N541US

Service difficulty reports · 144

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N541US' AND registry_match = 'registration'
  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 DALA14028815641Skin · damagedAFT LOWER FUSELAGE, ACCESS DOOR 313AL LANDING IS CORRODED BS 1885. REMOVED CHORD AFT LOWER FUSELAGE ACCESS DOOR 313AL LANDING IAW SRM 51-40-02, FABRICATED NEW IAW SRM 51-40-05, 51-10-02 & DWG 148N3601, REV A. INSTALLED IAW SRM 51-40-02 AND DWG 148N3601, REVMay 8, 2014 · N541US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA14029055641Door Sill · corrodedFWD CARGO DOOR CUTOUT LOWER SILL IS CORRODED 2 PLACES BS 580. REF CP53-122-01L DOT 11-01. REMOVED CORROSION ASSOCIATED ER/A 00-524961 ADDED FOR AC 5641, ACCOMPLISHED REPAIR ON FWD CARGO DOOR CUTOUT LOWER SILL IAW ER/A 524961-14, REV ORIGINAL. SECTION I, REPAIMay 5, 2014 · N541US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA14028745641Gate · corrodedR4 DOOR LOWER GATE, LOWER SURFACE CORRODED IN SEVERAL AREAS. R & R LOWER GATE IAW MM 52-11-38. PERFORMED SATISFACTORY LEAK CHECK IAW MM 05-51-24.May 5, 2014 · N541US · Boeing 757251 · Service DoorsSDR DALA14028005641Floor Support · corrodedMAIN CABIN BETWEEN BS 408-418, LBL 64, FLOOR SUPPORT CORRODED. REMOVED CORROSION AT CREASE BEAM. ASSOCIATED ER/A 00-524963 ADDED FOR REMOVED CORROSION AT CREASE BEAM IAW SRM 51-10-02 OUT OF LIMITS IAW SRM 53-30-13, FIG 101, CUT OUT DAMAGED AREA 22" LONG IAW Apr 29, 2014 · N541US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA14027025641Skin · dentedPREVIOUSLY INSTALLED EXTERNAL REPAIR DOUBLER ON LT FUSELAGE, BS 580-610 BETWEEN STR 15-18L HAS DENT DAMAGE. REMOVED PREVIOUS REPAIR. DOUBLER STA 580-STA 610, STR 15-STR 18 LT ASSOCIATED ER/A 00-524965, ADDED FOR AC 5641.Apr 28, 2014 · N541US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA14028805641Skin · corrodedLEFT WING UPPER INBD SURFACE, IN THE WING WALK AREA NUMEROUS AREAS OF CORROSION. WS 70.5-W.S 150 FROM SKIN SPLICE TO REAR SPAR. REMOVED CORROSION, PERFORMED DVI HFEC OF REWORKED AREA & FASTENERS HOLES, PENETRANT INSP. NO DEFECTS NOTED. FLAP, TOP COATED WORKEApr 27, 2014 · N541US · Boeing 757251 · Wing, Plate/SkinSDR DALA14026455641Membrane · corrodedMAIN CABIN, BS 1680-1720, LBL 54-RBL 54 MEMBRANE UPPER SURFACE HAS MULTIPLE AREAS OF CORROSION. REMOVED CORROSION IAW SRM 51-10-02 AND 51-20-01. COMPLIED WITH UT THICKNESS INSPECTION TO AREAS IAW NDTM P4 51-00-10. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51,Apr 25, 2014 · N541US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA14025965641Floor Support · corrodedMAIN CABIN AT BS 407, RBL 12, FLOOR SUPPORT CORRODED. REMOVED DAMAGE FLOOR SUPPORT IAW SRM 51-40-02. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51. LOCATED AND DRILLED NEW FLOOR SUPPORT IAW DWG 141N5185 AND 141N5161 AND SRM 51-40-05. INApr 24, 2014 · N541US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA14025955641Crease Beam · corrodedMAIN CABIN CREASE BEAM BS 1020-1040, RBL 64, CORRODED. REMOVED CORROSION IAW SRM 53-40-13 & 51-20-01. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13. CUT OUT DAMAGE SECTION OF CREASE BEAM IAW ER/A 52495-14, REV D, HFEC INSPECTED CUT OUT AREA IAW NDTM 51-00-19. Apr 24, 2014 · N541US · Boeing 757251 · Fuselage Main, StructureSDR DALA14025925641Angle · corrodedMAIN CABIN AT BS 760, LBL 60 ANGLE CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13. CUTOUT DAMAGE IAW ER/A 524951-14, REV O, HFEC INSPECTED CUTOUT AREA IAW NDTM P6, 51-00-19, NO CRACKS NOTED. FABRICATED NEW PARTS IAApr 24, 2014 · N541US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA14025915641Floor Support · corrodedMAIN CABIN FLOOR SUPPORT AT BS 412, RBL 12, CORRODED. REMOVED DAMAGED FLOOR SUPPORT IAW SRM 51-40-02 AND REMOVED CORROSION FROM FLOOR SUPPORT. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51. FABRICATED FLOOR SUPPORT IAW DWG 141N5185, REV A AND DWG 141N5161RWC, Apr 24, 2014 · N541US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA14025945641Floor Support · corrodedAFT CARGO FLOOR SUPPORT CORRODED BS 1520, S29L. REMOVED FLOOR SUPPORT IAW SRM 51-40-02. FABRICATED FLOOR SUPPORT IAW DWG PL146N5443, REV J. LOCATED AND DRILLED NEW FLOOR SUPPORT IAW SRM 51-40-05. INSTALLED IAW 51-40-02, DWG PL146N5443, REV J.Apr 22, 2014 · N541US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA14027015641Skin · corrodedAFT LOWER FUSELAGE SKIN SHOWS LARGE AREA OF CORROSION ON PRODUCTION SPLICE, BS 1720 BETWEEN STR 27-30R, REMOVED CORROSION AT AFT LOWER FUSELAGE SKIN.Apr 20, 2014 · N541US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA14024555641Crease Beam · corrodedMAIN CABIN AT BS 780, CREASE BEAM CORRODED. REPAIRED IAW ER/A 524962-14, REV O.Apr 20, 2014 · N541US · Boeing 757251 · Fuselage Main, StructureSDR DALA14024545641Floorbeam · corrodedMAIN CABIN FLOORBEAM AT BS 365, BL 0-RBL 62 CORRODED. REMOVED CORROSION. COMPLIED WITH UT THICKNESS INSPECTION TO AREA IAW NDTM P4, 51-00-10 A 9710, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51. CUTOUT FLOORBEAM UPPER TEE FROM LBL 11-RBL 70. COMPLIED WITH HApr 18, 2014 · N541US · Boeing 757251 · Fuselage Main, Floor BeamSDR DALA14025175641Crease Beam · corrodedMAIN CABIN BETWEEN BS 720-755, RBL 64 CREASE BEAM CORRODED. REMOVED CREASE BEAM. LOCATED AND DRILLED NEW CREASE BEAM AND INSTALLED IAW SRM 51-40-02, PAR 7 AND 4 AND 51-40-05 AND 51-40-08Apr 15, 2014 · N541US · Boeing 757251 · Fuselage Main, StructureSDR DALA14022975641Floorbeam · corrodedMAIN CABIN FLOORBEAM AT BS 680, LBL 30 HAS LIGHT CORROSION. REMOVED CORROSION ON FLOORBEAM IAW SRM 51-10-03, PAR 15 AND 51-20-01, PAR 4. COMPLIED WITH UT INSPECTION TO AREA IAW NDT P5 51-10-00. FOUND TO BE OUT OF LIMITS IAW SRM 51-00-06. CUTOUT DAMAGE, FABApr 12, 2014 · N541US · Boeing 757251 · Fuselage Main, Floor BeamSDR DALA14022965641Deck Plate · corrodedMAIN CABIN AFT UPPER DECK PLATE HAS CORROSION AT BS 1712, RBL 51. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51, FIG 101, FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 53-60-51, FIG 201, REPAIR 2.Apr 12, 2014 · N541US · Boeing 757251 · Fuselage Floor PanelSDR DALA14022955641Deck Plate · corrodedMAIN CABIN AFT UPPER DECK PLATE HAS CORROSION AT BS 1714, RBL 28. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51, FIG 101 & 51-20-01 FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 53-60-51, FIG 201, REPAIR 2.Apr 12, 2014 · N541US · Boeing 757251 · Fuselage Floor PanelSDR DALA14022945641Deck Plate · corrodedMAIN CABIN AFT UPPER DECK PLATE HAS CORROSION AT BS 1713, BL 0. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51, FIG 101 & 51-20-01. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 53-60-51, FIG 201, REPAIR 2 AND INSTALLED.Apr 12, 2014 · N541US · Boeing 757251 · Fuselage Floor PanelSDR DALA14022935641Deck Plate · corrodedMAIN CABIN AFT UPPER DECK PLATE HAS CORROSION AT BS 1687, BL 0. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51, FIG 101 & 51-20-01. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 53-60-51, FIG 201, REPAIR 2 AND INSTALLED.Apr 12, 2014 · N541US · Boeing 757251 · Fuselage Floor PanelSDR DALA14022925641Deck Plate · corrodedMAIN CABIN AFT UPPER DECK PLATE HAS CORROSION AT BS 1682, LBL 13. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51, FIG 101 & 51-20-01, FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 53-60-51, FIG 201, REPAIR 2 AND INSTALLED.Apr 12, 2014 · N541US · Boeing 757251 · Fuselage Floor PanelSDR DALA14022915641Seat Track · gougedMAIN CABIN BS 880, RBL 25 SEAT TRACK GOUGED. REMOVED SEAT TRACK BS 880 - 900, IAW SRM 51-40-02 AND INSTALLED NEW IAW SRM 51-40-02.Apr 10, 2014 · N541US · Boeing 757251 · Fuselage, Seat/Cargo Attach FittingsSDR DALA14021775641Seat Track · gougedMAIN CABIN SEAT TRACK AT BS 879, RBL 25 GOUGED. EVALUATED GOUGED FOUND TO BE PUNTURE 100 PERCENT MATERIAL LOSS, OUT OF LIMITS IAW SRM 53-00-52. REMOVED SEAT TRACK FROM BS 780 TO 879, IAW SRM,Apr 8, 2014 · N541US · Boeing 757251 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13042825641Battery Pack · inoperativeEMERGENCY LIGHTS FOR AISLE SEATS 24 THRU 28 INOPERATIVE. R & R BATTERY PACK, OPS CHECKED GOOD IAW MM 33-51.Sep 4, 2013 · N541US · Boeing 757251 · Emergency LightingSDR DALA13011375641Skin · damagedLIGHTNING STRIKE FWD BS 218.4 STRINGER 29R. DRILLED OUT DAMAGED FASTENER IAW SRM 53-00-01. PERFORMED HFEC REF NDTM PT 6. 51-00-16. NO DEFECTS NOTED. INSTALLED FASTENER IAW SRM 53-00-01. ACFT OK FOR SERVICE.Mar 8, 2013 · N541US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA12016535641Connector · disconnectedEMERGENCY LIGHTS AT ROW 31 AND 33 INOPERATIVE. REINSERTED CONNECTOR AT SEAT 31 AND CLEANED CONNECTOR AT SEAT 33. CHECKED OK AT BOTH SEATS.Dec 18, 2012 · N541US · Boeing 757251 · Light System WiringSDR DALA12016195641Skin · damagedMULTIPLE LIGHTNING STRIKES ON LEFT LOWER FUSELAGE. INSPECTED LIGHTNING STRIKES, REPAIRED LIGHTNING STRIKES IAW SRM 53-00-01, SECTION 1.Dec 13, 2012 · N541US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA1166605641Skin · crackedNR 2 ENGINE PYLON OUTBOARD FORWARD LIGHTENING HOLE CRACK 1.5 INCH LONG UNDER STIFFENER. NR 2 PYLON RIGHT STRUT SKIN AT NAC STA 128 NAC WL 138 REPAIRED IAW ER/A 490588-14 REV A.Nov 23, 2011 · N541US · Boeing 757251 · Nacelle/Pylon, Plate/SkinSDR DALA1164335641Floor Support · corrodedAFT CARGO CUTOUT FLOOR SUPPORT FOUND CORRODED FROM STA 1380 STA 1440. FLOOR SUPPORT REPLACED AS PER B757-200 SRM 51-10-02 & INSTALLED AS PER B757-200 SRM 51-40-02.Nov 22, 2011 · N541US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1164325641Panel · corrodedAFT CARGO STA 1377, LBL 20-23 SIDE PANEL FOUND CORRODED. AFT CARGO STA 1377 LBL 20-23 SIDE PANEL REPAIRED IAW B757- 200 SRM 51-70-13 FIG 1.Nov 22, 2011 · N541US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1164385641Skin · crackedPASSENGER TELEPHONE ANTENNAS AT BS 1550 STR 28R FWD MOUNTING HOLE 1EA RIVET HOLE FOUND CRACK APPROX 3/32 INCH LONG AS MARKED STR 28R. PASSENGER TELEPHONE ANTENNAS FWD MOUNTING SKIN HOLE 1EA REPAIRED IAW ER/A 497645-14 REV O. DENT DECAL INSTALLED FOR INSP/MTCNov 17, 2011 · N541US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA1164375641Skin · dentedPAX DOOR - L4 DOOR INT SKIN FOUND PUNCH MARK AT UPPER HINGE ARM. L4 DOOR INTERIOR SKIN AT UPPER HINGE ARM AREA PATCH. REPAIRED IAW ER/A 497647-14 REV O.Nov 17, 2011 · N541US · Boeing 757251 · Passenger/Crew DoorsSDR DALA1158695641Battery Pack · inoperativeDURING MAINTENANCE VISIT, FOUND BOTH EXTERIOR, AFT EMERGENCY LIGHTS INOP AND FOUND AISLE EMERGENCY LIGHTS AT SEAT LOCATIONS 22ABC, 26ABC AND 28DEF INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK FOR INOPERATIVE EXTERIOR LIGHTS AND REPLACED POWER SUPPLY FOR AISOct 17, 2011 · N541US · Boeing 757251 · Emergency LightingSDR DALA1138665641Adi · defectiveEN ROUTE NRT TO SPN AT THE HALFWAY POINT, PILOTS REPORTED ELECTRICAL SHORT AND FUMES FROM FIRST OFFICERS ADI. PULLED CIRCUIT BREAKER AND SHORT AND FUMES STOPPED. PILOTS DID NOT DECLARE AN EMERGENCY. MAINTENANCE PERFORMED WIRING CHECKS AND REPLACED THE ADI. Jun 8, 2011 · N541US · Boeing 757251 · Integrated Flight SystemSDR DALA1134955641Bleed Air Sys · warning messageABORTED TAKEOFF AT LESS THAN 80 KNOTS DUE TO A RIGHT ENGINE BLEED MESSAGE. MAINTENANCE PERFORMED PNEUMATIC HEALTH CHECK ANE REPLACED MULTIPLE PARTS. HIGH POWER ENGINE RUN AND OPERATIONAL CHECKS WERE GOOD.May 15, 2011 · N541US · Boeing 757251 · Engine Bleed Air SystemSDR DALA1107985641Power Supply · inoperativeEMERGENCY EGRESS EXTERIOR LIGHTS AT DOOR 4L INOP. REPLACED POWER SUPPLY, CHECKED OK.Feb 1, 2011 · N541US · Boeing 757251 · Emergency LightingSDR NWAA092645641Power Supply · defectiveDURING AN OVERNIGHT LINE CHECK MAINTENANCE FOUND THE EMERGENCY EXIT SIGN AT DOOR ONE LEFT TO BE INOPERATIVE. MAINTENANCE FOUND THE POWER SUPPLY TO BE DEFECTIVE AND REPLACED IT. SYSTEM OPERATION WAS NORMAL AFTER THE POWER SUPPLY WAS REPLACED.Jul 28, 2009 · N541US · Boeing 757251 · Emergency LightingSDR NWAA074035641Stringer · crackedDURING "M" CHECK, FOUND CRACK IN STRINGER AT BS 1680-1681 S15L. REPAIRED PER EA 56-210582.Dec 7, 2007 · N541US · Boeing 757251 · Fuselage Main, Longeron/StringerSDR 0301655641O-Ring · rupturedLEFT HYDRAULIC QUANTITY DECREASED TO .14, EDP DEPRESSURIZED. WITH ELECTRIC PUMP OFF QUANTITY CONTINUED TO DECREASE UNTIL THERE WAS A TOTAL LOSS OF FLUID. AIRCRAFT DIVERTED TO ALB DECLARING A YELLOW EMERGENCY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. INSPECTED AAug 27, 2003 · N541US · Boeing 757251 · Hydraulic Pump (Electric/Engine), MainSDR 0002525641Indicator · failedUPON GEAR EXTENSION FOR LANDING, THE LEFT AND RIGHT MAIN LANDING GEAR GREEN LIGHTS DID NOT INDICATE DOWN AND LOCKED. EXTENDED GEAR USING ALTERNATE METHOD. DECLARED AN EMERGENCY. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE LEFT AND RIGHT GEAR INDICATORJul 19, 2000 · N541US · Boeing 757251 · Landing Gear Position and WarningSDR 0001685641Sequence Valve · malfunctionedDURING LANDING GEAR RETRACTION AFTER TAKEOFF, RECEIVED ''DOORS'' AND ''GEAR'' AMBER DISAGREE LIGHTS ALONG WITH EICAS MESSAGES ''GEAR DISAGREE'' AND ''GEAR DOOR''. ALSO, HAD STRONG BUFFET APPARENTLY FROM NOSE GEAR. CYCLED LANDING GEAR AND LIGHTS AND MESSAGES CMay 2, 2000 · N541US · Boeing 757251 · Landing Gear Door Retract SectionSDR 9800095641Compressor · stalledDURING TAKEOFF ROLL, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL. TAKEOFF WAS ABORTED AT 10 KTS. BORESCOPE INSPECTION REVEALED COMPRESSOR DAMAGE. MAINTENANCE REPLACED THE NR 2 ENGINE.Jan 2, 1998 · N541US · Boeing 757251 · Turbine Engine Compressor SectionSDR 9705175641Fuel Cutoff Sw · out of positionDURING CLIMB, THE NR 2 ENGINE FUEL CONTROL CUTOFF SWITCH WAS INADVERTENTLY KNOCKED TO CUTOFF POSITION. SWITCH WAS RETURNED TO CORRECT POSITION IMMEDIATELY. NO ENGINE POWER LOSS OR PARAMETER EXCEEDANCE OCCURRED BUT AN ENGINE STALL WAS EXPERIENCED DUE TO THE FMar 9, 1997 · N541US · Boeing 757251 · Engine Fuel Distribution
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