-00-00-200-807-F00, TRIM BALANCE IAW AMM 71-00-00, TASK 71-00-00-750-803-F00, PLSDR ASMF201503004Heat Exchanger · leakingAIRCRAFT RETURNED TO PLATFORM DUE TO DURING RT ENG START, AN OIL LEAK WAS DETECTED. PERFORMED REVISION, DETECTING OIL LEAK IN THE OIL & FUEL HEAT EXCHANGER DRAIN. THE RT HEAT EXCHANGER WAS REPLACED IAW AMM 79-21-02, TESTED CORRECT.SDR SWAA2015021736656Wedge · crackedRIGHT WING NR 5 SLAT LOWER TE WEDGE CRACKED AT OTBD AUX TRACK. REPAIRED WEDGE IAW EA.SDR ASMF201503002Mixing Valve · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE DUCT OVER HEAT LIGHT TURNED ON. DURING MX REVISION, THE AIR CYCLE MACHINE IN THE LT AIR CONDITIONED PACK WAS DETECTED WITHOUT TEMPERATURE CONTROL IN MANUAL & AUTOMATIC MODE, SO THE LT AIR CONDITIONED PACSDR ASMF201503001Blade · damagedDURING OVERNIGHT CHECK, IT WAS DETECTED IN THE RT ENG A MISSING MATERIAL AT FAN BLADE ABRADABLE SHROUD & DISTORTION AT FAN BLADE LE. PERFORMED REVISION DETECTING A MISSING MATERIAL AT RT ENG FAN BLADE OF 1.0 INCH LENGTH, 0.200 INCH DEPTH, 0.500 INCH WIDE, SO SDR ASMF201501025O-Ring · damagedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING RT ENG START, A FUEL & HYD LEAKS WERE DETECTED. THE PLATFORM WAS CLEANED. PERFORMED REVISION, DETECTING FUEL LEAK IN THE TRANSIENT BLEED VLV DRAIN PORT. THE RT ENG WAS MOTORING AFTER IT WAS STARTED & ENG OPERATIONSDR SWAA2015012836156Attach Angle · crackedRIGHT WING TRANSVERSE WEB ATTACH ANGLE CRACKED AT PROGRAM ROLLER SUPPORT ARM ATTACH POINT. R & R ANGLE IAW SRM.SDR SWAA2015012836155Gusset · crackedRIGHT WING UPPER TE PANEL SUPPORT GUSSET CRACKED AT TRANSVERSE WEB ATTACH POINT. R & R GUSSET IAW SRM.SDR SWAA2015012836154Bracket · crackedLEFT WING FIXED TE AT ORSS 261, CTR ATTACH BRACKET CRACKED. R & R BRACKET IAW SRM.SDR SWAA2015020436329Light · brokenAFT CEILING PANEL EMER LIGHT ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY IAW MM.SDR SWAA2015013036230Seat Track · crackedSEAT TRACK CRACKED AT BS 727B, RBL 45.5 INBD FLANGE AFT HOLES, OTBD FLANGE FWD HOLE. REPAIRED SEAT TRACK IAW ER & EA.SDR SWAA2015013036229Seat Track · crackedSEAT TRACK CRACKED AT BS 727B, RBL 24.75 INBD FLANGE FWD & AFT HOLES, OTBD FLANGE FWD HOLE. REPAIRED SEAT TRACK IAW ER & EA.SDR SWAA2015013036228Seat Track · crackedSEAT TRACK CRACKED AT BS 727B, LBL 24.75 OTBD FLANGE FWD & AFT HOLES, INBD FLANGE FWD HOLE. REPAIRED SEAT TRACK IAW ER & EA.SDR SWAA2015013036227Seat Track · crackedSEAT TRACK CRACKED AT BS 727B, LBL 45.5 OTBD FLANGE FWD & AFT HOLES, INBD FLANGE FWD HOLE. REPAIRED SEAT TRACK IAW ER & EA.SDR SWAA2015012636085Plate · crackedRIGHT WING WIGGLE PLATE CRACKED AT REMOVABLE PANEL 661CB. R & R WIGGLE PLATE IAW SRM.SDR SWAA2015021836698Skin · crackedSKIN CRACKED AT BS 540, STRINGER 22L. REPAIRED SKIN IAW EA.SDR SWAA2015012836152Window Frame · crackedLEFT NR 3 WINDOW FRAME CRACKED AT THE SECOND FROM BOTTOM FWD HOLE. REPAIRED FRAME IAW ACO.
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