N575UP

Service difficulty reports · 252

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 = 'N575UP' 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 IPXA2026102153875Window · crackedARRIVAL FOUND L1 WINDOW CRACK.Oct 21, 2026 · N575UP · Boeing 74744AF · Flight Compartment WindowsSDR IPXA2026042797242Adapter · corrodedADDITION SDR AND CPCP FOR SATELLITE COMMUNICATIONS (SATCOM) SYSTEM [T3F18E0082B65]. REVIEWED PER GMM-MTX 09.05.01.09.Apr 27, 2026 · N575UP · Boeing 74744AF · Fuselage Miscellaneous StructureSDR IPXA2026042329452Bolt · wornRIGHT WING OUTBOARD MID FLAP, T/E UPPER SKIN, BOLT WORN 1 EA. REMOVE THE WORN MATERIALS AND CLEAN. I.A.W DWG 65B08533, SHEET 3, ZONE C12, VIEW 2B6, REV.C. AND PSDL 65B08533 SHEET DL, REV.A. INSTALL THE RH WING OUTBD MID FLAP SUPPORT STRUT.Apr 16, 2026 · N575UP · Boeing 74744AF · Trailing Edge FlapsSDR IPXA2026042187945Fairing · damagedENLARGED HOLE NR 4 AFT FAIRING HOLE .IAW AMM 51-24-11-477-083 REV.116, REPAINT PEEL OFF AREA. CHECK NORMAL.Apr 14, 2026 · N575UP · Boeing 74744AF · Trailing Edge FlapsSDR IPXA2026042571341Angle · crackedFOUND MAIN DECK SIDE CARGO DOOR ANGLE ASSY DAMAGE. IAW SRM 51-40-02-0G REV.106. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G REV.106, AND DWG 65B57353, SH 2, REV G, INSTALLED NEW CLIP.Apr 13, 2026 · N575UP · Boeing 74744AF · Cargo/Baggage DoorsSDR IPXA2026042162642Fitting · chafedFOUND L1 ENTRY DOOR CUTOUT AFT LOWER FITTING CHAFING. REQUEST PERFORM OK TO CLOSE CHECK FOR L1 DOOR AFT SIDE LOWER SIDEWALL PANEL.Apr 12, 2026 · N575UP · Boeing 74744AF · Fuselage Miscellaneous StructureSDR IPXA2026041750112Seal · brokenBROKEN SEAL, LT WING LANDING GEAR W/W CUTOUT FWD LWR SEAL. IAW SRM 51-40-02-0G, REV 106. REMOVED DAMAGE SEAL IAW SRM 51-40-02-0G REV. 106 AND DWG 65B10555, SH 3, REV G INSTALLED NEW SEAL.Apr 11, 2026 · N575UP · Boeing 74744AF · Fuselage Main, StructureSDR IPXA2026042047400Rub Strip · chafedCHAFED STRIP , NR 2 ENGINE LT CORE COWL INNER AFT UPPER AREA. IAW AMM 71-11-06-004-001-J00, REV 116. REMOVED THE CORE COWL. IAW SRM 51-40-02-0G, REV. 106, REMOVED DAMAGE STRIP IAW SRM 51-40-02-0G, REV 106, AND CMM IPL 71-13-23, REV 47. INSTALLED NEW STRIP IApr 11, 2026 · N575UP · Boeing 74744AF · Nacelle/Pylon, Main FrameSDR IPXA2026042547996Tube · wornWORN FLARED TUBE OF ENG-1 ADP. I.A.W.AMM 29-11-15-002-001 REV116 AND AMM29-11-15-402-009, REV 116. REPLACED THE SPEED CONTROL AIR PRESSURE LINEApr 11, 2026 · N575UP · Boeing 74744AF · Hydraulic System, MainSDR IPXA2026042447341Retainer · crackedCRACKED RETAINER, NR 2 ENG RT T/R TRANSLATING COWL UPPER TEE TRACK HINGE PIN CRACKED. IAW AMM 70-50-00-912-034, REV 116 REPLACED THE RETAINER.Apr 11, 2026 · N575UP · Boeing 74744AF · Engine Thrust ReverserSDR IPXA2026042046129Rub Strip · brokenNO. 2 ENG NOSE COWL AFT FLANGE WEAR STRIP , AT 6 O'CLOCK POSITION. I.A.W SRM 51-40-02-0G REV. 106 AND GOODRICH AEROSTRUCTURES CMM IPL 71-11-16 REV.54 INSTALLED NEW STRIP.Apr 11, 2026 · N575UP · Boeing 74744AF · Nacelle/Pylon, Main FrameSDR IPXA2026042147492Seal · frayedFRAYED SEAL, NR 1 PYLON OTBD AFT FAIRING DOOR LWR SEAL. IAW SRM 51-40-02-0G, REV 106, REMOVED DAMAGE SEAL. IAW GMM-MTX 9.08, REV 15, REQUIREMENT AND EGAT WORK SHEET 60275 AND DWG 323U2325, SH 11, REV A. DWG 323U2325-153, PL, REV A, AND ORIGINAL PART AS Apr 11, 2026 · N575UP · Boeing 74744AF · Nacelle/Pylon, Main FrameSDR IPXA2026042150427Angle · crackedCRACKED ANGLE, NR 4 ENG RT THRUST REVERSER DRIAN TUBE SUPPORT CLAMP. IAW SRM 51-40-02-0G, REV 106. REMOVED DAMAGE ANGLE. IAW SRM 51-40-02-0G, REV 106, & IPC 78-32-52, REV 96. INSTALLED NEW ANGLE.Apr 11, 2026 · N575UP · Boeing 74744AF · Engine Thrust ReverserSDR IPXA2026042047446Seal · brokenBROKEN SEAL, NR 4 PYLON LT AFT FAIRING DOOR LWR SEAL. IAW SRM 51-40-02-0G, REV 106 REMOVED DAMAGE SEAL. IAW GMM-MTX CH 9.08, REV 15 REQUIREMENT AND EGAT WORK SHEET 60267 AND DWG 323U2325, SH 11, REV A, DWG 323U2325-153, PL REV A, AND ORIGINAL PART AS A SAMApr 11, 2026 · N575UP · Boeing 74744AF · Nacelle/Pylon, Main FrameSDR IPXA2026041649774Scoop · damagedENLARGED HOLE, LT WING OUTBD LOWER FUEL VENT SCOOP PANEL FWD FASTENER HOLE. IAW DWG 112U0700, SHEET 01, REV D. REMOVED LT WING FUEL VENT SCOOP PANEL IAW DWG 112U0700, SHEET 01, REV. D. INSTALLED LT WING FUEL VENT SCOOP PANEL.Apr 11, 2026 · N575UP · Boeing 74744AF · Wing Main, Frame StructureSDR IPXA2026041547552Bracket · chafedCHAFED BRACKET, NR 1 ENG LT T/R LWR FWD CLOSURE DOOR T/E AREA. I.A.W SRM 51-40-02-0G REV. 106 REMOVED DAMAGE BRACKET. I.A.W SRM 51-40-02-0G REV. 106 AND ST ENGINEERING IPC 78-32-21 REV. 96 INSTALLED NEW BRACKET.Apr 11, 2026 · N575UP · Boeing 74744AF · Engine Thrust ReverserSDR IPXA2026041547525Bracket · chafedCHAFED BRACKET, NR 1 ENG RT THRUST REVERSER LWR FWD CLOSURE DOOR T/E AREA. I.A.W SRM 51-40-02-0G REV. 106 REMOVED DAMAGE BRACKET. I.A.W SRM 51-40-02-0G REV. 106 AND ST ENGINEERING IPC 78-32-22 REV. 96 INSTALLED NEW BRACKET.Apr 11, 2026 · N575UP · Boeing 74744AF · Engine Thrust ReverserSDR IPXA2026041547574Bracket · chafedCHAFED BRACKET, NR 2 ENG RT THRUST REVERSER FWD LWR CLOSURE DOOR T/E AREA. IAW SRM 51-40-02-0G, REV 106 REMOVED DAMAGE BRACKET. IAW SRM 51-40-02-0G, REV 106 & IPC 78-32-22 REV. 96 INSTALLED NEW BRACKET.Apr 11, 2026 · N575UP · Boeing 74744AF · Engine Thrust ReverserSDR IPXA2026042128355Seal · brokenBROKEN SEAL , NR 3 ENG, LT THRUST REVERSER AFT LWR AREA. IAW SRM 51-40-02-0G, REV 106, AND IPC 78-32-21 REV. 96, INSTALLED NEW SEAL.Apr 10, 2026 · N575UP · Boeing 74744AF · Engine Thrust ReverserSDR IPXA2026042028336Bracket · crackedCRACKED BRACKET, NR 3 ENG LT THRUST REVERSER HINGE PANEL SUPPORT BRACKET. IAW SRM 51-40-02-0G, REV 106. REMOVED DAMAGE BRACKET. IAW SRM 51-40-02-0G, REV 106, AND IPC 78-32-21, REV 96 INSTALLED NEW BRACKET.Apr 10, 2026 · N575UP · Boeing 74744AF · Engine Thrust ReverserSDR IPXA2026042711816Cover · crackedFAULT - R/H WING L/E VARIABLE CAMBER FLAP #17 INBD ROTARY ACTUATOR HAS CRACKED OTBD COVER. NO.5385. I.A.W AMM 27-81-07-004-001 REV 116 REMOVE NO.17 V.C FLAP INBD'S OUTBD ROTARY ACTUATOR. I.A.W AMM 27-81-07-404-008 REV.116 STEP 3.F.(2).(P) TO STEP 3.G.(2) ACCApr 9, 2026 · N575UP · Boeing 74744AF · Trailing Edge Flap ActuatorSDR IPXA2026042711853Cover · crackedFAULT - R/H WING L/E VARIABLE CAMBER FLAP #17 OTBD ROTARY ACTUATOR HAS CRACKED OTBD COVER. NO.5311. I.A.W AMM 27-81-07-004-001 REV 116 REMOVE NO.17 V.C FLAP ROTARY ACTUATOR. I.A.W AMM 27-81-07-404-008 REV.116 STEP 3.F.(2).(P) TO STEP 3.G.(2) ACCOMPLISHED THE IApr 9, 2026 · N575UP · Boeing 74744AF · Trailing Edge Flap ActuatorSDR IPXA2026042711764Cover · crackedLT WING L/E VARIABLE CAMBER FLAP NR 2 ROTARY ACTUATOR AT HAS CRACKED COVER. IAW AMM 27-81-07-004-001 REV 116 REMOVE NR 2 V.C FLAP ROTARY ACTUATOR. IAW AMM 27-81-07-404-008, REV.116, STEP 3.F.(2).(P) TO STEP 3.G.(2). ACCOMPLISHED THE INSTALLATION AND ADJUST Apr 9, 2026 · N575UP · Boeing 74744AF · Trailing Edge Flap ActuatorSDR IPXA2026042713748Cover · crackedRIGHT WING L/E VARIABLE CAMBER FLAP 24 ROTARY ACTUATOR AT HAS CRACKED COVER. IAW AMM 27-81-07-004-001, REV 116. REMOVE 24 V.C FLAP ROTARY ACTUATOR. IAW AMM 27-81-07-404-008, REV 116. STEP 3.F.(2).(P) TO STEP 3.G.(2). ACCOMPLISHED THE INSTALLATION AND AApr 9, 2026 · N575UP · Boeing 74744AF · Trailing Edge Flap ActuatorSDR IPXA2026042711916Cover · crackedLEFT WING LE VARIABLE CAMBER FLAP NR 5, ROTARY ACTUATOR AT HAS CRACKED COVER. 5386. IAW AMM 27-81-07-004-001, REV 116. REMOVED NR 5 VC FLAP ROTARY ACTUATOR. I.A.W AMM 27-81-07-404-008 REV.116 STEP 3.F.(2). P TO STEP 3.G. (2). ACCOMPLISHED THE INSTALLATION ANApr 9, 2026 · N575UP · Boeing 74744AF · Trailing Edge Flap ActuatorSDR IPXA2026042411547Cover · crackedCRACK- COVER, NO.4 ENG R/H T/R ACTUATOR ACCESS PNL 446B, 446C, 445C. I.A.W.AMM 78-31-10-004-001-J00 REV116 REMOVED THE PANEL 446B 446C 445C. I.A.W.AMM 78-31-10-404-008-J00 REV116 INSTALLED THE PANEL 446B 446C 445C WITH NEW.Apr 9, 2026 · N575UP · Boeing 74744AF · Engine Thrust ReverserSDR IPXA2026042411487Cover · crackedCRACK- COVER, NO.3 ENG R/H T/R ACTUATOR ACCESS PNL 436B, 436C. I.A.W.AMM 78-31-10-004-001-J00 REV116 REMOVED THE PANEL 436B 436C. I.A.W.AMM 78-31-10-404-008-J00 REV116 INSTALLED THE PANEL 436B 436C WITH NEW.Apr 9, 2026 · N575UP · Boeing 74744AF · Engine Thrust ReverserSDR IPXA2026042014756Rub Strip · chafedCHAFED RUB STRIP, NR 3 ENG RT CORE COWL AFT UPR RUB STRIP. I.A.W SRM 51-40-02-0G REV. 106 AND CMM IPL 71-13-24 REV.50 INSTALLED NEW STRIP.Apr 9, 2026 · N575UP · Boeing 74744AF · Nacelle/Pylon, Main FrameSDR IPXA2026042114858Seal · brokenBROKEN - SEAL, NR 4 ENG RT T/R CLOSURE DOOR FWD AREA. I.A.W SRM 51-40-02-0G REV. 106 REMOVED DAMAGE SEAL. I.A.W SRM 51-40-02-0G REV. 106 AND ST ENGINEERING IPC 78-32-22 REV. 96 INSTALLED NEW SEAL.Apr 9, 2026 · N575UP · Boeing 74744AF · Engine Thrust ReverserSDR IPXA2026042014715Rub Strip · chafedCHAFING AND MISSING - STRIP AND RIVET, NO.3 ENG L/H CORE COWL AFT UPR WEAR STRIP. IAW SRM 51-40-02-0G REV. 106 AND GOODRICH AEROSTRUCTURES CMM IPL 71-13-23 REV.47 INSTALLED NEW STRIP.Apr 9, 2026 · N575UP · Boeing 74744AF · Nacelle/Pylon, Main FrameSDR IPXA2026042315124Nose Cowl · dentedDENTED SKIN, NR 2 ENG NOSE COWL INNER BARREL NEAR 2:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.4", 5.5" FROM AFT EDGE, 59.5" FROM LWR EDGE, AT 2 O'CLOCK ON THE INNER BARREL OF NO.2 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESIVE CUREDApr 9, 2026 · N575UP · Boeing 74744AF · Nacelle/Pylon, Main FrameSDR IPXA2026042214799Seal Depressor · crackedCRACKED DEPRESSURE SEAL, AFT CARGO DOOR CUTOUT AFT SIDE. I.A.W SRM 51-40-02-0G REV.106 REMOVE DAMAGE DRPRESSOR SEAL AND DEPRESSOR. I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG NO.65B01865 SH10 REV E AND BOEING DWG NO.65B06880 SH2 REV B INSTALL NEW DRPRESSOR Apr 9, 2026 · N575UP · Boeing 74744AF · Cargo/Baggage DoorsSDR IPXA2026041815210Fairing · dentedDENTED SKIN, LT WING T/E FLAP NR 4 AFT FAIRING EXTERNAL SURFACE LOWER SIDE ADJACENT AFT CONE. IAW SRM 57-53-70-2R-1 REFER TO SRM 51-70-17-0G-0 REV. 106 PERFORM REPAIR AS BELOW STEP: 1.1 REMOVE THE DAMAGE MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CApr 9, 2026 · N575UP · Boeing 74744AF · Trailing Edge FlapsSDR IPXA2026041811914Skin · crackedRIGHT WING INBOARD T/E UPPER FIXED PANEL SKIN CRACK, WBL 235.2. I.A.W. 747-400F SRM 57-51-01-2R-1 REFER TO SRM 51-70-07-0G-0 REV. 106 PERFORM REPAIR AS BELOW STEP: 1.1 REMOVE THE CRACK MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 26Apr 9, 2026 · N575UP · Boeing 74744AF · Wing, Plate/SkinSDR IPXA2026041214960Floorboard · damagedMAJOR REPAIR. DAMAGED FLOORBOARD ON RT MAIN CARGO DECK BS 1220. REMOVE THE DAMAGED PANEL IN ACCORDANCE WITH AMM 53-21-02. INSTALL THE REPLACEMENT FLOOR PANEL PER AMM 53-21-02.Apr 9, 2026 · N575UP · Boeing 74744AF · Fuselage Floor PanelSDR IPXA2026042573876Panel · brokenFWD CARGO COMPARTMENT CEILING PANEL ASSY ZIPPER BROKEN AT STA 840 - 860. .I.A.W AMM25-52-01-004-049 REV116 AND I.A.W AMM25-52-01-404-062 REV116 REPLACE PANEL ASSY WITH NEW PARTS.Apr 7, 2026 · N575UP · Boeing 74744AF · Cargo CompartmentsSDR IPXA2026042355538Support · wornFOUND LT WING OTBD FLAP NR 7 SUPPORT STRUT (OTBD TO INBD) UPPER AND LOWER PANEL WORN. I.A.W DWG 65B08533, SHEET 3, ZONE C12, VIEW 2B6, REV.C. REMOVED THE LH WING OUTBD FLAP NO.7 SUPPORT STRUT (OUTBD TO INBD). FAULT- FOUND LH WING OUTBD FLAP NO.7 SUPPORT STRUTApr 6, 2026 · N575UP · Boeing 74744AF · Wing Miscellaneous StructureSDR IPXA2026042634350Clamp · crackedCRACKED CLAMP - APU ACOC COOLING DUCT. I.A.W.AMM 49-51-04-004-001 REV116 AND AMM 49-51-04-404-011 REV116 REPLACED THE CLAMP WITH NEW.Apr 4, 2026 · N575UP · Boeing 74744AF · APU Bleed Air SystemSDR IPXA2026042119204Skin · damagedLIGHTNING STRIKE- SKIN, RT NOSE AREA (ABOVE UPS LOGO) SUSPECTED LIGHTENING STRIKE ON FASTENER. BLEND OUT THE DAMAGE AREA I.A.W SRM 51-10-02-0G REV.106. ACCOMPLISHMENT LIGHTNING STRIKE REPAIR I.A.W UPS EO-97134-REQ1 REV.1.Apr 3, 2026 · N575UP · Boeing 74744AF · Fuselage Main, Plate/SkinSDR IPXA2026042072963Ring · crackedCRACKED ACSR-ON ENG-2 , R/H THRUST REVERSER HALF. IAW AMM 78-31-01-004-001-J00 REV 116 REMOVED THE T/R HALF. RII NO.2 ENG R/H THRUST REVERSER HALF OK TO INSTALLED CHECKED OK AND INSTALLED CHECKED OK.Apr 1, 2026 · N575UP · Boeing 74744AF · Engine Thrust ReverserSDR IPXA2026042075055Fitting · crackedFND 3L T/R AGB FITTING CRACK AT 7 O'CLOCK POSITION. I.A.W. AMM 78-31-01-004-001-J00 REV116 REMOVED THE T/R HALF. I.A.W SRM 51-40-02-0G REV.106 REMOVE DAMAGE AGB FITTING. RII NO.3 ENG L/H THRUST REVERSER HALF OK TO INSTALLED CHECKED OK AND INSTALLED CHECKED OK.Apr 1, 2026 · N575UP · Boeing 74744AF · Engine Thrust ReverserSDR IPXA2026041557453Angle · crackedDURING PERFORMANCE OF EO-95214-JIC2, FOUND RT WING LG SHOCK STRUT DOOR FAIRING SEAL DEPRESSOR. I.A.W SRM 51-40-02-0G REV.106 REMOVED DAMAGE DEPRESSOR. I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG NO.65B11675 SH. 2 REV. G INSTALLED NEW DEPRESSOR.Mar 31, 2026 · N575UP · Boeing 74744AF · Wing Miscellaneous StructureSDR IPXA2026041557510Angle · crackedDURING PERFORM EO-95214-JIC2, FOUND RT WING SHOCK STRUT DOOR FAIRING CLIP CRACKED. I.A.W SRM 51-40-02-0G REV. 106 REMOVED DAMAGE CLIP. I.A.W SRM 51-40-02-0G REV. 106 AND BOEING DWG NO: 65B11675 SHEET 1 REV. K INSTALLED FABRICATED CLIP.Mar 31, 2026 · N575UP · Boeing 74744AF · Wing Miscellaneous StructureSDR IPXA2026040554363Fairing · puncturedPUNCTURE IN FWD OTBD AREA OF #1 MOVEABLE FLAP TRACK FAIRING. I.A.W. 747-400F SRM 57-53-70-2R-1 REFER TO SRM 51-70-07-0G-0 REV.106 PERFORM REPAIR AS BELOW STEP: 1.1 REMOVE THE PUNCTURE MATERIALS AND CLEAN. 1.2 MEASURE THE DAMAGE AREA (DIA:1", 2.5" FROM THE PAMar 6, 2026 · N575UP · Boeing 74744AF · Trailing Edge FlapsSDR IPXA2026030919342Floorboard · wornMAJOR REPAIR, FLOORBOARD INSIDE L1 DOOR THRESHOLD IS WORN AND IS SHOWING CORE MATERIAL. INSTALLED NEW FLOORBOARD INSIDE L1 DOOR THRESHOLD IAW AMM 53-21-02.Mar 4, 2026 · N575UP · Boeing 74744AF · Fuselage Floor PanelSDR IPXA2026030908993Door Frame · damagedFOUND DAMAGE ON UNDERLYING STRUCTURE BEHIND SEAL DEPRESSOR SPLICE AT FS 615 APPROX WL 170. ALL STEPS ARE COMPLETE EO-96726-REQ1.Mar 4, 2026 · N575UP · Boeing 74744AF · Fuselage Main, StructureSDR IPXA2026041369914Skin · dentedNR 25 VCF HAS DENT ON LEADING INB END RII COMPLETED STEP 13 I.A.W AMM 27-81-02-404-010 REV.116 ASSEMBLY THE NR 26 FOLDING NOSE AND INSTALLED THE NR 26 V.C FLAP CHECK OK. ACCOMPLISHED REPAIR I.A.W EGAT WORK SHEET NO.60222 AND SRM 57-43-02-2R-2 REPAIR2 REV.106Mar 1, 2026 · N575UP · Boeing 74744AF · Leading Edge DevicesSDR IPXA2024052554554Battery · inoperativeFOUND THE L1 DOOR EMERGENCY LIGHT INOP. REPLACED THE EMERGENCY LIGHT BATTERY (M5170) AT UPPER DECK (STA550 WL323 LBL83)I.A.W AMM 33-51-04-902-001-001 REV.110 AND SSM 33-51-01 REV.44May 19, 2024 · N575UP · Boeing 74744AF · Emergency LightingSDR IPXA2024052554537Battery · inoperativeFAULT - FOUND THE EMERGENCY EXIT SIGN LIGHT INOP AT UPPER DECK STA 410. (REPLACE) .I.A.W AMM 33-51-04-902-001-001 REV.110 AND SSM 33-51-01 REV.44 REPLACED THE EMERGENCY LIGHT BATTERY (M5169) AT UPPER DECK (STA590 WL323 RBL83). REVIEW COMPLETEDMay 19, 2024 · N575UP · Boeing 74744AF · Emergency LightingSDR IPXA2024052054554Light · inoperativeFOUND THE L1 DOOR EMERGENCY LIGHT INOP. (REPLACE) OK TO WORKMay 19, 2024 · N575UP · Boeing 74744AF · Emergency Lighting
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