Boeing 757-232
Service difficulty reports · 15,843
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 = '757232' 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 = '757232' 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 DU4R2007145Floorbeam · corrodedFOUND CORROSION ON UPPER T-CAP OF CABIN FLOORBEAM AT BS 345 B/L 48R. REPAIRED BY FABRICATING AND INSTALLING T-CAP PAN 75-3/4 FROM BAC 1505-100617, SPLICES 12 BY 2 BY ¾ FROM 7075-T6 .050 AND 8 BY 2 BY ¾ FROM 075-T6 .063”, STRIPS 11-1/2, 1 BY 6 BY 1 AND 10 BY SDR DU4R2007146Floorbeam · corrodedFOUND CORROSION ON UPPER T-CAP OF CABIN FLOORBEAM AT BS 365, B/L 3-R TO B/L 32R. REPAIRED BY FABRICATING AND INSTALLING T-CAP REPAIR 52 BY 2.5 FROM 7075-T6 .071, SUPPORT ANGLE 11 BY 1.75 FROM 7075-T6 .063, SUPPORT ANGLE 8.5 BY 1.75 7075-T6 .090, RADIUS FILLERSDR DL757070836Spoiler · stuckON APPROACH, "R YAW DAMP INOP" ILLUMINATED ON EICAS FOLLOWED BY "SPOILER" LIGHT. ALMOST FULL RT AILERON NEEDED TO MAINTAIN LEVEL FLIGHT. ALSO STAB TRIM LIGHT ILLUMINATED ON LANDING. ON CLIMB-OUT C-HYD SYSTEM PRESSURE AND OVERHEAD SYS PRESSURE LIGHTS ILLUMINSDR DL757070834Skin · dentedFUSELAGE SKIN HAS A DENT AT FS608, S-16L. CUT OUT DAMAGED SKIN AND INSTALLED A REPAIR DOUBLER.SDR DU4R2007143Skin · dentedFOUND DENT IN FUSELAGE SKIN BS 606 AND DENTED STRINGER 16L. REPAIRED BY CUTTING OUT DENTED AREA, FABRICATING AND INSTALLING REPAIR DOUBLER 9-3/4 BY 7-1/2 FROM 2024-T3 .050, STRINGER REPAIR 10-1/2 BY 3-1/4 FROM BAC1498-200 IAW B757 SRM 53-00-03 FIG 201 AND DESDR DU4R2007144Angle · corrodedFOUND HEAVY CORROSION IN AFT PIT ON MAIN ANGLE AT BS 1480 STR 27 RT. REPAIRED BY REMOVING ANGLE. DRILLED UP, TREATED, PRIMED AND INSTALLED CHORD P/N 146N8522-57 IAW 51-40-05 PG 1, 51-40-02 AND 51-20-01.SDR DL757070784Engine · leakingAFTER T/O FROM SNA RIGHT ENGINE OIL PRESSURE LIGHT FOLLOWED BY EICAS MSG THEN OIL QTY WENT TO ZERO SHUTDOWN ENGINE IN FLIGHT. COMPLETED ENGINE SHUTDOWN REPORT. REPLACED LEAKING AIR/OIL COOLER. NO METAL FOUND ON CHIP DETECTORS OR MAIN OIL FILTER. RAN ENGINESDR DL757070724Skin · gougedMAJOR REPAIR LOCATED AT STA 1428 BETWEEN STOP BEAMS 5 AND 6 ON C2 CARGO DOOR.SDR DL757070723Skin · gougedMAJOR REPAIR INSTALLED ON C2 CARGO DOOR STA 1407 STOP BEAM 4. REPAIR REF SRM 52-30-01 FIG 201.SDR DL757070718Skin · dentedDURING CURRENT HMV AT TIMCO LCQ, TWO DENTS WERE NOTED ON THE FUSELAGE SKIN BETWEEN BODY STATION 1681.8 AND 1701, BETWEEN S-14R AND S-16R. THE SUBJECT DAMAGE WAS BEYOND THE ALLOWABLE DAMAGE LIMITS OF THE SRM. EACH OF THE DAMAGED AREAS WAS TRIMMED OUT, AND A BSDR DU4R2007136Skin · dentedFOUND DENT AT BS 1685 FROM S-16R TO S-14R ACROSS S-15R. REPAIRED BY CUTTING OUT DENTED AREA, HFEC CUT OUT PER B757 TM PT. 6-51-00-19, NO RELEVANT INDICATIONS NOTED. FABRICATED AND INSTALLED REPAIR DOUBLER 16-1/4 BY 15-1/40 BY 15-3/4" FROM 2024-T3 .080 AND FISDR DL757070725Skin · gougedMAJOR REPAIR LOCATED STA 1384 AT STOP BEAM 3 OF CARGO DOOR.SDR DL757070709Battery · dischargedF/C EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY.SDR DU4R2007142Torque Tube · corrodedFOUND LT I/B FLAP I/B FAIL SAFE TORQUE TUBE CORRODED. REPAIRED CORRODED LT WING I/B FLAP FAIL SAFE TORQUE TUBE BY REMOVING AND REPLACE TORQUE TUBE WITH P/N’S 113N2105-1 AND 113N2108-1 IAW B757 MM 57-53-44.SDR DU4R2007141Torque Tube · corrodedFOUND RUSTED RT I/B FLAP I/B TORQUE TUBE. REPAIRED BY REMOVING AND REPLACING TORQUE TUBE AND FAIL SAFE TUBE WITH P/N’S 113N2105-2 AND 113N2108-1 IAW B757 MM 57-53-44.SDR DU4R2007134Brace · out of limitsFOUND NR 1 DIAGONAL BRACE ID 2.003 OUT OF LIMITS. REPAIRED OVERSIZED LUG ON NR 1 DIAGONAL BRACE BY HONING, FABRICATING AND INSTALLING BUSHINGS IAW DELTA ERA 461664-14AD DATED 6/7/07 APPROVED BY FAA FORM 8100-9 WITH AMOC TO PARAGRAPH (A) OF AD 2003-18-05.SDR DU4R2007131Bulkhead · chafedFOUND CHAFED LOWER OUTBOARD CORNER OF NR 2 PYLON AFT BULKHEAD. REPAIRED BY FABRICATING AND INSTALLING GUSSET 4.34 BY 2.88 BY 1.2 BY .100 FROM 7050-T7451 AND FILLER FROM 15-5PH.125 IAW DELTA ERA 461663-14AD DATED 6/7/07 REV ORIG APPROVED BY FAA FORM 8100-9, WISDR DU4R2007132Bulkhead · chafedFOUND CHAFED LOWER OUTBOARD CORNER OF NR 1 PYLON AFT BULKHEAD. REPAIRED BY FABRICATING AND INSTALLING GUSSET 4.34 BY 2.88 BY 1.2 BY .100 FROM 7050-T7451 AND FILLER FROM 15-5PH.125 IAW DELTA ERA 461663-14AD DATED 6/7/07 REV ORIG APPROVED BY FAA FORM 8100-9, WISDR DU4R2007135Brace · out of limitsFOUND NR 2 DIAGONAL BRACE ID 2.003 (OUT OF LIMITS). REPAIRED OVERSIZED LUG ON NR 2 DIAGONAL BRACE BY HONING, FABRICATING AND INSTALLING BUSHINGS IAW DELTA ERA 461664-14AD DATED 6/7/07 APPROVED BY FAA FORM 8100-9 WITH AMOC TO PARAGRAPH (A) OF AD 2003-18-05.SDR DU4R2007137Drag Link · corrodedFOUND CORRODED NLG LOWER DRAG LINK. REPAIRED BY REMOVING AND REPLACING P/N 162N2201-1 IAW B757 AMM 32-24-04.SDR DL757070698Brace · damagedDURING CURRENT HMV, THE NR 1 PYLON DIAGONAL BRACE REQUIRED OVERSIZING BEYOND THE EA LIMITS. AS SUCH, BOEING WAS CONTACTED FOR APPROVAL TO OVERSIZE BEYOND LIMITS DUE TO AD 2003-18-05, AND THE WORK IS DOCUMENTED IN ERA 461664-14AD.SDR DU4R2007133Frame · dentedAFT PIT FRAME DENTED BS 1440, STR 27L. REMOVED OLD REPAIR, FABRICATED AND INSTALLED FRAME REPAIR 16"BY 3" BY 1" FROM 7075-T6 .071" IAW B757 SRM 51-40-02, 51-40-05, 51-70-11, 53-00-07, 51-20-01 AND 51-20-02.SDR DU4R2007128Frame · dentedFOUND DENT IN UPPER CAP OF AFT PIT MAIN FRAME BS 1400 BETWEEN S-27 AND S-26 LT. REPAIRED BY FABRICATING AND INSTALLING FRAME REPAIR 9 BY 14 FROM 7075-T6 .071 IAW DELTA ERA 380490-14MA REV ORIG, DELTA PROCESS STANDARD 900-5-1 NR 4, B757 SRM 51-40-02, PG 2, 7, SDR DU4R2007139Web · corrodedFOUND WEB CORRODED AT AFT CARGO DOOR LOWER FWD CORNER BS 1380 AND S-27R BY REMOVING WEB. REPAIRED BY FABRICATING AND INSTALLING REPAIR WEB 4-1/2 BY 22 FROM 7075-T6 .071 IAW B757 SRM 51-40-02 AND 51-30-01.SDR DL757070634Battery · dischargedEMERGENCY FLASHLIGHT AT R4 DOOR INOP. REPLACED BATTERY.SDR DL757070633Brake · seizedAFTER LANDING NR 5 BRAKE SHOWED 5. AFTER BLOCKED FUSE PLUG BLOWN AND TIRE DEFLATED. ON LANDING AUTO BRAKES WERE SET AT 1 AND USED VERY LIGHTLY. FOUND ASSY SEIZED. REMOVED AND REPLACED NR 5 MAIN BRAKE ASSY LEAK CK OK. REINSTALLED WHEEL ASSY PER M/M.SDR DU4R2007129Stringer · corrodedFOUND S-29L CORRODED IN AFT PIT AT BS 1480. REPAIRED CORRODED STRINGER BY REMOVING AND INSTALLING STRINGER P/N 146N3110-8201 AND SPLICE IAW B757 SRM 53-00-03.SDR DU4R20070123Skin · damagedFOUND LIGHTNING STRIKE BS 310 BETWEEN S-8L AND S-9L. REPAIRED BY REMOVING SHEAR TIE, CUT OUT STRIKE AREA, HFEC CUT OUT IAW B757 NTM PT6 51-00-01, 51-00-19 NO RELEVANT INDICATIONS NOTED. TRIMMED OUT AN EXTRA .040” MATERIAL. FABRICATED AND INSTALLED SHEAR TIESDR DL757070608Duct · splitON CLIMB-OUT, THE OVERHEAD DISTRIBUTION DUCT AT ROW 33/34 AREA LET GO. THE RUPTURE CAUSED THE CEILING PANEL TO BE BLOWN OFF INTO THE CABIN. THE A/C RETURNED TO SJU.SDR DU4R20070125Frame · dentedFOUND DENT MAIN FRAME UPPER CAP IN FWD PIT BS 720 AT B/L 0. REPAIRED BY FABRICATING AND INSTALLING DOUBLER 5-5/8 BY 1-7/8 BY 1 FROM 7075-T6 .063 IAW B757 SRM 51-40-05, 51-40-02 AND 51-20-01.SDR DU4R20070127Skin · dentedFOUND DENTED STRINGER 15L ON EXTERNAL SKIN AT BS 569. REPAIRED BY CUTTING OUT DENT IAW B757 SRM 53-00-01 SECTION OF FRAME HFEC CUT OUT EDGES HFEC DENT IAW B757 D634N301, PT 6-51-00-19, NO DEFECTS NOTED. FABRICATED AND INSTALLED DOUBLER 10.5 BY 9.25 FROM 2024SDR DL757070606Skin · dentedREPAIR OF DENT AND GOUGE AT FS 495 AND STRINGER 28R. DAMAGE CUTOUT AND DOUBLER INSTALLED.SDR DL757070605Door · missingON DEPARTURE FROM SEA, AFTER CLIMBING THROUGH FL270 MULTIPLE CREW MEMBERS CONTACTED THE FLT DECK WITH EXCESSIVE NOISE AND VIBRATION VICENITY OF 2L TO WING AREA. FOUND LT RAM AIR DOOR ACCESS PANEL MISSING. ROBBED DOOR FROM A/C 6717.SDR DL757070669Lanyard · looseFOUND LT OVERWING SLIDE PACK PARTIALLY DEPLOYED DURING ROUTINE DEACTIVATION OF EMEGENCY ESCAPE SYSTEM. LANYARD WAS PULLED FREE FROM SLIDE PACK. C/W OPN 7809 NR 1L ESCAPE DOOR SLIDE REPLACEMENT REF RC 650-651.SDR DL757070631Skin · damagedLIGHTNING DAMAGE IN FUSELAGE SKIN S-4L LAP SPLICE. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLERS.SDR DU4R2007138Bearing · corrodedFOUND OUTER HOUSING OF LT MLG AFT TRUNNION CORRODED. REPAIRED BY REMOVING AND REPLACING WITH P/N S113N103-5 IAW B757 MM 57-54-07.SDR DU4R2007140Bearing · corrodedFOUND RIGHT MLG AFT TRUNNION BEARING HOUSING CORRODED AT RACE AND AFT TANG FWD OF THREADS. REPAIRED BY REMOVING AND REPLACING BEARING P/N S113N103-5 IAW B757 MM 57-54-07.SDR DU4R20070126Frame · bentFOUND BENT MAIN FRAME UPPER SURFACE IN FWD PIT BS 660 AT S-24L. REPAIRED BY CUTTING OUT BENT SECTION OF FRAME. FABRICATED AND INSTALLED DOUBLER 11-1/2 BY ¼ BY 1 BY 2 FROM 7075-T6 .063 IAW B757 SRM 53-00-07 AND 51-20-01.SDR DU4R2007120Skin · damagedFOUND LIGHTNING STRIKE AT BS 310 BETWEEN S-2R AND S-3R. REPAIRED BY CUTTING OUT STRIKE AREA, HFEC INSPECTED IAW B757 NTM PT6 51-00-01, 51-00-19 NO RELEVANT INDICATIONS NOTED. FABRICATED AND INSTALLED REPAIR DOUBLER 8.0 BY 7.75 FROM 2024-T3 .071 IAW B757 SRM SDR DL757070570Skin · damagedDURING CURRENT HMV, A DENT WAS FOUND ON THE EXTERIOR SKIN PANEL P/N 143N3320-3 JUST ABOVE S-17L AT FS 443. THE SUBJECT DAMAGE WAS OUTSIDE OF THE ALLOWABLE DAMAGE LIMITS OF THE SRM. THE DAMAGE WAS TRIMMED OUT AND AN EXTERNAL REPAIR DOUBLER INSTALLED PER ER/A SDR DU4R2007121Stringer · corrodedFOUND CORROSION ON STRINGER AND SKIN AT BS 750 S-23R. REPAIRED BY CUTTING OUT SECTION OF STRINGER. FABRICATED AND INSTALLED STRINGER REPAIR 14 BY 3.5 FROM BAC1498-204 IAW B757 SRM 51-20-01 AND 53-00-03 FIG 201.SDR DU4R2007130Attach Angle · corrodedFOUND CORROSION AFT PIT MAIN FRAME FWD ATTACH ANGLE BS 1680 BETWEEN S-28 - S-29R. REPAIRED CORROSION ON FRAME ATTACH ANGLE BY FABRICATING AND INSTALLING NEW FRAME ATTACH ANGLE FROM 7075-T6 .071" CLAD IAW B757 SRM 51-40-02, 51-70-11 AND 51-20-01.SDR DU4R2007124Stringer · corrodedFOUND STRINGER 29R AT BS 1681 CORRODED. REPAIRED CORROSION ON STRINGER S-29R AT BS 1681 BY CUTTING OUT AND REMOVING CORRODED SECTION OF STRINGER BS 1670 TO BS 1720 IAW B757 SRM 53-00-53 AND 51-40-02. FABRICATED AND INSTALLED STRINGER SECTION 50 BY 3 REPAIR FSDR DL757070561Skin · puncturedA SERVICE TRUCK STRUCK THE FUSELAGE PUNCTURING THE SKIN AT FS 1705, S20L. THE DAMAGED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.SDR DL757070529Unknown · odorDURING DESCENT, F/A ADVISED US OF A HOT PLASTIC ODOR TOWARD THE MIDCABIN AREA, SMELL DISSIPATED AFTER APPROX 4 MIN. CHECKED LIGHTS IN CABIN AND PERFORMED CABIN WALK THROUGH. NO ABNORMAL ODORS NOTED. OPERATED PNEUMATICS. ALL CHECK NORMAL WITH NO ABNORMAL ODSDR DU4R2007122Skin · dentedFOUND DENT BELOW STR 17L, BS 440. REPAIRED BY CUTTING OUT DENTED SECTION OF SKIN, HFEC CUT OUT IAW B757 NTM PT6, 51-00-01, NO RELEVANT INDICATIONS NOTED. FABRICATED AND INSTALLED REPAIR DOUBLER 15-1/4 BY 13-1/2 FROM 2024-T3 .063 IAW B757 SRM 53-00-01 FIG 201SDR DL757070446Fitting · damagedDURING ACCOMPLISHMENT OF EA 06-070332-03AD, SIP MOD, HOLE NR 51 AS IDENTIFIED IN THE EA REQUIRED OVERSIZING BEYOND THE EA MAX. THE EA ALLOWS OVERSIZING TO 1ST OVER, AND THE HOLE REQUIRED OVERSIZING TO 2ND OVER. BOEING PROVIDED AMOC 8100 APPROVAL OF THE OVERSSDR DL757070385Engine · malfunctionedRT ENG ROLLED BACK AND THEN SHUTDOWN. NO ABNORMAL INDICATION PRIOR TO THIS EVENT. RT ENG SIMPLY QUIT ON ITS OWN, DUE TO EPCS MSG OF S PDIU AND HISTORY OF R ENG SEC CONT STATUS MSG. REPLACED RT ENG EEC, RT ENG PDIU AND RT ENG PMA STATOR. ALSO, INSPECTED ASSSDR DU4R2007116Skin · corrodedFOUND CORRODED SKIN AT BS 1845 BS 1850 LBL 24 (EMPENNAGE INTERNAL). REPAIRED BY TRIMMING OUT CORRODED AREA, HFEC INSPECTED NO CRACKING NOTED. FABRICATING AND INSTALLING PERMANENT REPAIR DOUBLER 9.5 BY 10.0 FROM 7075-T6 .063 AND FILLER FROM 7075-T6 .071 CLAD SDR DU4R2007115Stringer · corrodedFOUND CORRODED STRINGER 25L AT BS 1850 (EMPENNAGE INTERNAL). REPAIRED BY REMOVING SHEAR TIE AND SECTION OF STRINGER. FABRICATED AND INSTALLED STRINGER 25.0 FROM BAC 1498-132 AND SPLICE 10.0 FROM BAC1498-144 IAW B757 SRM 53-00-03 FIG 201, 51-20-01 AND 51-40-0
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