N150UP

Service difficulty reports · 241

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 = 'N150UP' 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 IPXA13177568Floor Panel · delaminatedINSPECTION TYPE:10YR, BULK CARGO FLOOR PANEL 161GF DELAMINATED. FABRICATED FLOOR PANEL IAW EO A300-5320-16407-E, APPENDIX D.Mar 12, 2013 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA3177683Floor Panel · puncturedINSPECTION TYPE:10YR FWD CARGO FLOOR PANEL 132AH PUNCTURED AND CRACKED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-D, PARA 6A.Mar 11, 2013 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA3177682Floor Panel · puncturedINSPECTION TYPE:10YR, FWD CARGO FLOOR PANEL 131SG PUNCTURED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-D, PARA 6 A.Mar 11, 2013 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA3177681Floor Panel · puncturedINSPECTION TYPE:10YR, FWD CARGO FLOOR PANEL 132PG PUNCTURED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-D, PARA 6A.Mar 11, 2013 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA3177680Floor Panel · puncturedINSPECTION TYPE:10YR, FWD CARGO FLOOR PANEL 131RG PUNCTURED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-D, PARA 6A.Mar 11, 2013 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA13177566Floor Panel · puncturedINSPECTION TYPE:10YR, FWD CARGO FLOOR PANEL 131BH PUNCTURED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-D, PARA 6A.Mar 11, 2013 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA13177565Floor Panel · puncturedINSPECTION TYPE:10YR, FWD CARGO FLOOR PANEL 131GE PUNCTURED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-D, PARA 6A.Mar 11, 2013 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA13177564Floor Panel · puncturedINSPECTION TYPE:10YR, FWD CARGO FLOOR PANEL 132MG PUNCTURED. REPAIRED FLOOR PANEL PER EO A300-5320-42721-D, PARA 6A.Mar 11, 2013 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA13177563Floor Panel · puncturedINSPECTION TYPE:10YR, FWD CARGO FLOOR PANEL 131MG PUNCTURED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-D, PARA 6A.Mar 11, 2013 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA13177540Floor Panel · puncturedINSPECTION TYPE:10YR, FWD CARGO FLOOR PANEL 132QG PUNCTURED. FABRICATED FLOOR PANEL IAW EO A300-5320-16407-E.Mar 11, 2013 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA13177539Floor Panel · puncturedINSPECTION TYPE:10YR FWD CARGO FLOOR PANEL 132SG PUNCTURED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-D.Mar 11, 2013 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA13177538Floor Panel · puncturedINSPECTION TYPE:10YR FWD CARGO FLOOR PANEL 131DE PUNCTURED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-D.Mar 11, 2013 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA13177537Floor Panel · puncturedINSPECTION TYPE:10YR, FWD CARGO FLOOR PANEL 132FE IS PUNCTURED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-D.Mar 11, 2013 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA13177536Floor Panel · puncturedINSPECTION TYPE:10YR, FWD CARGO BAY FLOOR PANEL 131FE PUNCTURED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-D.Mar 11, 2013 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA13177535Floor Panel · puncturedINSPECTION TYPE:10YR, FWD CARGO BAY FLOOR PANEL 132RG LOWER SKIN HAS FOUR PUNCTURES AND ONE AREA DELAMINATED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-D.Mar 11, 2013 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA12174790Floorboard · chippedINSPECTION TYPE: 4C, MAIN CABIN FLOORBOARD 221VF IS CHIPPED ON ITS SIDE. FABRICATED MAIN CABIN FLOORBOARD IAW EO APPENDIX B.Aug 6, 2012 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA12174809Seat Track · corrodedINSPECTION TYPE: 4C, SEAT TRACK CORRODED AT FR79, Y1131.1. REPAIRED SEAT TRACK AT FR79, Y1131.1 IAW SRM 53-10-16, FIG 201, PARA 4, REV 21. REF: RCD, CONTROL NR 554793.Aug 1, 2012 · N150UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA12174802Seat Track · corrodedINSPECTION TYPE: 4C, MAIN CABIN SEAT TRACK AT FR 79, STA Y794.3 CORRODED ACCOMPLISHED REPAIR ON MAIN CABIN SEAT TRACK AT FR 79, STA Y794 IAW SRM 53-10-16, PB 201, FIG 201.Aug 1, 2012 · N150UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA12174803Seat Track · corrodedINSPECTION TYPE:4C, MAIN CABIN FLOOR SEAT TRACK AT FR 79, STA Y0 IS CORRODED. ACCOMPLISHED REPAIR ON MAIN CABIN SEAT TRACK AT FR 79, STA Y0 IAW SRM 53-10-16, FIG 201.Jul 28, 2012 · N150UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA12174791Skin · chafedINSPECTION TYPE: 4C, LT INBD FLAP UPPER SKIN IS CHAFED AT OTBD SIDE. ACCOMPLISHED REPAIR ON LT INBD FLAP UPPER SKIN IAW SRM 57-50-00, FIG 205, PARA 4E.Jul 28, 2012 · N150UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA11165175Wire Harness · burnedWHEN CROSSING 18,000 TURNED LANDING LIGHT OFF BUT ECAM SHOWS LIGHT EXTENDED. LANDING LIGHT SUPPLY AND CTL BREAKERS POPPED AND WILL NOT RESET. FOUND WIRES JUST OTBD OF 1937VC THRU FUSELAGE FEED THRU BURNED & BROKEN. RETERMINATED ALL WIRES AT CONNECTOR 1937VC Mar 5, 2011 · N150UP · Airbus A300F4622R · Light System WiringSDR IPXA1165076Slide · low pressureESCAPE SLIDE PRESSURE NOT IN GREEN BAND, DEF M448056, INSTALLED MAIN CABIN DOOR ESCAPE SLIDE IAW MM 25-61-21. DOOR OPS CHECKS NORMAL. M448056 CLEARED.Feb 27, 2011 · N150UP · Airbus A300F4622R · Escape SlideSDR IPXA10162872Control Unit · inoperativeON 25 MILE BASE TO FINAL AT SJC 6000 FT, WITH AUTOPILOT ON, FROM WINGS LEVEL ACFT ROLLED ABRUPTLY 20 DEGREES TO THE RT THEN THROUGH NEUTRAL TO APPROX 20 DEGREES TO THE LT. TURNED OFF A/P SPOILER 7 SWITCH AND 3 AND 2 SWITCH BOTH SHOWED FAULT. TOWER DECLARED EMESep 29, 2010 · N150UP · Airbus A300F4622R · Drag Control SystemSDR IPXA10159942Oil Cooler · inoperativeAPU AUTO SHUTDOWN RESULTING IN SINGLE GENERATOR OPERATION. DECLARED EMERGENCY AND DIVERTED, APU OIL QUANTITY INDICATES 'MIN'. INDICATED OVER 3/4 IN AUS. ATTEMPTED RESTART BUT APU AUTO SHUTDOWN EACH ATTEMPT. R & R OIL COOLER AND FAN IAW MM 49-91-15-04 AND 49May 20, 2010 · N150UP · Airbus A300F4622R · APU Oil SystemSDR IPXA10158639Floor Panel · misrepairedINSPECTION TYPE:3C, PANEL 252SJ REQUIRES REPLACEMENT IAW EO A300-5100-30624C DUE TO REPAIRS DONE TO FLOORBOARD IAW SRM. FABRICATED FLOOR PANEL 252SJ IAW EO A300-5320-16407-D APPENDIX B.Feb 16, 2010 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158642Floorboard · misrepairedINSPECTION TYPE:3C, PANEL NR 161LF REQUIRES REPLACEMENT IAW EO A300-5100-30624-C DUE TO REPAIRS DONE TO FLOORBOARD IAW AMM. FABRICATED FLOORBOARD NR161LF IAW EO A300-5320-16407-D APPENDIX D.Feb 15, 2010 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158641Floorboard · misrepairedINSPECTION TYPE:3C, PANEL NR 161MF REQUIRES REPLACEMENT IAW EO A300-5100-30624-C DUE TO REPAIRS DONE TO FLOORBOARD IAW AMM. FABRICATED FLOORBOARD NR 161MF IAW EO A300-5320-16407-D APPENDIX D.Feb 15, 2010 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158640Floorboard · damagedINSPECTION TYPE:3C, PANEL 262RF REQUIRES REPLACEMENT IAW EO A300-5100-30624-C DUE TO REPAIRS DONE TO FLOORBOARD IAW AMM. FABRICATED FLOORBOARD 262RF IAW EO A300-5320-16407-D APPENDIX B.Feb 15, 2010 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158591Skin · gougedINSP TYPE:3/C LT WING CTR FLAP UPPER SKIN GOUGED 12IN. FWD OF RUB STRIP ABOVE NR 4 FLAP TRACK. REPAIRED IAW SRM 57-50-00 FIG. 205, PARA 4E.Feb 12, 2010 · N150UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA10158176Floor Panel · damagedAFT BULK PIT FLOOR PANEL DAMAGED. REPRAIRED IAW EO A300-5320-16407-D.Jan 17, 2010 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA09156357Lens · missingINSPECTION TYPE:N/A WALL MOUNTED EMERGENCY LIGHT MISSING LENS. REMOVED AND REPLACED WALL MOUNTED EMERGENCY LIGHT ASSY PER MM 33-51-17-04. OPS CHECKS OK.Jun 13, 2009 · N150UP · Airbus A300F4622R · Emergency LightingSDR UPS08153928Skin · damagedINSPECTION TYPE:N/A SKIN PLATE DAMAGED BETWEEN FR 78 AND 79 STR 44L AND 45L. REPAIRED IAW EO A300-5330-31201.Nov 16, 2008 · N150UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR UPS08152169Lock · brokenAT LEVEL OFF, CREW HEARD A MUFFLED BOOM AND SLIGHT SHAKE OF THE A/C. UPON DESCENT, CREW REPORTED A LOAD SHIFT. MX INSPECTED LOCKS AND SEAT TRACK. ONE BROKEN LOCK WAS DEFERRED. NO SEAT TRACK DAMAGE. CREW DECLARED AN EMERGENCY. UPON ENTERING CARGO AREA NOTMay 6, 2008 · N150UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR UPS08151997Skin · dentedINSPECTION TYPE:5YR RIGHT I/B FLAP LOWER SKIN I/B OF NR 2 FLAP TRACK DENT. MEASURED DENT AND FOUND OUT OF LIMITS IAW A300 SRM 57-50-00 FIG 101. CUT OUT DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SAA EA 300-5730-01-A1334.Mar 24, 2008 · N150UP · Airbus A300F4622R · Trailing Edge FlapsSDR UPS07151262A/C Pack · smokeINSPECTION TYPE:N/A DURING LOADING, LOADING CREW REPORTED SMOKEY HAZE IN THE CARGO AREA NO SMOKE DETECTION WAS SENSED BY SYSTEM. THERE WAS AN ODOR PRESENT FROM THE PACKS. TEMPS AT MIX VALVES WERE NORMAL EXCEPT MID 138. A/C HAD 380 (PLUS) LBS OF DRY ICE ON BDec 7, 2007 · N150UP · Airbus A300F4622R · Air Distribution SystemSDR UPS07149824A/C Pack · odorDURING ADVANCE OF THRUST FOR TAKEOFF, A STRONG BURNING ODOR ENTERED THE AIR SYSTEM. THE ODOR WAS PERSISTENT UNTIL THRUST REDUCTION. UPON DESCENT AND LANDING THE SMELL CAME BACK STRONGER. PERFORMED ENGINE RUN AND OPERATED BOTH PACKS. NO DEFECTS NOTED.May 16, 2007 · N150UP · Airbus A300F4622R · Cabin Cooling SystemSDR UPS06147833Compressor · stalledINSPECTION TYPE: N/A AIR DIVERT, INITIAL DESCENT COMPRESSOR STALL WITH NO SECONDARIES. ON SUBSEQUENT DESCENTS NUMEROUS COMPRESSOR STALLS ON NR 1 ENGINE. NO FLUCTUATIONS ON ANY OF THE ENGINE INSTRUMENTS. PERFORMED ENGINE STALL PROCEDURES. DECLARED EMERGENCY BECAug 29, 2006 · N150UP · Airbus A300F4622R · Turbine Engine Compressor SectionSDR UPS06146535Bottle · leakingCANNOT SEE SLIDE PRESSURE GAUGE ON MAIN CARGO DOOR. CHECKED DRAIN LINE FOR LEAKAGE; NO LEAKAGE FOUND AFTER 15 MINS. BEFORE LEAKAGE QUIT IT WAS 4 DROPS PER MIN WITHIN LIMITS IN ACCORDANCE TO M/M 71-00-00-2 PAR 3.Mar 21, 2006 · N150UP · Airbus A300F4622R · Escape SlideSDR UPS06146424Flex Drive · failedNR 1 ENG T/R FAILED ON EXTENSION, IT THEN TORE ITSELF UP ON RETRACTION AND IS STUCK. UPPER FLEX SHAFT CABLE DAMAGED ON INBOARD SIDE NR 1 REVERSER. C/W T/R REMVL TO SECT 3B PG 4.C.T.91454 C/W MM 71-13-03-4 TO PG 7 PARA C ITEM (20) C/W MM 71-13-03-4 PG 7 PARA Mar 9, 2006 · N150UP · Airbus A300F4622R · Engine Thrust ReverserSDR UPS06146046Slide · will not armESCAPE SLIDE ON CABIN DOOR WILL NOT MOVE TO THE ARMED POSITION. REMOVED AND REINSTALLED GIRT BAR IAW MM 25-61-21-4. SLIDE ARM AND DISARM OPERATION GOOD. THIS CLEARS M318706.Jan 24, 2006 · N150UP · Airbus A300F4622R · Escape SlideSDR UPS04141963Brake · inoperativeTAXIING TO PARK, NORMAL BRAKING FAILED. SWITCHED TO ALT BRAKE, BRAKE CAME ACTIVE RIGHT AWAY. TAXI WAY WAS COVERED WITH ICE. NORMAL BRAKE SYSTEM CHECK IAW MM 32-43-00-5 SATISFACTORY.Feb 26, 2004 · N150UP · Airbus A300F4622R · Landing Gear Brake System
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