Boeing 757-24APF
Service difficulty reports · 16,054
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 IPXA2026040178991Angle · crackedFAULT - Z400 - STR #1 PYLON INBD SIDE THROUGH CIRCLE ACCESS PANEL, INTERNAL AFT UPPER SURFACE HAS A CRACKED STRUCTURAL CLIP. DOT 93-012. REMOVED CRACKED CLIP AT #1 PILON I/B SIDE INTERNAL AREA AFT UPPER SURFACE IAW B757-200 SRM 51-40-02. INSTALLED CLIP IAW B75SDR IPXA2026032668052Gusset · crackedLEFT AND RIGHT LATCH STOPS AT THE CUT-OUT, FOUR BRACKETS ARE CORRODED. INSTALLED THE FOUR BRACKETS, LT OTBD GUSSET LT INBD GUSSET, RT INBD GUSSET, RT OTBD GUSSET IAW SRM 51-40-02.SDR IPXA2026032579167Angle · crackedFWD CARGO THROUGH ACCESS PANEL 122AZ CUTOUT HAS A CRACK. INSTALLED NEW CORNER ANGLE ON INNER LOWER STRUCTURE AND REINSTALLED INNER LOWER STRUCTURE ON ACCESS PANEL 122AZ I.A.W SRM 51-40-02.SDR IPXA2026031475944Web · corrodedCORROSION ON FLOOR FORWARD OF PILOTS CONTROL COLUMN.SDR IPXA2026032179037Bracket · crackedRIGHT MLG WHEEL WELL, FWD SEAL RETAINER, SECOND FROM MOST OUTBD BRACKET IS CRACKED. DOT 93-013 INSTALLED ANGLE AT RH MLG WHEEL WELL, FWD SEAL RETAINER, SECOND FROM MOST OUTBD IAW SRM 51-40-02-0G-0.SDR IPXA2026032070105Check Valve · faultedFUEL IMBALANCE IN FLIGHT OF 1900LBS WITH FUEL CONFIG MESSAGE. 7.2 LBS LEFT TANK, 9.1 LBS RIGHT TANK. ALL ENGINE INSTRUMENTS NORMAL INCLUDING FUEL FLOW. FMC CALCULATED AND TOTALIZER FUEL WITHIN 100 LBS NO FUEL IMBALANCE NOTED DURING ENGINE RUNS. REMOVED AND RESDR IPXA2026031670105Fuel Sys · out of balanceFUEL IMBALANCE IN FLIGHT OF 1900LBS WITH FUEL CONFIG MESSAGE. 7.2 LBS LEFT TANK, 9.1 LBS RIGHT TANK. ALL ENGINE INSTRUMENTS NORMAL INCLUDING FUEL FLOW.SDR IPXA2026040360672Plate · crackedMAJOR REPAIR. MAIN DECK CARGO DOOR INNER AFT LOWER SKIN PLATE BROKEN. INSTALLED AFT LINNING PANEL AT MAIN DECK CARGO DOOR IAW B757-200 AMM 25-55-00-400-807SDR IPXA2026032857090Support Channel · crackedLH MLG WW, DOOR FWD CUTOUT, APPROX STA1080, BELOW BULB SEAL HAS BRACKET AT O/B SIDE BROKEN. DOT 103-25. REMOVED PANEL 197CL, SEAL RETEINER AND SUPPORT- CHANNEL (BROKEN) I.A.W. B757-200 SRM 51-40-02. INSTALLED PANEL 197BL IAW B757-200 SRM 51-40-02-0G. INSPECTSDR IPXA2026040156533Bracket · crackedLEFT MLG WW, BULKHEAD BS 1180, THROUGH PANEL 143XAL, VERTICAL BRACKET AT JOGGLE AREA HAS A CRACK. INSTALLED VERTICAL BRACKET AT LH MLG WW, BULKHEAD 1180, I.A.W B757-200 SRM 51-40-02.SDR IPXA2026032853253Support Channel · crackedRIGHT MLG WW CUT-OUT FWD SEAL RETAINER ATTACHMENT FRAME OTBD END CRACKED. INSTALLED THE SUPPORT CHANNEL AND SEAL RETAINER IAW SRM 51-40-02.SDR IPXA2026032762155Skin · delaminatedMAJOR REPAIR. SKIN PANEL AT STA 1992 - 1963 HAS DAMAGED HONEYCOMB. REPAIR ACCOMPLISHED IAW PER SRM 51-70-10-2R-4 (REPAIRS TO LARGE USING SRM 51-70-10-2R-0 REPAIR GENERAL GUIDELINES PER SRM 53-80-01-2R-0SDR IPXA2026032057044Angle · crackedLH MLG WW, DOOR FWD CUTOUT, APPROX STA1080, HAS BRACKETS BROKEN (6EA). INSTALLED ANGLES (6EA) AT LT MLG WW, DOOR FWD CUTOUT, APPROX BS 1080 IAW SRM 51-40-02-0G-0.SDR IPXA2026033150191Strap · corrodedMAJOR REPAIR, APU INLET DOOR AFT STRAP AT STA 1825 WITH CORROSION. REMOVED CORROSION IAW B757 -200 SRM 51-10 02. OK TO INSTALL REPAIR PARTS AT APU INLET DOOR AFT STRAP STA 1825. COMPLIED WITH EA 757-5380-27-A4405 PRELIM 1 REV - AND COMPLIED WITH ALL REQUIREMESDR IPXA2026031646305Door · blownDURING WALK AROUND FOUND A BLOW OUT PANEL DAMAGED ON THE RIGHT ENGINE PYLON R & R STRUT RELIEF AND ACCESS DOOR PER AMM 54-53-01SDR IPXA2026040406218Door Frame · crackedMAIN CARGO DOOR LOWER FWD SIDE FRAME HAS A CRACK ON UPPER RADIUS NEXT TO CAM FITTING MAIN CARGO DOOR (P/N: 65-25326-18, S.N: 056) AT STATION 483 TO 488 AND WL.210 ON LOWER BEAM (P/N: 65-25338-60) A CRACK DAMAGE REPAIR ACCOMPLISHED PER STE SAA E.A # 757-5232-0SDR IPXA2026031153938Angle · crackedNUMBER 2 ENG PYLON FWD LOWER PLATE CRACKED INBD-OTBD SIDE. INSTALLED ANGLE AT NR 2 ENG PYLON FWD LOWER IAW SRM 51-40-02.SDR IPXA2026030647384Light · inoperativeEMERG LIGHT INOP REPLACED EMERGENCY LIGHT PUSHBUTTON SW CKT DRAWER AND BOTH LAMPS, REF SWPM 20-84-18. OPS CK GOOD, REF MM33-51-00-715-003.SDR IPXA2026031834297Strap · corrodedAFT CARGO COMP. CEILING STABILIZATION STRAP HAS CORROSION, APPROX BTW BS 1400 AND BS 1420, RBL 45.50, ID STICKER NUM. (085-073). ATA 53-20 INSTALLED CEILING STABILIZATION STRAP, REPLACEMENT SECTION AND 2EA REPAIR SPLICES IN AFT CARGO COMPARTMENT BETWEEN STA SDR IPXA2026030934060Strap · corrodedAFT CARGO COMP. CEILING STABILIZATION STRAP HAS CORROSION, APPROX BTW BS 1400 AND BS 1420, RBL 24.75, ID STICKER NUM. (085-078). ATA 53-20 INSTALLED NEW STABILIZATION STRAP P/N STESAA7003349028-2 FOR AFT CARGO CEILING COMP BETWEEN STA 1360 AND STA 1440 IAW B7SDR IPXA2026040633932Frame · dentedMAJOR REPAIR. AFT CARGO BAY FRAME UPPER ANGLE DENTED, APPROX AT BS 1220, BTW STGR 26L AND STGR 27 L, REPAIR WAS ACCOMPLISHED IAW EO-96988-REQ1 AND VT-SAA EA 757-5360-01-B0699 REV IR PRIOR TO FURTHER FLIGHT.SDR IPXA2026040233747Frame · dentedMAJOR REPAIR, AFT CARGO COMP. FRAME UPPER CHORD HAS 3 EA DENT, APPROX AT BS 1360, BTW STGR 25R AND STGR 27 R, ID STICKER NUM. (085-068). ATA 53-10. REMOVED (3EA) SOLID RIVETS FROM DISCREPANT AREAS AT FS 1360 INBD OF STR 26R FOR ACCESS IAW B757-200PF SRM 51-40-SDR IPXA2026040133784Intercostal · dentedAFT CARGO COMP. INTERCOSTAL HAS A DEFORMATION APPROX BTW BS 1360 AND BS 1380, BTW STGR 24R AND STGR 25 R, ID STICKER NUM. (085-069). ATA 53-10 INSTALLED 1EA. SHIM AND NEW INTERCOSTAL IAW B757-200PF SRM 51-40-02-0G-0.SDR IPXA2026033134415Floorbeam · corrodedMAJOR REPAIR, MAIN DECK CARGO COMP. FLOOR BEAM LWR CHORD HAS CORROSION, APPROX AT BS 1400, BTW RBL 24.75 AND RBL 45.50, ID STICKER NUM. (085-074). ATA 53-10. REMOVED CORROSION AT MAIN CARGO COMP. FLOOR BEAM LWR CHORD APPROX. AT BS 1400, BTW RBL 24.75 AND RBLSDR IPXA2026033134469Floorbeam · corrodedMAJOR REPAIR, MAIN DECK CARGO COMP. FLOOR BEAM LWR CHORD HAS CORROSION, APPROX AT BS 1420, BTW RBL 24.75 AND RBL 45.50, ID STICKER NUM. (085-075). ATA 53-10. REMOVED 5EA ANGLES FROM AFT CARGO COMP. FRAME UPPER CHORD APPROX AT BS 1360, BTW STGR 25R AND STGR 27SDR IPXA2026031939735Tee Angle · corrodedFAULT-STR-ZONE 100. RH LOWER MIDDLE FUSELAGE STA 1040-1060 RBL 65 T-CHORD CORRODED. DOT 28-05 INSTALLED NEW T-CHORD AT RH LOWER MIDDLE FUSELAGE STA 1040-1060 RBL 65 IAW B757-200PF SRM 51-40-02-0G-0SDR IPXA2026030931783Window · warning messageRIGHT FWD WINDOW EICAS POSTED DURING TAXI IN, AFTER LANDING. REMOVED AND REPLACED FO'S WINDSHIELD IAW AMM 56-11-01. OPS CHECKED GOOD.SDR IPXA2026030541774Adc · inoperativeAIR TURN BACK - UNRELIABLE AIRSPEED DURING CLIMB OUT. R&R L/H ADC , OPS CHECK GOOD IAW 757 AMM 34-12-01. WORK DONE BY CAT QUALIFIED MECHANIC.SDR IPXA2026030531783Terminal · out of toleranceR FWD WINDOW EICAS POSTED ON TAXI IN AFTER LANDING AS PER FIM 30-41 FT 804 NOTE, APU HISTORY REVIEWED IN MTX AND NO START DISCREPANCIES NOTED IN PAST 60 DAYS. T/S PER FIM 30-41- FT 803, FOUND WINDOW POWER TERMINAL RESISTANCES TO BE OUT OF TOLERANCE. J1-J5 11.2SDR IPXA2026032721947Floor Panel · corrodedEXFOLIATION FLOOR PANEL RT SIDE AFT CARGO BS 1600-1560, STR 27 AND 28R. REMOVED CORROSION FROM FLOOR PANEL RT SIDE AFT CARGO. MAT LOSS MORE THAN 50%. MAX ALLOWABLE IS 10%. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 101. INSTALLED REPAIR DOUBLER IN SDR IPXA2026031919295Tee Angle · corrodedLOWER HALF OF FUSELAGE TEE ANGLE BETWEEN BS 1040 & 1060, AROUND STRINGER 25R HAD CORROSION. INSTALLED A NEW TEE ANGLE BTWN BS 1040 - 1060, STRINGER 25R IAW SRM 51-40-02-0G-0.SDR IPXA2026032119365Angle · corrodedLOWER HALF OF FUSELAGE RH PACK HOT AIR EXHAUST FRONT STRUCTURE ANGLE BETWEEN STR 1040 AND STR 1060 HAS CORROSION DOT 115-004. INSTALLED NEW INTERCOSTAL AND REINSTALLED COVER SUPPORT HOT AIR EXHAUST, IAW B757-200PF, SRM 51-40-02.SDR IPXA2026032803895Splice Angle · corrodedBS 1992 AT THE 6 O`CLOCK POSITION HAD CORROSION BETWEEN FRAME AND SPLICE ANGLE TO INCLUDE SURROUNDING EXTERNAL SURFACES. VERIFIED STEP 10 IAW GMM. INSTALLED REPLACED SPLICE, REINSTALLED DOUBLER AT STA. 1992, 6:0 O'CLOCK PER B757-200PF SRM 51-40-02-0G-0SDR IPXA2026031600239Support Angle · corrodedAFT CARGO COMPT RIGHT LOWER BULKHEAD SUPPORT AT STA.1640 SHOWS EVIDENCE OF CORROSION AND A CRACK DOT 47-11 INSTALLED 2 ANGLES IAW SRM 51-40-02.SDR IPXA2026030974670Floorboard · brokenMAJOR REPAIR, MCD FLOORBOARD 241XCF AFT CORNER IS BROKEN. THE FLOORBOARD FABRICATED IAW SREO-9692-REQ001, VERIFIED RII REQUIREMENT COMPLETED, IAW UPS GMM 04.02.01.15.SDR IPXA2026031579385Transition Panel · corrodedTRANSITION PANEL FROM AFT CARGO COMPARTMENT STA1310 TO STA 1360 R/H CORROSION AND HOLES DAMAGED. INSTALLED NEW TRANSITION PANEL AFT CARGO COMPARTMENT STA 1310 TO STA 1360 R/H IAW SRM 51-40-02-0GSDR IPXA2026031784226Angle · crackedNR 1 ENG AFT PYLON FARING SUPPORT ANGLE L BRACKET ON INBD SIDE IS CRACKED. REMOVED BRACKET ON NR 1 ENGINE AFT PYLON FARING IAW SRM 51-40-02. INSTALLED A NEW L ANGLE IAW SRM 51-40-02.SDR IPXA2026032470530Filler · corrodedAFT CARGO, BS 1480 BILDGE AREA, NEAR ANTENNA LOWER SURFACE HAS CORRODED. INSTALLED NEW FILLER RADIUS IAW SRM 51-40-02-0G.SDR IPXA2026030970913Floor Panel · damagedMAJOR REPAIR, FLOOR PANEL 241XDF IS DAMAGED IN A CORNER. DOT 23-027 INSPECTION FABRICATION OF FLOOR PANEL,VERIFIED RII REQUIREMENT COMPLETED, IAW UPS GMM 04.02.01.15.SDR IPXA2026031770646Panel · corrodedAFT CARGO STA 1540 ON LH SIDE FLOOR ANCHOR POINT HAS CORROSION AROUND FASTENER. INSTALLED NEW REPAIR DOUBLER, NEW SIDE PANEL IAW B757-200PF, SRM 51-40-02.SDR IPXA2026031763179Support Channel · crackedLEFT MLG WW, TANG DOOR FWD CUTOUT, BRACKET SUPPORT AT LOWER SIDE HAS A CRACK. REMOVED DAMAGED BRACKET SUPPORT IAW SRM 51-40-02. INSTALLED PANEL 197DL, IAW AMM 53-36-02-404-006.SDR IPXA2026032854460Skin · corrodedAPU, RIGHT DOOR 316 EXTERNAL SKIN EDGE HAS EVIDENCE OF CORROSION AT APPROX BS 1963.8, VERIFIED EO NO DEFERRALS REQUIRED EA 757-5240-01-B0698, REV P1, STEP 16. ACCOMPLISHED REPAIR PER EO-96910-REQ1 AND VT-SAA EA 757-5240-01-B0698, REV IRSDR IPXA2026032658517Skin · damagedMAJOR REPAIR, TAIL EXTERNAL FUSELAGE, BTWN BS 1896.2 - 1992.8, 11 O'CLOCK POSITION, HAS 11EA POINTS WITH LIGHTNING STRIKE DAMAGE. BONDED REPAIR DOUBLER IAW SRM 51-70-10-2R-2A.SDR IPXA2026032458260Rivet · shearedMAJOR REPAIR. EXTERNAL LOWER FUSELAGE, BS 1460, S29R HAD A SHEAR RIVET, EVIDENCE OF CORROSION INSIDE. VERIFIED REPAIR ACCOMPLISHED PER EO-96803-REQ1 AND VT-MAE EA 757-5360-27-A4377 REV-, PRIOR TO FURTHER FLIGHT.SDR IPXA2026032153766Strap · corrodedMAJOR REPAIR, APU INLET DOOR CUTOUT AFT STRAP HAS EVIDENCE OF CORROSION INSTALLED ALL PARTS OF REPAIR: FILLER MIDDLE STRAP [3], FILLER SHEAR TIE [4], STRAP [2], STRAP [1] (DOUBLER METAL) I.A.W. B757-200 SRM 53-80-15-2R-1 AND SRM 51-40-02-0G-0SDR IPXA2026032054456Tee Fitting · corrodedLOWER FUSELAGE, STA 1040 T-CHORD RBL 6 TO RBL 25 HAS EVIDENCE OF CORROSION AND BARE METAL INSTALLED NEW T-CHORD ON, LOWER FUSELAGE, STA 1040, IAW B757-200PF, SRM 51-40-02.SDR IPXA2026032453721Strap · corrodedAPU INLET DOOR CUTOUT FWD STRAP HAS EVIDENCE OF CORROSION INSTALLED FWD STRAP IAW SRM 51-40-02-0G-0.SDR IPXA2026031653968Support Angle · corrodedAPU INLET DOOR CUTOUT LOWER CORNER ANGLE BRACKET HAS EVIDENCE OF CORROSION INSTALLED LOWER CORNER ANGLE I.A.W. B757-200 SRM 51-40-02-0G-0SDR IPXA2026031753310Support Angle · corrodedAPU INLET DOOR CUTOUT LOWER ANGLE SUPPORT HAS CORROSION INSTALLED 1EA NEW ANGLE IAW SRM 51-40-02-0G-0SDR IPXA2026031753605Support Angle · corrodedAPU INLET DOOR CUTOUT UPPER ANGLE SUPPORT HAS EVIDENCE OF CORROSION INSTALLED 1EA NEW UPPER ANGLE I.A.W. B757-200PF SRM 51-40-02-0G-0
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