Boeing 757-251

Service difficulty reports · 4,706

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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 = '757251'
  ORDER BY difficulty_date DESC"

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SDR DALA2016030901804Stringer · gougedAFT RT CABIN FS 1480 AT STR 5 GOUGED FWD AND AFT OF FRAME. SUMMARY, SEE NR FOR ADDITIONAL INFORMATION 193-0001:2526-01257-03B/009 00132, PRI 543886-14, REV ORIG DATED 09FEB16 AT 1900, MATCHES FINAL ERA 543886-14, REV ORIG, REPAIR COMPLETED IAW ERA 543886-14, Mar 8, 2016 · N541US · Boeing 757251 · Fuselage Main, Longeron/StringerSDR DALA2016030801802Web · corrodedAFT CARGO BAY BS 1440-1460, RBL 23, OTBD SIDE CORNER CORRODED ON WEB. FOUND WEB AT BS 1440 TO 1460, RBL 23 IN AFT PIT TO BE CORRODED 80 PERCENT THRU MATERIAL, THIS IS OUT OF LIMITS IAW SRM 53-60-15, PAGE 107. R & R WEB IAW DWG 146N8522, REV E. SRM 51-40-02, Mar 7, 2016 · N538US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA2016030601798Skin · damagedLIGHTNING STRIKE DAMAGE AT BS 800, STR 3-4 LT SIDE. WORKING PRI 544587-14. C/W PRI INSTRUCTIONS PRI 544587-14, REV 3. C/W FINAL ERA544587-14AD, REV ORIGINAL SECTION 1 PERMANENT REPAIR COMPARED FINAL ERA TO PRI INSTRUCTIONS NO CHANGES NOTED.Mar 5, 2016 · N555NW · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA2016030601797Skin · damagedLIGHTNING STRIKE DAMAGE AT BS 500, ETR 7, LT SIDE 2 LOC. REMOVED DAMAGE AT LOWER LOCATION W 5/32 DRILL BIT HFEC INSPECTED IAW SRM 53-00-01, REPAIR 6 WITH NO ITEMS AT LOCATION BS 500, STR 7L. CUTOUT DAMAGE IAW SRM 53-00-01, REPAIR 2, FIG 201. C/W HFEC OF CUTOMar 5, 2016 · N555NW · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA2018013100599Structure · dentedDENT FOUND ON THE AFT CARGO DOOR FWD LOWER CORNER. LOCATED DRILLED, ALODINED, PRIMED, INSTALLED AND APPLIED TOP COAT TO DOUBLER FOR AFT CARGO DOOR LOWER FWD, CORNER IAW SRM.Feb 29, 2016 · N548US · Boeing 757251 · Cargo/Baggage DoorsSDR DALA2016022901659Light · shortedGIRT BAR CIRCUIT BREAKER TRIPPED ON ARRIVAL AT AIRCRAFT. FOUND ARM LIGHT AT 2R SHORTED REPLACED SAME IAW ASM 25-66-01. OPS CK OK FOR SERVICE.Feb 28, 2016 · N536US · Boeing 757251 · Door System WiringSDR DALA2019092705570Shim · missingWINGLET INSTALLATION MOD. SHIMS HAVE BEEN FOUND TO BE MISSING, INSPECTION STRINGERS U-9.5 AND U-11.5 SHIMS HAVE BEEN FOUND TO BE MISSING, COMPLIED WITH ERA 544393-14 REV.CFeb 26, 2016 · N541US · Boeing 757251 · Wing Miscellaneous StructureSDR DALA2016022601469Girt Bar · dirtyL2 DOOR WILL NOT DISARM UPON ARRIVAL. CLEANED GIRT BAR DOOR ARMS/DISARM OK.Feb 26, 2016 · N542US · Boeing 757251 · Emergency EquipmentSDR DALA2016022001344Seat Track · crackedDURING INSTALLATION OF LAV G FITTING, MOD FOUND SEAT TRACK SUPPORT CHANNEL CRACKED AT BS 653, RBL 45. REMOVED SEAT TRACK SUPPORT FROM BS TO 780, RBL 45 . VERIFIED MATERIAL AND FABRICATED IAW DWG 143N5120, REV C, LOCATED AND DRILLED IAW DWG 143N5120 INSTALLED Feb 19, 2016 · N536US · Boeing 757251 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016022501438Skin · damagedNR 2 SLAT ASSY, L/E SKIN WAS DAMAGED AND ASSY WAS REMOVED FROM THE ACFT. L/E BOTTOM SKIN WAS GOUGED FROM OSS 642.8 THRU 646.8. EA 56-215777 WAS ISSUED AND SEC I REPAIR WAS ACCOMPLISHED IAW SHOP ORDER, OM812-206435. FOLLOW ON STEPS REQUIRED: SEC II. INSPECTIOFeb 16, 2016 · N535US · Boeing 757251 · Leading Edge DevicesSDR DALA2016020901018Seat Track · brokenUPON REMOVAL OF SEATS, FOUND BROKEN SEAT TRACK SCALLOP AT APPROXIMATELY LBL 45, BS 1442. REPLACED BROKEN SEAT TRACK IAW SRM 53-00-52, REPAIR 1, FIG 201, FROM BS 1320-1540.Feb 8, 2016 · N536US · Boeing 757251 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016020900992Access Panel · corrodedLT WING FUEL TANK PANEL ACCESS CUTOUT 541 FB HAS LIGHT CORROSION.Feb 8, 2016 · N541US · Boeing 757251 · Wing, Plate/SkinSDR DALA2016020800991Proximity Sensor · failedCIRCUIT BREAKER TRIPS WHEN ENTRY DOORS ARE ARMED FOR PUSHBACK. TROUBLESHOT IAW WDM 25-66-11, VERIFIED RT PROXIMITY SENSOR BAD. R & R RT GIRT BAR PROXIMATELY SENSOR AT 4R DOOR REF WDM 25-66-11 AND SWPM CH 20-30. DOOR SLIDE ARM LIGHT. OPS CHECK NORMAL.Feb 3, 2016 · N549US · Boeing 757251 · Emergency EquipmentSDR DALA2016022501430Ballscrew · corrodedNR 5 INBD T/E BALLSCREW CORRODED IAW NR 159. REPLACED NR 5 BALLSCREW, REF: AMM 27-51-11 ON NR 159. UNSUCCESSFUL PARTS CHANGE SENT TO RECORDS 63783.Feb 2, 2016 · N541US · Boeing 757251 · Trailing Edge Flap ActuatorSDR DALA2016121510233Skin · damagedERA 532818-14 SECTION I WAS ISSUED FOR A FUSELAGE SKIN REPAIR AT STA 660, S-7L TO S-8L. CURRENT ERA REVISION IS 'A'. SCHEDULING HAS CHANGED. ACCOMPLISHED SKIN REPAIR STA 640 AT S-7L PER ERA 532818-14 REV C SECTION II PERMANENT REPAIR ACCOMPLISHED ID REPAIR PEFeb 1, 2016 · N550NW · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA2016020100810Battery Pack · inoperative2R DOOR EXIT SIGN AND CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY & CKS NORMAL IAW AMM 33-51.Jan 30, 2016 · N537US · Boeing 757251 · Emergency LightingSDR DALA2016012900803Stringer · damagedLEFT CABIN STR AT BS 1280 HAS 3 EA OUT OF ROUND HOLES FOR STOW BIN MOUNT HANGAR FITTING. REMOVED DAMAGE LT CABIN STR AT BS 1274-1286, STR 5 IAW SRM 53-00-03, REP 1, FIG 201 SHEET 1, STEP 1, INSTALLED NEW -2 FILLER SECTION AND FWD AND AFT HAT SECTION IAW SRM 5Jan 28, 2016 · N550NW · Boeing 757251 · Fuselage Main, Longeron/StringerSDR DALA2016012700670Stringer · damagedSTRINGER 16L DAMAGED AT BS 610 IAW ER/A 543429-14, STEP 14 ACCOMPLISHED STRINGER REPAIR ON STR 16L IAW SRM 53-00-03, REPAIR 1.Jan 27, 2016 · N557NW · Boeing 757251 · Fuselage Main, Longeron/StringerSDR DALA2016012700673Skin · damagedSKIN DAMAGED BETWEEN BS 620 AND 640 AND STRINERS 17 - 18L.Jan 25, 2016 · N557NW · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA2016012600640Handle · detachedL4 DOOR HANDLE FELL OFF. REPLACED HANDLE, OK FOR SERVICE.Jan 25, 2016 · N540US · Boeing 757251 · Passenger/Crew DoorsSDR DALA2016012500575Fitting · damagedLEFT CABIN STR AT BS 1280 HAS 3 EA OUT OF ROUND HOLES FOR STOW BIN MOUNT HANGAR FITTING. REMOVED DAMAGE LT CABIN STR AT BS 1274-1286, STR 5 IAW SRM 53-00-03, REP 1, FIG 201, SHEET 1, STEP 1, INSTALLED NEW -2 FILLER SECTION AND FWD AND AFT HAT SECTION IAW SRMJan 24, 2016 · N550NW · Boeing 757251 · Fuselage Main, Attach FittingsSDR DALA2016012500579Unknown · smokePERFORMED AN AIR TURNBACK, DUE TO SMOKE IN THE CABIN. IAW LOG 7893748, INSPECTED DOOR AREA HEATERS NTF, INSPECTED ENGINES AT FULL THRUST TAKEOFF POWER WITH ENGINE A/I ON/OFF NTF, INSPECTED ENGINES FOR FLUID LEAKS AND BLEED SYSTEM NTF. INSPECTED 2.5 BLEED PORTSJan 23, 2016 · N545US · Boeing 757251 · Air Distribution SystemSDR DALA2016012000515Bearing · corrodedLT WING-FLAP TORQUE TUBE BEARING, HANGER BEARINGS LOOSE/RUSTY AT NR 3-NR 4 TORQUE TUBE. R & R AND OPS TESTED FOR THE TORQUE TUBE SUPPORT BEARING IAW AMM 27-51-25.Jan 18, 2016 · N548US · Boeing 757251 · Trailing Edge Flap Control SystemSDR DALA2016011900465Lug · corrodedNR 5 FLAP BALL SCREW YOKE LUGS PITTED. SUMMARY, NR FOR ADDITIONAL INFORMATION 318-0001:2751-2538/003, 00265. REPLACED BALL SCREW, REF AMDS 2751-0001.Jan 16, 2016 · N549US · Boeing 757251 · Trailing Edge FlapsSDR DALA2016011400324Door Sill · corrodedAFT CARGO DOOR SILL HAS CORROSION ON NUT PLATE STRIP. INSTALLED CORNER SCUFF PLATES IAW AMM 53-13-02. COMPLETED INSTALL OF NUT STRIP IAW DWG 146N8522.Jan 14, 2016 · N549US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA2016011400323Window Frame · corrodedWINDOW FRAME CORRODED, RT SIDE FWD OF R2 DOOR BETWEEN BS 620 AND BS 640. SUMMARY, FOR ADDITIONAL INFORMATION, NR 190-0001:2522-01090- 01B/001 00281. REPAIRED IAW SRM 56-20-02.Jan 13, 2016 · N549US · Boeing 757251 · Fuselage Main, StructureSDR DALA2016011400316Ball Screw · corrodedBALLSCREW INNER HOUSING RUSTED. REPLACED NR 4 FLAP BALLSCREW ON AMDS WORKCARD 113-0001: 2751-2538. BALL, SCREW & N OFF 55-2743-9-0002 05648 ON 55-2743-9-0002 00154.Jan 13, 2016 · N548US · Boeing 757251 · Trailing Edge Flap Control SystemSDR DALA2016011100168Skin · corrodedRT HORIZONTAL STABILIZER UPPER SKIN CORRODED AT APPROXIMATELY RIB 12-11, BS 272. BLENDED CORROSION FOUND 100 PERCENT MATERIAL LOSS, OUT OF LIMITS IAW SRM 55-10-01, FIG 1.0, DETAIL V REPAIRED IAW ERA 540731-14, REV ORIGINAL.Jan 10, 2016 · N547US · Boeing 757251 · Horizontal Stabilizer, Plate/SkinSDR DALA2016011100169Yoke · corrodedLEFT WING NR 3 FLAP DRIVE UNIVERSAL AFT YOKE HAS CORROSION/RUST INSIDE YOKE BORE. REPLACED YOKE, REF: AMM 27-51-11.Jan 8, 2016 · N549US · Boeing 757251 · Trailing Edge Flap Control SystemSDR DALA2016010700075Plate · damagedDAMAGE FOUND ON UPPER CONDUCTIVE PLATE OTBD OF LT ELEVATOR. REMOVED DISBONDED SECTION AND APPLIED TAPE IAW AMM 53-23- 01-801. DEFER TO MON. AT NEXT C CHECK REMOVE SPEED TAPE. CHECK FOR LOOSE FASTENERS, REINSTALL SPEEDTAPE AND RESEAL THE EDGES WITH BMS5-95. REJan 7, 2016 · N547US · Boeing 757251 · Horizontal Stabilizer StructureSDR DALA2016011500371Jackscrew · corrodedNR 5 FLAP SCREWJACK INNER HOUSING RUSTED. INSTALLED IAW AMDS CARD 113-0002: 2751-2542 BALL, SCREW & N OFF 55-2743-9-0002, 05166 ON 55-2743-9-0002, 00110.Jan 1, 2016 · N548US · Boeing 757251 · Trailing Edge Flap Control SystemSDR DALA2016010100038Threshold · corrodedAFT CARGO COMPARTMENT, DOOR THRESHOLD SIDE PLATE HAS 3 EA SPOTS OF CORROSION. REMOVED CORROSION ORIG "T" .063 REMAINING .047 LOSS OF .016, LOSS IS OUT OF LIMITS. R & R SIDE PLATE IAW SRM 51-40-02, DWG 146N5393.Dec 31, 2015 · N547US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA2015123007761Charger · inoperativeEMERGENCY LIGHT AT M731 INOPERATIVE. REPLACED CHARGER ASSY IAW AMM 33-50, CHECKED OK FOR SERVICE.Dec 29, 2015 · N543US · Boeing 757251 · Emergency LightingSDR DALA2015122807734Battery Pack · inoperativeEMERGENCY EXIT SIGNS INOPERATIVE AT EXIT HATCH AREA. REPLACED BATTERY PACK AT M10567. OPS TESTED NORMAL IAW AMM 33-51.Dec 25, 2015 · N535US · Boeing 757251 · Emergency LightingSDR DALA2015122807733Battery Pack · inoperativeEXTERIOR EMERGENCY LIGHT AT AFT SIDE OF FUSELAGE ON BOTH WING INOPERATIVE. REPLACED BATTERY OF M10954 FOR POWER SUPPLY. OPS CHECKED NORMAL IAW AMM 33-51.Dec 25, 2015 · N535US · Boeing 757251 · Emergency LightingSDR DALA2016011200211Structure · gougedNR 2 CORE COWL AFTER RUB STRIP WAS REMOVED A 4" GOUGE WAS FOUND IN COWL MATERIAL. REMOVED NR 2 ENGINE INBD CORE COWL IAW AMM 71-11-06-004-037-P00. FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 54-41-01, PG 1.0 DETAIL III. INSTALLED A SERVICEABLE CORE COWL IAW AMDec 23, 2015 · N547US · Boeing 757251 · Nacelle/Pylon, Main FrameSDR DALA2015122807732Light · inoperativeEXTERIOR EMERGENCY LIGHT AT DOOR 2R INOPERATIVE. REPLACED DOOR 2R EXTERIOR EMERGENCY LIGHT ASSY IAW AMM 33-51-06. CHECKS OK. LIGHT ASSY BP FROM UA. PN 30-2044-5. SN 9501 ITEM DEF TO BP. REPLACED DOOR 2R EXTERIOR EMERGENCY LIGHT ASSY & EMERGENCY LIGHT OPS Dec 22, 2015 · N539US · Boeing 757251 · Emergency LightingSDR DALA2015122207695Fuse · failedDURING SERVICE CHECK, FOUND LT OUTSIDE EMERGENCY LIGHT OUT. REPLACED THE FUSE. FOUND BETWEEN PIN NR 9, D7764 AND GROUND, 100 OHM MORE. RESEQURED GD2994-DC TERMINAL AND CKS NORMAL IAW MM33-51, WDM 33-51-13.Dec 21, 2015 · N543US · Boeing 757251 · Emergency LightingSDR DALA2015121607631Battery Pack · inoperativeEXTERIOR EMERGENCY LIGHT AT DOOR 1 RT & EMERGENCY LIGHT AT ROW 1 THRU 3 INOPERATIVE. ISOL & T/S BATTERY PACK INOPERATIVE. REPLACED THE BATTERY PACK AND CHECKED OK.Dec 15, 2015 · N543US · Boeing 757251 · Emergency LightingSDR DALA2015120407483Strap · crackedSTABILIZER STRAP AT BS 370, LBL 45 CRACKED. REPAIRED CRACK ON STABILIZER STRAP, BS 370 LBL 45 REF: SRM.Dec 3, 2015 · N551NW · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA2015120207368Battery Pack · inoperativeEMERGENCY LIGHT INOPERATIVE AT 25C AND 29C CEILING LIGHT. REPLACED BATTERY PACK AT POWER SUPPLY M10954, ROW 29F FLOOR IAW AMM 33-51, OPS CK GOOD.Dec 2, 2015 · N556NW · Boeing 757251 · Emergency LightingSDR DALA2015120107344Skin · dentedEXTERNAL UPPER FUSELAGE DENT LOCATED APPROXIMATELY BS 530, STR 3L. FOUND WITHIN ALLOWABLE LIMITS OF SRM 53-00-01, PG 104, DETAIL III. ACCOMPLISHED HFEC INSP IAW NDT PT6 51-00-19, NO DEFECTS NOTED.Nov 30, 2015 · N551NW · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA2015113007303Battery Pack · inoperativeFOUND EMERGENCY LIGHT INOPERATIVE BETWEEN SEAT 26ABC - 30ABC. REPLACED BATTERY PACK AND FUNCTION CHECKED OK IAW AMM33-51.Nov 29, 2015 · N547US · Boeing 757251 · Emergency LightingSDR DALA2015120107345Frame · corrodedDURING H-CHECK, THE BS 138, FRAME WEB WAS FOUND CORRODED AND THE FRAME INNER CHORD WAS FOUND CRACKED BETWEEN STR 23R AND 24R. A REPAIR WAS ACCOMPLISHED IAW SECTION I OF ERA 520461-14. THE REPAIR ACCOMPLISHED IAW SECTION I OF ERA 520461-14 IS APPROV ED FOR STNov 28, 2015 · N545US · Boeing 757251 · Fuselage Main, FrameSDR DALA2015121807669Sidewall Panel · corrodedAFT CARGO COMP RT SIDE PANEL HAS CORROSION AT APPROXIMATELY BS 1445 UPPER SURFACE. R & R IAW SRM 51-40-02 AND DWG 146N5392, REV B; RT SIDE TRANSITION PANEL FROM BS 1400 TO 1480 PN 146N5391 A-TAG NR 64117. CLOSED LOG AND REMOVED MONITOR INSPECTION.Nov 25, 2015 · N551NW · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA2015121007550Frame · crackedCORROSION AND CRACK NOTED ON BS 1380 FRAME WEB AND CHORD. REF ERA 520461-14AD, REV A.Nov 25, 2015 · N545US · Boeing 757251 · Fuselage Main, FrameSDR DALA2015112607299Strap · brokenSTABILIZER STRAP AT BS 377, LBL 45.25 BELOW MAIN CABIN FLOOR FRAME IS BROKEN. REPAIRED STABILIZATION STRAP AT BS 377, LBL 45.25 IAW SRM.Nov 25, 2015 · N545US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA2015112507295Fork · shearedDURING R2 DOOR PASSENGER POWER ACTUATION CABLE CHECK TRIGGER SHAFT SHEARED. REMOVED R2 DOOR TRIGGER FORK AND ROLL PIN IAW AMM 52-11. INSTALLED NEW TRIGGER FORK AND ROLL PIN IAW AMM. PERFORMED ADJUSTMENT CHECK, CKS GOOD.Nov 24, 2015 · N545US · Boeing 757251 · Service DoorsSDR DALA2018032701974Plate · wornCHECK LATCH ON PAX DOOR ON BUTTERFLY SURROUND PLATE. PLATE HAS WEAR THROUGH THE PLATE ON RIGHT SIDE OF HANDLE. REMOVED AND REPLACED THE BLIND BOLTS IAW ER/A 541753-14, REV. ORIGINAL, SECTION III. AMMS 52-11-13-201, AND 52-11-13-902-012.Nov 23, 2015 · N541US · Boeing 757251 · Passenger/Crew DoorsSDR DALA2015112307188Skin · corrodedLT WINGLET EXTRIOR SURFACE OTBD SIDE HAS AREA OF CORROSION AT T/E APPROXIMATELY 18" ABOVE BOTTOM OF WING. REPAIRED IAW PRI 540728-14, REV 0 AND ERA 540728-14, REV ORIGINAL.Nov 21, 2015 · N545US · Boeing 757251 · Wing, Plate/Skin
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