N174UP

Service difficulty reports · 182

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 = 'N174UP' 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 IPXA2021031366762Angle · crackedINSPECTION TYPE:CRH WING L/E KRUGER FLAP WELL WEB SUPPORT STRUCTURE CRACKEDREMOVED AND REPLACED ANGLE IAW SRM 51-40-21Feb 24, 2021 · N174UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2021031466787Landing · crackedINSPECTION TYPE:CENGINE #2 OUTBD T/R COWL FWD SUPPORT STRUCTURE FOR FAN COWL SUPPORT BRACKET 2EA CRACKED LOC 3'OCLOCK POSREPAIRED DOOR LANDING IAW PW SRM 54-05-02Feb 24, 2021 · N174UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2021031166736Flange · damagedINSPECTION TYPE:CFAIRING 485AL I/B 2ND ATTACH FLANGE HAS 11 ELONGATED HOLES AND CHAFFED AREAS ON I/B SURFACEREMOVED AND REPLACED UPPER LONGERON IAW AMM 51-40-21Feb 24, 2021 · N174UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous StructureSDR IPXA2021031166734Flange · damagedINSPECTION TYPE:CFAIRING 475AL OB ST ATTACH FLANGE AND REPAIR STRIP HAVE 4 ELONGATED HOLES AND CHAFFED AREAS ON IB SURFACEREMOVED AND REPLACED IAW SRM 51-40-21Feb 24, 2021 · N174UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous StructureSDR IPXA2021031066661Attach Fitting · chafedINSPECTION TYPE:CFAIRING 485AL OB 2ND ATTACH FLANGE HAS 6 ELONGATED HOLES AND CHAFFED AREAS ON IB SURFACEREMOVED AND REPLACED UPPER ONGERON IAW SR 51-40-21Feb 24, 2021 · N174UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2021030666479Support · damagedINSPECTION TYPE:CAFT CARGO COMPARTMENT - CEILING SUPPORT STRUCTURE AT FRAME #54.2 HAS AREAS OF CORROSION AND DISBONDED SEALANT BETWEEN FLOOR BEAM AND FILLER STRIPREMOVED AND REPLACED IAW SRM 51-40-21Feb 23, 2021 · N174UP · Airbus A300F4622R · Passenger Compartment WindowsSDR IPXA2021030666477Support · damagedINSPECTION TYPE:C AFT CARGO COMPARTMENT - CEILING SUPPORT STRUCTURE AT FRAME #54.2 HAS AREAS OF CORROSION AND DISBONDED SEALANT BETWEEN FLOOR BEAM AND FILLER STRIPREMOVED AND REPLACED IAW SRM 51-40-21Feb 23, 2021 · N174UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2021030666478Support · damagedINSPECTION TYPE:CAFT CARGO COMPARTMENT - CEILING SUPPORT STRUCTURE AT FRAME #54.2 HAS AREAS OF CORROSION AND DISBONDED SEALANT BETWEEN FLOOR BEAM AND FILLER STRIPREMOVED AND REPLACED IAW SRM 51-40-21Feb 23, 2021 · N174UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2021030566462Doubler · damagedINSPECTION TYPE:A300NO. 1 PYLON LH SIDE FIXED FAIRING REPAIR DOUBLER ABOVE THE EXHAUST NOZZIE IS CHAFFED WITH SHEARED RIVETREMOVED AND REPLACE DOUBLER IAW 54-56-10 FIG 201.Feb 22, 2021 · N174UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2021030566461Thrust Reverser · damagedINSPECTION TYPE:A300#1 OB TR AFT UPPER CORNER ABOVE THE EXHAUST NOZZLE IS CHAFFED AND DEFORMEDREPAIRED IAW PW SRM 54-30-00 REPAIR 43Feb 22, 2021 · N174UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2021031466785Landing · crackedINSPECTION TYPE:CENGINE #2 OUTBD T/R COWL FWD SUPPORT STRUCTURE FOR FAN COWL SUPPORT BRACKET 2EA CRACKED LOC 3'OCLOCK POSREPAIRED DOOR LANDING IAW PW SRM 54-05-02Jan 24, 2021 · N174UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2020072258074Selector Valve · malfunctionedCREW CONTACTED FLIGHT CONTROL DURING CLIMB, TO STATE THAT THEIR LANDING GEAR WOULD NOT RETRACT. DID NOT HAVE ENOUGH FUEL TO CONT TO DESTINATION WITH GEAR DOWN, THE FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR SLECTOR VALVES IAW AMM 32-31-Jul 21, 2020 · N174UP · Airbus A300F4622R · Landing Gear Retraction/Extension SystemSDR IPXA2020051355234Angle · crackedINSPECTION TYPE:SEGAFT CARGO ABOVE FWD PBH BELOW Y1599 HAS 1 (ANGLE) CRACKED.REMOVED AND REPLACED ANGLE IAW SRM 51-40-21May 12, 2020 · N174UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2020041054076Slide · deployedINSPECTION TYPE:N/A** SUPPLEMENTAL SDR ** CREW ENTRY DOOR SLIDE DEPLOYED INADVERTANTLY. DEFERRED L1 DOOR EMERGENCY SLIDE I.A.W. MEL 52-11-01-5. DMP 52-11-01-5 IS ACCOMPLISHED. (PARTS IN PFM) M704207 ASSIGNED PLACARD INSTALLED.INSTALLED EMERGENCY EVAC SLIDE PERApr 9, 2020 · N174UP · Airbus A300F4622R · Escape SlideSDR IPXA2019103148520Control Unit · inoperativeINSPECTION TYPE:N/A** DIVERSION ** GEAR WOULD NOT RETRACT AFTER TAKEOFF. COMPLIED WITH QRH. UNABLE TO RETRACT WITH THE OTHER SYSTEM. HANDLE WOULD NOT MOVE PAST THE NEUTRAL POSITION.PREPARED AIRCRAFT FOR JACKS AND GEAR SWING REF 07-11-00. FOUND FAULTY LANDING GOct 31, 2019 · N174UP · Airbus A300F4622R · Landing Gear Retraction/Extension SystemSDR IPXA2019051542146Coalescer Bag · odorINSPECTION TYPE:N/A SULFUR LIKE ODOR AT 130 INTO FLIGHT SWITCHED OFF PACK 1 AND THEN RAN SINGLE PACK ON PACK 2 ODOR THEN SUBSIDED ODOR STRONGEST IN SUPERIOR AREA NO ODOR IN CARGO COMPT OR AVIONICS BAY NO ECAM ADVISORIES OBSERVED. ENTERED TO DI LOG PER MEL 21-May 14, 2019 · N174UP · Airbus A300F4622R · Humidity Control SystemSDR IPXA2019041240972Pin · brokenDOOR SLIDE PIN BROKE OFF PRIOR TO ARMING SLIDE.REMOVED BROKEN DOOR SLIDE PIN, PLACED NEW PIN WITH FLIGHT CREW FOR DOOR SLIDE ARMING PROCEDURE AS REQ.Apr 12, 2019 · N174UP · Airbus A300F4622R · Escape SlideSDR IPXA2019021543909Arming Lever · inoperativeSLIDE ARMING HANDLE DOES NOT MOVE ALL THE WAY FORWARD.FOUND RAIN ABSORBANT MATERIAL IN FORWARD GIRT BAR FITTING. REMOVED MATERIAL. OPERATED ARMING HANDLE. CKS OK. REF AMM 52-10-00.Feb 14, 2019 · N174UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA2018081763884Skin · dentedEXTERIOR FUSELAGE SKIN, 12 INCHES FWD OF FRAME 10 HAD TWO DENTS, 6 AND 10 INCHES ABOVE THE LAP SEAM. REPAIRED THE AREA IAW EO A300-5330-69533-A, AND REO-G21522, REV IR.Aug 12, 2018 · N174UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA2018081543823Skin · gougedLEFT WING, OTBD FLAP LE SKIN WAS GOUGED ON A PREVIOUS REPAIR. REPAIRED IAW SRM 57-50-00, P.231, STEP H.Jul 31, 2018 · N174UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2018081543813Skin · gougedNR 1 SLAT TRAILING EDGE WEDGE, LOWER SKIN WAS GOUGED. REPAIRED IAW REO-G21524, REV IR, AND EO A300-5730-69562, REV A.Jul 31, 2018 · N174UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2018081533784Channel · crackedNR 1 ENGINE LEFT THRUST REVERSER PANEL CHANNEL, AT FWD BI-FURCATION LATCH WAS CRACKED. REMOVED AND REPLACED THE CHANNEL IAW SRM 54-04-01.Jul 31, 2018 · N174UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2017042616505Indicator · inoperativeRECEIVED A 40 DEGREE FLAP INDICATION MESSAGE. R & R THE SLAT/FLAP INDICATOR IAW AMM 27-55-11. OPS CHECKED GOOD. NO DEFECTS NOTEDApr 21, 2017 · N174UP · Airbus A300F4622R · Trailing Flap Position Indicating SystemSDR IPXA2017020813839Warning Light · false activationDURING CLIMBOUT THRU 10000 FT, THE LT CABIN DOOR NOT CLOSED ILLUMINATED, CABIN PSI APPRX. 4.0 FOLLOWED ECAM, NO ABNORMALS. CABIN PRESSURIZED NORMALLY. WARNING WENT AWAY THRU 10000 FT DURING DESENT. 5.0 PSI DIFF. PERFORMED OPS TEST IAW AMM 52-71-11. TEST OK AFeb 7, 2017 · N174UP · Airbus A300F4622R · Door Warning SystemSDR IPXA2016081607126Solenoid Valve · inoperativeAFTER TAKE OFF AND DURING NORMAL FLAP RETRACTION, RECEIVED AN ECAM MESSAGE FOR THE KRUEGER NOT RETRACTED. HAD AMBER KRUEGER LIGHT. BUFFETING FELT. REPLACED THE KRUEGER SELECTOR SOLENOID VALVE IAW MM 27-88-12-0401.Aug 13, 2016 · N174UP · Airbus A300F4622R · Leading Edge Slat Control SystemSDR IPXA2016070205323Connector · not seatedEMERGENCY LIGHTS WILL NOT TEST. RESET CONNECTOR ON EMERGENCY LIGHT CONTROLLER. OPS CK NORMAL AMM 33-51-00-0501.Jul 2, 2016 · N174UP · Airbus A300F4622R · Light System WiringSDR IPXA2016052203663Sidewall Panel · damagedINSPECTION TYPE: 1C2C, BULK PIT PANEL 161 MW HAS FASTENER HOLES THAT HAVE INNER HONEY CONE CRUSHED. REPAIRED DAMAGED AREAS IAW EO A300-5320-42721-F.May 19, 2016 · N174UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2016052203662Ceiling Panel · damagedINSPECTION TYPE: 1C2C, AFT PIT CEILING PANEL 152QC IS CRACKED ON UPPER SIDE. REPAIRED DAMAGED AREA IAW EO A300-5320-42721-F.May 19, 2016 · N174UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2016052303681Sidewall Panel · delaminatedINSPECTION TYPE:10YR, FOWARD CARGO SIDEWALL PANEL 131TW IS DELAMINATED ON BOTTOM EDGE. REPAIRED THE SIDEWALL PANEL IAW AMM 25-00-00-0801.May 16, 2016 · N174UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2016052303680Sidewall Panel · delaminatedINSPECTION TYPE: 10YR, FORWARD CARGO SIDEWALL PANEL 131RW IS DELAMINATED ON BOTTOM EDGE. REPAIRED THE SIDEWALL PANEL IAW AMM 25-00-00-0801.May 16, 2016 · N174UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2016051603467Bracket · crackedINSPECTION TYPE: 10Y, AFT CARGO BULKHEAD AT FRAME 54, LBL 77 ATTACH BRACKET CRACKED. REMOVED AND PLACED BRACKET IAW AIRBUS DWG A53410765200.May 16, 2016 · N174UP · Airbus A300F4622R · Fuselage Main, BulkheadSDR IPXA2016051703477Rib · corrodedINSPECTION TYPE:10Y, NR 1 PYLON, CENTER ATTACH LUG BUSHING IS PITTED R & R RIB 18 FITTING IAW AMM 54-51-75-0401.May 12, 2016 · N174UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/RibSDR IPXA2016051703475Support Angle · crackedINSPECTION TYPE:10YR, AFT PIT FWD BULKHEAD UPPER SUPPORT ANGLE CRACKED. R & R THE CRACKED SUPPORT ANGLE IAW UPS SRM 51-40-21.May 7, 2016 · N174UP · Airbus A300F4622R · Fuselage Main, BulkheadSDR IPXA2016051603463Bracket · crackedINSPECTION TYPE:10YR, AFT PIT FWD BULKHEAD UPPER PANEL SUPPORT ANGLE IS CRACKED. R & R THE CRACKED ANGLE IAW SRM 51-40-21.May 7, 2016 · N174UP · Airbus A300F4622R · Fuselage Main, BulkheadSDR IPXA2016051403328Bracket · crackedINSPECTION TYPE:10YR, AFT PIT BULKHEAD UPPER PANEL SUPPORT ANGLE CRACKED. R & R CRACKED SUPPORT ANGLE IAW SRM 51-40-21.May 7, 2016 · N174UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2016051303321Bracket · crackedINSPECTION TYPE: 5YR, AFT PIT FWD BULKHEAD UPPER PANEL SUPPORT BRACKET CRACKED. R & R IAW SRM 51-40-21.May 7, 2016 · N174UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2016051303314Floorboard · brokenINSPECTION TYPE:10YR, MAIN CARGO DECK FLOORBOARD AT MCD ENTRANCE 231LG IS BROKEN AT THE FWD END OF FLOORBOARD. REPAIRED MAIN CARGO PANEL 231LG IAW SREO A300-5320-42721-F.May 6, 2016 · N174UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2016052403779Skin · chafedINSPECTION TYPE:10YR, RT WING INBD FLAP IS CHAFING UPPER SURFACE OTBD EDGE REPAIR RT WING INBD FLAP IAW SRM 57-50-00 PARA 4E FIG 205.May 4, 2016 · N174UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2016051403326Intercostal · crackedINSPECTION TYPE: 5YR, INTERCOSTAL CRACKED AT FRAME 85-86, 35L. R & R INTERCOSTAL IAW SRM 51-40-21.May 4, 2016 · N174UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2016052403793Skin · gougedINSPECTION TYPE: 10YR, LOW OTBD FLAP L/E GOUGED ON INBD END REPAIRED L/E IAW SRM 57-50-00, FIG 208, SHT 2.May 3, 2016 · N174UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2016051903581Floorbeam · crackedINSPECTION TYPE:1C2C, MAIN CABIN FLOORBEAM AT LT FRAME 79 1580 IS CRACKED. REPAIRED IAW EO A300-8310-60663-A.May 1, 2016 · N174UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR IPXA2016051903573Floorbeam · crackedINSPECTION TYPE:1C2C, MAIN CABIN FLOORBEAM AT RT FR 79- 1580 IS CRACKED. REPAIRED IAW EO A300-5310-60663-A.May 1, 2016 · N174UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR IPXA2175305Floorboard · crackedINSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 231PH HAS LOWER SKIN CRACKED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.Sep 12, 2012 · N174UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175306Floorboard · puncturedINSPECTION TYPE:SV, MAIN CABIN FLOORBOARD 232HG HAS LOWER SKIN PUNCTURED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6ASep 11, 2012 · N174UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA12172994Skin · damagedFUSELAGE SKIN DAMAGED FWD OF FR 85 BETWEEN STRINGER 44L AND 45L (AT TAIL BALL). REPAIRED IAW EO A300-5330-46654-B.Apr 16, 2012 · N174UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA2171280Skin · dentedLEFT AILERON DENTED AND DELAMINATED. REPAIRED REF EO A300-5750-45620-B.Jan 30, 2012 · N174UP · Airbus A300F4622R · AileronsSDR IPXA11168132Floorboard · crackedINSPECTION TYPE:5YR, MAIN CABIN FLOORBOARD NR 252DF IS CRACKED ON LOWER SURFACE. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 252DF IAW EO A300-5320-42721-A PARA. 6A.Jul 22, 2011 · N174UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA11168167Floor Panel · crackedINSPECTION TYPE:5YR, FWD CARGO COMPT FLOOR PANEL 131AH IS CRACKED. FABRICATED FWD CARGO COMPT FLOOR PANEL 131AH IAW EO A300-5320-16407-E.Jul 20, 2011 · N174UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA1168102Floorboard · delaminatedINSPECTION TYPE:5YR, MAIN CABIN FLOORBOARD NR 231PJ IS DELAMINATED AT UPPER SURFACE. FABRICATED MAIN CABIN FLOORBOARD NR 231PJ IAW EO A300-5320-40552-A, APPENDIX B.Jul 15, 2011 · N174UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA1168030Floorboard · puncturedINSPECTION TYPE:5YR, MAIN CABIN FLOORBOARD NR 231LH HAS A HOLE ON LOWER SURFACE. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 231LH IAW EO A300-5320-42721-A PARA 6A.Jul 15, 2011 · N174UP · Airbus A300F4622R · Fuselage Floor Panel
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