Boeing 757-222
Service difficulty reports · 15,539
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 = '757222' 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 = '757222' 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 UALA2011040601672Handle · out of adjustL-1 DOOR BUTTERFLY HANDLES DO NOT FLUSH DURING OPERATIONAL CHECK. REPLACED L-1 DOOR EXTERNAL HANDLES CENTER SHAFT, INNER SHAFT AND CLUTCH COLLAR PER MM. ADJUSTED AND OPS CHECK GOOD PER CMM ON NON ROUTINE 31885.SDR UALA2011040601671Structure · damagedR-2 DOOR SLIDE SHELF DAMAGED IN TWO SPOTS ON EDGE. REMOVED AND REPLACED THE R-2 DOOR SLIDE SHELF.SDR UALA2011040601670Control Rod · corrodedMAIN CABIN L-4 DOOR LOWER AFT GIRT BAR CONTROL ROD IS CORRODED. REMOVED AND REPLACED MAIN CABIN L-4 DOOR LOWER AFT GIRT BAR CONTROL ROD PER MM AND OPS CHECKED L-4 DOOR GIRT BAR MECHANISM GOOD.SDR UALA2011040601669Slide · misinstalledFOUND MAIN CABIN L-2 DOOR EMERGENCY EVACUATION SLIDE INSTALLED INCORRECTLY AT UPPER ATTACH POINTS. REMOVED SLIDE AND REINSTALLED PER MM ON NON ROUTINE BY MECH AND INSP QC385. FULLY INSTALLED THE MAIN CABIN L-2 DOOR EMERGENCY EVACUATION SLIDE SAFETY PIN PER MM SDR UALA2011040601668Floor Panel · damagedSPONGY FLOOR MIDDLE OF AISLE JUST FWD OF OVERWING EXITS. INSTALLED NEW FLOORBOARD REF DWG 15F6868-599.SDR UALA2011040601662Floorboard · damagedAISLE FLOOR ROW 20 HAS A DEEP INDENTATION. REPLACED ROW 20 AISLE FLOORBOARD IAW MM. ACFT RETURNED TO NORMAL CONFIGURATION.SDR UALA2011040701676Tee Fitting · corrodedCORROSION AT STA 324 TEE FITTING. A REPAIR WAS PERFORMED.SDR UALA2011040501639Wire Harness · faultyTHE INSULATION ON WIRE BUNDLE LEADING TO F/O WINDOW IS DETERIORATED. OUTER PROTECTIVE INSULATION SPIRAL CABLE DETERIORATED FOR THE FO NR 2 WINDOW HEAT. WIRE INSULATION & CLEAR INSULATION STILL GOOD. CABLE NEEDS TO BE REPLACED. C-B PULLED & COLLARED PER MEL. SDR UALA2011040601661Mechanism · lack of lubeDOOR 4L EXTERNAL DOOR HANDLE DOES NOT RETRACT. REMOVED EXTERNAL HANDLE CENTER SHAFT AND CLUTCH COLLAR, LUBED EXTERNAL HANDLE MECH AND ADJUSTED EXTERNAL HANDLE MECH. NOW WITHIN TOLERANCE.SDR UALA2011040601657Floorbeam · corrodedCORROSION ON TOP OF FLOORBEAM AT STA 1640 RBL 24. MAJOR REPAIR ACCOMPLISHED: AFTER REMOVING CORROSION FOUND TO BE OUT OF LIMITS PER SRM. REMOVED TOP CHORD AT 1640 LB 10 THRU RBL 68. FABRICATED REPLACEMENT T-CHORD, ANGLES AND STRAPS FROM 7075-T6511 PER SRM.SDR UALA2011040501638Battery · faultyMAIN BATTERY CHARGER STATUS MESSAGE IN CRUISE. REPLACED MAIN BATTERY AND CHARGER PER MM, OPS CHECKED NORMAL.SDR UALA2011040501635Beam · corrodedCORROSION ON SUB BEAM AT STA 1713, RBL 40 TO RBL 60. MAJOR REPAIR ACCOMPLISHED: REPLACED SUB BEAM AT STA 1713, RBL 40 TO RBL 60, PER SRM.SDR UALA2011040501634Intercostal · corrodedINTERCOSTAL CORRODED AT R1 DOOR BS 324 TO 367. MAJOR REPAIR ACCOMPLISHED: REPLACED INTERCOSTAL AT DOOR R1 STA 324 TO STA 367 PER SRM.SDR UALA2011040401623Fitting · corrodedSTA 1720 RT CUSP TO BULKHEAD T-FITTING CORRODED AT PRESSURE DECK. MAJOR REPAIR ACCOMPLISHED: RT T-FITTING AT STA 1720 REPLACED PER SRM.SDR UALA2011040401622Crease Beam · corrodedCREASE BEAM TRUSS BETWEEN BS 500 AND BS 480 HAS EVIDENCE OF CORROSION. MAJOR REPAIR ACCOMPLISHED: AFTER CORROSION FOUND OUT OF LIMITS PER SRM. FABRICATED CREASE BEAM ANGLES OUT OF 7075-T6 PER SRM. TREATED, PRIMED AND INSTALLED PER SRM.SDR UALA2011040401621Floor Support · corrodedFLOOR SUPPORT CORRODED STA 322, RBL 42. MAJOR REPAIR ACCOMPLISHED: FLOOR SUPPORT FROM STA 310.5 TO 322, RBL 42 REPLACED PER SRM.SDR UALA2011040401628Panel · delaminatedLT VERTICAL STABILIZER PANEL AT APPROX STA 1770 TO STA 1808 PNL P/N 175N2001-35, FOR REPAIR. STARTED LT VERTICAL STAB PANEL REMOVAL, NEED TO CONTINUE WITH REMOVING PANEL FASTENERS.SDR UALA2011040401608Bracket · crackedDOOR 4R LWR GATE COVER BRACKET THAT SLIDE CHAIN ATTACHES TO IS CRACKED. INSTALLED NEW HARNESS LATCH BRACKET (P/N 69-59926-3) N-R 32131.SDR UALA2011040501651Guide Arm · looseDOOR 3L VERY DIFFICULT TO OPEN AND CLOSE. FOUND GUIDE ARM ATTACH BOLTS TO DOOR LOOSE AND GUIDE ARM ROD ARM BEARING WORN AND SERPENTINE GUIDE PIN WORN. REPLACED GUIDE ARM AND RIGGED. DOOR STILL VERY HARD TO OPERATE. FOUND HANDLE MECHANISM VERY STIFF. WILL SDR UALA2011040401616Relay · failedFUEL PROBLEM, FLT DIVERTED. COMPLIED WITH MEL 2822J, CTR TANK QTY 3.8K, CB'S PULLED AND WRAPPED WITH DF STICKER F20 F14, DF STICKER APPLIED OVER RT AND LT LENS COVER. DF555. WORK IN CONJUNCTION WITH DF554 FOR LT CTR PUMP INOP, PREVIOUSLY DEFERRED. COA 50722SDR UALA2011040401600Guide Arm · defectiveDOOR 3R (AFT PAX DOOR) VERY DIFFICULT TO OPEN AND CLOSED. FOUND GUIDE ARM ATTACH BOLTS TO DOOR LOOSE AND GUIDE ARM ROD ARM BEARING WORN AND SERPENTINE GUIDE PIN WORN. REPLACED GUIDE ARM AND RIGGED. DOOR STILL VERY HARD TO OPERATE. FOUND HANDLE MECHANISM VESDR UALA2011040401594Radio Altimeter · faultyWHEN THRUST IDLE IN DESCENT EICAS GEAR NOT DOWN CAME ON L RA YELLOW BOX FLASHING ON AND OFF. REPLACED LEFT RADIO ALTIMETER IAW MM. LANDING CONFIG SYS TEST CHECKED OKAY.SDR UALA2011040401610Housing · damagedRT MLG FWD TRUNNION SUPPORT BEARING HOUSING REPAIR HAS RECEIVED FIRST STAGE APPROVAL FOR STATIC STRENGTH AND IS TIME LIMITED TO 03APR11. A NEW FAA 8100-9 IS REQUIRED BY 03APR11 OR THE AIRWORTHINESS CERTIFICATE OF THIS AIRPLANE IS NO LONGER CURRENT. SFOLM TRUSDR UALA2011040401605Light · inoperativeSEAT 23C EEL LT INOPERATIVE. REPLACED LIGHT ASSY, OPS CHECKED OKAY.SDR UALA2011040401604Light · inoperativeEMERGENCY LIGHTS INOP AFT CABIN ROWS 25 AND 33. RELAMPED BOTH POSITIONS, OPS CHECKED OKAY.SDR UALA2011040401602Valve · faultyENG DUCT PRESSURES SPLIT DURING CRUISE WITH ISOL VLV CLOSED & BLEED SW SELECTED ON. RECORD DUCT PRESSURES. CREW COMMENTS: LEFT 45 PSI RIGHT 30 PSI CRUISE AT 26000FT. APPLIED MEL 3611A. REPLACED HIGH STAGE PILOT VALVE PER AMM. RAN ENGINE AT HIGH POWER PERSDR UALA2011040101565Light · bowedEMERGENCY LIGHT STRIP BOWING AT AISLE 13. CHECKED EEL TRACK LIGHTING. ROW 13 IS BULKHEAD FEED TO STRIP CAUSING SLIGHT RISE IN CARPET. NO DEFECTS NOTED. OK PER SMFMM.SDR UALA2011040101563Floorbeam · corrodedSTA 365 FLOORBEAM UPPER FLANGE CORRODED. MAJOR REPAIR ACCOMPLISHED: REPAIRED ON SM W-U E9952H PER SRM FROM LBL 8.5 TO RBL 59.SDR UALA2011033101549Girt Bar · obstructedF/A REPORTS DOOR 2R NOT INDICATING FULLY DISARMED WHEN DISARMED. REMOVED SLIDE COVER AND CLEANED FOD FROM SLIDE ENGAGE BAR. SATISFACTORY ARM AND DISARM FUNCTION. REINSTALLED SLIDE COVER. BRIEFED OUTBOUND FLIGHT ATTENDANT AT DOOR 2R.SDR UALA2011040101580Flow Divider · leakingFUEL LEAKING FROM APU DRAIN MAST. FOUND DRAIN FOR FUEL FLOW DIVIDER LEAKING ONLY WHEN APU NOT RUNNING AT 10 DROPS EVERY 14 SECONDS. LIMIT FOR STATIC LEAK ON THIS DRAIN IS 1 DROP PER SECOND. APU OK FOR SERVICE TO NEXT MAINT OP FOR FLOW DIVIDER CHANGE. REPLASDR UALA2011040101583Wire · brokenDURING NR 2 ENGINE START, LOST COCKPIT ELEC POWER. T-R MSG DISPLAYED ON LOWER EICAS. REPLACED LEFT TRU, NO HELP. LEFT ENG DID NOT TRANSFER PWR. SWAPPED LEFT AND RIGHT GCU, NO HELP. SWAPPED BACK. REPLACED LEFT GEN CNTL BREAKER C901 AND LEFT BUS TIE CNTL SDR UALA2011033101548Cover · unsecureCREW REPORT: EMERGENCY EXIT LIGHT COVER FELL OFF AT 17ABC. REPLACED EMERGENCY LIGHT STRIP COVER.SDR UALA2011033101543Pan · corrodedGALLEY G4B FLOOR PAN IS CORRODED FROM STA 1680 TO 1686 LBL 20 TO RBL 58. MAJOR REPAIR ACCOMPLISHED: REPAIRED WITH PTT SEQ 2572135 UNDER PEMCO EA PD57-53-097. REMOVED CORROSION AND FOUND AREAS TO BE OUT OF LIMITS PER SRM. REMOVED DAMAGE AND ACCOMPLISHED NDTSDR UALA2011033101542Structure · corrodedGALLEY G4B FLOOR DECK IS CORRODED FROM STA 1686, LBL 20 TO RBL 58. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION AND FOUND AREAS TO BE OUT OF LIMITS PER SRM. REMOVED DAMAGE AND ACCOMPLISHED NDT INSPECTION OF AREA WITH NO CRACKS FOUND. ACCOMP THE FABRICATIONSDR UALA2011033001524Lanyard · looseDOOR 3L WILL NOT ARM. SECURED LOOSE LANYARD IN POUCH. ARM DISARM FUNCTION CHECKS OKAY.SDR UALA2011033101547Fan Blade · damagedNR 2 ENG N1 FAN 3EA FAN BLADES EVIDENCE OF FOD DAMAGE. NEED TO DRESS BLADES. REPAIRED 3 EA FAN BLADES (MARKED ON BLADE ROOT) ON NR 2 N1 FAN.SDR UALA2011033001536Floorbeam · corrodedFLOORBEAM CAP AT STA 365.25 HAS CORROSION FROM RBL 2 TO RBL 50. MAJOR REPAIR ACCOMPLISHED: FLOORBEAM CAP HAS PREVIOUS REPAIR WHICH IS ALSO CORRODED. CORR OUT OF LIMITS, CUT OUT DAMAGE, FABBED T-CHORD, 2 EA ANGLES, 2 EA. STRAPS & INSTALLED PER AMM'S.SDR UALA2011033001517Feeder Cable · damagedWHILE TROUBLESHOOTING LOG 1 (EEL LIGHTS) FOUND NO OUTPUT FROM INVERTER (SEAT 28A). INPUT 6 VOLTS. INVERTER (560-0853) IS ON AOG. AOG H6079. REPLACED INVERTER AT 28A, NO HELP. REPLACED DAMAGED POWER FEEDER CABLE AND SECURED TRACK AND COVER AND RPL END CAP.SDR UALA2011033001516Crease Beam · corrodedRIGHT CREASE BEAM UPPER SURFACE HAS CORROSION AT BS 975 AT RBL 71. MAJOR REPAIR ACCOMPLISHED: CORROSION FOUND TO BE OUT OF LIMITS PER SRM. FABRICATED NEW CREASE BEAM WEB OUT OF 7075-0 .063 PER SRM. HEAT TREATED AND PRIMED PER AMM. TOP COATED CREASE BEAM WSDR UALA2011033001515Frame · dentedFWD CARGO FRAME HAS DENTS IN TWO LOCATIONS AT BS 580 BETWEEN S-25L AND S-24L. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED FRAME. NDT INSPECTED AREA AND FOUND NO CRACKS PER NDT. FABRICATED FRAME OUT OF 7075 T-6 .063. HEAT TREATED PER PEMCO TRAVLER 2486N0041SDR UALA2011033001514Frame · crackedFWD CARGO FRAME HAS CRACK AT BS 600 AT STR 24L. MAJOR REPAIR ACCOMPLISHED: CUT OUT AND REMOVED DAMAGE FRAME, ACCOMPLISHED NDT OF AREA & FOUND NO CRACKS PER REF NDT. FABRICATED REPLACEMENT FRAME ASSEMBLY FROM 7075 T6 ,063 AND HEAT TREATED ON TRAVLER 2486N004SDR UALA2011033001513Web · damagedELONGATED HOLES IN WEB AT STATION 324 RBL 30 - RBL 68. MAJOR REPAIR ACCOMPLISHED: REMOVED WEB ASSEMBLY AT STA 324 RBL 30 - RBL 68 AND FABRICATED NEW SECTION OUT OF 2024 - T3 .063 IAW B757 SRM. LOCATED AND DRILLED NEW WEB PER SRM. PRIMED AND ALODINED NEW PASDR UALA2011033001512Girt Bar · obstructedCREW REPORTED 1R GIRT BAR HARD TO DISARM. FOUND ICE AROUND GIRT. REMOVED ICE AND EXERCISED ARMING LEVER. OPS NORMAL.SDR UALA2011033101561Plate · missingLOUD AIR NOISE IN FORWARD CABIN. REMOVE CEILING PANELS AS REQUIRED AND CHECK AIR DISTRIBUTION DUCT FOR DAMAGE AND CONDITION. REMOVED PANELS. FOUND ALL INTACT. RE-INSTALLED ALL PANELS. REMOVED NOZZLE BETWEEN MONITORS 2 AND 3. FWD OF MONITOR 3 FOUND 6" SECSDR UALA2011032901499Guard · looseEMERGENCY EXIT LIGHT SWITCH COVER LOOSE AT DOOR 1L. REPLACED GUARD.SDR UALA2011032901498Floorbeam · corrodedSTATION 324 RBL 41 FLOORBEAM HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: REMOVED AND REPLACED FLOORBEAM STA 324, RBL 41 IAW PEMCO EA PD57-536-096.SDR UALA2011032901497Beam · corrodedAFT CARGO COMPARTMENT STATION 1620 LAP BEAM AT SW-30 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION, FABBED AND INSTALLED REPAIR DOUBLER PER PEMCO EA PD57-53-103.SDR UALA2011032901496Crease Beam · corrodedLEFT CREASE BEAM O/B FLANGE COMMON TO INTERNAL FUSELAGE CORRODED AT STA 1006, LBL 71. AGING ACFT INSP FINDINGS. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION, FABBED ANGLE, ACP'D HFEC ON ALL HOLES AND AREA FOR CRACKS. NO DEFECTS NOTED. INSTALLED ANGLE PER SDR UALA2011032801489Skin · damagedLT INBOARD AFT FLAP INBOARD END POTTING SPLIT OPEN BOTH UPPER AND LOWER SKIN. MAJOR REPAIR ACCOMPLISHED: AREA FROM FWD SPAR T/E AFT 13 INCH ON UPPER SKIN AND 12 INCH ON LOWER SKIN AND OUTBOARD FROM INBD END OTBD 8 INCHES BOTH SIDES HAS DELAMINATION & FROZEN SDR UALA2011032801482Relay · faultedMAIN BATTERY CHARGER MESSAGE, SUSPECT RIGHT BUS NOT POWERED. REPLACED MAIN SHIP BATTERY AND MAIN BATTERY CHARGER, NO HELP. REPLACED MAIN BATTERY CHARGER DISABLE RELAY K115, NO HELP. PER FIM 24-31-00 P106 PAGE BLOCK 7. FOUND A1-90VAC, B1-77VAC, C1-115VAC. T
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