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 IPXA2023093077320Skin · dented*** MAJOR REPAIR *** FAULT-THREE DENT-OUT ON MAIN CARGO DOOR SKIN AT UPPER-AFT SIDE; DOT 117-010. REINSTALLED MAIN CARGO DOOR AFT LIFT PANEL TO FOM IAW SRM 52-30-01-2R-4, SHEET 1. SUPPLEMENTAL INSPECTION REQUIREMENTS DEFERRED IAW B757-200PF REV. 117.00, SRM CHSDR IPXA2023092874848Seat Track · corroded*** SUPPLEMENTAL SDR *** FAULT-MAIN CARGO COMPARTMENT STA 340 TO STA 440 LBL 45.5 SEAT TRACK SPOTS WITH CORROSION. DOT 68-76 REMOVE AND REPLACE LBL 45.50 SEAT TRACK (PN: 141N5131-46) BETWEEN STA 324 AND STA 440 PER BOEING DRAWING 141N5131 AND SRM 51-40-02SDR IPXA2023091974848Unknown · unknownFAULT-MAIN CARGO COMPARTMENT STA 340 TO STA 440 LBL 45.5 SEAT TRACK SPOTS WITH CORROSION. DOT 68-76 GIVEN THE OK TO INSTALL FITTING STA 345 TO 333 LBL 45.50. OPENSDR IPXA2023100466790Crease Beam · corrodedFAULT-MAIN CABIN UPPER FLIGHT DECK STA 320 TO STA 340 LBL 62.225 SEVERAL CORROSION. DOT 68-68 ACCOMPLISHED WORK PER UPS EO 88246-REQ 1 AND VT MAE EA 757-5310-27-A3378-REV.SDR IPXA2023090640446Probe · unknownAT 300€™ EICAS MSG TAT FOLLOWED BY AUTO THROTTLE MSG. RAN QRH, DID AIR TURN BACK. ONCE ON GROUND, TAT EICAS MSG WENT AWAY. R AND R€™D TOTAL AIR TEMP PROBE PER MM 32-12-02-401. OPS CHECKS GOOD.SDR IPXA202309050446Unknown · unknown*** ATB *** *** SDR FILED OPEN *** AT 300€™ EICAS MSG TAT FOLLOWED BY AUTO THROTTLE MSG. RAN QRH, DID AIR TURN BACK. ONCE ON GROUND, TAT EICAS MSG WENT AWAY. R AND R€™D TOTAL AIR TEMP PROBE PER MM 32-12-02-401. OPS CHECKS GOOD.SDR IPXA2023092836764Floorbeam · corrodedFAULT-MAIN CABIN SHEAR WEB STA 1680 TO STA 1720 BL 0 TO LBL 24.75 SPOTS WITH CORROSION AS MARKED. DOT 68-49 REVIEWEDSDR IPXA2023090520554Control Panel · inoperativeWEATHER RADAR PANEL REMOVED AND INSTALLED WX RADAR CONTROL PANEL IAW AMM 34-43-02. OPS CHECK GOOD.SDR IPXA2023100413250Frame · noneFAULT: EXISTING FRAME REPAIR FOUND AT AFT CARGO COMPARTMENT STA 1360 R/H STR 26 ACCOMPLISHED WORK PER UPS EO 87164-REQ 1 AND VT MAE EA 757-5360-27-A3349 REV-SDR IPXA2023092691136Tee Fitting · corrodedFAULT: R/H WING TO BODY, T-CHORD STA 1200, AT RBL 63, FOUND EXFOLIATE CORROSION INSTALLED NEW T-CHORD STA 1200, AT RBL 63 IAW B757 SRM 51-40-02-0G REVIEWED.SDR IPXA2023092699104Tee Fitting · corrodedFAULT: THE T-CHORD FOR THE RAT DOOR HINGES, STA. 1180 - STA. 1240, RBL 58 HAS EXFOLIATING CORROSION. INSTALLED RAT DOOR IAW AMM 29-21-09-424-008. REVIEWED.SDR IPXA2023092691224Tee Fitting · corrodedFAULT: R/H WING TO BODY, T-CHORD STA 1220, AT RBL 63, FOUND EXFOLIATED CORROSION. INSTALLED OUTER CHORD AT STA 1220 RBL 63 AND NUT PLATES IAW SRM 51-40-02-0G. REVIEWED.SDR IPXA2023092688659Tee Fitting · corrodedFAULT: R/H, AFT WING TO BODY, T-CHORD, RBL 63, BETWEEN STA 1180 TO STA 1240 FOUND EXFOLIATED CORROSION. INSTALLED NEW T-CHORD I.A.W. SRM 51-40-02-0G. REVIEWED.SDR IPXA2023092588707Unknown · corrodedFAULT: R/H WING TO BODY, T-CHORD, AT STA 1180, RBL 35 FOUND NUT PLATE HOLE, EXFOLIATED CORROSION. INSTALLED NEW T-CHORD AT STA 1180, RBL 35, IAW B757 SRM 51-40-02. REVIEWED.SDR IPXA2023092588988Unknown · corroded*** SUPPLEMENTAL SDR *** FAULT: FWD, WING TO BODY T-CHORD STA 900 BETWEEN RBL 48 TO LBL 34, FOUND EXFOLIATED CORROSION AND CHAFFING, MARKED ON RED INSTALLED T-CHORD AND SPLICE PLATES I.A.W. B757-200 S.R.M. 51-40-02. REVIEWED.SDR IPXA2023091488707Unknown · corroded**SDR FILED OPEN**FAULT: R/H WING TO BODY, T-CHORD, AT STA 1180, RBL 35 FOUND NUT PLATE HOLE, EXFOLIATED CORROSION. SDR AND CPCP SUBTASKS COMPLETED.SDR IPXA2023091888988Unknown · corroded**SDR FILED OPEN**FAULT: FWD, WING TO BODY T-CHORD STA 900 BETWEEN RBL 48 TO LBL 34, FOUND EXFOLIATED CORROSION AND CHAFFING, MARKED ON RED REVIEWED.SDR IPXA2023092872753Transition Panel · corroded*** SUPPLEMENTAL SDR *** FAULT: AFT CARO PIT, SURFACE CORROSION ON R/H TRANSITION PANEL FROM FRS 1180 TO FRS 1310. INSTALLED TIE DOWN AND SPLICE DOUBLERS IAW B757 SRM 51-40-02-0G REVIEWED.SDR IPXA2023092674043Angle · corrodedFAULT - WTB UNDER PANEL 193FL FWD "Z" ANGLE STRUCTURE WITH EXFOLIATION INSIDE NUTPALTE MARKED IN RED INSTALLED "Z" ANGLE I.A.W SRM 51-40-02 REVIEWED.SDR IPXA2023092174790Angle · corroded*** SUPPLEMENTAL SDR *** FAULT - WTB UNDER PANEL 191CL AFT STRUCTURE WITH CORROSION MARKED IN RED APPLIED CIC ON THE REPAIR AREA IAW B757 AMM 51-24-03-377-008. ACCOMPLISHED REPAIR IAW EO-88197-REQ1 AND VT MAE EA 757-5340-27-A3367 REV-. REVIEWED.SDR IPXA2023092674265Tee Fitting · corrodedFAULT - WTB UNDER PANEL 195CL DOWN INSIDE STRUCTURE WITH CORROSION ARROUND TWO NUTPLATES MARKED IN RED INSTALLED T-CHORD AT STA 1220 BETWEEN LBL63 AND LBL84, IAW B757 SRM 51-40-02-0G. REVIEWED.SDR IPXA2023092673683Bracket · corrodedFAULT - KEEL BEAM AREA UNDER PANEL 139CL STRUCTURE AFT WITH CORROSION MARKED IN RED INSTALLED NEW SUPPORT ANGLE IAW SRM 51-40-02. REVIEWED.SDR IPXA2023092074790Angle · unknown**SDR FILED OPEN**FAULT - WTB UNDER PANEL 191CL AFT STRUCTURE WITH CORROSION MARKED IN RED IN REFERRENCE TO STEP 21: VERIFIED PERFORMED DVI IAW B757 SRM 51-10-08, VERIFIED NO ADDITIONAL DAMAGE FOUNDSDR IPXA2023091871606Unknown · unknown**SDR FILED OPEN**FAULT RT WING L/E BETWEEN SLAT#9 AND SLAT#10 HAS CRACK SHOWING COMPOSITE DOT #47-06 VERIFIED TOPCOAT.SDR IPXA2023091872753Unknown · unknown**SDR FILED OPEN**FAULT: AFT CARO PIT, SURFACE CORROSION ON R/H TRANSITION PANEL FROM FRS 1180 TO FRS 1310. CPCP AND SDR INFO RECORDED.SDR IPXA2023082964367Unknown · unknown**SDR FILED OPEN**EMERGENCY LIGHTS WILL NOT ILLUMINATE WITH SWITCH IN ON POSITION. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-07-902-001. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.SDR IPXA2023092663271Panel · corrodedFAULT: AFT CARGO COMPT, R/H SIDE PANEL, BETWEEN STA 1380 TO STA 1440, FOUND EXFOLIATED CORROSION, OUT OF LIMITS. INSTALLED NEW SIDE PANEL IAW SRM 51-40-02. REVIEWED.SDR IPXA2023090659216Light · inoperative*** SUPPLEMENTAL SDR *** INTERIOR EMERGENCY LIGHTS INOP R&R'D BATTERY AND CHARGER IAW AMM 33-51-07. OPS CHK GOOD. PLACARD REMOVED.SDR IPXA2023082859216Unknown · unknownINTERIOR EMERGENCY LIGHTS INOP DERFERRAL MEL 33-51-1-1. PLACARD INSTALLEDSDR IPXA2023091848102Frame · unknownMAJOR REPAIR FAULT: AFT CARGO RH FRAME STA 1280 HAS A PREVIOUS REPAIR AT STR 25R ACCOMPLISHED REPAIR IAW EO-88073-REQ 1 AND VT-MAE EA 757-5360-27-A3342, REV.SDR IPXA2023091048144Unknown · unknown*SDR FILED OPEN* *MAJOR REPAIR* FAULT: 1 EA DENT FOUND ON LH FRAME STA 800 AT STR 26L REF STEP 31. OUT FOF SEQUENCE. INSPECTED AND VERIFIED SHEAR TIE AND STRINGER IS INSTALLED. JOB COMPLETED. INSPECTION COMPLETED.SDR IPXA2023090848136Frame · dented*** MAJOR REPAIR *** FAULT: 2 EA. DENT FOUND ON LH FRAME STA 1500 AT STR 26L VERIFIED INSTALLATION OF 3 (EA) STRINGER CLIP AT STA 1500 BETWEEN STR 24 L/H, 25 L/H, AND 26 L/H I.A.W. SRM 53-00-07-2R-5 DETAL LLL. JOB COMPLETESDR IPXA2023092640796Unknown · gougedMAJOR REPAIR FAULT-LEFT HORIZONTAL STABILIZER GOUGE AT LEADING EDGE. DOT119-009 ACCOMPLISH REPAIR PER EO 88121-REQ1 AND VT-MAE EA 757-5510-27-A3353, REV. -. REVIEWEDSDR IPXA2023091840796Unknown · unknown**SDR FILED OPEN**FAULT-LEFT HORIZONTAL STABILIZER GOUGE AT LEADING EDGE. DOT119-009 ACCOMPLISH REPAIR PER EO 88121-REQ1 AND VT-MAE EA 757-5510-27-A3353, REV. -.SDR IPXA2023092421339Panel · corroded*** SUPPLEMENTAL SDR *** FAULT: REMOVE THE #2 R/H TRANSITION PANEL TO FOM FOR SUSPECTED CORROSION BELOW PANEL AT STA 1380 INSTALLED NEW TRANSITION PANEL IAW SRM 51-40-02. REVIEWED.SDR IPXA2023090612540Unknown · unknown*** SUPPLEMENTAL SDR *** LH WING WILL NOT TAKE FUEL. **OII 2** CLEANED CANNON PLUG L/H FUEL SHUTOFF VALVE AND OPS CHECK IAW AMM 28-21-02. OPS CHECK GOOD. PLACARD REMOVED. THIS CLEARS DEFERRAL.SDR IPXA2023082412540Unknown · unknown*** SDR FILED OPEN *** LH WING WILL NOT TAKE FUEL. **OII 2** DEFFERED LH WING FUEL SHUTOFF VALVE PER MEL 28-21-1-1. DMP COMPLIED WITH PLACARD INSTALLED.SDR IPXA2023090693849Skin · crackedLEFT WING FIXED LEADING EDGE HAS CRACK BEHIND SLAT#4 OUTBOARD END REPAIR ACCOMPLISHED ON FAULT: T3F18E002792J. INSTALLED REPAIR PARTS I.A.W. B757-200 S.R.M. 51-40-02-OG REVIEWED T3F18E002792J.SDR IPXA2023090377830Shear Tie · dented*** MAJOR REPAIR *** FAULT: AFT CARGO PIT STA 1500 AND STR 26 LH - STR 25 LH FRAME HAS A DENT. INSTALLED STRINGER CLIP (2E/A) AT AFT CARGO PIT STA 1500 IAW SRM 53-00-07-2R-5. VERIFIED FINAL INSTALLATION OF FRAME REPAIR.JOB COMPLETESDR IPXA2023090298791Shear Tie · dented*** MAJOR REPAIR *** FAULT: AFT CARGO COMPT, FRAME, STA 1580 R/H, AT S-26R HAS A DENT. ACCOMPLISHED REINFORCING ANGLE REPAIR IAW PER 757-200PF SRM REV 117.00 CHAPTER 53-00-07-2R-5, DETAIL I PER SRM 53-60-07-2R. VERIFIED FINAL INSTALLATION OF FRAME REPAIR.JOBSDR IPXA2023083177842Shear Tie · dentedAFT CARGO PIT STA 1500 AND STR 26 RH FRAME HAS A DENT. ACCOMPLISHED REINFORCING ANGLE REPAIR IAW PER 757-200PF SRM REV 117.00 CHAPTER 53-00-07-2R-5, DETAIL I PER SRM 53-60-07-2R. VERIFIED FINAL INSTALLATION OF FRAME REPAIR. JOB COMPLETESDR IPXA2023083177808Frame · dentedAFT CARGO PIT STA 1480 AND STR 26 LH FRAME HAS A DENT VERIFIED FINAL INSTALLATION OF FRAME REPAIR.JOB COMPLETE. IAW B757-200PF REV 117.00 SRM 53-00-07-2R-5, TABLE #3, FOR ZONE #1. MAJOR REPAIR.SDR IPXA202308230001Unknown · unknown*** SDR FILED OPEN *** FAULT: LEFT WING FIXED LEADING EDGE HAS CRACK BEHIND SLAT#4 OUTBOARD ENDSDR IPXA2023090760281Stringer · corrodedMAJOR REPAIR. LOWER FUSELAGE SKIN AT STA.1440, STRINGER 29L HAS A BULDGE BETWEEN STRINGER ATTACH RIVETS. DOT 8-001. APPLIED CIC AT NEW STRINGER I.A.W. AMM 51-00-59. VERIFIED ALL WORK COMPLETE.SDR IPXA2023090660307Shear Tie · corrodedFAULT- AFT FUSELAGE SKIN BETWEEN STA. 1680-1700, S-27L HAS BULDGING BETWEEN TWO STRINGER RIVETS. DOT 8-002. VERIFIED JOB COMPLETE.SDR IPXA2023081951407Unknown · unknownAFT FUSELAGE WHERE MEETS APU EXHAUST HAS CORROSION AND CRACK.***SM100/LMX TO EVAL*** ++ACCOMPLISHED PART REPLACEMENT AS PER SRM 51-40-02 DWG 148N3750SDR IPXA2023081724432Life Raft · unknown01 LIFE RAFT HAS ARMED PIN PULLED OUT. R & R'D LWR LIFE RAFT IAW MM 25-64-00-201.SDR IPXA2023081710329Light · inoperativeEMER EXIT LIGHTS INOP REMOVED & REPLACED EMERGENCY EXIT LIGHT POWER SUPPLY W/REF TO M/M 33-51-07-862-054, OPS CHECK GOODSDR IPXA2023082295116Slat · warning messageLE SLAT DISAGREE EICAS MSG ON DEPARTURE PASSING 3000 MSL. INDICATOR LIGHT AND INDICATED > UP BUT LESS THAN 5. MSG AND LIGHT DID NOT CLEAR. CHECKLIST DIRECTED LE SLAT ASYMMETRY LANDING. REMOVED AND REPLACED LE PDU REF BARCODE T3F18E00291H0 FOR MX ACTIONSSDR IPXA20230815116Unknown · unknown**SDR FILED OPEN** **ATB**LE SLAT DISAGREE EICAS MSG ON DEPARTURE PASSING 3000 MSL. INDICATOR LIGHT AND INDICATED > UP BUT LESS THAN 5. MSG AND LIGHT DID NOT CLEAR. CHECKLIST DIRECTED LE SLAT ASYMMETRY LANDING.
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