# Service difficulty reports: N57111

A list on [N57111](https://openairdocs.org/aircraft/N57111.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 120 reports

- [SDR CALA2026102120497](https://openairdocs.org/sdr/CALA2026102120497.md): Skin · cracked · Oct 17, 2026 · N57111 · Boeing 757224 · Wing, Plate/Skin
  > RT 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 CALA2026083119096](https://openairdocs.org/sdr/CALA2026083119096.md): Lamp · inoperative · Aug 29, 2026 · N57111 · Boeing 757224 · Emergency Lighting
  > R2 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 NORMAL
- [SDR CALA2026061617129](https://openairdocs.org/sdr/CALA2026061617129.md): Power Supply · faulted · Jun 13, 2026 · N57111 · Boeing 757224 · Emergency Lighting
  > EMERGENCY 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 EMERGENC
- [SDR CALA2026061517118](https://openairdocs.org/sdr/CALA2026061517118.md): Feeder Cable · faulted · Jun 12, 2026 · N57111 · Boeing 757224 · Light System Wiring
  > EMERGENCY 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 CALA2026042315659](https://openairdocs.org/sdr/CALA2026042315659.md): Girt Bar · fod · Apr 19, 2026 · N57111 · Boeing 757224 · Emergency Equipment
  > 2L SLIDE LIGHT WILL NOT SHOW ARMED FOUND DEBRI IN GIRT BAR AREA CLEANED AREA SLIDE ARMS NORMAL LIGHT TURNS ON AND NORMAL
- [SDR CALA2025122912500](https://openairdocs.org/sdr/CALA2025122912500.md): Warning Message · intermittent · Dec 26, 2025 · N57111 · Boeing 757224 · Trailing Edge Flap Control System
  > TE 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 CHEC
- [SDR CALA2025101710213](https://openairdocs.org/sdr/CALA2025101710213.md): Slide · low pressure · Oct 15, 2025 · N57111 · Boeing 757224 · Escape Slide
  > SLIDE 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 CALA2025093009446](https://openairdocs.org/sdr/CALA2025093009446.md): Warning Message · false activation · Sep 27, 2025 · N57111 · Boeing 757224 · Trailing Flap Position Indicating System
  > TE 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 CALA2025090108310](https://openairdocs.org/sdr/CALA2025090108310.md): Transmission · faulty · Aug 29, 2025 · N57111 · Boeing 757224 · Trailing Edge Flap Actuator
  > TE 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 FL
- [SDR CALA2025081207621](https://openairdocs.org/sdr/CALA2025081207621.md): Slide · no discrepancy · Aug 9, 2025 · N57111 · Boeing 757224 · Escape Slide
  > DOOR 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 CALA2025070306203](https://openairdocs.org/sdr/CALA2025070306203.md): Sensor · faulted · Jun 30, 2025 · N57111 · Boeing 757224 · Engine RPM Indicating System
  > AFTER 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: 36-10
- [SDR CALA2025062706006](https://openairdocs.org/sdr/CALA2025062706006.md): Oil Filter · damaged · Jun 24, 2025 · N57111 · Boeing 757224 · Turbine Engine Oil System
  > RT 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 M
- [SDR CALA2025061605555](https://openairdocs.org/sdr/CALA2025061605555.md): Slat System · faulted · Jun 12, 2025 · N57111 · Boeing 757224 · Leading Edge Slat Control System
  > LE 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 SLA
- [SDR CALA2025061305546](https://openairdocs.org/sdr/CALA2025061305546.md): Indicator · faulty · Jun 11, 2025 · N57111 · Boeing 757224 · Trailing Flap Position Indicating System
  > TE 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. TRO
- [SDR CALA2025042304163](https://openairdocs.org/sdr/CALA2025042304163.md): Frame · deformed · Apr 18, 2025 · N57111 · Boeing 757224 · Fuselage Main, Frame
  > FRAME 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 AFT
- [SDR CALA2025042104048](https://openairdocs.org/sdr/CALA2025042104048.md): Skin · gouged · Apr 18, 2025 · N57111 · Boeing 757224 · Trailing Edge Flaps
  > RIGHT 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'S
- [SDR CALA2025041803977](https://openairdocs.org/sdr/CALA2025041803977.md): Skin · damaged · Apr 17, 2025 · N57111 · Boeing 757224 · Fuselage Main, Plate/Skin
  > (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 CALA2025041703945](https://openairdocs.org/sdr/CALA2025041703945.md): Bulkhead · damaged · Apr 16, 2025 · N57111 · Boeing 757224 · Fuselage Main, Bulkhead
  > MLG WHEEL WELL FWD BULKHEAD LH SIDE AREA APROX 30 INCHES IN LENGTH STARTING AT INBD END. REF: NRC 1 24970.
- [SDR CALA2025041703944](https://openairdocs.org/sdr/CALA2025041703944.md): Gate · corroded · Apr 16, 2025 · N57111 · Boeing 757224 · Service Doors
  > R4 PAX DOOR UPPER GATE INTERNAL HAS AN AREA WITH CORROSI ON.REF: 124893.
- [SDR CALA2025041703943](https://openairdocs.org/sdr/CALA2025041703943.md): Skin · corroded · Apr 15, 2025 · N57111 · Boeing 757224 · Fuselage Main, Plate/Skin
  > L1 DOOR SURROUND STRUCTURE 1 3 EA FASTENER HOLES WITH DAMAGE AND CORROSION INDICATIONS. REF: NRC 124869
- [SDR CALA2025041703942](https://openairdocs.org/sdr/CALA2025041703942.md): Bear Strap · cracked · Apr 15, 2025 · N57111 · Boeing 757224 · Fuselage Main, Plate/Skin
  > L1 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 CALA2025041703947](https://openairdocs.org/sdr/CALA2025041703947.md): Frame · delaminated · Apr 12, 2025 · N57111 · Boeing 757224 · Fuselage Main, Frame
  > DENT 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 CYC
- [SDR CALA2025041703941](https://openairdocs.org/sdr/CALA2025041703941.md): Skin · dented · Apr 12, 2025 · N57111 · Boeing 757224 · Cargo/Baggage Doors
  > AFT CARGO DOOR INNER SKIN BTW RIB 5-6 STA 1400-1420 WITH DENT.
- [SDR CALA2025041503847](https://openairdocs.org/sdr/CALA2025041503847.md): Frame · dented · Apr 12, 2025 · N57111 · Boeing 757224 · Fuselage Main, Frame
  > SUPPORT 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 PERFORMED
- [SDR CALA2025041503855](https://openairdocs.org/sdr/CALA2025041503855.md): Frame Splice · gouged · Apr 11, 2025 · N57111 · Boeing 757224 · Fuselage Main, Frame
  > AFT 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 51-40-02
- [SDR CALA2025041503852](https://openairdocs.org/sdr/CALA2025041503852.md): Stiffener · gouged · Apr 11, 2025 · N57111 · Boeing 757224 · Nacelle/Pylon Miscellaneous Structure
  > (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 CALA2025041403769](https://openairdocs.org/sdr/CALA2025041403769.md): Panel · cracked · Apr 11, 2025 · N57111 · Boeing 757224 · Wing, Plate/Skin
  > RIGHT 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 CALA2025041403768](https://openairdocs.org/sdr/CALA2025041403768.md): Bracket · corroded · Apr 11, 2025 · N57111 · Boeing 757224 · Fuselage Main, Attach Fittings
  > LEFT 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- 02
- [SDR CALA2025041403767](https://openairdocs.org/sdr/CALA2025041403767.md): Intercostal · corroded · Apr 11, 2025 · N57111 · Boeing 757224 · Fuselage Miscellaneous Structure
  > INTERCOSTAL HAS CORROSION BTW STA 1420 AND 1440 LBL 10.4 5. REF: 124766 SDR REPORTING ONLY REMOVED AND REPLACED INTERCOSTAL IAW B757 SRM 51-40-02
- [SDR CALA2025041403766](https://openairdocs.org/sdr/CALA2025041403766.md): Channel · cracked · Apr 11, 2025 · N57111 · Boeing 757224 · Fuselage Miscellaneous Structure
  > UPON 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 TRA
- [SDR CALA2025041403765](https://openairdocs.org/sdr/CALA2025041403765.md): Floor Support · cracked · Apr 11, 2025 · N57111 · Boeing 757224 · Fuselage Miscellaneous Structure
  > (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 T
- [SDR CALA2025041503850](https://openairdocs.org/sdr/CALA2025041503850.md): Floor Panel · cracked · Apr 10, 2025 · N57111 · Boeing 757224 · Fuselage Floor Panel
  > UPON 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 CALA2025041703946](https://openairdocs.org/sdr/CALA2025041703946.md): Frame · dented · Apr 9, 2025 · N57111 · Boeing 757224 · Fuselage Main, Frame
  > FRAME 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. INSP
- [SDR CALA2025041103702](https://openairdocs.org/sdr/CALA2025041103702.md): Stringer · dented · Apr 9, 2025 · N57111 · Boeing 757224 · Fuselage Main, Longeron/Stringer
  > (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 VII
- [SDR CALA2025041403752](https://openairdocs.org/sdr/CALA2025041403752.md): Gate · corroded · Apr 8, 2025 · N57111 · Boeing 757224 · Passenger/Crew Doors
  > EA 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 CALA2025041103698](https://openairdocs.org/sdr/CALA2025041103698.md): Fairing · damaged · Apr 8, 2025 · N57111 · Boeing 757224 · Aerodynamic Fairings
  > (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 REP
- [SDR CALA2025041103696](https://openairdocs.org/sdr/CALA2025041103696.md): Door · corroded · Apr 8, 2025 · N57111 · Boeing 757224 · Passenger/Crew Doors
  > (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 CALA2025041103695](https://openairdocs.org/sdr/CALA2025041103695.md): Channel · cracked · Apr 8, 2025 · N57111 · Boeing 757224 · Fuselage Miscellaneous Structure
  > (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 CALA2025041103692](https://openairdocs.org/sdr/CALA2025041103692.md): Nut Plate · corroded · Apr 8, 2025 · N57111 · Boeing 757224 · APU Cowling/Containment
  > (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 CALA2025041103691](https://openairdocs.org/sdr/CALA2025041103691.md): Angle · damaged · Apr 8, 2025 · N57111 · Boeing 757224 · Aerodynamic Fairings
  > (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 EXIT
- [SDR CALA2025040703582](https://openairdocs.org/sdr/CALA2025040703582.md): Intercostal · corroded · Apr 3, 2025 · N57111 · Boeing 757224 · Fuselage Miscellaneous Structure
  > CORROSION 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 CALA2025011001859](https://openairdocs.org/sdr/CALA2025011001859.md): Light · detached · Jan 8, 2025 · N57111 · Boeing 757224 · Emergency Lighting
  > SEAT 40C EMERGENCY PATH LIGHT HANGING FROM SEAT RESECURED LIGHT ASSY. OK TO CONTINUE.
- [SDR CALA2024121101472](https://openairdocs.org/sdr/CALA2024121101472.md): Slide · faulty · Dec 8, 2024 · N57111 · Boeing 757224 · Escape Slide
  > REMOVED 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 REQUIREME
- [SDR CALA2024112502923](https://openairdocs.org/sdr/CALA2024112502923.md): Actuator · misinstalled · Nov 22, 2024 · N57111 · Boeing 757224 · Aileron Tab Control System
  > FOUND AILERON TRIM ACTUATOR INSTALLED INCORRECTLY, BARREL NUT RETAINER MISSING. CORRECTLY REINSTALLED BOLT RETERNER IAW AMM 27-11-14-022-008.
- [SDR CALA2024093000704](https://openairdocs.org/sdr/CALA2024093000704.md): Screen · faulted · Sep 27, 2024 · N57111 · Boeing 757224 · Compressor Bleed Valve
  > PDA 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 I
- [SDR CALA2024092400682](https://openairdocs.org/sdr/CALA2024092400682.md): Governor · faulty · Sep 21, 2024 · N57111 · Boeing 757224 · Fuel Controlling System
  > RIGHT 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 O
- [SDR CALA2024091900656](https://openairdocs.org/sdr/CALA2024091900656.md): Bottle · low pressure · Sep 17, 2024 · N57111 · Boeing 757224 · Emergency Equipment
  > PASSENGER 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, T
- [SDR CALA2024071102006](https://openairdocs.org/sdr/CALA2024071102006.md): Tire · failed · Jul 9, 2024 · N57111 · Boeing 757224 · Tire
  > #5 MLG TIRE BLOWN ON LANDING. REMOVED AND REPLACED #5 MAIN TIRE IAW BOEING 757 AMM 32-45-01.
- [SDR CALA2024060301665](https://openairdocs.org/sdr/CALA2024060301665.md): Radome · delaminated · Jun 2, 2024 · N57111 · Boeing 757224 · Emergency Lighting
  > REVIEW 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 CALA2024022300514](https://openairdocs.org/sdr/CALA2024022300514.md): Slat · torn · Feb 19, 2024 · N57111 · Boeing 757224 · Leading Edge Devices
  > RT 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

Next page: https://openairdocs.org/aircraft/N57111/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N57111/reports

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