N250UP

Service difficulty reports · 294

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 = 'N250UP' 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 IPXA2016090507861Nut Plate · brokenINSPECTION TYPE:3C, BROKEN NUTPLATE IN RCB ALONG LOWER FORWARD FACE AT X=65. RCB REPAIRED IAW EA 011-5320-01-A6424, REV IR AND EO MD11-5310-61760-A, MAJOR.Aug 26, 2016 · N250UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016090507860Nut Plate · brokenINSPECTION TYPE:3C, BROKEN NUTPLATE IN RCB ALONG LOWER FWD FACE AT X=72. RCB REPAIRED IAW EA 011-5320-01-A6424, REV IR AND EO MD11-5310-61760-A, MAJOR.Aug 26, 2016 · N250UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016090507858Nut Plate · brokenINSPECTION TYPE:3C, BROKEN NUTPLATE IN RCB ALONG LOWER FWD FACE AT X=60. NUTPLATE REPAIRED EA 011-5320-01-A6424, REV IR AND EO MD11-5310-61760-A.Aug 26, 2016 · N250UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016082907556Skin · corrodedINSPECTION TYPE: 3C, AFT EXTENDED FUSELAGE SKIN PANEL BELOW LT HORIZONTAL STAB., HSS 2122.881 IS CORRODED AT LONGERON 12L. REPAIRED THE SKIN PANEL IAW EA 011-5330-01-A6415 REV. I/R AND EO MD11-5330-61706-A.Aug 18, 2016 · N250UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2016090207764Former · crackedINSPECTION TYPE:3C, NR 2 PYLON AFT UPPER FAIRING INTERNAL FORMER CRACKED AT STA 2351, Z=232. REPAIRED FORMER IAW EA 011-5410-01-A6408, REV IR AND EO MD11-5450-61750-A, MINOR.Aug 16, 2016 · N250UP · Doug MD11F · Nacelle/Pylon, Frame/Spar/RibSDR IPXA2016082407422Floor Panel · corrodedINSPECTION TYPE: 3C, RCB AREA FLOOR PANEL WSP0785-501 CORRODED BEYOND ALLOWABLE LIMITS. REPAIRED THE FLOOR PANEL IAW EA 011-5310-01-A6403 REV. IR AND EO MD11-5320-61666-A.Aug 10, 2016 · N250UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2016090207768Duct · chafedINSPECTION TYPE:3C, CHAFE DAMAGE ON NR 2 ENGINE HEAT EXCHANGER PNEUMATIC DUCT ASSEMBLY. CHAFE DAMAGE REPAIRED IAW EA 011-3610-01-A6421, REV IR AND EO MD11-3610-61740-A.Aug 9, 2016 · N250UP · Doug MD11F · Pneumatic Distribution SystemSDR IPXA2016090107711Slat · corrodedINSPECTION TYPE:3C, LT NR 3 SLAT TRACK RIB XOS 484.5 FORWARD MOUNT HOLE CORRODED. REPAIRED NOTED CORROSION IAW EA 011-5754-00-A6414, REV IR AND EO MD11-5740-61728-A, MINOR.Aug 9, 2016 · N250UP · Doug MD11F · Leading Edge DevicesSDR IPXA2016082407435Floor Panel · corrodedINSPECTION TYPE: 3C, RCB AREA FLOOR PANEL WSP0785-501 CORRODED AT RBL 29. REPAIRED IAW EA 011-5310-01-A6402 REV. IR AND EO MD11-5320-61654-A.Aug 9, 2016 · N250UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2016082407423Floor Panel · corrodedINSPECTION TYPE: 3C, RCB AREA FLOOR PANEL WSP0789-501 CORRODED BEYOND ALLOWABLE LIMITS. REMOVED AND REPLACED THE FLOOR PANEL IAW SRM 53-21-01-400-801.Aug 9, 2016 · N250UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2016090207765Doubler · chafedINSPECTION TYPE:3C, EXTENDED TAILCONE LT SIDE INTERNAL DOUBLER CHAFE DAMAGE REPAIR AT STA 2165.6 Z=60.0. REPAIRED CHAFE DAMAGE IAW EA 011-5320-01-A6385, REV IR AND EO MD11-5350-61475-A, MINOR.Aug 8, 2016 · N250UP · Doug MD11F · Aerodynamic FairingsSDR IPXA2016082807528Tail Cone · damagedINSPECTION TYPE: 3C, FWD TAILCONE RT SIDE SKIN CREASED BS 2224 - 2229 BELOW DOOR HINGE SKIN CREASE. REPAIRED IAW EA 011-5320-01-A6397 REV. IR AND EO MD11-5350-61631-A.Aug 8, 2016 · N250UP · Doug MD11F · Aerodynamic FairingsSDR IPXA2016090707987Fitting · corrodedINSPECTION TYPE: 3C, RCB FLOOR FITTING NR 7 CORRODED. FITTING REPAIRED IAW EA 011-5310-01-A6393 REV. IR AND EO MD11-5310-61671-A.Aug 7, 2016 · N250UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2016090707965Fitting · corrodedINSPECTION TYPE:3C, RIGID CARGO BARRIER FLOOR FITTING NR 10 IS CORRODED. R & R CORRODED RCB FLOOR FITTING IAW AMM 25-59-13-400-802C1.Aug 7, 2016 · N250UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016090707964Channel · corrodedINSPECTION TYPE:3C, FORWARD LOWER CARGO COMPARTMENT AFT BULKHEAD FLOOR CHANNEL CORRODED STA 6-73 X= -24. FLOOR CHANNEL REPAIRED EA 011-5310-01-A6422 REV IR AND EO MD11-5310-61784-A, MAJOR.Aug 7, 2016 · N250UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016090107723Floor Support · corrodedINSPECTION TYPE:3C, AFT CARGO COMPARTMENT FLOOR SUPPORT UPPER FLANGE CORRODED STA 1841 X=51, FLANGE REPAIRED IAW EA 011-5300-01-A6390, REV IR AND EO MD11-5340-61744-A, MAJOR.Aug 7, 2016 · N250UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016083107680Fuel Cell · corrodedINSPECTION TYPE: 3C, CENTER WING TANK UPPER AFT SKIN CORRODED AT XCW 114 ALONG STRINGER 3. REPAIRED IAW EA 011-5730-01-A6395 REV. IR AND EO MD11-5730-61653-A.Aug 7, 2016 · N250UP · Doug MD11F · Fuel StorageSDR IPXA2016082807527Skin · crackedINSPECTION TYPE: 3C, R3 DOOR INNER FRAME SKIN CRACKED AT UPPER AFT CORNER CRACKED. REPAIRED IAW EA 011-5310-01-A6388 REV. IR AND EO MD11-5310-61688-A. MAJORAug 7, 2016 · N250UP · Doug MD11F · Service DoorsSDR IPXA2016082407436Skin · gougedINSPECTION TYPE: 3C, LEFT HORIZONTAL STAB LEADING EDGE INNER RIB STIFFENER GOUGED. STIFFENER REPAIRED PER EA 011-5510-01-A6401 REV. IR AND EO MD11-5510-61675-A.Aug 7, 2016 · N250UP · Doug MD11F · Horizontal Stabilizer, Plate/SkinSDR IPXA2016082507464Longeron · crackedINSPECTION TYPE: 3C, LONGERON 27L CRACKED IN SUBFLOOR AREA BELOW L3 DOOR. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW DWG AEA7127, SRM 51-31-01, AND 51-33-01.Aug 7, 2016 · N250UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2016082407434Structure · corrodedINSPECTION TYPE: 3C, MAIN CABIN SUBFLOOR CENTER TANK UPPER STRUCTURE CORRODED XCW 31R - 46R STRINGER 18-19. REPAIRED PER EA 011-5730-01-A6391 REV. IR AND EO MD11-5730-61660-A.Aug 7, 2016 · N250UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2016081907238Bulkhead · gougedINSPECTION TYPE:3C, HORIZONTAL STABILIZER CONSTANT SECTION RT SIDE TRIM ACTUATOR ATTACH ARM OPERATING, BULKHEAD GOUGED. GOUGED BULKHEAD REPAIRED IAW EA 011-5510-01-A6392, REV IR AND EO MD11-5510-61621-A, MINOR.Aug 7, 2016 · N250UP · Doug MD11F · Horizontal Stabilizer, Spar/RibSDR IPXA2016081907232Skin · dentedINSPECTION TYPE: 3C, R1 DOOR EXTERIOR SKIN DENTED ALONG FWD AND AFT EDGES BETWEEN BEAMS 4 AND 5. THE R1 DOOR WAS REPAIRED IAW EA 011-5210-01-A6389 REV. IR AND EO MD11-5230-61604-A.Aug 7, 2016 · N250UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2016081507050Door Frame · crackedINSPECTION TYPE: 3C, R3 DOOR FRAME INTERIOR WEB CRACKED AT LOWER FWD LIGHTENING HOLE, BS 1305, Z-18. REPAIRED THE DOOR FRAME WEB IAW SRM 53-40-15 REPAIR 3 FIG. 201.Aug 7, 2016 · N250UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2016090707989Former · crackedINSPECTION TYPE:3C, NR 2 PYLON LOWER AFT FAIRING RT SIDE INTERNAL FORMER CRACKED. PYLON FAIRING REPAIRED IAW EA 011-5410-01-A6407 REV IR AND EO MD11-61785-A.Aug 6, 2016 · N250UP · Doug MD11F · Nacelle/Pylon, Main FrameSDR IPXA2016090407807Skin · corrodedINSPECTION TYPE:3C, AFT FUSELAGE SKIN AT STA 1997.750 TO 2150 AND BETWEEN L32R-L35R IS CORRODED. REPAIRED CORRODED AFT FUSELAGE SKIN AT STA 1997.750 TO 2150 BETWEEN L32R-35R IAW EA 011-5330-01-A6412, REV I/R AND EO MD11-5330-61755-A.Aug 6, 2016 · N250UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2016090407805Skin · corrodedINSPECTION TYPE:3C, AFT FUSELAGE SKIN BETWEEN STA 1986-2163, LT-10R TO LT-13R IS CORRODED. REPAIRED CORRODED FUSELAGE SKIN AT STA 1986-2163 BETWEEN L-1OR TO L-13R IAW EA 011-5330-01-A6417, REV I/R AND EO MD11-5330-61765-A.Aug 6, 2016 · N250UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2016090307792Skin · corrodedINSPECTION TYPE:3C, AFT EXTERIOR FUSELAGE SKIN CORRODED STA 1986-2015, L10L - L11L. AFT FUSELAGE SKIN CORROSION REPAIRED IAW EA 011-5330-01-A6423 REV IR AND EO MD11-5330-61761-A.Aug 6, 2016 · N250UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2016082807519Support · corrodedINSPECTION TYPE: 3C, RT FUSELAGE HORIZONTAL STAB FAIRING SUPPORT CORRODED BEYOND LIMITS, BS 2026. REMOVED FABRICATED AND INSTALLED A REPLACEMENT FAIRING SUPPORT IAW DWG AJC7405, SRM 51-31-01, AND 51-35-01.Aug 6, 2016 · N250UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016081707138Longeron Splice · crackedINSPECTION TYPE: 3C, LONGERON 24R SPLICE FITTING CRACKED AT STA. 5-123. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT SPLICE FITTING IAW DWG A5A7112 AND SRM 51-33-01.Aug 6, 2016 · N250UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2016090707983Fitting · corrodedINSPECTION TYPE:3C, RCB FLOOR FITTING NR 4 CORRODED. FITTING REPAIRED IAW EA 011-5310-01-A6384 REV IR AND EO MD11-2550-61655-A, MINOR.Aug 5, 2016 · N250UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016083107679Roller Tray · corrodedINSPECTION TYPE: 3C, CENTER CARGO BAY ROLLER TRAY CORRODED AT RT SIDE, BS 1701. REPAIRED IAW EA 011-2550-01-A6411 REV. IR AND EO MD11-2550-61652-A.Aug 5, 2016 · N250UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016082807526Pan · gougedINSPECTION TYPE: 3C, MAIN CARGO DOOR FWD PAN GOUGED JUST ABOVE LOWER CORNER GOUGED. REPAIRED IAW EA 011-5230-01-A6383 REV. IR AND EO MD11-5230-61600-A.Aug 5, 2016 · N250UP · Doug MD11F · Cargo/Baggage DoorsSDR IPXA2016082607485Longeron · corrodedINSPECTION TYPE:3C, LONGERON 49R CORRODED AT BS 1129. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT SECTION OF THE LONGERON IAW DWG A6A7026 AND SRM 51-33-01.Aug 5, 2016 · N250UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2016082407419Floor Panel · corrodedINSPECTION TYPE :3C, RCB AREA FLOOR PANEL WSP0792-501 CORRODED BEYOND ALLOWABLE LIMITS. REMOVED AND REPLACED THE FLOOR PANEL IAW SRM 53-21-04-400-801.Aug 5, 2016 · N250UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2016081707157Fitting · corrodedFLOOR FITTNG AT RBL 47 CORRODED ON LOWER SURFACE. REPAIRED IAW EA 011-5340-01-A6376 REV. A AND EO MD11-5340-61584-B.Aug 5, 2016 · N250UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2016081707156Seat Track · corrodedSEAT TRACK CORRODED AT BS 488 LBL 27 CORRODED. THE SEAT TRACK WAS REPAIRED IAW EA 011-5310-01-A6387 REV. IR AND EO MD11-5340-61591-A.Aug 5, 2016 · N250UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2016090107722Support · corrodedINSPECTION TYPE:3C, UPPER FORWARD RUDDER BALANCE WEIGHT SUPPORT ASSEMBLY CORRODED. CORROSION REPAIRED IAW EA 011-5540-01-A6396, REV IR AND EO MD11-5540-61702-A, MAJOR.Aug 4, 2016 · N250UP · Doug MD11F · Rudder Miscellaneous StructureSDR IPXA2016082307383Access Panel · damagedINSPECTION TYPE: 3C, RT WING L/E LOWER ACCESS PANEL 616AB DAMAGED. REMOVED, FABRICATED, AND INSTALLED A NEW ACCESS PANEL IAW DWG ARB3032 AND SRM 51-31-01.Aug 4, 2016 · N250UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2016082107273Stringer · crackedINSPECTION TYPE:3C, RT WING STR NR 15 IS CRACKED AT STA XORS 440. REPAIRED CRACKED RT WING, STR 15 BETWEEN STA XORS 433 TO 455 IAW SRM 57-20-03, REPAIR 3, FIG 201.Aug 4, 2016 · N250UP · Doug MD11F · Wing, Longeron/StringerSDR IPXA2016081507063Stringer · crackedINSPECTION TYPE: 3C, RIGHT WING STRINGER 12 CRACKED XORS 622 - 653. STRINGER REPAIRED IAW SRM 57-00-03 REPAIR 5 FIG. 202. MAJOR.Aug 4, 2016 · N250UP · Doug MD11F · Wing, Longeron/StringerSDR IPXA2016081507061Stringer · crackedINSPECTION TYPE: 3C, RIGHT WING STRINGER 11 CRACKED XORS 683 - 713 CRACKED. STRINGER REPAIRED IAW SRM 57-00-03 REPAIR 5 FIG. 202. (MAJOR)Aug 4, 2016 · N250UP · Doug MD11F · Wing, Longeron/StringerSDR IPXA2016090708002Structure · corrodedINSPECTION TYPE: 3C, RCB WALL HAS CORROSION IN IN FWD SIDE AT MATING SURACE OF FLOOR FITTING LEFT SIDE. REPAIRED RCB WALL IAW EA 011-5310-01-A6378 I/R, AND ER MD11-5310-61777-A.Aug 3, 2016 · N250UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2016090707990Support Channel · crackedINSPECTION TYPE:3C, FWD CARGO PIT CEILING SUPPORT CHANNEL CRACKED STA 918, RBL 13. SUPPORT CHANNEL REPAIRED IAW EA 011-2552-01-A6418, REV IR AND EO MD11-2550-61786-A.Aug 3, 2016 · N250UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016090307786Skin · crackedINSPECTION TYPE:3C, CRACKS AT MULTIPLE RIVETS AROUND PERIPHERY OF NR 2 ENGINE INLET NOSE COWL LIP SKINS. R & R NR 2 INLET COWL ASSY IAW AMM 54-22-01.Aug 3, 2016 · N250UP · Doug MD11F · Engine Cowling SystemSDR IPXA2016090307785Skin · chafedINSPECTION TYPE:3C, AREA OF CHAFE DAMAGE AND CORROSION ON FUSELAGE SKIN STA 1137-1156, L43R -L44R. SKIN PANEL REPAIRED IAW EA 011-5330-01-A6377, REV IR AND EO MD11-5330-61753-A.Aug 3, 2016 · N250UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2016081707141Skin · chafedINSPECTION TYPE: 3C, LEFT WING FIXED L/E PANEL 517AB CHAFED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SKIN IAW DWG ARB1055 AND SRM 51-35-01.Aug 3, 2016 · N250UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2016081607124Skin · chafedINSPECTION TYPE: 3C, CHAFE DAMAGE IN EXTERNAL FUSELAGE SKIN BS 1156 BETWEEN LONGERONS 43 - 44L. REPAIRED IAW SRM 53-40-01 REPAIR 2 FIG. 201. MAJOR.Aug 3, 2016 · N250UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2016081507062Attach Fitting · crackedINSPECTION TYPE: 3C, RIGHT MLG WW INBD DOOR RETRACT CYLINDER UPPER ATTACH FITTING CRACKED. REPAIRED THE ATTACH FITTING IAW SRM 53-40-12 REPAIR 3 FIG. 201. (MAJOR)Aug 3, 2016 · N250UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2016081206933Stiffener · crackedINSPECTION TYPE: 3C, RIGHT MLG WW AFT OTBD WALL, 3RD VERTICAL STIFFNER IS CRACKED. REMOVED, FABRICATED AND REPLACED THE STIFFNER IAW DWG ANB7203 AND SRM 51-35-01.Aug 3, 2016 · N250UP · Doug MD11F · Fuselage Miscellaneous Structure
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