Boeing 757-231
Service difficulty reports · 1,658
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 = '757231' 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 = '757231' 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 DALA1122626817Charger · inoperativeDURING A LAYOVER CHECK, MAINTENANCE FOUND A CEILING EMERGENCY EXIT SIGN AT ROW 34 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. OPERATIONAL CHECK WAS GOOD.SDR FDEA201103231184Skin · damagedFUSELAGE SKIN BETWEEN BS 1620 AND 1630 AT STRINGER 1, AREA HAS TOOLMARKS ON 5 LOCATIONS, AS MARKED AT 12 0'CLOCK. ACCOMPLISHED AND COMPLIED WITH EA F-5330-146390. MAJOR REPAIR.SDR FDEA201102170591Skin · dentedRT, EXTERNAL FUSELAGE AT STA 1655, BETWEEN STR 24R & 25R, HAS A DENT. DENT FOUND OUT OF LIMITS PER SRM 53-00-01, FIG.101, DETAIL 3, PG.104. CLEANED DAMAGED SKIN PER SRM 53-00-01 AT RH EXTERNAL FUSELAGE BY BS 1655, BETWEEN S24-25R. FABRICATED A REPAIR DOUSDR DALA1108846815Switch · malfunctionedDURING FLIGHT, CREW REPORTED EMERGENCY LIGHTING CYCLING ON AND OFF IN VARIOUS LOCATIONS. MX REPLACED THE EMERGENCY LIGHT TEST SWITCH. OPS CHECKS WERE GOOD.SDR FDEA201102020452Skin · crackedRT WING NR9 SLAT, OTBD IDLER ATTACHMENT HARDWARE APPEARS TO HAVE CRACKS COMING FROM FASTENER. COVE SKIN AT ISS 615 TO ISS 663, CRACKED AND FOUND TO BE OUT OF LIMITS, IAW SRM 57-43- 01, FIG 101, DETAIL II, PG 102. REMOVED AND REPLACED COVE SKIN AT ISS 615 TO SDR DALA1108336815Battery Pack · dischargedPILOT REPORTS THE EMERGENCY PATH LIGHTS AT 19DEF THROUGH 26DEF WILL NOT SHUT OFF. MAINTENANCE REPLACED THE BATTERY PACK AT DOOR 2R. OPERATIONAL CHECK WAS GOOD. (2011-D0143)SDR FDEA201101270389Firewall · gougedAPU COMPARTMENT, FIREWALL JUST ABOVE RT DOOR LATCH BRACKET GOUGE IN FIREWALL. GOUGE ON FIREWALL APU WEB FOUND OUT OF LIMITS ORIG. MAT. .016" LOSS .012" REMAINING .004" AS PER SRM 53-80-08 DET. IX FIG 101 P. 109. FABRICATED DOUBLER AS PER SRM 53-80-08 TABLESDR FDEA201101180277Skin · dentedEXTERNAL FUSELAGE SKIN STA 1520-1540 BETWEEN STR 22R TO STR 23R HAS DENT. FOUND OUT LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. CUT-OUT DAMAGE AREA 1.100" LONG X 0.800" WIDE AT STA 1522 BETWEEN STR 22R- STR 23R IAW SRM 53-00-01 REPAIR 16. PERFORMED SURFACSDR FDEA201101150178Stringer · corrodedSTRINGER 22-R INSIDE FWD CARGO COMPARTMENT BS 740-760 HAS CORROSION. REMOVED CORROSION ON S-22R STA 740-760 IAW SRM 51-10-02. BLENDED AREA L=1.5 W=1.0 D=.020. ORIGINAL MATERIAL .071 AFTER REWORK .051. NO ALLOWABLE DAMAGE FOR SF STRINGERS. REPAIRED STRINGER SDR FDEA201101130137Seat Track · gougedMAIN CABIN, STA 418-440, RBL 25, WL 208, SEAT TRACK IS GOUGED. REMOVED GOUGE FROM SEAT TRACK STA 418-440 RBL 25 AND FOUND TO OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL V. R & R SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR.SDR FDEA201101130134Seat Track · gougedMAIN CABIN, STA 418-440, RBL 45,WL 208, SEAT TRACK IS GOUGED. REMOVED GOUGE ON SEAT TRACK STA 418-440 RBL 45 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DETAIL V. R & R SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR.SDR FDEA201101130130Frame · gougedAFT CARGO COMPT FRAME GOUGED AT STA 1480, BETWEEN STR 24R AND 25R, UPPER CHORD SPLICE. REMOVED PRODUCTION SPLICE FROM FRAME BS 1480, S24R/25R, SRM 51-40-02. GOUGES FOUND OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL 2, PG. 103. NEW SPLICE FABRICATED ON TRSDR FDEA201101130132Floorbeam · corrodedMAIN CABIN,STA 377, RBL 11, WL 208, FLOORBEAM TOP STRAP (PLATE) HAS CORROSION. REMOVED CORROSION ON PREVIOUSLY INSTALLED FLOORBEAM REPAIR AT STA 377, RBL 11 IAW SRM 53-0051, REPAIR 3 FOUND TO BE OUT OF LIMITS ARIG MAT 0.125 AFTER REWORK 0.101. REMOVED FLOOSDR FDEA201101110105Floorbeam · corrodedFLOORBEAM, STA 1661, BL 0, WL 208 CORRODED MAIN CABIN. REMOVED CORROSION ON FLOORBEAM, STA 1661, BL 0 IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51. ORIG MATERIAL .125 MATERIAL LOSS .035. R & R STA 1661 FLOORBEAM IAW SRM 51-40-02. CATEGORSDR DALA1111756815Floorbeam · corrodedMAIN DECK FLOORBEAM STA 377.7 HAS LIGHT CORROSION AROUND FASTENERS HOLES BETWEEN BL0-LBL 16. REPAIRED DURING HMV AT SAA ON NRC 176096.SDR DALA1111736815Floorbeam · corrodedMAIN DECK FLOORBEAM STA 365 HAS UPPER FLANGE CORRODED BETWEEN BL0 AND RBL 48. REPAIRED DURING HMV AT SAA ON NRC 176080.SDR FDEA201101070074Angle · corrodedNR 10 SLAT COVE ANGLE CORRODED. REMOVED CORROSION ON NR 10 SLAT IAW SRM 51-10-02. ORIG MATERIAL .063 AFTER REWORK .000 MATERIAL LOSS .063 FOUND OUT OF LIMITS IAW SRM 57-43-02, FIG 101, DETAIL II. L= 131" X W=2" X D=.063. R & R COVE ANGLE IAW SRM 51-40-02. SDR FDEA201101070072Channel · corrodedNLG WHEELWELL FWD BOTTOM "L" CHANNEL AT STA 263 JUST BELOW NLG DOOR UNSAFE LIGHT IS CORRODED. COMPLIED WITH EA F-5310-146250. MAJOR REPAIR.SDR DALA1105126815Girt Bar · corrodedL4 DOOR GIRT BAR RESTRAINT IS CORRODED. REPLACED GIRT BAR RESTRAINT AT SAA. DURING HMV, ON NR CARD 171239.SDR DALA1105076815Girt Bar · corrodedR1 DOOR GIRT BAR RESTRAINT HAS CORROSION. REPLACED GIRT BAR RESTRAINT AT SAA. DURING HMV, ON N/R CARD 181916.SDR DALA1100156810Frame · dentedFWD CARGO FRAME DENTED ON UPPER FLANGE STA 520 FROM 24 TO 25 LT. REPAIRED IAW ER/A 488097-14.SDR DALA1100146810Frame · dentedFWD CARGO FRAME DENTED IN 2 PLACES ON UPPER FLANGE AND RADIUS, STA 540 FROM STR 24 TO 25 LT. REPAIRED IAW ER/A 488006-14 REV, ORIGINAL.SDR DALA1100406810Crease Beam · corrodedMAIN CABIN CREASE BEAM INNER CHORD CORRODED STA 333-377, LT AT L1 DOOR OPENING. REPLACED CHORD.SDR DALA1100306810Frame · dentedFWD CARGO FRAME DENTED STA 660 ON UPPER FLANGE BTWN STR 23 & 24 LT. REPAIRED IAW 53-00-07, FIG 201, REPAIR 5.SDR DALA1100416810Seat Track · corrodedMAIN CABIN SEAT TRACK CRACKED IN FWD LOWER RADIUS STA 521, LBL 24. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR III.SDR DALA1100336810Seat Track · crackedMAIN CABIN SEAT TRACK CRACKED IN FWD LOWER RADIUS STA 521, LBL 24. REPAIRED IAW SRM 53-00-52, FIG 201.SDR DALA1100356810Plate · corrodedMAIN CABIN AFT DECK PLATE CORRODED STA 1680-1720, BL 0-LBL 59. REPAIRED IAW SRM 53-60-51, ALTERNATIVE II, FIG 201, PG 202, STEP 10.SDR DALA1100346810Structure · corrodedMAIN CABIN BL 0 CHORD CORRODED STA 345-377. REPLACED CHORD.SDR FDEA201012104631Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER SURFACE BS700 RBL48 TO RBL58 HAS CORROSION. REMOVED CORROSION FROM BS 700, RBL 48-58, PER SRM 51-10-02. ORIGINAL MATERIAL; .125", MATERIAL LOSS; .046", W=2", L=7". FOUND TO BE OUT OF LIMITS PER SRM 53-00-01, FIG.101, DETAIL 2. CUSDR DALA1100426810Floorbeam · corrodedMAIN CABIN FLOORBEAM HAS AREAS OF CORROSION STA 1640, BL0 TO LBL 62. REPAIRED IAW ERA 481634-14MA.SDR DALA1100466810Bracket · gougedL2 DOOR ESCAPE SLIDE SPADE BRACKETS ARE GOUGED 2 EA. R & R BOTH BRACKETS AFT BRACKET PN416N2201-16, FWD BRACKET PN 416N2201U17SDR DALA1100436810Girt Bar · corrodedR4 GIRT BAR HAS CORRODED RESTRAINT. REPLACED RESTRAINT.SDR DALA1034186814Wire · disconnectedDURING LAYOVER CHECK FOUND EMERGENCY PATH LIGHT INOPERATIVE AT MID GALLEY FWD PARTITION WALL BEHIND SEAT 4D. MX RECONNECTED THE LIGHT ASSY. OPS CHECKS GOOD.SDR DALA1033290723Inverter · malfunctionedON APPROACH, AIRCRAFT EXPERIENCED A STANDBY INVERTER MESSAGE FOLLOWED BY A REPORT OF FUMES IN THE CABIN. WATER HAD BEEN SPILLED IN THE COCKPIT. AN EMERGENCY WAS DECLARED AND LANDING NORMAL. MAINTENANCE REPLACED THE STATIC INVERTER AND THE BATTERY CHARGER. SDR DALA1316766811Floorbeam · corrodedFUSELAGE PASSENGER COMPARTMENT FLOORBEAM BS 365, LBL 9.5 TO RBL 70.5 UPPER TEE CAP CORROSION. REPAIR IAW ERA 486304-14.SDR DALA1016226811Fire · detectedA CARDBOARD FOOD BOX IN AFT OVEN NR 5 IGNITED BRIEFLY AND WAS QUICKLY EXTINGUISHED. DOOR 4R FIRE EXTINGUISHER WAS USED OR SEAL BROKEN. MAINTENANCE INSPECTED OVEN AND NO PROBLEMS WERE FOUND. THE MISSING PIN FOR FIRE EXTINGUISHER WAS REPLACED AND SECURED PER SDR DALA1015966814Engine · bird ingestionNR 2 ENGINE HAD BIRD STRIKE FOLLOWED BY VIBS - DIVERTED TO MAD PERFORMED BIRD STRIKE INSPECTION PER 05-51-18 AMM AIRCRAFT FUSELAGE NO DEFECTS NOTED RT ENGINE SHOWS DAMAGE ON FAN BLADES AND ACOUSTIC LINER (DL75E101749).SDR DALAFAR145SDR101Slide · no testDURING A SCHEDULED C-8 VISIT, AN INTENTIONAL SLIDE DEPLOYMENT WAS SCHEDULED. THE SLIDE AT THE L-3 DOOR FAILED TO INFLATE AUTOMATICALLY WITH THE OPENING OF THE DOOR. HOWEVER ONCE THE MANUAL HANDLE WAS PULLED, THE SLIDE INFLATED PROPERLY.SDR DL75E101187Reservoir · dischargedTHE PRESSURE IN THE EMERGENCY POWER RESERVOIR FOR DOOR 4R WAS FOUND TO BE DEPLETED. THE RESERVOIR WAS REPLACED AND THE SYSTEM WAS RETURNED TO NORMAL OPERATING CONDITION PER MM 52-11-30.SDR DL75E100935Contact · sticksDOORS 1L, 2L, AND 3L EXTERIOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND DOOR 1L AND 3L LAMP ASSEMBLIES CENTER CONTACT STICKING AND CORRECTED. DEFERRED DOOR 2L PER MEL 33-51-02 AND PLACARD DAY OPS ONLY. SFO MAINTENANCE RE-LAMPED DOOR 2L.SDR DL75E100873Line · leakingCTR HYD SYS RESVR DROPPED TO 0.24 AFTER T/O SYS PRESS STAYED NORMAL. FOUND 2 HYD LINES CHAFED AND LEAKING FROM CI PUMP, REF IPC 29-11-51-20A ITEMS 130 AND 605. INSTALLED 2 TEMP LINES. SCVD HYD AND LEAK CKS OK.SDR DL75E100759Check Valve · rupturedREPEAT WRITE-UP. SEE ITEM 004 THIS LOGSHEET. CABIN PRESS UNCONTROLLABLE IN AUTO 1/ AUTO 2 AND MANUAL. OUTFLOW MANUALLY CLOSED. DUCT PRESS 40 PSI BUT CABIN WILL NOT HOLD PRESSURIZATION. FOUND LT PACK DUCT SUPPLY CHECK VALVE WITH 4 INCH SQ SECTION BLOWN. BLOWSDR DL75E100756Check Valve · crackedAFTER T/O BOTH AUTO PRESS CONTROLLERS FAILED. PILOTS COULD NOT CONTROL CABIN PRESS ELECTED TO DESCEND AND DIVERT. CONTRACT MX FOUND A SEAL OUT OF PLACE ON EMERGENCY EXIT DOOR REINSTALLED SAME AND PRESSURIZED ACFT WITH CREW ALL NORMAL. AFTER LEAVING AIRPORT, SDR DL75E100228Gcu · inoperativeAFTER HARD-START PROCEDURES -RT ENG GEN CONTROL WOULD NOT SOME ON - RT ENG GEN OFF EICAS MSG. FWD TO MCO AND PLAC IAW MEL 24-00-01 RT ENG DISCONNECTED AND APU VERIFIED FULL.SDR DL75E091917Fmc · failedBOTH LT AND RT FMC WILL NOT HOLD ROUTE DATA T/S IN WORK. R & R CAPTS FMS COMPUTER IAW MM AND UPDATED NAV AND OP PROGRAM DATABASE IAW MM. ALSO RELOADED RT FMS NAV DATABASE IAW MM ALL OPS NML. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK.SDR DL75E091941Computer · faultedBOTH FMCS WOULD NOT DISPLAY SPEED/ALTITUDE ETSS/ FUEL. COULD NOT MANUALLY ENTER DATA CA-R/R CAPTS FMS COMPUTER IAW MM AND UPDATED NAV AND OP PROGRAM DATABASE IAW MM. ALSO RELOADED RT FMS NAV DATABASE IAW MM, ALL OPS NORMAL. ETOPS CATEGORY 'E': PROBLEMS WITHSDR DL75E091661Starter · faultyLEFT ENG START HUNG UP AT 42 PERCENT N2. NO N2 RISE ON SECOND START ATTEMPT. START VALVE LIGHT CYCLED NORMAL. REMOVED AND REPLACED NR 1 ENGINE STARTER PER AMM PERFORMED LEAK CHECK. NO LEAKS NOTED. PERFORMED ENGINE NR 1 RUN UP ALL INDICATIONS NORMAL. ETOPSDR DL75E091625Oven · dirtyFIRST CLASS NR1 OVEN PRODUCED SMOKE IN FLIGHT. MX DEACTIVATED OVEN AND FORWARDED TO NEF ITEM.SDR DL75E091575Irs · malfunctionedDURING QUICK ALIGN A/C MOVEMENT SENSED. AIRCRAFT ON ROLL BEFORE ALIGN COMPLETE. FAULT CAUSED BY AIRCRAFT MOVEMENT BEFORE ALIGN CYCLE COMPLETE. IRS OPS CHECK OK PER AMM 34-21-00-715. REALIGN IRS NO FAULT NOTED. A/C OK FOR SERVICE. ETOPS CATEGORY 'B': DIVSDR DL75E091472Mechanism · lack of lubeAFTER DEPARTING GATE A/C UNABLE TO TURN RIGHT, ALL HYD IND NORMAL, A/C CAN TURN LEFT. INSPECTED STEERING CABLES AND PULLEY, FOUND ALL NORMAL. REMOVED STEERING ACTUATOR COVER AND LUBRICATED ACTUATOR COMMAND MECHANISM. OPS CHECK GOOD. ETOPS CATEGORY 'E': PR
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