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 FDEA201803270785Assist System · making metalL1 DOOR ASSIST SYSTEM INADVERTENTLY ACTIVATED WHEN OPENING DOOR MANUALLY. SLIDE DID NOT DEPLOY. REMOVED AND REPLACED THE L1 DOOR EMERGENCY POWER RESERVOIR CYLINDER IAW AMM 52-11-30-4. INSTALLED THE ORGINAL L1 DOOR SLIDE IAW AMM 25-66-01-4. OPS CHECKED GOSDR FDEA201803200741Unknown · malfunctionedDURING APPROACH TO LANDING TE FLAP DISAGREE APPEARED ON EICAS. FLAPS WOULD NOT MOVE, STUCK ABOUT 22. EXECUTED MISSED APPROACH AND FOLLOWED QRH. UNEVENTFUL LANDING AFTER DECLARING EMERGENCY. PERFORMED BITE TO FSEU NR 1, NR 2, & NR 3 AND CYCLED SEVERAL TIMES FLSDR FDEA201803130673Gear · brokenDURING PREFLIGHT FOUND L1 LOCKING OPEN MECHANISM GEAR BROKE, DOOR OPENS AND CLOSES NORMALLY, LOCKING CLOSED MECHANISM GOOD. REMOVED AND REPLACED THE L1 DOOR HOLD OPEN LOCK IAW AMM 52-11-08-4-0. OPS CHECKED NORMAL. ACFT OK FOR SERVICE.SDR FDEA201803110651Girt Bar · out of adjustL1 DOOR WILL NOT ARM WHEN CLOSED. PERFORMED ADJ/TEST OF L1 DOOR GIRT BAR MECHANISM. OPS CHECKED GOOD IAW MM 52-11-25-5.SDR FDEA201803060603Switch · malfunctionedAFTER DEPARTING, WHEN MOVING FLAPS FROM FLAPS 1 TO FLAPS UP, RECEIVED AN LE SLAT ASSYMETERY. EMERGENCY DECLAIRED, RAN QRH, RETURNED TO DEPARTURE. REMOVED AND REPLACED THE LT OTBD SLAT LOSS SENSING SWITCH IAW MM 27-81-42-4. ADJUSTED SWITCH IAW MM 27-81-42SDR FDEA201803050598Transmitter · failedLE FLAP ASYMMETRY ON APPROCH. COMPLIED WIHT QRH. CONTINUED TO UNEVENTFUL LANDING. PERFORMED BITE CHECK OF FSEU NR 1, 2, & 3. FOUND SLAT LOSS ON LEG 0 AND SLAT DISAGREE ON LEG 1 OF FSEU NR 1. FOUND SLAT LOSS/SLAT SYSTEM ON FSEU NR 2. NO FAULTS ON FSEU NR 3. SDR FDEA201802280521Track · wornON FINAL APPROACH, LE FLAP ASYMETRY EICAS MESSAGE WITH LEADING EDGE LIGHT. ACCOMPLISHED LE FLAP ASYMETRY CHECKLIST AND LANDED UNEVENTFULLY. INSTALLED A LT INBD SLAT LOSS SWITCH NON ADJUSTABLE TRACK IAW AMM 757-27-81-41-5. CYCLED SLATS THROUGH SEVERAL CYCSDR FDEA201802220479Lamp · inoperativeL1 DOOR ARM LIGHT DOES NOT ILLUMINATE WHEN DOOR SLIDE IS ARMED. REPLACED THE LAMP IAW MM 33-16-02-2.SDR FDEA201802130375Proximity Sensor · out of toleranceDURING DEPARTURE, SPEED TAPE ZIPPER WOULD NOT RETRACT ABOVE 267 KNOTS. BOTH CAPTAIN`S AND FIRST OFFICER`S ZIPPERS WERE FROZEN. NO EICAS MESSAGES, NO FLIGHT CONTROL PROBLEMS. PERFORMED A PSEU BITE IAW FIM 32-09, FAULT TREE 805, FAULT CODE 003 DISPLAYEDSDR FDEA201802080329Pump · leakingLEFT HYD QTY LOW EICAS MESSAGE, FOLLOWED BY LT HYD SYS PRESSURE LOW DURING CRUISE FLIGHT, APPROX ONE HOUR PRIOR TO LANDING. AP FOLLOWING QRH PROCEDURES TURNED OFF THE ENGINE HYD PUMP AND LT ELEC HYD PUMP.HYD QTY INDICATED 0.04 ON STATUS PAGE. FOUND HYDSDR FDEA201802060309Autothrottle Sys · malfunctionedLEFT ENGINE THRUST LEVER FROZE IN FLIGHT AT APROXIMTELY 1.5 EPR, WHILE PASSING 30,000 FT, TURNED AUTOTHROTTLES OFF AND MADE NO DIFFERENCE. ABLE TO BREAK LOOSE WITH A SUBSEQUENT BIND, BROKE FREE AGAIN AND WAS OK THE REMAINDER OF THE FLIGHT. PERFORMED AN INSDR FDEA201802030298Warning System · activatedTRAILING EDGE FLAP DISAGREE MASTER CAUTION ON SHORT FINAL. EXECUTED A GO AROUND. COMPLIED WITH QRH LANDED FLAPS 20 KPWM. ONCE DOWN POWERED RETRACTED FLAPS, PER FIM 27-51-00 FT 808. CHECKED FSEU NO "LRU" FAULTS. RETURN A/C TO NORMAL CONFIGURATION.SDR FDEA201802020292Control Unit · inoperativeEICAS FOR ANTI SKID, NUMEROUS TIMES DURING FLIGHT REMOVED & REPLACED THE ANTI-SKID, AUTOBRAKE CONTROL UNIT ASSY, OPS CHECKED NORMAL IAWAMM 32-42-01-4.SDR FDEA201801300277Cam · deformedFOUND THE MAIN DECK CARGO DOOR CAM LATCH NR 7 LIP DEFORMED. REMOVED AND REPLACED THE CAM LATCH IAW MM 52-32-00-0-0. ADJUSTED AND TEST PERFORMED IAW MM 52-32-00-05. TESTED OK.SDR FDEA201801230200Fan · failedBURNING ODOR FOLLOWED BY EQPT OVERHEAT EICAS AND EQUIPMENT COOLING OVERHEAT LIGHT. RAN QRH, OVHT INDICATION REMAINED ON. LANDED AIRCRAFT, NO OTHER PROBLEMS. REMOVED AND REPLACED THE NR 1 FWD EQUIPMENT COOLING SUPPLY AIR FAN IAW MM 21-58-06-4, OPS CHECKESDR FDEA201801140091Girt Bar · bentLEFT L1 DOOR GIRT BAR TAB BENT. REMOVED AND REPLACED L1 DOOR GIRT BAR IN REF TO AMM 25-6601-4. OPS CHECK NORMAL. OK TO CONTINUE.SDR FDEA201801040024Cabin Pressure · malfunctionedCABIN ALTITUDE MASTER WARNING IN FLIGHT AT FL280, WITH ONLY RIGHT PACK OPERATING. CABIN ALTITUDE READ 10,000 FT. DECENDED TO FL 200 AND CABIN DECENDED TO 8,000 FT. MODE SELECT WAS ON AUTO 1. COMPLIED WITH FIM 21-30 FAULT TREE 802, AND PERFORMED A LEFT ASDR FDEA201712013330Valve · inoperativeNOTE: CAPTAIN REPORT TO GOC & MOCC = EMERGENCY LANDING TO STN DUE TO THE LOSS OF THE CABIN PRESSURIZATION PDIS 910 21-30 8396 01DEC17 STN CABIN ALTITUDE WARNING @ FL280 QRH COMPLIED WITH. CABIN @10000 FEET. ACCOMPLISHED FIM FAULT TREE 80SDR FDEA201711213289Battery · dischargedDURING SERVICE CHECK FOUND EMERGENCY LIGHT INOP. PER AMM 33-51-07-2, REMOVED AND REPLACED THE BATTERY AND EMERGENCY LIGHT. OPS TEST NORMAL. A/C OK FOR SVC.SDR FDEA201711073188Rope · exposedDOOR L1 HAD A PIECE OF EQUIPMENT EXPOSED AFTER CLOSING. RAMP PERSONNEL HAD US RE-OPEN DOOR TO SECURE. CALLED MX. SECURED DOOR SLIDE ROPE AND SLIDE COVER REF MM CH. 25-66-01-4. OK TO CONTINUE. OPS CHECKED NORMAL.SDR FDEA201711013128Guide · out of adjustUNABLE TO CLOSE THE L1 DOOR. DOOR PROGRAMMING INCORRECT. TIGHT AT FRONT, GAP AT TOP AFT CORNER. REMOVED THE L1 DOOR SLIDE COVER IAW AMM 52-11-00-5. ADJUSTED THE L1 DOOR GUIDE ARM AND HANDLE MECHANISM IAW AMM 52-11-04-2, AND 52-11-13-2. OPS CHECKED GOOD SDR FDEA201710303105Skin Panel · gougedBULK CARGO DOOR EXTERIOR SKIN HAS GOUGE ABOVE DOOR HANDLE CUTOUT. REPAIRED BULK CARGO DOOR EXTERIOR SKIN ABOVE DOOR HANDLE CUT OUT AS REQUIRED IAW EA F-5230-T0336231 P1.SDR FDEA201710162966Battery Pack · inoperativeR1 INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE M730 POWER SUPPLY BATTERY PACK IAW AMM 33-51-07-2, OPS CHECKED GOOD.SDR FDEA201710032848Light · inoperativeRIGHT DOOR SLIDE ARM LIGHT NOT ILLUMINATED WHEN FIRST OFFICER WENT TO DISARM THE DOOR. RT DOOR SLIDE ARM LIGHT FILLARMENTS REPLACED IAW AMM 33-20-00. OPS TESTED GOOD.SDR FDEA201709142571Girt Bar · contaminatedLEFT DOOR ARMING HANDLE IS STIFF TO MOVE TO THE ARM POSITION AMM 25-66-10-2. GIRT BAR FLOOR FITTINGS FOUND CONTAMINATED WITH DEBRIS. FITTINGS CLEANED AND DEBRIS REMOVED. DOOR ARMING NOW SATISFACTORY TO CREW.SDR FDEA201709012442Sensor · damagedL1 DOOR SLIDE ARMED LIGHT IS ILLUMINATED WITH THE HANDLE IN THE DISARMED POSITION. R & R THE SENSOR S10215 IAW SWPM 20. PERFORMED ADJUSTMENT AND TEST IAW MM 52-11-25-5. OPS CHECKED GOOD.SDR FDEA201708182273Floorbeam · crackedMAIN CARGO BAY STUB FLOORBEAM AT BS 580, LBL 45.5 - 58.22, AFT FLANGE IS CRACKED. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-40-02, AND DWG 657N4311, REV -.SDR FDEA201708112187Lamp · inoperativeR1 DOOR EMERGENCY SLIDE LIGHT FOUND INOPERATIVE DURING TEST. REPLACED THE LAMP AND OPS CHECKED NORMAL IAW MM 33-51-06-2-1. ACFT OK FOR SERVICE.SDR FDEA201708102173Shear Plate · crackedMAIN CARGO BAY SHEAR PLATE IS CRACKED AT BS 580, LBL 45.5. REPAIRED THE SHEAR PLATE IAW EA F-5310-T0334835 P1.SDR FDEA201708082148Seat Track · corrodedCORROSION ON COURIER SEAT TRACK R1 DOOR ENTRY BS 345 TO 377, LBL 5. REMOVED CORROSION, HAD 100% MATERIAL LOSS AND IS OUT OF LIMITS. FABRICATED A NEW SEAT TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02, 51-10-02, 53-00-52-1A, 51-40-05 AND DWGS SDR FDEA201708042116Seat Track · crackedMAIN CARGO COMPARTMENT SEAT TRACK AT BS 580 LBL 45.5 IS CRACKED ON IB FLANGE AT FLOORBEAM. REMOVED THE SEAT TRACK . FABRICATED A REPLACEMENT SEAT TRACK AND INSTALLED IAW SRM 51-40-02 AND DWG 143N5090, REV-, AND 143N5080, REV A.SDR FDEA201708032105Pitot Tube · dirtyREJECT TAKE OFF, NO AIRSPEED ON CAPTAIN SIDE ON HUD OR ND. REMOVED AND REPLACED CAPTAIN`S PITOT PROBE UP TO SEP 3.F.(21). COMPLETED INSTALLATION FROM STEP 22 IAW AMM 34-11-04-14-4. OP CHECKED NORMAL.SDR FDEA201708022097Door Frame · puncturedTOP OF LOWER FRAME PUNCTURED BS 231 AT THE FORWARD ACCESSORY DOOR CUTOUT. COMPLIED WITH FED EX EA F-5310-T0334685 P1. REPAIRED THE DOOR FRAME IAW SRM 53-00-00-07-1A. REMOVED DAMAGE TO .500 DIA, FABRICATED REPAIR ANGLE AND INSTALLED ANGLE IAW EA F-5310-T033SDR FDEA201707272059Fmc · malfunctionedON TWO OCCASIONS DURING FLIGHT, RT FMC GAVE INCORRECT PITCH COMMANDS TO AUTOPILOT. R & R THE RT FMC IAW AMM 34-61-01-4-2.SDR FDEA201707141943Battery Pack · inoperativeL1 DOOR EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACE THE NR 1 BATTERY PACK IAW MM 33-51-07-2. OPS CHECKED GOOD.SDR FDEA201707141942Battery Pack · inoperativeL1 DOOR INTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK. OPS CHECKED GOOD.SDR FDEA201707061871Engine · overtempAT 10,000, CLIMBING IN CLIMB, POWER LEFT ENGINE FUEL FLOW GOT HIGH AND EGT YELLOW. RAN QRH AND RETURNED TO AIRPORT. ONLY REASON ENGINE DID NOT GO INTO RED EGT IS PILOT ACTION. REMOVED AND REPLACED THE NR 1 ENG P1 PROBE IAW AMM 73-21-04-4, OPS NORSDR FDEA201707061870Warning Message · false activationLEFT ENGINE, HIGH EGT AND FUEL FLOW AT 10,000 FT WHEN CHANGING POWER FROM CLIMB 2 TO NORMAL CLIMB. RAN THE QRH, CONTINUED TO OPERATE ENGINE (LEFT) AT LOWER POWER AND RETURNED TO AIRPORT. INSPECTED NR 1 ENGINE INLET AND EXHAUST WITH NO DEFECTS NOTED IAW MMSDR FDEA201707051853Door · corrodedLAVATORY SERVICE DOOR, AFT RIGHT CORNER DELAMINATED AND HAS CORRODED. REMOVED AND REPLACED THE FWD LAVATORY SERVICE DOOR IAW SRM 51-40-02.SDR FDEA201707031845Frame · gougedFWD E & E BAY BS 231.25, BL. 0 FRAME GOUGED ON UPPER SURFACE. REPAIRED THE FRAME IAW SRM 53-00-07-1A. FIG 101 DETAIL II.SDR FDEA201707031844Floor Panel · damagedMAIN CARGO COMPARTMENT FLOOR PANEL AT POSITION 6R IS DAMAGED. REPAIRED MAIN CARGO FLOOR PANEL AT POSITION 6R IAW SRM 53-00-50, REV 121.SDR FDEA201706301851Floor Panel · damagedMAIN CARO BAY FLOOR PANEL 6R IS DAMAGED. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50, REV 121.SDR FDEA201706261761Floorbeam · corrodedMAIN DECK BS 377.7, LBL 24.75 - 58.22, FLOORBEAM CORRODED. REPAIRED THE FLOORBEAM IAW EA F-5310- T0333967 P1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201706201712Proximity Sensor · out of adjustGEAR DOORS EICAS WITH DOOR ANNUCIATOR, AFTER TAKEOFF. WITH GEAR HANDLE PLACED IN THE OFF POSITION. INSPECTED LEFT AND RIGHT MAIN GEAR DOORS, STOPS, STOP PLATES, AND SENSORS. FOUND LEFT AND RIGHT FORWARD STOP BOLTS WORN BEYOND LIMITS. LEFT READS .017, RIGHSDR FDEA201706161681Controller · malfunctionedCABIN ALTITUDE EICAS WARNING AT FL380. COMPLIED WITH QRH, DESCENDED TO FINAL ALTITUDE FL250. RECOVERED CABIN PRESSURE IN AUTO 2 AT CABIN ALTITUDE 7500. NORMAL DESCENT AND PRESSURE UNTIL LFPG. REPLACED THE NR 1 CPC IAW MM 21-31-02-4, TESTED OK. COMPLYED WISDR FDEA201706141652Girt Bar · obstructedLEFT ENTRY DOOR WILL NOT CLOSE PROPERLY. FOUND LOOSE LANYARD INTERFERRING WITH GIRT BAR. RESTOWED LANYARD IAW AMM 25-66-01-4. OPS CHECK SATISFACTORY.SDR FDEA201706141644Line · tangledLEFT ENTRY DOOR SLIDE LIGHT INOPERATIVE. TROUBLESHOT TO STATIC LINE CAUGHT IN GIRT BAR. UNTANGLED THE STATIC LINE & TUCKED INTO FOLDED GIRT BAR SLIDE POUCH IAW AMM 25-66-01-4.SDR FDEA201706011552Frame · dentedMAIN DECK, BS 520 FRAME DENTED AT STRINGER 6R. REPAIRED THE FRAME IAW SRM 53-00-07-2R, REPAIR 3. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201705181454Plug · detachedAT FL 350, THE RT ENG OIL PRESSURE ALERT ACTIVATED. OIL QTY RAPIDLY DECREASED TO ZERO. WINDMILLED FOR 30 MINUTES. FOUND THE ENGINE CUP PLUG HAD FALLEN OUT OF THE HIGH SPEED GEARBOX REINSTALLED THE PLUG, SERVICED OIL TANK, INSPECTED CHIP DETECTORS, NO MSDR FDEA201705131408Collar · brokenWHILE SECURING AIRCRAFT FOUND L1 DOOR HOLD OPEN LOCK COLLAR BROKEN. DOOR WOULD NOT LOCK IN THE OPEN POSITION. REMOVED AND REPLACED L1 DOOR HOLD-OPEN LOCK COLLAR IAW AMM 52-11-08-8. DOOR OPS CHECKED GOOD
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