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 FDEA201108303581Gate · corrodedDOOR LOWER GATE BOTTOM EDGE FWD AND AFT CORNER ARE CHAFED. REMOVED CORROSION PER SRM 51-10-02. BEFORE: 0200", AFTER: .150", LOSS: .050", FOUND TO BE OUT OF LIMITS PER SRM 52-10-02, FIG. 101, DETAIL 4. REMOVED AND REPLACED L4 DOOR LWR GATE ASSY PER AMM 52-SDR FDEA201108303580Gate · corrodedDOOR LOWER GATE BOTTOM EDGE CORRODED. REMOVED CORROSION PER SRM 51-10-02. ORIGINAL MATERIAL: .200", REMOVED: .015", REMAINING: .185", FOUND TO BE OUT OF LIMITS PER SRM 52-10-02, FIG. 101, DETAIL 4. REMOVED AND REPLACED L2 LOWER GATE ASSY PER AMM 52-11-38SDR FDEA201108293567Gate · corrodedR2 DOOR LOWER GATE HAS CORROSION ON THE BOTTOM EDGE. FOUND OUT OF LIMITS PER SRM 52-10-02, FIG. 101, DETAIL 4; EXCEEDS .100" FROM EDGE. REMOVED AND REPLACED R2 DOOR LOWER GATE ASSY PER AMM 52-11-38. PERFORMED R2 DOOR ADJUSTMENT CHECK PER AMM 52-11-00-5. ADJUSSDR FDEA201108293566Skin · damagedFOUND SCRIBE LINE AT BSTA 1681.8 THROUGH 1700.55 S-10L LAP JOINT. ACCOMPLISHED EA F-5330-147692 PART 1 ONLY, VERIFICATION OF NO ADDITIONAL SCRIBLINES AT BUTT JOINT STA 1621 TO 1720 ALONG S-10L. PART 2 REQUIRED AT 1500FC AFTER PART 1 AND PART 3 OF EA REQUIRED SDR FDEA201108293565Skin · damagedFOUND SCRIBE LINE AT BSTA 1533 THROUGH 1534.25 S4L LAP JOINT ACCOMPLISHED EA F-5330-147690 PART 1 ONLY, VERIFICATION OF NO ADDITIONAL SCRIBELINES AT BUTT JOINT STA 1459 TO STA 1621 ALONG S-4L. PART 2 OF EA REQUIRED AT 1500 FC AFTER PART 1 AND PART 3 OF EA REQSDR DALA1150560693Support · corrodedMAIN CABIN FLOOR BL 0 CHORD CORROSION STA 345 TO 365. LOCATED AND DRILLED HOLE ON REPLACEMENT CHORD (SUPPORT) P/N 141N5191-1 B/N 0002095260 PER REF B757SRM 51-40-05 PG 1-10. INSTALLED CHORD (SUPPORT) AT MAIN CABIN FLOOR BL 0 FROM 324 TO STA 440 PER REF B757 SDR FDEA201108263519Frame · misrepairedFUSELAGE FRAME STA 720 AT S30 MISREPAIRED. R & R FRAME IAW SRM 51-40-02. MAJOR REPAIR.SDR DALA1150550693Skin Panel · crackedSLAT 2 COVE SKIN PANEL IS CRACKED INBOARD SIDE OF INBOARD MAIN TRACK. FABRICATED FILLER DOUBLER TO SKIN COVE IAW ER/A 366767-14 MA REV A STEP 4 AND 6. TREATED AND PRIMED IAW STEPS 8 AND 9 INSTALLED PER ER/A AT SAA/SAT DURING HMV ON (N/R 191024) W/O 885954200SDR DALA1149990660Battery Pack · dischargedDURING A LAYOVER CHECK, MAINTENANCE FOUND THE FIRST CLASS EMERGENCY PATH LIGHTS WOULD NOT TEST. MAINTENANCE REPLACED THE POWER SUPPLY BATTERY PACK. OPERATIONAL CHECK WAS GOOD.SDR FDEA201108243459Frame Splice · misrepairedFRAME SPLICE REPAIR AT BS 720, S29L- S29R, REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH APPROVED DATA. FRAME SPLICE REPAIR REPLACED IAW EA F-5310-147720. MAJOR REPAIR.SDR DALA1149750655Oxygen Mask · malfunctionedDURING FLIGHT, CABIN PRESSURIZATION WAS LOST AND CABIN O2 MASKS DEPLOYED. THE MASKS AT SEAT ROW 23ABC DID NOT DEPLOY. MAINTENANCE REPLACED THE O2 GENERATORS AND TESTED THE MASKS. OPERATION WAS NORMAL. REFER TO LOG PAGE 526588002.SDR DALA1149380655Shutoff Valve · seizedFLIGHT DIVERTED TO SJU DUE TO A LOSS OF PRESSURIZATION. CABIN O2 MASKS WERE DEPLOYED. MAINTENANCE REPLACED LEFT ENGINE FAN AIR TEMP SENSOR AND RIGHT ENGINE PRSOV. ENGINE RUN-UP RESULTED IN NORMAL TEMPERATURES AND PRESSURES.SDR DALA1150530693Frame · dentedAFT CARGO FRAME DENTED STA 1400 ABOVE STR 26L. FABRICATED J SECTION REPAIR IAW B757 SRM 53-00-07 REPAIR 5 STEP 4 FIG 201 PG 201 DETAIL I. INSTALLED REPAIR J SECTION ON STA 1400 S 26L. AFT CARGO COMPT IAW B757 SRM 53-00-07 REPAIR 5 DETAIL I FIG 201 PG 201 STSDR DALA1150760693Structure · damagedDENT ON FUSELAGE WITH 3 GOUGES INSIDE STA 1703 ABOVE STR 18L. FABRICATED REPAIR DOUBLER REF 757 SRM 53-00-01 REPAIR 3 PAGE 201 FIG 201 STEP 6. INSTALLED REPAIR DOUBLER REF 757 SRM 53-00-01 REPAIR 3 PAGE 201 FIG 201. AT SAA/SAT DURING HMV ON (N/R 203367) W/SDR DALA1150040693Floorbeam · corrodedMAIN CABIN FLOORBEAM CORRODED STA 1640 RBL 15 TO LBL 10. INSTALLED FABBED REPLACED CHORD IAW B757 SRM 53-00-01 REP 3 STEP 9, 10 FIG 201 PG 201.SDR DALA1153300693Frame · gougedAFT CARGO FRAME GOUGED ON UPPER RADIUS STA 1520 ABOVE STR 23-26R / FORMED NEW REPAIR SECTION J PER SRM 53-00-07 REPAIR 5 PG 201-212. THIS IS A CATEGORY B WITH THRESHOLD REPETITIVE INSP TO START AT 5010.0 AIRFRAME FLIGHT CYCLES. METHOD HIGH FREQUENCY EDDY CURSDR DALA1151900693Stringer · corrodedAFT CARGO STR CORRODED STA 1430-1460 AT 29R. PROCURED REPL STRINGER INSTALLED IAW 51-40-05 FIG 3 PG 4.SDR FDEA201108183360Frame · misrepairedFRAME REPAIR LOCATED AT BS 1520 S29R TO S29L DOES NOT CONFORM TO CURRENT SRM REQUIREMENTS. FRAME REPAIR REPLACED IAW EA. F-5310-147719.SDR C8GA2011000017Static Port · obstructedDURING TAKEOFF ROLL THE CREW NOTED A NEGATIVE AIRSPEED INDICATION. THE TAKEOFF WAS ABORTED AND THE ACFT RETURNED TO BLOCKS WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED NOTING DEBRIS IN THE F/O'S STATIC PORT. REMOVED DEBRIS AND PERFORMED PITOT STATISDR C8GA20110818001Adc · inoperativeDURING TAKEOFF ROLL, THE F/O NOTED A NEGATIVE AIRSPEED INDICATION. AN ABORTED TAKEOFF WAS PERFORMED AND THE ACFT RETURNED TO THE BLOCKS WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED NOTING THAT THE AIR DATA COMPUTER WAS AT FAULT. R & R THE AIR DATASDR DALA1150070693Skin Panel · crackedSLAT 2 COVE SKIN PANEL CRACKED O/B OF I/B MAIN TRACK. INSTALLED DOUBLER REPAIR PER ERA 366767-14MA REV A.SDR DALA1150060693Skin Panel · crackedSLAT 1 COVE PANEL CRACK I/B SIDE OF I/B MAIN TRACK. INSTALLED REPAIR PER ERA 366767 - 14MA REV A.SDR DALA1150050693Skin Panel · crackedSLAT 2 COVE SKIN PANEL CRACKED O/B SIDE OF MAIN TRACK. INSTALLED REPAIR PER ERA 366767-14MA REV A.SDR DALA1150010693Skin Panel · crackedTHREE CRACKS ON NR 9 SLAT COVE PANEL AT I/B TRACK. REPAIRED PER ERA 366767-14MA REV A.SDR DALA1150020693Skin · dentedDENT ON FUSE WITH 3 GOUGES STA 1703 ABOVE S 18L. PERM CAT B REPAIR PER SRM 53-00-01 REPAIR 3 PG 201 FIG 201.SDR DALA1147970641Control Panel · shortedSMOKE-FUMES EMITTED FROM THE VOR/DME CONTROL PANEL. MAINTENANCE INSPECTED WIRING AND REPLACED THE CONTROL PANEL. OPERATIONAL CHECK WAS GOOD.SDR DALA1154170693Structure · dentedFSTA 640 BETWEEN S-6L DENT ON FUSELAGE. COMPLIED WITH ERA 495296-14 REV ORIGINAL DURING HMV AT ST AEROSPACE SAN ANTONIO.SDR DALA1150030693Skin · dentedFUSE SKIN HAS 6 EA DENTS STA 600-640 S 15-17L AND 4 EA GOUGES ON S 16L STA 625-628. INSTALLED PERM CAT B REPAIR PER SRM 53-00-01 REP 3 FIG 201 PG 201.SDR DALA1148410612Wire · looseDURING A LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY PATHLIGHT AT SEAT 2C INOPERATIVE. MAINTENANCE SECURED THE WIRING. OPERATIONAL CHECK WAS GOOD.SDR DALA1148400612Wire · looseDURING A LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY PATHLIGHT AT SEAT 19D INOPERATIVE. MAINTENANCE SECURED THE WIRING. OPERATIONAL CHECK WAS GOOD.SDR DALA1147720672Pan · gougedWATER SERVICE PAN GOUGED. ACCOMPLISHED PERM REPAIR PER ERA 494626-14 REV O.SDR DALA1147710672Beam · corrodedMAIN CABIN FLOOR EXFOLIATED STA 324 O BL TO RBL 52. ACCOMPLISHED PERM REPAIR PER ERA 493508-14 REV O.SDR DALA1147700672Skin · gougedRT WING I/B FLAP UPPER SURFACE GOUGE I/B OF NR 7 SPOILER. ACCOMPLISHED PERM REPAIR PER ERA 494623-14 REV O.SDR DALA1147670672Skin · corrodedAFT CARGO SKIN CORROSION STA 1462 S29-30R. ACCOMPLISHED PERM REPAIR PER ERA 494610-14 REV O.SDR DALA1147660672Frame · chafedCABIN FRAME HAS CHAFE DAMAGE STA 1640 S6R. ACCOMPLISHED PERM REPAIR PER ERA 494625-14 REV O.SDR DALA1147650672Skin · gougedRT WING I/B FLAP UPPER SURFACE GOUGE I/B OF NR 7 SPOILER. ACCOMPLISHED PERM REPAIR PER ERA 494623-14 REV O.SDR DALA1147640672Skin · dentedFUSELAGE DENT STA 1716 S20-21R. ACCOMPLISHED PERM REPAIR PER ERA 493505-14 AD REV A.SDR DALA1147630672Floorbeam · corrodedMAIN CABIN FLOORBEAM UPPER SURFACE HAS CORROSION SAT 1640 LBL 58 TO RBL 58. ACCOMPLISHED PERM REPAIR PER ERA 494611-14 REV O.SDR DALA1147580683Skin · damagedWHILE ACCOMPLISHING MTC SEVERAL MISDRILLED HOLES CAUSING 17 DAMAGED HOLES AT STA 1400 STR 27 LT TO 28 RT AT THE BUTT SPLICE AREA OF THE SKIN ONLYERA 495021-14 REV 0.SDR DALA1147570672Stringer Splice · corrodedCORROSION ON STRINGER SPLICE STA 1620 S20L. REMOVED AND REPLACED SPLICE PER SRM 51-40-02 PG7.SDR DALA1147540672Frame · dentedAFT CARGO FRAME DENTED STA 1220 S 26L. PERM REPAIR PER ERA 494620-14 REV O.SDR DALA1147530672Frame · dentedAFT CARGO FRAME DENT STA 1240 S26L. PERM REPAIR PER ERA 494622-14 REV O.SDR DALA1147520672Doubler · gougedLT EXT FUSE REPAIR GOUGED STA 600. PERM REPAIR PER ERA 493507-14 REV O.SDR DALA1147560672Stringer Splice · corrodedSTRINGER SPLICE CORRODED STA 160 S21L. REPLACED SPLICE AND CLIP PER SRM 51-40-02 PG 7.SDR DALA1147550672Skin · dentedFUSE MULT DENTS STA 479-485 S18-19L. PERM REPAIR PER ERA 494607-14 REV O.SDR DALA1147440683Skin · damagedWHILE ACCOMPLISHING MAINTENANCE IN ATL, MTC MISDRILLED SEVERAL RIVET HOLES, CAUSING SEVENTEEN DAMAGED HOLE AT STATION 1400, FROM STRINGER 27 LEFT TO 28 RIGHT AT BUTT SPLICE AREA IN THE SKIN ONLY.SDR FDEA201108103181Mount · corrodedNR 2 PYLON FWD ENG MOUNT STRUT FITTING WITH CORROSION ON LOWER SURFACE FWD AND AFT MOUNT MATING. REMOVED CORROSION BY BLENDING AREA PER SRM-54-51-90 PG.104 FIG.101 DET.VII, REMOVED AND REPLACED FWD. STRUT MOUNT FITTING, PER SRM-51-40-02.SDR DALA1147460686Bottle · dischargedDURING LINE CHECK FOUND L4 DOOR ASSIST BOTTLE READS EMPTY. REMOVED ASSIST BOTTLE PER B757 AMM 52-11. INSTALLED ASSIST BOTTLE PER B757 AMM 52-11. INSPECTED FINAL INSTALLATION AND SAFETY PER B757 AMM 52-11-30. A/C OK FOR SVC.SDR FDEA201108053111Skin · misrepairedSKIN REPAIR LOCATED AT STA 1680, S-20L DOES NOT CONFORM TO CURRENT SRM CONFIGURATION.SDR DALA1147600683Splice · corrodedINTERNAL BUTT SPLICE STA 1401 HAD SEVERE CORROSION ON THE INTERNAL SURFACE BETWEEN STR 27L AND 28L. REPAIRED AREA PER ERA 379695-14.
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