Boeing 757-230
Service difficulty reports · 608
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 = '757230' 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 = '757230' 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 I5PA2020122468802Warning Message · false activationDISCREPANCY-STATUS MESSAGE "RT OIL FILTER" AFTER START RETURN TO GATE. CORRECTIVE ACTION: REMOVED AND REPLACED RT ENGINE MAIN OIL FILTER, IAW AMM 79-21-05. NO METAL OR DEBRIS ON FILTER AND MCD NOTED. RAN ENGINE LEAK CHECK AND OPERATIONS CHECK OK.SDR FDEA202012223194Slide · dislodgedAFTER COMPLETING PREFLIGHT WHILE CLOSE R-1 DOOR FOUND GIRT BAR HANGING OUT. OPENED DOOR AND FOUND SLIDE FELL OUT OF DOOR. MEL 22DEC20 00:27 FNT U. RELEASED FOR SERVICE, PER MEL: 52-11-01-A CATEGORY: B EXPIRATION: 25DEC20 "MEL 52-11-01-A: R1 DOOR OR SLIDE-RESDR I5PA2020122288803Display · inoperativeCAPT MCDU INOPERATIVE. PART WAS REPLACED AND CONFIRMED OPERATIONAL.SDR FDEA202012183188Crank Assy · brokenWHILE PERFORMING MEL VERIFICATION FOR MEL 25-66-05-A WRI 8405. FOUND GIRT BAR IS NOT ENGAGING. SUSPECT BAD LINKAGE. VERIFIED SLIDE LIGHT COMES ON WHEN WHEN PLACING MAGNETS OVER SENSOR NEAR FOOT RETAINERS, REF AMM 25-66-11-2. R1 DOOR SLIDE IS INOPERABLE. FSDR FDEA202012153158Crank Assy · inoperativeR-1 DOOR ARMING LIGHT INOPERABLE WHILE PERFORMING MEL VERIFICATION FOUND GIRT BAR IS NOT ENGAGING. SUSPECT BAD LINKAGE. VERIFIED SLIDE LIGHT COMES ON WHEN WHEN PLACING MAGNETS OVER SENSOR NEAR FOOT RETAINERS, REF AMM 25_66_11_2 AMM 25-66-04-4, CMM 52-11-05. SDR I5PA2020121468801Ignition Unit · failedDISCREPANCY-APU WOULD NOT START ON ARRIVAL. CORRECTIVE ACTION: REMOVED AND REPLACED APU IGNITION UNIT, IAW AMM 49-41-03. OPERATIONS CHECK OK.SDR I5PA2020120988802Warning Switch · damagedFIRE WARNING LIGHT ILLUMINATED ON APPROACH MOMENTARILY. NO EICAS MESSAGES OR AURAL WARNINGS WERE ASSOCIATED WITH THE LIGHT. THE DEFECT WAS CAUSED DUE TO A BROKEN FIRE WARNING SWITCH LIGHT.SDR I5PA2020120488801Selector · faultyDISCREPANCY: "FWD CABIN TEMP" EICAS MESSAGE. CORRECTIVE ACTION: REMOVED AND REPLACED FWD CABIN TEMP SELECTOR, IAW AMM 21-61-04. OPERATIONS CHECK OK. ZONE TEMP CONTROLLER BITE, NO FAULT NOTED.SDR I5PA2020111488802Transmitter · faultyETOPS SIGNIFICANT ITEM-RT ENGINE MAIN OIL PRESSURE TRANSMITTER INOPERATIVE.SDR I5PA2020111368802B-Nut · leakingDISCREPANCY: "RT GEN DRIVE" EICAS MESSAGE (AIR RETURN). CORRECTIVE ACTION: FOUND "RT IDG LOW OIL PRESS" ON BPCU. EXAMINED DPI, NOT EXTENDED. RE-CONNECTED IDG AND PERFORMED IDG OIL SERVICING, PER AMM 12-13-03, AND FOUND OIL LEAK FROM B-NUTS ON IDG. TIGHTENESDR I5PA2020111168801Start Valve · faultyDISCREPANCY: RT ENGINE STARTER CUTOUT "VALVE" LIGHT STAYED. CORRECTIVE ACTION: REMOVED AND REPLACED RT ENGINE STARTER VALVE, IAW AMM 80-11-02. LEAK CHECK AND OPERATIONS CHECK OK.SDR I5PA2020102668803Controller · faulted"FLIGHT DECK ZONE TRIM AIR MODULATING VALVE INOPERABLE". REMOVED AND REPLACED ZONE TEMP CONTROLLER, IAW AMM 21-61-03.SDR I5PA2020102668802Filter · unserviceable"RT OIL FILTER" STATUS MESSAGE. INSPECTED MAG CHIP DETECTORS, IAW AMM 79-21-10. NO DEFECTS NOTED. REMOVED AND REPLACED RIGHT ENGINE MAIN OIL FILTER, IAW AMM 79-21-05. RAN RIGHT ENGINE NO LEAK NOTED.SDR FDEA202010212577Controller · failedDECLARED EMERGENCY DUE TO CABIN ALTITUDE WARNING. PERFORMED PHASE 1 AND QRH. RETURNED TO FIELD. THE RIGHT PACK WAS OFF AT THE TIME, DUE TO RUNNING THE CABIN ALTITUDE HOT QRH MOMENTS BEFORE. TROUBLESHOT, PER FIM 21-30 FAULT TREE 802. UPON DISCOVERY FOUND TSDR FDEA202010202564Sensor · failedON TAXI OUT, LT FWD ENTRY DOOR EICAS MESSAGE WITH ASSOCIATED DOOR LIGHT ILLUMINATED OPENED/SHUT DOOR, CONDITION REPEATED. REMOVED AND REPLACED LT DOOR SENSOR, PER MM 52-71-00-4. OPERATIONS CHECKS GOOD. OPENED AND CLOSED DOOR SEVERAL TIMES WITH NO FAULTS. RSDR I5PA2020101868801Seal · wornRIGHT ENGINE OIL CONSUMPTION ABOVE NORMAL. REMOVED AND REPLACED RIGHT ACCESSORY GEAR BOX STARTER DRIVE SEAL, IAW AMM 72-61-02. RAN RIGHT ENGINE NO LEAK NOTED.SDR I5PA2020100488801Apu · inoperativeAPU EGT OUT OF LIMITS, WHEN A PNEUMATIC LOAD IS PLACED AND DURING ENGINE START. APU WAS REPLACED AND CONFIRMED OPERATIONAL.SDR I5PA2020091408801Controller · defectiveSMOKE REPORTED IN THE COCKPIT COMING FROM F/O R1 WINDSHIELD AREA. FLIGHT DIVERTED DUE TO DECLARED EMERGENCY. MX FOUND FAULTY WINDOW HEAT CONTROLLER. REPLACED DEFECTIVE WINDOW HEAT CONTROLLER AND R1 WINDOW.SDR I5PA2020090328801Drive Unit · faultedWEATHER RADAR INOPERABLE. REMOVED AND REPLACED WEATHER RADAR ANTENNA DRIVE UNIT IAW AMM 34-43-05. OPERATIONAL CHECK GOOD.SDR FDEA202009012077Wheel · damagedPDIS 997 32-41 8143 01SEP20 MEM OPEN U. DURING TAXI IN OBSERVED ABNORMAL SOUND AND VIBRATION FROM LANDING GEAR/TIRES/WHEELS. SET BRAKE, SHUTDOWN, COORDINATED TOW IN TO GATE. SHGN 01SEP20 08:55 MEM U. THE LEFT NOSE TIRE, WHEEL HUB/WHEEL ASSY HALVES ARE BRSDR FDEA202008252024Controller · failedCABIN ALTITUDE WARNING AT FL 340. REMOVED AND REPLACED BOTH NR 1 AND 2 AUTO PRESSURE CONTROLLERS PER MM 21-31-02-4, BOTH OPS CHECK GOOD. ALSO RIGHT PACK FLOW CONTROL VALVE CHANGED ON WRI 2130-7144.SDR FDEA202008252018Valve · malfunctionedTRAILING EDGE FLA DISAGREE EICAS MESSAGE WHEN SELECTING FLAPS 1, RAN QRH USED ALTN FLAPS 20 FOR LANDING. AFW U HAD CONFERENCE WITH INBOUND CAPTAIN, STATED WHEN MOVED TO FLAPS 1 HAD NO ACTION, HAD NO ROLL SITUATION ALSO. WENT TO ALTN FLAPS AND LANDISDR I5PA2020072838801Display · inoperativeFO MCDU INOP DURING PRE FLIGHT CHECK . MCDU WAS CONFIRMED DEFECTIVE AND REPLACEDSDR I5PA2020072606801Pressure Switch · malfunctioned"C HYD SYS PRESS" EICAS MSG APPEARED IN FLIGHT. THE FLIGHT CREW VERIFIED NO OTHER ABNORMALITIES WERE ASSOCIATED WITH THE SYSTEM. AFTER FOLLOWING QRH PROCEDURES, THE FLIGHT CREW DECLARED AN EMERGENCY AS PRECAUTION ALTHOUGH NO EMERGENCY ACTION WAS REQUIRED PER TSDR FDEA202007171559Receptacle · damagedR1 DOOR WILL NOT ARM AND SLIDE LIGHT WILL NOT ILLUMINATE. FOUND R1 DOOR GIRT BAR ANNUCIATOR LIGHT RECEPTACLE L404 PIN 2 READING ZERO VOLTS. REMOVED AND REPLACED THE RECEPTACLE L404 IAW IAW SWPM 20-84-00. NO OTHER DEFECTS NOTED. DOOR ARMING OPS NORMAL.SDR I5PA2020072858802Pilot Valve · defectiveLH ENG HP PILOT WAS REPLACED DUE TO LOW BLEED PRESSURE AT IDLE POWERSDR FDEA2020070871458Girt Bar · bindingL1 DOOR OPENS NORMALLY WITH THE HANDLE TO THE 2 O'CLOCK POSITION. VERY DIFFICULT TO MOVE THE HANDLE PAST 2 O'CLOCK POSITION TO THE LEFT- FULLY OPEN. FOUND L1 DOOR GIRT BAR JAMMED- RMVD AND RPLD GIRT BAR- DOOR OPENS AND CLOSES NORMAL AND ARMS AND DISARMSSDR FDEA2020071031416Slide · low pressureL1 RAFT BATTERY GAUGE IN DOOR OUT OF GREEN BAND. REPLACED THE L1 DOOR SLIDE RAFT IAW AMM 25-66-01-4. OPS CHECKED GOOD. ACFT OK FOR SERVICE.SDR FDEA202006301394Battery · dischargedL1 RAFT BATTERY GAUGE IN DOOR OUT OF GREEN BAND. REPLACED L1 DOOR SLIDE RAFT IN REF TO AMM 25-66-01-4. OPS CHECK GOOD. AC OK FOR SERVICE. REMOVED SLIDE RAFT: PN D30654-122. SN 2055RP.SDR FDEA2020070201416Battery · dischargedL1 RAFT BATTERY GAUGE IN DOOR OUT OF GREEN BAND.SDR FDEA202004270807Rudder · failedSMIS 985 55-40 5529 23APR20 MEM OPEN U MOD TYPE T MOD NO. F-5540-T0353729 REV NO. PS P1 STABILIZERS - RUDDER - MAINTENANCE PROGRAM INSPECTION COMPLY WITH E..A. F-5540-T0353729 REV NO. POS. P1 DUE TO FAILED RUDDER INSPECTION R&R'ING RUDDER SDR FDEA2020043060845Access Door · missingDURING AIRCRAFT ARRIVAL MAINTENANCE FOUND L/H LOWER FUSALAGE AIRSTART ACCESS DOOR DETACHED AND MISSING FROM AIRCRAFT FUSELAGE, UPON ACCESS DOOR LEAVING FUSELAGE IN FLIGHT, SMALLER HOLE WAS MADE AT CENTER OF FUSEALAGE CENTERLING. INSTALLED LH GROUNDSDR I5PA2020040188801Starter · damagedRH ENG STARTER FAILED DURING START. INSPECTION INDICATED INTERNAL DAMAGE. STARTER WAS REPLACED AND AIRCRAFT WAS PLACED BACK INTO SERVICESDR I5PA2020031101Ecu · faultyAIRCAFT ARRIVED IN HNL WITH APU UNABLE TO START ON DURING TAXI INTO THE GATE. APU ECU WAS CONFIRMED FAULTY AFTER PERFORMING OPERATIONAL CHECKS. ECU WAS REPLACED AND APU STARTED WITHOUT ANY FURTHER ISSUES.SDR I5PA2020022766803Transmitter · out of tolerance"FUEL DISAGREE PROG 2". FUEL FLOW DISAGREE BY 600#'S TOTALIZE FUEL ONLY INTO FLIGHT. RIGHT HIGHER THAN LEFT. REMOVED AND REPLACED #2 ENGINE FUEL FLOW TRANSMITTER I.A.W. AMM 73-31-01 AND PERFORMED ENGINE RUN AND LEAK CHECK. LECH CHECK GOOD, FUEL FLOW NOW AT 1.1SDR I5PA2020021948802Fire Loop · shortedRH ENG FIRE LOOP DETECTOR NO 2 MSG APPEARED IN FLIGHT. ITEM WAS PLACED ON MEL. PART WAS THEN REPLACED WITHOUT FURTHER DEFECTSSDR I5PA2020021966801Fire Loop · shortedRH ENG FIRE LOOP DETECTOR NO 2 WAS FOUND FAULTY DURING A PRE FLIGHT CHECK. PART WAS REPLACED WITHOUT ANY FURTHER DEFECTSSDR FDEA202001230212Control Valve · failedAT CRUISE FL410COCKPIT OVERTEMP OCCURED WITH TEMP CONTROL INPUTS HAVING NO EFFECT. RAN QRH PROCEDURE, "CABIN TEMP INOP" TO STEP 4 WHICH DIRECTED US TO "CABIN TEMP HOT" PROCEDURE. WE MADE IT TO STEP 12 WITH LEFT PACK SELECTED AUTO, RIGHT PACK OFF. THE LEFT PACKSDR FDEA2019112653092Skin · dentedLARGE DENT SHOWING AT NR 8 SLAT WEDGE UPPER SKIN. ACCOMPLISHED REPAIR ON NR 8 SLAT T/E WEDGE UPPER SKIN IAW SRM 57-43-02-2R AND IAW SRM 51-70-10-2R REP 4 AND IAW EA T F-5750-T0351070 P1. WING - FLIGHT SURFACES - NR 8 SLAT TRAILING EDGE WEDGE UPPER SURFACE RSDR FDEA201911223045Shear Web · corrodedMAIN CABIN BETWEEN STA 1681-1720, BL0-LBL50 WEB CORRODED. REMOVED CORR ON SHEAR WEB STA 1681-1720 BL0 - LBL50 IAW SRM 51-10-02 ALL AREAS IN LIMITS EXCEPT STA 1701 LBL5 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A FIG 101. AT STA 1701 LBL5 FABRICATED AND INSSDR FDEA201911223044Doubler · crackedMAIN CARGO COMPT. L-4 DOOR INTERNAL STRUCTURE, FWD. AND NEAR TO LOWER CORNER GUSSET HAS 1EA. DEEP GOUGE. REMOVED GUSSET (DOUBLER) L-4 DOOR INTERNAL STRUCTURE LWR CORNER IAW B757 SRM 51-40-02. FABRICATED AND INSTALLED NEW GUSSET (DOUBLER) IAW BOEING DWG 14SDR FDEA2019112213026Web · corrodedMAIN CABIN BETWEEN STA 1700-1720, BL0-RBL50 WEB CORRORED. REMOVED CORR ON SHEAR WEB 1700-1720 BL0 -RBL50 IAW B757 SRM 51-10-02. ALL AREA'S IN LIMIITS EXCEPT STA 1705 RBL6 IAW B757 SRM 53-00-51-1A FIG 101. FABRICATED AND INSTALLED DOUBLER AT STA 1705 RBL6 SDR FDEA201910112600Actuator · inoperativeGEAR DISAGREE AFTER TAKEOFF. RAISED GEAR PER QRH. REMOVED & REPLACED RT MAIN GEAR TRUCK POSITIONER ACTUATOR IAW AMM 32-32-15-4. OPS AND LEAK CHECKED GOOD.SDR I5PA2019100792503Anti-Ice Valve · defectiveL ENGINE ANTI-ICE INOPERATIVE.SDR FDEA2019082071925Panel · crackedFOUND CRACK ON UPPER AFT O/B FIXED WING PANEL. WHERE THE SKIN PANEL 112N3501-5 ATTACHES AT I/B AFT CORNER. REF WRI 57-20/7350. REMOVED PANEL 113N1640-31 FROM OUTBD END OF UPPER LEFT WING FOR REPAIR. THE DAMAGE IS APPROX 1' LONG ON EDGE LAND APPROX 61" FROM SDR FDEA201907241684Stowage Box · failedF/O?S O2 MASK STOWAGE BOX WILL NOT TEST. REPLACED FO'S O2 MASK/STOWAGE BOX PER AMM 35-11-51-4-98. TAG# 7G3378 FOR P/N MXP891-3, S/N SE47881. SYSTEM WILL NOT TAKE TAG #. OFF P/N MXP891-3, S/N SE37958.SDR FDEA201907161578Computer · failedPDIS 998 34-11 5664 16JUL19 OKC OPEN U LOGPAGES:3000296 ON TAKEOFF AIRSPEED DISAGREE, COMPLIED WITH QRH, IDENTIFIED IT AS F/O AIRSPEED. OPS CHECKED AND LEAK CHECKED F/O PITOT TUBE IAW AMM 30-31-00-5. REPLACED RT AIR DATA COMPUTER IAW AMM 34-12-0SDR FDEA2019080281790Skin · damagedDELAMINATION ON L/H OUTER WING SKIN AT PANEL 112N3501. DAMAGE IS APPROX. BETWEEN WS 813.50 & WS 830.00. DAMAGE AREA IS 16.4IN LENGTH, 13.50 WIDTH. COMPLIED WITH PART 1 OF EA F-5710-T0348642.SDR FDEA2019061321280Floorbeam · corrodedFLOOR BEAM AT STA.377 FWD FLANGE HAS CORROSION FROM LBL.25-LBL.58 COMPLIED WITH FEDEX EA#F-5310-T0347236 P1, STA.377 FLOOR BEAM UPPER FORWARD FLANGE REPAIR BETWEEN LBL.24 ABD LBL.58.SDR FDEA2019061321276Floorbeam · corrodedFLOOR SUPPORT AT STA.376, LBL.10 - LBL. 24 HAS CORROSION. CORROSION FOUND TO BE OUT OF LIMITS, 100% MATERIAL LOSS ON FLOOR SUPPORT AT STA.376 LBL.10 TO LBL.24 IAW B757 SRM 53-00-51-1A, REMOVED, FABRICATED AND INSTALLED NEW FLOOR SUPPORT FROM 2024-T3 ..071,
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