Boeing 757-23A
Service difficulty reports · 1,397
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 = '75723A' 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 = '75723A' 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 FDEA201708032103Seat Track · corrodedMDCC BS 1180 - 1200, RBL 45.5 SEAT TRACK CORRODED. FABRICATED A NEW SEAT TRACK IAW DWG 146N5130. REPLACED THE SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201708032101Seat Track · corrodedMDCC BS 1080 - 1180, LBL 45.5 SEAT TRACK CORRODED. FABRICATED A NEW SEAT TRACK IAW DWG 144N5021. REPLACED THE SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201707222019Slider · bindingLEFT CREW DOOR WILL NOT ARM IAW AMM 52-11-25-5 ADJUSTMENT AND TEST. FOUND THAT THE GIRT BAR SLIDERS WHERE CATCHING ON THE FLOOR FITTINGS. ADJUSTED THE FLOOR FITTING INBOARD AND OPS CHECKED THE DOOR LOCKING AND ARMING SYSTEM.. OPS CHECKED GOOD. ACFT OK FORSDR FDEA201707212725Floorbeam · corrodedEVIDENCE OF CORROSION FOUND AT LBL 2.90 FLOORBEAM LOCATED AT AFT CARGO COMPARTMENT BETWEEN BSTA 1330 AND 1440 APPROX. CARRIED OUT REPAIRS TO FLOORBEAM AT BSTA 1330 AND 1365 LBL 2.9 IAW SRM 53-00-53 REPAIR 1.SDR FDEA201707212716Floor Support · corrodedCORROSION FOUND ON THE RBL 16.1 FLOOR SUPPORT IN THE AFT CARGO BAY BETWEEN BS 1330 AND 1440. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, REV 121.SDR FDEA201707212715Floor Support · corrodedRBL 16.10 FLOOR SUPPORT IN THE AFT CARGO BAY BETWEEN B 1330 AND 1440 CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, REV 121.SDR FDEA201707061860Bottle · low pressureFOUND THE L1 DOOR ASSIST BOTTLE PRESSURE LOW R & R THE L1 DOOR ASSIST BOTTLE IAW AMM 52-11-30-4.SDR FDEA201707011813Fitting · out of adjustL1 DOOR HARD TO ARM FOR FLIGHT. ADJUSTED THE GIRT BAR FLOOR FITTINGS IAW AMM 52-11-25-5-0. DOOR SLIDE ARM HANDLE OPS CHECKED GOOD. ACFT OK FOR SERVICE.SDR FDEA201706301841Skin Panel · corrodedLT HORIZ STAB LOWER I/B PANEL HAS CORROSION TO OUTER SKIN 8" FROM I/B EDGE. T/E REPAIRED IAW EA F-5510-T0333919 A P3.SDR FDEA201706301788Hydraulic System · leakingINFLIGHT EICAS LT HYD QTY INDICATED 0.45. QUANTITY CONTINUED DECREASING AND LOST ENTIRE L HYDRAULIC SYSTEM AFTER LANDING ROLLOUT, NO NLG STEERING AVAILABLE. OPENSDR FDEA201706261763Life Raft · out of positionL1 DOOR WILL NOT OPEN PAST INITIAL UNLATCH. FOUND THE LIFE RAFT NOT IN THE PROPER POSITION, ADJUSTED THE RAFT IAW MM 25-66-01/401. ACFT OK FOR SERVICE .SDR FDEA201706231749Skin · damagedDURING WALKAROUND, FOUND DAMAGE TO LOWER LT STABILIZER SKIN, APPROXIMATELY 12.5 INCHES LONG AND 7 INCHES IN WIDTH. FOUND HONEYCOMB EXPOSED 0.5 IN DIAMETER. PERFORMED A TEMPORARY REPAIR IAW EA F-5510-T0333837.SDR FDEA201706131635Indicator · obstructedARMING INDICATION IS NOT POPPING OUT CORRECTLY. IT WAS CORRECTLY INDICATING AT PUSH BACK. BUT TOOK A FEW TRIES. FOUND THAT THE L1 DOOR ARM INDICATOR STICKER WAS SNAGGING ON THE DOOR COVER EDGE. CLEANED STICKER AND CLEANED THE OPENING EDGE ON THE DOOR LSDR FDEA201705261520Slide · out of adjustAT BLOCK IN , WHEN FIRST OFFICER TRIED TO OPEN RT SIDE DOOR, IT MET WITH RESISTANCE. MX FOUND THE R1 SLIDE RAFT DROPPED AND TOUCHING THE LOWER VENT DOOR CREATING FORCE TO OPENED THE DOOR . R1 SLIDE RAFT ADJUSTED IAW MM 25-66-00-5. OPS CHECKED OK, DOOR OSDR FDEA201705051360Pdu · trippedTE FLAP DISAGREE MESSAGE AFTER SELECTING FLAPS 20 ON VISUAL APPROACH. QRH COMPLETED AND LANDED FLAPS 20. TROUBLESHOT TE FLAP DISAGREE IAW FIM 27-51 FT 808. FOUND LEFT INBOARD PDU OVERLOAD INDICATOR TRIPPED. BITE CHECKED ALL 3 FSEU'S AND NO FAULTS WERE FSDR FDEA201704281295Stiffener · crackedRT WW AFT PRESSURE BULKHEAD LWR INBD STIFFENER CRACKED. REMOVED THE STIFFENER LOCATED, DRILLED NEW AND INSTALLED IAW SRM 51-40-02-0G AND SRM 51-40-05-0G.SDR FDEA201704201244Skin · dentedFUSELAGE SKIN HAS THREE PROTUDING DENTS IN EXTERNAL SKIN LOWER FUSELAGE AT BS 520 AND TWO INCHES INBD OF STRINGER 26L. SKIN REPAIRED IAW EA F-5330-T0332752 P1.SDR FDEA201704111131Flap System · malfunctionedDURING FINAL APPROACH, EXTENDED FLAPS 15 TO 20, FLAPS STUCK AT 17 DEGREES. RECEIVED A TE FLAP DISAGREE EICAS MESSAGE. DECLARED AN EMERGENCY PERFORMED QRH. UNEVENTFUL SECOND APPROACH. BITE FSEU NR 1, RECEIVED A FAULT CODE 305. FOLLOWED FIM AND PERFORMED ISDR FDEA201704041093Proximity Sensor · dirtySLIDE ARMED LIGHT ON R1 DOOR WOULD NOT ILLUMINATE. REPLACED THE BULB, WORKED INTERMITTENT IAW AMM 33-20-00. CONTACTS CLEANED AND DEBRIS REMOVED FROM GIRT BAR PROXIMITY SWITCHES ON FLOOR. ALL OPS NOW GOOD.SDR FDEA201703210965Spoiler · damagedSPOILER NR 3 TRAILING EDGE DAMAGE DUE TO CONTACT WITH LOOSE SCREW ON TRAILING EDGE FLAP. REPLACED SPOILER NR 3 IAW AMM 27-61-01.SDR FDEA201701200230Indication Sys · malfunctionedSIGNIFICANT DISCREPANCY BETWEEN CAPTAIN`S AND FIRST OFFICER MINIMUM MANEUVERING SPEED INDICATORS AT 5000 FT, THERE WAS A 10KNOT DIFFERENCE, FO'S INDICATING A HIGHER MMS. THERE WAS A 10KNOT DIFFERENCE WITH THE STALL WARNING INDICATOR. AIRSPEED ON BOTH PFD'S SDR FDEA201701160218Lamp · inoperativeIN COURIER AREA, RIGHT SLIDE LIGHT IS INOPERATIVE. REPLACED THE LAMP IAW AMM 33-16-02-2. OPS CHECKED GOOD.SDR FDEA201612304580Module · inoperativeDURING DECENT, AUTOPILOT FAILED TO CAPTURE ALTITUDE (5000'). ALT WARNING WORKED. R&R THE STAB TRIM ASSY MODULE, PASSES MCDP TEST 65 AS WELL AS MCDP GROUND TEST 30 AND AUTOLAND TEST 40. RESET 30 DAY TIMER, OK FOR SERVICE. IAW AMM 27-09-00-2, 22-00-00-2.SDR FDEA201612164471Module · malfunctionedAFTER LANDING, COMING OUT OF TURN ONTO TAXIWAY, NOSE WHEEL STEERING WAS UNRESPONDING FEELS AS THOUGH NWS TILLER WAS BINDING. PERFORMED RIGGING CHECK AND SYSTEM TEST OF NOSE WHEEL STEERING IAW MM 32-51-00-5-3. TEST PASSED 3 TIMES. TILLER MOVES NORMALLY LSDR FDEA201612144446Control Panel · failedDURING PREFLIGHT, FOUND OVERHEAD EMERGENCY LIGHT SWITCH INOP. REPEAT WRITE UP. SWAPPED EMERGENCY LIGHT/PASENGER OXY CONTROL PANEL PER MM 33-51-08-4. PERFORMED TEST PER MM 33-51-00-05.SDR FDEA201612144426Module · defectiveREPEAT WRITE UP-UNARMED LIGHT DOES NOT ILLUMINATE WHEN COCKPIT OVERHEAD EMERGENCY LIGHTS SWITCH PLACED TO OFF POSITION. R&R BOTH OF FUSE DIODE MODULE AND LENS CAP ASSEMBLY PER STANDARD WIRING PRACTICES MANUAL 20-84-18. OPS CHECK GOOD. A/C OK FOR SERVICE.SDR FDEA201612144425Light · not seatedEMERGENCY EXIT 'UNARMED' LIGHT DOES NOT ILLUMINATE WHEN EMERGENCY LIGHT SWITCH IS POSITIONED TO OFF. LIGHT CHECKS OK WHEN LIGHTS ARE TESTED, ITS NOT A BURNT OUT BULB. EMERGENCY 'UNARMED' CAUTION LIGHT FILAMENTS RESEATED. EMERGENCY LIGHTS TESTED FROM PILOTS SDR FDEA201612094365Door · lack of lubeL1 CABIN DOOR VERY DIFFICULT TO MOVE, OPEN, AND CLOSE AFTER BLOCK IN AT GATE. CLEANED AND LUBED THE L1 DOOR. OPERATES NORMAL IAW MM 52-11-00-2. ACFT OK FOR SERVICE.SDR FDEA201612064341Flap System · malfunctionedDISAGREE ON DESCENT & APPROACH AFTER SELECTING ALT FLAPS 20 TEF EICAS RESOLVED, TWO MORE APPROACHES FLOWN WITH NORMAL FLAP OPERATION. FOUND NO RELATED EICAS MESSAGES FOR THIS FAULT, PERFORMED A READOUT OF EXISTING FAULTS AT FSEU NR 1 & 2, NO FAULTS RECORDSDR FDEA201612044320Idg · inoperativeRIGHT GENERATOR DROPPED OFFLINE ON 2 MILE FINAL AND LANDING, AUTOTHROTLLE LOST ELECTRICAL POWER AND RIGHT UTILITY BUSS WENT OFFLINE. STARTED APU WHICH RESTARTED POWER. HOWEVER, APU DROPPED OFFLINE ENTERING PARKING. ACFT THEN WOULD NOT ACCEPTE EXTERNAL POWERSDR FDEA201611224199Frame · dentedAFT CARGO FRAME AT BS 1340 HAS A DENT BETWEEN STRINGERS 25L AND 26L. REPAIRED IAW EA F-5310-T0329984 P1. MAJOR REPAIR.SDR FDEA201611224200Frame · dentedAFT CARGO BAY FRAME AT BS 1420 HAS A DENT ABOVE STRINGER 26L. COMPLIED WITH EA F-5310-T0329906 P1.SDR FDEA201611154022Web · corrodedMAIN CARGO WEB AT BS 4121 RBL 67, FOUND CORRODED, UPPER RT CORNER. REMOVED AND REPLACED THE WEB IAW DRAWING 146N5590 REV E.SDR FDEA201611154028Girt Bar · dirtyR1 DOOR - UNABLE TO DISARM THE SLIDE. FOUND DIRT AND TRASH AT THE GIRT BAR SLIDE MECHANISM. REMOVED,CLEANED AND LUBRICATED THE GIRT BAR MECHANISM IAW AMM 12-21-18-3. OPS CHECKED GOOD IAW AMM 25-66-00.SDR FDEA201611093907Cover · unsecureLIFE RAFT COVER ON L1 DOOR SEPERATED. THE COVER SECURED IAW AMM 25-66-01-4.SDR FDEA201610243680Skin · damagedLEFT ELEVATOR DAMAGED ON UPPER SURFACE. REPAIRED IAW EA F-5520-T0329101 P1.SDR FDEA201610213674Skin · damagedLIGHTNING STRIKE ON FUSELAGE SKIN AT BS 402, 1.5'' ABOVE 24R REPAIRED LIGHTNING STRIKE IAW SRM 53-00-01, FIG 201, REPAIR 6, SECTION I, REV 118.SDR FDEA201610213673Skin · damagedLIGHTNING STRIKE AT BS 282, 29'' BELOW LAPJOINT STR 20R. REPAIRED LIGHTNING STRIKE IAW SRM 53-00-01, FIG 201, REPAIR 6, SECTION I, REV 118.SDR FDEA201610213672Skin · damagedLIGHTNING STRIKE AT BS 535, 2.5'' ABOVE STR 23 RT. REPAIRED LIGHTNING STRIKE IAW SRM 53-00-01 FIG 201, REPAIR 6 ,SECTION I, REV 118.SDR FDEA201610213671Skin · damagedLIGHTNING STRIKE AT BS 692, 1.5'' BELOW STR 21R. REPAIRED LIGHTNING STRIKE IAW SRM 53-00-01 FIG 201, REPAIR 6, SECTION I REV 118.SDR FDEA201610213670Skin · damagedLIGHTNING STRIKE AT BS 329, 1.5'' ABOVE STR 24 RT. REPAIRED LIGHTNING STRIKE IAW SRM 53-00-01 FIG 201 REPAIR 6 SECTION I REV 118.SDR FDEA201610213669Skin · damagedLIGHTNING STRIKE AT BS 370, 1.5'' ABOVE STR 24RT. REPAIRED LIGHTNING STRIKE IAW SRM 53-00-01 FIG 201 REPAIR 6, SECTION I REV 118.SDR FDEA201610213668Skin · damagedLIGHTNING STRIKE AT BS 409, 1.5'' ABOVE STR 24R. REPAIRED LIGHTNING STRIKE IAW SRM 53-00-01 FIG 201, REPAIR 6 SECTION I REV 118.SDR FDEA201610113681Wedge · delaminatedDELAMINATION FOUND IN THE RT OTBD SLAT NR 7 T/E WEDGE UPPER AND LOWER SURFACE AT IB END. REMOVED AND REPLACED IAW AMM 27-81-02 ACCOMPLISHED EA F-5750-T0329030.SDR FDEA201610053475Spring · out of positionMECHANICAL ARMED INDICATOR ON R1 DOOR INOPERATIVE. TROUBLESHOT IAW MM 52-11-20-5, FOUND ON R1 DOOR RETRACTABLE DOOR MECHANISM SPRING INOPERATIVE. FOUND THE SPRING WAS NOT CORRECTLY POSITIONED. SPRING REPOSITIONED IAW AMM 52-11-20-5.SDR FDEA201610043454Girt Bar · damagedL1 DOOR SLIDE ARMED LIGHT WILL NOT ILLUMINATE. THE GIRT BAR WILL NOT FULLY ENGAGE. R & R THE GIRT BAR IAW MM 25-66-10-2. PERFORMED ADJUSTMENT AND TEST IAW MM 25-66-11-2 . OPS CHECKED GOOD.SDR FDEA201610043457Proximity Sensor · inoperativeESCAPE SLIDE ARMED LIGHT FAILED TO ILLUMINATE WHEN THE LEFT DOOR WAS CLOSED, LOCKED AND THE SLIDE WAS ARMED. R & R THE GIRT BAR FWD PROXIMITY SENSOR IAW AMM 25-66-11-2. TEST PASSED.SDR FDEA201608263041Lanyard · unsecureATTACHING LANYARD ARE HANGING OUT OF THE R FWD DOOR SLIDE HOUSING. THE DOOR SLIDE ROPE PUT BACK IN NORMAL POSITION IAW AMM 25-66-00-2. ACFT OK FOR SERVICE.SDR FDEA201605311771Girt Bar · misalignedDOOR 1R WOULD NOT CLOSE & LATCH PROPERLY. REINSTALLED GIRT BAR IAW AMM 25-66-10-2. OPERATION CHECKED OK. ACFT OK TO CONTINUE.SDR FDEA201605251730Steering Sys · out of rigDURING TAKEOFF, AFTER ENGAGING THE THRUST TILE, THE ACFT WOULD NOT HOLD CENTERLINE. REJECTED TAKEOFF 08 L CDG. BOTH THRUST LEVERS WERE ALIGNED, RUDDER & AILERON WERE CENTERED. TROUBLE SHOT IAW FIM 32-51 TASK 802 & FOUND NOSE WHEEL STEERING NOT PROPERLY RIGG
Back to Boeing 757-23A