Boeing 757-324
Service difficulty reports · 703
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 = '757324' 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 = '757324' 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 CALA2023013000254Skin · corrodedSKIN BUBBLED JUST AFT OF LOWER CARGO DOOR AT APPROX STA 1440 STR 30 BL0. FOUND STR 30 CORRODED. CUT OUT DAMAGE AND INSTALLED REPAIR IAW SRM 53-00-03-2R-1. WORK PEROFRMED ON AMES ILN N/R 154944-010 0-0010.SDR CALA2023012500193Drive Assy · faultedTE FLAP ASSYM EICAS AFTER T/O RAN QRH 90.10. NUMBER 1FSEU SHOWS RT FLAG DRIVE FAULT. FOUND R/H OUTBOARD FLAP TRANSMISSION NOT MOVING TORQUE TUBE. REMOVED AND REPLACED FLAP INDICATOR. VERIFIED PERFORMED ADJUSTMENT OF T/E FLAPS LH AND RH POSITION TRANSMITTER, PSDR CALA2023012500209Indicator · faultedSPLIT FLAP INDICATION BETWEEN FLAPS 15 AND 30 NO EICAS MSG FOUND TE FLAP INDICATOR TO BE STICKING INTERNALLY. REPLACED TE FLAP POSITION INDICATOR PER AMM27-58-02, COMPLETED OPS CHECK PER AMM27-58-02-704-010. INSPECTED ALL TE FLAP INDICATION COMPONENTS, NO DEFESDR CALA2023012500198Frame · crackedUPPER CABIN INTERIOR FUSELAGE FRAME IS CRACKED AT STATION 1540 STRINGER 8LL AT THE OVERHEAD BIN ATTACH RACKET. REPAIRED RH FUSELAGE FRAME AT FS 1540 STR 8L IAW B757-300 SRM 53-00-07 REPAIR 8. FOR DETAILS SEE PWA AND PWS #30 PG 1 OF 1.SDR CALA2023012500197Frame · crackedFRAME CRACKED THROUGH RIVET HOLE FOR OVERHEAD BIN ATTACH BRACKET AT STA 780 + 20 AND JUST BELOW STR 8 REPAIRED RH FUSELAGE FRAME AT FS 780 + 20 STR 8 IAW B757-300 SRM 53-00-07 REPAIR 8. FOR DETAILS SEE PWA AND PWS #31 PG 1 OF 1.SDR CALA2023012000164Reservoir · lowLT HYD QTY EICAS C, LEFT HYDRAULIC RESERVOIR QUANTITY IS LOW, HYD AUTO EVEN T RAN CHKLIST IAW QRH. AFT ER SECURING BOTH L PUMPS RUDDER RATIO DISPLAYED. QTY SLOWLY RETURNED NORMAL & LANDING WITH ALL MESSAGES & INDICATIONS RETURNING TO NORMAL. CREW STATED LT SDR CALA2022121903436Access Panel · detachedPDA 2 #2 ENG INBOARD ACCESS PANEL 443HL FOUND MISSING. PASS REPORTED FELL OFF DURING REVERSER DEPLOYMENT DURING LANDING. REF IPC 54-53-01-05A ITEM 60 INSTALL #2 ENGINE PYLON ACCESS PANEL 443HL. IAW REF 54-53-01-404-005-001 ACCOMPLISHED VISUAL INSPECTION OF SURSDR CALA2022121203349Intercostal · crackedFLOOR BEAM INTERCOSTAL CRACKED IN MULTIPLE PLACES ALONG THE UPPER L CHANNEL BETWEEN FS1280, BL0. REPLACED NEW UPPER CHORD AT STATION 1260-1288 BL0 IAW SRM 51-40-07 PAR.7. WORKED PERFORMED AT AMES IN ILN ON N/R 152595-0100-0058 BY V931825 AS A MAJOR REPAIR.SDR CALA2022120803336None · noneAS REQUIRED BY AD 2012-25-11, ACCOMPLISH AN NDT INSPECTION OF THE FUSELAGE SKIN DOUBLER (INSTALLED PER EA 5330-04213 OP4) BEFORE 37,500 TOTAL AIRCRAFT CYCLES. AFTER THE ACCUMULATION OF 34,500 TOTAL AIRCRAFT FLIGHT CYCLES, BUT BEFORE 35,000 TOTAL AIRCRAFT FLIGHSDR CALA2022120703327Floorbeam · crackedFLOORBEAM CRACKED AT STA.490 RBL 11. REMOVED AND REPLACED UPPER TEE, BS 490 RBL 11 IAW SRM 51-40-02, PARA 7.SDR CALA2022120703311None · noneTHE REPAIR INCORPORATED VIA ECRA 5310-08079 IS APPROVED AS TIME LIMITED UNTIL 37,500 TOTAL AIRCRAFT FLIGHT CYCLES PENDING THE RESULTS OF A DAMAGE TOLERANCE ANALYSIS (DTA). REMOVE THE AIRCRAFT FROM SERVICE ON OR BEFORE 37,500 TOTAL AIRCRAFT FLIGHT CYCLES, UNLESSDR CALA2022120703310None · noneTHE REPAIR INCORPORATED VIA ECRA 5360-5360-01680 STATION 1440 FUSELAGE FRAME BETWEEN S-29R AND S-29L STRINGERS IS APPROVED AS TI ME LIMITED UNTIL 50,000 TOTAL AIRCRAFT FLIGHT CYCLES PENDING THE RESULTS OF A DAMAGE TOLERANCE ANALYSIS (DTA). REMOVE THE AIRCRA FTSDR CALA2022120703307None · noneTHE REPAIR INCORPORATED VIA EC/RA 5360-01678 BS 1420 FRAME, S24L & S27L. APPROVED AS TIME LIMITED UNTIL 25,600 TOTAL AIRCRAFT FLIGHT CYCLES PENDING THE RE SULTS OF A DAMAGE TOLERANCE ANALYSIS (DTA). REMOVE ACFT FROM SERVICERE 25,600 TOTAL AIRCRAFT FLIGHT CYCSDR CALA2022120503304Frame · dentedEA 5310-07582 REV A FRAME 1420 INSIDE THE AFT CARGO COMPARTMENT NEAR S-26L HAS TWO DENTS ON TOP OF THE FRAME FLANGE, DAMAGE MARK ED IN RED. DENTS FOUND TO BE OUT OF LIMITS PER 53-00-07-1A-1 FIG 1. REPAIRE D FRAME AT STA 1420 L/H PER EA 757-5360-13-A3083 REV A SDR CALA2022120503281Floorbeam · crackedFLOOR BEAM CRACKED AT STA.490 BL 11. REFERENCE NR IS 151231-0200-0246.SDR CALA2022112803234Bushing · noneREF AMES NR 151231-0400-0353 #1 PYLON DIAGONAL BRACE FWD FITTING (ON PYLON) BUSHINGS REQUIRE REPLACEMENT. (WILL REQUIRE MACHINE SHOP ASSISTANCE) CALABRIA V93 1830 REF AMES NR 151231-0400-0353. REMOVED & REPLACED #1 PYLON DIAGONAL BRACE FWD FITTING BUSHINGS IAWSDR CALA2022112803233Bushing · noneREF AMES NR 151231-0400-0345 #1 PYLON UPPER LINK BUSHINGS (ON PYLON) REQUIRE REPLACEMENT. (WI LL REQUIRE MACHINE SHOP ASSISTANCE) CALABRIA V931830 REF AMES NR 151231-0400-0345. REMOVD & REPLACED #1 PYLON UPPER LINK BUSHINGS ON PYLON IAW B757 SRM 54-50-90-3. SESDR CALA2022112503224Light · inoperativeEMERGENCY LIGHT AFT OF DOOR 2 RIGHT INOP HELP. REINSTALLED ORIGINAL BATTERY. INSTALLED EMERGENCY LIGHT FOR 2L FWD AND 2R AFT POSITION IN KNOW GOOD LOCATION AND BOTH ASSYEMBLIES WORK, REINSTALLED IN OTIGINAL LOCATION. STILL DO NOT LIGHT UP DURING EMERGENCY LIGSDR CALA2022112503223Light · inoperativeEMERGENCY LIGHT FORWARD OF DOOR 2 LEFT INOP HELP. REINSTALLED ORIGINAL BATTERY. INSTALLED EMERGENCY LIGHT FOR 2L FWD AND 2R AFT POSITION IN KNOW GOOD LOCATION AND BOTH ASSYEMBLIES WORK, REINSTALLED IN OTIGINAL LOCATION. STILL DO NOT LIGHT UP DURING EMERGENCY SDR CALA2022112503222Light · inoperativeEMERGENCY LIGHT AT DOOR 1 LEFT ON FORWARD BULKHEAD INOP LIGHT.. STILL DOESNT LIGHT UP DURING TEST, NEEDS MORE TROUBLESHOOTING.. PARTS USED: 29-3351-3-0031,QTY :1 REPLACED LAMP ASSY., NO HELP, FURTHER TROUBLESHOOTING NEEDED. REPLACED EMERGENCY LIGHT BATTERY CSDR CALA2022111103119Skin · corrodedEA 5530-04213 REV C OPERATION 003 DURING ROTO INSP OF L1 DOOR SURROND STRUCTURE DOUBLER PREVENTATIVE MODIFICATION, 2 HOLES HAVE BEEN STEPPED UP TO .214" AND STILL HAVE REJECTABLE DAMAGE AND CORROSION INDICATIONS. INSTALLED REPAIR PER EC/RA 5310-08065 AND EA 75SDR CALA2022111103105Stringer · corrodedFOUND STRINGER EDGES CORRODED UNDER THE SPLICE AND EXFOLIATION BETWEEN STRINGER AND SKIN. THIS CORROSION IS AT SAME LOCATION AS BUBBLE IN SKIN STA. 1450 STR 30. REMOVED DAMAGE AT STR 30 FROM STA 1448 TO STA 1451 IAW SRM 51-10-02-06-0, FABRICATED REPAIR FILLERSDR CALA2022082402164Window · openHIGH SPEED ABORT DUE TO FIRST OFFICERS WINDOW COMING OPEN ON TAK EOFF ROLL. HIGH ENERGY STOP INSPECTION COMPLETED ON L/P 9359946. PERFORMED OPERATIONAL CHECK OF F/O''S SLIDING WINDOW REF AMM 56-11-02-715-020. NO FAULTS NOTED AT THIS TIME.SDR CALA2022082402169Skin · dentedSUPPORT TASK LEFT WING OB FWD FLAP UPPER SKIN HAS DENTS AS MARK TRANSCRIBED FROM HAECO GSO NR 9286084 EVALUATED, REMOVED DAMAGE AND REPAIRED AND RESTORED FINSIH OF L /H WING O/B FWD FLAP UPPER SKIN IAW B757-300 SRM 51-70-07, SRM 5 7-53-01 B757-300 AMM 51-21-0SDR CALA2022071301719Cover Plate · missingPDA 3 R1 DOOR LWR HINGE CNTR COVER PLATE MISSING. REQUEST CDL FOR R1 LWR HING PLATE. DEFER R1 LWR HING COVER MISSING. DISPATCH DESK: 51 NAME: YA DATE: 09-JUL-22- OK TO DEFER R1 DOOR HINGE COVER MISSING. PICTURES ATTACHED. INSTALLED R1 DOOR SDR CALA2022071101709Cooling Fan · inoperativeBURNING ELECTRICAL FUMES IN COCKPIT. RAN CHEKLIST SMELL WENT AWA Y. NO VISIBLE SMOKE. SUSPECT RIGHT REC. FAN WHEN AIRCRAFT ARRIVED AT GATE EQUIPMENT COOLING HORN WAS SUSPECT RT RECIRCULATION FAN 53-2125-9-0001 REPLACED RIGHT HAND RECIRCULATION FAN / FAN IS STSDR CALA2022062001541Hydraulic System · inoperativeHYD SYSTEM REMAINED AT .25 AND HELD THERE UNTIL GEAR EXTENSION A ND DROP THEN TO .10 AND THAT AND RPR OF HYD LOSS. FOUND LH HYD QTY AT 2 GALS - SERVICED WITH 3 GALS OF HYD FLUID TO RUN ELEC HYD PUMPS FOR TROUBLESHOOTING. NO OBVIOUS LEAK.REMOVED AND REPLACED RSDR CALA2022040800928Drain Line · damagedLOSS OF C HYD FLUID 1 HOUR PRIOR TO LANDING. NO SPECIFIC AIRCRAFT CONFIGURATION CHANGE DURING LOSS SEE IPC-29-11-75-02 ITEM 190 PN LJ38085 OR M&E 19-2911-3-0148, FOUND ON RIGHT ENGINE 2 O''CLOCK POSITION HYDRAULIC LINE LEAKING CORRECTION RIGHT SYSTEM HYDRAULICSDR CALA2022030700607Pitot Head · fod*EMERGENCY DECLARED* HAD AIRSPEED DISAGREE ON TAKEOFF. APPEARED TO BE CAPT SIDE THAT WAS IN ERROR. SWITCHED SOURCE BACK TO ''L'', THEN CAPT SD AIRSPEED IND WAS SHOWING 10KTS LESS THAN F/O & STBY INDICATORS ON REST OF FLT. INFO PER FLT CREW DEBRIEF - ON TAKEOFFSDR CALA2022022200478Angle · corrodedREF AMES ILN NRC 142584-0100-0035. BLENDED DAMAGE ORIGINAL THICK NESS .090 REMOVED .045 OUT OF LIMITS IAW 757 SRM 53-00-51 FIG 10 1 DETAIL III REPLACED SUPPORT ANGLE PN 146N5300-77. V931851. REGUIRES SFRSDR CALA2022022200477Floor Support · corrodedREF AMES ILN NRC 142584-0200-0208. C/W ERCA 5300-02802 AND REA 47494REA03 BLENDED DAMAGE AREA AT STA 350 BL4. REMOVED .020 ORIG .140 REMAINING .120 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 - 1A-1. REPAIRED AREA IAW SRM 53-00-51-2R-10.V929460. REGS SFRSDR CALA2022022200476Floor Support · corrodedREF AMES ILN NRC 142584-0800-0095. REMOVED CORROSION FROM 2 FLOO R PANS. .008 REMOVED FROM FWD PAN AND .010 FROM AFT PAN. FLOOR P ANS DAMAGE FOUND TO BE BEYOND LIMTS SRM 53-10-15-1A ALLOWABLE DA MAGE FIG 101 DETAIL VI. BOTH PANS REQ REPLACEMENT. REG''S SFR. V9SDR CALA2022012700252Floorbeam · corroded(B757-53-3-0479) R1 DOOR THRESHOLD UPPER CORD FORWARD OF FLOOR B EAM 365.25 - SURFACE CORROSION, TRANSCRIBED FROM HAECO GSO NR LP 9281117 ACCOMPLISHED REPLACEMENT OF CORRODED R1 DOOR THRESHOLD UPPER CHO RD IAW B757-300 SRM 51-40-02, DWG 141N5160, B757-300 SRM SDR CALA2022011800181Floorbeam · corrodedREF AMES NR 142584-0200-0194 UPPER CABIN FLOOR BEAM STA 1681 BL0 THE UPPER GUSSET IS CORRODED. REMOVED AND REINSTALL NEWLY GUSSET PLATE, FABRICATED OUT OF 7075 -T6- .063 CLAD ALUM PO#0159539 IAW B757 SRM 51-40-02 PG.7 AND BO EING DRAWING #146N5230 SEE PARTIAL SDR CALA2022011400153Flap System · asymetricTE FLAP ASYM EICAS FOLLO WED BY FLAP LD RELIEF WHEN FLAP LEVER M OVED FROM 20 TO 25 AND 30 ON ARRIVAL HAD FLA FAIL, MSG 217. ACCOMPLISHED FIM 27-51 FAULT TREE 810 FOR FLAP LOAD RELIEF FAULT. ALL STEPS WERE PASSED ANDTHEN OPERATED THE FLAPS UP AND DOWN COUPLE OSDR CALA2022010300017Warning Message · illuminated*EMERGENCY DECLARED* TE FLAP DISAGREE ON LANDING DUE HEAVY RAIN AND WIND ON APPORACH, CREW EXPEDITE LANDING. SUSPECT HEAVY FLAP LOADS, CAUSED LOCK UP. FLAPS STOWED ELECTRICALLY, BITE FSCU, SYSTEM RESET FLAPS-SLATS OPS NORMAL FULL RANGE UP-DOWN. SEVERAL TIMESSDR CALA2021112902193Hydraulic System · none*EMERGENCY DECLARED* R HYD SYS PRESS AND R HYD QTY CAUTION MSG ON EICAS. HYD QTY .16 HYD PRESS 30 FOUND #1 ENG PYLON PRESSURE TUBE ASSY LEAKING. REF AIPC CLAMP. INSTALLED FILTER MODULE AND COMPONENTS OF THE RIGHT EDP 29-11-17-03 ITEM 798 WORN THROUGH AT AFT CLSDR CALA2021112302167Indicator · trippedTE FLAP ASSYMETRY FLAPS SET TO 20. RH STOPPED AT 15, LH WENT TO 20. CREW WENT TO OPERATED FLAPS UP AND DOWN, NO ASSYMETRY EVENT OCCURED. ALTERNATE BOTH TO 20. INTERROGATED FSAM AND FSEU1,2. FOUND FESU FAULT CODES 305 AND 328. CONTINUED T/S WIH FIM 27-51 FAULT SDR CALA2021110802042Oven · odorBURNED PLASTIC OR BURNED ELECTRICAL SMELL IN COCKPIT INSPECTED BEHIND OVERHEAD CIRCUIT PANELS OR DAMAGED WIRES OR BURN SMELL. NO FAULTS FOUND. INSPECTED FIRST CLASS GALLEY FOR FOREIGN MATTER ON COFFEE BURNERS AND IN OVENS. COULD NOT FIND ANY SMELL. FLIGHT CRSDR CALA2021110502037None · inoperativeCAPTAIN STATED, ON INITIAL LEVEL OFF AT 5000 FT OUT OF HNL, LEFT AUTO THROTTLE UNABLE TO RETARD THRUST BACK TO MATCH RIGHT ENGINE. AFTER AUTO THROTTLE DISCONNECTION UNABLE TO MANUALLY RETARD THROTTLE TO MATCH RIGHT SIDE ALSO. LEFT THROTTLE WAS 20 PERCENT N1 HISDR CALA2021090301501Lens · missingPDA 3 REF LOG 6972100 R/H NAV LIGHT COVER (LENS) MISSING, FRAME WAS STILL INTACT REF LOG 6972100 FOR R/H NAV LIGHT LENS REPLACEMENTSDR CALA2021080901308Generator · failedLEFT GEN FAILED AT CRUISE.ATTEMPTED 1 RESET AS PER QRH..... FAILED 2ND TIME REPLACED BUS TIE CIRCUIT BREAKER IAW AMM24-22-03. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1631709 SN OFF 6616 IPC REFERENCE # IPC24-22-01-03 BREAKER. REF. M&E # 6616, SHOULD READ RSDR CALA2021071901130Fitting · gougedSUPPORT TASK L2 DOOR TOP FWD DOOR STOP BRACKET ON FUSELAGE SIDE OF DOOR CUTOUT HAS GOUGE TRANSCRIBED FROM HAECO GSO NR 9282409 M ECH V900838 REMOVED AND INSTALLED A NEW DOOR STOP BRACKET AT L-2 DOOR TOP FW D PN 143N8381-1 PO#1005221.1 IAW B757-300 SRM 51-40-02SDR CALA2020121401370Oxygen Mask · damagedFOUND DAMAGED CAPTS 02 MASK DURING REACTIVATION OF SYSTEM. MASK STRAP IS LEAKING BEHIND HEAD WHEN PRESSURIZED. SPT-7000581. REMOVED AND REPLACED CAPTS O2 MASK/REGULATOR WITH SERVICEABLE MASK/REGULATOR PN MC10-25-104 SN 52474, IAW B757 AMM 35-11-51-004-0 27 SDR CALA2020112501303Panel · inoperativeUNABLE TO LOCK FLIGHT DECK DOOR. REPLACED DOOR SWITCH CONTROL PANEL, REF AMM 52-52-01-000-801C9. OPERATIONS CHECKED GOOD, REF AMM 52-52-01-700-801C3. TRACKING TAG NR 113608 8. S/N OFF 0014 S/N ON 0048. ROTABLE PARTS CHANGE WAS INDICATED-TT NR 1136088 SN OSDR CALA2020101601199Bulb · burned outEMERGENCY LIGHTS (USING CONTROL SWITCHES) OPERATIONAL CHECK . EMERGENCY LIGHT OUT SIDE OF L4 INOP. RELAMPED PER AMM 33-51-06-962-001-002 OPS CHK OKSDR CALA2020101601198Bulb · burned outEMERGENCY LIGHTS (USING CONTROL SWITCHES) OPERATIONAL CHECK . EMERGENCY LIGHT OUT SIDE OF L4 INOP. RELAMPED PER AMM 33-51-06-962-001-002 OPS CHK OKSDR CALA2020100901168Fire Detector · out of limitsENGINE FIRE DETECTION FIRE PROTECTION SYSTEM FAIL LGT ON. EICAS MESSAGE FIRE/OVHT SYS DISPLAYED. EICAS STATUS MESSAGE (01=L, 02= R) ENG OH LP 1 AND LP 2 DISPLAYED 01 FIRE/OVHT SYS EICAS WARNING DISPLAYED L ENG OH LP 1 AND 2 STATUS DISPLAYED. ADDING CREW PHOTO SDR CALA2020072701074Latch · no testR4 DOOR SLIDE LATCH BLOCK WILL NOT PASS PULL TEST.SDR CALA2020072701073Latch · no testESCAPE SLIDE LATCH ASSEMBLY ON R1 DOOR FAILS PULL TEST LP 700132 5 SPT
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