Boeing 757-2Y0
Service difficulty reports · 830
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 = '7572Y0' 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 = '7572Y0' 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 IXXA20221001136Hose · leakingLEFT HYDRAULIC SYSTEM TOTAL LOSS OF QUANTITY AND PRESSURE PUMPS SHUTOFF PRIOR TO ZERO QUANTITY 27%. RIGHT ENGINE HYDRAULIC OVERHEAT-PUMP SHUT OFF. RIGHT ENGINE HYDRAULIC ELECTRIC-PUMP SHUT OFF. BOTH PUMPS SHUTOFF IMMEDIATELY. STATUS MESSAGE 8 RIGHT HYDRAULIC SSDR FDEA202209222356Fseu · failedMOVING FLAP LEVER FROM 20 TO 25 A TRAILING EDGE FLAP DISAGREE EICAS MESSAGE DISPLAYED. QRH COMPLIED WITH AND EMERGENCY DECLARED. EMERGENCY DECLARED. REMOVED AND REPLACED #1 FSEU IAW AMM 27-51-01-2. OPS CHECK GOOD. NO DEFECTS NOTED. A/C OK FOR SERVICE. SDR IXXA2022072808Door · corrodedL2 ENTRY DOOR LOWER GATE CORRODEDSDR IXXA20220529116Eicas · fault messageENROUTE FROM PHIK TO PKWA, RIGHT ENGINE BLEED OFF EICAS MESSAGE DISPLAYED. CREW DECLARED EMERGENCY AND DESCENDED TO FL100. 9 EACH OXGEN GENERATORS DEPLOYED. FLIGHT CONTINUED AS AFFECTED TO DESTINATION STATION PHIK. LANDING WAS UNEVENTFUL WITH NO ADDITIONAL PRESDR IXXAEicas · fault messageAPPROXIMATELY FL 310 CABIN PRESSURE EICAS MESSAGE DISPLAYED. MASTER CAUTION OUTFLOW VALVE SHOWED CLOSED. NO CHANGE WHEN SWITCHED FROM AUTO 1 TO AUTO 2. AIR TURN BACK TO PKWA WITH AN EMERGENCY DECLARATION. LANDING WAS UNEVENTFUL
ON ARRIVAL, AIRACRAFT GROUNED FSDR FDEA202203220646Skin · dentedL/H LOWER LOBE FUSE SKIN AT STA. 247 AT STR23L HAS A CREASE BULGE ON FWD SIDE OF FRAME, NEEDS EVAL. EVALUATED DENT AT STA 247 S-23L, DAMAGE LOCATION IS LESS THAN 0.5" AWAY FROM FRAME AT STA 247, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01-1A FIG 101, DET. ISDR IXXA202201317005None · nonePRE-DEPARTURE, L1 DOOR WILL NOT CLOSE. AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. WORK IN PROGRESSSDR IXXA202201287003None · noneON POST FLIGHT INSPECTION INBOUND FROM KNGU LINE MAINTENANCE IDENTIFIED DAMAGE ON THE LEFT INBOUND LEADING SLAT PANEL. GROUNDED FOR UNSCHEDULED MAINTENANCE. WORK IN PROGRESS.SDR FDEA202110092503Flap System · faultedTE FLAP DISAGREE ON APPROACH. RAN QRH. DECLARED EMERGENCY. LANDED. REPEAT WRITE UP. INTERROGATED FSEU, #1 SHOWS FAULT 305: FLAP ISOL VLV. T/S CONTINUE DURING INSPECTION, FOUND LACK OF LUBRICATION ON L/H AND R/H INBOARD DRIVE OF BOTH INNER FLAP WITH OVERLOAD ISDR FDEA202110092501Unknown · faultedTE FLAPS EICAS WHEN SELECTING FLAPS 1 FOR APPROACH. DUE TO QRH AND CHECKLIST DEMANDS, OPTED TO DISCONTINUE APPROACH. COORDINATED A HOLDING PATTERN AND RAN THE QRH AND ASSOCIATED CHECKLISTS. WERE ABLE TO COMPLETE ALTERNATE FLAPS TO 20 AND LAND NORMALLY. SDR FDEA202107081705Skin · gougedFUSELAGE SKIN GOUGED AT STA 520 2", 3" IB OF STR 29L. MARKED WITH TAPE. 1" HOLE IN FUSELAGE REPAIRED PER 757 SRM 53-00-01 REP7.SDR FDEA202104241024Lamp · inoperativeL1 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED L1 DOOR SLIDE LIGHT PER B757-200 AMM 33-51-06-2-1, OP'S CHECKS NORMAL.SDR FDEA202104241023Lamp · inoperativeL1 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED L1 DOOR SLIDE LIGHT PER B757-200 AMM 33-51-06-2-1, OP'S CHECKS NORMAL.SDR FDEA202103010518Intercostal · corrodedUPON REMOVAL SPLICE STRAP STA 1400 FOUND CORROSION ON INTERCOSTAL BETWEEN STA 1400 - 1420 LBL 19. REMOVED INTERCOSTAL AT AFT CARGO BETWEEN STA 1400 - 1420 LBL 19 IAW B 757 SRM 51- 40-02-OG.UPON EVALUATION FOUND CORROSION 100% MAT LOSS OUT OF LIMITS IAW B 7SDR FDEA202102270498Splice · corrodedUPON REMOVAL OF SHEAR TIE STA 1400 BETWEEN S26L - S27L,FOUND CORROSION ON INTERNAL FUSELAGE SPLICE STRAP. REMOVED INTERNAL FUSELAGE SPLICE STRAP AT AFT CARGO STA 1400 BETWEEN STR 26L TO TO 27R IAW B 757 SRM 51-40-02-OG,UPON EVALUATION FOUND CORROSION 100% MSDR FDEA202102270499Shear Tie · corrodedSHEARED / PILLOWED RIVETS STA 1400 BETWEEN STR 26L - 27L. REMOVED 3EA RIVETS AT STA 1400 BETWEEN STR 26L - 27L IAW B 757 SRM 51-40-02-OG. UPON UPON FURTHER EVALUATION FOUND SHEAR TIE AT STA 1400 BETWEEN STR 26L - 27L OUT OF LIMITS LIMITS DUE TO CORROSION WISDR FDEA202102270497Floor Support · corrodedMAIN CABIN FLOOR SUPPORT ANGLE HAS AREAS OF CORROSION ON UPPER SURFACE BS 700 TO BS 720 LBL 62.5 EVALUATED CORROSION AT MAIN CABIN FLOOR SUPPORT ANGLE BS 700 TO BS 720 LBL 62.5 FOUND 100% MAT LOSS IAW B 757 SRM 51-10-02-OG. REMOVED,LOCATED,DRILLED AND ISDR FDEA202102180403Crease Beam · corrodedMAIN CABIN R/H FLOOR MOP SILL / CREASE WEB ANGLE HAS AREAS OF CORROSION ON UPPER SURFACE BETWEEN BS 1320 AND BS 1360. REMOVED CORROSION AT MAIN CABIN R/H CREASE WEB ANGLE "CHORD" ON UPPER SURFACE BETWEEN BS 1320 - 1360 IAW B 757 SRM 51-10-02-OG.EVALUATED ASDR FDEA202102180402Seat Track · corrodedMAIN CABIN RBL 24.75 SEAT TRACK HAS AREAS OF CORROSION ON UPPER SURFACE AT BS 1320. COMPLIED WITH FEDEX EA.# :F-5310-T039848 P1. TITLE : FUSELAGE - MAINFRAME - RBL 24 SEAT TRACK REPAIR BETWEEN STA 1320 - 1340 - SRM REPAIR DEVIATION FOR ALTERNATE FINISH.SDR FDEA202102180399Battery Pack · inoperativeMDIS 974 33-50 7299 18FEB21 MUC OPEN U SEE ALSO 33-50 WRI 7298: EMRGENCY LIGHTS IN CABIN MID AND RIGHT AND RIGHT EXTERIOR DOES NOT ILLUMINATE IN ALL POSITIONS. TROUBLESHOOTING PERFORMED, FOUND NO ILLUMINATION ON SDR FDEA202102180398Battery Pack · misinstalledMDIS 974 33-50 7298 18FEB21 MUC OPEN U AFTER AIRCRAFT POWER OFF FOUND EMERGENCY LIGHT IN COCKPIT LEFT SIDE ABOVE DOOR AND LEFT EXTERIOR LIGHT ILLUMINATED. WITH AC POWER ON LIGHTS GO OFF . CHECKED AND MOVED EMERG. LIGHT SWITCH IN COCKPIT SEVERSDR FDEA202102170387Seat Track · damagedMAIN CABIN RBL 24.75 SEAT TRACK UPPER CROWN BROKEN OFF AT BS 820. REMOVED SEAT TRACK SECTION,MAIN CABIN BETWEEN STA 780 TO 880 RBL 24.75,FOUND AREA OUT OF LIMITS IAW B 757 SRM 51-40-02-OG AND 53-00-52-1A FIG 101,FABRICATED NEW SEAT TRACK IAW BOEING DWG 143SDR IXXA20210124002Light · inoperativeDURING THE COURSE OF SCHEDULED MAINTENANCE CHECKS, TECHNICIAN IDENTIFIES EMERGENCY EXIT SIGN NEXT TO R1 DOOR INOPERATIVE. AIRCRAFT OUT OF SERVICE, WORK IN PROGRESS. CORRECTIVE ACTION PENDING.SDR 6PMR202012270001Spar · corrodedLT WING UPPER SKIN, FRONT SPAR, APPROXIMATELY WING STA 285 HAS CORROSION AROUND FASTENERS. CORRECTIVE ACTION: COMPLIED WITH EO 20495-6.SDR 6PMR2020122408318Skin · corrodedLEFT WING UPPER SKIN, FRONT SPAR APPROXIMATELY WING STA 238 HAS CORROSION AROUND FASTENER. CORRECTIVE ACTION: REMOVED CORROSION, BLENDED AREA, ACCOMPLISHED NDT AND SHOT PEEN. REAPPLIED SURFACE PROTECTION, IAW EO 20495-6. PEMCO NON-ROUTINE 10248-0318.SDR 6PMR2020122480315Spar · corrodedLT WING UPPER SKIN, FRONT SPAR, APPROXIMATELY WING STA 170 HAS CORROSION AROUND FASTENER. CORRECTIVE ACTION: REMOVED CORROSION AND BLENDED AREA. ACCOMPLISHED NDT, SHOT PEEN. REAPPLIED CORROSION PROTECTION, IAW EO 20495-6. PEMCO NON-ROUTINE 10248-0315.SDR FDEA202012233202Autopilot Sys · inoperativeTEST FLIGHT: ON CLIMB OUT WITH CENTER AUTO PILOT ON, STAB TRIM WENT FULL UP. DISENGAGE AUTO PILOT AND WAS ABLE TO CONTROL TRIM. HAPPENED TWICE MORE ON CLIMBOUT. DURING DESCENT ON RT AUTOPILOT STAB TRIM WENT FULL NOSE DOWN TRIM. HAND FLOWN THE REMAINDER OF SDR 6PMR202012230002Stringer · corrodedRIGHT WING FUEL TANK, CORROSION ON UPPER STRINGER BETWEEN WS 719 AND WS 743. CORRECTIVE ACTION: REMOVED AND REPLACED STRINGER SECTION BETWEEN STA 719 AND STA 743, IAW B-757 SRM 57-00-03, REPAIR 1 AND B-757 SRM 51-40-02. PEMCO NON-ROUTINE 10248-0549.SDR 6PMR2020122131223Skin · corrodedAREAS WITH CORROSION ON UPPER LEFT AFT SKIN SURFACE OF CENTER HORIZONTAL STABILIZER BOX, BETWEEN HYDRAULIC LINES CONNECTION AND LEFT ATTACH MOUNT PLATE AROUND FASTENERS AND ALONG EDGE. CORRECTIVE ACTION: ACCOMPLISHED EO 20495-3, REV IR. REMOVED CORROSION, ACSDR 6PMR202012170001Skin · corrodedLEFT WING UPPER SKIN, FRONT SPAR, APPROXIMATELY WING STA 660 HAS CORROSION AROUND VORTEX GENERATOR. CORRECTIVE ACTION: BLENDED AREA, IAW EO 20495-6, REV IR PEMCO NON-ROUTINE 10248-0320.SDR 6PMR202012164551Skin · dentedFUSELAGE SKIN DENTED AND SCRATCHED ON TOP OF EXISTING DOT AT LAP SEAQM ON TOP OF FASTENER AT STA 1714 AND STR 14AL. CORRECTIVE ACTION: REPAIRED FUSELAGE SKIN WITH CUTOUT, FILLER AND DOUBLER, TRIPLER, IAW EO 20492-1 REV IR. PEMCO NON-ROUTINE10248-0045.SDR IXXA20201216041Battery Pack · inoperativePOST LANDING: EMERGENCY EXIT SIGN AT 3R DOOR INOPERATIVE. REMOVED AND REPLACED POWER PACK BATTERY AT R3 DOOR, IAW B757 AMM 33-51-07. OPERATIONAL CHECK SATISFACTORY. NO ADDITIONAL DEFECTS NOTED. AIRCRAFT RELEASED TO SERVICE.SDR 6PMR1024804661210Seat Track · gougedMAIN DECK SEAT TRACK AT STA 905 AND RBL 24075 HAS DEEP GOUGES ON SCALLOP TABS. CORRECTIVE ACTION: REPLACED AND REPAIRED SEAT TRACK IN ACCORDANCE B757-200 SRM 53-00-52 REPAIR 4. PEMCO NON-ROUTINE 10248-0466.SDR 6PMR1024806201210Strap · crackedFOUND OVERHEAD STABILIZER STRAP AT BS 1380 LT CRACKED. MANUFACTURED LAP PATCH AND FILLER, IAW B-757-200 SRM 53-00-51 REPAIR 12.SDR 6PMR1024802981210Skin · corrodedNR 2 PYLON, CORROSION ON PYLON SKIN OUTBOARD SIDE JUST AFT OF 441AL. CORRECTIVE ACTION: INSTALLED REPAIR, IAW EO 20495-4 REV IR. PEMCO NON/ROUTINE 10248-0298.SDR 6PMR1024800441210Skin · gougedEXT FUSELAGE SKIN HAS GOUGES AT STA 1680-1690 AT STR 17L. CORRECTIVE ACTION: BLENDED GOUGES, IAW EA PD 57-53-350 PEMCO NON-ROUTINE 10248-0044.SDR FDEA202012093089Floor Support · corrodedAFT CARGO INTERCOSTAL HAS CORROSION ON LOWER OUTBOARD SIDE AT RBL-5 STA 1417. REMOVED INTERCOSTAL AT AFT CARGO STA 1417 RBL 5 AND EVALUATED AND FOUND OUT OF LIMITS, IAW B757 SRM 51-40-02-0G AND B757 SRM 53-00-04-1A FIG 101 DET V. REPLACED INTERCOSTAL BY FABRSDR 6PMR1024803260812Skin · corrodedDISCREPANCY: PEMCO NON-ROUTINE 10248-0326: LEFT WING UPPER SKIN REAR SPAR, APPROXIMATELY WING STATION 600 HAS CORROSION UNDER PANEL AND AROUND FASTENER. CORRECTIVE ACTION: REMOVED CORROSION AND EVALUATED LT WING UPPER SKIN. REAR SPAR FOUND TO BE OUT OF LIMITSDR FDEA202012053044Cusp Web · corrodedMAIN CABIN RT CUSP WEB CORRODED BETWEEN STA 580 AND STA 600. REMOVED CORROSION AT MAIN CABIN RT CUSP WEB BETWEEN STA 580 TO STA 600 AND AFTER EVALUATION FOUND CUSP WEB OUT OF LIMITS, IAW B757 SRM 51-10-02, 53-30-13-1A FIG 101 DET VIII. FABRICATED AND INSTASDR FDEA202012053043Cusp Web · corrodedMAIN CABIN RT CUSP WEB CORRODED BETWEEN STA 600 TO 620. REMOVED CORROSION AT MAIN CABIN RT CUSP WEB BETWEEN STA. 600 TO 620 AND EVALUATED ORIGINAL MAT .036", MAT LOSS .015", MAT REM .021". FOUND OUT OF LIMITS, IAW B757 SRM 53-30-13-1A FIG 101 DET VIII. FABRSDR FDEA202012053042Failsafe · corrodedMAIN CABIN LT SIDE JUST ABOVE STR 17 STA 1520 ON FRAME CORRODED. COMPLIED WITH FEDEX EA NR F-5310-T0358418 P1. FUSELAGE-MAINFRAME-STA 1520 FAILSAFE CHORD CORROSION ABOVE S-17L.SDR FDEA202012043026Shim · crackedMAIN CARGO FLOOR SUPPORT SHIM DAMAGED AT STA 1058 BETWEEN LBL 24 AND LBL 45. REMOVED SHIM (COVER PLATE) AT MAIN CARGO FLOOR SUPPORT STA 1058 BETWEEN LBL 24 AND LBL 45 AND FOUND CRACK AND OUT OF LIMITS, IAW B757 SRM 51-40-02-0G 53-00-51-1A. FABRICATED AND INSSDR FDEA202012023015Seat Track · corrodedMAIN CABIN SEAT TRACK FLANGE HAS CORROSION AT RBL 45 STA 1540. REMOVED CORROSION AT MAIN CABIN SEAT TRACK FLANGE RBL 45 STA 1540 AND AFTER EVALUATION FOUND SEAT TRACK OUT OF LIMITS, IAW B757 SRM 51-10-02-0G AND B757 SRM 53-00-52-1A FIG 101 DET VII. REMOVEDSDR FDEA202012023014Seat Track · corrodedMAIN CABAIN STA 1540 LBL 45 SEAT TRACK FLANGE CORRODED. REMOVED CORROSION AT MAIN CABIN STA 1540 LBL 45 SEAT TRACK FLANGE AND AFTER EVALUATION FOUND SEAT TRACK FLANGE OUT OF LIMITS, IAW B757 SRM 51-10-02-0G AND B757 SRM 53-00-52-1A FIG 101 DET VII. REMOVED ASDR FDEA202012023013Crease Beam · corrodedMAIN CABIN RT SIDE STA 450 TO 665 CREASE BEAM CORRODED. REMOVED CORROSION AT MAIN CABIN RT SIDE CREASE BEAM BETWEEN STA 450 TO 665 AND AFTER EVALUATION FOUND CREASE BEAM OUT OF LIMITS, IAW B757 SRM 53-30-13-1A FIG 101 DET VIII, SRM 51-10-02. REMOVED AND RESDR FDEA202011172886Pump · failedEMERGENCY DECLARED. LT HYD QTY AMBER CAS FOLLOWED LT ENGINE PUMP AMBER CAS, FOLLOWED BY LT HYD RESERVOIR AND LOSS OF FLUID .01 RF SHOWING. ALTN FLAP AND ALTN GEAR EXTENSIONS. T/S FOUND HYD FLUID COMING FROM THE NR 1 ENGINE HYD PUMP SEAL DRAIN WHILE SERVICINSDR 6PMR202012090466Seat Track · damagedAIRBORNE/PEMCO N/R 10248.0466 DISCREPANCY: MAIN DECK SEAT TRACK AT STA 905 AND RBL 24.75 HAS DEEP GOUGES ON SCALLOP TABS WHERE LOADING SYSTEM COMPONENT LOCKS DOWN. CORRECTIVE ACTION: REPAIRED MAIN DECK SEAT TRACK AT STA 905 RBL 24.75, IAW B757-200 SRM 53-00-5SDR 6PMR202012160327Skin · corrodedAIRBORNE/PEMCO N/R 10248.0327 DISCREPANCY: LT WING UPPER SKIN, FRONT SPAR, APPROXIMATELY WING STA 660 HAS CORROSION AROUND VORTEX GEN. CORRECTIVE ACTION: COMPLIED WITH RES 15402 FOR LT WING SKIN, FRONT SPAR WING STA 660 AROUND VORTEX GEN AREA, IAW EO 20495-6 SDR 6PMR202012160321Skin · corrodedAIRBORNE/PEMCO N/R 10248.0321 DISCREPANCY: LT WING UPPER SKIN, FRONT SPAR, APPROXIMATELY WING STA 342 HAS CORROSION AROUND FASTENER. CORRECTIVE ACTION: COMPLIED WITH RES 15402 FOR LT WING UPPER SKIN FRONT SPAR, WING STA 342 AREA, IAW EO 20495-6 REV IR.SDR 6PMR202012160322Skin · corrodedAIRBORNE/PEMCO N/R 10248.0322 DISCREPANCY: LT WING UPPER SKIN, FRONT SPAR, APPROXIMATELY WING STA 395 HAS CORROSION AROUND VORTEX GEN. CORRECTIVE ACTION: COMPLIED WITH RES NR 15402 FOR LT WING UPPER SKIN FRONT SPAR W/S 395 AROUND VORTEX GEN AREA (RES SEE COPY
Back to Boeing 757-2Y0