N57111
Service difficulty reports · 120
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N57111' AND registry_match = 'registration' 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 n_number = 'N57111' AND registry_match = 'registration' 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 CALA2026102120497Skin · crackedRT WING SKIN UNDER ACCESS PANEL 643BB CRACKED AT HOLE 5. CRACK LOCATION IS AT THE 6 AND 12 0'CLOCK LOCATION. (FWD AND AFT)SDR CALA2026083119096Lamp · inoperativeR2 DOOR EXTERIOR EMERGENCY LIGHT INOP REPLACED LAMP REF AMM 33-51-00 NO HELP, FUTHER TROUBLE SHOOTING REQUIRED. RELAMPED R2 DOOR EXT EMERG LIGHT IAW 33-51-00. OPS CHECK NORMALSDR CALA2026061617129Power Supply · faultedEMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - LT AFT OVERWING LIGHT INOPERATIVE TROUBLESHOT SYS PER WDM 33-51-13, REMOVED AND REPLACED POWER SUPPLY M10954 PER AMM 33-51-07/201 AND PERFORMED OPERATIONAL CHECK OF LEFT AFT OVERWING EMERGENCSDR CALA2026061517118Feeder Cable · faultedEMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - ROW 25 PATHWAYS LIGHT INOP REMOVED ROW 25 PATHWAY LIGHT REF. AMM 33-51-11-963-065. FOUND LOOSE CABLE. RECONNECTED CABLE AND REINSTALLED LIGHT. OPS CHECK GOOD.SDR CALA2026042315659Girt Bar · fod2L SLIDE LIGHT WILL NOT SHOW ARMED FOUND DEBRI IN GIRT BAR AREA CLEANED AREA SLIDE ARMS NORMAL LIGHT TURNS ON AND NORMALSDR CALA2025122912500Warning Message · intermittentTE FLAP DISAGREE, EMERGENCY LANDING FLAPS 1 191K LBS SOFT LANDING. PERFORMED BITEOF ALL 3 FSUU PER AMM 27-51-TASK 803. FSEU 1 AND 3 BITE NO FAULTS, FSEU 2 HAD LE SLAT ASYM, INTERMITTENT FAULT. RESET AND RAN THE FLAPS COUPLE OF TIME UP AND DOWN. SYSTEM CHECSDR CALA2025101710213Slide · low pressureSLIDE PACK 4R IN RED R4 DOOR SLIDE PRESSURE NEEDLE IS APPROXIMATELY 2 TO 3 NEEDLES WITH INTO THE RED BAND. REF AMM 25-66-01-206-024. EMERGENCY ESCAPE SLIDE NIS AT IAH. HAS 2 PREVIOUS WRITE-UPS ON R4 DOOR SLIDE, REMOVED AND REPLACED 4R ESCAPE SLIDE REF AMM SDR CALA2025093009446Warning Message · false activationTE FLAPS DISAGREE CAUTION MSG FSEU 1 LAST LEG HAD FAULT 305 - INTERMITTENT, FSEU 2 HAD FAULT 327. PERFORMED FIM 27-51 TREE 805, BITE TEST GOOD, NO EXISTING FAULTS. MSG CLEARED. CYCLED FLAPS THROUGH FULL TRAVEL MULTIPLE TIMES, FLAPS OPERATED NORMALLY.SDR CALA2025090108310Transmission · faultyTE FLAP DISAGREE EICAS WHEN SELECTING FLAP 1 FROM UP. QRH ACTION ED ALT FLAP 20 LANDING, DECLARED EMERGENCY, FOUND # 8 TE FLAP OVERLOAD INDICATOR ON FLAP TRANSMISSION TRIPPED. PERFORMED STEP D.(8) IN AMM TASK 27-51-17-024-001 FOR FSEU 1 RESOLVER INPUTS, L FLSDR CALA2025081207621Slide · no discrepancyDOOR 4R SLIDE OUTSIDE GREEN BAND. INSPECTED DOOR 4 R DOOR SLIDE PER AMM 25-66-01-206-041 FOUND WITH LIMITS THE GREEN TEMP CAN GO 1/2 WIDTH OF GREEN BAND OK TO CONT.SDR CALA2025070306203Sensor · faultedAFTER TAKEOFF DURING INITIAL CLIMBS THE LEFT BLEED OFF LIGHT AND ASSOCIATED PACK OFF LIGHT ILLUMINATED. WE FOLLOWED THE QRH PROCEDURE AND WERE UNABLE TO RESET IT. AFTER CONTACTING TOMC A SECOND ATTEMPT WAS MADE AT 1.22 EPR AND STILL NOT RESET. REFERENCE: 36-10SDR CALA2025062706006Oil Filter · damagedRT ENGINE LOW OIL PSI ON TAKEOFF PRECAUTIONARY SHUTDOWN INFLT ESFR REQUIRED T/S RT ENGINE LOW OIL PSI IAW FIM 79-32 FT 805. REMOVED SCAVANGE AND PRESSURE FILTER IAW AM 79-00-00/601 FOUND DAMAGE ON SCAVANGE FILTER. SEE PICTURES ATTACHED. SEE BLOCK 23 FOR NEXT MSDR CALA2025061605555Slat System · faultedLE SLAT ASYM RAN THE QRH LANED WITH FLAPS 20 AFTER T/O DURING FLAP RETRACTION GOT LE ASSYM LIGHT AND EICAS ACFT ARRIVED AT GATE LE RETRACTED AND FLAPS AT 20 CONFIRMED PHYSICAL L/E ASYM. R SLAT = 25.96 DEG. L SLAT = 10.35 DEG. SLAT PDU = 9.51 DEGFOUND RIGHT SLASDR CALA2025061305546Indicator · faultyTE FLAP DISAGREE AT APPROX 1000FT. FLAPS STUCK AT 25.. INITIATED GO AROUND. CREW REPORTED THAT WHEN FLAP HANDLE WAS MOVED TO 30 THE FLAPS REMAINED AT 25 WITH TE FLAP DISAGREE MESSAGE. AFTER THEY MOVED THE HANDLE BACK TO 25 PER CHECKLIST MESSAGE WENT AWAY. TROSDR CALA2025042304163Frame · deformedFRAME STA 1440 BTW STR 26LH-27LH HAS A DENT ESFR ENTRY DENT OF FRAMESTA 1440 DIMENSIONS; L=1.5, W=.900 D=.070. PERFORME D REPAIR AS PER SRM 53-00-07-2R-5. REQUIRES REPEAT INSPECTIONS ADD EMP:V940985 PER SRM 53-00-07-2R-5 TABLE 2 ZONE 1 37,500 FLIGHT CYCLES AFTSDR CALA2025042104048Skin · gougedRIGHT WING O/B GLAP I/B L/E OF THE MAIN FL AP HAS A DEEP GOUGE. ECRA 5753-02305 ACCOMPLISHED ECRA 5753-02305 ON ST ENGINEERING NR 124688 SENT TO AVN FOR REPAIR ENTRY'SSDR CALA2025041803977Skin · damaged(SDR) - R/FUSELAGE BTWN STA 660/640 AND STRG 7/8 FOUND SMALL HOL E AT SKIN AREA. NO DOT. REF: NRC 125035 SMALL HOLE IN SKIN AREA BTWN STA 640-660 STR 7-8.SDR CALA2025041703945Bulkhead · damagedMLG WHEEL WELL FWD BULKHEAD LH SIDE AREA APROX 30 INCHES IN LENGTH STARTING AT INBD END. REF: NRC 1 24970.SDR CALA2025041703944Gate · corrodedR4 PAX DOOR UPPER GATE INTERNAL HAS AN AREA WITH CORROSI ON.REF: 124893.SDR CALA2025041703943Skin · corrodedL1 DOOR SURROUND STRUCTURE 1 3 EA FASTENER HOLES WITH DAMAGE AND CORROSION INDICATIONS. REF: NRC 124869SDR CALA2025041703942Bear Strap · crackedL1 DOOR SURROUND STRUCTURE 01 EA FASTENER HOLE WITH CRACK INDICATIONS AT 11 O'CLOCK POSITION ON BEAR STRAP LAYER (HOLE #1). REF: NRC 124873.SDR CALA2025041703947Frame · delaminatedDENT ON FRAME AT STA 760 STR 24 RH, REPAIRED DENT ON FRAME AT STA 760 STR 24RH PER 757-200 SRM 53-00-07-2R-5 REPAIR 5 FIG 201 DETAIL II. INSPECTION THRESHOLD 37500 OR 50000 AIRFRAME FLIGHT CYCLES, WHICHEVER COMES FIRST. REPEAT INSPECTIONS AT 12000 FLIGHT CYCSDR CALA2025041703941Skin · dentedAFT CARGO DOOR INNER SKIN BTW RIB 5-6 STA 1400-1420 WITH DENT.SDR CALA2025041503847Frame · dentedSUPPORT TASK: FRAME STA 1420 STR 25LH HAS A DENT. REPAIRED IAW B757-200 SRM 53-00-07-2R-5 FIG 201 DETAIL III DIP # 4483385 CREATED IAW B757-200SRM 53-00-07-2R-5 FIG 201 TABLE III RII VERIFIED REPAIR PERFORMEDSDR CALA2025041503855Frame Splice · gougedAFT CARGO COMP. FRAME SPLICE STA RH BTW STRG 23R-25R WITH GOUGES(3EA). ENTRY FOR SDR REPORTING FRAME SPLICE FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FRA ME SPLICE FABRICATED ON VT/MAE TRAV T25/1808559 IAW B757-200 SRM 53-00-07-1A-1 FIG 1 51-40-02SDR CALA2025041503852Stiffener · gouged(SDR) - B757-54-3-0055 ENGINE #1 NACELLE STRUT INTERNAL METAL CROSS BEAM LOCATED UNDER PRECOOLER HAS A GOUGE. DOT 75-005 HA-75. REWORKED CROSSBEAM PER EC/RA 5450-03002 AND VT MAE EA 754-5420-1 3-A3877 REV -.SDR CALA2025041403769Panel · crackedRIGHT WING GAP PANEL DAMAGED, BROKEN CORNER PART ON PANEL RACK BRACKET BROKEN IAW B757-200 SRM 51-40-02-0G-0. 03 NEW PARTS; 02 CORNER ANGLE#+25/1806839.SDR CALA2025041403768Bracket · corrodedLEFT MAIN WHEEL WELL LEADING-EDGE SEAL OUTBOARD BRACKET SHOWS SIGNS OF CORROSION AND DAMAGE. REMOVED AND REPLACED LE SEAL O/B BRACKET IAW B757-200 SRM 57-40- 02SDR CALA2025041403767Intercostal · corrodedINTERCOSTAL HAS CORROSION BTW STA 1420 AND 1440 LBL 10.4 5. REF: 124766 SDR REPORTING ONLY REMOVED AND REPLACED INTERCOSTAL IAW B757 SRM 51-40-02SDR CALA2025041403766Channel · crackedUPON REMOVAL OF O/B LH MLG BRACKET, CRACK FOUND AT MLG DOOR SEAL RETAINER SUPPORT CHANNEL AT FUS STA 1040 FROM LBL 3.0 TO LBL 63 .0 (REPAIR) REF: 124936 SDR REPORTING ONLY REMOVED AND REPLACED SEAL RETAINER SUPPORT CHANNEL IAW B757-200 SRM 51-40-02. VT MAE TRASDR CALA2025041403765Floor Support · cracked(SUPPORT TASK) CLOSE ZONE 110: NLG W/W THROUGH ACCESS PANEL 117C L NOSE FWD FUSELAGE MAIN DECK FLOORBEAM CHANNEL STA 345 BL0 CRAC KED. SDR REPORTING ONLY REPAIRED MAIN DESK FLOOR STABILIZER IAW B757-2 SRM 53-00-51-2R-1 2 AND REMOVED AND REINSTALL PANEL 117CL TSDR CALA2025041503850Floor Panel · crackedUPON PRE-INSTALL INSPECTION, CRACK FOUND AT FWD CARGO FLOOR PANEL 121BF - REF: NRC 125014 6100577518 SDR REPORTING ONLY REPAIRED FWD CARGO DECK PLATE (121BF) IAW B757-200 SRM 51-70-13- 0G-0.SDR CALA2025041703946Frame · dentedFRAME STA 1500 STR 26LH HAS A DENT. REPAIRED STA 1500 STR 26LH FRAME IAW B757-200 SRM 53-00-07-2R-S-DETAIL II. ACCOMPLIHSED ON VT NR 124726. INSPECTION THRESHOLD AT 37500 FLIGHT CYCLES AFTER REPAIR OR 50000 AIRCRAFT FLIGHT CYCLES WHICHEVER COMES FIRST. INSPSDR CALA2025041103702Stringer · dented(SDR) STRINGER HAS A DENT STA 1300 TO 1320 LBL 2.75. STRINGER FROM STA 1280 TO 1340 WAS REPAIRED DUE TO SRM B757-200 53-00-53 DOES NOT PERMIT DENT ON FLOOR STRINGER, AREA WAS REPAIR ED IAW B757-200 SRM 51-70-12 DETAIL VIISDR CALA2025041403752Gate · corrodedEA 5210-03219 REV B: R-2 DOOR UPPER GATE HAS CORROSION I N THE POCKETS. REMOVED AND REPLACED UPPER GATE AT R-2 DOOR IAW B757-200 AMM 52- 11-38-004-001 AND 52-11-38-404-009 AND ADJUSTMENT MUST BE PERFOR MED WITH EA 5210-03219 REVISION B.SDR CALA2025041103698Fairing · damaged(SDR) - LH WING-TO-BODY FAIRING 197BL HAS A FEW AFT SUPPORT CLIP FASTENER HOLES ELONGATED (OVER DRILLED) FROM RIVET REMOVALS WIT H 1EA RIVET NOT PUNCHED OUT ENTIRELY RESULTING IN A BENT ANGLE A ND POTENTIAL CRACK. REF: 124978 SDR REPORTING ONLY REMOVED AND REPSDR CALA2025041103696Door · corroded(SDR) - EA5210-03219 REV B:4L DOOR UPPER GATE HAS CORROSION IN T HE POCKETS REF: NRC 124892 SDR REPORTING PURPOSE ONLY REMOVED AND REPLACED L4 DOOR UPPER GATE IAW B757 AMM 52-11-38-40 4-009.SDR CALA2025041103695Channel · cracked(SDR) - RIGHT MAIN WHEEL WELL LEADING EDGE SEAL CRACKED, FROM OU T BOARD IN FRONT OF THE SECOND BRACKET. REF: NRC 124935 61005774 39 SDR REPORTING PURPOSE ONLY REMOVED AND REPLACED SUPPORT CHANNEL IAW B757 SRM 51-40-02.SDR CALA2025041103692Nut Plate · corroded(SDR) - (B757-06-3-0272) AT APU INLET INSIDE AFT TAIL COMPARTMEN T FWD INTERNAL NUTPLATE STRAP HAS CORROSION. DOT 140-009. REF: N RC 124486 SDR REPORTING PURPOSE ONLY REMOVED AND REPLACED NUT PLATE STRAPS IAW B757 SRM 57-40-02.SDR CALA2025041103691Angle · damaged(SDR) - LEFT WING SIDE OF BODY SPLICE INTERNAL LOWER METALIC ANG LE LOCATED BELOW OVERWING EMERGENCY EXIT HAS 02 PIECES OF SCREW STUCKED INTO NUT PLATE (02 EA). DOT 75-067 HA-75. REF: 124735 SDR REPORTING PURPOSE ONLY ANGLE LOCATED BELOW OVERWING EMRGENCY EXITSDR CALA2025040703582Intercostal · corrodedCORROSION ON AFT CARGO COMP INTERCOSTAL CHORD BTW STA 1480-1500 STRG 126-127. REF: NRC 124913. INTERCOSTAL ANGLE WAS REMOVED, NEW IN TERCOSTAL ANGLE WAS RECIEVED WITH TRAVELER#T25/1805770 AND NEW I NTERCOSTAL ANGLE WAS INSTALLED I.A.W. B757-200 SRM 51-40-02.SDR CALA2025011001859Light · detachedSEAT 40C EMERGENCY PATH LIGHT HANGING FROM SEAT RESECURED LIGHT ASSY. OK TO CONTINUE.SDR CALA2024121101472Slide · faultyREMOVED R1 DOOR SLIDE REMOVED AND REPLACED R1 DOOR SLIDE IAW AMM 25-66-01. PARTS USED: 19-2566-9-0002, QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1375666 SN OFF 0965.SLIDE, B757-200 OFF 19-2566-9-0002 0965 ON 19-2566-9-0002 5075 RII INSPECTION REQUIREMESDR CALA2024112502923Actuator · misinstalledFOUND AILERON TRIM ACTUATOR INSTALLED INCORRECTLY, BARREL NUT RETAINER MISSING. CORRECTLY REINSTALLED BOLT RETERNER IAW AMM 27-11-14-022-008.SDR 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 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 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 CALA2024071102006Tire · failed#5 MLG TIRE BLOWN ON LANDING. REMOVED AND REPLACED #5 MAIN TIRE IAW BOEING 757 AMM 32-45-01.SDR CALA2024060301665Radome · delaminatedREVIEW ALL DISCREPANCIES RECORDED AND INITIATE SFR/SDR REPORTS AS REQUIRED. {B757-05-3-0003} - SDR TO BE RAISED POST RADOME REPLACEMENT DUE AIRCRAFT BEING OUT OF SERVICE PER GMM 04-20-16 PER GMM 04-20-16 SDR BEING RAISED DUE TO AIRCRAFT BEING OUT OF SERVICE SDR CALA2024022300514Slat · tornRT WING INBD SLAT T/E TORN. 4 FT X 1 FT SECT SKIN RIPPED OFF HNY COMB EXPOSED AND MISSING SLAT INSTL-WING LE NO. 5 AND NO. 6 INBD REFERENCE: 27-81-01-01 PHOTOS LABOR HOUR AND GROUND TIME INFORMATION UPDATE ONLY. PART ORDERED, REMOVED NO.6 INBOARD LE SLAT IN RE
Back to N57111