N257UP

Service difficulty reports · 450

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 = 'N257UP' 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 IPXA2020061756679Fitting · wornINSPECTION TYPE:2C LT IB ELEVATOR OB CAM FITTING IS WORN. REPAIRED LT IB ELEVATOR WORN OB CAM FITTING IAW EA 011-5520-01-A8342 REV IR AND EO MD11-5520-76847-A. (MINOR)Jun 7, 2020 · N257UP · Doug MD11F · Elevator Miscellaneous StructureSDR IPXA2020061756678Fitting · wornINSPECTION TYPE:2C RT OB ELEVATOR CAM FITTING IS WORN IB OF NR 9 BEARING. REPAIRED RT OB ELEVATOR WORN CAM FITTING IB OF NR 9 BEARING IAW EA 011-5520-01-A8342 REV IR AND EO MD11-5520-76847-A. (MINOR)Jun 7, 2020 · N257UP · Doug MD11F · Elevator Miscellaneous StructureSDR IPXA2020061756677Fitting · wornINSPECTION TYPE:2C LT OB ELEVATOR CAM FITTING IS WORN OB OF NR 7 BEARING. REPAIRED LT OB ELEVATOR WORN CAM FITTING OB OF NR 7 BEARING IAW EA 011-5520-01-A8342 REV IR AND EO MD11-5520-76847-A. (MINOR)Jun 7, 2020 · N257UP · Doug MD11F · Elevator Miscellaneous StructureSDR IPXA2020062967023Rib · crackedINSPECTION TYPE:2CEXTENDED TAILCONE L/H FAIRING SUPPORT RIB IS CRACKED.REMOVED AND REPLACED CRACKED EXTENDED TAILCONE L/H FAIRING SUPPORT RIB IAW MD-11 SRM 51-31-01 & 51-35-01. (MINOR)Jun 6, 2020 · N257UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2020070157158Frame · damagedINSPECTION TYPE:2C TAIL CONE LT PATIO DOOR AFT FRAME IS BENT AND DAMAGED. REMOVED, FABRICATED AND REPLACED FRAME IAW DWG AKC7820 AND SRM 51-35-01. (MINOR)Jun 5, 2020 · N257UP · Doug MD11F · Aerodynamic FairingsSDR IPXA2020062977046Frame · crackedINSPECTION TYPE:2CFWD TAILCONE AFT R/H FRAME HAS 2 CRACKS IN RADIUS AT UPPER AND LOWER LATCH FITTINGS.REMOVED AND REPLACED CRACKED FWD TAILCONE AFT R/H FRAME IAW MD-11 SRM 51-33-01 AND 51-35-01. (MINOR)Jun 5, 2020 · N257UP · Doug MD11F · Fuselage Main, FrameSDR IPXA2020062656961Intercostal · crackedINSPECTION TYPE:2C LOWER VERTICAL STABILIZER REAR CENTER SPAR TO LOWER PANEL INTERCOSTAL RT SIDE IS CRACKED AT STA YID= 375 AND XID= -7.1. REPAIRED CRACKED LOWER VERTICAL STABILIZER REAR CENTER SPAR TO LOWER PANEL INTERCOSTAL RT SIDE AT STA YID= 375 AND XID= Jun 5, 2020 · N257UP · Doug MD11F · Vertical Stabilizer Miscellaneous StructureSDR IPXA2020062656972Cap · crackedINSPECTION TYPE:2C RT UNDER WING CANTED PANEL CAP IS CRACKED AT STA 1236.8 AND Z= -100. REPAIRED CRACKED RT UNDER WING CANTED PANEL CAP AT STA 1236.8 AND Z= -100 IAW EO MD11-5310-76799-A. (MAJOR)Jun 5, 2020 · N257UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020062456949Frame · chafedINSPECTION TYPE:2CTAILCONE FWD UPPER FRAME (BEAM) IS CHAFED IN 4 AREAS.REPAIRED TAILCONE FWD UPPER FRAME (BEAM) CHAFE DAMAGE IAW MD-11 SRM 53-00-00 FIG. 210. (MINOR)Jun 5, 2020 · N257UP · Doug MD11F · Aerodynamic FairingsSDR IPXA2020062957109Cap · corrodedINSPECTION TYPE:2CL/H WING T/E LOWER CAP HAS CORROSION BETWEEN STA. XW= 276.029 TO XW= 328.00.REPAIRED CORRODED L/H WING T/E LOWER CAP BETWEEN STA XW= 276.029 TO XW= 328.00 IAW SRM 57-50-02 REPAIR 9 FIG. 201. (MAJOR)Jun 4, 2020 · N257UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2020062967022Support · crackedINSPECTION TYPE:2CLT WING I/B FLAP I/B HINGE FWD O/B UPPER SUPPORT IS CRACKED.REMOVED AND REPLACED CRACKED LT WING I/B FLAP I/B HINGE FWD O/B UPPER SUPPORT IAW MD-11 SRM 51-33-01 & 51-35-01. (MINOR)Jun 4, 2020 · N257UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2020062657011Longeron · corrodedINSPECTION TYPE:2C CENTER CARGO LONGERON 48L IS CORRODED BETWEEN STA 1531 TO 1551. REPAIRED CORRODED LONGERON 48L BETWEEN STA 1531 TO 1551 IAW EA 011-5310-01-A8338 REV I/R AND EO MD11-5310-76915-A. (MAJOR)Jun 4, 2020 · N257UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2020062656973Longeron · corrodedINSPECTION TYPE:2C CENTER CARGO LONGERON 44R HAS CORROSION AT STA 1611. REPAIRED CORRODED LONGERON 44R BETWEEN STA 1610 TO 1632 IAW SRM 53-00-05 REPAIR 1 FIG 201. (MAJOR)Jun 4, 2020 · N257UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2020062256792Skin · gougedINSPECTION TYPE:2C LT I/B AILERON LOWER L/E SKIN IS GOUGED AT O/B END. REMOVED AND REPLACED GOUGED LT I/B AILERON LOWER L/E SKIN IAW SRM 51-31-01. (MINOR)Jun 4, 2020 · N257UP · Doug MD11F · AileronsSDR IPXA2020061756676Longeron · corrodedINSPECTION TYPE:2C CENTER CARGO LONGERON 48R HAS EXFOLIATION CORROSION AT APPROX STA 1609. REPAIRED CENTER CARGO LONGERON 48R CORROSION BETWEEN STA 1601 - 1621 IAW EA 011-5310-01-A8330 REV IR AND EO MD11-5310-76874-A. (MINOR)Jun 4, 2020 · N257UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2020062967021Beam · crackedINSPECTION TYPE:2C, RT WING O/B FLAP I/B FWD HINGE FAIRING BEAM IS CRACKED.REMOVED AND REPLACED CRACKED RT WING O/B FLAP I/B FWD HINGE FAIRING BEAM IAW MD-11 SRM 51-33-01. (MINOR)Jun 3, 2020 · N257UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2020062256791Intercostal · crackedINSPECTION TYPE:2C TAILCONE INTERCOSTAL IS CRACKED AT FWD UPPER GUIDE PIN. REMOVED AND REPLACED CRACKED INTERCOSTAL AT UPPER FWD TAILCONE GUIDE PIN IAW SRM 51-33-01 AND 51-35-01. (MINOR)Jun 3, 2020 · N257UP · Doug MD11F · Aerodynamic FairingsSDR IPXA2020062256864Skin · crackedINSPECTION TYPE:2C LT OUTER WING LOWER FUEL ACCESS PANEL (536AB) LANDING HAS 8 EA FASTENER HOLES CRACKED BETWEEN STA XORS 683.40 TO 713.65. REPAIRED CRACKED LT OUTER WING LOWER FUEL ACCESS PANEL (536AB) LANDING BETWEEN STA XORS 683.40 TO 713.65 IAW SRM 57-20-Jun 3, 2020 · N257UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020062256863Skin · crackedINSPECTION TYPE:2C RT OUTER WING LOWER FUEL ACCESS PANEL( 636AB) LANDING HAS 7EA FASTENER HOLES CRACKED BETWEEN STA XORS 683.40 TO 713.65. REPAIRED CRACKED RT OUTER WING LOWER FUEL ACCESS PANEL LANDING BETWEEN STA XORS 683.40 TO 713.65 IAW SRM 57-20-05 REPAIRJun 3, 2020 · N257UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020061956754Door Frame · crackedINSPECTION TYPE:2CL-3 DOOR JAMB LOWER WEB IS CRACKED AT STA. 1307.25 & Z= -18.REPAIRED CRACKED L-3 DOOR JAMB LOWER WEB AT STA. 1307 & Z= -18 IAW SRM 53-40-15 REPAIR 3 FIG. 201. (MAJOR)Jun 3, 2020 · N257UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2020061766652Angle · crackedINSPECTION TYPE:2CMAIN CABIN LONGERON 15R "T" ANGLE IS CRACKED AT APPROX STA 1305.REMOVED AND REPLACED CRACKED LONGERON 15R "T" ANGLE BETWEEN STA 1305 - 1321 IAW MD-11 SRM 51-33-01 & 51-35-01. (MINOR)Jun 3, 2020 · N257UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2020061756651Angle · crackedINSPECTION TYPE:2C MAIN CABIN LONGERON 15L "T" ANGLE IS CRACKED AT APPROX STA 1305. REMOVED AND REPLACED CRACKED LONGERON 15L "T" ANGLE BETWEEN STA 1305 - 1321 IAW SRM 51-31-01. (MINOR)Jun 3, 2020 · N257UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020061756684Cap · corrodedINSPECTION TYPE:2C AFT CARGO FRAME SUPPORT (CAP) AT STA 1841 LONGERON 43R HAS CORROSION. REPAIRED AFT CARGO FRAME CAP CORROSION AT STA 1841 & X=-55 IAW EA 0115310-01-A8343 REV IR AND EO MD11-5310-76881-A. (MINOR)Jun 3, 2020 · N257UP · Doug MD11F · Fuselage Main, FrameSDR IPXA2020061256464Filler · chafedINSPECTION TYPE:2C TAILCONE LT FWD UPPER PRODUCTION DOUBLER REPAIR FILLER IS CHAFED. REPAIRED CHAFED TAILCONE LT FWD UPPER PRODUCTION DOUBLER FILLER IAW EO MD11-5350-66790-A APPENDIX B. (MINOR).Jun 3, 2020 · N257UP · Doug MD11F · Aerodynamic FairingsSDR IPXA2020062967019Intercostal · crackedINSPECTION TYPE:2C, AFT FUSELAGE COMPARTMENT 316 UPPER SURGE DUCT MOUNT INTERCOSTAL IS CRACKED.REMOVED AND REPLACED AFT FUSELAGE COMPARTMENT 316 UPPER SURGE DUCT MOUNT CRACKED INTERCOSTAL IAW MD-11 SRM 51-33-01 & 51-35-01. (MINOR)Jun 2, 2020 · N257UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020062967018Rib · crackedINSPECTION TYPE:2C, LT WING FIXED L/E UPPER ACCESS PANEL 516ET HAS A CRACKED ZEE RIB.REMOVED AND REPLACED CRACKED LT WING FIXED L/E UPPER ACCESS PANEL 516ET ZEE RIB IAW MD-11 SRM 51-35-01. (MINOR)Jun 2, 2020 · N257UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020061756698Frame · crackedINSPECTION TYPE: 2C, FWD AVIONICS COMPARTMENT LT TRANSVERS FRAME AT BS 469 WAS CRACKED. REPAIRED CRACKED FWD AVIONICS COMPARTMENT LT TRANSVERS FRAME AT BS 469.173 CANT & X=60 IAW SRM 53-10-07, REPAIR 1, FIGURE 201. MAJOR.Jun 2, 2020 · N257UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2020061556546Doubler · crackedINSPECTION TYPE:2C RT WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA XOS= 789.6 TO 795.7. REPAIRED CRACKED RT WING FIXED L/E BEADED DOUBLER BETWEEN STA XOS= 789.6 TO 795.7 IAW SRM 57-40-02 REPAIR 15 FIG 205. (MAJOR)Jun 2, 2020 · N257UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020062657009Frame · crackedINSPECTION TYPE:2C FUSELAGE MAIN FRAME IS CRACKED AT STA 469.173 AND X=-60. REPAIRED CRACKED FUSELAGE MAIN FRAME AT STA 469.173 AND X= -60 IAW EA 011-5310-01-A8355 REV I/R AND EO MD11-5310-76977-A. (MAJOR)Jun 1, 2020 · N257UP · Doug MD11F · Fuselage Main, FrameSDR IPXA2020062656962Closeout Panel · crackedINSPECTION TYPE:2C FUSELAGE INTERMEDIATE PRESSURE CLOSING PANEL IS CRACKED AT STA 1376, X= -31.5 AND BETWEEN Z= -25.613 & Z= -56.5. REPAIRED CRACKED FUSELAGE INTERMEDIATE PRESSURE CLOSING PANEL AT STA 1376, X= -31.5 AND BEWTEEN Z= -25.613 & Z= -56.5 IAW EA 01May 31, 2020 · N257UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020061056356Fitting · wornINSPECTION TYPE:4C LT O/B ELEVATOR CAM FITTING I/B OF NR 7 BEARING IS WORN. REPAIRED WORN LT O/B ELEVATOR CAM FITTING I/B OF NR 7 BEARING IAW EA 011-5520-01-A8302 REV IR AND EO MD11-5520-76695-A. (MINOR)May 27, 2020 · N257UP · Doug MD11F · Elevator Miscellaneous StructureSDR IPXA2020033053685Panel · delaminatedINSPECTION TYPE:N/ADELAM AND CUT OUT OF 4.5" X 2" AND 2" DIAMETER.REPAIRED PER EO MD11-5530-72242Mar 29, 2020 · N257UP · Doug MD11F · Vertical Stabilizer, Plate/SkinSDR IPXA2019110348586Seat Track · crackedINSPECTION TYPE:N/ASEAT TRACK CRACKED AND CORRODED ATSTA 1520 8.50 RREPAIRED PER EO MD11-5310-74517 SEAT TRACK SPLICE REPAIRNov 3, 2019 · N257UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2019110348585Seat Track · corrodedINSPECTION TYPE:N/ASEAT TRACK CRACKED AND CORRODED AT STA.1520-8.50LEFTREPAIRED PER EO MD11-5310-74517A SEAT TRACK SPLICE REPAIRNov 3, 2019 · N257UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2019110148547Solenoid · inoperativeINSPECTION TYPE:N/A2L DOOR INOP.R&R ED L1 SOLENOID PER AMM 52 10 06 401 DOOR OPERATES NORMAL. OK FOR SERVICE. IPC 52 11 70 01 ITEM 070JNov 1, 2019 · N257UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2019103098436Door · unknownINSPECTION TYPE:N/ADFW GROUND CREW REPORTED L1 DOOR WILL NOT CLOSE OR OPENPERFORMED OPERATIONAL TEST OF L1 DOOR IN REF TO MD11 M/M 52-11-02-700-802. OPS CHECKS NORMAL.Oct 28, 2019 · N257UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2019083046152Control Unit · faultedINTERMITTANT FIRE DETECTOR 2 FAULT LEVEL ONE ALERT IN FLIGHT. REPLACED THE NR 2 FIRE DETECTION CONTROL UNIT. OPS CHECKED GOOD IAW AMM 26-11-02.Aug 30, 2019 · N257UP · Doug MD11F · Detection SystemSDR IPXA2019070844198Cooling Fan · defectiveINSPECTION TYPE:N/A ELEC SMELL FROM FWD AVIONICS COMPARTMENT. REPLACED # 1 AVIONICS COOLING FAN REF MM 21-26-02 . P/N 29680 S/N OFF 538 , S/N ON 562 IPC 21-26-15-01-545. AIRCRAFT OK FOR SERVICE.Jul 7, 2019 · N257UP · Doug MD11F · Air Distribution FanSDR IPXA2019062854734Line · brokenAIR TURNBACK AFTER TAKE OFF. RECEIVED LEVEL 2 ALERT HYD 3 FAIL. DURING INSPECTION, FOUND THE LT LANDING GEAR HYD TRIM CYLINDER PRESSURE PIPE BROKEN. TEMP REPAIR OF HYD RIGID PIPES WITH FLEXIBLE WAS APPROVED BY ENGINEERING IAW AMM 20-10-01-300-805, THREE FLEJun 25, 2019 · N257UP · Doug MD11F · Hydraulic System, MainSDR IPXA2019041754178Battery · inoperativeMESSAGE EMERGENCY LIGHT LOW BATTERY DISPLAYED. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY IN REF TO MD11 MM 33 51 01 400 802. EMERGENCY LIGHTING BATTERY POWER SUPPLY OPS TEST GOOD IN REF TO MD11 MM 33 51 01 700 802 MD11 IPC 33 51 10 01 005JApr 15, 2019 · N257UP · Doug MD11F · Emergency LightingSDR IPXA2018091033806Skin Panel · damagedLEFT SIDE FUSELAGE SKIN DAMAGE AT STA 655 BETWEEN L41 AND L42. REPAIRED IAW SRM 53-00-01-2R-1, FIG 201, REPAIR 1.Sep 9, 2018 · N257UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2018082983309Indicator · brokenL1 DOOR DISARMED LIGHT WAS BROKEN. REPLACED L1 DOOR DISARMED LIGHT IAW WDM 52-11-01. TESTED GOOD.Aug 27, 2018 · N257UP · Doug MD11F · Emergency EquipmentSDR IPXA2018082983308Indicator · brokenR1 DOOR DISARMED LIGHT WAS BROKEN. REPLACED THE DOOR DISARMED LIGHT IAW WDM 52-11-01. TESTED GOOD.Aug 27, 2018 · N257UP · Doug MD11F · Emergency EquipmentSDR IPXA2018060130225Intercostal · crackedDURING REMOVAL OF THE PNEUMATIC DUCT IAW NRC 379144, FOUND AN INTERCOSTAL GOUGED & CRACKED, BS 1781 - 1801. FABRICATED A REPLACEMENT INTERCOSTAL IAW DWG AGA7177. AND INSTALLED.May 22, 2018 · N257UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2018053030179Web · crackedWHILE ACCOMPLISHING EO MD11-5710-65285-C APPX. B, STEP 5. ONE CRACK DETECTED ON THE RT WEB OTBD LOWER STIFFENER .250 IN LENGTH, DEPTH GREATER THAN .050. REPAIRED THE FUEL TANK WEB IAW EO MD11-5710-68621-A. MAJOR.May 22, 2018 · N257UP · Doug MD11F · Fuel StorageSDR IPXA2018060130223Floor Panel · corrodedRCB AREA FLOOR PANEL WSP0788-502 HAD CORROSION BETWEEN BS 476 - 480, RBL 37. REPAIRED THE FLOOR PANEL IAW EA 011-5330-01-A7289, REV IR, AND EO MD11-5330-68700-A.May 20, 2018 · N257UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2018060643312Skin · crackedNR 2 ENGINE, RT CORE COWL HAD A CRACK ON THE OUTER SKIN AT THE FWD LATCH. REPAIRED THE DAMAGE IAW EA 011-5430-01-A7295, REV I/R, AND EO MD11-5430-68739-A.May 18, 2018 · N257UP · Doug MD11F · Nacelle/Pylon, Plate/SkinSDR IPXA2018060430281Cap · crackedLEFT UNDERWING BARREL CANTED PANEL CAP IS CRACKED AT BS 1278 AND Z -100. REPAIRED THE PANEL CAP IAW EA 011-5310-01-A7281, REV I/R, AND EO MD11-5340-68712-A. MAJOR.May 18, 2018 · N257UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2018060430280Spar Cap · corrodedRIGHT WING REAR SPAR UPPER CAP HAD CORROSION BETWEEN XORS. 666.2 TO 680.7. REPAIRED THE SPAR CAP IAW EA 011-5710-01-A7288, REV I/R, AND EO MD11-5710-68701-A.May 18, 2018 · N257UP · Doug MD11F · Wing SparSDR IPXA201806040270Support Angle · damagedLEFT WING LOWER T/E PANEL SUPPORT ANGLE WAS CHAFED, ADJACENT TO PANEL 551BB. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT SUPPORT ANGLE IAW DWG ARC0744, AND SRM 51-33-01.May 18, 2018 · N257UP · Doug MD11F · Wing Miscellaneous Structure
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