N305UP

Service difficulty reports · 216

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 = 'N305UP' 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 IPXA10660759Window · out of adjustF/O SLIDING WINDOW HANDLE REQUIRES EXCESSIVE FORCE TO OPERATE. ADJUSTED F/O SLIDING WINDOW IAW 56-11-02-5. OPS NORMAL. NOTE: WINDOW HEAT TERMINAL WAS NOT DISTURBED.Jun 24, 2010 · N305UP · Boeing 76734AF · Flight Compartment WindowsSDR IPXA10660544Bracket · inoperativeF/O WINDOW BRACKET BROKEN WHEN WINDOW WAS CLOSED. R & R F/O'S SLIDING WINDOW BEWTWEEN BRACKET IAW AMM 56-11-04-4. ALL SATISFACTORY.Jun 15, 2010 · N305UP · Boeing 76734AF · Flight Compartment WindowsSDR IPXA10659546Crank Assy · bindingL2 WINDOW CRANK BINDING TOWARD CLOSE. ADJUSTED THE L2 WINDOW IAW MM 56-11-02-5. OPS GOOD.Apr 27, 2010 · N305UP · Boeing 76734AF · Flight Compartment WindowsSDR 2010F00023Control Cable · icedON ARRIVAL, CREW REPORTED STAB TRIM NO MOVEMENT IN NORM OR ALT MODES. ON INVESTIGATION STAB BAY FOUND TO HAVE ICE FORMATION APPROX 10 INCHES DEEP IN BILGE AREA. ICE FORMATION HAD PREVENTED POSITION MODULES AND FOLLOW UP CABLES FROM MOVING. THIS RESULTED IN CAFeb 1, 2010 · N305UP · Boeing 76734AF · Stabilizer Control SystemSDR UPS09654398Skin Panel · misrepairedINSPECTION TYPE:C EMP - LT HORIZONTAL STAB UPPER L/E FIXED PANEL SURVEY SEQ 305-S1-12 TO 16 EXISTING REPAIR PATCH NON STANDARD REPAIR. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 2 FIG 201.Jan 17, 2009 · N305UP · Boeing 76734AF · Horizontal Stabilizer, Plate/SkinSDR UPS09654397Skin Panel · misrepairedINSPECTION TYPE:C EMP - LT HORIZONTAL STAB UPPER L/E FIXED PANEL EXISTING REPAIR PATCH NON STANDARD REPAIR. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 2 FIG 201.Jan 17, 2009 · N305UP · Boeing 76734AF · Horizontal Stabilizer, Plate/SkinSDR UPS09654396Skin Panel · misrepairedINSPECTION TYPE:C EMP - LT HORIZONTAL STAB UPPER L/E FIXED PANEL EXISTING REPAIR PATCH NON STANDARD REPAIR. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 2 FIG 201.Jan 17, 2009 · N305UP · Boeing 76734AF · Horizontal Stabilizer, Plate/SkinSDR UPS09654395Skin Panel · misrepairedINSPECTION TYPE:C EMP - LT HORIZONTAL STAB UPPER L/E FIXED PANEL EXISTING REPAIR PATCH NON STANDARD REPAIR. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 2 FIG 203.Jan 17, 2009 · N305UP · Boeing 76734AF · Horizontal Stabilizer, Plate/SkinSDR UPS09654394Skin Panel · debondedINSPECTION TYPE:C EMP - RT HORIZONTAL STAB UPPER L/E FIXED PANEL EXISTING REPAIR PATCH DISBOND. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 2 FIG 201.Jan 17, 2009 · N305UP · Boeing 76734AF · Horizontal Stabilizer, Plate/SkinSDR UPS09654387Skin · misrepairedINSPECTION TYPE:C RT WING NR 10 SPOILER T/E UPPER SURFACE EXISTING REPAIR PATCH NON STANDARD REPAIR. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4A (1) FIG 10.Jan 11, 2009 · N305UP · Boeing 76734AF · SpoilersSDR UPS09654386Skin · misrepairedINSPECTION TYPE:C RT WING NR 12 SPOILER UPPER SURFACE 1EA EXISTING REPAIR PATCH NON STANDARD REPAIR. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4A FIG 10.Jan 11, 2009 · N305UP · Boeing 76734AF · SpoilersSDR UPS09654385Skin · misrepairedINSPECTION TYPE:C RT WING NR 12 SPOILER UPPER SURFACE 1EA EXISTING REPAIR PATCH NON STANDARD REPAIR. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4A FIG 10.Jan 11, 2009 · N305UP · Boeing 76734AF · SpoilersSDR UPS09654352Skin · misrepairedINSPECTION TYPE: C RT WING NR 12 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W4-55, -56, REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511194-1.Jan 8, 2009 · N305UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654351Skin · misrepairedINSPECTION TYPE: C RT WING NR 9 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR REF SURVEY SEQ NR 305-W4-30, REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511210-1.Jan 8, 2009 · N305UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654350Skin · misrepairedINSPECTION TYPE: C RT WING NR 10 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W4-38, REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511178-1.Jan 8, 2009 · N305UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654349Skin · misrepairedINSPECTION TYPE: C LT WING NR 4 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W3-31, -32, REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511244-1.Jan 8, 2009 · N305UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654348Skin · misrepairedINSPECTION TYPE: C RT WING NR 8 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W4-23, -24, REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511145-1.Jan 8, 2009 · N305UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654347Skin · misrepairedINSPECTION TYPE: C RT WING NR 7 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W4-5, -6, -7, REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511160-1.Jan 8, 2009 · N305UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654346Skin · misrepairedINSPECTION TYPE: C RT WING NR 8 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W4-16, -17. REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511129-1.Jan 8, 2009 · N305UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654345Skin · misrepairedINSPECTION TYPE: C RT WING NR 12 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W4-53, -54. REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511228-1.Jan 8, 2009 · N305UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654344Skin · misrepairedINSPECTION TYPE: C RT WING NR 8 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W4-13, 14. REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511202-1.Jan 8, 2009 · N305UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654341Skin · misrepairedINSPECTION TYPE: C RT WING NR 8 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W4-20,21. RT WING NR 8 SLAT T/E WEDGE UPPER SKIN REPAIRED IAW SRM 51-70-10 AND COMPONENT WORK PROCESS CARD NR BTF 511152-1.Jan 8, 2009 · N305UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654340Skin · misrepairedINSPECTION TYPE: C RT WING NR 8 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR REF SURVEY SEQ NR 305-W4-18, -19, RT WING NR 8 SLAT T/E WEDGE UPPER SKIN REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511137-1.Jan 8, 2009 · N305UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654339Skin · misrepairedINSPECTION TYPE: C LT WING NR 4 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W3-34, -35, LT WING NR 4 SLAT T/E WEDGE UPPER SKIN REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511251-1.Jan 8, 2009 · N305UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654338Skin · misrepairedINSPECTION TYPE: C LT WING NR 4 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ. 305-W3-26, LT WING NR 4 SLAT T/E WEDGE UPPER SKIN REPAIRED IAW SRM 51-70-10 AND COMPONENT WORK PROCESS CARD NR BTF511236-1.Jan 8, 2009 · N305UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654337Skin · misrepairedINSPECTION TYPE: C RT WING NR 12 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W4-51,52 RHW NR12 SLAT T/E WEDGE UPPER SKIN REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511186-1.Jan 8, 2009 · N305UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654392Skin · damagedINSPECTION TYPE:C FX- BS 132.5-145.6 STR 38R - 39R AREA SKIN REPAIR ISN'T APPLICABLE TO THE AREA WITHIN 22 INCHES OF A DOOR CUTOUT AS PER SRM 53-00-01 2R 14 FIG 201 REF TO SURVEY SEQ 305-F1-01. THE SURVEY SEQ 305-F1-01 FUSELAGE BS 132.5 - 145.6 STR 38R- 39R AJan 1, 2009 · N305UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR UPS09654391Skin · damagedINSPECTION TYPE:C FX- BS 164-172 STR 39R AREA SKIN REPAIR ISN'T APPLICABLE TO THE AREA WITHIN 22 INCHES OF A DOOR CUTOUT AS PER SRM 53-00-01 2R 14 FIG 201 REF TO SURVEY SEQ 305-F1-03. THE SURVEY SEQ 305-F1-03 FUSELAGE BS 164-172 STR 39R AREA SKIN REPAIRED AS Jan 1, 2009 · N305UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR UPS09654390Skin · damagedINSPECTION TYPE:C THE REPAIR CONFIGURATION IS NOT FULFILLED WITH THE SRM AT THE AREA BS 1310.5-1329 STR 27R-28R AREA REF SURVEY SEQ 305-F1-08. THE SURVEY SEQ 305-F1-08 FUSELAGE BS 1310.5 - 1329 STR 27R - 28R AREA DOOR SKIN REPAIRED AS PER HX RS R52-34-36254 AJan 1, 2009 · N305UP · Boeing 76734AF · Cargo/Baggage DoorsSDR UPS09654327Skin · damagedINSPECTION TYPE:C SURVEY SEQ 305-F1-07 FUSELAGE BS 654+22 TO 654+44 STR 23R-25R SKIN REPAIR CAN'T DETERMINE THE REPAIR CONFIGURATION AS PER SRM DUE TO NO CUTOUT FOUND REFER SRM. SURVEY SEQ 305-F1-07 FUSELAGE BS 654+22 TO BS 654+44 BETWEEN STR 23R-25R SKIN REPJan 1, 2009 · N305UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR UPS09654326Fairing · delaminatedINSPECTION TYPE:C RT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAPA 5A (1) FIG 5.Jan 1, 2009 · N305UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS09654322Fairing · delaminatedINSPECTION TYPE:C LT WING O/B FLAP L/E MID FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PARA 5A (1) FIG 5.Jan 1, 2009 · N305UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS09654320Fairing · delaminatedINSPECTION TYPE:C LT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PARA 5A (1) FIG 5.Jan 1, 2009 · N305UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS09654316Skin Panel · delaminatedINSPECTION TYPE:C LT WING I/B MAIN FLAP AFT UPPER FIXED PANEL UPPER SURFACE DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PARA 5A (1) FIG 5.Jan 1, 2009 · N305UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS09654393Skin · delaminatedINSPECTION TYPE:C LT WING NR 5 SPOILER LOWER SURFACE DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER HX RS R57-70-36252 REV B AND UPS EO B767-5750-31918-A.Dec 31, 2008 · N305UP · Boeing 76734AF · SpoilersSDR UPS09654292Fitting · crackedINSPECTION TYPE: C LT WING INBD MAIN FLAP INBD AFT FLAP SUPPORT FTG UPPR AREA FLANGE FOUND CRACKED. REPAIRED IAW SRM 57-53-02-2R1 FIG 201.Dec 31, 2008 · N305UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS09654325Attach Angle · crackedINSPECTION TYPE:C AFT OF BULK CARGO STA 1580 LBL 80 MAIN DECK SEAT TRACK ATTACH ANGLE CRACK. AFT OF BULK CARGO BS 1580 LBL 80 MAIN DECK SEAT TRACK ATTACH ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.Dec 31, 2008 · N305UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR UPS09654324Stiffener · crackedINSPECTION TYPE:C FX MEC COMPT BS 246 RBL 10 MAIN DECK FLOOR SUPPORT BEAM ATTACH STIFFENER CRACK. MEC BS 246 RBL 10 FLOOR SUPPORT BEAM ATTACH STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.Dec 31, 2008 · N305UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR UPS09654321Skin Panel · delaminatedINSPECTION TYPE:C EMP - VERTICAL STABILIZER PANEL 322CR DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A (1) FIG 9.Dec 31, 2008 · N305UP · Boeing 76734AF · Vertical Stabilizer, Plate/SkinSDR UPS09654315Skin Panel · delaminatedINSPECTION TYPE:C RT WING I/B MAIN FLAP T/E UPPER SURFACE DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PARA 5A (1) FIG 5.Dec 31, 2008 · N305UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS09654408Floor Panel · damagedINSPECTION TYPE:C M/D STA 363 WL 200 RBL 71 FLOOR PANEL FOUND REPAIR PATCH. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R.Dec 30, 2008 · N305UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS09654328Skin · dentedINSPECTION TYPE:C SURVEY SEQUENCE 305-F1-05 FX BS 444-458.5 STR 23R-24R EXISTING REPAIR DOUBLER TOP SURFACE PREVIOUS BLENDING FOUND WITH SLIGHTLY DENT. SURVEY SEQUENCE 305-F1-05 FUSELAGE BS 444-458.5 BETWEEN STR 23R-24R SKIN REPAIRED WITH ZERO TIMING AS PER SDec 30, 2008 · N305UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR UPS09654318Panel · debondedINSPECTION TYPE:C EMP VERTICAL STABILIZER RT LOWER SURFACE PREVIOUS REPAIR AREA DEBOND. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 4.Dec 30, 2008 · N305UP · Boeing 76734AF · Vertical Stabilizer, Plate/SkinSDR UPS09654317Bracket · crackedINSPECTION TYPE:C RT WING LES 675 L/E SUPPORT AFT UPPER FRONT SPAR BRACKET FOUND CRACKED. RT WING LES 675 L/E SUPPORT AFT UPPER FRONT SPAR BRACKET REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.Dec 30, 2008 · N305UP · Boeing 76734AF · Wing SparSDR UPS09654409Floor Panel · damagedINSPECTION TYPE:C M/D STA 410 WL 200 RBL 83 FLOOR PANEL FOUND REPAIR PATCH. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R.Dec 29, 2008 · N305UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS09654286Floorbeam · crackedINSPECTION TYPE: C, AFT CARGO COMPT BS 1087 RBL 26 INCHES BELOW FLOOR ANGLE SUPPORT FOUND CRACK. AFT CARGO COMPT BS 1087 RBL 26 INCHES BELOW FLOOR SUPPORT ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02.Dec 28, 2008 · N305UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR UPS09654293Floorbeam · crackedINSPECTION TYPE: C AFT CARGO COMPT BS 1087 LBL 26 INBD BELOW FLOOR ANGLE SUPPORT FOUND CRACKED. AFT CARGO COMPT BS 1087 LBL 26 INCH BELOW FLOOR SUPPORT ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02.Dec 28, 2008 · N305UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR UPS09654323Intercostal · crackedINSPECTION TYPE:C FX MEC COMPT BS 246 LBL 50 FLOORBEAM AFT FACE INTERCOSTAL UPPER AREA FOUND CRACK. MEC COMPT BS 246 LBL 50 FLOORBEAM AFT FACE INTERCOSTAL UPPER AREA REPAIRED AS PER SRM 51-70-11-0G FIG 1.Dec 28, 2008 · N305UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS09654319Support Angle · crackedINSPECTION TYPE:C MEC BS246 LBL 40 FLOORBEAM FRONT FACE SUPPORT ANGLE FWD CRACK. MEC BS 246 LBL 40 FLOORBEAM FRONT FACE SUPPORT ANGLE REPAIRED AS PER SRM 53-10-51-2R4 FIG 201. REPEAT INSP IS REQUIRED AS PER SRM 53-10-51-2R4 FIG 201 SHT 2 TABLE II UPS MPI P20Dec 28, 2008 · N305UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR UPS09654343Angle · crackedINSPECTION TYPE: C FX MEC COMPT BS 246 LBL 25 INCH FLOORBEAM FRONT FACE SUPPORT ANGLE FOUND CRACKED. REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02.Dec 28, 2008 · N305UP · Boeing 76734AF · Fuselage Miscellaneous Structure
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