Boeing 757-2G5
Service difficulty reports · 557
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 = '7572G5' 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 = '7572G5' 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 FDEA202007091480Floorbeam · crackedMAIN DECK FLOOR BEAM CRACKED, BS 580 BELOW SEAT TRACK LBL 44.5. TRIMMED UPPER FLANGE OF THE FLOORBEAM SPLICE, FABRICATD A REPAIR ANGLE , RADIUS STRAP, AND INSTALLED IAW EA TF-5310-T0355035 P1.SDR FDEA2020071091480Floorbeam · crackedMAIN DECK FLOORBEAM CRACKED BS 580 BELOW SEAT TRACK LBL 44.5.SDR 2020F00301Doubler · corrodedNR 2 NACELLE STRUT DOOR (443LL) HAS CORROSION ON FWD BOTTOM CORNER ON DOOR LANDING. ACCOMPLISHED REPAIR IAW ENGINEERING ORDER CONTROL 20191, TITLED REPAIR-DOUBLER, INBOARD NACELLE SIDE SKIN PANEL ASSEMBLY NR 2 ENG, PPS 176.25.SDR 2020F00289Support Beam · corrodedNON-ROUTINE 2832N248 DISCREPANCY. LMWW, CORROSION ON FWD LOWER FLANGE OF LT MAIN GEAR DOOR ACTUATOR SUPPORT BEAM STA 1120. CORRECTIVE ACTION, LT WHEEL WELL MAIN GEAR DOOR ACTUATOR SUPPORT REPAIRED IAW FVCI EO CONTROL 20184.SDR 2020F00275Keelbeam · corrodedAIRBORNE/PEMCO NON-ROUTINE 2832N241 DISCREPANCY: CORROSION ON KEEL BEAM LOWER SURFACE NLEFT CHORD AT STA 1170 CORRECTIVE ACTION: REPAIRED PER FVCI E.O. #20174SDR 2020F00319Floor Support · corrodedFWD WET AREA, FLOOR SUPPORT BETWEEN BS 324 AND 345 CORRODED AT RBL 40. ACCOMPLISHED EO 20215, REPAIR OF SEC. 41 WITHOUT ANY DEVIATIONS.SDR 2020F00302Doubler · corrodedNR 2 NACELLE STRUT DOOR (443LL) HAS CORROSION ON FWD BOTTOM CORNER ON DOOR LANDING. ACCOMPLISHED REPAIR IAW ENGINEERING ORDER CONTROL 20191, TITLED REPAIR-DOUBLER, INBOARD NACELLE SIDE SKIN PANEL ASSEMBLY NR 2 ENG, PPS. 176.25.SDR 2020F00330Service Panel · corrodedFWD LAV SVC PANEL INSIDE ALL FASTENER ARE CORRODED AND 2EA COVER PLATES HAVE CORROSION. REMOVED AND REPLACED FASTENERS AND FABRICATED 2EA COVER PLATES ON 2832N1011, ACCOMPLISHED EO 20195 ON N/R 2832N245 WITHOUT ANY DEVIATIONS.SDR 2020F00328Panel · corrodedNON-ROUTINE 2832N283, NR 1 ENG ZONE 433 NACELLE STRUT MID STRUCTURE O/B PANEL, LWR AFT CORNER; FOUND EXCESSIVE CORROSION. REPAIRED NR 1 ENGINE NACELLE STRUT MID STRUCTURE O/B PANEL, ACCOMPLISHED REPAIR ON ENGINEERING ORDER 20192, WITHOUT ANY DEVIATIONS.SDR 2020F00299Keelbeam · corrodedNON-ROUTINE 2832N258 DISCREPANCY. RMWW, CORROSION ON KEEL BEAM RIGHT CHORD UPPER SURFACE IN RADIUS OF TAB THAT ATTACHES TO STA 1120 GEAR DOOR ACTUATOR SUPPORT BEAM. CORROSION RUNS UNDER SUPPORT BEAM. CORRECTIVE ACTION. REMOVED CORROSION ON RT KEEL BEAM CHOSDR 2020F00297Structure · corrodedNWW LOWER CHORD HAS CORROSION BETWEEN RT AFT GEAR DOOR AND HINGE FITTINGS. REMOVED CORROSION ON NWW LWR CHORD RT AFT AREA IAW-B757-200-SRM-53-10-14. GRID MAP LWR CHORD AREA 2 EA AREA ON LWR CHORD, IAW- PRELIMINARY-E.O. CONTROL 20613. HFEC ACCOMPLISHED IAW-NTMSDR 2020F00298Bulkhead · corrodedNON-ROUTINE 2832N271 DISCREPANCY, NWW, STA 263 BLKHD AFT FACE, LOWER CHORD HAS CORROSION FROM STR 26L TO STR 26R. CORRECTIVE ACTION: REPAIRED NWW STA 263 BULKHEAD LOWR CHORD PER EO CONTROL 20172 + 20181.SDR FDEA2020040620689Reservoir · failedR1 DOOR EMERGENCY POWER RESERVOIR HAS NO PRESSURE. REMOVED AND REPLACED EMERGENCY POWER RESERVOIR REF B757 AMM 52-11-30-4. OPS CHECK SATIS. A/C OK TO CONT SERVICE. RII BYSDR FDEA2019122313275Collar · inoperativeGUST LOCK ON L FWD ENTRY DOOR WILL NOT MOVE TO ALLOW DOOR TO CLOSE. REF MM 52-11-08-08, INSTALLED NEW HOLD OPEN LOCK COLLAR ON L1 DOOR. L1 DOOR HOLD OPEN LOCK COLLAR OPERATES NORMALLY. PART INSTALLED PN 10-N6008-1 / SN 20-024.SDR FDEA2019110762899Circuit Card · malfunctionedDURING CLIMBOUT GOT STATUS MESSAGE L ENG OH LP2 PER CREW REPORT , STATUS MESSAGE WENT OUT ON LANDING. NO STATUS MESSAGE SHOWN. TROUBLESHOT PER 757 FIM 26-11/802 BLOCK 103. SYSTEM BITE SHOWED NO FAULTS. PER BLOCKK 103 REMOVED AND REINSTALLED AFOLTS CARD MSDR FDEA2019061741301Bottle · emptyFOUND POWER ASSIST RESIVOUR FOR L1 DOOR BLOWN. REMOVED AND REPLACED L1 DOOR ASSIST BOTTLE PER AMM 52-11-30-4-0 NOMENCLATURE-CYLINDER, EMERGENCY POWER RESERVOIR, /N 803300-35A, S/N 1394SDR FDEA201905171088Collar · brokenUNABLE TO CLOSE LEFT ENTRY DOOR L1 DOOR GUSLOCK HOLD OPEN COLLAR BROKEN INSTALLED SERVICEABLE HOLD OPEN LOCK COLLAR ON L1 DOOR CPN 5217125 REF; AMM 52-11-08-8, PERFORMED SATISFACTORY OPERATIONAL CHECK, REMOVED MEL. CONT. 7185890.SDR FDEA2019022860509Hose · defectiveL HYD SYS PRESS LIGHT ILLUMINATED ON FINAL AFTER LANDING GEAR DOWN AND LOCKED AND FLAPS AT FINAL CONFIGURATION. FOLLOWED BY L HYD SYS PRESS AND L YAW DAMPER. CLEARED RUNWAY AFTER LANDING- MAINT TOW TO GATE . REMOVED AND REPLACED DEFECTIVE FLEX HOSE OSDR FDEA201902150425Shoulder Belt · malfunctionedFIRST OFFICER SHOULDER HARNESS WILL NOT RETRACT ALL THE WAY. TRY TO ENGAGE & DISENGAGE SHOULDER LOCK BUT NO HELP. REMOVED & REPLACED FIRST OFFICERS SEAT ASSY. REF 757 AMM 25-11-01-2 . OPS CHECK OK.SDR FDEA201901210187Skin · crackedLEFT O/B MAIN FLAP HAS A PUNCTURE IN COMPOSITE SKIN ON UPPER SURFACE INBD OF 2ND AFT FLAP TRACK. REPAIRED LEFT O/B MAIN FLAP PUNCTURE IN COMPOSITE SKIN ON UPPER SURFACE INBD OF 2ND AFT FLAP TRACK IAW 51-70-17 P4B, & SRM 57-53-01-2R REPAIR 1, TABLE III, SRM 51-SDR FDEA201901210188Structure · puncturedLT WING INBD MAIN FLAP INTERNAL STRUCTURE HAS 4EA PUNCTURES IN THE HONEYCOMB, VIEW THRU OUTBD UPPER ACCESS PNL, INTERNAL INBD LOWER END AREA. REPAIRED LT WING INBD MAIN FLAP INTERNAL STRUCTURE 4EA PUNCTURES IN THE HONEYCOMB IAW SRM 57-53-01-2R REPAIR 1, DETAILSDR FDEA201901190173Stringer · corrodedWHILE REMOVING A DOMENUT AT BS1340 STR23L FOUND STRINGER TO BE CORRODED. EVALUATED STRINGER AT BS 1340 STR 23L FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGE AREA IAW SRM 53-00-03-1A FIG 101 DETAIL II AND 53-00-03-2R FIG 201 DET II REPAIR 1. FABRICATED NEW STRINGERSDR FDEA201901150136Stringer · crackedCABIN BS 1440 STR 4LT. UPPER EDGE IS CRACKED PERFORMED STRINGER REPAIR AT STR 4L FROM BS 1424 TO BS 1456 IAW SRM 53-00-03 03-2R FIG 201 DETAIL II REPAIR 2. DAMAGE DIM OF STRINGER 26.1".SDR FDEA201901100083Floorbeam · crackedCRACK FORWARD CARGO CEILING LBL 45 STA 580 MAIN CABIN FLOORBEAM "T" CAP ON THE RADIUS. DOT 88-001 REMOVED DAMAGED SECTION OF THE LT BS580 LBL45 "T" CORD. FABRICATED ANGLE AND RADIUS STRAP INSTALLED REPAIR PARTS IAW EA 5310-T0344538 P1. COMPLIED WITH FUSELAGE -SDR FDEA201811123187Shim · migratedRT PYLON UPPER AFT DRAG LINK SPAR FITTING SHOWS SIGNS OF SHIM MIGRATION. COMPLIED WITH EA F-5740-T0343112 PART 1. RT WING DRAG FITTING TO WING UPPER SKIN SHIM MIGRATION REPAIR.SDR FDEA201810303054Skin · crackedCRACK LIKE INDICATION WAS NOTED AROUND AND BELOW FASTENER DURING NDT INSPECTION OF REPAIR AREA AT BS 1360 APPROX 4 INCHES ABOVE STR 5L. STRIP/REMOVED PAINT AT MARKED AREA FOR FURTHER NDT INSPECTIONS OF THE AREA. COMPLIED WITH EA F-5330-T0343048 P1. FUSELAGE SKSDR FDEA201810283036Floorbeam · crackedSUB BEAM AT STA 580 IS CRACKED. TRIMMED ENTIRE UPPER FLANGE OF THE BS 580 FLOOR BEAM SPLICE. FABRICATED REPAIR ANGLE AND RADIUS STRAP AND INSTALLED IAW EA F-5310-T0343027 P-1.SDR FDEA20181113017Skin · corrodedCORROSION FOUND AFT LOWER SKIN, APPROX @ WSTA-681.50 RIGHT WING AFT OF FUEL VENT PANEL. ALL WORK ACCOMPLISHED IAW FEDEX EA F-5730-T0343147 P1 WINGS - PLATES AND SKINS - RH WING LOWER SKIN CORROSION AT TRAILING EDGE, WSTA 711.50 RH WING LOWER SKIN CORROSISDR FDEA201810162904Light · inoperativeEMER LIGHTS "UNARMED" LIGHT DOES NOT ILLUMINATE WHEN SWITCH IS OFF. REMOVED AND REPLACED UNARMED LIGHT BASE ASSY MANUFACTURER PN 434-1031-2001 CPN 3312041 REF AMM 33-16-02-2. LIGHT OPS CHECKS NORMAL. A/C OK FOR SERVICE.SDR IXXA20180405015Spar Cap · corrodedCORRODED UPPER AFT SPAR CAP AT LEFT WS 180. REPAIRED THE SPAR CAP IAW 47313REA05.SDR IXXA20180403014Support Beam · corrodedPANEL SUPPORT BEAM INBD OF PANEL 197BL IS CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04. REMOVED AND REPLACED IAW DWG 149N7550, AND SRM 51-40-02, PARA 7. AIRCRAFT GROUNDEDSDR IXXA20180423019Stiffener · corrodedRIGHT MLG WW BS 1040 BULKHEAD ABOVE ECS DUCT,STIFFENER IS CORRODED AT FASTENER. REMOVED & REPLACED THE CHANNEL STIFFENER IAW SRM 51-40-02 & 58-757-35-0024.SDR IXXA20180409017Tube · crackedNR 1 PYLON AFT MOUNT BARREL NUT FWD GUIDE TUBE IS CRACKED, LANYARDS ARE NOT SECURE. REPAIRED THE MOUNT BARREL NUT FWD GUIDE TUBE IAW AMES 47313REA01 AND SECURED THE LANYARDS IAW AMM 71-21-03.SDR IXXA20180409016Web · corrodedLWR KEEL WEB HAS AREA OF CORROSION AROUND HYD LINE BULKHEAD FITTING JUST FWD AND ABOVE LANDING GEAR DOOR ACTUATOR. REPAIRED THE VERTICAL LWR KEEL WEB IAW REA47313 REA 03.REINSTALLED ABOVE THE GEAR DOOR ACTUATOR. LEAK CHECKED IAW IAW AMM 29-11-00. ACFT GROUNSDR IXXA20180403013Skin · corrodedRT OTBD FORE FLAP LOWER SURFACE HAS 2 SMALL AREAS OF CORROSION OTBD OF THE OTBD SUPPORT MECHANISM. REPAIRED THE AREAS OF CORROSION ON THE RT WING OTBD FORE FLAP LOWER SURFACE IAW SRM 57-53-01, REPAIR 5, FIG 201. AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE.SDR FDEA201803010538Fseu · malfunctionedDURING CRUISE, HAD A TE FLAP ASYMETERY EICAS MESSAGE. PERFORMED QRH PROCEDURE AND LANDED FLAPS UP. HAPPENED AFTER ABOUT 1.5 HOURS IN MODERATE TO LIGHT TURBULANCE. TROUBLESHOT IAW FIM 27-51, FAULT TREE 803. FOUND THE NR 1 FSEU FAULT, LEFT WING ASYMETERSDR FDEA201802130379Collar · crackedL1 DOOR HOLD-OPEN LOCK COLLAR CRACKED. REMOVED AND REPLACED THE L1 DOOR HOLD OPEN LOCK COLLAR AND CATCH IAW AMM 52-11-08-08.SDR FDEA201801300276Sensor · malfunctionedDURING CRUISE, NOTICED THE SLIDE LIGHT FOR THE L1 DOOR WAS EXTINGUISHED. REPLACED THE SENSOR IAW AMM 25-66-11-4. OPS CHECKED GOOD.SDR IXXA2017ATN254Battery · inoperativeL4 INBOUND FLASHLIGHT BATTERY DEAD. REMOVED AND REPLACED THE BATTERY IAW AMM 25-60-00.SDR FDEA201708112188Cover · dislodgedLEFT FWD ENTRY DOOR SLIDE COVER DISLODGED. IAW MM 25-66-01-4, REINSTALLED THE SLIDE COVER. OK FOR SERVICE.SDR IXXA20170807268Battery · inoperativeCAPTAIN'S EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT BATTERIES IAW AMM 25-64-00. OPS CHECKED SATISFACTORY. AIRCRAFT RELEASED TO SERVICE.SDR FDEA201707282079Adc · malfunctionedAFTER TAKEOFF, LOST MULTIPLE AVIONICS, PILOTS ALTITUDE, AIRSPEED, RADIO ALTIMETER, AUTOTHROTTLES. FIRST OFFICER`S FLT DISPLAY WAS SIMILAR BUT REGAINED AIRSPEED, ALTITUDE, BUT NO AUTOTHROTTLES. LAST FLIGHT FAULTED ADC SYS L WITH FAULT CODES 110401, AND 13040SDR FDEA201707282078Landing Gear · malfunctionedAFTER TAKE OFF, PUT GEAR UP. GEAR RETRACTED. WHEN GEAR HANDLE WAS PUT TO OFF, GEAR CAME DOWN. PUT GEAR DOWN FOR LANDING AND RECEIVED GOOD DOWN INDICATION. PERFORMED A BITE OF THE PSEU AND FOUND NO FAULTS ON THE BOX IAW AMM 32-09-06, STEP 4. E. JACKED AIRSDR FDEA201706201720Collar · brokenL1 HOLD OPEN LOCK IS BROKEN. REPLACED HOLD OPEN COLLAR HALVES AND CATCH ASSEMBLY IAW AMM 52-11-08-8. OK FOR SERVICE.SDR FDEA201703160941Pressure Switch · defectiveDURING DESCENT HAD SPOILERS EICAS WITH ASSOCIATED SPOILERS LIGHT OVERHEAD FELT SLIGHT ROLL TO RIGHT. REMOVED AND REPLACED HYDRAULIC PRESSURE SW (S27) PER AMM 27-11-17-4. REACTIVATED SPOILERS 5 & 8 AND OPS CHECKED SPOILER SYSTEM PER AMM 27-61-00-5; OPS CK WAS NSDR IXXA20170310155Compressor · stalledIN FLIGHT EMERGENCY DECLARATION. AIR TURN BACK. 5 COMPRESSOR STALLS/SURGES WITH ENGINE EXCEEDANCE VALUES RECORDED. INDICATIONS RETURNED TO NORMAL THEREAFTER AND PRIOR TO LANDING. AIRCRAFT GROUNDED FOR BORESCOPE INSPECTION AND FURTHER ANALYSIS. WORK IN PROGRESSSDR IXXA20170217153Skin · dentedSKIN DENTED BETWEEN BS 1701 AND 1720, STRINGER 11 TO 16L. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIGURE 101. REPAIRED THE AREA IAW ENGINEERING DOCUMENT 47255REA01.SDR FDEA201612064327Gust Lock · malfunctionedFOUND THAT L1 DOOR GUST LOCK DOES NOT ENGAGE WHEN DOOR IS PLACED IN FULL OPEN POSITION. R & R THE L1 DOOR HOLD OPEN LOCK COLLAR IAW MM 52-11-08-4. OK FOR SERVICE.SDR FDEA201610013404Floorbeam · crackedSTUB FRAME BS 580 LBL 44-46 CRACKED. REMOVED AND REPLACED FLOORBEAM SECTION REINFORCEMENT STUB FRAME IAW DWG 657N4311 REV - AND SRM 51-40-05-0G, 51-40-02-0G. MAJOR REPAIR.SDR FDEA201607292656Hinge · dirtyLEFT CABIN DOOR HARD TO CLOSE. FOUND DEBRIS IN DOOR HINGE. CLEANED AND OPERATED THE DOOR SEVERAL TIMES IAW AMM 52-11-00-2, NO DEFECTS NOTED.
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