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.

SDR 2005UALA00900Frame · dentedFRAME DENTED AT STA 1620, STR 25R. TRIMMED OUT DAMAGES, ACP HEFC INSP, NO CRACK FOUND. FABRICATE, ALODINE, PRIME, AND INSTALL REPAIR PER TIMCO REO-G10821, REV B.Aug 26, 2005 · N588UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00899Frame · dentedFRAME DENTED AT STA 1500, STR 25L. TRIMMED OUT DAMAGE, ACP HEFC INSP, NO CRACK FOUND. FABRICATE, ALODINE, PRIME, AND INSTALL REPAIR PER TIMCO REO-G10823.Aug 26, 2005 · N588UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00898Frame · dentedFRAME DENTED AT STA 1460 BETWEEN S25L AND S26L. TRIMMED OUT DAMAGES, ACP HEFC INSP, NO CRACK FOUND. FABRICATE, ALODINE, PRIME, AND INSTALL REPAIR PER TIMCO REO-G10825.Aug 26, 2005 · N588UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00897Frame · dentedFRAME DENTED AT STA 1440 BETWEEN S26L AND S27L. TRIMMED OUT DAMAGES, ACP HEFC INSP, NO CRACK FOUND. FABRICATE, ALODINE, PRIME, AND INSTALL REPAIR PER TIMCO REO-G10826.Aug 26, 2005 · N588UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00896Frame · dentedFRAME DENTED AT STA 1380 BETWEEN S26L AND S27L. TRIMMED OUT DAMAGES, ACP HEFC INSP, NO CRACK FOUND. FABRICATE, ALODINE, PRIME, AND INSTALL REPAIR PER TIMCO REO-G10819, REV B.Aug 26, 2005 · N588UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00895Frame · dentedFRAME DENTED AT STA 1540 BETWEEN STR 25R AND STR 26R. TRIMMED OUT DAMAGES, ACP HEFC INSP, NO CRACK. FABRICATE, ALODINE, PRIME AND INSTALL REPAIR PER TIMCO REO-G10820, REV B.Aug 26, 2005 · N588UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00894Frame · dentedFRAME DENTED AT STATION 1480 BTWN S25L AND S26L. TRIMMED OUT DAMAGES, ACP HEFC INSP, NO CRACK FOUND. FABRICATE, ALODINE, PRIME, AND INSTALL REPAIR PER TIMCO REO G10824, REV B.Aug 26, 2005 · N588UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00909Actuator · failedLEADING EDGE SLAT DISAGREE MESSAGE. LEADING EDGE SLAT DISAGREE MSG PER CREW. FOUND NR 6 SLAT ACTUATORS NR 11 AND 12 OVERLOAD INDICATORS POPPED. REPLACED BOTH NR 11 AND 12 SLAT ACTUATORS.Aug 25, 2005 · N507UA · Boeing 757222 · Leading Edge Slat ActuatorSDR 2005UALA00890Actuator · failedDIVERTED TO EWR WITH A SLAT DISAGREE PROBLEM. FOUND NR 6 SLAT ACTUATORS NR 11 AND 12 OVERLOAD INDICATORS POPPED. REPLACED BOTH NR 11 AND 12 SLAT ACTUATORS.Aug 25, 2005 · N507UA · Boeing 757222 · Leading Edge Slat ActuatorSDR 2005UALA00889Smoke · detectedDIVERTED DUE TO SMOKE IN THE CABIN & COCKPIT. MODERATE SMOKE AND FUMES OF ELECTRICAL TYPE IN CABIN AND COCKPIT. FLIGHT DIVERTED TO DTW. INSPECTED GALLEYS, CABIN, CARGO PITS AND BOTH E&E BAYS FOR ELECTRICAL RELATED PROBLEMS. FOUND AUDIO ACCESSORY UNIT WITH STROAug 25, 2005 · N550UA · Boeing 757222 · Air Distribution SystemSDR 2005UALA00888Frame · bentSTA 1340 LEFT HAND SIDE FRAME BENT AT STR 25L. REMOVED EXISTING PRODUCTION SPLICE AND FABRICATED A NEW PRODUCTION SPLICE ANGLE PER TIMCO REO(EVA) G10831, REV C.Aug 25, 2005 · N588UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00887Frame · dentedFRAME HAS A DENT AT STA 1400 BETWEEN STR 26L AND STR 27L, AFT PIT, INBOARD FLANGE. REPAIRED FRAME FLANGE WITH NESTED J-ANGLE TO EXISTING CHORD PER TIMCO REO (EVA) G10828, REV B.Aug 25, 2005 · N588UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00886Frame · dentedFRAME DENTED AT STA 1540 AT STR 26L, AFT PIT, INBOARD FLANGE. REPAIRED FRAME WITH NESTED J-ANGLE REPAIR TO EXISTING CHORD PER TIMCO REO (EVA) G10818, REV BAug 25, 2005 · N588UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00882Fan · failedSTRONG ELECTRICAL ODOR IN MID GALLEY. STRONG ELECTRICAL ODOR IN MID GALLEY AFTER APU GEN FIELD TRIP. REPLACED NR 1 FWD EQUIP SUPPLY FAN.Aug 24, 2005 · N589UA · Boeing 757222 · Air Distribution FanSDR 2005UALA00879Floorbeam · corrodedFLOORBEAM AT BS 324 IS CORRODED FROM THE CIRCUMFERENTIAL FRAME TO THE SPLICE AT RBL 50, AND THE T-CAP. FABED REPAIR PARTS PER SRM 53-00-51, ALODINE, PRIME, AND PAINT. INSTALL REPAIR PARTS PER MM 53-00-98.Aug 24, 2005 · N505UA · Boeing 757222 · Fuselage Main, Floor BeamSDR 2005UALA00858Odor · detectedDIVERTED DUE TO ELECTRICAL ODOR IN THE COCKPIT AND CABIN. ACCORDING TO THE SHOP REPORT, RESISTOR R170 WAS DAMAGED BY OVERHEAT AND CAUSED SOME DISCOLORATION ON THE CIRCUIT BOARD. THIS IS THE TYPE OF FAILURE REPORTED ON BOEING SERVICE LETTER 757-SL-24-069-A. Aug 21, 2005 · N504UA · Boeing 757222 · Air Distribution SystemSDR 2005UALA00874Engine · smokeOBSERVED SMOKE FROM BOTTOM OF NR 1 ENGINE COWLING ON TAXI INTO ORD. LINE MAINTENANCE DETERMINED THAT HYDRAULIC FLUID WAS LEAKING FROM A LOOSE B-NUT. B-NUT WAS TIGHTENED AND SYSTEM WAS CHECKED. NO OTHER LEAKS NOTED.Aug 19, 2005 · N565UA · Boeing 757222 · Engine (Turbine/Turboprop)SDR 2005UALA00854Shear Tie · corrodedSTA 1480 TO 1470 SKIN AND FRAME HAS CORROSION AROUND VHF ANTENNA. REMOVED CORROSION ON SKIN AND FRAME, REPLACED SHEAR TIE PER MM 51-10-02, 51-40-02. MEASURE AFTER DAMAGE REMOVAL, FOUND SKIN AND FRAME ARE WITHIN LIMITS.Aug 19, 2005 · N588UA · Boeing 757222 · Fuselage Internal Mounting StructureSDR 2005UALA00843Battery · dischargedSECTION OF COACH EMERGENCY LIGHTS INOP, REPLACED BATTERY.Aug 18, 2005 · N587UA · Boeing 757222 · Emergency LightingSDR 2005UALA00955Shear Web · corrodedCABIN CORROSION UNDER MIKATA BLOCK AT SHEAR WEB, BS APPROX RBL 56.0. REMOVE CORROSION, ACP HEFC INSP, NO CRACK FOUND. INSTALLED REPAIR DOUBLER PER SRM 41-40-02.Aug 13, 2005 · N588UA · Boeing 757222 · Fuselage Miscellaneous StructureSDR 2005UALA00816Skin · lightning strikeLIGHTNING STRIKE DAMAGE AT STA 860, STR 5L. DRILLED OUT DAMAGE PER SRM 53-00-01, ACP HFEC INSP, NO CRACK FOUND. INSTALLED SOLID FASTENER PER MM 53-00-01.Aug 13, 2005 · N588UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2005UALA01181Flap System · malfunctionedDIVERTED TO SFO DUE TO FLAP RETRACTION PROBLEM.Aug 11, 2005 · N507UA · Boeing 757222 · Trailing Edge Flap Control SystemSDR 2005UALA00818Smoke · detectedSTRONG SMOKE ODOR IN FLIGHT DECK AND SMOKE ODOR AT ROW 16. THE SMELL IN THE CABIN WAS CORRECTED BY SEVERAL RELATED ACTIONS DURING THE TROUBLESHOOTING OF THE AIRCONDITIONING SYSTEM. THE PACKS WERE RECYCLED AND SEVERAL FILTERS WERE REPLACED. NOTE: OVEN WAS REMAug 11, 2005 · N526UA · Boeing 757222 · Air Distribution SystemSDR 2005UALA00811Clamp · looseLOST CABIN PRESSURE. FOUND CLAMP LOOSE IN LEFT AC BAY. REPLACED NUMEROUS SEALS IN LT AND RT AC BAY. PRESSURIZED ACFT. PRESSURIZED OK .Aug 11, 2005 · N546UA · Boeing 757222 · Cabin Pressure Control SystemSDR 2005UALA00802Warning System · activatedRETURNED TO FIELD DUE TO LE SLAT DISAGREE EICAS MESSAGE. FOUND FSCU HAD INTERMITTE FAULT ON SLAT PDU XMIT. CLEANED CONNECTOR. ACP SYSTEM CYCLE OPS NORMAL.Aug 10, 2005 · N507UA · Boeing 757222 · Leading Edge Slat Position Indicating SystemSDR 2005UALA00801Carbon Seal · damagedDIVERTED TO OGG UNDER AMBER ALERT WITH NR 1 ENGINE SHUTDOWN DUE TO LOW OIL QUANTITY INDICATION. ROOT CAUSE WAS THE FAILURE OF THE DE-OILER CARBON SEAL. THIS IS AN ANOMALY, AS THERE WAS NO HISTORY OF HOC PRIOR TO THE EVENT. ALSO IT WAS NOT DUE TO INFANT MORTAug 10, 2005 · Boeing 757222 · Turbine Engine Oil SystemSDR 2005UALA00791Switch · inoperativeL-2 DOOR EMERGENCY LIGHT TEST SWITCH INOP. REPLACED SWITCH.Aug 7, 2005 · N87UA · Boeing 757222 · Emergency LightingSDR 2005UALA00781Skin · damagedFUSELAGE SKIN IS CREASED AT STA 620 LT AND STR 17L. REMOVED DAMAGE SKIN AND REPLACED PER MM 53-30-92- SKIN SPLICE REPAIR, AND REF UA-EVA- 50527.Aug 7, 2005 · N87UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2005UALA00953Floor Panel · corrodedAFT CABIN FLOOR BS 1680 TO 1720, RBL 51 METAL FLOOR CORRODED. REMOVE GALLEY MOUNT FOR ACCESS, REMOVE CORROSION AND INSTALL DOUBLER, ALODINE, PRIME, AND PAINT PER SRM 51-20-01.Aug 6, 2005 · N87UA · Boeing 757222 · Fuselage Floor PanelSDR 2005UALA00777Light · inoperativeEEL FLOOR LIGHT AT SEAT ROW 15 INOP. REPLACE LIGHT STRIP.Aug 6, 2005 · N87UA · Boeing 757222 · Emergency LightingSDR 2005UALA00775Frame · dentedFWD PIT FRAME STA 600, LT 2 EACH DENT STR 24L. TRIMMED OUT DAMAGE, ACP HFEC INSP, NO CRACK FOUND. FABRICATE AND INSTALL REPAIR PER TIMCO REO-G10763, REV B, AND UA EVA-50518.Aug 6, 2005 · N587UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00774Frame · dentedAFT PIT FRAME DENTED STA 1400, STR 26L. TRIMMED OUT DAMAGE, ACP HFEC INSP, NO CRACK FOUND. FABRICATE REPAIR ANGLE PER TIMCO REO- G10758, REV B, AND UA EVA-50516.Aug 6, 2005 · N587UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00773Frame · dentedDENT IN FRAME AT STA 580, STR 24L. TRIMMED OUT DAMAGE, ACP HFEC INSP, NO CRACK FOUND. FABRICATE ANGLE REPAIR PER TIMCO REO-G10764 AND UA EVA-50105.Aug 6, 2005 · N587UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00772Skin · dentedFUSELAGE SKIN IS DENTED AT STR 20R, STA 1719. REMOVE DAMAGE, ACP HEFC INSP, NO CRACK FOUND. FABRICATE AND INSTALL DOUBLER PER TIMCO REO-G10787, AND UA EVA 50524.Aug 6, 2005 · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2005UALA00771Splice · dentedFRAME SPLICE AT STA 1420 BETWEEN STR 24L AND 25L IS DENTED ON TOP IN AFT CARGO PIT. TRIMMED OUT DAMAGE, ACP HEFC NDT INSP, NO CRACK FOUND. REPAIR PER TIMCO REO-G10762, REV B, AND UAL EVA 50517.Aug 6, 2005 · N587UA · Boeing 757222 · Fuselage Main, FrameSDR 2005UALA00883Slide · separatedTHE RIGHT SLIDE BUMPER SEPARATED DURING OVERPRESSURE. INTERNAL SEAM FAILURE CAUSED BUMPER PROFILE TO DISTORT. ANALYSIS BY OEM OF BUMPER INTERNAL SEAM FAILURE SHOWED PROPER SEAM ASSEMBLY. INFLATABLE WAS REPLACED.Aug 3, 2005 · N503UA · Boeing 757222 · Escape SlideSDR 2005UALA00841Skin · damagedEXTERNAL FUSELAGE SKIN DAMAGE AT BS 1701 BTWN STRINGERS 19L-20L. ACCOMPLISH DOUBLER PER EVA-40245.Aug 3, 2005 · N594UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2005UALA00753Skin · dentedEXTERNAL FUSELAGE SKIN AT STA 490, STR 15L HAS DENT. REMOVE DAMAGE AND INSTALL REPAIR DOUBLER PER SRM 53-00-01, REPAIR 4, P201. REPAIR IS A CATEGORY A REPAIR.Aug 3, 2005 · N587UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2005UALA00752Skin · dentedEXTERNAL FUSELAGE SKIN DENTED STA 1723 AT STR 21L. MAJOR REPAIR ACCOMPLISHED PER EVA-40245A.Aug 3, 2005 · N594UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2005UALA00798Slide · leakingTUBE ASSY FAILED AIR RETENTION TEST DUE TO EXCESSIVE POROSITY LEAKING THROUGH TUBE FABRIC NOTED ON VARIOUS LOCATIONS. DURING COMPONENT SHOP MAINTENANCE SLIDE FAILED AIR RETENTION TEST DUE TO FABRIC POROSITY. POROSITY WAS BEYOND CMM LIMITS. SLIDE WAS RETURNED Aug 2, 2005 · N542UA · Boeing 757222 · Escape SlideSDR 2005UALA00746Engine · contaminatedRETURNED TO FIELD UNDER AMBER ALERT DUE TO FUMES IN THE COCKPIT. ODOR DISSAPATED DURING RETURN TO GATE. THE DETERGENT WASH OF THE ENGINES IS THE SORCE OF THE ODOR. PER MM 72-05-99 PAGE 701, ENGINE NEEDS HIGH POWER RUN AFTER WASH TO REMOVE ANY DETERGENT RESIDUAug 1, 2005 · N595UA · Boeing 757222 · Engine (Turbine/Turboprop)SDR 2005UALA00741Pdu · vibrationRETURNED TO FIELD DUE TO AIRCRAFT VIBRATION. TE FLAP PDU DID NOT FUNCTION PROPERLY. REPLACED SUBJECT PDU.Jul 31, 2005 · N502UA · Boeing 757222 · Standard Practices/StructuresSDR 2005UALA00723Battery · dischargedEXTERIOR EMERGENCY SLIDE LIGHT IS INOP. REPLACE EEL BATTERY CHARGER AT DOOR 1L.Jul 27, 2005 · N510UA · Boeing 757222 · Emergency LightingSDR 2005UALA00705Warning Light · illuminatedRETURNED TO FIELD DUE TO THE LEFT GENERATOR DRIVE LIGHT. SHOP FINDINGS INDICATED THAT NO FAULT WAS FOUND. THE IDG OIL PRESSURE SWITCH WAS REPLACED PRECAUTIONARY.Jul 24, 2005 · N544UA · Boeing 757222 · AC Generator-AlternatorSDR 2005UALA00706Lamp · burned outEMERGENCY AISLE ILLUMINATION LIGHT INOP AT ROW 5. REPLACED LAMP.Jul 23, 2005 · N513UA · Boeing 757222 · Emergency LightingSDR 2005UALA00677Keelbeam · corrodedKEEL BEAM CORROSION. EXT CHORD BS 1180 TO 1176, APPROXIMATELY 6 LBL TO 6 RBL. REMOVE CORROSION AND CK LIMIT PER SRM 53-30-12. ORIGINAL THICKNESS=.130", AFTER REPAIR THI CKNESS=.124", LOSS OF MATERIAL IS WITHIN LIMIT PER SRM 53-30-12Jul 20, 2005 · N542UA · Boeing 757222 · Fuselage Main, KeelSDR 2005UALA00799Slide · leakingTUBE ASSY FAILED AIR RETENTION TEST DUE TO EXCESSIVE POROSITY LEAKING THROUGH TUBE FABRIC NOTED ON VARIOUS LOCATIONS. DURING COMPONENT SHOP MAINTENANCE SLIDE FAILED AIR RETENTION TEST DUE TO FABRIC POROSITY. POROSITY WAS BEYOND CMM LIMITS. SLIDE WAS RETURNEDJul 18, 2005 · N513UA · Boeing 757222 · Escape SlideSDR 2005UALA00670Switch · malfunctionedLANDED SFO UNDER AMBER ALERT DUE TO LOSS OF GENERATOR AND APU NO-START. GENERATOR DELTA-P SWITCH REPLACED. OPS CHECK GOOD. NO METAL FOUND ON CHIP DET. IN ADDITION TO REPLACEMENT OF GEN DELTA P SWITCH, CH ITEM INCLUDED TO REPLACE APU GENERATOR DUE TO MULTIPJul 18, 2005 · N517UA · Boeing 757222 · APU Core EngineSDR 2005UALA00689Battery · inoperativeEMERGENCY EXIT LIGHTS AT DOOR 1R INOPERATIVE. REPLACED BATTERY PACK AT M730. REPLACED BATTERY PACK AT M730.Jul 17, 2005 · N596UA · Boeing 757222 · Emergency LightingSDR 2005UALA00669Coffeemaker · shortedCOFFEEMAKER DELIVERED SHOCK TO FLIGHT ATTENDANT IN REAR GALLEY. UNIT TESTED ONLY AFTER BURST HEATER WAS REPLACED. CAN ONLY SPECULATE BURST HEATER CARTRIDGE IN WATER MAY HAVE BEEN SOURCE OF STRAY CURRENT. UNIT BONDING OK.Jul 15, 2005 · N520UA · Boeing 757222 · Buffet/Galleys
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