Boeing 757-224
Service difficulty reports · 3,824
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 = '757224' 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 = '757224' 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 CALA2024110801074Girt Bar · faulty4L SLIDE LIGHT INOP ON INITIAL INSPECTION GIRT BAR DETACHED INSTALLED L4 GIRT BAR REF AMM 25-66-10-402-022, SAFETY PIN HAS BEEN REMOVED, PERFORMED AN OPERATIONAL CK OF L4 DOOR ARMING AND DESARMING OF DOOR SLIDE REF AMM 25-66-01-404-044 INSTALLED L4 GIRT BAR RSDR CALA2024110801082Lamp · inoperativeEMERGENCY LIGHTS (USING CONTROL SWITCHES) OPERATIONAL CHECK {MULT-33-3-0001} - #2 L/H DOOR EMERGENCY SLIDE LIGHT INOP REMOVED AND REPLACED LIGHT IN REFERENCE WITH AMM 33-51-06. NO HELP. ALSO CHECKED BATTERY PACK FUSES FOR CONTINUITY, ALL 4 FUSES ARE GOOD. REMOSDR CALA2024110802808Frame · corrodedCORROSION FOUND ON FWD SIDE OF FRAME AT STA 1360 BETWEEN STR 26-27R.SDR CALA2024110601046None · noneINSTALED SAFETY PIN IN ESCAPE SLIDE AT DR-4L FOR MX. REMOVED AND STOW SAFETY PIN AT DR-4L REF AMM 25-66-11.SDR CALA2024110601044Lock · faultyWHILE ACCOMPLISHING J/C# 19-2560-1-9801 ON L4 DOOR, OBSERVED L4 'SLIDE ARM LIGHT' FLICKERING INTERMITENTLY WHEN ARMED. R/R L4 DOOR GIRT BAR (M&E 19-2566-3-0005) AND FWD AND AFT BAR LOCK ASSY (M&E 19-2566-3-0002) IAW AMM 25-66-10. OPS CHECKS NORMAL AT THIS TIMESDR CALA2024110501010Proximity Sensor · faultyDOOR 4L SLIDE LIGHT WILL NOT EXTINGUISH WHEN DOOR IS DISARMED REQUESTING MEL . COMPLIED WITH MEL , CONFIRMED GRITBAR OPERATIONAL. REMOVED SLIDE LIGHT INDICATOR BULB OFF. ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT DOOR 4L - MEL 2566U PLACED ON MEL. REMOVED AND RESDR CALA2024110501006Door · no discrepancyREMOVED EMERGENCY EXIT HATCH DOOR AS PER NEF LOG PAGE 9708092 INSTALLED RIGHT FORWARD OVERWING EMERGENCY EXIT HATCH UPTO AND INCLUDING STEP AMM 52-22-01 3.D.9. STEP 10 TO COMPLETION REQUIRED. QC VERIFIED INSTALLATION OF RIGHT FORWARD OVERWING EMERGENCY EXIT HSDR CALA2024110401003Lamp · inoperativeEMERGENCY LIGHTS AMBER UNARMED LIGHT NEEDS TO BE RELAMPED. PERFORMED OPERATIONAL CHECK OF AMBER EMERGENCY LIGHT. OPS CHECK NORMAL.SDR CALA2024110601053Elec Connector · unsecureREPEAT WRITE UP RTO 80 KTS ENGINE 2 WILL NOT GO ABOVE 1.5 EPR REFERENCE FIM 71-06 TASK 807 FOR TROUBLESHOOTING. TOMC-MEREDITH CARRIED OUT TROUBLE SHOOTING AS PER FIM 73-21-00-301. EEC BITE CARRIED OUT PER FIM 73-21-00-902-001-R01, BITE SHOWS FAULT CODE 35 (LVSDR CALA2024110501022Engine · faultyDURING INCOMING INSPECTION AND DISASSEMBLY OF ENGINE ESN 31805, SASAI HAS DISCOVERED A HOLE IN THE OUTER CASE OF THE 04 MODULE. PICTURES HAVE BEEN UPLOADED TO EXOSTAR UNDER THE INVESTIGATIONS-UNIQUE EVENTS FOLDER. THE HOLE/DAMAGE DENOTED ON THE OUTER CASE IS SDR CALA2024103000971Girt Bar · fodDOOR ARMED LIGHT ON DR 4L WENT OFF DURING FLIGHT. WAS ILLUMINATE D ON GROUND. REMOVED BOTTLE CAP FROM GIRT BAR ATTACH FITTING. DOOR 4L OP CK GOOD.SDR CALA2024103000968Lavatory · odorG2 REPORTS THAT LAV K HAS A FOUL ODOR AFTER CLEANING SPRAYED LYSOL IN LAV K . OKAY FOR SERVICESDR CALA2024102902748Stringer · corroded(B757-53-3-0526) AFT CARGO COMPT. STA 1380 STR 28 UNDER FACTORY SPLACE IS EXFOLIATED. DOT 34-043.SDR CALA2024102900947Pcb · faultedREJECTED TAKE OFF DUE TO UNSCHED STAB TRIM EICAS MSG.AIRSPEED APROX 50 KTS RIGHT SAM MODULE HAS A SPM YELLOW BALL SHOWN, REPLACED RIGHT SPM CARD ASSY, GND TEST PASSED BUT YELLOW BALL DOES NOT DISAPPEAR. GND TEST OF RIGHT GPM WAS DONE PER AMM 27-48-03-424-009. SDR CALA2024102900945None · noneNEED TO PERFORM CONDITIONAL INSPECTION PER AMM 05-51-58-910-801-C1 PERFORMED CONDITIONAL INSPECTION PER AMM05-51-58-910-801-C1, UP TO AND NOT INCLUDING STEP D AND ON.PER TOMC MIGUEL. NO FURTHER STEPS REQUIRED. ALL TESTS PASS BUT PUT RT RECIRC FAN AND FWD GALLESDR CALA2024102900949Light · detached28C EMERGENCY ROW LT HANGING FROM HARNESS NEEDS SECURED RESECURED LIGHT, OPS CHECK GOOD, OK TO CONTINUE.SDR CALA2024102500928Fan · failedLEAVING 12000 WE HAD A VERY STRONG ODOR OF FUMES IN THE COCKPIT AND FORWARD CABIN REF LP 9655264 FOR UPDATES AND CORRECTIVE ACTIONS FOR SMOKE / ODOR SMOKE FIRE AND FUMES ON THE FLTDECK CHECKLIST WAS ACTIONED. FOUND RIGHT RECIRC FAN DISPLAY INOP WHEN SELECTED SDR CALA2024102502726Skin · misrepairedWHILE LAYING OUT NEW FASTENER LOCATIONS FOR L-1 DOOR SURROUND PREVENT MOD DOUBLER EA 5330-04213 REV D IT WAS DISCOVERED THAT SEVERAL INITIAL FASTENER LOCATIONS ON THE REPAIR DRAWING DO NOT MATCH UP WITH THE CONFIGURATION ON THE AIRCRAFT. ALSO, ONE FASTENER WILSDR CALA2024102302711Door Frame · crackedEA 5330-04213 REV: L1 DOOR FRAME SURROUND CUTOUT AREA FOUND A CR ACK. DOT 68-50SDR CALA2024102300901Girt Bar · fod1R SLIDE ARMINGING LIGHT INOP DURING ARMING. REMOVED DEBRIS FROM GIRT FLOOR FITTING, ARMING LIGHT OPS CK GOOD. OK TO CONTINUE.SDR CALA2024102102686Door Seal · crackedB757-32-3-6064 L/H MLG WHEEL WELL AT STA1049 KEEL EXTENDING TO OUTER PANEL 197EL FWD DOOR SEAL HAS TWO CRACKS.SDR CALA2024101800863Line · faultyR HYD QTY EICAS FOLLOWED BY R HYD SYS PRESS MSQ QTY BEGAN 0.38 A ND WAS 0.7 WITHIN 2 MINS RH ENGINE LEAKING HYDRAULIC FLUID. REMOVED AND REPLACED NR. 2 ENGINE EDP CASE DRAIN HARD LINE SECTION WITH A SERVICEABLE UNIT, REF IPC 29-11-75-02 ITEM NR. 190. TORQUED SDR CALA2024102802739Slat Track · corrodedNUMBER 3 SLAT I/B & O/B MAIN TRACKS HAVE CORROSION.SDR CALA2024111102830Bushing · damagedWHILE PERFORMING GVI OF UPPER DRAG LINK INNER BUSHINGS FOR OK TO INSTALL, FOUND RH BUSHINGS TO BE SCORED AND METAL SHAVINGS.SDR CALA2024102302710Bushing · damagedWHILE PERFORMING GVI OF NOSE LANDING GEAR LH AND RH BUSHINGS FOUND BOTH BUSHINGS TO BE SCORED AND METAL SHAVINGS.SDR CALA2024101502648Intercostal · corroded(B757-57-3-0367) EXFOLIATION AT J SECTION FROM STA 880-900 AT WT B PANEL 193AL LWR MID FUSELAGE LBL 5. DOT 140-024SDR CALA2024120503020Door Frame · corrodedAPU DOOR INTERNAL SURROUND STRUCTURE HAS SEVERAL AREAS OF CORROSION FWD, AFT & O/B.SDR CALA2024100402562Shear Tie · corrodedAPU INLET DOOR O/B OPENING SHEAR TIE HAS CORROSION STR 6R AT STA 1806. REPAIR WORK DOCUMENTED ON LP 9448205. REF AMES NR 172653-0300-0112 FABRICATED AND REPLACED ON NR 172653-0300-0010 SSFR IS ACCOMPLIS HED NR GENERATED FOR TRACKING PURPOSE ONLYSDR CALA2024100402557Circuit Breaker · inoperativeEICAS CONT PNL CAUTION ON TO PAST 100KTS. REF FOUND C/B POPPED 115 VAC BUS R SECT 2 ON P32 PANEL. PERFORMED BPCU BITE PROCEDURE IN REFERENCE TO B757 FIM 24-20 FAULT TREE 801 BPCU BITE SHOWED NO EXISTING FAULTS OR FAULTS FOR THE INBOUND LEG REST BREAKER WITH EXSDR CALA2024100400753Probe · faultedR ENG PROBE HEAT STATUS AFTER ENG START SUSPECT RT ENG PROBE M&E 19-7321-3-0002 MEL 3034B DISPATCH ADVISES THERE IS ICING NEAR BOS. ON DEFERRAL R&R ENG 2 P1 PROBE PER AMM TASK 73-21-04 AND OPS CHECKED GOOD AND PERFORMED IDLE RUN TO MAKE MSG DID NOT COME BACKSDR CALA2024100302551Tie Down · corrodedGEN ITEM: GENERATING ITEM ALC FLOOR CARGO NET TIE DOWN FITTING HAS CORROSION @BS 1300,1320,1340,1360, AND 1375 RBL 24SDR CALA2024100302552Angle · corrodedGEN ITEM: EA 5100-02338 REV A OP 001 UPON ACCOMPLISH FLS DAMAGE TOLERANCE FLEET REPAIR SURVEY RIGHT WING NOTICED ON UPPER T/E PNL AT OTBD AILERON WSTA760 CORROSION ON T/E PNL SUPPORT ANGLE.SDR CALA2024100102536Skin · damagedGEN ITEM;EA 5720-03041 REV E OP 015/// JC EA 5720-03041 REV E LH UPPER SKIN & DRAG FITTING FASTENER HOLE NO 5 HAS HFEC OPEN HOLE DEFECT INDICATION, CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS ENTER EC/RA NO ON STEP 1.4. REPORTED BY V921197SDR CALA2024093000714Fuel Cap · faultyLEFT OVERWING FUEL CAP LEAKING IN FLIGHT REMOVED AND REPLACED LEFT OVERWING FUEL FILL CAP PER B757-200 AMM 28-11-04. B757-200 IPC 28-11-04 ITEM 50 P/N 38222-3. PERFORMED LEAK CHECK AFTER FUEL SERVICE. LT TANK AT 15000LBS AND NO LEAKS OBSERVED.SDR CALA2024093000723Liner · missingPDA 2 ON ENG 2 DISCOVERED MISSING ACOUSTIC ATTENUATOR LOCATED AT 9 OCLOCK POSITION. SEE PHOTO REMOVED AND REPLACED ENG NO.2 9 OCLOCK ACOUSTIC ATTENUATOR IAW MM 75-32-10 OK TO CONTINUESDR CALA2024093000704Screen · faultedPDA 2 ON E2 AT 9OCLOCK POSITION. DISCOVERED MISSING ATTENUATOR SCREEN. EWR REPORTED E1 LEFT BLEED VALVE ATTENUATION SCREEN IS MISSING. NO IDEA WHEN IT MAY HAVE DEPARTED THE ENGINE. IT MEASURES APPROX 6 INCH DIAMETER (28.27 INSQ). PER THE GMM 2-30-95 THIS ISDR CALA2024093000721Skin · damagedNR 6 LEADING EDGE SLAT DAMAGE, APPROXIMATELY 66 SQUARE INCH SECTION OF THE INBOARD TRAILING EDGE WEDGE DEPARTED THE AIRCRAFT.SDR CALA2024092602492Panel · damagedREF AMES NON ROUTINE 174011-0400-0096. PER CUSTOMER REQUEST; REPAIR #2 O/B T/R INNER LINER T/E. REPAIRED #2 O/B T/R INNER LINER IAW AIRBORNE DOCUMENT#47634REA02 AND UNITED EC/RA 7500-01389.SDR CALA2024093000709Skin · damagedRII INSPECTION REQUIRED REPAIR ON FUSE STA 587L TO STA 594L STR 18L SEE L/P 9287975 INSPECTION WAS NOT NOTIFIED FOR FINAL INSPECTION PRIOR TO EDGE SEALANT AND PAINT. REQUIERS PAINT STRIP AND SEALANT REMOVED FOR FINAL INSPECTION, OF SRM 53-00-01-2R-13 STEPS 7 TSDR CALA2024093002514Skin · corrodedGEN ITEM; 19-5705-1-2004///RW UPPER SKINHAS CORROSION AT RW BL S TA U-18 MARKED.SDR CALA2024092402478Transition Panel · corrodedREMOVED FLOOR PANEL STRUCTURE FOR STA 1540-1640 AND FOUND CORROSION. REMOVED CORROSION ON TRANSITION PANEL FOUND TO BE OUT OF LIMITS. REMOVED PANEL AND INSTALLED NEW PANEL PART NO 146N5431VY2 BATCH NO RC-102-4496 IAW B757 SRM 51-40-02-00-0G P 7 & 9 REF UNITEDSDR CALA2024092400682Governor · faultyRIGHT ENGINE EGT EXCEEDANCE ON CLIMB, CREW REPORTED POWER REQUIRED REDUCTION TO LIMIT EGT. CHECK INLET AND EXHAUST AND CHECK EXCEEDANCE PER FIM 71-05 TASK 824 AND FIM 71-05 TASK 819. EICAS ENGINE EXCEEDANCE REPORT VERIFIED RIGHT ENGINE EGT REACHED A MAX TEMP OSDR CALA2024092300668Unknown · smokeCREW REPORTED SMOKE AND ODOR ON CLIMB @ 170 IN FLIGHT DECK AND MID CABIN. DISSIPATED SHORTLY THERE AFTER WITH NO EICAS MESSAGES OR VISUAL FAULTS ON OVERHEAD PANEL. CREW NEEDS TO FILL OUT SMOKE ODOR FORM 46-6020 AND WORK AMM TASK 05-51-58-910-801-C1 SMOKE ODOR SDR CALA2024091902445Frame · chafedCHAFFE MARKS ON THE UPPER CHORD OF FRAME 1640, BETWEEN STR. 5R AND STR. 6R.SDR CALA2024091900656Bottle · low pressurePASSENGER DOOR GIRT BAR SLIDING MECHANISM LUBRICATE {B757-52-3-0071} - DURING INSPECTION OF L-1 DOOR ASSIST BOTTLES, FOUND PLUMBING LINE AND BOTTLE CAPED. REPLACED RESERVOIR BOTTLE PER AMM 52-11-30/401.FUNCTIONS DURING AN ACTUAL EMERGENCY OR DURING TRAINING, TSDR CALA2024092302460Skin · dentedREF AMES NON ROUTINE 174011-0200-0084.PER CUSTOMER REQUEST. FORWARD OF THEL2 DOOR,FORWARD REPAIR DOUBLER, THE UPPER FORWARD CORNER APPEARS TO BE DENTED. MEASURED DENT (A)=7.5" (Y)DEPTH .160" A/Y=46 DENT FOUND TO BE O REPAIR PERFORM INSP PER PART 2 OF LATEST RSDR CALA2024091800651Door · missingENGINE 1 PANEL 413CL MISSING ON ARRIVAL INTO SNN OFF FLIGHT 976-16. REF IPC 71-11-04-02 ITEM 345. M/E 19-7111-3-0005 . PDA EVENT. DUPLICATE LOG, SEE 9272069 FOR ACTIONS TAKEN FOR REPAIR. THIS LOG FOR REPORTING.IDG OIL ACCESS PANEL ENG L SHEARD OFF QC REVIEWED SDR CALA2024091702438Clamp · crackedRIGHT WING FUEL DISTRIBUTION TUBE CL AMP MOUNTING BRACKET IS CRACKD INSIDE PANEL 631AB LOOKING AFT, R IGHT WING FUEL ENTRY REQUIRED REMOVED AND REPLACED RW FUEL DISTRIBUTION TUBE CLAMP MOUNTING BR ACKET IN G31AB IAW B767 SRM 51-40-02.SEE PWA #182 PG 1 OF 2., FSDR CALA2024091602424Floor Support · crackedFLOOR SUPPORT ANGLE CRACKED AROUND N UTPLATE IN ALC STA 1520 TO 1540 BL-0-LOOKING UP. REPORTED BY V89 4037 REMOVED AND REPLACED FLOOR SUPPORT ANGLE IN ALC STA 1520-1540 BL O IAW B757-200 SRM 51-40-02 PAR 7. SEE NON-ROUTINE 174011-0100-0 062 FOR DETIALSSDR CALA2024091302417Plate · corrodedCORROSION ON THE UPPER SURFACE OF THE CABIN SUB FLOOR, AT STA.1710 TO STA.1715, LBL48 TO LBL52.
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