Boeing 757-222

Service difficulty reports · 15,539

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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"

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SDR FDEA201405191077Crease Beam · corrodedCREASE BEAM UPPER SURFACE CORRODED BS 1040 - 1020, RT SIDE. REMOVED CORROSION IAW SRM 51-10-02 AND FOUND OUT OF LIMITS IAW SRM 53-40- 13, FIG. 101, DETAIL VII. REMOVED AND REPLACED CREASE BEAM INNER ANGLE BS 900-1040 IAW SRM 51-40-02 AND DWGS 144N5152, SH. May 19, 2014 · N797FD · Boeing 757222 · Fuselage Main, StructureSDR CALA2014052291112Hydraulic System · malfunctionedC HYD SYS PRESSURE MESSAGE ON EICAS. PERFORMED QRH PROCEDURE. YAW DAMPER KICKED OFF & NOTICED DIFFERENCE IN FLIGHT CONTROL PERFORMANCE. PRESSURE WENT TO ZERO ON BOTH CENTER ELECTRIC PUMPS. RECEIVED CTR HYD EICAS MESSAGE & IAW QRH SHUT OFF CTR PUMPS. DURINGMay 19, 2014 · N576UA · Boeing 757222 · Hydraulic System, MainSDR FDEA201405191078Frame · dentedFORWARD PIT RT FRAME INNER FLANGE DENTED AT BS 640, BETWEEN STRINGER 23R - 24R. FOUND TO BE OUT OF LIMITS. R & R FRAME IAW SRM 51-40-02 & DWG 143N1011-38. MAJOR REPAIR.May 19, 2014 · N797FD · Boeing 757222 · Fuselage Main, FrameSDR CALA2014051991070Floorbeam · scratchedSCRATCHES ON TOP OF MAIN CABIN FLOORBEAM AT BS 680 BETWEEN LBL 23 TO RBL 23. REPAIRED CABIN FLOORBEAM BS 680 RBL 24 IAW ECRA 5310-05536. REMOVED SCRATCHES ON FLOORBEAM BS 680 LBL 23 TO FLOORBEAM REPAIR IAW SRM 51-10-02 FIG 1 004.May 19, 2014 · N522UA · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA201405181068Skin · damagedFUSELAGE SKIN HAS NUMEROUS NICKS & SCRATCHES BETWEEN STRINGER 26LT & RT BS 520 - 540. REPAIRED IAW SRM 53-00-01 FIG.201, REPAIR 16, REV.111. MAJOR REPAIR.May 18, 2014 · N795FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR CALA2014051991071Pressure Switch · faultyLEADING EDGE SLAT DISAGREE MSG ON EICAS, FLAPS STUCK BETWEEN 1 & UP WOULD NOT MOVE IAW CHECKLIST. REPLACED FLAP & SLAT DEPRESSURIZATION MODULE V10060 PRESS SWITCH IAW WDM 27-51-31, ITEM 95 REF IPC 27-51-29 IAW AMM 27-51-29 PG 213 PARK. ACCOMPLISHED OPERATIONMay 18, 2014 · N574UA · Boeing 757222 · Trailing Edge Flap Control SystemSDR CALA2014051991068Bearing · wornRIGHT ELEVATOR OTBD PCA IDLER LINK INBD BEARING WORN HAS APPROXIMATELY .070 RADIAL PLAY. LIMIT IAW MM 27-31-05 P G 601 .003 INCH. REACTION LINK TRUNION BEARING SPINS IN TRUNION HOUSING.May 18, 2014 · N510UA · Boeing 757222 · Elevator Control SystemSDR CALA2014051991072Idler Link · wornDURING INSPECTION, LT ELEVATOR PCA'S FOUND ALL THREE IDLER LINKS WITH EXCESSIVE WEAR. WEAR LIMIT IAW 27-31-05-6 01 IS REFERRED TO BY AMM 27-31-05 PG 424 SUB PARAGRAPH F 1. LARGEST LIMIT FOR ANY BEARING IN THIS REFERENCE .003 INCHES. MOVEMENT NOTED APPROXIMAMay 17, 2014 · N597UA · Boeing 757222 · Elevator Control SystemSDR FDEA201405161047Cargo Track · corrodedMAIN DECK CARGO TRACK AT RBL 45.5 BETWEEN BS 700 & 780 HAS SEVERAL AREAS CORRODED. REMOVED CORROSION IAW SRM 51-10-02 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 DETAIL I FIG. 101 PAGE 102. REMOVED AND REPLACED CARGO TRACK IAW SRM 51-40- 02 AND DWG 143N50May 16, 2014 · N797FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2014051691035Bushing · wornDOOR 2 LT HAS DAMAGE TO OUTSIDE OF DOOR HANDLE PAN ASSEMBLY, APPEARS TO BE FROM DOOR HANDLE RUBBING INTO PAN ASSEMBLY. 2 LT MED HANDLE ASSEMBLY REMOVED FOR TROUBLESHOOTING EXCESSIVE HANDLE MOVEMENT & FORCE REQUIRED. NUMEROUS PARTS WORN & LOOSE. AFTER REPLACMay 16, 2014 · N563UA · Boeing 757222 · Passenger/Crew DoorsSDR FDEA201405151040Floorbeam · corrodedMAIN DECK CARGO FLOORBEAM UPPER TEE HAS AREAS CORRODED BS 1640. FOUND OUT OF LIMITS IAW SRM 53-00-51 PG 104 DET.III. REMOVED AND REPLACED FLOORBEAM TEE IAW SRM 51-40-02 AND DRAWING 146N8211. MAJOR REPAIR.May 15, 2014 · N797FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA201405151032Fitting · wornAFTER REMOVAL OF NR 2 PYLON AFT ENGINE MOUNT FWD SHEAR BOLT FLANGED BUSHING, FOUND BUSHING HOLE OUT OF DWG TOLERANCE. REPAIRED IAW EA F-5450-T036994. REPAIR CLASSIFIED AS MAJOR.May 15, 2014 · N795FD · Boeing 757222 · Engine Mount SectionSDR FDEA201405151030Bushing · out of toleranceAFTER REMOVAL OF NR 1 PYLON AFT ENGINE MOUNT, FWD SHEAR BOLT FLANGED BUSHING FOUND HOLE OUT OF DWG TOLERANCE. REPAIRED IAW EA F0-5450-T036967. REPAIR CLASSIFIED AS MAJOR.May 15, 2014 · N795FD · Boeing 757222 · Engine Mount SectionSDR FDEA201405151046Floorbeam · corrodedMAIN DECK CARGO FLOORBEAM UPPER TEE CORRODED AT BS 1661. REMOVED CORROSION IAW 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIGURE 101, NOTE B PAGE 103. R & R FLOORBEAM TEE IAM SRM 51-40-02 & DWG 146N0501. MAJOR REPAIR.May 15, 2014 · N797FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA201405130993Spar · corrodedRT REAR SPAR AT IRSS 183 CORROSION NOTED. REPAIRED IAW EA F-5710-T0307459 P1.May 13, 2014 · N786FD · Boeing 757222 · Wing Main, Frame StructureSDR CALA2014051691037Lead · damagedEEL STRIP LIGHTING INOPERATIVE FROM ROW 8 THRU ROW 12. REPLACED DAMAGE CROSS AISLE LEAD.May 13, 2014 · N580UA · Boeing 757222 · Light System WiringSDR CALA2014051691036Gate · corrodedNR 2R MED DOOR LOWER GATE FOUND CORRODED. R & R R2 MED DOOR LOWER GATE IAW SM-09-13-25-10-JD.May 13, 2014 · N547UA · Boeing 757222 · Service DoorsSDR FDEA201405130995Fitting · gougedIAW NR N00032 DURING OK TO INSTALL NR 1 PYLON FOUND MID SPAR FITTING INBD LUG BUSHING INNER BORE HAS DEEP SCORED MARKS, WING SIDE. REPAIRED IAW EA F-5740-T0307296 DATED APR 30,2014. TITLE, WINGS & ATTACH FITTINGS NR 1 ENG PYLON INBD WING MOUNTED SIDE LOAD May 13, 2014 · N786FD · Boeing 757222 · Wing, Nacelle/Pylon Attach FittingsSDR FDEA201405130994Frame Splice · corrodedAFT CARGO COMPARTMENT STATION 1540 STRINGER 24L FRAME SPLICE HAS CORROSION. REMOVED FRAME SPLICE STATION 1540 DUE TO ELONGATED HOLES, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DET I. R & R FRAME SPLICE IAW SRM 51-40-05 & DWG 146N1042. REMOVED CORROMay 13, 2014 · N786FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201405120986Floorbeam · corrodedFORWARD CABIN AT BS 365.25 BL 0 & RBL 64 FLOORBEAM CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG. 101, DETAIL VI. REPAIRED FLOORBEAM IAW SRM 53-00-51, REPAIR 8, FIG 201, DWG 141N5112. MAJOR REPAIR.May 12, 2014 · N797FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA201405120987Crease Beam · corrodedCORROSION FOUND ON THE CREASE BEAM INNER ANGLE BS 1040. REMOVED CORROSION IAW SRM 51-10-02, FOUND OUT OF LIMITS IAW SRM 53-40-13 FIG 101 DET. VII REMOVED AND REPLACED CREASE BEAM ANGLE IAW SRM 51-40-02 AND DWGS 144N5214 SHEET 1 AND 144N5200 SHEETS 2,3,4. MAJOMay 12, 2014 · N797FD · Boeing 757222 · Fuselage Main, StructureSDR CALA2014051391017Stringer · damagedBLIND FASTENER ON UPPER EXTERNAL FUSELAGE AT BS 572, STRINGER 6L. R & R BLIND FASTENERS WITH SOLID FASTENER ON UPPER FUSELAGE AT BS 572 STRINGER 6L IAW SRM 53-00-01. REPAIRED DAMAGE STRINGER COMMON TO THE BLIND FASTENER HOLE AT BS 572 STRINGER 6L IAW SRM 53-0May 12, 2014 · N535UA · Boeing 757222 · Fuselage Main, Longeron/StringerSDR FDEA201405110977Skin · corrodedEMPENNAGE RT SIDE APU INLET AREA, AFTER INLET REMOVAL FOUND CORROSION ON THE AFT SIDE OF THE CUT OUT AT BS 1825 FROM STRINGER 3 - 6R. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-80-15. REPAIRED IAW SRM 53-80-15 FIG 202 DETAIL 11 REPAIR 1 REV 112. May 11, 2014 · N795FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201405100972Floorbeam · corrodedCABIN, STATION 310.5 RBL 40 - RBL 42 FLOORBEAM UPPER CHORD FOUND CORROSION. COMPLIED WITH EA F-5310-T0307994 PART 1. MAIN DECK FLOOR BEAM UPPER CHORD REPAIR AT STA 310.5 RBL 36 TO RBL 44. REPAIR CLASSIFIED AS MAJOR.May 10, 2014 · N795FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA201405100973Crease Beam · crackedCABIN, STATION 996 - 1020 LT CREASE BEAM WEB CRACKED AT LIGHTING HOLE EDGE. EVALUATED CRACK & FOUND OUT OF LIMIT AS PER SRM 53-40-13 FIG 101 REV 111. CRACK CREASE BEAM WEB REMOVED AS PER SRM 51-40-02 REV 111. CREASE BEAM WEB FABRICATED & INSTALLED AS PER BOMay 10, 2014 · N795FD · Boeing 757222 · Fuselage Main, StructureSDR CALA2014051391016Cable · misinstalledDURING FCD 2560 - 02646 INSPECTION FOUND CABLE ATTACHED INCORRECTLY RT OVERWING SLIDE. REINSTALLED CABLE.May 10, 2014 · N504UA · Boeing 757222 · Emergency EquipmentSDR CALA2014050990996Skin · dentedSMALL DENT RT FUSE BS 1625 BELOW STRINGER 18 JUST FWD & BELOW 4 RT. REPAIRED DENT IN FUSELAGE EXTERNAL SKIN BS 1625 BETWEEN STRINGER 18R & STRINGER 19R IAW SRM 53-00-01 FIG 201 REPAIR 2. DENT WAS ON DOUBLER NO ALLOWABLE LIMITS NOTED.May 9, 2014 · N535UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201405080965Firewall · wornFUSELAGE RT SIDE AFT SIDE OF THE APU FIRE WALL AT BS 1885 THERE IS A WEAR MARK AT RBL 7 INCHES & 6 INCHES FROM THE BOTTOM OF THE FIRE WALL CAUSED BY THE RT APU DOOR SAFETY LATCH. REPAIRED IAW SRM 53-80-08, FIG 201, REPAIR 2, REV 111. REPAIR IS MAJOR.May 8, 2014 · N795FD · Boeing 757222 · Fuselage Main, BulkheadSDR FDEA201405080961Support Angle · corrodedDURING EMPENNAGE RT HAND SIDE, APU INLET AREA AFTER INLET REMOVAL, FOUND CORROSION ON THE UPPER SIDE OF THE CUT OUT AT BS 1790 - 1823 STRINGER 3R. SUPPORT ANGLE REPLACED IAW SRM & DWG 148N3105 SHT.1 REV. C. REPAIR IS MAJOR.May 8, 2014 · N795FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201405080962Strap · corrodedEMPENNAGE RT HAND SIDE APU INLET AREA. AFTER INLET REMOVAL FOUND CORROSION ON THE FWD SIDE OF THE CUT OUT AT BS 1790 FROM STRINGER 3 - 6. SKIN STRAP REMOVED AND REPLACED WITH NEW IAW DWG 148N3105 SHT.1 REV.C. REPAIR IS MAJOR.May 8, 2014 · N795FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR CALA2014050990995O-Ring · damagedFLUID DRIPPING FROM FRONT OF LT MAIN GEAR TRUCK. REPLACED BLEED PLUG O RING IAW IPC 32-32-15-005 ITEM 10. REINSTALLED PLUG IAW AMM 32-32-15 ITEM G STEP 12 PG 408. RESTORED HYD POWER & NO LEAKS NOTED.May 8, 2014 · N521UA · Boeing 757222 · Main Landing Gear Strut/Axle/TruckSDR FDEA201405070955Crease Beam · corrodedBS 1180 - 1200 LT CREASE BEAM WEB CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 111. FOUND OUT OF LIMITS IAW SRM 53-60-13. NEW CREASE BEAM WEB FABRICATED IAW DRAWING 146N5590 SHT 1 REV F. REMOVED & REPLACED IAW DRAWING 146N5590 SHT 1 REV F AND SRM 51May 7, 2014 · N795FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201405070957Seat Track · corrodedMID CABIN SEAT TRACK AT RBL 24.5 BETWEEN BS 700 - 780, HAS SEVERAL AREAS CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 DETAIL I FIG.101 PAGE 102. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40- 02 AND DWG 143N5090May 7, 2014 · N797FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2014050690968Apu · leakingAPU OIL CONSUMPTION ABOVE LIMIT, LEAK CHECKED APU FOUND OIL COMING OUT FROM THE DRAIN FOR THE BEARING CAVITY SEAL., OIL CONSUMPTION RATE IS MORE THAN LIMIT. APU CONTROL UNIT IS -20. START TO LOOK AT FIM49-11-00.May 6, 2014 · N543UA · Boeing 757222 · APU Core EngineSDR CALA2014050690969Altimeter · faulty2 ELEC ALTIMETER FLUCTUATES WITH NORMAL OR ALTERNATE STATIC SELECTED. POS, 01=CAPT, 02=F-0. FO ALTIMETER STICKS WHEN CLIMBING & JUMPS WHEN LEVEL. SWITCHED ADC, NO HELP. REPLACED FO`S ALTIMETER IAW MM34-13-01, OPERATIONS CHECKED GOOD.May 5, 2014 · N550UA · Boeing 757222 · Altimeter, Barometric/EncoderSDR CALA2014050690966Skin · dentedFUSE SKIN DENT AT STATION 275 JUST BELOW STRINGER 19R. CUT OUT DAMAGE & SKIN THICKNESS IS .045 INCH AREA. INSTALLED REPAIR DOUBLER THICKNESS IS .050 IAW SRM 53-00-01 REPAIR 3 FG 201.May 5, 2014 · N535UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR CALA2014050690965Interphone · malfunctionedCABIN CALL WORKS BETWEEN FA & COCKPIT, BUT TONE ALSO RINGS IN COCKPIT, NO LIGHTS, WHEN FA'S CALL, ABLE TO DUPLICATE PROBLEM . CHIME WAS EVEN GOING OFF CONTINUOUSLY. RESET POWER TO AC. CHIME & COMM BETWEEN FA STATIONS & FLIGHT DECK NOW ALL CHECK GOOD, NO HISTMay 5, 2014 · N521UA · Boeing 757222 · Interphone/Passenger Announcement (PA) SystemSDR CALA2014050690970Conduit · damagedFOUND NLG NOT COMPRESSED SENSOR, S10067, FLEXIBLE CONDUIT DAMAGED AMM 32-09-08 PAGE 201. REMOVED SENSOR & INSTALLED NEW ELBOW.May 4, 2014 · N578UA · Boeing 757222 · Landing Gear Position and WarningSDR CALA2014050690971Fuse · defectiveR1 PAX DOOR EMER LIGHT INOPERATIVE. RELAMPED R1 PAX DOOR EMER LIGHT. PERFORMED TROUBLESHOOTING & FOUND DEFECTIVE FUSE AT POWER SUPPLY M370. R & R FUSE & PERFORMED OPERATIONS TEST, TESTED OK IAW WDM 33-51-12 & AMM 33-15-07.May 3, 2014 · N587UA · Boeing 757222 · Emergency LightingSDR FDEA201405030932Frame Splice · corrodedHIDDEN DAMAGE FRAME SPLICE STA 1480 STRINGER 24L CORRODED. EVALUATED CORROSION IAW SRM 53-00-07 FIG 101 DETAIL 2, FOUND TO BE OUT OF LIMITS. ORIGINAL MATERIAL IS .071 INCHES, MATERIAL REMOVED IS .021 INCHES & MATERIAL REMAINING IS .050 INCHES. FABRICATED SPMay 3, 2014 · N786FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201405030931Frame Splice · corrodedHIDDEN DAMAGE FRAME SPLICE STA 1420, STRINGER 24L CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DET 1. R & R FRAME SPLICE PN FX146N1012-3 IAW SRM 51-40-02 & DWG 146N1012 STA 1420, STRINGER 24L. MAJOR REPAIR.May 3, 2014 · N786FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201405030928Frame · chafedCABIN STATION 1640 STRINGER 7L - 8L FRAME HAS CHAFED MARKS.May 3, 2014 · N795FD · Boeing 757222 · Fuselage Main, FrameSDR CALA2014050690967Controller · malfunctionedWHEN PERFORMING THE REVERSE FLOW PROTECTION CHECK THE LT NR 1 ENG APPEARED TO HAVE A COMPRESSOR STALL & WENT SUB-IDLE & STAYED THERE WITH BOTH ENG BLEED VLVS OPEN. THE ISOLATION VLV OPEN & BOTH THROTTLES INITIALLY AT IDLE THE DUCT PRESS WAS NORMAL AROUND 15 PMay 2, 2014 · N537UA · Boeing 757222 · Pneumatic Distribution SystemSDR CALA2014050290949Mechanism · lack of lubeLEFT OVERWING DISABLE HANDLE IS BINDING WHETHER ARMING OR DISARMING HANDLE. LUBED MECHANISM & HARDWARE, HANDLE MOVES FREELY, OK TO CONTINUE.May 2, 2014 · N514UA · Boeing 757222 · Emergency EquipmentSDR FDEA201404300890Frame · corrodedBS 1520 FRAME, STRINGERS 9-10L, OUTER FLANGE CORRODED. REPAIRED IAW SRM 53-00-07 FIG.201, REPAIR 3, REV.111 AND SRM 51-40-02 REV.111. REPAIR IS MAJOR.Apr 30, 2014 · N795FD · Boeing 757222 · Fuselage Main, FrameSDR CALA2014043090935Sill · corrodedCORROSION ON AFT CARGO COMPARTMENT DOOR CUT OUT LOWER SILL AT BS 1400 FRONT SIDE. CORROSION AFT CARGO BAY DOOR CUT OUT LOWER SILL BS 1400 STRINGER 27R FOUND TO BE OUT OF LIMITS MATERIAL LOSS .013 INCHES, ORIGINAL THICKNESS .071 INCHES, REMAINING .058 INCHES IApr 29, 2014 · N537UA · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201404290883Skin · damagedEXISTING REPAIR FINDING EXISTING REPAIR DOUBLER EXTERIOR SKIN HAS NICKS & SCRATCHES AT STATION 1825 - 1834, STRINGER 25L - 27L. EXISTING REPAIR DOUBLER REMOVED & NEW REPAIR CARRIED OUT IAW EA F-5330-T0308296 PART 1. EXISTING REPAIR FOUND ON FUSELAGE INTERIORApr 29, 2014 · N795FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201404280872Mount · damagedNR 2 ENGINE HOLES IN AFT MOUNT LOWER HANGER FITTING LT & RT BUSHING LUG FOUND OVERSIZED. REPLACED IAW EA F-7120-T0307726 PT1. REPAIR IS MAJOR.Apr 28, 2014 · N795FD · Boeing 757222 · Engine Mount SectionSDR FDEA201404280871Mount · damagedNR 1 ENG SN 727243 HOLES IN AFT MOUNT LOWER HANGER FITTING LT & RT BUSHING LUGS FOUND OVERSIZED. REPLACED IAW EA F-7120-T0307726 PT1. REPAIR IS MAJOR.Apr 28, 2014 · N795FD · Boeing 757222 · Engine Mount SectionSDR FDEA201404280874Frame · deformedFRAME AT BS 1380 S2L, LOWER FLANGE AFT EDGE FOUND DEFORMED. FRAME FROME S2-7L REPAIRED IAW SRM 53-00-07 FIG.201, REPAIR 3, REV.111. REPAIR IS MAJOR.Apr 28, 2014 · N795FD · Boeing 757222 · Fuselage Main, Frame
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