Boeing 757-2B7

Service difficulty reports · 3,730

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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 = '7572B7'
  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 BB07002Fuse · blownR4 DOOR EXTERIOR EMERGENCY LIGHT FOUND INOPERATIVE. MAINTENANCE REPLACED THE FUSE AND RELAMPED.Jan 3, 2007 · N939UW · Boeing 7572B7 · Emergency LightingSDR BB06094Pressure Switch · malfunctionedFLIGHT 1040, CLT-SJU: ON CLIMBOUT, THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED. FLIGHT RETURNED TO CLT. MAINTENANCE REPLACED THE RIGHT ENGINE HYDRAULIC PRESSURE SWITCH (S10541).Dec 31, 2006 · N928UW · Boeing 7572B7 · Hydraulic Pump (Electric/Engine), MainSDR BB06093Windshield · crackedFLIGHT 708, LAS-CLT: DURING FLIGHT, CAPTAINS WINDSHIELD CRACKED. CREW STATED WINDSHIELD WAS BEGINNING TO LEAK AIR. FLIGHT DIVERTED TO MEM. MAINTENANCE REPLACED THE CAPTAINS WINDSHIELD.Dec 28, 2006 · N201UU · Boeing 7572B7 · Flight Compartment WindowsSDR USAA061428Channel · corrodedINBOARD OF AFT LEFT DOOR SILL BETWEEN STA 1640-1660 OF FLOOR STRUCTURE CORRODED. REMOVED & REPLACED PART PER SRM 51-40-01, DEFECT SIZE: 2 X 2 INCHES.Dec 15, 2006 · N938UW · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR USAA061437Panel · crackedOUTBOARD END OF SLAT COVE PANEL CRACKED. FABRICATED NEW COVE PANEL ABOUT 27 INCHES LONG PER BOEING DWG 114N4003, DEFECT SIZE: 1 INCH.Dec 15, 2006 · N938UW · Boeing 7572B7 · Leading Edge DevicesSDR USAA061436Sill · corrodedRIGHT AFT DOOR SILL STA 1660-1680 CORRODED. REMOVED & REPLACED WITH NEW WEB PER SRM 51-40-00; CORR TASK JL-90-0900; LEVEL 1, DEFECT SIZE: 9 X 1.5 INCHES.Dec 15, 2006 · N938UW · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR USAA061435Angle · corrodedANGLE AT STA 300-377 RBL 61 CORRODED. FABRICATED & INSTALLED NEW ANGLE PER BAC DWG 141N8322; CORR TASK JL-43-53501; LEVEL 1, DEFECT SIZE: 1.5 X 9 INCHES.Dec 15, 2006 · N938UW · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR USAA061434Crease Beam · corrodedBETWEEN STA 324-327 RBL 60 CORRODED. REMOVED & REPLACED 2 CREASE BEAMS PER SRM 51-40-02; CORR TASK JL-46-53500, LEVEL 1, DEFECT SIZE: 120 SQ INCHES.Dec 15, 2006 · N938UW · Boeing 7572B7 · Fuselage Main, StructureSDR USAA061433Floorbeam · corrodedLOCATION: BETWEEN FR 16 AND 17 AND -Y50 REMOVED AND REPLACED FLOORBEAM AND BRACE IAW SRM 51-72-00; CORR TASK JA-220-53500; LEVEL 1 DEFECT SIZE: 5 SQ. IN.Dec 15, 2006 · N938UW · Boeing 7572B7 · Fuselage Main, Floor BeamSDR USAA061432Seat Track · corrodedFWD END SEAT TRACK LBL 45.5 AT STA 377.7 CORRODED. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER DWG 141N5131 & SRM 51-70-12, DEFECT SIZE: 1.5 INCH X 5 FEET.Dec 15, 2006 · N938UW · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA061431Floorbeam · corrodedNUMEROUS AREAS AROUND SCREW HOLES, TOP OF FLOORBEAM STA 377.7 CORRODED. INSTALLED T-CAP & SPLICE ANGLES PER SRM 53-00-51; CORR TASK JL-46-53500; LEVEL 1 DEFECT SIZE: 2.75 INCHES.Dec 15, 2006 · N938UW · Boeing 7572B7 · Fuselage Main, Floor BeamSDR USAA061438Skin · chafedINBOARD FOREFLAP, TRAILING EDGE, BOTTOM SIDE, 12 INCHES OUTBOARD OF AFT FLAP CUTOUT CHAFED. CUT OUT DAMAGE, HONEYCOMB REPAIR WITH DOUBLERS PER SRM 51-70-10, DEFECT SIZE: 1 INCH.Dec 15, 2006 · N938UW · Boeing 7572B7 · Trailing Edge FlapsSDR USAA061427Floorbeam · corrodedTOP CHORD OF FLOOR FRAME 1640 AT LBL 57 CORRODED; CORR TASK JL-58-53516L LEVEL 1. SPLICED IN NEW UPPER T-CAP CHORD & ANGLE DOUBLERS PER TYP REP 53-15-01; SRM 51-40-02; DEFECT SIZE: 2 X 2 INCHES.Dec 15, 2006 · N938UW · Boeing 7572B7 · Fuselage Main, Floor BeamSDR USAA061426Web · corrodedSPORADIC CORROSION BETWEEN STA 1681 & 1720 AND FROM LBL 51 - RBL 51 CORRODED. MANUFACTURED FLOOR WEB PER DWG 146N5300; CORR TASK C53-251-03; LEVEL 1, DEFECT SIZE: 5 SQ INCHES.Dec 15, 2006 · N938UW · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR USAA061425Floorbeam · corrodedSTA 1661 LBL 4 TOP SIDE OF BEAM AROUND HOLE CORRODED. REPLACED CAP OF FLOORBEAM PER TR 53-15-01, DEFECT SIZE: 1 X 2 INCHES.Dec 15, 2006 · N938UW · Boeing 7572B7 · Fuselage Main, Floor BeamSDR USAA061424Crease Beam · corrodedRIGHT CREASE BEAM BETWEEN CHORD & WEB AT STA 1636 CORRODED. REMOVED & REPLACED WEB PER SRM 51-40-02. CORR TASK JA-58-53516, LEVEL 1, DEFECT SIZE: 1 X 3 INCHES.Dec 15, 2006 · N938UW · Boeing 7572B7 · Fuselage Main, StructureSDR USAA061364Web · corrodedLEFT DOOR SILL AFT WEB & SUPPORT CLIP, BETWEEN STA 1660-1681 CORRODED. REMOVED CORROSON PER SRM 53-60-15, TREATED & PRIMED, FAB'D NEW SUPPORT CLIP. CORR TASK JL-58-53516, DEFECT SIZE: 1 X 1 INCH.Nov 29, 2006 · N938UW · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR USAA061266Skin · damagedBEHIND ENG I/B FLAP, 4 INCHES FROM O/B END OF FLAP AND 1 INCH FROM T/E ON RT SIDE. REMOVE DAMAGED FILL WITH POTTING COMPOUND BMS 5-28, INSTALL EXTERNAL DOUBLER SRM 51-70-10, DEFECT SIZE: 1 X .50 INCH.Oct 27, 2006 · N929UW · Boeing 7572B7 · Trailing Edge FlapsSDR USAABB06079Charger · inoperativeDURING MAINTENANCE, 4R EMERGENCY EXIT LIGHT FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND CHARGER.Oct 18, 2006 · N942UW · Boeing 7572B7 · Emergency LightingSDR BB060075Indicator · trippedFLIGHT 773, PHL-LAS: ON APPROACH, RECEIVED LEADING EDGE DISAGREE MESSAGE. EXECUTED GO-AROUND. WHEN CREW BEGAN TO SELECT ALTERNATE FLAP SWITCH, FLAP NEEDLES MATCHED AGAIN AND SYSTEM OPERATED NORMALLY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUNSep 28, 2006 · N940UW · Boeing 7572B7 · Leading Edge Slat Position Indicating SystemSDR BB06073Charger · inoperativePHL - MAINTENANCE REPORTED THE EMERGENCY EXIT SIGN ABOVE THE AFT RIGHT DOOR ALONG WITH THE LEFT LOWER EMERGENCY EXIT SIGN IN THE AFT GALLEY WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT RIGHT BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD.Sep 22, 2006 · N622AU · Boeing 7572B7 · Emergency LightingSDR USAA061150Skin · delaminatedLOCATION: NR 9 SLAT IB AND OB END, UPPER SURFACE FAB'D DOUBLER, APPLIED SEALANT AND TOPCOAT IAW SRM 51-70-10 & 51-70-10 DEFECT SIZE: .100 INCH W X .008 INCH D DENT AND 2 INCHES L X 2 INCHES W X .016 INCH D DELAMINATION..Sep 12, 2006 · N611AU · Boeing 7572B7 · Leading Edge DevicesSDR BB06071Charger · inoperativeMAINTENANCE FOUND EMERGENCY LIGHTS INOPERATIVE AT R4 DOOR EXTERIOR AND INTERIOR OVERHEAD POSITIONS. REPLACED BATTERY CHARGER. NO FURTHER FAULTS.Sep 5, 2006 · N622AU · Boeing 7572B7 · Emergency LightingSDR USAA061103Floorbeam · corrodedFOUND FLOORBEAM CORRODED, BS 700 BL 58L WL 208. FAB'D NEW T CHORD, ANGLES, TRAPS AND INSTALLED PER TYP REP 53-15-01; CORROSION TASK C53-123; LEVEL 1 DEFECT SIZE: 3.5"L BY 1"W BY .016"D.Aug 30, 2006 · N613AU · Boeing 7572B7 · Fuselage Main, Floor BeamSDR USAA061102Crease Beam · corrodedFOUND CORROSION, BS 640-660 BL58L WL 208 CREASE BEAM. FAB NEW SECTION OF CREASE BEAM AND TWO PLATES PER SRM 53-30-13, 51-70-02; CORROSION LEVEL 1; TASK C53-123, DEFECT SIZE: 2"L BY 1"W BY .022"D.Aug 30, 2006 · N613AU · Boeing 7572B7 · Fuselage Main, StructureSDR BB06069Coupling · leakingFLIGHT 0030, LAS-PHL: DURING CRUISE, APU SHUTDOWN WHILE THE RT GENERATOR WAS ALREADY ON MEL. FLIGHT DECLARED AND DIVERTED. MAINTENANCE SECURED THE APU OIL FILL PORT FITTING. THE RT IDG WAS REPLACED TO CLEAR THE RT GENERATOR MEL ON THE OVERNIGHT. NO FURTHER DAug 26, 2006 · N619AU · Boeing 7572B7 · APU Oil SystemSDR BB06067Transmission · failedFLIGHT 1026, TPA-CLT: ON APPROACH, FLAPS FAILED TO MOVE. T/E LIMIT ILLUMINATED AND EICAS MESSAGE (T/E FLAP DISAGREE) AND (FLAP ISOL VAL) DISPLAYED. FLAPS OPERATE NORMAL USING T/E ALTERNATE SYSTEM. CREW DECLARED AN EMERGENCY. LANDED WITH NO FURTHER DIFFICULTIAug 25, 2006 · N624AU · Boeing 7572B7 · Trailing Edge Flap Control SystemSDR USAA061065Gate · corrodedL-1 DOOR LOWER GATE 7/E OUTER SIDE CORROSION. REMOVED CORROSION AND TREATED PER SRM 52-10-02 FIG 101 DETAIL III, DEFECT SIZE: 12" L X 1.0"W X .05"D.Aug 24, 2006 · N613AU · Boeing 7572B7 · Service DoorsSDR USAA061066Gate · corrodedR-2 DOOR LOWER GATE T/E OUTER SIDE CORROSION. REMOVED CORROSION AND TREATED PER SRM 52-10-02 FIG 101 DETAIL XIII, DEFECT SIZE: 12"L X 1.0"W X .05"D.Aug 24, 2006 · N613AU · Boeing 7572B7 · Service DoorsSDR USAA061067Floorbeam · corrodedSTA 740 LBL 45 - LBL 58, WL 208L CORROSION. TREATED, PRIMED & INSTALLED REPAIR PARTS PER SRM 53-00-51; CORR TASK C53-123-02; LEVEL 1, DEFECT SIZE: 2" L X 3"W X .027"D.Aug 24, 2006 · N613AU · Boeing 7572B7 · Fuselage Main, Floor BeamSDR USAA061052Skin · chafedRT WING OUTBD FLAP APPROX 4 FT O/B OF I/B FLAP TRACK CHAFED. CUT OUT DAMAGE, INSTALLED REPAIR PARTS, TREATED, PRIMED & TOP COATED PER SRM 57-53-01 & 51-40-02, DEFECT SIZE: 2.1" X 1.1", DEPTH .060".Aug 22, 2006 · N617AU · Boeing 7572B7 · Trailing Edge FlapsSDR USAA061039Floorbeam · corrodedSTA 324 RBL 40-62 FLOORBEAM CORROSION. CUT OUT DAMAGE, REPLACED WITH NEW SECTION PER EA 97934; CORR TASK C53-221-03; LEVEL 1, DEFECT SIZE: 22" L X .063"D.Aug 10, 2006 · N624AU · Boeing 7572B7 · Fuselage Main, Floor BeamSDR USAA061038Floorbeam · corrodedSTA 310, RBL 40, WL 208, MAIN DECK CORROSION. FAB'D TEE, REPAIR ANGLES, FILLERS PER EA 97933, SRM 53-00-51, 51-40-02; CORR TASK C53-221-03, DEFECT SIZE: 8"L X 2"W X .038"D.Aug 10, 2006 · N624AU · Boeing 7572B7 · Fuselage Main, Floor BeamSDR USAA061015Floor Support · corrodedSTA 398-402, RBL 47-60 CORROSION. REMOVED & REPLACED PART PER SRM 53-10-51, 51-40-02; CORR LEVEL 1; TASK C53-222-03, DEFECT SIZE: 1.5 X 1 INCH.Aug 7, 2006 · N624AU · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR USAA061016Floorbeam · corrodedSTA 377 LBL 62 RBL 62, FLOORBEAM CORROSION. FAB'D NEW T-CHORD & INSTALLED PER TYP REP 53-15-01; CORR LEVEL 1; TASK C53-221-03, DEFECT SIZE: 2"L X 2"W X .024"D.Aug 7, 2006 · N624AU · Boeing 7572B7 · Fuselage Main, Floor BeamSDR BB06061Antenna · failedDURING CRUISE, RADAR ANTENNA FAILED. DIVERTED TO MCO DUE TO WEATHER. MAINTENANCE REPLACED THE RADAR ANTENNA. NO FURTHER FAULTS.Jul 30, 2006 · N610AU · Boeing 7572B7 · Weather Radar SystemSDR USAA060996Floorbeam · corrodedFOUND FLOORBEAM CORRODED FS 1640, RBL 24 RBL 54. INSTALLED NEW PER 53-15-01, 51-20-01, 51-40-02; CORROSION TASK C53-251-03; LEVEL 1 DEFECT SIZE: 1" BY 1" BY .014" AND 1" BY 1" BY .026" AND 1" BY 1" BY .044".Jul 28, 2006 · N624AU · Boeing 7572B7 · Fuselage Main, Floor BeamSDR USAA060995Intercostal · corrodedFOUND CABIN FLOOR BS 350 AND 377.7 BL0 WL 208 CORRODED. INSTALLED NEW INTERCOSTAL PER SRM 51-40-02, 51-40-05; CORROSION TASK C53-221-03; LEVEL 1 DEFECT SIZE: 2"L BY 2"W BY .010"D AND 2"L BY 2"W BY .029"D.Jul 28, 2006 · N624AU · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR USAA060994Floor Support · corrodedFLOOR SUPPORT CORRODED MAIN DECK AT STA 377-395 RBL 60. FAB'D NEW FLOOR SUPPORT AND INSTALLED PER SRM 51-20-01, 53-00-04, 51-40-02; CORROSION TASK C53-222-03, DEFECT SIZE:Jul 28, 2006 · N624AU · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR USAA060993Floor Support · corrodedFOUND CORROSION FLOOR SUPPORT STA 1660-1680, RBL: 54. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 53-00-04, 51-20-01, 51-40-02; CORROSION TASK C53-252-03; LEVEL 1, DEFECT SIZE: 11.5"L BY 1.5"W BY .020"D.Jul 28, 2006 · N624AU · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR USAA060992Floor Support · corrodedFOUND CORROSION MAIN CABIN FLOOR SUPPORT STA 1675 RBL 52. FAB'D NEW FLOOR SUPPORT AND INSTALLED PER SRM 51-20-01, 53-00-04, 51-40-02; CORROSION LEVEL 1; TASK C53-252, DEFECT SIZE: 1.5"L BY 1.0"W BY .050"D.Jul 28, 2006 · N624AU · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR USAA060991Plate · corrodedFOUND DECK PLATE CORRODED, STA 1710 RBL 19 - 29. REPAIR DOUBLER INSTALLED PER SRM 53-00-51, 51-20-01, 51-40-02; CORROSION LEVEL 1; TASK C53-252-03, DEFECT SIZE: 18" BY 6" BY 0.019".Jul 28, 2006 · N624AU · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR USAA060997Floorbeam · corrodedFOUND CORROSION BS 365 WL 208 LBL2 RBL10 RBL 60. FABRICATED NEW T CHORD AND SPLICES PER TYPICAL REPAIR 53-15-01, SRM 51-40-02, 51-40-05; TASK NR C53-221-03 DEFECT SIZE: 1" BY 2" BY .021" AND 2" BY 3" BY .092" AND 2" BY 6" BY .025".Jul 28, 2006 · N624AU · Boeing 7572B7 · Fuselage Main, Floor BeamSDR BB06058Overheat Sensor · failedFLIGHT 714, CLT-BOS: ON APPROACH TO BOS, CREW RECEIVED ENGINE 2 FIRE WARNING. THE NUMBER 2 ENGINE TURBINE OVERHEAT DETECTOR WAS ALREADY ON MEL. CREW SHUTDOWN THE NUMBER TWO ENGINE AND LANDED AT BOS WITH NO FURTHER DIFFICULTIES. MAINTENANCE REPLACED BOTH OVERHJul 23, 2006 · N610AU · Boeing 7572B7 · Overheat DetectionSDR BB06059Actuator · failedFLIGHT 1121, AFTER TAKEOFF, CREW WAS UNABLE TO RETRACT THE LANDING GEAR. FLIGHT RETURNED TO DEPARTURE. MAINTENANCE REPLACED THE RT GEAR TILT ACTUATOR AND LT GEAR TILT POSITIONAL SHUTTLE VALVE PRESSURE SWITCHES.Jul 21, 2006 · N621AU · Boeing 7572B7 · Landing Gear ActuatorSDR BB06055Sensor · openFLIGHT 621, CLT-LAS: AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. FLIGHT RETURNED TO CLT. MAINTENANCE PERFORMED BITE TEST OF PSEU. FOUND SENSOR S10060 FAULTED. REPLACED RIGHT TRUCK TILT SENSOR S10060 AND CONDUIT. EXTENSION AND RETRACTION TEST OK. NO FUJul 16, 2006 · N621AU · Boeing 7572B7 · Landing Gear Retraction/Extension SystemSDR USAA060868Skin · corrodedSTA 1840 STR 25L CORROSION. INSTALLED REPAIR DOUBLER IAW EA 82619, DEFECT SIZE: 6.125 X 4.25 INCHES.Jun 27, 2006 · N610AU · Boeing 7572B7 · Fuselage Main, Plate/SkinSDR USAA060864Skin · corrodedSTA 1840 STR 25L CORROSION. CUT OUT CORROSION INSTALLED DOUBLER IAW EA 82619, DEFECT SIZE: 6.25 X 4.25 INCHES.Jun 26, 2006 · N610AU · Boeing 7572B7 · Fuselage Main, Plate/SkinSDR USAA060861Skin · crackedNR 9 SLAT COVE SKIN AT D/B TRACK CUT-OUT AREA. FABRICATED AND INSTALLED NEW 966 AND 967 ANGLES IAW BOEING DWG 114N4003 AND SRM 57-43-01 FIG 01. DEFECT SIZE: 1.50"Jun 22, 2006 · N610AU · Boeing 7572B7 · Leading Edge DevicesSDR USAA060862Skin · crackedNR 10 SLAT COVE SKIN AT I/B TRACK CUTOUT ANGLE. FABRICATED AND INSTALLED NEW PANEL IAW BOEING DWG 114N4002 AND SRM 57-43-01 DEFECT SIZE: .75"Jun 22, 2006 · N610AU · Boeing 7572B7 · Leading Edge Devices
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