Boeing 757-236
Service difficulty reports · 2,544
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 = '757236' 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 = '757236' 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 PIDA07016Skin · damagedDURING INSPECTION, DAMAGE FOUND ON UPPER SURFACE OF THE LEADING EDGE OF THE LEFT WING O/B FLAP. REPAIRED DAMAGE PER SRM 57-53-01 FIGURE 201 REPAIR 2.SDR PIDA07002Skin · dentedDENT IN FUSELAGE SKIN AT BS 760 JUST AFT OF THE L2 DOOR. REPAIRED PER SRM 53-00-01 REPAIR 3.SDR CA061220008Pump · failed(CAN) LT ACMP LEAKING FLUID CAUSING LOSS OF HYDRAULIC QUANTITY AND SYSTEM PRESSURE. AIRCRAFT LANDED AND WAS TOWED OFF THE RUNWAY DUE TO NO NOSE WHEEL STEERING. (TC NR 20061220008)SDR ANCF200600039Filler · damagedDURING TAKEOFF, ABOUT 400FT, EXPERIENCED RT ENGINE FAILURE WITH BUMPING. RT EGT REACHES 933 DEGREES (C) AFTER THAT THE RT ENGINE WAS SHUTDOWN, EMERGENCY PROCEDURE WAS PERFORMED. THE INSPECTION ON GROUND SHOWED THAT ANNULUS FILLER FROM POS 9 WAS RELEASED CAUSSDR RYNA200600007Pcu · failedLOST LT SYSTEM HYDRAULIC FLUID DURING FLIGHT. REMOVED AND REPLACED RT ELEVATOR, CENTER POWER CONTROL UNIT (PCU) IAW MM 27-31-05. OPERATIONAL/FUNCTIONAL AND LEAK CHECKED GOOD.SDR RYNA200600006Software · malfunctionedIRS - SOFTWARE MALFUNCTION NAV ERROR ON ALL 3 IRS'S. RELOADED NAV DATA, RE-ALIGNED IRS AND NO MALFUNCTION NOTED.SDR PIDA06048Skin · delaminatedDURING A-5 CHECK, WHILE ACCOMPLISHING INSPECTION IN ACCORDANCE WITH AD 90-23-06, FOUND NR 10 LEADING EDGE SLAT DELAMINATED ON UPPER SURFACE 15 INCHES FROM INBOARD END JUST BEHIND A PREVIOUS REPAIR. REPLACED SLAT PER MM 27-81-02.SDR ANCF200600013Control Unit · malfunctionedLEFT ENGINE N2 RPM WENT TO OVERSPEED. IAW AMM 75-32-01 PAGE 401, REPLACED BLEED VALVE CONTROL UNIT. OPS CHECK OK FOR SERVICE.SDR RYNA200600004Bottle · low pressureR3 DOOR EVACUATION SLIDE BOTTLE PRESSURE LOW, IN RED. REMOVED AND REPLACED EVACUATION SLIDE.SDR ANCF200600012Warning Light · illuminatedDURING T/O ROLL, AMBER L REV LIGHT ON EICAS ILLUMINATED. T/O WAS REJECTED AT 110 KTS. TRANSFER TO DMI 003 MEL 78-31-1 CAT C.SDR CA060315005Monitor · odorELECTRICAL BURNING SMELL FROM MONITOR. MONITOR SWITCHED 'OFF'. SMELL DISSIPATED. MONITOR ELECTRICALLY DISCONNECTED.SDR PIDA06031Computer · failedRIGHT FCC COMPUTER HAS FAILED. RIGHT AUTO PILOT IS INOP. PLACED ON MEL 22-10-1.SDR PIDA06030Socket · failedAUTO THROTTLE WILL NOT ENGAGE. THRUST MANAGEMENT COMPUTER FAILS INTERFACE TEST; FAULTS OF NO INFORMATION AUTO THROTTLE WARNING-1 NORMAL & WARNING-1 BATTERY DUE TO LIGHT SOCKET BROKEN. REPLACED LIGHT SOCKET. THE LIGHT INDICATING CONTINUITY OF THE CIRCUIT DIDSDR ANCF200600011Smoke · unknownRETURNED TO GATE, SMOKE WAS DETECTED IN THE PASSENGER CABIN. AS PER FIM 21-00-01 PAGE 109 ITEM 6 PROCEDURE 4 WAS PERFORMED CHECK TO THE LT & RT RECIRCULATION FAN FILTERS. AS PER AMM 21-25-02 PAGE 401 THE PREFILTER ON RT RECIRCULATION FAN WAS REPLACED AND FILSDR PIDA06015Battery · dischargedR-2 EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED R-2 EMERGENCY EXIT LIGHT BATTERY IAW MM 33-50.SDR ANCF200400059Warning Light · false activationEICAS MSG (AFT CARGO DOOR 2) AFTER CLOSE DOORS IAW AMM 52-71-00 FIG 103 PAGE BLOCK 1 PSEU BITE WAS PERFORMED FIM 32-09-03 FIG 103.SDR ANCF200400055Warning Light · illuminatedEICAS MSG GEAR DOORS DISPLAYED WITH GEAR HANDLE UP. DOOR AMBER LGT ILLUM. GEAR AMBER LGT AND ALL GREEN DN LGTS EXTIN IAW FIM 32-30-00 PAG. 129. AIRCRAFT WAS RAISED ON JACKS TO PERFOM MLG OPERATIONAL TEST AMM 07-11-01 AMM 29-11-00 TEST SASTIFACTORY.SDR PIDA20050065Charger · inoperativeR4 DOOR EMERGENCY SLIDE LIGHT INOP. REPLACED M736 BATTERY CHARGER PER MM 33-51.SDR PIDA20050066Autopilot Sys · malfunctionedCENTER AUTO PILOT PITCHES NOSE DOWN WHEN ENGAGED. PLACED ON MEL 22-10-1.SDR PIDA20050064Servo Valve · inoperativeCENTER AUTOPILOT INOP, WILL NOT ENGAGE IN FLIGHT. PLACED ON MEL 22-10-1. 08/21/2005, REPLACED CENTER SYSTEM AILERON SERVO VALVE. OPS CHECKS GOOD PER MM 22-13-04.SDR CA050721001Battery · overheated(CAN) EICAS MSG 'MAIN BATT DISCH' OBSERVED DURING DAILY ROUTINE CHECK. BATTERY FOUND EXTREMELY HOT TO TOUCH. LIFE TIME REMAINING OF THIS COMPONENT UNTIL NEXT SCHEDULED REPLACEMENT WAS 142:47 HOURS.SDR PIDA20050060Bulb · inoperativeR4 AND L2 EXTERIOR EMERGENCY EXIT LIGHTS INOP. REPLACED BULBS AT R4 AND L2 EXTERIOR EMERGENCY EXIT LIGHTS PER MM 33-50. OPS CHECKS GOOD.SDR RYNA200500021Skin · dentedLT WING NR 3 LEADING EDGE SLAT TRAILIING EDGE WEDGE OUTBOARD FORWARD SURFACE HAS A DENT AT APPROX WS 560. REPAIRED DENT AT NR 3 SLAT TRAILING EDGE OUTBOARD LOWER SURFACE AT WS 560 IAW B757-SRM 51-70-10 AND 57-43-01.SDR RYNA200500025Shear Plate · corrodedSHEAR SKIN HAS CORRISION AT BS 1720 TO 1681 RBL 50 TO LBL 50 AFT CABIN. CLEANED CORROSION BELOW SHEAR PLATE AND FLOORBEAM IAW B757 SRM 51-40-2 (LIGHT CORRISION). ALODINED AND PRIMED AREA AND REINSTALLED FASTENERS.SDR RYNA200500024Skin · separatedTRAILING EDGE OF LEFT ELEVATOR AT STATION 76.547 IS SEPARATED APPROXIMATELY 1 INCH. ELEVATOR REPAIRED PER B757 SRM 51-70-04.SDR P9RA20050085Bulb · inoperativeJFK - R2 AND R4 DOOR SLIDES WILL NOT INDICATE ARMED. RELAMPED SLIDE ARM INDICATORS IAW M/M.SDR RYAN200500019Floorbeam · corrodedFLOORBEAM HAS CORROSION AT UPPER CAP BS 1640 RBL48.SDR P9RA20050082Odor · detectedEN ROUTE, FLT LEVEL 360, ELECTRICAL FUMES IN COCKPIT AND CABIN. HAD ENGINE ANTI ICE ON AND CONT IGNITION ON. SMELL DISSIPATED WHEN THESE ITEMS WERE SELECTED OFF. PERFORMED INSPECTIONS OF ENGINES, AIR CONDITIONING PACKS, IGNITION SYSTEMS. GROUND RAN AIRCRAFT SDR P9RA20050078Connector · looseLAS GATE ITEM 1P, FIRST WHITE TRACK LIGHT INOP ADJACENT TO LAVATORY. SECURED CONNECTOR ON FLOOR EMERGENCY LIGHT. OPS CHECKED GOOD.SDR P9RA20050077Bulb · inoperativeAIRCRAFT IN MAINTENANCE ORD; MID CABIN BULLNOSE EMERGENCY LIGHT INOP. RELAMPED MID CABIN EMERGENCY LIGHT IAW MM.SDR CA050401012Torque Ring · worn(CAN) AIRCRAFT ARRIVED WITH DAMAGE TO THE NR 2 ENG FORWARD THRUST REVERSER TORQUE BOX ON THE OB SIDE. CLOSER INSPECTION REVEALED THAT THE BLADE STRAP (PART OF THE ACTUATOR LOCKOUT MECHANISM) AFT ATTACHMENT POINT CAME LOOSE AND WHEN THE THRUST REVERSER STOWED SDR P9RA20050073Bulb · burned outAIRCRAFT IN MAINTENANCE, ROW 20 TO 23 EMERGENCY PATH LIGHTING INOPERATIVE. REPLACED BULBS PER MM.SDR P9RA20050072Light · burned outAIRCRAFT IN MAINTENANCE FLOOR EMERGENCY TRACK LIGHTS AFT CABIN INOPERATIVE. REPLACED FLOOR TRACK LIGHT ASSY PER MM.SDR P9RA20050070Proximity Switch · contaminatedCVG - LOW SPEED REJECTED TAKE OFF AT 70KTS FOR AFT CARGO DOOR INDICATION. PLACED DOOR INDICATION ON MEL 52-71-1. MAINTENANCE PROCEDURES COMPLIED WITH. ITEM CLEARED 2/19/2005; SYR MAINTENANCE ENTRY. TROUBLESHOT INDICATION SYSTEM PER FIM. SWITCH FOUND TO BESDR P9RA20050069Light · inoperativeAC IN MAINTENANCE CVG. FLOOR EMERGENCY LIGHTING BETWEEN ROWS 3-8 INOPERATIVE. REMOVED AND REPLACED LIGHT ASSY. IAW MM.SDR P9RA20050068Proximity Sensor · dirtyCANCUN - AFTER LANDING, FLIGHT ATTENDANT NOTICED R1 DOOR SLIDE LIGHT WAS NOT ILLUMINATED. ITEM DEFERRED PER MEL 25-66-5. INSPECTED, CLEANED GIRT BAR PROXIMITY SWITCHES. OPS CHECKED GOOD. CLEARED MEL 25-66-5.SDR ANCF200400039Controller · maladjustmentEICAS MSG CABIN ALTITUDE DISPLAYED, CABIN ALT AND CABIN ALTITUDE LIGHTS ILLUM. UNABLE TO RESTORE CABIN PRESS USING MANUAL MODE. AT 39000 FT CABIN ALTITUDE MSG DISPLAYED. THE CABIN ALTITUDE SHOW`S 12000 FT AND START THE DESCENT, THE DESCENT WAS ACCOMPLISHEDSDR CA050128005Cooling Fan · binding(CAN) CREW NOTICED A BURNING SMELL THROUGHOUT AIRCRAFT AND THEN HAD AN EICAS MESSAGE (EQUIPMENT OVERHEAT) . MAINTENANCE CONFIRMED FWD EQUIPMENT COOLING FAN BINDING AND A BURNT SMELL COMING FROM UNIT.SDR P9RA20050065Battery Pack · inoperativeAIRCRAFT IN MAINTENANCE ORD, DOORS 2L AND 2R EMERGENCY LIGHTING INOPERATIVE. REMOVED AND REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS IAW MM. L2 DOOR PART INFORMATION, PART NUMBER 2013A1, SERIAL NUMBER OFF 24696, BATTERY PACK. R2 DOOR AS STATED BELOW.SDR 757BJ0016Battery Pack · inoperativeFORWARD RIGHT EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK. OPS CHECKS OK.SDR 757BJ0015Control Cable · frayedAILERON CABLE FRAYED AT NR 1 FLAP TRACK. REPLACED CABLE PER MM 27-00-01 AND COMPLIED WITH BOEING SB 757-27-0109.SDR 757BJ0014Control Cable · wornAILERON CABLE WORN AT THE NR 8 FLAP TRACK. REPLACED CABLE PER MM 27-00-01 AND COMPLIED WITH BOEING SB 757-27-0109.SDR 757BJ0013Attach Angle · damagedATTACH ANGLE DAMAGED BENEATH THE LEFT TRANSITION ANGLE IN THE AFT CARGO BIN AT BS 1360. REPLACED ANGLE PER SRM 51-30-01, 51-40-05, AND 51-40-02.SDR 757BJ0012Stringer · corrodedCORROSION IN STRINGER 29 (BL 0) FROM BS 418 TO BS 426.5. REPLACED SECTION OF STRINGER PER SRM 51-10-00 AND BOEING DRAWING 141N3270.SDR 757BJ0011Drag Angle · wornWEAR ON THE VERTICAL LEG OF THE LEFT FIN ATTACH ANGLE (DRAG ANGLE) BETWEEN BS 1164 AND BS 1720. REPAIRED PER EA 53-319.SDR P9RA20050066Battery Pack · inoperativeAIRCRAFT IN MAINTENANCE DTW, EMERGENCY LIGHTS AT R2 DOOR INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK IAW MM.SDR P9RA20050064Proximity Sensor · dirtyAIRCRAFT IN MAINTENANCE CCS, DOOR 4R SLIDE ARM LIGHT INOPERATIVE. PLACARDED AND PLACED ON MEL. MAINTENANCE ENTRY 1-08-2005 SFB REF MEL 25-66-5. CLEANED SWITCH CONTACTS. OPS CHECKED GOOD AND CLEARED MEL. NO PARTS CHANGED.SDR RYNA200500001Module · fodLEFT ENGINE FIRE LOOP NR 2 STATUS MESSAGE ILLUMINATED ON DESCENT. CLEANED FOD FROM AFOLTS CARD FILE MODULE. OPERATIONAL CHECK NORMAL.SDR P9RA20040060Bulb · inoperativeA/C IN LAS. R1 & R3 EMERGENCY SLIDE LIGHT INOP. RELAMPED R1 & R3SDR ANCF200400038Radio · inoperativeRECEPTION ON L VHF COMM INOPERATIVE, TRANSMISSION O.K. AND R VHF INOPERATIVE AND DEFERRED. AFTER LANDING 2 VHF COMM BECOME NORMAL. IAW WDM 23-12-02 AND 23-12-02 VHF COMM CONTROL PANEL WIRING WAS CHECKED AND OPERATIONAL TEST WAS PERFORMED IAW AMM 23-12-00 PAGE
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