Boeing 757-2G5
Service difficulty reports · 556
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 = '7572G5' 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 = '7572G5' 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 FDEA202610121559Skin · corrodedLEFT WING INBD FLAP UPPER SURFACE O/B SIDE EXTERNAL SKIN SOME AREA WITH CORROSION. LT WING I/B FLAP UPPER SURFACE O/B SIDE WAS REPAIRED IAW B757 SRM 57-53-01-2R REPAIR 1 FIGURE 201 DETAIL I (SHEET 2) AND SRM 51-70-10-2RSDR FDEA202610091536Floorbeam · corrodedMAIN CARGO COMPARTMENT FLOORBEAM BS 1200 BETWEEN 24LBL TO 0BL SOME AREAS WITH CORROSION. AREA OUT OF LIMITS WAS REPAIRED AT MAIN CARGO COMPARTMENT FLOORBEAM BS 1200 BETWEEN 26LBL TO 13LBL IAW SRM 53-00-51-2R, REPAIR.1.SDR FDEA202610051478Skin · delaminatedTWO INDICATIONS OF DISBOND WERE FOUND OVER TWO DENTS ON THE UPPER SKIN OF THE LEFT ELEVATOR: ONE AT ELEV STA 107.360, 1.800 INCHES IN DIAMETER AND 13.5 INCHES FROM THE TRAILING EDGE; AND THE OTHER AT ELEV STA 109.430,1.300 INCHES IN DIAMETER AND 14.5 INCSDR FDEA202607220987Fitting · crackedCRACK FOUND ON #2 ENGINE LOWER OUTBD MIDSPAR BULKHEAD FITTING. REPAIRED OUTBD MIDSPAR BULKHEAD FITTNG IAW EA F-5450-T0387823 PT1, NACELLS / PYLON - WING PYLON / STRUT - #2 PYLON - PP STA 174.30 MID BULKHEAD - RH FITTING CRACKED AT LOWER VERTICAL FLANGE. MSDR FDEA202607030828Door · unsecureCOULD NOT GET R1 DOOR SLIDE LIGHT TO ILLUMINATE WHEN CLOSING DOOR. WHILE APPROACHING AIRCRAFT NOTED R1 DOOR NOT COMPLETELY CLOSED. CYCLED DOOR AND ARMED SLIDE, OPS CHECK NORMAL PER AMM 52-11-00-0.SDR IXXA20260501001Skin · corrodedCORROSION ON THE LOWER SURFACE OF THE RIGHT WING LOWER SKINSDR IXXA20260424001Bracket · corrodedLEFT WHEEL WELL ON THE H BEAM IS A HYDRAULIC LINE B NUT THATS SITTING RIGHT IN FRONT OF THE CUSHION CLAMP AND BRACKET, AND THE BRACKET IS CORRODED.SDR IXXA202604080002Support Fitting · corrodedCORROSION AROUND SUPPORT FITTING FASTENER AT STA 1180 RBL 28SDR IXXA2026040600001Support Angle · corrodedCORROSION ON SUPPORT ANGLE IN LWW FOR STRUT DOOR CUTOUTSDR IXXA20260403002Pad · gougedWHILE SERVICING MAIN LANDING GEAR STRUTS, THE AIRCRAFT TILTED TO THE LEFT CAUSING LEFT MAIN GEAR JACK TO COME INTO CONTACT LOWER WING AT JACKING PAD.SDR IXXA20260403001Pad · gougedWHILE DRILLING OUT FASTENER IN THE LEFT-WING JACK PAD DOUBLER, THE DRILL CONTACTED THE OUTER PERIMETER OF HOLE IN THE WING SKINSDR IXXA20260329002Keelbeam · corrodedCORROSION AT THE HYD TUBING PASS THRU AT THE KEEL WALL IN THE LWW BS 1171-1180.SDR IXXA20260329001Support Beam · corrodedLEFT WING UPPER FIXED WING SKIN PANEL SUPPORT BEAM CORRODED IN SEVERAL PLACESSDR IXXA20260316001Bracket · corrodedLEFT WING T/E INBD. OF DEFUEL VALVE HAS CABLE GUIDE BRACKET CORRODEDSDR IXXA20260315002Retainer · brokenSEAL RETAINER SUPPORT STRUCTURE BROKEN IN RWW MLG DOOR CUTOUTSDR IXXA20260315001Skin · corrodedFOUND SKIN CORROSION COMMON TO RT FILLET PANEL @ STA 793, 805, 825 ALL ON SKIN PANEL 143N3561-4SDR IXXA04062026CC01Bracket · crackedNR 1 ENGINE COMPRESSOR BOOST FRAME FLANGE BRACKET BENT AND CRACKED AT THE ENGINE 11 O'CLOCK POSITION.SDR IXXA2026031301Skin Panel · damagedREPAIRED CORRODED LEFT WING REAR SPAR UPPER PANEL SUPPORT LIP AND SKIN.SDR IXXA20260311001Skin · corrodedFUSELAGE SKIN IS CORRODED AT LOWER FWD WING TO BODY ATTACHMENT. STA 740-781, S18L- 18R. OTHER PN +143N3521-9,143N359-1/2SDR IXXA20260310001Skin · corrodedFUSEELAGE LEFT SIDE STA 785-855 LEVEL 2 CORROSION2 BODY TO WING PANELSSDR IXXA20260304001Skin Panel · corrodedRIGHT FUSELAGE CLOSEOUT FAIRING PANEL AFT OF MAIN CARGO DOOR FOUND CORROSION AT UPPER AND LOWER DOOR CORNERS NO PART NUMBERS FOUND ON REMOVE PANEL. FABRICATED NEW CLOSEOUT FAIRING PANEL, ASSIGNED NEW P/N 47696FAB01SDR IXXA20260302001Support Bracket · brokenNR 1 ENGINE REMOVED AND REPAIRED HP2 VALVE CASE BRACKET DUE TO BROKEN SUPPORT BRACKET NR 187303-0400-0178, AND AMES 47170REA622SDR IXXA20260223001Support Bracket · corrodedREAR SPAR HYD BLOCK CLAMP SUPPORT BRACKET CORRODED.PN 271N6114-22SDR IXXA20260222002Pressure Deck · corrodedRIGHT WHEEL WELL PRESSURE DECK CORRODED STA1160 RBL3 P/N 144N8142-10SDR IXXA20260222001Support Web · corrodedLW FUEL BOOST PUMP CUTOUT CORROSION IRSS 183SDR IXXA2026021901Bracket · corrodedLEADING EDGE JUST ABOVE PYLON HAS CORROSION AROUND NUT PLATESDR IXXA20260218001Bracket · corrodedLEFT LANDING GEAR ELECTICAL CONNECTOR BRACKET CORRODEDSDR IXXA2026020702Door · gougedRIGHT MLG DOOR IS GOUGED NEAR NO STEP PLACARD.SDR IXXA2026020701Web · corrodedREAR SPAR FUEL BOOST PUMP CUTOUT TO BE CORRRODEDSDR IXXA2026020605Skin · corrodedCORROSION ON THE UPPER EXTERIOR SURFACE OF THE RIGHT WING UPPER SKIN, LOCATED FWD OF THE RIGHT AILERON.SDR FDEA202602060138Bulb · failedFOUND L1 OVERHEAD EMERGENCY LIGHT DIM DURING MX PRE-FLIGHT CHECK. AMM: 33-51-01-2 REMOVED AND REPLACED 11 FAULTY BULBS AT THE L1 EMERGENCY EXIT SIGN AS PER ABOVE REF. OPS CHECK GOOD.SDR IXXA2026020603Skin · corrodedFOUND AREA OF LW LOWER SKIN CORRODED JUST O/B OF BBL 70.50, JUST FWD OF STR L-10 ON THE EXTERNAL SURFACESDR IXXA2026020602Support · corrodedCORROSION ON PANEL SUPPORT ATTACHED TO THE AFT WALL IN THE LWW, FROM LBL7 TO LBL34SDR IXXA2026020601Skin · damagedDURING REPAIR ON NR 187303-0100-0192 IT WAS DISCOVERED THAT THERE IS A SCRIBE JUST FWD OF THE REPAIR AREA AT STA 740 STR 19L COMMON TO THE SKIN LAP.SDR IXXA20260205002Stop Fitting · damagedL1 FWD DOOR STOP FITTING DAMAGE WAS REMOVED BY BLEND. THIS DAMAGE EXCEEDS ALLOWABLE LIMITS.SDR IXXA2026020404Bracket · corrodedLEFT WING T/E FRONT SECTION OF LANDING GEAR SUPPORT BEAM HAS CORRODED PANEL SUPPORT BRACKETSDR IXXA2026020403Bracket · corrodedLOWER FUSELAGE WING TO BODY PANEL SUPPORT BRACKET HAS CORROSION AT WIRING CLAMP HOOKUP BETWEEN LEFT WHEEL WELL AND GEARSDR IXXA20260111002Bracket · corrodedEDIT (NEW CONTROL NUMBER) FROM DUPLIACATE CONTROL NUMBER IXXA20260111001 - FOUND CORROSION ON THE BLOCK SUPPORT TUBING IN THE OUTBOARD UPPER AREA OF THE LEFT WHEEL WELL OUTBOARD OF THE ANTISKID VALVES.SDR IXX2026F00000Bracket · corrodedFOUND CORROSION ON THE BLOCK SUPPORT TUBING IN THE OUTBOARD UPPER AREA OF THE LEFT WHEEL WELL OUTBOARD OF THE ANTISKID VALVES.SDR IXXA20260205001Bearing · galledGALLING, LIGHT CORROSION AND GOUGE AROUND BEARING FACESDR IXXA20260112002Support Beam · corrodedRMLG STRUT DOOR SUPPORT BEAM IS CORRODED IN MULTIPLE AREASSDR FDEA202601060010Bulb · failedDURING MX PRE-FLIGHT, FOUND R1 EMERGENCY EXIT SIGN DIM. AMM: 33-51-01-2 FOUND R1 EMERGENCY EXIT SIGN HAS 9 BULBS OUT. REMOVED AND REPLACED 9 FAULTY BULBS AS PER ABOVE REF. PART NUMBER 0L3071BPEGPL. OPS CHECK GOOD. A/C OK FOR SERVICE.SDR FDEA202601060009Bulb · failedDURING MX PRE-FLIGHT, FOUND L1 EMERGENCY EXIT SIGN DIM. AMM 33-51-01-2 FOUND L1 EMERGENCY EXIT SIGN HAS 7 BULBS OUT. REMOVED AND REPLACED 7 FAULTY BULBS AS PER ABOVE OPS CHECK GOOD. A/C OK FOR SERVICE.SDR IXXA20260112001Channel · corrodedCORROSION ON THE INSIDE OF THE U CHANNEL THAT SUPPORTS THE HYD ISOLATION VALVE, LOCATED ON THE BACK WALL IN THE LEFT WHEEL WELL STA 1180SDR IXXA20251222001Skin · corroded.CORROSION OF THE UPPER EXTERIOR SURFACE OFTHE RIGHT WING UPPER SKIN FWD OF THE AILERONSDR IXXA04022026CC01Fitting · deformedREMOVED FOR ACCESS THE RW SIDE LINK ATTACH FITTING "MICKEY MOUSE FITTING" FOR SIDE LOAD FITTING ALIGHNMENT. DURING REMOVAL FOUND DAMAGED FREEZE PLUG/BUSHING IN HOLE.SDR IXXA20260111001Support Channel · corrodedRH AFT LOWER WING TO BODY FAIRING FRAME BS 1037 IS CORRODEDSDR IXXA121820250001Rub Block · crackedRIGHT WING INBD FLAP T/E FAIRING 671BB HAD A CRACKED RUB BLOCK AT FAIRING AFT ATTACH ARM.SDR IXXA03292026CC01Support · corrodedLEFT WING UNDER PANEL 551 AT SEVERAL AREA AROUND NUTPLATES ARE CORRODED.SDR IXXA03092026CC01Beam · wornRIGHT MLG STRUT DOOR SUPPORT BEAM IS HEAVILY WORN ALONG THE EDGE JUST FWD OF DRAG STRUT.
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