N330UP

Service difficulty reports · 132

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 = 'N330UP' 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 IPXA11664484Warning Light · illuminatedDIVERSION - EICAS MSG FLAP/SLAT ELEC DISPLAYED AFTER TAKEOFF. T/S C/O IAW FIM 29-51-00, FIG 114, SH 1 BLOCK 1 & 21. NO FAULTS NOTED, SYS OK. FIM REV 48.Jan 27, 2011 · N330UP · Boeing 76734AF · Leading Edge Slat Control SystemSDR IPXA10661875Sign · damagedINSPECTION TYPE:PS1, EMERGENCY EXIT LIGHT ASSY TABS TO HOLD LIGHT COVER ON WORN. R & R EMERGENCY LIGHT ASSY IAW MM 33-51-01-2.Aug 14, 2010 · N330UP · Boeing 76734AF · Emergency LightingSDR IPXA10661192Frame · crackedINSPECTION TYPE:C, NR 1 PYLON INTERNAL LT SIDE BS 285.45 VERTICAL FRAME CRACK NR1 PYLON INTERNAL LT SIDE BS285.45 VERTICAL FRAME REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02.Jul 15, 2010 · N330UP · Boeing 76734AF · Nacelle/Pylon, Frame/Spar/RibSDR IPXA10661211Floor Panel · damagedINSPECTION TYPE:C, MCD STA 540 TO 654+22 LBL 33 TO LBL 55, FLOOR PANEL FOUND 1EA DAMAGED AND 4 DENTS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND REINSTALLED IAW AMM 53-01-01.Jul 14, 2010 · N330UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10661210Floor Panel · damagedINSPECTION TYPE:C, MCD STA540 TO 654+22 LBL 55 TO LBL 77 FLOOR PANEL FOUND 1 DAMAGED & 6 DENTS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND REINSTALLED IAW AMM 53-01-01.Jul 14, 2010 · N330UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10661209Floor Panel · damagedINSPECTION TYPE:C, MCD STA 540 TO 654+22, LBL 11 TO RBL 11 FLOOR PANEL FOUND 4 DAMAGED & 10 DENT FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & REINSTALLED IAW AMM 53-01-01.Jul 14, 2010 · N330UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10661208Floor Panel · crackedINSPECTION TYPE:C, MCD STA 930 TO 977, RBL11 TO RBL33, FLOOR PANEL FOUND CRACK FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND REINSTALLED IAW AMM 53-01-01.Jul 14, 2010 · N330UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA10661207Floor Panel · damagedINSPECTION TYPE:C, MCD STA 540 TO 654+22, LBL 11 TO LBL 33, FLOOR PANEL, FOUND 1 DAMAGED & 9 DENT. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND REINSTALLED IAW AMM 53-01-01.Jul 14, 2010 · N330UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10661193Fairing · delaminatedINSPECTION TYPE:C, LT WING INBD MAIN FLAP L/E FOUND DELAMINATION COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A (1) FIG 5.Jul 14, 2010 · N330UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10661261Skin · misrepairedINSPECTION TYPE:C, SURVEY SEQUENCE NR 330-F1-02 THE EXISTING REPAIR DOES NOT CORRLATE TO A SRM JUST AT BS 328 TO BS 345 BETWEEN S35R AND S37R SURVEY SEQ NR 330-F1-02, FX SKIN REPAIRED IAW R53-31-36782 & EO B767-5330-38845 JUST AT BS328 TO BS345 BTN STR35R Jul 13, 2010 · N330UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA10661260Skin · misrepairedINSPECTION TYPE:C, SURVEY SEQUENCE NR 330-F1-01 THE EXISTING REPAIR DOES NOT CORRELATE TO A SRM JUST AT BS 143 TO BS 164 BETWEEN S21R AND S27R SURVEY SEQ 330-F1-01 FX SKIN REPAIRED IAW R53-11-36792 & EO B767-5330-38856 JUST AT BS143 TO BS164 BTN STR21R & SJul 13, 2010 · N330UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA10661194Wedge · chafedINSPECTION TYPE:C, RT WING NR 7 SLAT T/E WEDGE FOUND CHAFED. METAL HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-10-2R, REPAIR 4, FIG 202, SHEET 8.Jul 13, 2010 · N330UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10661172Stiffener · crackedINSPECTION TYPE:C, MEC COMPT STA 246 FLOORBEAM ATT STIFFENER FOUND CRACK AT LBL40" MEC COMPT BS 246 LBL40" FLOORBEAM ATT STIFFENER REPAIRED IAW SRM 53-10-51-2R4, FIG 201, ORG MATL IS BAC1490-2793-7075T62, CRK LENGTH IS 1", THIS REPAIR IS CLASSIFIED AS A MAJOJul 13, 2010 · N330UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA10661190Skin · crackedINSPECTION TYPE:C, DMI D423950 - E/E BAY ACCESS DOOR CRACK - INTERIM REPAIR E/E BAY ACCESS DOOR PREVIOUS CRACK AREA BLENDED DEPTH 0.20" AND LENGTH IS 1" IS ACCEPTACBLE IAW HX RS R52-00-36779 AND EO B767-5240-38816.Jul 12, 2010 · N330UP · Boeing 76734AF · Electrical/Electronic Compartment DoorsSDR UPS08653450Bracket · crackedINSPECTION TYPE:N/A RT WING NR 7 SLAT 3EA BRACKET NR 10, 11, 12 FOUND CRACK. CRACK LENGTH .5 INCH APPROX. RT WING NR 7 SLAT 3EA BRACKET NR 10, 11, 12 REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Sep 29, 2008 · N330UP · Boeing 76734AF · Leading Edge DevicesSDR UPS08653429Web · crackedINSPECTION TYPE:C RT WING FRONT SPAR AREA LES 680 D-NOSE WEB FOUND CRACK (CRACK LENGTH .5 INCH). D-NOSE WEB REPAIRED AS PER SRM 57-41-13-2R3 FIG 201 REPAIR 3.Sep 29, 2008 · N330UP · Boeing 76734AF · Wing Miscellaneous StructureSDR UPS08653449Bracket · crackedINSPECTION TYPE:N/A LT WING NR 6 SLAT INNER LOWER NR 5 AND NR 8 BRACKET FOUND CRACK 2EA CRACK LENGTH .5 INCH APPROX. TWO BRACKETS REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Sep 27, 2008 · N330UP · Boeing 76734AF · Leading Edge DevicesSDR UPS08653455Support Bracket · crackedINSPECTION TYPE:N/A EMP - JACKSCREW COMPARTMENT RT STA 1767.25 (STR 22) SUPPORT BRACKET FOUND CRACK. CRACK LENGTH .5 INCH APPROX. SUPPORT BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Sep 26, 2008 · N330UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS08653453Stiffener · crackedINSPECTION TYPE:N/A CABIN STA 240 LBL 25 FLOORBEAM ATT STIFFENER CRACKED. CRACK LENGTH 1 INCH. DEFECTIVE STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Sep 26, 2008 · N330UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR UPS08653452Stiffener · crackedINSPECTION TYPE:N/A CABIN STA 246 RBL 10 FLOORBEAM ATT STIFFENER CRACKED. CRACK LENGTH 1 INCH. DEFECTIVE STIFFENER REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02.Sep 26, 2008 · N330UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR UPS08653451Stiffener · crackedINSPECTION TYPE:N/A CABIN STA 246 LBL 50 FLOORBEAM ATT STIFFENER CRACKED. CRACK LENGTH 1 INCH. DEFECTIVE STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Sep 26, 2008 · N330UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR UPS08653448Hinge Fitting · crackedINSPECTION TYPE:N/A LT WING I/B MAIN FLAP AFT FLAP I/B SUPPORT FITTING FOUND CRACK. CRACK LENGTH .5 INCH APPROX. HINGE FITTING REPAIRED AS PER SRM 57-53-02-2R1 FIG 201.Sep 26, 2008 · N330UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS08653454Floor Support · crackedINSPECTION TYPE:N/A AFT CARGO COMPT STA 1324 FLOOR SUPPORT BEAM UPPER WEB FOUND CRACKED. CRACK LENGTH 1 INCH APPROX. FLOOR SUPPORT BEAM UPPER WEB REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Sep 25, 2008 · N330UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS08653456Skin · gougedINSPECTION TYPE:N/A DMID383810 - RT WING L/E SKIN GOUGE TEMP REPAIR I/B NR 2 ENG ABOVE KRUEGER FLAP. RT WING L/E SKIN AT BETWEEN ISS337.6-345.5 AREA SKIN REPAIRED AS PER RS R57-41-36117 & UPS EO B767-5730-30466-A.Sep 24, 2008 · N330UP · Boeing 76734AF · Wing, Plate/SkinSDR UPS08653430Bracket · crackedINSPECTION TYPE:C AFT CARGO COMPT STA 1087 RBL 25 UNDER FLOOR BRACKET FOUND CRACK (CRACK LENGTH 1 INCH). BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Sep 24, 2008 · N330UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS07650417Module · malfunctionedINSPECTION TYPE:ETOP APU BLEED INOP DEFERRED M 356254. T/S PER FIM APU BITE SHOWED PT SENSOR WITH MINIFLAG 14. REMOVED AND REPLACED FLOW SENSING MODULE PER MM 49-53-08-4. OPS AND BITE CHECK GOOD. THIS CLEARS M356254.Aug 9, 2007 · N330UP · Boeing 76734AF · APU Bleed Air SystemSDR UPS07649759Switch · defectiveINSPECTION TYPE:N/A THE EMERGENCY EXIT LIGHT SWITCH DOES NOT RETURN TO THE ARMED POSITION WHEN THE SWITCH CAP IS CLOSED. REMOVED AND REPLACED EMERGENCY LIGHT PANEL ASSY IAW AMM 33-50-00. OPS CHECKS OK.May 3, 2007 · N330UP · Boeing 76734AF · Emergency LightingSDR UPS07648938Unknown · malfunctionedINSPECTION TYPE:N/A DIVERSION - ALL 3 ILS SYSTEMS INOP. REPLACED ILS CONTROL PANEL PER AMM 34-31-02-4. OPS CHECKS GOOD.Jan 22, 2007 · N330UP · Boeing 76734AF · Localizer/VOR SystemSDR UPS06646529Radar · intermittentWEATHER FAIL ON HSI, BOTH SIDE (INTERMITTENT). T/S PERFORMED ACC TO FIM 34-43-001 FIG 103, NO FAULT FOUND. SYST WORKS PROPERLY. WEATHER RADAR DRIVE UNIT AND TRANS. REPLACED BY AMM 34-43-05-4, TRANSC P/N OFF 622-5432-101 S/N OFF: 2904 S/N ON: 2108 P/N ON: 6Mar 27, 2006 · N330UP · Boeing 767300 · Weather Radar SystemSDR UPS05643918Smoke Goggles · crackedINSPECTION TYPE:N/A, F/O SMOKE GOGGLES CRACKED. INSTALLED NEW SET OF SMOKE GOGGLES.Feb 22, 2005 · N330UP · Boeing 76734AF · Emergency EquipmentSDR UPS03640696Compressor · vibrationAT FL 330 RT ENG COMPRESSOR STALLED. 1ST STALL RT ENG VIB WAS 3.2 / 2ND VIB WAS 5.0. ENG THRUST WAS RETARDED TO IDLE. ON SHUTDOWN ENG READINGS WERE N1L 28.3 R28.7 EGTL 411 R480 N2L 69.0 R 72.0 FFL 1.3 R1. 5. R/R NR 2 ENG PER TC 6002 AND TC 6001. NO DEFECTS NMay 20, 2003 · N330UP · Boeing 767300 · Turbine Engine Compressor SectionSDR UPS01636634Door · leakingINSPECTION TYPE:N/A PILOT REP, FWD ENTRY DOOR SQUEALING. BUILT UP THRESHOLD AND PRESSURIZED A/C LEAK CHECKS GOOD.Aug 17, 2001 · N330UP · Boeing 767300 · Passenger/Crew Doors
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