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 2003UALA00980Clamp · looseUPON LEVEL OFF AT FL340 RECIEVED A RT BLEED DUCT LEAK EICAS MESSAGE. DUCT LEAK BITE PRODUCED STORED FAULT 64 (RT WING LEADING EDGE - BOTH LOOPS IN ZONE BAD) . ERASED CODE FROM MEMORY & CLEARED STATUS MSG. FOUND BLEED DUCT CLAMP IN THE RIGHT LEADING EDGE TO SDR 2003UALA00971Fan · failedRT RECIRCULATING FAN SENT BURNING ODOR THROUGHOUT THE CABIN. THE BEARING FAILED RESULTING IN FAN BLADE CONTACT WITH THE CASE. FAN REPLACEDSDR 2003UALA00977Light · inoperativeEMERGENCY AISLE LIGHT AT ROW 5 INOPERATIVE. RELAMPED.SDR 2003UALA00966Skin · damagedEXTERNAL SKIN FUSELAGE DOUBLER REPAIR INSTALLED AT STA 620 STR 8R AT HMV-2 ON 6-29-02 PER EVA IMC20373 REV B. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW DOUBLER REPAIR PER EVA IMC20373C.SDR 2003UALA00965Floorbeam · corrodedCABIN FLOORBEAM 365 AT RBL 10 TO RBL 45.5 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. CORROSION WAS REMOVED AND FLOORBEAM WAS REPAIRED.SDR 2003UALA00964Skin · crackedNR 2 PYLON OUTBOARD WEB CRACKED AT FORWARD ACCESS PANEL INBOARD SKIN LOWER AFT RADIUS. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED REPAIR OF PYLON SKIN PER MM 54-31-99 FIGURE 803.SDR 2003UALA00961Skin · dentedBODY STATION 588 TO 624 STR 15L TO 17L HAS A DOUBLER INSTALLED WITH DENTS NEXT TO IT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2003UALA00950Charger · inoperativeEMERGENCY LIGHTS INOP, OUTSIDE OF AFT CARGO DOOR, AISLE LIGHT AT ROW 25, EXIT SIGN ON CEILING PANEL AT ROW 16. REPLACED EMERGENCY BATTERY CHARGER AND BATTERY PACK.SDR 2003UALA00944Skin · dentedSKIN DENTED AT STA 732, STRINGER 28R. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2003UALA00940Skin · dentedFOUND SMALL DENT AFT OF DOOR 3 RIGHT, ABOUT 20 INCHES AFT OF DOOR 3 RIGHT OUTSIDE EMERGENCY LIGHT. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.SDR 2003UALA00939Web · corrodedAFT PIT CARGO DOOR CUTOUT THRESHOLD SILL WEB CORRODED UNDER THRESHOLD PLATE. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED WEB REPAIR.SDR 2003UALA00937Skin · dentedTWO DENTS LT FUSELAGE AT STA 606, STR 15L AND 16L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2003UALA00938Web · corrodedAFT PIT CARGO DOOR CUTOUT THRESHOLD SILL WEB CORRODED UNDER THRESHOLD PLATE. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED WEB REPAIR.SDR 2003UALA00915Skin · damagedLEFT EXTERNAL FUSELAGE SKIN, BS 600 ABOVE STR 18L IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. REPAIRED PER EVA MOC1-8454.SDR 2003UALA00914Battery Pack · malfunctionedFIRST CLASS EEL LIGHTS TURN OFF AFTER 1 MINUTE. REPLACED POWER SUPPLY & BATTERY PACK M732.SDR 2003UALA00898Anode Terminal · failedELEC BURNING ODOR EMANATING FROM VIDEO MONITOR. MONITOR WAS REPLACED. FOUND UNIT TO EMIT AN ELECTRICAL ODOR UPON INITIAL POWER UP TESTING. UNIT HAD A FAILURE OF THE HIGH VOLTAGE CRT ANODE TERMINAL OF THE FLYBACK TRANSFORMER. THIS FAILURE IS RARE.SDR 2003UALA00890Skin · damagedARCING ON EXTERNAL FUSELAGE SKIN AT STA 319.5, STR 2 RT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER REPAIR.SDR 2003UALA00889Skin · dentedEXTERNAL FUSELAGE SKIN DENTED SEVERAL LOCATIONS FWD OF DOOR 2L AT APPROX BS 608-627 BETWEEN STR 15L AND 17L. MAJOR REPAIR ACCOMPLISHED. REPLACED EXISTING SMALL DOUBLER AND INCORPORATED INTO LARGE EXTERNAL DOUBLER.SDR 2003UALA00883Relay · burnedGROUND CREW REPORTED SMOKE IN AFT PIT. SMOKE FROM DUCTING AND FORWARD WALL AREA. CAUSE APPEARS TO BE A STUCK AFT CARGO HEATER RELAY. STUCK RELAY ALLOWED HEATER TO OVERHEAT TO POINT WHERE SILICONE WRAPPED HEATER RIBBON MELTED, CAUSING SMOKE. MELTING OF RIBBSDR 2003UALA00880Frame · dentedFRAME RETURN FLANGE HAD DENT DAMAGE 2 PLACES BS 1400 AND BS 1420, BETWEEN STRINGERS 25L-27L. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.SDR 2003UALA00879Skin · damagedFUSELAGE SKIN BETWEEN STA 595-625 AND STR 15L TO STR 18L IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.SDR 2003UALA00878Skin · dentedTWO SMALL DENTS FWD OF DR2L. DENTS ARE APPROX 3 X .062 INCH D. SMOOTH, CRACK FREE AND NO PULLED FASTENERS. LOCATED APPROX 3 INCHES ABOVE WATERLINE BETWEEN STA 600 AND 620. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.SDR 2003UALA00872Fan · brokenELECTRICAL BURNING ODOR IN FORWARD CABIN AND FLIGHT DECK. THE EQUIPMENT COOLING FAN HAD A WORN SHAFT AND EXHIBITED SHAFT END PLAY, ALLOWING THE BLADES TO CONTACT THE HOUSING. THIS WAS THE ORIGINAL FAN INSTALLED. FAN REPLACEDSDR 2003UALA00868Idg · failedDIVERTED TO HNL WITH RIGHT ENGINE GENERATOR PROBLEM. RIGHT INTEGRATED DRIVE GENERATOR (IDG) FAILURE. REPLACED RIGHT IDG. NORMAL WEAR, FOUND ONE BAD DIODE.SDR 2003UALA00877Skin · dentedDENT AFT AND LOWER OF DOOR 3R. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.SDR 2003UALA00860Cover · brokenEMERGENCY EXIT LIGHTS SWITCH IN COCKPIT WON'T ARM SWITCH WHEN COVER IS CLOSED. REPLACED BROKEN SWITCH COVER. EMERGENCY LIGHTS TEST OK.SDR 2003UALA00851Skin · dentedFUSELAGE RIGHT SIDE LOWER SKIN DENTED AND CREASED BS 215, STR 26R. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED DOUBLER REPAIR.SDR 2003UALA00847Cap · installedRETURNED TO FIELD DUE TO SMOKE IN THE CABIN. A YELLOW PROTECTIVE CAP WAS LT ON THE DEOILER OVERBOARD BREATHER TUBE AFTER ENGINE INSTALLATION. AT ENGINE START, THE EXISTENCE OF THE CAP ALLOWED THE INTERNAL OIL PRESSURE TO BUILD UP SUFFICIENTLY TO UNSEAT SEVERSDR 2003UALA00832Intercostal · corrodedAFT PIT INTERCOSTAL HAS CORROSION STA 1500 TO 1513 STR 30R TO STR 29R. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW PART PER SRM 51-40-02 & BOEING DWG 146N5451.SDR 2003UALA00828Pitot Tube · obstructedCAPTAINS AIRSPEED INDICATOR FAILED TO ADVANCE PAST 80 KNOTS. RUDDER RATIO AND MACH SPEED TRIM MESSAGES ILLUMINATED. MECHANIC FOUND LARGE BUG NESTING INSIDE CAPTS PITOT PROBE. ( RESTRICTING RAM PRESSURE). REMOVED AND CLEANED OUT BUG. THE BUG WAS LIKELY INSSDR 2003UALA00824Wire Harness · damagedRT CENTER BOOST PUMP OVERRIDE CB POPS ON P6-4 PANEL. WIRING DAMAGE IN THE RH WHEEL WELL AS A RESULT OF ELECTRICAL ARCING. THE EVENT OCCURRED DURING A "C" CHECK VISIT WHEN TECHNICIANS WERE PERFORMING A ROUTINE INSULATION RESISTANCE CHECK OF THE FUEL PUMP. ANALSDR 2003UALA00820Shear Tie · corrodedSHEAR TIE HAS CORROSION, STA. 1628 TO STA 1620, AND STR 29L AND 28L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SHEAR TIE.SDR 2003UALA00819Shear Tie · corrodedAFT PIT WEB ON AFT SIDE OF STA 1540, AND AT STR 29R AND 29L HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SHEAR TIE.SDR 2003UALA00818Shear Tie · corrodedAFT PIT, STA 1520 & STR 29R AND 29L, SHEAR TIE HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SHEAR TIE.SDR 2003UALA00812Stud · failedRIGHT ENGINE SHUT DOWN DURING TAXI DUE TO HIGH ENGINE OIL TEMP. FUEL OIL HEAT EXCHANGER AND VALVE WERE REPLACED AND PROBLEM SEEMED FIXED. NO DISCREPANCIES FOR NEARLY FOUR WEEKS. THEN LOW OIL QUANTITY AND INCREASING OIL TEMPERATURE HIT AGAIN. NR 5 BEARING PRESSDR 2003UALA00806Module · leakingLT HYDRAULIC SYSTEM QUANTITY DECREASE. THE CAUSE OF THIS EVENT WAS AN INCORRECT UNION/SEAL COMBINATION ON THE LT SLAT/FLAP DEPRESSURIZATION MODULE. THE SEAL/RETAINER WAS REPLACED WITH THE CORRECT PACKING.SDR 2003UALA00837Wedge · delaminatedT/E WEDGE DELAMINATED, SLAT NR 6. MAJOR REPAIR ACCOMPLISHED. REPLACED WITH NEW T/E WEDGE.SDR 2003UALA00787Skin · damagedFUSELAGE SKIN AT STATION 525 & STRINGER 3R IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2003UALA00785Skin · gougedEXTERNAL FUSELAGE SKIN HAS 2EA GOUGES AT BOTTOM OF 3 INCH LONG BY 2 INCH HIGH DENT, AT STA 770 BETWEEN STR 15L AND 16L.SDR 2003UALA00776Skin · damagedFUSELAGE SKIN ON STA 610 AT STR 16LT IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE. INSTALLED DOUBLER AND FILLER REPAIR.SDR 2003UALA00772Valve · defectiveFUEL IMBALANCE BETWEEN LT AND RT TANKS. THE CAUSE OF THE FUEL IMBALANCE CONDITION WAS DUE TO A DEFECTIVE CROSS-FEED VALVE BODY ASSY. SHOP FINDINGS REVEALED THAT THE SPLINE AND SEAL ON THE VALVE DISK WERE WORN OUT. THIS WAS THE FIRST TIME THE VALVE WAS REMOVED SDR 2003UALA00756Frame · corrodedINBD CAP OF FRAME AT STA 1681 WL 209 IS EXFOLIATED. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED REPAIR IAW EVA MOCI-8433A.SDR 2003UALA00751Skin · dentedFUSELAGE SKIN DENTED AT BS 1690 AND STRINGER S-20L LAP. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2003UALA00750Skin · crackedFUSELAGE SKIN DENTED AND CRACKED AT STA 1600 AND STR 19L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2003UALA00749Stringer · dentedFUSELAGE STRINGER S-20L DENTED AT BS 1690 LAP. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2003UALA00748Stringer · dentedSTRINGER DENTED AT STATION 1600, STRINGER 19L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2003UALA00743Seal Seat · detectedFLT DIVERTED DUE TO SMOKE IN CABIN. ENGINE REMOVED AND NR 1, 2&3, NR 3 FORWARD & NR 3 AFT CARBON SEALS ALL REMOVED AND CHECKED. ALL CARBON SEALS CHECKED GOOD, MATING SURFACES OF SEAL SEATS OF NR 3 FWD & NR 3 AFT WERE FOUND TO HAVE HEAT CRACKS. MICROCRACKS ARE SDR 2003UALA00733Light · inoperativeRT AFT DOOR EXTERIOR EMERGENCY-SLIDE RAFT LIGHT IS INOPERATIVE. RELAMPED. CHECKS OK.SDR 2003UALA00726Line · crackedNR 2 ENGINE OIL QUANTITY DROPPED STEADILY IN FLIGHT. REPLACED CRACKED & LEAKING FUEL/OIL HEAT EXCHANGER RETURN LINE. LINE CRACKED DUE TO LIBERATED TUBE CLAMP.SDR 2003UALA00711Oil System · overheatedRETURNED TO FIELD DUE TO HIGH OIL TEMPERATURE NR 2 ENGINE. FUEL OIL HEAT EXCHANGER AND VALVE WERE REPLACED AND PROBLEM SEEMED FIXED. NO DISCREPANCIES FOR NEARLY FOUR WEEKS. THEN LOW OIL QUANTITY AND INCREASING OIL TEMPERATURE HIT AGAIN. NO. 5 BEARING PRESSURE
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