Boeing 757-230
Service difficulty reports · 608
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 = '757230' 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 = '757230' 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 FDEA202107131766Rib · crackedL/W L/E RIB FSS 213 IS CRACKED REPAIRED PER FEDEX EA # F-5720-T0362818-P1SDR FDEA202107121753Plate · crackedR/W T/E REAR SPAR WIGGLE PLATE IS CRACKED BENEATH #8 SPOILER REMOVED AND REPLACED PER BOEING DWG #113N1630 REV BSDR FDEA202107121752Attach Angle · crackedR/W L/E STRUCTURE FSS 560 ATTACH ANGLE IS CRACKED REMOVED AND REPLACED ANGLE PER DWG #114N2034 REV CSDR FDEA202107111724Panel · crackedLEFT WING, OUTBOARD AILERON, PCU HINGE PANEL IS CRACKED AT OUTBOARD PCU. REPAIRED L/W, OUTBOARD AILERON, PCU HINGE PANEL CRACKED AREA IAW BOEING 757- SRM 57-51-04-OI, ,51-70-05-OG 5.A, 57-51-01-2R FIG 201 SHEET 3.SDR FDEA202107091715Light · inoperativeMDIS 998 33-50 7148 09JUL21 DAY OPEN U COCKPIT EMERGENCY LIGHT WILL NOT ILLUMINATE REPLACED LAMP IAW 33-51-09-3, LIGHT IS STILL INOP MEL 09JUL21 23:59 DAY U RELEASED FOR SERVICE PER MEL : 33-51-01-01 CATEGORY : D EXPIRATION : 06NOV21 "MELSDR FDEA202107061696Skin · dentedL/H WING O/B AFT FLAP HAS 1EA DENT AT UPPER SURFACE APPROX 27" O/B OF THE 2ND TRACK OF THE AFT FLAPAND 9.25" FROM THE T/E REPAIREDL/W O/B AFT FLAP DENT AT THE UPPER SURFACE APPROX. 27" O/B OF THE 2ND TRACK OF THE AFT FLAP AND 9.25" FROM THE T/E IAW B757 SRSDR FDEA202107061695Skin · dentedL/H WING O/B AFT FLAP HAS 1EA DENT AT UPPER SURFACE APPROX. 13" I/B OF THE 2ND TRACK OF THE AFT FLAP AND 5" FROM THE T/E. REPAIREDL/W O/B AFT FLAPDENT AT THE UPPER SURFACE APPROX. 13" I/B OF THE 2ND TRACK OF THE AFT FLAPAND5" FROM THE T/E IAW B757 SRM: 57-SDR FDEA202107061694Skin · dentedL/H WING O/B AFT FLAP HAS 1EA. DENT AT UPPER SURFACE APPROX 2" FROM THE I/B SIDE AND 5" FROM THE T/E. REPAIRED L/W O/B AFT FLAP DENT AT UPPER SKIN APPROX. 2" FROM THE I/B SIDE AND 5" FROM THE T/E IAW B757 SRM: 57-53-01, 51-70-04-0G AND AMM 51-21-00/701 RESDR FDEA202107061693Skin · delaminatedRIGHT WING UPPER L/E I/B SKIN IS DELAMINATED AFT OF #6 SLAT REPAIRED PER SRM 57-41-01 FIG 201SDR FDEA202107021661Web · corrodedNOSE GEAR RIGHT SIDE TUNNEL AREA WEB LOWER SURFACE HAS CORROSION AT BS320 STR17R AS MARK. REMOVED .003" CORRODED MATERIAL FROM ORIGINAL .040" MATERIAL THICKNESS. REMAINING .037" MATERIAL THICKNESS FOUND TO BE WITHIN LIMITS IAW B757 SRM 53-10-15-1A. APPLISDR FDEA202107021660Scuff Plate · crackedL4 DOOR CUTOUT, FWD CORNER SECTION SCUFF PLATE IS CRACKED. REMOVED AND REPAIR AREA IAW FEDEX DWG NO- SR57-53-003 REV A. REINSTALLED SCUFF PLATE IAW AMM 53-13-01-4.SDR FDEA202107021659Rub Strip · crackedR/W I/B FLAP O/B SUPPORT CARRIAGE I/B AND O/B PHENOLIC RUB STRIPS ARE CRACKED REMOVED AND REPLACED RUB STRIPS PER DWG #113N2150 REV CSDR I5PA2021062668803Fuel Control · fluctuatesLOGPAGE 61085 ITEM 1. RIGHT ENGINE SURGE TAKE-OFF CLIMB TO 1500 FEETBETWEEN 1.16 TO 1.21 EPR. REMOVED AND REPLACED RIGHT ENGINE FUEL CONTROL UNIT PER AMM 73-21-02.
NO FURTHER ISSUES AFTER REPLACEMENT.SDR FDEA202106231586Spring · bindingAT BLOCK IN, R1 DOOR WAS DIFFICULT TO OPEN AND SLIDE COVER BECAME DISENGAGED. REINSTALLED COVER AND PERFORMED OPS CK OF R1 DOOR. FOUND WHILE DISARMING DOOR SLIDE, THE AFT LEAF SPRING ON GIRT BAR CAUSES CONTACT ISSUES ON GIRT BAR SLIDER. DOOR CLOSES OK ANDSDR I5PA2021062068802Gearbox · leakingDURING PREFLIGHT CHECK FOUND HEAVY OIL LEAK COMING FROM #2 ENGINE ORIGINATING FROM ANGLE GEARBOX (ALSO FOUND METAL SHAVINGS). REMOVED AND REPLACE #2 ENGINE MAIN AND ANGLE GEARBOX ASSEMBLY IAW AMM 72-61-01. PERFORMED ENGINE RUN AND LEAK CHECK WITH NO FURTHER LESDR FDEA202106171564Frame · crackedDURING ROTO PROBE OF RH BS 1640 AT S-14, CRACKS WERE FOUND IN BOTH BOTTOM HOLES AND BOTH HOLES HAVE INDICATIONS AT 3 O'CLOCK AND 9 O'CLOCK. IT APPEARS THE FRAME IS CRACKED ALL THE WAY ACROSS. COMPLIED WITH E.A. # T F-5310-T0361972 P1 EA TITLE FUSELLAGE-MAISDR I5PA2021061068801Fmc · faultedLEFT FMC REPLACED DUE TO UNIT FAILING ON POWER UP. AFTER REPLACEMENT FMC CONFIRMED OPERATIONAL.SDR I5PA2021051188802Ecu · faultedAPU BLEED FOUND INOP DUE TO A FAULTY ECU DURING THE BITE PROCEDURES. ECU WAS REPLACED AND APU BLEED WAS RESTORED.SDR I5PA2021050488801Sensor · faultedAMBIENT PRESSURE (P2) SENSOR FAILED (LESS THAN 8PSI ON THE GROUND). REPLACED SAME. OPS CHECK NORMAL.SDR I5PA2021042388803Regulator · intermittentLOW DUCT PRESSURE. REMOVED AND REPLACED PRSOV REGULATOR. OPS CHECK OK. DUCT PRESSURE NORMAL.SDR FDEA202104080851Skin · damagedDURING AGING AIRCRAFT INSPECTION OF EXISTING REPAIR LOCATED ON FUSELAGE SKIN AT STA 1380 STR 14L FOUND MULTIPLE TOOLING MARKS ON REPAIR DOUBLER ACCOMPLISHED FEDEX EA F-5330-T0309534-P6 FUSELAGE - PLATES AND SKINS - LOWER SKIN PANEL CORROSION AND DENT REPAISDR I5PA2021040588801Fire Detector · faultedDISCREPANCY - STATUS PAGE "L ENG FIRE LP 2". REMOVED AND REPLACED FIRE DETECTOR ELEMENT. OPS CHECK AND FIRE TEST OK. NO FURTHER STATUS MSG NOTED.SDR I5PA2021032688801Anti-Ice Valve · faultedRT ENG ANTI-ICE EICAS MSG. REMOVED AND REPLACED R ENG INLET THERMAL ANTI-ICE VALVE IAW AMM 30-21-03. LEAK CHECK AND OPS CHECK OK.SDR FDEA202103170676Hose · leakingPDIS 998 29-02 6907 17MAR21 MEM FACT U LOGPAGES:382326 L HYD QTY ADVISORY, L SYS RSVR LIGHT, L SYS PRESS LT AND SUBSEQUANT "L HYD SYS PRESS" CAUTION DURING TAXI AFTER SECOND (RT) ENGINE START. L HYD QTY INDICATES .13RF AND DROPPED RAPIDLY FRSDR I5PA2021022188806Exciter · inoperativeLEFT ENGINE IGNITION SYSTEM NUMBER 2 FOUND INOPERATIVE DUE TO A FAULTY IGNITION EXCITER. EXCITER WAS REPLACED AND CONFIRMED OPERATIONAL WITHOUT FURTHER ISSUES.SDR I5PA202100001Transceiver · faultyDISCREPANCY - LEFT HF INOPERATIVE. CORRECTIVE ACTION - REMOVED AND REPLACED LEFT HF TRANSCEIVER IAW AMM 23-11-03. OPS CHECK OK.SDR I5PA2021021168801Starter · wornDISCREPANCY - APU WON'T START
CORRECTIVE ACTION - REMOVED AND REPLACED APU STARTER MOTOR IAW AMM 49-41-01. OPS CHECK AND LEAK CHECK OK.SDR FDEA202102110326Valve · failedAFTER T/O AT ABOUT 6000' L/H ENGINE EPR STARTED TO FLUCTUATE ABOUT .05 UP AND DOWN. OIL PRESSURE ALSO FLUCTUATED /- 25 PSI. WE TURNED OFF TAI AND THE ENGINE SEEMED FINE.LESS THEN A MINUTE LATER THE SAME PROBLEM CAME BACK. PULLING THE POWER BACK ON DESCENSDR I5PA2021021088805Display · faultedFO MCDU BRIGHTNESS ADJUSTMENT CONTROL INOP. REMOVED AND REPLACED FO MCDU IAW AMM 34-61-02. OPS AND BRIGHTNESS ADJUSTMENT CONTROL CHECK OK.SDR I5PA2021020988804Pilot Valve · faultedDISCREPANCY - L ENG BLEED SURGES ON DESCENT
CORRECTIVE ACTION - REMOVED AND REPLACED L ENG HS PILOT IAW AMM 36-11-08. LEAK CHECK AND OPS CHECK OK.SDR I5PA2021020988803Isolation Valve · faultedDISCREPANCY - BLEED ISLN VALVE STAYS ILLUMINATED. REMOVED AND REPLACED BLEED ISOLATION VALVE IAW AMM 36-11-04. OPS CHECK OK.SDR I5PA2021020188802Modulating Valve · faultyDISCREPANCY FLT DECK COMP TEMP CONTROL INOPERATIVE. CORRECTIVE ACTION R & R FLT DECK TRIM AIR MODULATING VALVE IAW AMM 21-61-07. OPS CHECK OK.SDR I5PA2021020188801Coupler · faultyDISCREPANCY R HF INOPERATIVE. CORRECTIVE ACTION R & R R HF COUPLER IAW AMM 23-11-01. OPS CHECK OK.SDR I5PA2021012988806Scavenge Pump · failedRIGHT OIL SCAVENGE CLOSED.SDR I5PA2021012288805Heater · inoperativeF/O PITOT HEATER INOPERATIVE. REMOVED AND REPLACED PITOT PROBE, PER AMM 34-11-01. OPERATIONS CHECK NORMAL.SDR I5PA2021012188804Exciter · faultyDISCREPANCY NR 1 ENGINE FAILED TO START WITH IGN 1. STARTED OK WITH IGN SW BOTH POSITION. CORRECTIVE ACTION: REMOVED AND REPLACED LT ENGINE IGN 1 EXCITER, IAW AMM 74-11-01. AUDIBLE CHECK OK.SDR I5PA2021011868805Ecu · faultyAPU EGT 635. CORRECTIVE ACTION: REMOVED AND REPLACED APU ECU, IAW AMM 49-61-05. OPERATIONS CHECK AND BITE TEST OK. EGT NORMAL.SDR I5PA2021011788803Idg · inoperativeRIGHT ENGINE GEN DRIVE LIGHT INOPERABLE. ISSUE WAS ISOLATED TO A FAULTY IDG LOW OIL PRESSURE SWITCH. IDG WAS REPLACED AND CONFIRMED OPERATIONAL.SDR I5PA2021011588802Valve · inoperativeRIGHT ENGINE BLEED PRESSURE LOW THROUGHOUT FLIGHT. PRSOV WAS FOUND DEFECTIVE AND REPLACED WITHOUT FURTHER ISSUES.SDR I5PA2021011568804Chip Detector · damagedRT ENGINE MASTER MAGNETIC CHIP DETECTOR HOUSING DAMAGED. CORRECTIVE ACTION: REMOVED AND REPLACED RT ENGINE MCD HOUSING, IAW AMM 79-21-10. LEAK CHECK OK.SDR FDEA202101140101Frame · crackedCRACK INDICATION FOUND IN LOWER INBOARD FASTENER HOLE STA 1640 FUSELAGE FRAME WEB, OUTER CHORD, LOWER HINGE FITTING COMMON TO S-14R INTERCOSTAL TEE CLIP. COMPLIED WITH EA NR F-5310-T0358929 P1. MAJOR REPAIR. CATEGORY "C" REPAIR.SDR FDEA202101120068Floorbeam · crackedFLOOR BEAM INTEGRATION SEGMENT IS CRACKED IN THE AFT RADIUS UNDER THE LBL 45 SEAT TRACK AT STA 580. COMPLIED WITH EA F-5310-T0358814 TITLE: FUSELAGE-MAINFRAME-FLOOR BEAM AT STA 580 AND LBL 45 CRACKED. REPAIR PER DRAWING SR 57-53-004.SDR FDEA202101120067Hinge Fitting · crackedCRACK INDICATION FOUND AT LOWER INBOARD FASTENER HOLE STA 1640 FUSELAGE FRAME WEB, OUTER CHORD, LOWER HINGE FITTING COMMON TO S-14L INTERCOSTAL TEE CLIP. COMPLIED WITH EA F-5310-T0358855 P1. MAJOR REPAIR.SDR I5PA2021011188801Apu · inoperativeAPU AUTO SHUT DOWN. APU FAULT WAS FOUND DURING TROUBLESHOOTING. APU WAS REPLACED AND CONFIRMED OPERATIONAL.SDR I5PA2021011168803Monitor · faultyENGINE VIB INDICATION INTERMITTENT. ON AND OFF DURING FLIGHT. CORRECTIVE ACTION: FOUND AVM IS BAD FROM STOCK. REMOVED AND REPLACED AIRBORNE VIBRATION MONITOR SIGNAL CONDITIONER, IAW AMM 77-31-02. OPERATIONS CHECK OK.SDR I5PA2020010968802Ecu · inoperativeAPU WON'T START AFTER LANDING. REMOVED AND REPLACED APU ECU, IAW AMM 49-61-05. PERFORMED OPERATIONS CHECK, IAW AMM 49-11-00 SATISFACTORY.SDR I5PA2021010168801Signal Cond Unit · faultedDISCREPANCY MAINTENANCE MESSAGE "ENGINE VIB BITE". CORRECTIVE ACTION: REMOVED AND REPLACED AVM SIGNAL CONDITIONER, IAW AMM 77-31-00. TEST OK.SDR I5PA2020122888806Controller · faultedDISCREPANCY-STATUS MESSAGE "CABIN ALT AUTO 1". CORRECTIVE ACTION: REMOVED AND REPLACED NR 1 CABIN PRESS CONTROLLER, IAW AMM 21-31-02. OPERATIONS CHECK AND BITE TEST OK.SDR I5PA2020122488805Generator · failedAPU GENERATOR FAILED INTERNALLY CAUSING DAMAGE TO THE GENERATOR SCAVENGE PUMP. BOTH UNITS WERE REPLACED WHICH PLACED THE APU BACK IN SERVICE.SDR I5PA2020122488804Controller · faultedCABIN AUTO 1 INOPERABLE EICAS MESSAGE FOUND DUE TO A FAULTY CABIN PRESSURE CONTROLLER. PART WAS REPLACED AND CONFIRMED OPERATIONAL
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