N281UP

Service difficulty reports · 277

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 = 'N281UP' 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 IPXA09M56714Skin · damagedINSPECTION TYPE: 1C DRILL START IN FUSELAGE SKIN AT FUS STA 1626, ONE INCH ABOVE LONG 42L. REAMED HOLE, FABRICATED AND INSTALLED FREEZE PLUG, FABRICATED AND INSTALLED REPAIR DOUBLER IAW EA 011-5330-A1903 AND UPS EO MD11-5330-34312-AJul 1, 2009 · N281UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA09M56705Skin · damagedINSPECTION TYPE: 1C REPAIR SURVEY SEQ NR 281-W4-03 RT INBD AILERON LWR SKIN EXTERNAL DOUBLER BETWEEN STA XIH329.911 TO XIH335.767, 2 EA FASTENER HEADS PULLED. REMOVED EXISTING REPAIR FROM RT WING INBD AILERON LWR SKIN BETWEEN STA XIH 329.911 TO XIH 335.767. Jul 1, 2009 · N281UP · Doug MD11F · AileronsSDR IPXA09M56753Skin · gougedINSPECTION TYPE: 1C SURVEY SEQ NR281-F1-04 REPAIR DOUBLER ON LWR AFT CORNER OF CTR CARGO DOOR CUTOUT EXTERNAL SKIN HAS DEEP GOUGE. REMOVED EXISTING REPAIR AT LWR AFT CORNER OF CTR CARGO DOOR CUTOUT. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF SRM VOL1 53Jun 29, 2009 · N281UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA09M56701Skin · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQ 281-W3-02 LT WING L/E TELESCOPIC REPAIR DOUBLER DOES NOT CORRELATE TO SRM AND DAMAGED INBOARD UPPER CORNER STA ZOS 4 61-XOS 473. REMOVED EXISTING REPAIR FROM LT WING L/E TELESCOPIC DUCT CUTOUT AT XOS 464 AND XOS 470. FABRJun 29, 2009 · N281UP · Doug MD11F · Wing, Plate/SkinSDR IPXA09M56494Solenoid · inoperativeL1 DOOR INOP. SUSPECTED SOLENOID 52-730 FAULTY. REMOVED AND REPLACED SOLENOID DOOR LOCK PIN RELEASE ON L1 DOOR REF MD11 AMM 52-10-06-4. PERFORMED OPS CHECK OF THE L1 DOOR. OPS CHECK GOOD. REF MD11 AMM 52-11-02-2. NO ADJUSTMENT REQUIRED. RE42858 SAA019 SJun 27, 2009 · N281UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA09M55780Wire · damagedINSPECTION TYPE:N/A LEFT W/W WIRE BUNDLE DAMAGED.May 2, 2009 · N281UP · Doug MD11F · Electrical Power System WiringSDR IPXA09M55811Wire Harness · damagedINSPECTION TYPE:N/A DURING NR 1 ENG RUN TO T/S EPR PROBLEM SMOKE AND SPARKS APPEARED AT THE LT WHEEL WELL AREA. FOUND BEHIND LT WING TRAILING EDGE ACCESS PANELS WIRE BUNDLE BURNED. ALL AFFECTED WIRED TO BE REPLACED, REFER TO NRC 268256.May 1, 2009 · N281UP · Doug MD11F · Electrical Power System WiringSDR IPXA09M55495Radome · damagedINSPECTION TYPE:N/A AT 1500 TO 2000 MSL A/C PASSED THROUGH LARGE FLOCK OF BIRDS. TOOK MULTIPLE HITS, NO IMMEDIATE DAMAGE NOTED. A/C RETURNED TO AIRPORT NORMALLY. NO EMERGENCY. PERFORMED BIRD STRIKE INSPECTION PER AMM 72-00-02-6. NOSE RADOME DAMAGE FROM BIApr 10, 2009 · N281UP · Doug MD11F · Aerodynamic FairingsSDR UPS08M53949Support Fitting · gougedINSPECTION TYPE:SPV DURING SPECIAL VISIT FOR GEAR CHANGE AT SAA, CORROSION WAS FOUND ON THE CLG TRUNNION SUPPORT FITTING, RT SIDE. WHILE PERFORMING MACHINING TO SUPPORT FITTING FAYING SURFACE, PER SRM 53-40-00 FIG 16, THE SET SCREWS FOR THE CUTTER TOOL CAME LNov 18, 2008 · N281UP · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR UPS08M53948Pan · crackedINSPECTION TYPE:SPV DURING SPECIAL VISIT- SAA, FOR MLG CHANGE, NLG DOOR JAMB AFT LT WAS FOUND TO BE BENT AND CRACKED. TRIMMED OUT DAMAGED AREA 3 INCHES, REPAIRED PERFORMED PER EO -MD11- 5320-31154-A AND PER INSTRUCTIONS IN EA 011-5320-01-A1555.Nov 18, 2008 · N281UP · Doug MD11F · Fuselage Miscellaneous StructureSDR UPS08M53097Rib · crackedINSPECTION TYPE:2C LEFT WING FIXED L/E RIB XFS 1024 CRACKED ON AFT SIDE BETWEEN FASTENERS. REMOVED, FABRICATED, AND INSTALLED RIB IAW MD-11 SRM 51-33-01 AND DWG ARB2920.Aug 10, 2008 · N281UP · Doug MD11F · Wing, Rib/BulkheadSDR UPS08M53096Structure · crackedINSPECTION TYPE:2C LT WING FIXED L/E TELESCOPIC DOOR CUTOUT FOUND CRACKED ON ONE SIDE. REMOVED CRACK, FABRICATED, AND INSTALLED FILLER AND DOUBLER IAW MD-11 SRM 57-10-00 FIG 43, 51-21-01, 51-35-01, 51-33-01.Aug 5, 2008 · N281UP · Doug MD11F · Wing Main, Frame StructureSDR UPS08M53093Skin · crackedINSPECTION TYPE:2C LEFT WING L/E SKIN SPLICE STRAP XFS 669 CRACKED. REMOVED SKIN SPLICE STRAP, REPLACED SKIN SPLICE STRAP IAW MD-11 SRM 51-33-01.Aug 4, 2008 · N281UP · Doug MD11F · Wing, Plate/SkinSDR UPS08M53095Support Angle · crackedINSPECTION TYPE:2C, LT WING FIXED L/E ANGLE SUPPORT AT STA XORS 346 FOUND CRACKED. REMOVED, FABRICATED AND INSTALLED ANGLE IAW MD-11 SRM 51-33-01 DWG ARB2918 AND SRM 51-21-01.Jul 31, 2008 · N281UP · Doug MD11F · Wing Miscellaneous StructureSDR UPS08M53094Floor Panel · corrodedINSPECTION TYPE:2C RCB FLOOR PANEL PART NUMBER WSPO785-501 HAS AREAS OF CORROSION. REMOVED AND REPLACED FLOOR PANEL IAW UPS EO MD11-5330-27218-C.Jul 31, 2008 · N281UP · Doug MD11F · Fuselage Floor PanelSDR UPS08M53108Skin Panel · chafedINSPECTION TYPE:2C RT WING I/B FIXED L/E SKIN PANEL FOUND WITH CHAFE ON O/B EDGE CORNER JUST FWD OF PANEL 616HB. REMOVED, FABRICATED AND INSTALLED RT WING I/B FIXED L/E SKIN PANEL IAW DWG ARB2434 AND MD-11 SRM 51-33-01 & 51-35-01.Jul 27, 2008 · N281UP · Doug MD11F · Wing, Plate/SkinSDR UPS08M53107Skin · crackedINSPECTION TYPE:2C RT WING L/E SKIN SPLICE AT XFS669 IS CRACKED. REMOVED CRACKED SPLICE, FABRICATED AND INSTALLED REPLACEMENT IAW DWG ARB3954 AND MD-11 SRM 51-33-01.Jul 26, 2008 · N281UP · Doug MD11F · Wing, Plate/SkinSDR UPS07M51083Connector · shortedNR 2 ENGINE START VALVE LIGHT ILLUMINATED IN FLIGHT. DURING T/S, FOUND PIN "D" ON SOCKET R5-8235 SHORTED. REQUESTED P/N;DC60-28M15SX AND DC63-28K15PX. REPAIRED AT CONNECTOR P1-8235, REF STANDARD WIRING PRACTICES MANUAL CHAPTER 20. NR 2 ENG START VALVE AND Nov 1, 2007 · N281UP · Doug MD11F · Engine Starting System WiringSDR UPS07M50128Battery · dischargedINSPECTION TYPE:N/A EMERGENCY LIGHT BATTERY LOW ALERT ILLUMINATED DURING EMERGENCY LIGHT TEST. DEF NR 353905. T/S C/O IAW FIM 33-51-01-00. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY IAW MM 33-51-01-4. OPS CHECKED SATISFACTORY. THIS CLOSES DJul 5, 2007 · N281UP · Doug MD11F · Emergency LightingSDR UPS07M49200Paint · missingINSPECTION TYPE:N/A LEFT WING UPPER TRAILING EDGE SKIN HAS SEVERAL AREAS OF PAINT MISSING JUST INBD OF WINGLET. LEFT WING INBD SIDE OF WINGLET SKIN HAS SEVERAL AREAS OF PAINT MISSING COMPOSITE PANELS & T/E IS DELAMINATED. ITEM DEFERRED D344293. *S/D* REMOVFeb 15, 2007 · N281UP · Doug MD11F · Wing, Plate/SkinSDR UPS06M48240Warning Message · illuminatedATB - LEVEL 2 "AILERON DEFLECT DISAGREE" UPON CLEAN UP AFTER T/O. FOLLOWED CHECKLIST PROCEDURES AND WHEN COMPLETED, THE LEVEL 2 ALERT RETURNED. FUEL WAS DUMPED AND A/C RETURNED TO ANC. DEFERRED PER MEL 27-13-2-01-1, PLACARD INSTALLED, M335539. DMP 27-13-2 Oct 12, 2006 · N281UP · Doug MD11F · Aileron Control SystemSDR UPS06M47749Coffeemaker · overheatedHOT CUP OVERHEAT DUE TO DEFAULT OF TIMER AND SUBSEQUENT MELT-DOWN OF 3 PIN CONNECTIONS W/ACRID FUMES IN COCKPIT AND EXCESSIVE HEAT AROUND OVEN AREA. REPLACED HOT CUP JUG AND PERFORMED OPS TEST OF HOT CUP TIMER AND FOUND NORMAL IAW 25-32-14-2. TIMER OPERATION Aug 22, 2006 · N281UP · Doug MD11F · Buffet/GalleysSDR UPS06M46459Fire Warning · intermittentFIRE DET 1 FAULT MESSAGE DISPLAYED AFTER ENG START (INTERMITTENT) PERFORMED FCDU RTS, ALL SYSTEMS PASSED. OK FOR SERVICE.Mar 16, 2006 · N281UP · Doug MD11F · Fire DetectionSDR UPS05M45896Seat Track · corrodedINSPECTION TYPE:C CABIN AT STA 1381 RT RBL 107.25 SEAT TRACK CROWN FOUND WITH CORROSION. CORROSION REMOVED PER SRM 51-2101 REV 31 VOL II AT SEAT TRACK & MAT REMOVED 0.038 INCH ORIG THK 0.100 INCH & FOUND EXCEED LIMIT PER SRM 53-70-00 VOL I REV 37 FIG 3. NEW Oct 21, 2005 · N281UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS05M45897Seat Track · corrodedINSPECTION TYPE:C CABIN AT STA 1321 LBL 27.5 SEAT TRACK CROWN FOUND CORRODED. CABIN STA 1321 LBL 27.5 SEAT TRACK CROWN CORROSION REMOVED PER SRM 53-70-00 FIG 3 VOL I REV 37 MAT ORIG THK 0.145: & MAT REMOVED 0.035 FOUND EXCEED LIMIT PER SRM 53-70-00 FIG 3 VOL Oct 17, 2005 · N281UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS05M45895Seat Track · corrodedINSPECTION TYPE:C LT CURVED SEAT TRACK ST 1964 LBL 107.25 EXFOLIATION CORROSION. LT CURVED S/TRACK STA1964 LBL107.25 EXFOLIATION CORROSION REMOVED PER SRM53-70 -00 FIG3 VOL I REV 37 MAT ORIG THK 0.145" AND MAT REMOVED 0.070" FOUND EXCEED LIMIT PER SRM 53-70-0Oct 13, 2005 · N281UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS05M45894Seat Track · corrodedINSPECTION TYPE:C RT CURVED SEAT TRACK STN 1964, RBL 107.25 EXFOLIATION CORROSION, RT CURVED S/TRACK ST1964 RBL 107.25 EXFOLIATION CORROSION REMOVED PER SRM 53-7 0-00 FIG 3 VOL I REV37 MAT ORIG THK 0.145" AND MAT REMOVED 0.075" FOUND EXCEED LIMIT, NEW S/TRACK Oct 13, 2005 · N281UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
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