N274UP

Service difficulty reports · 350

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 = 'N274UP' 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 IPXA2017091421703Seat Track · corrodedINSPECTION TYPE: 3C, MAIN CABIN SEAT TRACK IS CORRODED BETWEEN BS 481 - 490, RBL 47.50. REPAIRED THE SEAT TRACK IAW EA 011-5310-01-A6958, REV I/R, AND EO MD11-5310-65497-A.Aug 21, 2017 · N274UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2017091421725Skin · gougedINSPECTION TYPE: 3C, EXTERIOR FUSELAGE SKIN IS GOUGED AT BS 1153, LONGERON 44L. REPAIRED THE SKIN IAW EA 011-5330-01-A6984, REV I/R, AND EO MD11-5330-65670-A. MAJOR.Aug 21, 2017 · N274UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2017091421724Skin · gougedINSPECTION TYPE: 3C, EXTERIOR FUSELAGE SKIN GOUGED, RT SIDE BS 1153, LONGERON 44R. REPAIRED IAW EA 011-5330-01-A6975, REV IR, AND EO MD11-5330-65671-A. MAJOR.Aug 21, 2017 · N274UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2017091421718Fire Seal · damagedINSPECTION TYPE: 3C, THE NR 1 ENGINE PYLON PANEL 438AL HAS A TORN FIRE SEAL. REPAIRED THE PYLON PANEL FIRE SEAL IAW EA 011-5430-01-A6950, REV I/R, AND EO MD11-5420-65606-A.Aug 21, 2017 · N274UP · Doug MD11F · Nacelle/Pylon, Plate/SkinSDR IPXA2017090821475Seat Track · corrodedINSPECTION TYPE: 3C, RCB AREA SEAT TRACK CORRODED ALONG RBL 27.5 BETWEEN BS 478 - 490. THE SEAT TRACK WAS REPAIRED IAW EA 011-5310-01-A6960, REV IR, AND EO MD11-5310-65583-A.Aug 21, 2017 · N274UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2017090821473Fairing · crackedINSPECTION TYPE: 3C, NR 3 PYLON LOWER AFT FAIRING ASSEMBLY INBOARD SIDE SKIN CRACKED. REPAIRED THE FAIRING SKIN IAW EA 011-5450-01-A6957, REV IR, AND EO MD11-5450-65522-A.Aug 21, 2017 · N274UP · Doug MD11F · Nacelle/Pylon, Main FrameSDR IPXA2017090821470Skin · corrodedINSPECTION TYPE: 3C, LEFT WING UPPER SKIN CORRODED ALONG STRINGER 8L BETWEEN XORS 820 - 823. REPAIRED IAW EA 011-5730-01-A6968, REV IR, AND EO MD11-5730-65578-A.Aug 21, 2017 · N274UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2017090721440Filler · chafedINSPECTION TYPE: 3C, TAILCONE RT INTERNAL DOUBLER SKIN FILLER CHAFED AT BS 2165, Z=61.5. REMOVED, FABRICATED, AND REPLACED THE TAILCONE DOUBLER SKIN FILLER IAW EO MD11-5330-59647-A.Aug 21, 2017 · N274UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2017090721445Seat Track · corrodedINSPECTION TYPE: 3C, SEAT TRACK CORRODED IN MAIN CABIN AT BS 485, LBL 27.5. REPAIRED THE SEAT TRACK BETWEEN BS 484.675 AND 489.675 IAW EA 011-5310-01-A6961, REV I/R, AND EO MD11-5310-65553-A.Aug 21, 2017 · N274UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2017090421292Stringer · crackedINSPECTION TYPE: 3C, LEFT WING STRINGER 12 IS CRACKED BETWEEN XORS 622 - 653. REPAIRED THE STRINGER IAW SRM 57-00-03, REPAIR 5, FIG. 202. MAJOR.Aug 21, 2017 · N274UP · Doug MD11F · Wing, Longeron/StringerSDR IPXA2017090121220Fitting · corrodedINSPECTION TYPE: 3C, RIGID CARGO BARRIER FLOOR FITTING NR 10 IS CORRODED. REMOVED AND REPLACED THE FLOOR FITTING IAW EO MD11-2520-58701-D.Aug 21, 2017 · N274UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2017090121219Fitting · corrodedINSPECTION TYPE: 3C, RIGID CARGO BARRIER FLOOR FITTING NR 8 IS CORRODED. REMOVED AND REPLACED THE FLOOR FITTING IAW EO MD11-2520-58701-D.Aug 21, 2017 · N274UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2017091421713Skin · corrodedINSPECTION TYPE: 3C, RT WING UPPER SKIN HAS CORROSION BETWEEN XORS 221 & 231, STRINGER 6R. REPAIRED THE WING SKIN IAW EA 011-5730-01-A6980, REV I/R, AND EO MD11-5730-65633-A.Aug 20, 2017 · N274UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2017091321685Doubler · crackedINSPECTION TYPE: 3C, LT WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN XOS 633.4 - 636.8. REPAIRED IAW EA 011-5730-01-A6959, REV I/R, AND EO MD11-5730-65648-A. MAJORAug 20, 2017 · N274UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2017091321674Spar Cap · corrodedINSPECTION TYPE: 3C, LEFT WING REAR SPAR UPPER CAP AFT FLANGE CORRODED XORS 964 - 978. REPAIRED IAW EA 011-5710-01-A6982, REV IR, AND EO MD11-5710-65659-A.Aug 20, 2017 · N274UP · Doug MD11F · Wing SparSDR IPXA2017091221632Skin · delaminatedINSPECTION TYPE: 3C, AREA ON OF DELAMINATION ON ON LOWER SURFACE OF RT OTBD AILERON. REPAIRED IAW SRM 57-60-80, REPAIR 1.Aug 20, 2017 · N274UP · Doug MD11F · AileronsSDR IPXA2017090821471Skin · corrodedINSPECTION TYPE: 3C, LEFT WING UPPER SKIN CORRODED ALONG THE REAR SPAR BETWEEN XORS 860 - 863. REPAIRED THE SKIN IAW EA 011-5730-01-A6967, REV IR, AND EO MD11-5730-65574-A.Aug 20, 2017 · N274UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2017090621421Frame · crackedINSPECTION TYPE: 3C, LT WING LE FRAME CRACKED AT XORS. 683. REMOVED, FABRICATED, AND REPLACED THE LT WING LE FRAME IAW DWG ARB3954, AND SRM 51-33-01.Aug 20, 2017 · N274UP · Doug MD11F · Wing SparSDR IPXA2017090521343Barrier · crackedINSPECTION TYPE: 3C, RIGID CARGO BARRIER LOWER CLOSEOUT IS CRACKED AT BS 488.1 & RBL 32. .REPAIRED THE CARGO BARRIER LOWER CLOSEOUT IAW SRM 53-20-53, REPAIR 1, FIGURE 201. MAJOR.Aug 19, 2017 · N274UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017091221626Skin · gougedINSPECTION TYPE: 3C, FUSELAGE SKIN AT BS 1781 - 1787, LONGERONS 39 - 42R GOUGED. REPAIRED THE SKIN IAW EA 011-5330-01-A6973, REV I/R, AND EO MD11-5330-65632-A.Aug 18, 2017 · N274UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2017090121240Former · crackedINSPECTION TYPE: 3C, RIGHT WING FIXED LEADING EDGE FORMER CRACKED, XOS 584. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT FORMER IAW DWG ARB2931 AND SRM 51-33-01.Aug 18, 2017 · N274UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2017090721442Trunnion · crackedINSPECTION TYPE: 3C, NOSE GEAR RT TRUNNION IS CRACKED AT BS 585.2, Z=-114, AND X= -24. REPAIRED THE TRUNNION IAW SRM 53-10-14, FIG 202, REPAIR 2. MAJOR.Aug 17, 2017 · N274UP · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR IPXA2017090121221Pan · crackedINSPECTION TYPE: 3C, NOSE GEAR AFT DOOR FRAME PAN IS CRACKED AT BS 586.5, RBL 22.5. REPAIRED THE DOOR FRAME PAN IAW EA 011-5310-01-A6956, REV I/R, AND EO MD11-5310-65475-A.Aug 17, 2017 · N274UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017082620971Stiffener · crackedINSPECTION TYPE: 3C, BULKHEAD WEB STIFFENER CRACKED IN THE LT MLG WW AT THE OTBD AFT CORNER. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-35-01.Aug 17, 2017 · N274UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017070418931Engine · fireDURING PUSH BACK, STARTING NR 3 ENGINE ON THE APU AFTER FUEL WAS SELECTED ON, THE ACFT LOST ELECTRICAL. MECHANIC REPORTED FLAMES 1 METER LONG COMING FROM THE TAIL. THE ENGINE WAS SHUTDOWN, THE FIRE HANDLE PULLED, AND ACFT TOWED BACK INTO BLOCKS. APU FAILEJul 4, 2017 · N274UP · Doug MD11F · Engine (Turbine/Turboprop)SDR IPXA2017030314642Latch · inoperativeFIRE EXTINGUISHER LATCH IN COURIER SECTION WILL NOT CLOSE. ADJUSTED THE QUICK-RELEASE STRAP AND INSTALLED THE FIRE EXTINGUISHER IAW AMM 26-24-01, PB 401, REV 88.Mar 2, 2017 · N274UP · Doug MD11F · Extinguishing SystemSDR IPXA2017011112615Solenoid · defectiveL1 DOOR MAKES LOUD KNOCKING NOISE WHEN OPENING DOOR. DEFERRED IAW MEL 52-10-1-2-0-1 DMP C/W PLACARD INSTALLED. R&R DOOR SOLENOID REF AMM 52-11-003. OPS CK GOOD.Jan 11, 2017 · N274UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2016111910809Floor Panel · damagedSUPERNUMERARY FLOOR PANEL DAMAGED. FABRICATE A NEW FLOOR PANEL IAW EO MD11-5320-61010-ANov 19, 2016 · N274UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2016101709503Controller · failedLEVEL 3 AIR MANIFOLD NR 2 FAILED. EMERGENCY DECLARED. RETARDED THROTTLE TO IDLE . ALERT WENT AWAY. OPERATED THE NR 2 ENGINE AT REDUCED THRUST. TROUBLESHOT IAW FIM 36-23-01. REMOVED AND REPLACED MANIFOLD FAIL DETECTOR CONTROLLER. OPS GOOD IAW AMM 36-23-01-0Oct 14, 2016 · N274UP · Doug MD11F · Pneumatic Distribution SystemSDR IPXA2016100308918Clamp · leakingMANIFOLD 2 FAILED WARNING RECEIVED IN FLIGHT. FOLLOWED AOM CHECKLIST, THE NR 2 ENGINE THRUST REDUCED TO EXTINGUISH WARNING. NOTE - THE NR 2 BLEED VALVE INDICATED OPEN THE ENTIRE TIME. EMERGENCY DECLARED. PERFORMED FIM 36-23-03, FOUND SEVERAL CLAMPS ON Oct 2, 2016 · N274UP · Doug MD11F · Engine (Turbine/Turboprop)SDR IPXA2016011497790Vane · delaminatedINSPECTION TYPE:2C, MULTIPLE AREAS OF DELAMINATION ON LOWER SURFACE OF LT INBD FLAP VANE REPAIRED DELAMINATED IAW SRM 57-50-80, REPAIR 2, FIG 201.Jan 14, 2016 · N274UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2016011497789Vane · delaminatedINSPECTION TYPE:2C, LT INBD FLAP VANE DELAMINATED AREA LOWER SURFACE INBD END REPAIRED DELAMINATED IAW SRM 57-50-80, REPAIR 2, FIG 201.Jan 14, 2016 · N274UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2016012998615Spar Cap · damagedINSPECTION TYPE:2CL, HORIZONTAL STABILIZER REAR SPAR LOWER CAP ELONGATED FASTENER HOLE REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SPAR CAP SECTION IAW DWG ALC8561, SRM 51-31-01, 51-35-01, 55-00-00.Jan 13, 2016 · N274UP · Doug MD11F · Horizontal Stabilizer, Spar/RibSDR IPXA2016012998614Skin · damagedINSPECTION TYPE: 2C, FWD TAILCONE SKIN ALONG RT SIDE CHAFE DAMAGE. REPAIRED FWD TAILCONE RT SKIN IAW EA 011-5330-01-A6049, REV IR AND EO MD11-5330-59647-A.Jan 9, 2016 · N274UP · Doug MD11F · Aerodynamic FairingsSDR IPXA2016012698481Skin · dentedINSPECTION TYPE:2C, AFT RT FUSELAGE SKIN HAS DENT WITH CREASE BS 2122 BETWEEN L7R AND L8R ACCOMPLISHED PERMANENT REPAIR ON AFT FUSELAGE SKIN AT BS 2122 BETWEEN L7R AND L8R IAW 011-5370-01-A6050, REV I/R AND EO MD11-5330-59608-A.Jan 5, 2016 · N274UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2016012698485Skin · chafedINSPECTION TYPE:2C, NR 2 RT T/R CORE COWL AFT UPPER SKIN CHAFE DAMAGE. REPAIRED CHAFE DAMAGE IAW EO MD11-7830- 59559-A AND EA 011-7830-01-A6047, REV IR.Jan 5, 2016 · N274UP · Doug MD11F · Engine Thrust ReverserSDR IPXA2016012498296Former · crackedINSPECTION TYPE:2C, LEFT WING L/E FORMER CRACKED AT XORS 917 REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FORMER IAW DWG ARB2920, SRM 51-31-01, 51-33-01.Jan 5, 2016 · N274UP · Doug MD11F · Wing SparSDR IPXA2016012598425Skin · crackedINSPECTION TYPE:2C, LEFT WING FIXED L/E EXTERIOR SKIN CRACKED AT CUTOUT FOR OTBD TRACK AT NR 4 SLAT. REPAIRED LT WING L/E SKIN IAW SRM 57-40-02, REPAIR 7, FIG 201.Jan 5, 2016 · N274UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2016012898570Panel · damagedINSPECTION TYPE:2C, NR 3 PYLON PANEL 487CR DAMAGED AROUND ATTACH FASTENER HOLES. REPAIRED PANEL IAW EA 011-5430-01-A6052, REV IR AND EO MD11-5430-59679-A.Jan 4, 2016 · N274UP · Doug MD11F · Nacelle/Pylon, Plate/SkinSDR IPXA2016012598426Hinge · chafedINSPECTION TYPE: 2C, RIGHT WING OTBD FLAP, OTBD HINGE HAS CHAFE DAMAGE ACCOMPLISHED PERMANENT BLEND REPAIR ON RT WING OTBD FLAP, OTBD HINGE BS XW 638.3, YW 595.6 AND ZW 5.6 IAW EA 011-5740-01-A6053, REV I/R AND EO 5710-59671-A.Jan 4, 2016 · N274UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2016022599912Vane · delaminatedINSPECTION TYPE:2C, RT OTBD FLAP VANE INBD LOWER SURFACE HAS AN AREA OF DELAMINATION AS MARKED, OTBD LOWER SURFACE ALSO DELAMINATED, DOCUMENTED ON VT-SAA NRC 307434. REMOVED RT OTBD FLAP VANE, INBD LOWER SURFACE AND SENT TO OUTSIDE VENDOR FOR REPAIR. INSTALLJan 3, 2016 · N274UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2016022599917Vane · delaminatedINSPECTION TYPE: 2C, RT OTBD FLAP VANE, OTBD LOWER SURFACE HAS AN AREA OF DELAMINATION AS MARKED, OTBD LOWER SURFACE ALSO DELAMINATED DOCUMENTED ON VT-SAA NRC 307433. REMOVED RT OTBD FLAP VANE, OTBD LOWER SURFACE, AND SENT TO OUTSIDE VENDOR FOR REPAIR. INSTAJan 3, 2016 · N274UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2016012798500Spar Cap · corrodedINSPECTION TYPE:2C, RT WING REAR SPAR UPPER CAP AFT FLANGE HAS CORROSION BETWEEN BS XORS 786 AND XORS 826 ACCOMPLISHED PERMANENT REPAIR ON RT WING REAR SPAR UPPER CAP AFT FLANGE AT BS XORS 786 TO XORS 826 IAW EA 011-5710-01-A6045, REV AND EO MD11-5710-59530A.Jan 3, 2016 · N274UP · Doug MD11F · Wing SparSDR IPXA2016012498293Skin · crackedINSPECTION TYPE:2C, LT WING L/E DROP SLAT UPPER SKIN CRACKED. REPAIRED LT DROOP L/E IAW SRM 57-40-01, REPAIR 5, FIG 201.Jan 3, 2016 · N274UP · Doug MD11F · Leading Edge DevicesSDR IPXA2015122897175Switch · inoperativeL1 DOOR ESCAPE SLIDE INDICATOR LIGHT INOPERATIVE. ACFT OK TO CONTINUE. R & R PUSH TO TEST SWITCH AND BOTH BATTERIES IAW MM 25-61-04-401. OPS TEST IS NORMAL IAW MM 25-61-04-710-801.Dec 24, 2015 · N274UP · Doug MD11F · Escape SlideSDR IPXA2015111295711Sign · detachedPOST FLIGHT WHEN GROUND CREW OPENED CABIN DOOR THE EMERGENCY EXIT SIGN FELL OFF. RE-INSTALLED EMERGENCY EXIT SIGN.Nov 11, 2015 · N274UP · Doug MD11F · Emergency LightingSDR IPXA5M85246Light · detachedLEFT EMERGENCY DOOR LIGHT HAS FALLEN OFF. R & R L1 DOOR EXIT SIGN IAW AMM 33-27-05.Jan 8, 2015 · N274UP · Doug MD11F · Emergency LightingSDR IPXA2014100884537Skin · gougedINSPECTION TYPE:1C, GOUGE DAMAGE ON FUSELAGE SKIN AFT EDGE AT CTR CARGO DOOR CUT-OUT, STA 1781, L40R-L42R. REPAIRED NOTED DAMAGE AT CTR CARGO DOOR CUT-OUT EDGE IAW SRM 53-00-05, REPAIR 8, FIG 202.Sep 28, 2014 · N274UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2014100684525Doubler · crackedINSPECTION TYPE:1C, RT WING L/E BEADED DOUBLER CRACKED AT STA XOS 655. ACCOMPLISHED PERMANENT REPAIR ON RT WING L/E BEADED DOUBLER STA XOS 653 TO XOS 657 IAW SRM 57-40-02 REPAIR 15, FIG 203.Sep 22, 2014 · N274UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2014100684524Doubler · crackedINSPECTION TYPE:1C, RT WING L/E BEADED DOUBLER CRACKED AT STA XOS 792, ACCOMPLISHED PERMANENT REPAIR ON RT WING L/E BEADED DOUBLER STA XOS 789 TO XOS 795 IAW SRM 57-40-02 REPAIR 15, FIG 203.Sep 22, 2014 · N274UP · Doug MD11F · Wing Main, Frame Structure
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