Boeing 757-24APF
Service difficulty reports · 16,046
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 = '75724APF' 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 = '75724APF' 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 IPXA2026090916126Strap · corrodedMAJOR REPAIR, APU INLET DOOR AFT STRAP HAD CORROSION. REMOVED OUTER STRAP IAW SRM 51-40-02-0G-0. INSTALLED NEW REPAIR PARTS AT INLET DOOR AFT STRAP IAW SRM 53-80-15-2R-1,REPAIR 1, DETAIL II.SDR IPXA2026083017738Screen · crackedAFT CARGO PANEL 152CZ SCREEN IS CRACKED. REMOVED CRACK SCREEN AND INSTALLED NEW SCREEN IAW AMM 25-50-03-404-003.SDR IPXA2026090305035Angle · brokenRIGHT WING #8 SLAT MAIN TRACK PANELS (2EA) ARE LOOSE. AFTER A MORE DETAILED INSPECTION, 02 LOOSE RIVETS AND 01 BROKEN ANGLE WERE FOUND ON THE PANELS. 02 RIVETS WERE REMOVED AND REPLACED, BROKEN ANGLE REMOVED. IAW B757-200PF SRM 51-40-02-0G-0. INSTALLED NEW BRSDR IPXA2026090305799Firewall · crackedNR 1 ENG OTBD T/R INTERNAL TOP METALLIC PLATE IS CRACKED. REMOVED INTERNAL TOP METALLIC PLATE DAMAGED AND REMOVED SEAL RETAINER (FOR ACCESS). #1 ENG O/B T/R. IAW B757-200PF SRM 51-40-02-0G-0. INSTALLED INTERNAL TOP METALLIC PLATE AND SEAL RETAINER. IAW B757-2SDR IPXA2026090314351Support Plate · corrodedFLOOR PANEL JOINT SKIN SUPPORT PLATE CORRODED BELOW NUT PLATE BS 1450 BETWEEN STRG 29-28 (BELOW FLOOR). REMOVED SPLICE STRAP BY SEVERELY EXFOLIATED AT AFT CARGO STA 1450 IAW SRM 51-40-02. INSTALLED NEW PART IAW SRM 51-40-02-0G.SDR IPXA2026090314733Strap · corrodedAPU INLET DOOR FWD STRAP HAS CORROSION. REMOVED FWD STRAP CORRODED I.A.W. B757-200PF SRM 51-40-02-0G-0. INSTALLED NEW STRAP ON APU INLET DOOR FWD IAW B757-200PF SRM 51-40-02.SDR IPXA2026090314768Angle · corrodedAPU INLET DOOR FWD UPPER CORNER ANGLE AT BS 1787.45, S3R HAS CORROSION. REMOVED UPPER CORNER ANGLE CORRODED IAW SRM 51-40-02-0G-0. INSTALLED NEW UPPER CORNER ANGLE APU INLET DOOR FWD UPPER BS 1787.45, S3R IAW SRM 51-40-02.SDR IPXA2026090514834Angle · corrodedAPU INLET DOOR FWD LOWER CORNER ANGLE AT STA 1787.45 S-6R HAS CORROSION. REMOVED LOWER CORNER ANGLE CORRODED IAW SRM 51-40-02-0G-0. INSTALLED NEW LOWER CORNER ON APU INLET DOOR BS 1787.45 S-6R IAW SRM 51-40-02.SDR IPXA2026090516057Angle · corrodedAPU INLET DOOR UPPER ANGLE FROM BS 1787.45 TO 1825.00 S-3R HAS A CORROSION. REMOVED UPPER ANGLE CORRODED IAW SRM 51-40-02-0G-0. INSTALLED NEW ANGLE UPPER ON APU INLET DOOR BS 1787.45 TO 1825, S3R IAW SRM 51-40-02.SDR IPXA2026091394413Panel · delaminatedFAULT: COMP-ZONE 600-RIGHT WING LE BEHIND #7 SLAT IB END HAS DELAMINATION. REMOVED FIXED PANEL DAMAGED R/WING I.A.W B757-200PF SRM 51-40-02-0G. CLEANED AND EVALUATED, ITEM IS REPAIRABLE. REMOVED DAMAGE AND FABRICATED NEW CORE PLUG. P/N HRH-10-1/8-3.0, B/N 000SDR IPXA2026090494430Skin · crackedRIGHT WING FIXED LEADING EDGE BEHIND THE NR 8 SLAT HAS A CRACK. ACOMPLISHED REPAIR IAW SREO-11855-REQ002.SDR IPXA2026091095169Panel · delaminatedMAJOR REPAIR, THE RT LWR FWD TORQUE BOX PANEL HAS 1EA DELAMINATED & DISBONDED AREA NEAR FSS 137.467. ACCOMPLISH REPAIR IAW SRM REV 125, 51-70-10-2R-2, 250 DEG F CURE USING SRM 51-70-10-2R-0. DAMAGE WAS REMOVED IAW SRM 51-70-10-2R. BONDED REPAIR PARTS IAW SDR IPXA2026082898567Angle · crackedFWD CARGO BAY, BS 560, RT E5 EE RACK ANGLE CRACKED. REMOVED THE DAMAGED ANGLE IAW SRM 51-40-02-0G. INSTALLED A NEW PART & FASTENERS IAW SRM 51-40-02-0G.SDR IPXA2026090886672Panel · corrodedMAJOR REPAIR, NR 1 ENGINE INBD INSIDE PANEL 443JL FWD LOWER PYLON SURFACE HAS CORROSION. CUT & REMOVED THE DAMAGE PART OF PYLON SKIN IAW SRM 51-10-02-0G-0. ACCOMPLISHED REPAIR IAW EO-98556-REQ1 AND STE-MAE EA 757-5450-27-A4612, REV-.SDR IPXA2026090787435Bracket · crackedTHS COMPARTMENT, APU PNEUMATIC DUCT LEFT CLIP SUPPORT CRACKED BS 1787.45. INSTALLED 1EA NEW BRACKET IAW SRM 51-40-02-0G-0.SDR IPXA2026082980687Bracket · crackedFAULT-STR-Z400 #2 ENG AFT PYLON, BRACKET UNDER DIAGONAL BRACE IS BROKEN. REMOVED NR 2 ENG AFT PYLON BRACKED UNDER DIAGONAL BRACE IAW 51-40-02. INSTALLED NEW BRACKET FOR NR 2 ENG AFT PYLON UNDER DIAGONAL BRACE AREA IAW SRM 51-40-02-0G.SDR IPXA2026082381790Bracket · misinstalledCREW ENTRY DOOR WARNING SENSOR BRACKET IS INCORRECTLY INSTALLED CAUSING CONTACT WITH CREW ENTRY DOOR SEAL WHEN CLOSING DEFERRED PER EO-98420 FOR 90 DAYS.SDR IPXA2026090472486Frame · crackedDEFERRAL. WHILE ACCOMPLISHED A DETAIL INSPECTION OF THE FUSELAGE SUPPORT, FRAME FOUND A 3 INCH LENGTH CRACK AT BS 1060. ACCOMPLISH THE PERMANENT REPAIR PER EO-98554-REQ1 AND STE-MAE EA 757-5340-27-A4611, REV.SDR IPXA2026090576186Bracket · crackedRT. MLG W/W FWD HD MODULE MOUNT SHOWS EVIDENCEOF A CRACK LOWER AREA. REMOVED MLG W/W FWD HD MODULE MOUNT IAW SRM 51-40-02-0G-0. INSTALLED NEW BRACKET (MLG W/W FWD HD MODULE MOUNT), IAW SRM 51-40-02-0G-0.SDR IPXA2026090377136Angle · corrodedFAULT Z-300 STR: APU INLET DOOR LOWER ANGLE FROM STA 1787.45 TO STA 1825 S-6R HAS CORROSION. REMOVED LOWER ANGLE CORRODED I.A.W. B757-200PF SRM 51-40-02-0G-0. INSTALLED NEW ANGLE LOWER ON APU INLET DOOR STA 1787.45 TO STA 1825 S-6R IAW B757-200PF SRM 51-40-02SDR IPXA2026082195946Unknown · odorAT FL 390-410 ACRID BURNING TYPE SMELL COMMING FROM THE PACKS. UNABLE TO DETERMINE WHICH ONE. BACK TO NORMAL ON DESCENT. ACCOMPLISHED TROUBLSHOOTING IAW FIM REF 21-00-01/301. INSPECTED CABIN RECIRCULATION SYSTEM & ACCOMPLISHED ADJ /TEST OF CABIN RECIRCULATIOSDR IPXA2026083072584Seat Track · corrodedAFTER REMOVAL OF RH OTBD FLOORBOARD IN MAIN CARGO FOUND RT OTBD SEAT TRACK INBD FLANGE UPPER SURFACE EXFOLIATED STA 440 RBL 45. ACCOMPLISHED THE PERMANENT REPAIR PER EO-98518-REQ1 AND STE-SAA EA 757-5310-01-B0818, REV. I/RSDR IPXA2026101651749Nut Plate · corrodedEXFOLATION FOUND AT MAIN CARGO DECK FS 1680 LBL 39.5 REMOVED 5 EA NUT-PLATE SUPPORTS ASSY, FOR ACCESS AT MAIN CARGO DECK, FLOOR STRUCTURE ON STEP 7.SDR IPXA2026081930589Flap System · warning messageEMD ON CLIMB OUT AT APPROX 3K' WE GOT A LE SLAT DISAGREE EICAS. MAINTAINED 230 KT OR LESS FOR ENTIRE FLIGHT. AFTER QRH PROCEDURE, MSG WENT OUT. PERFORMED BITE PROCEDURE IAW FIM 27-51 FAULT TREE 805 FLAP/SLAT ELECTRONIC UNIT (FSEU) BITE PROCEDURE. FOUND ALTERNASDR IPXA2026081830212Actuator · faultedATB, GEAR DISAGREE EICAS AND GEAR LIGHT. RAN CHECKLIST RETURN TO CAE & CAUTION LIGHT TOO. REVERSED DMP 32-30-1. REPLACED PROX SWITCH 065 REF FIM 32-09 FAULT TREE 821. ADJUSTED PROX SWITCHES 065 AND 078 AS REQUIRED TO 5.5 MILIHENRI NEAR BOTH LOCKED AND UNLOCKEDSDR IPXA2026101477713Deck Plate · corrodedMAJOR REPAIR, MAIN DECK CARGO, AFT DECK PLATE UPPER SURFACE HAD SEVERAL AREAS OF CORROSION, BS 1680 - 1700. REPAIRED IAW SRM 53-60-51-2R-5, REPAIR 5, FIGURE 201, DETAIL 1, REV 125. THIS IS A CATEGORY A REPAIR AND NO FURTHER ACTION IS REQUIRED.SDR IPXA2026090730575Mount · gougedSTR- DURING OK TO INSTALL FOUND #2 ENG PYLON AFT STRUT MOUNT I/B SIDE TO HAVE (3) GOUGES FROM BULGING SCREWS ON PNL 443ML ATA 54 ACCOMPLISHED THE REPAIR PER EO-98451-REQ1 AND STE-SAA EA 757-5724-01-B0812 REV IR. CASS FORM COMPLETED ON T3F18E009C5M2SDR IPXA2026081185235Bulb · burned outFLIGHT DECK EXIT SIGN LIGHTS BURNED OUT. REPLACED THE BULBS IAW AMM 33-51-01, OPS CHECK GOOD.SDR IPXA2026101456536Skin · debondedMAJOR REPAIR, LT ELEVATOR UPPER SKIN HAS ONE AREA OF DEBONDING 3 INCHES FROM T/E AND 4 INCHES OTBS OF ELEV STA 108.SDR IPXA2026082643744Spoiler Sys · malfunctioned***SUPPLEMENTAL SDR*** ON TOUCHDOWN SPOILERS DEPLOYED NORMALLY, BUT IMMEDIATELY RETRACTED. REQUIRED MANUAL RE-DEPLOYMENT + MANUAL BRAKES. REPLACED SPOILER SPEED BRAKE MECHANISM IAW AMM 27-62-02. SYSTEM FUNCTIONS NORMALLY. DMP REVERSED, PLACARDS REMOVED.SDR IPXA2026080643744Spoiler Sys · faultedON TOUCHDOWN SPOILERS DEPLOYED NORMALLY, BUT IMMEDIATELY RETRACTED. REQUIRED MANUAL RE-DEPLOYMENT & MANUAL BRAKES. STARTED REMOVAL OF SPEED BRAKE MECHANISM PER AMM 27-62-02 UP TO AND INCLUDING STEP H2.SDR IPXA2026080644501Window · scratchedFO€™S R2 WINDOW SCRATCHED HEAVILY AND IT IMPAIRS CREWS VIEW DURING GROUND OPS WITH BRIGHT LIGHT ON RAMP REPLACED WINDOW REF AMM 56-11-02.SDR IPXA2026090420255Gusset · corrodedAPU COMPARTMENT FWD BULKHEAD FWD SIDE BS 1885.2, LBL-12 & RBL-9. EXTENSIVE CORROSION. INSTALLED ONE SPLICE RING, ONE LOWER FRAME, ONE INNER TEE CHORD & TWO BRACKET ASSY (GUSSETS LT, RT) AT APU COMPARTMENT FWD BULKHEAD FWD SIDE BS 1885.2 LBL-12 & RBL-9 IAW SRM SDR IPXA2026082620255Bulkhead · corrodedAPU COMPARTMENT FWD BULKHEAD FWD SIDE BS 1885.2, LBL 12 & RBL 9. EXTENSIVE CORROSION.SDR IPXA2026080892392Splice Plate · corrodedUPON REMOVAL OF RT ELEVATOR TIP TRAILING EDGE WEDGE FOUND CORROSION ON UPPER SPLICE PLATE AND UPPER CONDUCTIVE FRAME. INSTALLED ONE UPPER SPLICE PLATE AT RT ELEVATOR IAW SRM 51-40-02-0G-0, & DWG 183N2901.SDR IPXA2026082469565Trunnion · corrodedLEFT MLG FWD TRUNNION BEARING INNER BORE HAS LIGHT PITTING CORROSION. INSTALLED LT MLG FWD TRUNNION SUPPORT ASSY IAW AMM 57-54-05-404-001.SDR IPXA2026080872397Bearing Race · corrodedLEFT MLG AFT TRUNNION BEARING RACE HAS PITTING CORROSION ON THE INSIDE. INSTALLED LMLG FWD TRUNNION SUPPORT ASSY IAW AMM 57-54-05-404-001, T/W ID: 21-968. PROCURED AND VERIFIED LT MLG AFT TRUNNION BEARING IS EFFECTIVE ON AIRCRAFT IAW AIPC 57-54-03-02, ITEM 66SDR IPXA2026080363542Duct · warning messageLEFT BLD DUCT LEAK EICAS MSG AT F340. QRH CHECKLIST COMPLETED AND L BLD DUCT LEAK MESSAGE WENT AWAY. PERFORMED FIM 26-90-15-00 SHEET 1 FIG 103 STEPS 1,10,2, SHEET 2 FIG 103 STEPS 3,4,11,12,13, & 14, HAD A FAULT CODE 14, PERFORMED STEP 15 FIG 103, SHEET 3. CARSDR IPXA2026081459454Seat Track · damagedMAJOR REPAIR, DURING THE INSPECTION FOR FLOORBEAM REPAIR AT BS 1200 AT MAIN CABIN, DAMAGE HOLE FOUND AT SEAT TRACK BS 1200 BL 0 (FWD HOLE) INSTALLED NEW SEAT TRACK, ANGLE AND STRAP IAW SRM 51-40-02 AND SRM-53-00-52-2R-7.SDR IPXA2026073130927Window · failedFO FWD WINDOW STARTED ARCING WE SHUT OF FWD WINDOW HEAT OUTER WINDOW SHATTERED RAN QRH PROCEDURE AND CONTINUED FLIGHT NO SIGNS OF LEAK OR WINDOW BEING DEFORMED. C/W REMAINING STEPS OF R1 WINDSHIELD INSTALL IAW AMM 56-11-01-424-015. OPS CK GOODSDR IPXA2026073030927Window · arcedFO FWD WINDOW STARTED ARCING WE SHUT OF FWD WINDOW HEAT OUTER WINDOW SHATTERED RAN QRH PROCEDURE AND CONTINUED FLIGHT NO SIGNS OF LEAK OR WINDOW BEING DEFORMED.SDR IPXA2026080421673Floorbeam · corrodedBULK CARGO MAIN CABIN FLOOR 2EA NUTPLATE RETAINERS CORRODED BS 1681 BL0 TO RBL6. INSTALLED 2EA NUTPLATE RETAINERS AT 1681 BL0 TO RBL6 IAW SRM 51-40-02-0G-0. AND DRAWING 146N5693.SDR IPXA2026090403739Doubler · corrodedRIGHT FUSELAGE, INSIDE TUNNEL OF TORQUE BOX NLG, WASTE PAN CORRODED. INSTALLED -81, -84, & -88 DOUBLERS, 4EA. GUSSETS, 6EA. TEECLIPS, 2EA. INTERCOSTAL CHANNELS, 10EA. CLIPS, 1EA. RING RETAINER, 1EA. DOOR LATCH ASSY, 4EA. SHIMS, 1EA. SERVICE VALVE ASSY & 1EA. SDR IPXA2026090803020Intercostal · bentINTERCOSTAL UPPER FLANGE IS BENT IN THE AFT LOWER CARGO BAY BS 1366 BETWEEN STR S24R-S25R. REMOVED 2EA STOP FITTINGS AT STA 1380 S24R 1EA CLIP AT STA 1360 S24R FOR ACCESS REMOVE 1EA INTERCOSTAL BETWEEN BS 1360-1380 S24R IAW SRM 51-40-02-0G-0 4. INSTALLED 2EASDR IPXA2026082401195Skin · misrepairedMAJOR REPAIR. MAJOR REPAIR F1-008 HAS WHAT APPEARS TO BE 2 SETS OF RIVET SET MARKS STA 1540-1580 STGR 28R-29R. VERIFIED STEP 34 ITEM HAS A REPETITIVE INSPECTION REQUIREMENT PER SRM 53-00-01-2R-29 REPAIR 29. AND GMM RII 04-02.SDR IPXA2026081797998Firewall · crackedFOUND A 0.400" LONG CRACK AT FIRE WALL SKIN LOWER AREA STA 1885.20 RBL 3.75" LOWER EDGE SKIN. ACCOMPLISHED THE REPAIR PER EO-98199-REQ1 AND EA 757-5380-27-A4583, REV. -, PRIOR TO FURTHER FLIGHT.SDR IPXA2026080995623Floor Panel · gougedACCOMPLISH A PERMANENT REPAIR PER SREO-3220-REQ002 AFT CARGO FLOOR PANEL. CUT OUT DAMAGE ON PANEL 153AF AFT CARGO FLOOR PANEL CUT OUT DIMENSIONS LENGTH 2.9" WIDTH 1.6" WITH A .500" RADIUS REF SREO-3220-REQ002 REV 1. INSTALLED REPAIR DOUBLER ON AFT CARGO COMPT SDR IPXA2026073088683Landing Gear · warning messageAIR TURN BACK, AFTER TK-OFF LANDING GEAR HANDLE IN UP POSITION AMBER GEAR DISCREET LIGHT ON AND EICAS GEAR DISAGREE MSG. QRH PROCEDURE COMPLETED AIR TURN BACK TO SLC. R&R NOSE LANDING GEAR RETRACT ACTUATOR PER AMM 32-34-01 UP TO AND INCLUDING STEP F.(13)(C)SDR IPXA2026072888683Warning Light · false activationAIR TURN BACK, AFTER TAKE-OFF LANDING GEAR HANDLE IN UP POSITION AMBER GEAR DISCREET LIGHT ON AND EICAS GEAR DISAGREE MSG. QRH PROCEDURE COMPLETED AIR TURN BACK TO SLC. PERFORMED NOSE GEAR SWING IAW AMM 32-34-00. OPS CHECKED GOOD AND GEAR SWING TIMES ARE WITHSDR IPXA2026090186382Web · crackedMAIN CABIN STA.515 APROX 10" RH FROM BUTTLINE HAS A CRACKED FLOOR SUPPORT WEB. INSTALLED FABRICATED FLOOR SUPPORT IAW SRM 51-40-02-0G-0.
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