N255UP

Service difficulty reports · 389

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 = 'N255UP' 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 IPXA2017030714849Barrier · corrodedINSPECTION TYPE: 2C, RIGID CARGO BARRIER LOWER CLOSURE HAS CORROSION AT X=69.5 AND X=76. REPAIRED THE CARGO BARRIER IAW EA 011-5320-01-A6690 REV I/R AND EO MD11-5310-63507-A.Feb 21, 2017 · N255UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017030714846Skin · corrodedINSPECTION TYPE: 2C, THE L3 DOOR CUTOUT INNER SKIN HAS CORROSION AT BS 1260 AND Z=-17 TO Z=-19. REPAIRED THE DOOR SKIN IAW SRM 53-40-15, REPAIR 4, FIG 201. (MAJOR)Feb 20, 2017 · N255UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2017030814881Floor Panel · corrodedINSPECTION TYPE: 2C, MAIN CABIN FLOOR PANEL AT BS 475-495, LBL 80 - 84.5 IS CORRODED. REMOVED AND REPLACED THE FLOOR PANEL IAW DWG WSP0791 AND SRM 53-20-05.Feb 19, 2017 · N255UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2017030614777Floor Panel · corrodedINSPECTION TYPE: 2C, MAIN CABIN FLOOR PANEL AT BS 475 - 500, BETWEEN LBL 19 - 27.5 HAS CORROSION. REPAIRED THE FLOOR PANEL IAW EA 011-5320-01-A6680 REV I/R, AND EO MD11-5320-63479-A.Feb 19, 2017 · N255UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2017030614776Floor Panel · corrodedINSPECTION TYPE: 2C, MAIN CABIN FLOOR PANEL BETWEEN BS 475 - 500, RBL 36 - 47.5 HAS HEAVY CORROSION. REMOVED AND REPLACED THE FLOOR PANEL IAW DWG WSP0788, AND SRM 51-33-01.Feb 19, 2017 · N255UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2017030314650Bulkhead Web · crackedINSPECTION TYPE: 2C, RIGHT MAIN LANDING GEAR WW WEB IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE BULKHEAD WEB IAW DWG ANB7180, AND SRM 51-35-01.Feb 19, 2017 · N255UP · Doug MD11F · Fuselage Main, BulkheadSDR IPXA2017030214618Fitting · chafedINSPECTION TYPE: 2C, RIGID CARGO BARRIER SIDE FITTING NR 13 HAS CHAFE DAMAGE. REPAIRED THE FITTING IAW EA 011-5340-01-A6668 REV I/R, AND EO MD11-5340-63366-A.Feb 19, 2017 · N255UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017030714836Fitting · corrodedINSPECTION TYPE: 2C, RIGID CARGO BARRIER FLOOR FITTING NR 6 HAS CORROSION. REPAIRED THE FITTTING IAW EA 011-5340-01-A6672 AND EO MD11-5340-63398-A.Feb 17, 2017 · N255UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2017030714835Fitting · corrodedINSPECTION TYPE: 2C, RIGID CARGO BARRIER FLOOR FITTING NR 8 HAS CORROSION. REPAIRED THE FITTING IAW EA 011-5340-01-A6674 REV I/R, AND EO MD11-5340-63424-A.Feb 17, 2017 · N255UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2017030514716Floor Panel · corrodedINSPECTION TYPE: 2C, MAIN CABIN FLOOR PANEL BETWEEN BS 475 - 500.175 BL 0 - LBL 8.5 HAS CORROSION. REPAIRED THE FLOOR PANEL IAW EA 011-5320-01-A6681 REV I/R, AND EO MD11-5320-63480-A.Feb 17, 2017 · N255UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2017030314653Floor Panel · corrodedINSPECTION TYPE: 2C, MAIN CABIN FLOOR PANEL BETWEEN BS 475 TO 500, RBL 62.190 - 73.340. REPAIRED THE FLOOR PANEL IAW EA 011-5310-01-A6676 REV I/R, AND EO MD11-5320-63466-A.Feb 17, 2017 · N255UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2017022814515Fitting · corrodedINSPECTION TYPE:2CRIGID CARGO BARRIER FLOOR FITTING AT POS. #5 HAS CORROSION.REMOVED AND REPLACED RIGID CARGO BARRIER FLOOR FITTING AT POS. #5 IAW DWG. SP11250221 AND SRM 53-20-50.Feb 17, 2017 · N255UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2017022814514Fitting · corrodedINSPECTION TYPE: 2C, RIGID CARGO BARRIER FLOOR FITTING AT NR 2 HAS CORROSION. REMOVED AND REPLACED THE FITTING IAW DWG SP11250221, AND SRM 53-20-50.Feb 17, 2017 · N255UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2017022814513Fitting · corrodedINSPECTION TYPE: 2C, RIGID CARGO BARRIER FLOOR FITTING NR 4 HAS CORROSION ON BOTTOM SURFACE. REMOVED AND REPLACED THE FITTING IAW DWG SP11250221 AND SRM 53-20-50.Feb 17, 2017 · N255UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2017022814512Fitting · corrodedINSPECTION TYPE: 2C, RIGID CARGO BARRIER FLOOR FITTING HAS CORROSION ON BOTTOM SURFACE.REMOVED AND REPLACED RIGID CARGO BARRIER FLOOR FITTING IAW DWG SP11250221, AND SRM 53-20-50, REPAIR 1 .Feb 17, 2017 · N255UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2017030714850Barrier · corrodedINSPECTION TYPE: 2C, RIGID CARGO BARRIER LOWER CLOSURE HAS CORROSION RBL 81 AND LBL 12.2. REPAIRED THE CARGO BARRIER LOWER CLOSURE IAW EA 011-5320-01-A6690 REV I/R, AND EO MD11-5310-63507-A.Feb 15, 2017 · N255UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017030614791Skin · corrodedINSPECTION TYPE: 2C, RIGHT WING UPPER SKIN HAS CORROSION AT XORS 440 - 530 AND BETWEEN STRINGERS 1 - 4. REPAIRED THE SKIN IAW EA 011-5730-01-A6686, REV I/R, AND EO MD11-5730-63514-A.Feb 15, 2017 · N255UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2017030614790Floor Panel · corrodedINSPECTION TYPE: 2C, MAIN CABIN FLOOR PANEL HAS CORROSION AT BS 488 BETWEEN RBL 17 - 27.5. REMOVED AND REPLACED THE FLOOR PANEL IAW DWG WSP0785 AND SRM 51-31-01.Feb 15, 2017 · N255UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2017030614788Skin · corrodedINSPECTION TYPE: 2C, RT WING UPPER SKIN HAS CORROSION AT XORS. 440 - 530 AND BETWEEN STRINGERS 1 - 4. REPAIRED THE SKIN IAW EA 011-5730-01-A6686, REV I/R, AND EO MD11-5730-63514-A.Feb 15, 2017 · N255UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2017030214619Longeron Splice · crackedINSPECTION TYPE: 2C, LONGERON SPLICE 30R CRACKED AT BS 1530. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT LONGERON SPLICE IAW DWG A5A7112, AND SRM 51-33-01.Feb 15, 2017 · N255UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2017030114564Longeron Splice · crackedINSPECTION TYPE: 2C, CENTER CARGO AT BS 1541, LONGERON 38L SPLICE IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SPLICE IAW DWG A5A7114, AND SRM 51-33-01.Feb 15, 2017 · N255UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2017030614807Support Angle · crackedINSPECTION TYPE: 2C, RT WING O/B FLAP I/B HINGE AFT FAIRING I/B SIDE SUPPORT ANGLE IS CRACKED.REMOVED, FABRICATED AND REPLACED THE SUPPORT ANGLE IAW DWG ARC2229 AND SRM 51-35-02.Feb 14, 2017 · N255UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2017030614805Beam · crackedINSPECTION TYPE: 2C, RIGHT WING OTBD FLAP INBD HINGE AFT FAIRING, OTBD SIDE SUPPORT BEAM IS CRACKED. REMOVED, FABRICATED, AND REPLACED FLAP FAIRING SUPPORT BEAM IAW DWG ARC2149-4, AND SRM 51-35-02.Feb 14, 2017 · N255UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2017030714857Stanchion · corrodedINSPECTION TYPE: 2C, FWD LOWER CARGO AT BS 6-70 LBL 57, VERTICAL STANCHION IS CORRODED. REPAIRED THE STANCHION IAW EA 011-5310-01-A6663 REV I/R AND EO MD11-5310-63528-A. (MAJOR)Feb 14, 2017 · N255UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017030614745Shear Tie · crackedINSPECTION TYPE: 2C, TAIL BS 2123, RBL 8 FRAME SHEAR TIE IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE SHEAR TIE IAW DWG AKC7372 AND SRM 51-31-01.Feb 14, 2017 · N255UP · Doug MD11F · Fuselage Internal Mounting StructureSDR IPXA2017030514718Skin · corrodedINSPECTION TYPE: 2C, RT WING UPPER SKIN HAS CORROSION AT XORS 337.5 & 355, ABOVE STRINGER 2. REPAIRED THE SKIN IAW EA 011-5730-01-A6685, REV I/R, AND EO MD11-5730-63487-A.Feb 14, 2017 · N255UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2017030514715Skin · corrodedINSPECTION TYPE: 2C, RIGHT WING UPPER SKIN HAS CORROSION BETWEEN XORS 230 - 253, XORS 278 - 284.5, AND XORS 276-298. REPAIRED THE SKIN IAW EA 011-5730-01-A6689 REV I/R, AND EO MD11-5730-63488-A.Feb 14, 2017 · N255UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2017022814529Longeron · corrodedINSPECTION TYPE: 2C, FWD LOWER CARGO AT BS 1119 LONGERON 51R IS CORRODED. REPAIRED THE LONGERON IAW SRM 53-00-05, REPAIR 1, FIG. 201.Feb 14, 2017 · N255UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2017030714860Vane · crackedINSPECTION TYPE: 2C, NR 2 ENGINE LEFT THRUST REVERSER CLOSURE WEB IS CRACKED JUST FWD OF THE NR 4 CASCADE VANE. REPAIRED THE VANE IAW EA 011-7830-01-A6682 REV I/R AND EO MD11-7830-63532-A.Feb 13, 2017 · N255UP · Doug MD11F · Engine Thrust ReverserSDR IPXA2017030514720Fastener · missingINSPECTION TYPE: 2C, NR 2 ENGINE INLET COWL HAS A MISSING FASTENER. INSTALLED THE FASTENER IAW EA 011-7110-01-A6677, REV. I/R AND UPS EO MD11-7110-63395-A.Feb 13, 2017 · N255UP · Doug MD11F · Turbine Engine Air Inlet SectionSDR IPXA2017030514717Torque Tube · chafedINSPECTION TYPE: 2C, R4 DOOR LOWER TORQUE TUBE CHAFED. REPAIRED THE TORQUE TUBE IAW EA 011-5210-01-A6673, REV I/R, AND EO MD11-5210-63432-A.Feb 13, 2017 · N255UP · Doug MD11F · Service DoorsSDR IPXA2017030614778Longeron · corrodedINSPECTION TYPE: 2C, LONGERON 28R HAS CORROSION BETWEEN BS 1245 AND 1335. REPAIREDTHE LONGERON IAW EA 011-5310-01-A6675 REV I/R AND EO MD11-5310-63486-A.Feb 13, 2017 · N255UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2017030314652Skin Splice · crackedINSPECTION TYPE: 2C, RT WING FIXED L/E SKIN SPLICE STRAP IS CRACKED AT XOS. 905.5. REMOVED, FABRICATED, AND REPLACED SKIN SPLICE STRAP IAW DWG ARB3954, AND SRM 51-33-01.Feb 13, 2017 · N255UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2017030314649Former · crackedINSPECTION TYPE: 2C, RT WING FIXED L/E SUPPORT FORMER IS CRACKED AT XOS. 905. REMOVED, FABRICATED, AND REPLACED THE SUPPORT FORMER IAW DWG. ARB1164 AND SRM 51-33-01.Feb 13, 2017 · N255UP · Doug MD11F · Wing Miscellaneous StructureSDR IPXA2017022814537Rib · crackedINSPECTION TYPE: 2C,RT WING FIXED L/E LOWER RIB, STIFFNER ANGLE IS CRACKED AT XOS. 542. REMOVED, FABRICATED, AND REPLACED R/H WING FIXED LOWER RIB IAW DWG ARB2918, SRM 51-33-01, AND 51-35-01.Feb 13, 2017 · N255UP · Doug MD11F · Wing, Rib/BulkheadSDR IPXA2017030114566Support Angle · crackedINSPECTION TYPE: 2C, RT WING FIXED L/E FUEL QUANTITY LOAD SELECTOR INBD SUPPORT ANGLE IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE SUPPORT ANGLE IAW DWG ARB2383, AND SRM 51-35-01.Feb 13, 2017 · N255UP · Doug MD11F · Wing Miscellaneous StructureSDR IPXA2017030114565Support Angle · crackedINSPECTION TYPE: 2C, RT WING FIXED L/E FUEL QUANTITY LOAD SELECTOR OTBD SUPPORT ANGLE IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE SUPPORT ANGLE IAW DWG ARB2382, AND SRM 51-35-01.Feb 13, 2017 · N255UP · Doug MD11F · Wing Miscellaneous StructureSDR IPXA2017022214335Doubler · crackedINSPECTION TYPE: 2C, RT WING FIXED L/E BEADED DOUBLER IS CRACKED AT XOS. 665. REPAIRED THE DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG. 203. (MAJOR)Feb 13, 2017 · N255UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2017030814891Tee Fitting · crackedINSPECTION TYPE: 2C, LOWER FWD. CARGO BULKHEAD BS 6-73, LBL 57 TEE WEB IS CRACKED AT Z=-95. REPAIRED THE BULKHEAD WEB TEE IAW EA 011-5310-01-A6667 REV I/R AND EO MD11-5310-63538-A. (MAJOR)Feb 12, 2017 · N255UP · Doug MD11F · Fuselage Main, BulkheadSDR IPXA2017030514719Intercostal · crackedINSPECTION TYPE: 2C, RIGHT MLG WHEEL WELL CENTER LOWER ACCUMULATOR INTERCOSTAL IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE INTERCOSTAL IAW DWG AEA0218 AND SRM 51-33-01.Feb 12, 2017 · N255UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017030314651Support Angle · crackedINSPECTION TYPE: 2C, RT MAIN GEAR WW SUPPORT ANGLE OTBD EDGE IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE SUPPORT ANGLE IAW DWG ANB7180 AND SRM 51-35-01.Feb 12, 2017 · N255UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017030114567Intercostal · crackedINSPECTION TYPE: 2C, LT WHEEL WELL FWD. ACCUMULATOR INTERCOSTAL IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE INTERCOSTAL IAW DWG. AEA0218 AND SRM 51-33-01 & 51-35-01.Feb 12, 2017 · N255UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017022714476Support · crackedINSPECTION TYPE: 2C, RT MLG WW OTBD, AFT BULKHEAD VERTICAL STIFFENER CHANNEL CRACKED. REMOVED FABRICATED AND INSTALLED REPLACEMENT SUPPORT STIFFENER IAW DWG ANB7203 AND SRM 51-33-010.Feb 12, 2017 · N255UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017030714825Hinge Fitting · wornINSPECTION TYPE: 2C, RIGHT FWD CENTER GEAR DOOR HINGE SUPPORT FITTING IS WORN. REPAIRED THE DOOR HINGE SUPPORT FITTING IAW EA 011-5310-01-A6671 REV I/R, AND EO MD11-5310-63520-A.Feb 10, 2017 · N255UP · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR IPXA2017030814883Fitting · crackedINSPECTION TYPE: 2C, RIGID CARGO BARRIER FLOOR FITTING NR 1 IS CRACKED. REMOVED AND REPLACED THE FITTING IAW EO MD11-2520-58701-D.Feb 10, 2017 · N255UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2016110310194Evas Unit · unsecureFO EVAS COMPARTMENT DOES NOT REMAIN ATTACHED TO BULKHEAD. SECURED IAW AMM 25-69-00-401 REV 86.02.Nov 2, 2016 · N255UP · Doug MD11F · Emergency EquipmentSDR IPXA2016060704347Handle · inoperativeGEAR HANDLE WOULD NOT RAISE TO THE UP POSITION. REPLACED LANDING GEAR CONTROL MECHANISM REF 32-31-02-401, OPS OK.Jun 4, 2016 · N255UP · Doug MD11F · Landing Gear SelectorSDR IPXA2016032201062Battery Pack · failedEMERGENCY LIGHTING BATTERY TEST FAILED ON PDC. R & R EMERGENCY POWER SUPPLY BATTERY IAW AMM 33-51-01. OPS CKS GOOD.Mar 21, 2016 · N255UP · Doug MD11F · Emergency LightingSDR IPXA2016012098134Bottle · low pressureENTRY DOOR L1 PNEUMATIC BOTTLE LOW. DEFERRED L1 ENTRY DOOR PNEUMATIC BOTTLE LOW IAW MEL 52-10-32. PLACARD INSTALLEDSERVICE PNEUMATIC BOTTLE IAW AMM 12-25-04. PLACARD REMOVED.Jan 20, 2016 · N255UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2015090993314Relay · inoperativeR1 DOOR WILL NOT OPEN. R & R RELAY R2-5325, IAW SWPM 20-00-09 AND WDM 52-11-01, SHEET 2.Sep 8, 2015 · N255UP · Doug MD11F · Service Doors
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