Boeing 757-28A
Service difficulty reports · 2,000
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 = '75728A' 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 = '75728A' 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 NOCA2905Bulb · inoperativeE PATH AT DOOR 4 ONE RED LIGHT AT END INOP.SDR NOCA2805Psu · openFPO AFTER LANDING PSU ROW 34DEF OPENED AND THE OXYGEN MASK WERE EXPOSED. OXYGEN GENERATORS WHERE NOT ACTIVATED. PSU AND SEATS DEFERRED.SDR NOCA2705Circuit Breaker · poppedSNN FLT 123 DOOR GIRT BAR INDICATION CIRCUIT BREAKER POPPED. WILL NOT RESET. DEFERRED CI 25-965 MEL 25-66-5SDR ANCF200400061Actuator · failedBOTH FLAP POINTERS ARE ON HALF POSITION WITH THE FLAP LEVER UP. L/E SLAT DISAGREE LIGHT ILLUMINATED. L/E SLAT DISAGREE DISPLAY ON EICAS. VOICE RECORDER CB WAS PULL OUT AS SB REQUEST. IAW AMM 27-58-01 PAGE 501 ACCOMPLISHED RIGGING ON TRANSMITTER POSITION SLASDR ANCF200400060Lever · malfunctionedBOTH FLAP POINTERS ARE ON HALF WITH THE FLAP LEVER IN UP. L/E SLAT DISAGREE LIGHT ILLUM. L/E SLAT DISAGREE DISPLAY ON EICAS. (VOICE RECORDER CB PULL OUT ACCORDING TO SECURITY BULLETIN) IAW AMM 27-09-00 PAGE 201 FSEU N° 2 AND 3 WERE SWAPPED. NO FAULT NOTED OSDR NOCA2505Bulb · inoperativeR1 DOOR ARM SLIDE INDICATOR INOPERATIVE. RELAMPED R1 DOOR SLIDE ARM LIGHT SYSTEM OPERATES NORMALLY.SDR NOCA1805Bulb · inoperativeDURING ROUTINE MAINTENANCE, FOUND EMERGENCY EXTERIOR LIGHT FROM L1 DOOR INOPERATIVE. REPLACED BULB, SYSTEM OPERATES NORMALLY.SDR NOCA1605Bulb · inoperativeJFK - ROUTINE MAINTENANCE FOUND 1L EMERGENCY EXIT EXTERIOR LIGHT INOP. RELAMPED 1L EMERGENCY EXIT LIGHT, OPS CHECK OK.SDR ANCF200400054Antenna · inoperative(WXR FAIL DISPLAYED ON HSI. WXR TEST INOP) IAW AMM 34-43-05/401 AND 34-3-00/401 WXR ANTENNA AND TRANSCEIVER WERE REPLACED. ANTENNA P/N 622-5135-202 S/N ON 1959 OFF 2967 TRANSCEIVER P/N 622-5132-101S/N ON 4604 OFF:6335SDR NOCA1405Connector · looseFOUND EMERGENCY PATH LIGHTING ROWS 31, 32 AND 36 INOP. SECURED CONNECTIONS AT ROWS 31, 32 AND 36 SYSTEM OPERATES NORMALLY.SDR RYNA200500029Line · leakingEICAS MESSAGE LEFT HYDRAULIC QUANTITY AND PRESSURE LOST. QUANTITY LEVEL 0.10 LT. REMOVED AND REPLACED RIGHT DOWNLOCK ACTUATOR RETURN LINE. LEAK CHECK GOOD, ALSO FOUND NR 1 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. REMOVED AND REPLACED ENGINE DRIVE PUMP AND PRESDR NOCA1105Oven · inoperativeSMOKE IN AFT GALLEY. FLIGHT ATTENDANTS AND CREW DETERMINED THAT THE SMOKE WAS ORIGINATING FROM BEHIND THE CONTROL PANEL OF NR 6 OVEN AND NOT FROM CONTENTS BEING COOKED. THE OVEN INSERT WAS REMOVED, CIRCUIT BREAKER FOR NR 6 OVEN PULLED AND POWER TO AFT GALLEYSDR CA050822004Strap · cracked(CAN) DURING DAILY INSPECTION, FOUND LOW PRESSURE CASE UPPER ACCESSORY MOUNTING STRAP BROKEN.SDR CA050816001Windshield · cracked(CAN) WHILE IN FLIGHT, THE FLIGHT CREW NOTICED ARCING INSIDE THE FIRST OFFICER WINDSHIELD WHICH RESULTED IN A SEVERELY CRACKED OUTER PANE.SDR 2005000007Accelerometer · faultyN1 ENG VIB HIGH ON CLIMB OUT (YELLOW) READ 2.7, ENG INDICATIONS NORMAL. VIBRATION RETURNED BELOW 2.5 WITH THRUST LEVER RETARDED ENG WAS NOT SHUT DOWN. TROUBLE SHOT ENG VIBRATION PER 757 FIM 77-31-00 RT ENG VIBRATION CONTROLLER BOX HAD FAULT CODE B8 DISPLAYEDSDR CA050531003Engine · making metal(CAN) DURING ENGINE START, ENGINE FAILED TO ACHIEVE APPROPRIATE RPM. START ABORTED. TROUBLESHOOTING FOUND DEBRIS IN THREE CHIP DETECTORS. ENGINE WILL BE CHANGED AND SHIPPED BACK TO OVERHAUL FACILITY FOR INVESTIGATION.SDR NOCA0605Apu · shutdownAPU SHUTDOWN WHEN LEFT PACK WAS TURNED OFF PERFORMED BITE PER FIM 49-11-00. RESET APU STARTED AGAIN OPS CHECKED NORMAL.SDR 2005000006Indicator · failedCAPTIANS AIRSPEED FAILED TO RISE BY 80 KNOTS REJECTED T/O 95 KNOTS. DISCONNECTED CAPTIANS PITOT LINE FROM ADC. CLEANED OUT LINE FOUND LINE TO BE BLOCKED BY A BUG. RECONNECTED PITOT LINE AND ADC. PERFORMED PITOT/STATIC TEST PER 757 MM 34-11-10.SDR 2005000005Indicator · failedCAPTIANS AIRSPEED FAILED TO RISE ON TAKEOFF ROLL REJECTED T/O AT 100 KNOTS. REPLACED CAPTIANS AIRSPEED INDICATOR PER AMM 34-13.SDR CA050517006Bolt · missing(CAN) DURING C CHECK, IT WAS FOUND THAT THE FRONT MOUNT ASSEMBLY HAD A KEEPER BOLT MISSING FROM THE AFT PICKUP BEARING BUSHING. THE BEARING BUSHING HAD SHIFTED TRANSFERING ALL WEIGHT TO ONE LUG OF THE BRACKET. COMPLETE MOUNT WAS REPLACED AS A PRECAUTION. APPRSDR CA060502007Heat Shield · delaminated(CAN) NR 1 ENG RT THRUST REVERSER COWL AFT HEAT SHIELD DAMAGED (DISBONDED). REPAIR FOR HEATSHIELD IN OEM MANUAL. (TC NR 20060502007)SDR RYNA200500015Warning Light · illuminatedAFTER TAKEOFF FROM NKW, EXPERIENCED AN APU FIRE WARNING INDICATION WITH ALL FIRE WARNING LIGHTS BUT NO HORN DURING CLIMB. APU WAS SHUTDOWN BEFORE TAXI. CREW FOLLOWED EMERGENCY PROCEDURES, DISCHARGED THE FIRE BOTTLE AND RETURNED TO UKW. AIRCRAFT LANDED WITHOSDR ANCF200400049Transceiver · unknownWXR FAIL DISPLAYED ON HSI AND WXR TEST DISPLAYS WRX FAIL RT. WITH AMM 34-43-01 PAGE 401 WAS REPLACED TRANSCEIVER ALSO WAS CLEANED THE FILTER OF TRANSCEIVER RADAR COOLING.SDR NOCA0405Governor · faultyOAK - ON PUSHBACK RT ENGINE SHUTDOWN 30 SECONDS AFTER START AIRCRAFT RETURNED TO GATE. TROUBLESHOT AND REPLACED RT ENGINE FUEL FLOWGOVERNOR. PRECAUTIONARY CHANGE OF RT ENGINE SPAR VALVE ACTUATOR.SDR RYNA200500012Transmitter · inoperativeDURING CLIMB-OUT ABOVE 14,000, THE CREW NOTICED AN ABNORMAL SPLIT IN ENGINE PARAMETERS WITH THRUST LEVERS MATCHED UP. WHEN TRYING TO MATCH EPR, THERE WAS A HUGE SPLIT IN THRUST LEVER POSITION AND N1, N2, N3, EGT AND FUEL FLOW. AIRCRAFT RETURNED TO ORD AND LASDR RYNA200500013Tube · crackedDURING CLIMB FROM ORD, THE NR 2 ENGINE N1 WAS INDICATING .16 LOWER THAN THE NR 1 ENGINE. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED CRACKED TUBE OFF NR 2 ENGINE P1 PROBE. OPERATIONAL CHECK NORMAL.SDR NOCA0205Reservoir · dischargedFOUND L1 DOOR ASSIST BOTTLE PRESSURE LOW. REMOVED AND REPLACED L1 DOOR ASSIST BOTTLE IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL.SDR CA050114003Motor · leaking(CAN) A/C DEPARTED AND TURNED AROUND AFTER NOTICING SLOW STEADY DECLINE IN CENTER SYSTEM QUANTITY. MAINTENANCE FOUND FLUID LEAKING FROM FUSELAGE DRAIN HOLES IN THS COMPARTMENT. UPON INVESTIGATION MAINTENANCE FOUND CENTER SYSTEM HYD MOTOR ON THIS GEARBOX LEAKINSDR CA041022002Control Panel · failed(CAN) AFTER DEPARTURE YVR ENROUTE LAX, CREW NOTICED NUMBEROUS FAILURES IN AUTOFLIGHT MODE CONTROL PANEL.NOT ABLE TO SELECT SPECIFIC HEADING. HEADING INDICATIONS ON CAPT/FO EHSI DIFFERENT. UNABLE TO SELECT ALTITUDE, ALSO AUTOPILOT WOULD NOT CONTROL AIRCRAFT TOSDR ANCF200400026Slat · out of adjustEICAS MESSAGE LT SLAT DISAGREE DISPLAYED. WITH THE FLAP LEVER IN 1 BOTH FLAP POINTERS INDICATE .5. LT SLAT DISAGREE CHECK LIST ACCOMPLISHED AND MESSAGE REMAINED ON AFTER PROCEDURE COMPLETED. PERFORMED FIM PROCEDURE 27-81-00 PAGE 116 BLOCKS 1 AND 27 AND ADJUSDR 2004000008Hydraulic System · lowLEFT HYDRAULIC SYSTEM QUANTITY LOW. SERVICED LEFT HYDRAULIC SYSTEM.SDR CA040503011Governor · inoperative(CAN) LT ENG VALVE LIGHT ILLUMINATED AND EICAS MSG L ENG FUEL VAL DISPLAYED WITH FUEL CONDITION SWITCH IN RUN. NO FUEL FLOW INDICATED. LT ENG FFG REPLACED C/O IAW AMM 73-21-01. TEST 1, 2, 9 AND 10 CARRIED OUT SATIFACTORY.SDR CA040316006Wire · chafed(CAN) RT SPAR FUEL SHUTOFF VALVE CB C1062 ACTIVATED DURING SHUTDOWN AFTER FLIGHT. CB WOULD NOT RESET, AND SPAR VALVE DISAGREEMENT LIGHT ALSO ILLUMINATED. TROUBLESHOOTING REVEALED WIRE HAD CHAFING DAMAGE AT BULKHEAD LOCATED AT STATION PP STN 208.40 VISIBLE BEHSDR CA040303005Brake · contaminated(CAN) NR 5 BRAKE SMOKING ON ARRIVAL. A/C HAS JUST RETURNED FROM PAINT, IT IS SUSPECTED THAT EXCESS FLUID HAD COLLECTED ON THE SURROUNDING AREA OF NR 5 BRAKE. BRAKE AND WHEEL AREA THOROUGHLY CLEANED.SDR ANCF200400003Engine · surgesRT ENGINE SURGE DURING ACCEL (AFTER SELECTING CLIMB THRUST) AT 5000 FT ENG OPERATION ABNORMAL AFTER SURGE. ENG WAS NOT SHUTDOWN. BOROSCOPE INSPECTION WAS PERFORMED IAW AMM 71-00-00/601, FIM 71-06-00, FIG 105A NEGATIVE TEST, THE ENGINE WILL BE REPLACE ON FEBRUSDR AMTA200400020Battery · inoperativeEXTERIOR EMERGENCY LIGHT AT DOOR 1 RIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK POWER SUPPLY IAW MM 33-51-07. OPS CEHCK NORMAL. (M)SDR CNMA200300009Transformer · arcedELECTRICAL (ARCING) AND STRONG FUMES ROWS 20DEF AND 24DEF.SDR AMTA200300589Connector · looseEMERGENCY ESCAPE PATH LIGHTING OUT FROM ROW 1 THROUGH ROW 5. RESEATED LOOSE CONNECTORS AT ROW 5 LIGHT ASSEMBLY, OPS CHECKS GOOD PER AMM 33-51-00. (M)SDR AMTA200300317Duct · damagedEICAS STATUS MESSAGE RIGHT STRUT O/H DET 1 DISPLAYED. REMOVED AND REPLACED RIGHT ENGINE SUPPLY HIGH PRESSURE DUCT IAW MM 36-11-01. OPS CHECK NORMAL. (M)SDR ANCF200300009Service difficultyduring flight from Bogotá to Aruba at cruise engine experienced low oil press, high oil temperature and flamed the engine out and N3 indication went to zero. Engine with windmilling for 25 minutes aprox. and landed in Aruba.PARTIAL ACTIONS:Initial inspection wSDR AMTA200300285Pump · inoperativeRIGHT AFT FUEL BOOST PUMP C/B POPPED. PERFORMED INSULATION RESISTANCE AND BONDING CHECKS PER MM 28-22-03. OPS CHECKED OK. REFERENCE LP 543952 FOR RIGHT AFT BOOST PUMP REMOVED AND REPLACED. (M)SDR AMTA200300155Light · brokenEMERGENCY EXIT LIGHT AT 2R DOOR BROKEN. REMOVED AND INSTALLED EMERGENCY EXIT LAMP ASSEMBLY AS REQUIRED PER MM CHAPTER 33, OPS CHECK GOOD, OK FOR SERVICE. (M)SDR 2003F00091Governor · malfunctioned(ORIG-CLOSED) FLT 864. NR 2 ENGINE MAX POWER IN CLIMB WAS 1.30 EPR, DROPPING TO 1.20 IN CLIMB AT FL 230. EEC/LIMITER OFF NO HELP. AIRCRAFT CONTINUED. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE FUEL FLOW GOVERNOR IAW AMM. LEAK CHECKS GOOD, COMPLIED WITH SDR 2002F01017Duct · failed(ORIG-CLOSED) FLIGHT NUMBER 790. DURING CRUISE EICAS STATUS MESSAGE "R STRUT OH DET 1" DISPLAYED. MAINTENANCE REMOVED AND REPLACED HIGH PRESSURE DUCT, MESAGE ERASED AND REMAINED OFF ON ENGINE RUN. AIRCRAFT RETURNED TO SERVICE.SDR 2002F01018Engine · vibration(ORIG-CLOSED) FLIGHT NUMBER 159. AFTER STARTING RIGHT ENGINE-VIBRATION HEARD AND FELT THROUGHOUT AIRCRAFT AT IDLE POWER. VIBERATION GOES AWAY WHEN POWER ADVANCED. MAINTENANCE PERFORMED TEST NR 10 HIGH/LOW IDLE CHECK PER MM 71-00-00, NO FAULTS FOUND. PERFORMED SDR 2002F00995Controller · inoperative(SUPP-CLOSED) FLIGHT NUMBER 73. DURING CRUISE LEFT PACK TEMP EICAS MESSAGE AND PACK INOP LIGHT ILLUMINATED IN AUTO MODE/MANUAL MODE OPERATES NORMAL. MAINTENANCE REMOVED AND REPLACED LEFT PACK TEMP CONTROLLER PER MM 21-51-14-4. OPERATIONAL CHECKS NORMAL.SDR 2002F00976A/C Pack · malfunctionedFLIGHT NUMBER 73. DURING CRUISE LT PACK TEMP EICAS MESSAGE AND PACK INOPERATIVE LIGHT ILLUMINATED IN AUTO. MANUAL MODE OPERATES NORMAL.SDR 02102802Computer · malfunctionedSPOILER CONFIGURATION LIGHT AND HORN ON TAKEOFF. ABORTED TAKEOFF, RETURNED TO GATE TO RESET COMPUTER AND CHECK. PERFORMED SPOILER SYSTEM OPS CHECK AS PER M/M. OPS CHECK NORMAL, NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICESDR O2102801Light · inoperativeFOUND FIRST THREE FLOOR EMERGENCY EGRESS LIGHTS OUT NEAR LAVATORY F. RELAMPED, OPS CHECK NORMAL AS PER M/M 33-51-11.SDR CA021110002Bolt · sheared(CAN) DURING WALK AROUND INSPECTION, A MAIN WHEEL WAS FOUND WITH ONE TIE BOLT MISSING AND TWO OTHERS NOT SAFE (TORQUE WISE). THEY COULD BE ROTATED USING HAND FORCE. ALL THE BOLTS AFFECTED WERE SIDE BY SIDE. UPON FURTHER INVESTIGATION THE FINAL FINDINGS WERE: 1
Back to Boeing 757-28A