Boeing 757-2G5
Service difficulty reports · 557
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 IXXA03092026CC01Beam · wornRIGHT MLG STRUT DOOR SUPPORT BEAM IS HEAVILY WORN ALONG THE EDGE JUST FWD OF DRAG STRUT.SDR IXXA03142026CC01Frame · corrodedRH AFT WING TO BODY FAIRING ATTACH FRAME AT STA 1220 IS CORRODED.SDR IXXA20262026003Door · gougedLEFT MLG DOOR GOUGED.SDR IXXA04082026CC01Angle · corrodedRH AFT LOWER WING TO BODY FAIRING FRAME STA 1050 IS CORRODED.SDR IXXA20262026002Support Bracket · corrodedLEFT LOWER WING - BODY FAIRING SUPPORT BRACKET STA 958 IS CORRODED.SDR IXXA20262026001Skin · corrodedFUSELAGE EXTERNAL SKIN IS CORRODED AT LAP SEAM S-20L BS 1718.SDR IXXA03062026CC01Skin · corrodedRIGHT WING LOWER SURFACE (INSPAR) IS CORRODED AROUND FASTENER AND RUNS UNDER PYLON RIGHT AT I/B SIDE OF PYLON APROX 5 INCHES AFT OF FWD SPAR AT STRINGER 14.SDR IXXA20250817045Reservoir · unserviceableFOUND L1 DOOR ACTUATOR EMERGENCY RESERVIOIR UNSERVICABLE. REMOVED AND REPLACED L1 DOOR ACTUATOR EMERGENCY RESERVOIR IN ACCORDANCE WITH BOEING 757 AIRCRAFT MAINTENANCE MANUAL 52-11-30.SDR FDEA202507151221Actuator · failedAFTER ROTATE THE AIRCRAFT BEGAN TO SHAKE IN THE RUDDER PEDALS THEN ENTERED INTO A SUSTAINED DUTCH ROLL THAT CONTINUED TO WORSEN AS WE ACCELERATED. EMERGENCY DECLARED. AMM: 22-00-02-2 AMM: 27-23-00-5 AMM: 22-21-00-5 PERFORMED MCDP TEST 30/40. RUDDER PCU SDR FDEA202507011087Idg · faultedIN FLIGHT L GEN OFF AND ASSOCIATED EICAS. L AC BUS OFF. RESET IN FLIGHT. OPERATED NORMALLY FOR 20 MINUTES. SAME MALFUNCTION AGAIN DURING DESCENT. EMERGENCY DECLARED. BITE CHECKED BPCU PER FIM 24-20 F/T 801. FOUND SAME MESSAGES AS PREVIOUS L GEN SYSTEM DSDR FDEA202412201823Gust Lock · wornL1 DOOR GUST LOCK COLLAR BROKEN. INSTALLED SERVICEABLE L1 DOOR LOCK COLLAR. DOOR LOCKS AND UNLOCKS NORMAL. MEL REMOVEDSDR FDEA202409041238Light · inoperativeL1 DOOR EMERGENCY EXIT LIGHT INOP. RELEASED FOR SERVICE PER MEL 33-51-01-01. ACFT OK FOR SERVICE.SDR IXXA20240818056Display · inoperativePRIOR TO ETOPS ENTRY POINT CREW REPORTED, BOTH FLIGHT MANAGEMENT COMPUTER DISPLAYS BLANK. ADDITIONALLY, AIR TRAFFIC CONTROL REPORTED NO ADS-B DATA RECEIVED. AIRCRAFT WAS IN IMC, ALTERNATIVELY, NO LIGHTING WAS SIGHTED. WITH COMPONENT FAULTS PRESENTING, FLIGHTSDR FDEA202407251050Tach Generator · failedAFTER TAKEOFF, RECEIVED L ENG BLEED OFF EICAS RAN QRH 2.1.14 LEVELED AT FL360. NOTICED CABIN ALT AT 8000 WHILE 5 MIN CABIN ALT AT 9500 DESCENDED DOWN TO LOWER ALT IN DESCENT RECEIVED CABIN ALT HIGH MASTER WARNING AND EICAS MSG. RAN QRC THEN QRH 2.1.1 CONTISDR IXXA20240611001Splice · corrodedLH WING, WING SIDE OF BODY SPLICE, UPPER SPLICE EVIDENCE OF CORRION BS 900 TO BS 940.SDR FDEA202406040767Floorbeam · corrodedMAIN CABIN COURIER AREA, STA 346 ALONG TOP SIDE HAS SEVERAL AREAS OF BARE METAL AND CORROSION ON PREVIOSLY BLENDED AREA OF BEAM. PREVIOUS BLEND OUT ON FLOOR BEAM UPPER CHORD AT MAIN CABIN STA 344-346 BETWEEN LBL 7 - LBL 21, AFTER EVALUATION FOUND OUT OF SDR FDEA202405010582Window · wornAT F.L. 330 R FWD WINDOW STARTED TO ARCH. WE RAN THE QRH, AND THEN ONE OF THE PANES SHATTERED. DECLARED AN EMERGENCY INTO BOISE. OFF MPN: 141T4801-50 POS: RH SRL: 15063H5303 ON MPN: 141T4801-50 CPN: 5610425 SRLSDR FDEA202404230275Collar · crackedR1 DOOR HOLD-OPEN LOCK(GUST LOCK) BROKEN. R1 DOOR HOLD-OPEN LOCK (GUST LOCK) WAS REMOVED AND REPLACED REF 757 AMM 52-11-08-8. OPS CHECK GOOD. A/C OK FOR CONTINUED SERVICE.SDR FDEA202404230274Collar · crackedL1 DOOR HOLD-OPEN LOC(GUST LOCK) BROKEN. L1 DOOR HOLD-OPEN LOCK (GUST LOCK) WAS REMOVED AND REPLACED REF 757 AMM 52-11-08-8. OPS CHECK GOOD. A/C OK FOR CONTINUED SERVICE. L1 DOOR HOLD-OPEN LOCK (GUST LOCK) WAS REMOVED AND REPLACED REF AMM 52-11-08-8. OSDR IXXA2024032301Tee Fitting · corrodedCORROSION ON NOSE LANDING GEAR WHEEL WELL RIGHT HAND T-CHORD.SDR IXXA20231130086Unknown · unknownMULTIPLE TIMES DURING FLIGHT, R EMER DOOR EICAS MESSAGE DISPLAYED. FLIGHT CONTINUED UNAFFECTED. NO ADDITIONAL FAULTS NOTED. IAW B757 FAULT ISOLATION MANUAL 52-71-FAULT TREE 805, CLEARED DEBRIS AND VERIFIED SECURITY AND INTEGRITY OF DOOR SILL AREA. DOOR FOUNDSDR IXXA20231019072Battery · inoperativePOST FLIGHT LINE MAINTENANCE IDENTIFIED, L4 DOOR EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED L4 EMERGENCY FLASHLIGHT BATTERY PER B757 AMM 25-64-00. OPERATIONAL CHECK GOOD.SDR IXXA20230908055Unknown · unknownPOST FLIGHT LINE MAINTENANCE REPORTED, R4 EMERGENCY FLASHLIGHT INOPERTIVE. REMOVED AND REPLACED EMERGENCY FLASH LIGHT BATTERY IAW 757 AMM 25-64-00. OPERATIONAL CHECK GOOD.SDR FDEA202301170123Floorboard · delaminatedCOURIER AREA FLOORBOARD 221 MBF IS DELAMINATED. FABRICATED COURIER FLOORBOARD 221 MBF ON VTMAE TRAVELER # T23/1654447 IAW DWG # SRZ-25-005 REVISION R. MAJOR REPAIRSDR 2022F00491Structure · corrodedRIGHT OB LOWER MAIN AFT FLAP CORROSION ON LOWER SURFACESDR 2022F00490Structure · corrodedRIGHT OB LOWER MAIN AFT FLAP CORROSION ON LOWER SURFACE.SDR IXXA2022111602Fitting · damagedUPON REMOVAL OF # 2 PYLON INBOARD BATHTUB FITTING FOUND TO BE DAMAGED.SDR IXXA2022111601Channel · worn# 2 PYLON ANGLE CHANNEL COVER WORN SEVERAL AREAS.SDR IXXA2022111200001Doubler · corrodedRIGHT WHEEL WELL FS 1148 UPPER PRESSURE DECK RBL 3 CORROSION ON DOUBLER AROUND HYDRAULIC FITTING.SDR IXXA2022111100001Keeper · corrodedLEFT WHEEL WELL FS 1060 10 INCHS OUTBOARD OF KEEL WEB TOP SIDE OF WHEEL WELL HYDRAULIC LINE ISOLATOR GROMMET KEEPER CORRODED HARDWARE AND CORROSION ON ANCHORING ANGLE.SDR IXXA2022110900006Skin · corrodedLEFT WING LOWER SURFACE CORROSION AROUND FUEL STICK 7 PANEL STATION 606.SDR IXXA2022110900005Skin · corrodedCORROSION ON UPPER SURFACE LEFT WING ABOVE PYLON AREA 3 SPOTS.SDR IXXA2022110900004Skin · corrodedTHREE AREAS OF CORROSION ON EXTERNAL LOWER SURFACE OF LEFT WING SKIN ON STRINGER L6 AT WS 150.50 TO 177.50.SDR IXXA2022110900002Bracket · corrodedRIGHT WING TRAILING EDGE SUPPORT BRACKET ATTACHING TO FUSELAGE FOR PANEL HAS CORROSION BL. 70.50 STATION 1158.SDR IXXA2022110900001Web · corrodedRIGHT WHEEL WELL RBL 0 STATION 1096 HAS CORROSION ON INTER VERTICAL WEB AT MULTIPLE LOCATIONS.SDR IXXA2022110800008Skin · corroded#2 PYLON ACCESS THRU PANEL 443HL LOWER FORWARD CORNER STRUCTURE INTERNALLY HAS CORROSION.SDR IXXA2022110800007Skin · corrodedRIGHT WING SKIN LOWER SURFACE IS CORRODED AT WS 742.SDR IXXA2022110800006Skin · corrodedRIGHT WING SKIN LOWER SURFACE CORRODED AT WS 663 REAR SPAR.SDR IXXA2022110800004Stringer · corrodedAFT LOWER CARGO COMPARTMENT STA 1412 BELLY OF FRAME APPROX 29L STRINGER END HAS BAD CORROSION ON EAR OF STRINGER.SDR IXXA2022110800003Skin · corrodedPREVIOUS REPAIR ON LEFT WING UPPER SKIN AT WS 150.5 THRU WS 204.5 NEEDS REACCOMPLISHED PER AMES REA 47508REA41 AND FVCI ENGINEERING ORDER 22082-22 REV C.SDR IXXA2022110800002Skin · corrodedCORROSION ON EXTERNAL SIDE OFM LEFT WING LOWER SKIN AT WS 21.00 AND AFT FUEL PANEL 531CB CUTOUT.SDR IXXA2022110800001Skin · corrodedNUMBER 2 PYLON THRU ACCESS PANEL 443AR INTERNAL SKIN LWR SECTION AROUND OPENING HAS CORROSION.SDR FDEA202211042728Pan · gougedR1 DOOR EXTERIOR HANDLE PAN WORN REMOVED AND REPLACED R1 DOOR HANDLE PAN IAW DWG 141N6200 REV T AND AMM 52-11-13-02.SDR FDEA202211032725Wedge · delaminated#6 SLAT T/E WEDGE IS DISBONDED REMOVED AND REPLACED PER B757 AMM 81-01-4SDR FDEA202211032724Wedge · delaminated#4 SLAT T/E WEDGE IS DISBONDED REMOVED AND REPLACED PER B757 AMM 27-81-02-4SDR FDEA202211032723Wedge · delaminated#3 SLAT T/E WEDGE IS DISBONDED REMOVED AND REPLACED PER B757 AMM 27-81-02-4SDR FDEA202211032722Wedge · delaminated#5 SLAT T/E WEDGE IS DISBONDED REMOVED AND REPLACED PER B757 AMM 27-81-01-4SDR FDEA202211022713Floorbeam · corrodedMAIN CABIN FLOOR BEAM STA 1681 IS CORRODED ON THE AFT FACE AND LOWER SURFACE OF THE UPPER CAP AT APPROX RBL 48 ACCOMPLISHED FEDEX EA # F-5310-T0371106 FUSELAGE - MAINFRAME - FLOOR BEAM, STA 1681, LBL 23, LBL 5, RBL 48, CORRODED DAMAGE. ORIG SUBMISSION DATESDR FDEA202211022714Floorbeam · corrodedMAIN CABIN FLOOR BEAM IS CORRODED AT FASTENER HOLE BS 310 LBL 20 ACCOMPLISHED FEDEX EA # F-5310-T0371036 FUSELAGE - MAINFRAME - FLOOR BEAM TEE CAP, STA 310, LBL 20, CORROSION REPAIRSDR FDEA202211022712Panel · cracked#1 PYLON PANEL 434DR HAS A CORNER CRACKED REPAIRED #1 PYLON PANEL 434DR CRACKED CORNER WITH 350 DEGREE REPAIR IAW B757 SRM 54-50-70-2R FIG 201 REPAIR 1 SHEET 3, 51-40-02,51-70-04,54-50-70-0IAND AMM 51-24-02-7, 51-21-00/701, B757NDTM PART 1 51-01-01.
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