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.

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 RNov 6, 2024 · N21108 · Boeing 757224 · Emergency EquipmentSDR 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. REMONov 5, 2024 · N13113 · Boeing 757224 · Emergency LightingSDR CALA2024110802808Frame · corrodedCORROSION FOUND ON FWD SIDE OF FRAME AT STA 1360 BETWEEN STR 26-27R.Nov 5, 2024 · N14121 · Boeing 757224 · Fuselage Main, FrameSDR 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.Nov 4, 2024 · N13138 · Boeing 757224 · Standard Practices/StructuresSDR 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 TIMENov 4, 2024 · N58101 · Boeing 757224 · Emergency EquipmentSDR 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 RENov 3, 2024 · N13138 · Boeing 757224 · Door Warning SystemSDR 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 HNov 3, 2024 · N18112 · Boeing 757224 · Emergency ExitsSDR CALA2024110401003Lamp · inoperativeEMERGENCY LIGHTS AMBER UNARMED LIGHT NEEDS TO BE RELAMPED. PERFORMED OPERATIONAL CHECK OF AMBER EMERGENCY LIGHT. OPS CHECK NORMAL.Nov 3, 2024 · N19130 · Boeing 757224 · Emergency LightingSDR 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 (LVNov 2, 2024 · N13113 · Boeing 757224 · Engine Fuel System WiringSDR 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 Nov 1, 2024 · N41140 · Boeing 757224 · Engine (Turbine/Turboprop)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.Oct 28, 2024 · N67134 · Boeing 757224 · Emergency EquipmentSDR CALA2024103000968Lavatory · odorG2 REPORTS THAT LAV K HAS A FOUL ODOR AFTER CLEANING SPRAYED LYSOL IN LAV K . OKAY FOR SERVICEOct 28, 2024 · N12116 · Boeing 757224 · Waste Disposal SystemSDR CALA2024102902748Stringer · corroded(B757-53-3-0526) AFT CARGO COMPT. STA 1380 STR 28 UNDER FACTORY SPLACE IS EXFOLIATED. DOT 34-043.Oct 28, 2024 · N14102 · Boeing 757224 · Fuselage Main, Longeron/StringerSDR 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. Oct 27, 2024 · N33103 · Boeing 757224 · Flight Control System WiringSDR 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 GALLEOct 26, 2024 · N13110 · Boeing 757224 · Standard Practices/StructuresSDR CALA2024102900949Light · detached28C EMERGENCY ROW LT HANGING FROM HARNESS NEEDS SECURED RESECURED LIGHT, OPS CHECK GOOD, OK TO CONTINUE.Oct 26, 2024 · N67134 · Boeing 757224 · Emergency LightingSDR 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 Oct 23, 2024 · N13110 · Boeing 757224 · Air Distribution FanSDR 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 WILOct 23, 2024 · N17122 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA2024102302711Door Frame · crackedEA 5330-04213 REV: L1 DOOR FRAME SURROUND CUTOUT AREA FOUND A CR ACK. DOT 68-50Oct 22, 2024 · N14102 · Boeing 757224 · Fuselage Main, StructureSDR CALA2024102300901Girt Bar · fod1R SLIDE ARMINGING LIGHT INOP DURING ARMING. REMOVED DEBRIS FROM GIRT FLOOR FITTING, ARMING LIGHT OPS CK GOOD. OK TO CONTINUE.Oct 20, 2024 · N14115 · Boeing 757224 · Emergency EquipmentSDR 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.Oct 18, 2024 · N14102 · Boeing 757224 · Fuselage Main, StructureSDR 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 Oct 18, 2024 · N41140 · Boeing 757224 · Hydraulic System, MainSDR CALA2024102802739Slat Track · corrodedNUMBER 3 SLAT I/B & O/B MAIN TRACKS HAVE CORROSION.Oct 15, 2024 · N14121 · Boeing 757224 · Leading Edge DevicesSDR CALA2024111102830Bushing · damagedWHILE PERFORMING GVI OF UPPER DRAG LINK INNER BUSHINGS FOR OK TO INSTALL, FOUND RH BUSHINGS TO BE SCORED AND METAL SHAVINGS.Oct 14, 2024 · N14121 · Boeing 757224 · Nose/Tail Landing GearSDR CALA2024102302710Bushing · damagedWHILE PERFORMING GVI OF NOSE LANDING GEAR LH AND RH BUSHINGS FOUND BOTH BUSHINGS TO BE SCORED AND METAL SHAVINGS.Oct 14, 2024 · N14121 · Boeing 757224 · Nose/Tail Landing GearSDR 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 140-024Oct 14, 2024 · N14102 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2024120503020Door Frame · corrodedAPU DOOR INTERNAL SURROUND STRUCTURE HAS SEVERAL AREAS OF CORROSION FWD, AFT & O/B.Oct 3, 2024 · N14121 · Boeing 757224 · Fuselage Main, StructureSDR 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 ONLYOct 3, 2024 · N14121 · Boeing 757224 · Fuselage Internal Mounting StructureSDR 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 EXOct 2, 2024 · N12125 · Boeing 757224 · Electrical Power SystemSDR 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 BACKOct 2, 2024 · N19141 · Boeing 757224 · Engine Indicating SystemSDR CALA2024100302551Tie Down · corrodedGEN ITEM: GENERATING ITEM ALC FLOOR CARGO NET TIE DOWN FITTING HAS CORROSION @BS 1300,1320,1340,1360, AND 1375 RBL 24Oct 2, 2024 · N14121 · Boeing 757224 · Fuselage, Seat/Cargo Attach FittingsSDR 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.Oct 1, 2024 · N14121 · Boeing 757224 · Wing Miscellaneous StructureSDR 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 V921197Sep 30, 2024 · N14121 · Boeing 757224 · Wing, Plate/SkinSDR 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.Sep 30, 2024 · N18119 · Boeing 757224 · Fuel StorageSDR 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 CONTINUESep 27, 2024 · N14107 · Boeing 757224 · Engine Bleed Air SystemSDR 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 ISep 27, 2024 · N57111 · Boeing 757224 · Compressor Bleed ValveSDR CALA2024093000721Skin · damagedNR 6 LEADING EDGE SLAT DAMAGE, APPROXIMATELY 66 SQUARE INCH SECTION OF THE INBOARD TRAILING EDGE WEDGE DEPARTED THE AIRCRAFT.Sep 25, 2024 · N14106 · Boeing 757224 · Leading Edge DevicesSDR 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.Sep 24, 2024 · N17139 · Boeing 757224 · Engine Thrust ReverserSDR 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 TSep 23, 2024 · N41140 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA2024093002514Skin · corrodedGEN ITEM; 19-5705-1-2004///RW UPPER SKINHAS CORROSION AT RW BL S TA U-18 MARKED.Sep 23, 2024 · N14121 · Boeing 757224 · Wing, Plate/SkinSDR 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 UNITEDSep 23, 2024 · N14121 · Boeing 757224 · Fuselage Miscellaneous StructureSDR 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 OSep 21, 2024 · N57111 · Boeing 757224 · Fuel Controlling SystemSDR 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 Sep 21, 2024 · N29124 · Boeing 757224 · Air Distribution SystemSDR CALA2024091902445Frame · chafedCHAFFE MARKS ON THE UPPER CHORD OF FRAME 1640, BETWEEN STR. 5R AND STR. 6R.Sep 17, 2024 · N14121 · Boeing 757224 · Fuselage Main, FrameSDR 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, TSep 17, 2024 · N57111 · Boeing 757224 · Emergency EquipmentSDR 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 RSep 16, 2024 · N17139 · Boeing 757224 · Fuselage Structure (General)SDR 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 Sep 16, 2024 · N33132 · Boeing 757224 · Nacelle/Pylon, Main FrameSDR 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., FSep 14, 2024 · N14121 · Boeing 757224 · Aircraft Fuel Distribution SystemSDR 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 DETIALSSep 13, 2024 · N17139 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2024091302417Plate · corrodedCORROSION ON THE UPPER SURFACE OF THE CABIN SUB FLOOR, AT STA.1710 TO STA.1715, LBL48 TO LBL52.Sep 12, 2024 · N14121 · Boeing 757224 · Fuselage Miscellaneous Structure
Back to Boeing 757-224