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 2006UALA00170Light · inoperativeEEL STRIP IN FRONT OF AFT CABIN FWD LAV INOP.SDR 2006UALA00144Repair · dentedDENT ON EXISTING REPAIR AT STA 620 & STR 16L. NDT NO CRACKS. ACCOMPLISHED HFEC OF DENT COMMON TO REPAIR. CUTOUT SECTION OF STR 16L. MFG STRINGER, DRILLED TREATED & PRIMED. INSTALLED STRINGER & SHEARTIES, INSTALLED GUSSET(TRUSSES) 2EA.SDR 2006UALA00143Repair · dentedDENT ON EXISTING REPAIR AT STA 620 & STR 16L. NDT NO CRACKS. ACCOMPLISHED HFEC OF DENT COMMON TO REPAIR. CUTOUT SECTION OF STR 16L. MFG STRINGER, DRILLED TREATED & PRIMED. INSTALLED STRINGER & SHEARTIES, INSTALLED GUSSET(TRUSSES) 2EA.SDR 2006UALA00169Generator · trippedRETURN TO FIELD AFTER LEFT GENERATOR TRIPPED OFF. MAINTENANCE LOG INDICATED THAT THE LEFT INTEGRATED DRIVE GENERATOR (IDG) WAS REMOVED AND REPLACED. FURTHER TROUBLESHOOTING FOUND THAT IDG CONNECTOR D05132, PIN (2) WIRE W5608-3501B-18 WAS SHORTED TO THE SHIESDR 2006UALA00168Odor · detectedRETURN TO FIELD DUE TO SMOKE AND ELECT SMELL IN CABIN. FOUND RIGHT RECIRC FAN INOP LIGHT ILLUMINATED. REPLACED FAN, OPS CHECK OK.SDR 2006UALA00081Warning Light · illuminatedFLIGHT DIVERTED DUE TO MACH SPEED TRIM EICAS AND LIGHT ILLUMINATED. A NUISANCE FAULT TRIPPED THE AIR/GROUND FAULT BALLS ON THE LT AND RT STABILIZER/ELEVATOR ASYMMETRY MODULES (SAMS), WHICH GENERATED THE MACH TRIM EICAS MESSAGE AND CAUTION LIGHT. THE AIR-GRSDR 2006UALA00218Skin · dentedA 2 INCH GOUGE AND DENT AT DOOR 3L, 2 FEET AFT AND BELOW DOOR AT STA 1700. INSTALLED REPAIR DOUBLER PER SRM 53-00-01.SDR 2006UALA00046Unknown · peelingLT WING NR 5 LEADING EDGE SLAT TRAILING EDGE WEDGE DAMAGED, PNL ON TOP OF WING JUST AFT OF NR 5 SLAT ALSO DAMAGED. ENGINEERING IS CONDUCTING ADDITIONAL INVESTIGATIONS FOR CAUSES OF THIS TYPE OF FAILURE. FAILURE OF THE LAMINATE ON WING. LE SLATS IS A SYSTEMICSDR 2006UALA00047Switch · failedFLIGHT DIVERTED DUE TO LOSS OF L GENERATOR DRIVE AND INABILITY OF INFLIGHT START ON APU. PROBLEM IS WITH APU SEL ECTOR SWITCH, IT WILL CAUSE CHRONIC NO STARTS. IF INTERNAL INTERLOCK SWITCH OPENS DURING START SEQ APU WON'T EVEN TURN UNLESS START SWITCH IS HELSDR 2006UALA00892Duct · looseRETURNED TO THE FIELD AT ORD AFTER A DUCT CAME LOOSE IN THE AFT CABIN CEILING.SDR 2006UALA00007Computer · failedRETURNED TO LAX DUE TO FAILED LEFT EICAS COMPUTER. THE LEFT EICAS COMPUTER WAS REPLACED AND THE FLIGHT DEPARTED. THE SHOP TESTED THE UNIT AND FOUND NO FAULT.SDR 2005UALA01535Warning Light · illuminatedRETURNED TO THE FIELD UNDER AMBER ALERT DUE TO A FLAP ASYMMETRY INDICATION. THE ASYMMETRY INDICATION WAS ILLUMINATED DUE TO A FAILED TE FLAP POSITION TRANSMITTER ON THE LEFT WING. THE SUBJECT LEFT WING POSITION TRANSMITTER WAS REPLACED PER 757 MM 27-58-03. ASDR 2005UALA01539Light · inoperativeEXT EMERGENCY LIGHT AT DOOR 4L INOP.SDR 2005UALA01525Wire · burnedFOUND BURNED WIRES BEHIND CONNECTOR D40496 UNDER THE P37 PANEL. FIVE WIRES WERE FOUND DAMAGED WITHIN THE P37 PANEL IN THE VICINITY OF CONNECTOR D40496J ON AIRCRAFT 5596. FOUR WIRES WERE BURNT THROUGH AND ONE WIRE HAD INSULATION DAMAGE PRESENT UPON WIRE BUNDLE SDR 2005UALA01515Warning System · activatedRETURNED TO THE FIELD DUE TO A FLAP ASYMMETRY PROBLEM. THIS EVENT IS CONSIDERED BY ENGINEERING TO BE A ONE-TIME NUISANCE EVENT. THE LE SLAT ASYMMETRY STATUS MESSAGE WAS GENERATED BY THE FLAP/SLAT ELECTRONICS UNIT (FSEU). THE NR 2 FSEU WAS RESET AND ALL OVERLSDR 2005UALA01512Odor · detectedMADE DESCENT TO 11,000 FEET DUE TO CABIN PRESSURE PROBLEM AND ODOR IN THE CABIN. REPLACED AUTO PRESSURE CONTROLLER PER MM21-31-02. OPS CHECK OK.SDR 2005UALA01531Frame · dentedAFT PIT STA 1580 FRAME HAS A DENT BETWEEN STR 25L AND 26L ON UPPER FLANGE. TRIMMED DAMAGE, INSURANCE CUT, INSTALLED ANGLE DOUBLER PER REO G-10195 AND EVA-50003.SDR 2005UALA01530Frame · dentedAFT PIT FRAME STA 1500, STR 25L AND 26L HAS DENT UPPER FLANGE. CUTOUT DAMAGE AND REPAIRED PER REO G10197 AND EVA-50005.SDR 2005UALA01529Frame · damagedAFT PIT STA 1520 FRAME HAS A DENT BETWEEN STR 25L AND 26L ON UPPER FLANGE. TRIMMED OUT DAMAGE TO FRAME, INSURANCE CUT, INSTALLED ANGLE REPAIR PER REO G10198 AND EVA 50006.SDR 2005UALA01528Frame · damagedAFT PIT STA 1600 FRAME HAS A DENT BETWEEN STR 25L AND 26L ON UPPER FLANGE. CUT OUT DAMAGE, INSURANCE CUT, INSTALLED DOUBLER REPAIR PER RE0-G10199, AND EVA-50007.SDR 2005UALA01511Indicator · malfunctionedABORTED TAKEOFF AT 100 KTS AND RETURNED TO THE BLOCKS DUE TO AN AIRSPEED INDICATOR PROBLEM. CAPTAIN'S MACH/AIRSPEED INDICATOR AND LEFT AIR DATA COMPUTER WERE REPLACED IN DEN FOLLOWNG THE EVENT. THE MASI HAD A BROKEN AIRSPEED POINTER RETURN SPRING AND THE DASDR 2005UALA01538Light · inoperativeEEL INOP AT ROW 34.SDR 2005UALA01537Light · inoperativeEEL INOP AT AND AROUND DOOR 3L.SDR 2005UALA01509Warning Light · illuminatedRETURNED TO MCI, DUE TO NR 1 ENGINE OVERHEAT LIGHT. REPLACED CARD M10224 AND RESEATED M10229 AND M10276. CHECKED ENG DUCTING WITH APU AIR ON AND NO LEAKS FOUND. SHOOK LOOP WHILE WATCHING LIGHT AND OKSDR 2005UALA01477Slide · unserviceableBOTTOM INFLATION TUBE HAS A HOLE IN EXCESS OF 1 INCH WHICH WOULD NOT PASS AR TEST. SLIDE WAS REMOVED FROM AIRCRAFT AT NORMAL MAINTENANCE INTERVAL. SLIDE FAILED AIR RETENTION TEST DUE TO HOLE IN INFLATABLE LOWER TUBE. IT WAS OBSERVED THAT SLIDE HAD BEEN PACKESDR 2005UALA01475Slide · unserviceableASPIRATOR VALVES LEAKING. SLIDE WAS REMOVED FROM AIRCRAFT AT NORMAL MAINTENANCE INTERVAL. ASPIRATOR FLAPPER VALVE WAS OBSERVED LEAKING DURING SLIDE OVERHAUL AIR RETENTION TEST. SPECIFIC CAUSE OF LEAK WAS NOT DETERMINED. ASPIRATOR WAS REPLACED.SDR 2005UALA01451Skin · gougedLEFTHAND FUSELAGE, AFT OF DOOR 2L, DENT AND GOUGED SKIN ON FRAME AT STA 760 AND S16. ACCOMPLISHED INTERIM RPR PER SRM53-00-01 RPR#2 PG.201-206. LFEC TO BE ACCOMPLISHED EVERY 3 000 CYCLES.SDR 2005UALA01462Smoke · detectedDURING TEST FLIGHT CREW EXPERIENCED SMOKE OUT IN CABIN. REPLACED LOWER RECIRC FAN, OPS CHECK OK.SDR 2005UALA01403A/C Pack · smokeAFTER TAKEOFF 1ST OFFICER NOTICED SMOKE FROM VENT SLIT BEHIND REAR WINDOW. COCKPIT NOTICED SMOKE & ODOR RISING FROM SIDE WINDOW VENTS DURING T-O ROLL AND C-O. TURNED OFF LEFT PACK, SMOKE DISSIPATED. NO ODOR WAS DETECTED IN MAIN CABIN. MAINTENANCE VERIFIED NOSDR 2005UALA01426Light · inoperativeEXTERIOR EEL LIGHT LT OVERWING AFT IS INOP. RELAMPEDSDR 2005UALA01428Wedge · delaminatedT/E WEDGE DELAMINATED NR 5 SLAT. REPAIRED WEDGE IN SHOP 273 AUTOCLAVE PER SRM 50-57-56-01 ON R66 864.SDR 2005UALA01352Life Vest · incorrectINFANT LIFE VEST INSTALLED AT SEAT 25D.SDR 2005UALA01335Warning Light · inoperativeONE BULB OF GIRT BAR WARNING LIGHT WILL NOT ILLUMINATE. REPLACED LIGHT ASSY.SDR 2005UALA01333Indicator · malfunctionedRETURNED TO THE FIELD DUE TO AN ERRATIC AIRSPEED INDICATOR. NUMBER 2 MACH AIRSPEED INDICATOR WAS REPLACED. THE AIRSPEED POINTER RETURN SPRING WAS FOUND BROKEN.SDR 2005UALA01332Landing Gear · malfunctionedRETURNED TO SFO DUE TO NOSE GEAR RETRACTION PROBLEM. REPLACED NOSE LANDING GEAR LOCK ACTUATOR. OPS CHECK OK.SDR 2005UALA01317Light · inoperativeEMERGENCY FLOOR PROX LIGHTS INOPERATIVE FROM ROWS 31 THROUGH ROW 34. REPLACED POWER SUPPLY M10817.SDR 2005UALA01316Floorbeam · crackedCABIN FLOORBEAM CRACKED UPPER FLANGE FWD SIDE, LBL 26.SDR 2005UALA01305Skin · bird strikeBIRD STRIKE TO RIGHT OUTBOARD WING L/E. REPAIRED NR 10 LE SLAT NOSE SKIN PER SRM 57-43-01.SDR 2005UALA01279Light · burned outSLIDE LIGHT AT 2L BURNED OUT. REPLACED.SDR 2005UALA01278Light · no testDOOR 2R SLIDE LIGHT NOT ILLUMINATED WITH DOOR ARMED PER CREW. REPLACED.SDR 2005UALA01274Engine · power lossTHRUST LOSS OCCURRED MULTIPLE TIMES WITH NR 2 ENGINE. REMOVED AND ROUTED THE EEC, PERFORMED A DATA DUMP, NO FAULTS OR FAILURES FOUND. THE EEC BEING MADE SERVICEABLY AND RETURNED. REMOVED THE N2 TRANSDUCER ALTENATOR STATOR. CONPONENT PASSED ALL ELECTRICAL TESSDR 2005UALA01277Slide · dislodgedDOOR 1L SLIDE PACK OFF OF DOOR. PER AMIS HISTORY, DURING THE PERIOD OF 1OCT&14NOV 2005, THERE WAS NO REPORTED PREVIOUS ACTIVITY RELATED TO THE 1L DOOR SLIDE THAT COULD HELP IN PINPOINTING A PROBABLE CAUSE WHY THE SLIDE WAS OFF THE DOOR. A PROBABLE CAUSE THATSDR 2005UALA01273Warning Light · intermittentAN INTERMITTENT EICAS ANTI-SKID WARNING LIGHT CAUSED A DIVERSION DUE TO CONCERNS WITH A SHORT RUNWAY AT PLANNED DESTINATION. REPLACED ANTISKID-AUTOBRAKE CONTROL UNIT PER MM 32-42-01. OPS CHECK NORMAL.SDR 2005UALA01242Wire · burnedWORKING INOP BLD FOUND CB'S FOR WATER HEATERS & DRAIN MAST POPPED. FOUND BURNED WIRES. *S/D* WIRES BURNED THRU AT STA 1681 , WL 208 DUE TO CHAFE THRU BY HOSE BAND CLAMP FROM IMPROPERLY ROUTED WIRES AND VENT HOSES WHICH LED TO ARCING AND BURN-THRU OF WIRES. SDR 2005UALA01218Wire · burnedFOUND C/B'S FOR WATER HEATERS & DRAIN MAST POPPED. FOUND BURNED WIRES. WIRES BURNED THRU AT STA 1681 , WL 208 DUE TO CHAFE THRU BY HOSE BAND CLAMP FROM IMPROPERLY ROUTED WIRES AND VENT HOSES WHICH LED TO ARCING AND BURN-THRU OF WIRES. BOEING NOTIFIED, AND NSDR 2005UALA01215Power Supply · activatedTHE FOLLOWING EMERGENCY LIGHTS ARE INOP: EXTERIOR, LEFT FWD OVERWING, DOOR 4L. INTERIOR, EXIT SIGN OVER DOOR 4L, EXIT MARKERS AT DOORS 4L & 4R, OVERHEAD EXIT SIGN IN AFT GALLEY, AISLE LIGHTS AT ROWS 29 & 32. LEFT AFT HATCH ILLUMINATION LIGHTS, AFT LIGHT IN RISDR 2005UALA01202Light · inoperativeEXTERIOR EMERGENCY SLIDE LIGHT L41 AT DOOR 2RT IS INOPERATIVE. RE-SECURED TERMINAL LUGS.SDR 2005UALA01197Skin · dentedLT FUSELAGE APPROX STA 618 TO 620, S-15 TO S-16 HAS A DENT. REMOVED DAMAGED ACP NDT INSP, NO CRACKS NOTED. FABRICATED REPAIR AND INSTALLED IAW SRM 53-00-01.SDR 2005UALA01196Skin · damagedFOUND DENT AT 6 O'CLOCK POSITION STA 1600. FOUND DENT WITHIN LIMITS IAW SRM 53-00-01. BURNISHED AND SMOOTHED OUT DENT.SDR 2005UALA01201Skin · damagedNR 2 ENGINE PYLON IB SIDE FWD ACCESS HOLE, DAMAGED. MAJOR REPAIR ACP ON NR 2 ENGINE PYLON INBD SIDE FWD ACCESS HOLE REF DOCK W.U.G2788H.
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