N254UP

Service difficulty reports · 345

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 = 'N254UP' 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 UPS08M53944Doubler · damagedINSPECTION TYPE:1C SURVEY SEQUENCE NUMBER 254-F1-007 OF MD11-5100-30530 APPENDIX C SECTION D, BLEND ON DOUBLER AT FWD LWR SIDE STA 1984 L39L. REMOVED EXISTING DOUBLER AND FILLER, FABRICATED FILLER AND DOUBLER 1 AND REPAIR DOUBLER 2 AND INSTALLED IAW MD11 VOL Nov 15, 2008 · N254UP · Doug MD11F · Fuselage Main, Plate/SkinSDR UPS08M53933Skin · corrodedINSPECTION TYPE:1C SURVEY SEQUENCE NUMBER 254-F1-008 OF MD11-5100-30530 APPENDIX C ITEM 2 CORROSION FOUND ON FASTENER HOLE ON REPAIR DOUBLER RT SIDE STA 2134 L33R- L35R. REMOVED REPAIR, FABRICATED, AND INSTALLED NEW REPAIR DOUBLER IAW MD-11 SRM VOL 1 53-00-01Nov 15, 2008 · N254UP · Doug MD11F · Fuselage Main, Plate/SkinSDR UPS08M53931Web · crackedINSPECTION TYPE:1C NR 2 ENGINE RT T/R LOWER FWD WEB FOUND CRACKED AND 2 EA FASTENERS BROKEN AT 5 O'CLOCK POSITION. STOP DRILLED CRACK, FABRICATED, AND INSTALLED DOUBLER IAW CF6-80C2 CMM 78-32-02, REPAIR 24.Nov 14, 2008 · N254UP · Doug MD11F · Engine Thrust ReverserSDR UPS08M53916Acoustic Panel · dentedINSPECTION TYPE:1C 2 EA DENTS AT 6 O'CLOCK POSITION 6 INCHES AND 18 INCHES FROM NOSE LIP IN NR 1 ENG INLET ACOUSTIC PANEL. REMOVED DAMAGE, FABRICATED AND INSTALLED PLUGS AND APPLIED FIBERGLASS IAW MD-11 SRM 54-10-00 REPAIR 18 STEPS C-F AND G-O.Nov 13, 2008 · N254UP · Doug MD11F · Engine Air Intake SystemSDR UPS08M53895Doubler · crackedINSPECTION TYPE:1C RT WING FIXED L/E COMPT AT XORS 506 HAS CRACK 4 EA AROUND FASTENERS HOLE ON BEADED DOUBLER. REMOVED DAMAGE, FABRICATED FILLER, ANGLES, AND DOUBLER, AND INSTALLED IAW MD-11 SRM 57-10-00 VOL 1 FIG 2.Nov 10, 2008 · N254UP · Doug MD11F · Wing Miscellaneous StructureSDR UPS08M53943Doubler · gougedINSPECTION TYPE:1C SURVEY SEQUENCE NUMBER 254-F1-003 OF MD11-5100-30530 APPENDIX C ITEM 3, GOUGE FOUND ON AFT EDGE OF REPAIR DOUBLER RT 879 TO 889 L38R TO L42R. REMOVED EXISTING DOUBLER 1, 2 AND 3, FABRICATED AND INSTALLED REPAIR DOUBLER 1, 2 AND 3 IAW MD11 VNov 9, 2008 · N254UP · Doug MD11F · Fuselage Main, Plate/SkinSDR UPS08M53926Doubler · gougedINSPECTION TYPE:1C SURVEY SEQUENCE NUMBER 254-F1-004 OF MD11-5100-30530 APPENDIX C SECTION C ITEM 3, FOUND 2 GOUGES ON FWD EDGE OF DOUBLER REPAIR STA 999 L-39R- L-42R. REMOVED PREVIOUS REPAIR DOUBLER, FABRICATED, AND INSTALLED NEW REPAIR DOUBLER 1 AND REPAIR Nov 9, 2008 · N254UP · Doug MD11F · Fuselage Main, Plate/SkinSDR UPS08M53894Doubler · crackedINSPECTION TYPE:1C RT WING FIXED L/E COMPT AT XORS 562 HAS CRACK 4 EA AROUND FASTENERS HOLE ON BEADED DOUBLER. REMOVED DAMAGE, FABRICATED FILLER, ANGLES AND DOUBLER, AND INSTALLED IAW MD-11 SRM 57-10-00 VOL 1 FIG 27.Nov 8, 2008 · N254UP · Doug MD11F · Wing Miscellaneous StructureSDR UPS08M53927Attach Fitting · crackedINSPECTION TYPE:1C LT WING AT STA XORS 562 FIXED L/E RIB ATTACH STRAP CRACKED. REMOVED, FABRICATED, AND INSTALLED STRAP IAW MD11 SRM 51-33-01 AND DWG ARB3954.Nov 6, 2008 · N254UP · Doug MD11F · Wing, Rib/BulkheadSDR UPS08M53983Web · gougedINSPECTION TYPE:1C NR 2 ENGINE RT T/R CENTER FWD WEB FOUND WITH GOUGE AT 3 O`CLOCK POSITION. GOUGE FOUND OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER IAW UPS EO MD11-7830-31193-A AND CF6-80C2 CMM 78-32-02 REPAIR 24.Oct 26, 2008 · N254UP · Doug MD11F · Engine Thrust ReverserSDR UPS08M53982Skin · dentedINSPECTION TYPE:1C RT WING O/B FLAP LOWER SURFACE 22 INCHES O/B OF PANEL 657FB 39 INCHES FROM T/E FOUND DENT. REMOVED DAMAGE AND BONDED REPLIES IAW UPS EO MD11-5750-31266-A AND SAA EA 011-5750-01-A1564.Oct 25, 2008 · N254UP · Doug MD11F · Trailing Edge FlapsSDR UPS08M53980Skin Panel · dentedINSPECTION TYPE:1C RT WING O/B FLAP LOWER SURFACE 18.5 INCHES O/B OF PANEL 657FB 36 INCHES FROM T/E FOUND DENT. REMOVED DAMAGE AND BONDED REPAIR PLIES IAW UPS EO MD11-5750-31247 -A AND SAA EA 011-5750-01-A1563.Oct 25, 2008 · N254UP · Doug MD11F · Trailing Edge FlapsSDR UPS08M53979Skin · erodedINSPECTION TYPE:1C AREA AT BOTTOM OF RT ELEVATOR AT O/B DAMPER HAS EROSION THRU COMPOSITE. REMOVED EXTERIOR COATING, DAMAGED COMPOSITE AND REPAIRED RT O/B ELEVATOR L/E IAW UPS EO MD11-5520-31233-A, SAA EA 011-5512-01 -A1559, MD-11 SRM 55-90-00 AND MD-11 SRM 5Oct 25, 2008 · N254UP · Doug MD11F · Elevator, Plate/SkinSDR UPS08M53978Skin · dentedINSPECTION TYPE:1C DENT ON RT EXTERIOR FUSELAGE SKIN STA 512 2 INCHES ABOVE S28R. CUT OUT DENT, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW MD-11 SRM 53-20-00 FIG 2.Oct 24, 2008 · N254UP · Doug MD11F · Fuselage Main, Plate/SkinSDR UPS08M51489Door · inoperativeCREW PREFLIGHT, L1 ENTRY DOOR WILL NOT OPEN, DEFERRED THE L1 DOOR PER MEL (M367452 ASSIGNED). REPLACED L1 DOOR UP LIMIT SWITCH S1-592 REF MD11 WDM 52-11-01 PG 1. OPS CHECK PER MD11 MM 52-12-00-0 AND 52-11-05-2. CHECKS OK, THIS CLEARS M367452. PLACARD REMOVJan 22, 2008 · N254UP · Doug MD11F · Passenger/Crew DoorsSDR UPS08M51407Valve · defectiveINSPECTION TYPE:N/A ATB - LEVEL 1 ALERT; ANTI ICE FAIL MESSAGE. PER BOW#TS2220 998 WAN #1316400 PERFORMED LEAK TEST AND PROOF TEST NR 1 ENG HIGH STAGE VALVE SENSE LINE PER MM 36-10-00-5. NO LEAK NOTED. REPLACED HIGH STAGE PILOT VALVE PER MM 36-11-20. REPLAJan 12, 2008 · N254UP · Doug MD11F · Pneumatic Distribution SystemSDR UPS08M51397Sensor · failedINSPECTION TYPE:N/A DIVERSION - ANTI ICE SENSOR FAIL (DIVERTED DUE TO ICING CONDITIONS) A/C IS OOS. PER FIM 30-82-00-1, FOUND SYSTEM IS OK. T/S IAW FIM 36-11-00-1, BUT COULDN'T DUPLICATE FAULT. PERFORMED VISUAL INSP OF THE NR 1 ENG HIGH STAGE SENSE LINE AND Jan 10, 2008 · N254UP · Doug MD11F · Airfoil Anti/De-ice SystemSDR UPS07M50674Skin · corrodedINSPECTION TYPE:4C RIGHT AFT EXTERIOR FUSELAGE SKIN STA 1879 TO 2153, LOWER AREA HAS CORROSION DAMAGE. REMOVED CORROSION FROM RIGHT AFT EXTERIOR FUSELAGE SKIN STA 1879-2153. ALL AREAS FOUND WITHIN LIMITS EXCEPT AT STA 2153 WAS OUT OF LIMITS. CUT OUT DAMAGE,Aug 25, 2007 · N254UP · Doug MD11F · Fuselage Main, Plate/SkinSDR UPS07M50623Rib · crackedINSPECTION TYPE:4C RIGHT WING NR 16 SLAT TRACK I/B FITTING (RIB) IS CRACKED. REMOVED AND REPLACED RIGHT WING NR 16 SLAT TRACK I/B FITTING (RIB) IAW MD-11 SRM 51-33-01 AND 51-35-01.Aug 16, 2007 · N254UP · Doug MD11F · Wing, Rib/BulkheadSDR UPS07M50622Rib · crackedINSPECTION TYPE:4C LEFT WING NR 16 SLAT TRACK I/B FITTING (RIB) IS CRACKED. REMOVED AND REPLACED LEFT WING NR 16 SLAT TRACK I/B FITTING (RIB) IAW MD-11 SRM 51-33-01 AND 51-35-01.Aug 16, 2007 · N254UP · Doug MD11F · Wing, Rib/BulkheadSDR UPS07M50120Sensor · malfunctionedINSPECTION TYPE:N/A ATB - NR 2 MANIFOLD FAIL MESSAGE. FUEL IMBALANCE, DUMPED 55.0 LBS OF FUEL TO LAND. DEFERRED UNDER M353851. AFTER CLEARING WAN 136845 REPLACED ALL 6 ZONE SENSORS NR 2 ENG ESC OP CHECKS NORMAL IN AUTO AND MANUAL MODE. ESC PASSES RTS TEST Jul 3, 2007 · N254UP · Doug MD11F · Pneumatic Distribution SystemSDR UPS07M49726Cover · unsecureLEFT SLIDE PACK COVER (EMERG EGRESS NOT SEATED PROPERLY). RESECURED COVER.Apr 30, 2007 · N254UP · Doug MD11F · Escape SlideSDR UPS07M48815Skin · crackedLEADING EDGE CRACK AFT OF NR 7 SLAT. FIXED L/E SKIN AFT OF NR 7 LT SLAT I/B SIDE AT STA X0S 906 REF 57-10-00 PG 104. DMG REMOVED. ROLLED DBLR & PICK UP HOLES FAB FROM 7075-76-063. DRILLED,TRIMMED, BEVELED & PRIMED SURFACE PER SRM 57-10-00. INSTALL DBLR. INSTJan 1, 2007 · N254UP · Doug MD11F · Wing, Plate/SkinSDR UPS06M47399Web · crackedNR 2 ENG PYLON WEB CRACKED ABOVE AFT HOIST ATTACH POINT LT SIDE. REMOVED DAMAGED LOWER WEB, ANGLE FITTING AND SUPPORT STRUT. ROUTED TE S/M SHOP FOR REPAIR. REWORKED SUPPORT STRUT LINK BY COLD WORKING PER EO MD11-5410-24738. ACCOMPLISHED HFEC OF LINK PER HDJul 22, 2006 · N254UP · Doug MD11F · Nacelle/Pylon Miscellaneous StructureSDR UPS06M47199Skin · crackedINSPECTION TYPE:3C FROM DMI LOG D326504: CTR LWR CARGO DOOR INTERIM REPAIR. ACCOMPLISHED PERMANENT REPAIR OF LOWER CENTER CARGO DOOR OUTER SKIN FORWARD LOWER CORNER EDGE CRACK IAW UPS ENGINEERING FILE NUMBER: MD11-52-20012 DATED:6/20/06,SAA EA011-5230-01-A02Jun 8, 2006 · N254UP · Doug MD11F · Cargo/Baggage DoorsSDR UPS06M46862Oxygen Mask · no testINSPECTION TYPE:N/A LEFT OBSERVERS 02 MASK IN FLT DECK WILL NOT TEST. ADJUSTED PLUNGER ACTUATOR AND INSTALLED MASK PER AMM 35-13-01, OPS OK.May 12, 2006 · N254UP · Doug MD11F · Crew Oxygen SystemSDR UPS05M45883Oxygen Mask · inoperativeFO O2 MASK FAILED TEST. SWAPPED F/O 02 MASK WITH 2ND OBSERVERS MASK IAW MM 35-13-10-4.Dec 19, 2005 · N254UP · Doug MD11F · Crew Oxygen SystemSDR UPS05M45537Windshield · crackedF/O FRONT WINDOW HAS A CRACK. R & R R1 WINDOW IAW MM 56-11-01-4.Sep 29, 2005 · N254UP · Doug MD11F · Flight Compartment WindowsSDR UPS05M44909Landing Gear · malfunctionedNOSE GEAR DOES NOT LOCK IN UP POS. INSPECTED NOSE GEAR LINKAGES, DOORS WHEEL WELL AND NOSE WHEEL STEERING NIL DEFECTS FOUND. JACKED A/C PER MD11 AMM 07-11-00-2 AND ILLEG NOSE GEAR PER AMM 32-30-00 FOUND NORMAL.Jul 14, 2005 · N254UP · Doug MD11 · Landing Gear Retraction/Extension SystemSDR UPS05M44908Landing Gear · malfunctionedNOSE GEAR DOES NOT LOCK IN UP POS. INSPECTED NOSE GEAR AND SHER WELL. NIL DAMAGE NOTED ALL LINKAGE CHK'D AND LUBED. NOSE WHEEL OPERATING OPS NORMAL PER KD-11 AMM 32-50-00 PSEU TEST IN PRIMARY AND ALT ILLE PER MD AMM 32-60-00Jul 14, 2005 · N254UP · Doug MD11 · Landing Gear Retraction/Extension SystemSDR UPS05M44674Spar Cap · corrodedINSPECTION TYPE: 2C, LT WING, UPPER SURFACE, AFT WING SPAR JUST FWD OF NR 3 SPOILER, STRAP HAS BULGE & CRACKED SEALANT, NEED TO EVALUATE FOR CORROSION (2 SPOTS). PERFORMED CORROSION REPAIR ON LT WING UPPER SURFACE AFT WING SPAR IAW SAA SK 254-796823 & UPS REPMay 8, 2005 · N254UP · Doug MD11F · Wing SparSDR UPS05M43681Bulb · inoperativeDOOR R1 BOTTLE PRESSURE TEST LIGHT INOP. PLACED R1 DOOR EVAC DOOR SLIDE PRESS TO TEST LIGHT ON DEFERRAL M-295479 IAW MD MEL 25-61-2. PERFORMED DMP 25-61-2. REMOVED AND REPLACED BATTERIES AND BULBS IAW MM 25-61-04, CHECKED FOUND SATISFACTORY. THIS CLEARS DEJan 19, 2005 · N254UP · Doug MD11F · Escape SlideSDR UPS04M42832Transponder · inoperativeINSPECTION TYPE:N/A, DIVERSION - BOTH ATC TRANSPONDER MODE C FUNC INOP. ATC REQUIRED DIV TO STN. *S/D* SWAPPED POSITIONS OF ATC TRANSPONDERS IAW 34-54-01. PERFORMED BITE CHECK ON BOTH ATC TRANSPONDERS CHECKED OK AS PER AMM 34-54-00 (OPERATIONAL TEST) POSITAug 1, 2004 · N254UP · Doug MD11F · ATC Transponder SystemSDR UPS04M42406Engine · malfunctionedON DESCENT, 8000 FT ALL ENGS DID NOT RESPOND TO THROTTLE COMMAND. PUSHED THROTTLES FULL FWD NO RESPONSE. TURNED ON IGN OVRD END CAME BACK. BOTH MCP PNLS CONFIRMED ENG OUT THRUST LIMITS SHOWED MCT EAD. OIL PRESS ON 1&3 FELL BELOW 19 PSI, ENG 2 OIL 22 PSI. N1'May 24, 2004 · N254UP · Doug MD11F · Engine (Turbine/Turboprop)SDR UPS04M41786Slide · will not testINSPECTION TYPE:N/A R1 DOOR EVACUATION SLIDE PRESS TO TEST INOP DEFERRED M 273762 PER MEL 25-61-2 PLACARD. RELAMPED R1 DOOR SLIDE WARNING LIGHT MM 25-61-04. THIS CLEARS M 273762.Jan 6, 2004 · N254UP · Doug MD11F · Escape SlideSDR UPS02M39529Frame · crackedINSPECTION TYPE:C CRACK FOUND ON OUTBOARD FLANGE OF FRAME AT SPLICE AREA STA 495 BETWEEN L13L TO L14L. CABIN STA 495 BETWEEN L13L-L14L O/B FRAME FLANGE CRACK AREA TRIMMED OUT AS PER EN NR 1110-02. FILLER FABRICATE AND INSTALLED AS PER EN NR 1110-02.Aug 26, 2002 · N254UP · Doug MD11F · Fuselage Main, FrameSDR UPS02M39835Seat Track · corrodedINSPECTION TYPE:C CABIN - SEAT TRACK CROWN HAS CORROSION AT STA 1361 X=107.25. SEAT TRACK BADLY CORRODED, EXCEEDED LIMITS IAW SRM 53-70-00 FIG 3 VOL 1 REV 31. NEW SEAT TRACK, SPLICE HAT REWORKED, SPLICE PLATE FABRICATED AND INSTALLED PER SRM 53-70-00 FIG.1 VAug 22, 2002 · N254UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS02M39421Seat Track · corrodedINSPECTION TYPE:C CORROSION FOUND ON SEAT TRACK CROWN AT STA 1964 X=-107. SEAT TRACK CORROSION EXCEEDS LIMIT IAW SRM 53-70-00 FIG 3 VOL 1. SEAT TRACK REMOVED PER SRM 51-31-01. SPLICE HAT AND PLATE FABRICATE IAW SRM 53-70-00 FIG 1. INSTALLED PER SRM 53-70-0Aug 12, 2002 · N254UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS02M39420Doubler · corrodedINSPECTION TYPE: C, STA 1905 STR 27 RT, SHEAR WEB LOWER SURFACE, CORRODED APPROXIMATELY 4 SQ INCHES WHERE INDICATED. RT WEB LOWER DOUBLER STA 1905, STR 27 RT, BADLY CORRODED & EXCEEDS LIMITS IAW SRM 53-00-01. REMOVED PER SRM 51-31-01. NEW DOUBLER FABAug 11, 2002 · N254UP · Doug MD11F · Fuselage Miscellaneous StructureSDR UPS02M39589Seat Track · corrodedINSPECTION TYPE:C CABIN SEAT TRACK HAS CORROSION AT STA 1351-1361 X=-75.25. SEAT TRACK AT STA 1351-1361 CORROSION EXCEED LIMITS PER SRM 53-70-00 FIG3 VOL1 REV31. SEAT TRACK FABRICATED & REPLACED FROM STA 1260 TO 1391 AS PER SRM53- 70-00 FIG1 VOL1 REV31.Aug 9, 2002 · N254UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS02M39218Doubler · corrodedINSPECTION TYPE:C, UPPER AUX TANK UPPER EXTERNAL SKIN HAS SLIGHT SURFACE CORROSION AT STA 1375 X=-47 TO X=-90. UPPER AUX TANK UPPER EXTERNAL SKIN CORROSION REMOVED BY HAND, CLEAN AND TREATED IAW SRM 51-21-01 VOL II REV 31. CORROSION FOUND WITHIN LIMIT EXCEPTAug 9, 2002 · N254UP · Doug MD11F · Fuel StorageSDR UPS02M39590Seat Track · corrodedINSPECTION TYPE:C CABIN SEAT TRACK CORRODED FROM STA1321 TO 1361X=75.25 & TRACK JOINER AT STA1351X=75.25. SEAT TRACK AT STA 1321 TO STA1361,X=75.25 & STA1351,X=75.25 EXCEEDED LIMIT AS PER SRM 53-70-00 FIG3 VOL1 REV31. SEAT TRACK FABRICATED & REPLACED FROM STAug 7, 2002 · N254UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS02M39422Floorbeam · corrodedINSPECTION TYPE:C CABIN FLOORBEAM HAS SURFACE CORROSION AND FASTENERS CORRODED AT STA 1361 X=115.00 TO X=107.25. FLOORBEAM AREA CORROSION BLENDED OUT AND FOUND EXCEEDS LIMIT PER SRM 53-00-01 VOL I.Aug 7, 2002 · N254UP · Doug MD11F · Fuselage Main, Floor BeamSDR UPS02M39351Skin · corrodedINSPECTION TYPE:C CABIN - UPPER AUX UPPER EXTERNAL SKIN HAS SURFACE CORROSION IN NINE PLACES FROM STA 1341 TO 1375 X=65 TO X=90.00. UPPER EXT SKIN SURFACE CORRODED CLEANED AND FOUND 2EA DOUBLERS EXCEEDED LIMIT IAW SRM 57-00-01 FIG 1A VOL I. DOUBLER FABRICATEAug 7, 2002 · N254UP · Doug MD11F · Fuselage Main, Plate/SkinSDR UPS02M39219Seat Track · corrodedINSPECTION TYPE:C, CABIN FLOOR SEAT TRACK HAS CORROSION AT STA 800 TO 805 X=8.5. SEAT TRACK CROWN CORROSION REMOVED, FOUND EXCEEDED LIMIT PER SRM 53-70-00 FIG 3 VOL I REV 31. SEAT TRACK SECTIONAL REPLACED FROM STA 783 TO STA 909 X=8.5.Aug 5, 2002 · N254UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
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