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 FDEA201105251988Firewall · chafedAPU COMPARTMENT FWD FIRE WALL HAS CHAFING MARKS 20" FROM BOTTOM EDGE OF COMPARTMENT. CHAFE MARK FOUND TO .004" DEEP, DETERMINED TO BE OUT OF LIMITS IAW SRM 53-80-01 FIG 101 DETAIL IX PG 109. REPAIRED DAMAGE IAW SRM 53-80-08, FIG 201, SHEET 1, PG 201, STA 18SDR FDEA201105241960Floorbeam · gougedFLOORBEAM AT STA 1600 HAS NUMEROUS GOUGES BETWEEN RBL 60 TO LBL 60. REMOVED AND REPLACED FLOORBEAM, FOUND TO BE OUT OF LIMITS PER SRM 53-00-51 FIG.101 DETAIL 3. LOCATED AND DRILLED FASTENER HOLES IN NEW FLOORBEAM PER SRM 51-40-02. APPLIED TOP COAT PER SRM 51SDR FDEA201105241968Seat Track · corrodedMAIN DECK STA 1155, RBL 45 SEAT TRACK CORRODED. REMOVED CORROSION WITH .070" MATERIAL LOSS. MAX ALLOWED IS .040". AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 4. R & R TRACK IAW SRM 51-40-01, 51-40-05, 51-40- 02. MAJOR REPAIR.SDR FDEA201105241967Seat Track · corrodedMAIN DECK STA 1140, RBL 45 SEAT TRACK CORRODED.SDR FDEA201105241965Seat Track · gougedMAIN CABIN COMPARTMENT STA 1170, LBL 45 SEAT TRACK GOUGED. R & R SEAT TRACK IAW SRM 51-40-01, 51-40-02, AND 51-40-05. MAJOR REPAIR.SDR FDEA201105241964Seat Track · corrodedMAIN CABIN STA 1120, LBL 25 SEAT TRACK CORRODED. BLENDED AREAS OF CORROSION WITH MATERIAL LOSS OF .070. CLEAN UP MAX ALLOWED IS .040". AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 4. R & R SEAT TRACK IAW SRM 51-10-02, 51-40-02, 51-40-05SDR FDEA201105241963Frame · misrepairedFRAME REPAIR LOCATED AT STA 1340 BETWEEN STR 26R AND STR 27R DOES NOT CONFORM TO CURRENT SRM CONFIGURATIONS. ACCOMPLISHED EA F5310-147704. MAJOR REPAIR.SDR FDEA201105241962Frame · misrepairedFRAME REPAIR LOCATED AT STA 1340 BETWEEN STR 25L AND STR 27L DOES NOT CONFORM TO CURRENT SRM CONFIGURATIONS. REPAIRED IAW EA F5310-147704.SDR FDEA201105241961Frame · misrepairedFRAME REPAIR LOCATED AT STA 1340 BETWEEN STR 25L AND 27L DOES NOT CONFORM TO SRM CONFIGURATION.SDR FDEA201105241955Skin · dentedEXTERIOR FUSELAGE SKIN HAS A DENT AT STA 435, BETWEEN S21-22R. FOUND OUT OF LIMITS IAW-SRM-53-00-01 FIG 101, DET III . REPAIRED DENT IAW-SRM-53-00-01 FIG 201, REPAIR 16. THIS IS A CLASS B REPAIR.SDR DALA1136120688Transition Panel · corrodedFWD PIT LT TRANSITION PANEL CORRODED FROM STA 640 TO 765. R & R TRANSITION PANEL IAW SRM 51-40-02, FIG 8, DETAIL II.SDR DALA1136100692Wire Harness · defectiveDURING A LAYOVER CHECK, MAINTENANCE FOUND THE FIRST CLASS CABIN EMERGENCY PATH LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT HARNESS, AND THE BATTERY PACK AND CHARGER. OPERATIONAL CHECK WAS GOOD.SDR FDEA201105211925Floorbeam · gougedSTA 1200, FLOORBEAM UPPER FLANGE GOUGED BL 0 TO LBL 64. FOUND OUT OF LIMITS IAW SRM 53-00-51 DETAIL III. REPAIRED FLOORBEAM AT STA 1200 LBL 19.5 IAW SRM 53-00-51 DETAIL 1, AND REPAIR 3. BLENDED GOUGES; L=2.5, W=1.0, D=.002, ORIGINAL MATERIAL WAS .125, FOUSDR FDEA201105211923Floorbeam · damagedMAIN CABIN FLOOR AREA AT STA 1520, LBL 14 FLOORBEAM WITH FASTNER HOLE ELONGATED REPAIRED FLOORBEAM AT STA 1520 IAW SRM 53-00-51, REPAIR 5 CATEGORY "A" MAJOR REPAIR.SDR FDEA201105201916Floorbeam · damagedMAIN DECK FLOORBEAM UPPER T-CHORD HAS 2 EA ELONGATED FASTENER HOLES BETWEEN RBL 45 AND RBL 63 AT STA 460. FOUND TO BE OUT OF LIMITS .250 MAX DIA. AFTER .310 IAW SRM 53-00-51 FIG 101. REPAIRED FLOORBEAM AT STA 460 RBL 33- 63 IAW SRM 53-00-51 FIG 201. CATSDR FDEA201105201915Floorbeam · damagedMAIN DECK FLOORBEAM UPPER TEE FITTING HAS 2 EA. ELONGATED FASTENER HOLES AT STA 480 BETWEEN RBL 45 TO RBL 63. FOUND OUT OF LIMITS PER SRM 53-00-51, FIG.101. REMOVED AND INSTALLED ANGLES, BS 480, RBL 50, PER SRM 51-40-02, FOR ACCESS. REMOVED DAMAGED TEE FITSDR FDEA201105201901Seat Track · brokenLBL 24 SEAT TRACK SCALLOP BROKEN AT BS 1200. TRANSFERED FROM N00741, REMOVED SEAT TRACK FS 1180-1320 LBL 24 IAW SRM 51-40-02, FABBED NEW SEAT TRACK FROM BAC1520- 792, BATCH 1904663, LOCATED AND DRILLED IAW SRM 51-10-02 AND 51-10-55, TREATED, PRIMED AND TOPSDR FDEA201105201913Stringer · crackedSTRINGER 23R IS CRACKED AT A FASTNER HOLE IN THE LOWER WEB AT APPROX STA 1660. REPAIRED STR 23R, STA 1650-1670 IAW SRM 53-00-03, FIG 201, REPAIR NR 2 USING BAC 1498-203 TCH 2031079 AND T11/883136. A MAJOR REPAIR NO FOLLOW UP INSP REQUIRE.SDR FDEA201105201910Frame · corrodedAFT CARGO FRAME BS 1400 HAS CORROSION UNDER DOOR SILL AREA. CORROSION FOUND OUT OF LIMITS IAW 53-00-07, PG 104, FIG 101, DET V, RECEIVED NEW FRAME & SPLICE. R & R FRAME IAW SRM 51-40-02 & DWG 146N1028. MAJOR REPAIR.SDR FDEA201105201900Seat Track · corrodedMAIN CABIN STA 900 RBL 45 SEAT TRACK CORRODED. BLENDED CORROSION . ORIGINAL MATERIAL .230, MATERIAL REMOVED .050. MATERIAL REMAINING .180 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 DETAIL I FIG 101. R & R SEAT TRACK AT STA 900, RBL 45 IAW SRM 51-40-02, PG 8.SDR FDEA201105191882Seat Track · crackedSEAT TRACK AT STA 640, LBL 24.75 IS CRACKED. REMOVED DAMAGE SECTION IAW SRM 53-00-52. FABRICATED REPAIR SECTION IAW SRM 53-00-52 REPAIR 1 FIG 201. INSTALLED REPAIR SECTION IAW SRM 53-00-52 REPAIR 1 AT STA 640 LBL 24.75. CATEGORY "A" MAJOR REPAIRSDR FDEA201105191875Seat Track · gougedMAIN CABIN SEAT TRACK CROWN HAS GOUGE AT STA 877 RBL 45 REMOVED AND REPLACED SEAT TRACK STA 760- 879 RBL 45 IAW 51-10-02, PN BAC1520-792, BATCH 1904663. SEAT TRACK WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-52, FIG.101, DETAIL 1; ORIGINAL MATERIAL .145", ASDR FDEA201105191876Seat Track · corrodedCABIN SEAT TRACK STA 760-879 LBL 24, CORRODED. REMOVED AND REPLACED SEAT TRACK AT STA 760 - 879 LBL 24 IAW SRM 51-40-02 P/N BAC1520-792 BATCH 1904663, FABRICATED WITH SEAT TRACK WAS FOUND OUT OF LIMITS IAW 53-00-52 FIG 101 DETAIL I. ORG MATERIAL .188 AFTERSDR DALA1135130680Coffeemaker · smokeDURING FLIGHT, CREW NOTICED SMOKE COMING FROM COFFEEMAKER IN THE G2D GALLEY. APPLICABLE CIRCUIT BREAKERS WERE PULLED AND THE SMOKE STOPPED. MAINTENANCE REPLACED THE COFFEEMAKER. WIRE HARNESS INSPECTION SHOWED NO EVIDENCE OF BURNT WIRES. OPERATIONAL CHECK WASSDR FDEA201105181873Skin · misrepairedSKIN REPAIR AT STA 1684, S-27 L DOES NOT COMPLY WITH CURRENT SRM REQUIREMENTS. REMOVED REPAIR AND FILLER IAW SRM 51-40-02. REPLACED REPAIRE AND REINSTALLED FILLER IAW SRM 51-40-02 FIG 201 REPAIR 15. THIS IS CLASS B REPAIR, MAJOR REPAIR.SDR FDEA201105181874Skin · misrepairedSKIN REPAIR AT BS 1560 BETWEEN STR 1R TO S-2R DOES NOT COMPLY WITH CURRENT SRM REQUIREMENTS. REMOVED REPAIR DOUBLER AT SKIN BS 1560 BETWEEN S-1R TO S-2R IAW SRM 51-40-02, INSTALLED REPAIR DOUBLER IAW SRM 53-00-01, FIG 201, REPAIR NR 16 THIS IS CLASS "B" REPAISDR FDEA201105171853Floorbeam · corrodedSTA. 365, FLOORBEAM CORRODED BL-0 - 24L. REMOVED CORROSION AT STA 365 LBL 6 ORGINAL MAT .125 MATERIAL REMOVED .060 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETAIL III. FABERICATED FLOORBEAM IAW SRM 53-10-51 FIG 101 DETAIL II PART MARKED IAW GMM 7-0SDR FDEA201105171859Floorbeam · corrodedFLOOR BEAM AT STA. 345, LBL10 CORRODED. REMOVED; .040", FOUND TO BE OUT OF LIMITS PER SRM 53-00-51, DETAIL 3. REMOVED FLOORBEAM PER SRM 51-40-02. FABRICATED NEW FLOORBEAM PER SRM 53-10-51 & INSTALLED PER SRM 51-40-02. MAJOR REPAIRSDR DALA1138570627Rod End · corrodedLT OVERWING SLIDE CARRIER SNUBBER RODEND CORRODED. REPLACED ROD END AT SAA ON N/R CARD 188054.SDR DALA1135230681Light · inoperativeDURING A LAYOVER CHECK, MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY PATH LIGHT AT 25D INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD.SDR FDEA201105171856Skin · dentedEXTERIOR FUSELAGE SKIN HAS DENT AT STA 1422, BETWEEN S28L AND S29L EVALUATED DENT AT EXTERIOR FUSELAGE SKIN STA 1422 BETWEEN S28L AND S29L A=.040 Y=.020 A/Y=20 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET III, PAGE 104. REPAIRED DENT IAW SRM 53-SDR DALA1138560627Floorbeam · corrodedMAIN CABIN FLOORBEAM UPPER SURFACE CORRODED STA 680 LBL 24 RBL 24. REPAIRED DURING HMV AT SAA ON N/R CARD 187261.SDR DALA1138550627Floorbeam · corrodedMAIN CABIN FLOORBEAM CORRODED STA 760 LBL 3 TO LBL 22. REPAIRED DURING HMV AT SAA ON N/R CARD 187266.SDR DALA1138540627Gate · corrodedR4 DOOR LOWER GATE HAS CORROSION THRU-OUT. REPLACED GATE AT SAA ON N/R CARD 194538.SDR DALA1138430627Lifter · damagedL4 DOOR FWD AND AFT GIRT BAR LIFTER GOUGED AND CORRODED. REPLACED LIFTERS AT SAA ON N/R CARD 194541.SDR DALA1135016706Battery Pack · inoperativeDURING A LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT AT ROW 44F INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONAL CHECK WAS GOOD.SDR FDEA201105121831Floorbeam · corrodedSTA. 377 FLOORBEAM CORRODED BL 24 - 45 L. REMOVED CORROSION IAW SRM 51-10-02. AREA OUT OF LIMITS IAW SRM 53-00-51 FIGURE 101 DETAIL III. ORIG. MAT. .125 AFTER REWORK .107 MAT. LOSS EXCEED MAX. ALLOWED. REMOVED FLOORBEAM IAW SRM 51-40-02. FABRICATED NEW FLOOSDR DALA1133560672Skin · damagedCOMPLIED WITH ERA 492565-14 REV. A.SDR FDEA201105121830Skin · misrepairedPREVIOUSLY INSTALLED SKIN REPAIR AT STA 1700 BETWEEN S-15L TO S-16L DOES NOT COMPLY WITH CURRENT SRM REQUIREMENTS REMOVED DOUBLER AT STA 1700 BETWEEN S-15L TO S-16L ON THE SKIN IAW SRM 51-40-02. INSTALLED NEW DOUBLER IAW SRM 53-00-01 FIG 201 REPAIR 16. CLASSDR FDEA201105121829Skin · misrepairedPREVIOUSLY INSTALLED SKIN REPAIR AT STA 1625 BETWEEN S-27L TO S-28L DOES NOT COMPLY WITH CURRENT SRM REQUIREMENTS. REMOVED DOUBLER AT STA 1625 BETWEEN S-27L TO S-28L ON THE SKIN IAW SRM 51-40-02. REPAIRED AREA IAW SRM 53-00-01, FIG 201, REPAIR 16. CLASSISDR FDEA201105101792Doubler · crackedMAIN AVIONICS ACCESS DOOR CRACKED AS MARKED. CUT AND REMOVED DAMAGE PORTION IAW SRM 51-70-13, FABRICATED REPAIR DOUBLER FROM 20-24-T3 .050 IAW SRM 51-70-13, INSTALLED NEW REPAIR DOUBLER AT MAIN AVIONICS DOOR IAW SRM 51-70-13, DETAIL I, FIG 1. CATEGORY "A" REPSDR DALA1138520627Skin · dented1 EA DENT 3 INCHES LONG ON FUSELAGE SKIN STA 612 BELOW STR 17L. ACCOMPLISHED ERA 492129-14 AD AT SAA ON N/R CARDS 181078.SDR DALA1138490627Skin · dented1 EA DENT ON FUSELAGE SKIN STA 633 BELOW STR 17L NO ID TAG. ACCOMPLISHED ERA 492129-14 AD AT SAA ON N/R CARD 181076.SDR FDEA201105091786Seat Track · corrodedMAIN CABIN AREA BETWEEN STA 470-660, LBL 45 SEAT TRACK HAS CORROSION SEAT TRACK STA 470-660, LBL 45 FOUND OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL V. ORIG MATERIAL .165 AFTER REWORK .085. L=2.1 W=.750. R & R SEAT TRACK IAW SRM 51-40-02. CLASSIFIEDSDR DALA1133860688Frame · dentedDURING HMV A DENT WAS FOUND AT AFT CARGO COMP FRAME STA 1480 BTW STRINGER S25L-S26L. FRAME WAS REPAIRED IAW SRM 53-00-07 REPAIR 5.SDR DALA1133890688Floorbeam · corrodedDURING HMV CORROSION WAS FOUND ON CABIN FLOOR SUPPORT BEAM UPPER SURFACE STA 1640 LBL8-RBL8. FLOOR SUPPORT WAS REPAIRED IAW SRM 53-00-51 FIG 201 REPAIR 3.SDR DALA1133880688Frame · dentedDURING HMV A DENT WAS FOUND BULK CARGO COMP FRAME STA 1600 BTW S25L-S26L. FRAME WAS REPAIRED IAW SRM 53-00-07 REPAIR 5 FIG 201 SHEETS (1-15).SDR DALA1133870688Frame · dentedDURING HMV A DENT WAS FOUND BULK CARGO COMP AT FRAME STA 1500 ABOVE S25L. FRAME WAS REPAIRED IAW SRM 53-00-07 FIG 201 SHEET (1-15) REPAIR 5.SDR DALA1133850688Floorbeam · corrodedDURING HMV CORROSION WAS FOUND ON MAIN DECK FLOORBEAM UPPER CORD BTW BL0-RBL25 BS 365.25. FLOORBEAM WAS REPAIRED IAW SRM 53-00-51 R1.SDR DALA1133840688Frame · dentedDURING HMV A DENT WAS FOUND FWD CARGO COMPARTMENT FRAME STA 580 BETWEEN STRINGERS S23L-S24L. FRAME WAS REPAIRED IAW SRM 53-00-07 REPAIR NR 5 FIG 201 SHEETS (1-15).
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