N302UP

Service difficulty reports · 189

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 = 'N302UP' 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 IPXA1670462Floor Panel · damagedFLOOR PANEL DAMAGED. FABRICATED NEW PANEL IAW EO B767-5320-9693-H.Nov 27, 2011 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1670461Floor Panel · damagedFLOOR PANEL DAMAGE. FABRICATED NEW PANEL IAW EO B767-5320-9693-H.Nov 27, 2011 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1670407Floor Panel · damagedMCD FLOOR PANEL POS 6 FWD CENTER HAS HOLE. REPAIRED FLOOR PANEL IAW SRM 53-00-50-2R.Nov 21, 2011 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1670406Floor Panel · damagedMCD FLOOR PANEL NR 6 CENTER FWD HAS 3 HOLES. REPAIRED FLOOR PANEL IAW SRM 53-00-50-2R.Nov 21, 2011 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1670405Floor Panel · damagedMCD POS 6 CENTER FWD HAS 3 HOLES. REPAIR IAW SRM 53-00-50-2R.Nov 21, 2011 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1670404Floor Panel · damagedFLOOR PANEL POS NR 9L, 3RD PANEL FROM LT HAS HOLE. REPAIRED IAW SRM 53-00-50-2R.Nov 21, 2011 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1670403Floor Panel · damagedMCD FLOOR PANEL POS 9 CENTER AFT END HAS HOLE. REPAIRED IAW SRM 53-00-50-2R.Nov 21, 2011 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11670353Floor Panel · damagedMAIN CARGO FLOOR PANEL DAMAGED AT STA 654+98. REPAIRED IAW SRM 53-00-50-2R.Nov 14, 2011 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11670352Floor Panel · damagedFLOOR PANEL DAMAGED STA 654+110. REPAIRED IAW SRM 53-00-50-2R.Nov 14, 2011 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11670350Floor Panel · damagedMCD FLOOR PANEL POS NR 5 CENTER HAS HOLE STA 654.110 7 INCHES RIGHT OF CENTER. REPAIRED IAW SRM 53-00-50-2R.Nov 14, 2011 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11670346Floor Panel · damagedMAIN CARGO DECK POS 4 FWD CENTER OF PANEL HAS A HOLE. REPAIRED REF SRM 53-00-50-2R, REPAIR 1.Nov 14, 2011 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11670351Floor Panel · damagedMCD POS 5 CTR FLOOR PANEL HAS HOLE STA 654.98 1 INCH RT OF CTR. REPAIRED IAW SRM 53-00-50-2R.Nov 13, 2011 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11670345Floor Panel · damagedMAIN CARGO DECK POSITION 4 AFT CENTER OF PANEL HAS A HOLE. REPAIRED IAW SRM 53-00-50-2R.Nov 13, 2011 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11670339Floor Panel · damagedFLOOR PANEL DAMAGED. REPAIRED IAW SRM 53-00-50.Nov 13, 2011 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11670338Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL DAMAGED. REPAIRED IAW SRM 53-00-50.Nov 13, 2011 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11670336Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL DAMAGED. REPAIRED IAW SRM 53-00-50.Nov 13, 2011 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11670335Floor Panel · damagedMAIN CARGO FLOOR PANEL DAMAGED. REPAIRED IAW SRM 53-00-50.Nov 13, 2011 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1664979Escape Rope · out of trackROPE END HAD FALLEN OUT OF TRACK IN DOOR CUT OUT. STOWED ROPE END BACK IN TRACK IAW AMM 25-61-04-2.Feb 24, 2011 · N302UP · Boeing 76734AF · Emergency EquipmentSDR IPXA1664522Wedge · dentedLT HAND OTBD FLAP T/E WEDGE HAS DENT AND DEBONDED AT STA 254.69. REPAIRED IAW EO B767-5750-40481-B.Jan 31, 2011 · N302UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10663424Connector · brokenINSPECTION TYPE:ETOP DIVERSION - "CARGO DET AIR" EICAS MESSAGE. M438137. R & R SMOKE DETECTOR VACUUM SWITCH IAW AMM 26-16- 04-4. FOUND CONNECTOR BROKEN ON SWITCH.Oct 29, 2010 · N302UP · Boeing 76734AF · Fire Protection System WiringSDR IPXA0660660Skin · damagedRT OTBD AILERON HAS 4 OTHER AREAS OF LIGHTNING STRIKE DAMAGE ON UPPER SURFACE OF WEDGE MARKED. STARTED SANDING AREA, FWD LIMITS TO ENGR. FINISHED DAMAGE REMOVAL REF SRM 57-60-02-2R. STARTED NR 346819. REPAIR COMPLETE SEE NRC 346819 AND ECA 020462. THIS REPAIJun 21, 2010 · N302UP · Boeing 76734AF · AileronsSDR IPXA0660654Wedge · damagedRT OTBD AILERON T/E WEDGE LIGHTNING DAMAGE. REPAIRED IAW EO B767-5750-38137-B.Jun 21, 2010 · N302UP · Boeing 76734AF · AileronsSDR IPXA10659516Shim · unknownINSPECTION TYPE:C FUS REMOVE FASTENERS / PARTS IDENTIFIED IN EO B767-5350-17922-E APP C, FIG 6 AS NECESSARY TO INSTALL A PROTECTIVE SHIM FASTENER / PARTS. REMOVED AND REINSTALLED IAW EO B767-5350-17922-E APPENDIX C FIG 6 IN ORDER TO INSTALL A PROTECTIVE SHIM Apr 22, 2010 · N302UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA10659433Skin · misrepairedINSPECTION TYPE:C, SURVEY SEQ NR 302-F1-02 FUSELAGE BETWEEN BS 439 TO BS 463 AND STR 23R-25R EXISTING REPAIR DOES NOT CORRELATED TO A SRM. SURVEY SEQ 302-F1-02 FX BTN BS436-463 & STR23R-25R SKIN REPAIRED IAW RS R53-00-36706, EO B767-5330-37489, ORG MATL IS 20Apr 21, 2010 · N302UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA10659519Failsafe · crackedINSP TYPE:C FUS RT BS 955 BULKHEAD FITTING AREA CRACK AT FAIL SAFE STRAP APPROX .2500" & .3750" IN LENGTH. REFER NRC 50422 FOR DETAIL, FUSELAGE RT BS 955 REAR SPAR BULKHEAD FITTING AREA FAIL SAFE STRAP REPAIRED IAW EO B767-5350-17922-E, APPENDIX D.Apr 15, 2010 · N302UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA10659512Fitting · crackedINSPECTION TYPE:C, FUS RT BS 955 REAR SPAR BULKHEAD FITTING AREA 1EA FASTENER HOLE FOUND CRACKED INDICATIONS RUNNING BOTH FWD & AFT FUSELAGE RT BS 955 REAR SPAR BULKHEAD FITTING AREA FAIL SAFE STRAP REPAIRED IAW EO B767-5350-17922-E, APPENDIX D.Apr 15, 2010 · N302UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA10659485Fitting · corrodedINSPECTION TYPE:C, FX - RT STA 955 BULKHEAD FITTING AREA CORROSION FOUND AT "T" FITTING HOLE AROUND THE HOLE BORE SURFACE. RT STA 955 BULKHEAD FITTING AREA "T" FITTING REPLACED AND INSTALLED IAW EO B767-5350-17922-E APPENDIX D, FIG 6.Apr 15, 2010 · N302UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA10659409Bracket · crackedINSPECTION TYPE:C, LT WING - L/E LES675 FIXED FAIRING SUPPORT WEB AFT FRONT SPAR BRACKET FOUND CRACKED. LT WING L/E LES675 FIXED FAIRING SUPPORT WEB AFT FRONT SPAR BRACKET, REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02.Apr 15, 2010 · N302UP · Boeing 76734AF · Wing, Attach FittingsSDR IPXA10659390Wedge · crackedINSPECTION TYPE:C RT WING O/B TRAILING EDGE FLAP TRAILING EDGE WEDGE I/B AFT EDGE AREA CRACKED. COMPOSITE PREP REG LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5G FIG 14.Apr 15, 2010 · N302UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10659515Failsafe · crackedINSPECTION TYPE:C FUS LT B S955 BULKHEAD FITTING FAIL SAFE STRAP CRACK FOUND AT FWD SIDE THRU THICKNESS AT 9 O/C POSN AFT SDE CRACK AT 5 O/C POSITION (LOCKING INBD) APPROX 0.040" REF NRC 50425 FOR DETAIL. FUSELAGE LT BS955 REAR SPAR BULKHEAD FITTING AREA FAIL Apr 14, 2010 · N302UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA10659486Fitting · crackedINSPECTION TYPE:C FX - LT STA 955 BULKHEAD TEE FITTING CRACK FOUND AT 7 O`CLOCK POSITION APPROX .0625" LONG. FX - LT STA 955 BULKHEAD TEE FITTING REPLACED AND INSTALLED IAW EO B767-5350-17922-E APPENDIX C, FIG 6.Apr 14, 2010 · N302UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA10659588Support Angle · crackedINSPECTION TYPE:C, RT WING L/E LES 160 FRONT SPAR UPPER SUPPORT ANGLE FOUND CRACKED CRACK LENGTH .3750". RT WING L/E LES 160 FRONT SPAR UPPER SUPPORT ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 46.Apr 13, 2010 · N302UP · Boeing 76734AF · Wing Miscellaneous StructureSDR IPXA10659518Panel · chippedINSP TYPE:C EMP - RT INBD ELEVATOR T/E OTBD CORNER UPPER SURFACE CHIPPED COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW RS R55-20-36704, REV A AND EO B767-5520-37442-A.Apr 13, 2010 · N302UP · Boeing 76734AF · Elevator, Plate/SkinSDR IPXA10659513Fitting · crackedINSPECTION TYPE:C FUS LT BS955 REAR SPAR BULKHEAD FITTING AREA 1EA FASTENER HOLE FOUND CRACKED INDICATIONS RUNNING BOTH FWD & AFT FUSELAGE LT BS 955 REAR SPAR BULKHEAD FITTING AREA FAIL SAFE STRAP REPAIRED IAW EO B767-5350-17922-E, APPENDIX C.Apr 13, 2010 · N302UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA10659326Floor Panel · misrepairedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND DAMAGE AND INCORRECT REPAIR EXISTING AT STN 833 TO STN933 LBL11" TO RBL11". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Apr 13, 2010 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659325Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND PUNCTURE DAMAGE AT STN975 TO 1114 LBL11" TO RBL11". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Apr 13, 2010 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659324Floor Panel · misrepairedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND DAMAGE AND INCORRECT REPAIR EXISTING AT STN 654+22 TO STN690 LBL33" TO LBL55". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Apr 13, 2010 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659323Floor Panel · puncturedINSP TYPE:C, MCD FLOOR PANEL FOUND PUNCTURED, DAMAGED AT STN 588 TO 654+22 RBL 77" TO RBL 88". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Apr 13, 2010 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659549Rib · crackedINSPECTION TYPE:8C, LT WING - INBD AILERON INBD RIB FITTING UPPER AFT FLANGE FOUND CRACKED. LT WING INBD AILERON INBD RIB FITTING UPPER AFT FLANGE REPAIRED IAW HX RS NO R-57-00-36699 REV A & UPS EO NO. B767-5740-37473-A. ORG MAT'L IS 7075T73 FORGING, CRK LApr 12, 2010 · N302UP · Boeing 76734AF · Wing, Rib/BulkheadSDR IPXA10659432Rib · crackedINSPECTION TYPE:C, RT WING INBD AILERON INBD RIB FTG UPPER AFT FLANGE FOUND CRACKED. RT WING INBD AILERON INBD RIB FTG UPR AFT FLANGE REPAIRED IAW RS R57-00-36698 & EO B767-5740-37472-A, ORG MATL IS 7075T73FORGING, CRACK LENGTH IS 1.1", FINAL CUTOUT SIZE IS 1Apr 12, 2010 · N302UP · Boeing 76734AF · Wing, Rib/BulkheadSDR IPXA10659431Floorbeam · crackedINSPECTION TYPE:C, MAIN DECK STA 246 FLOORBEAM ATTACH ANGLE FOUND CRACKED AT LBL 25". MAIN DECK STA 246 FLOORBEAM AT LBL 25" ATTACH ANGLE REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02.Apr 12, 2010 · N302UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA10659430Floorbeam · crackedINSPECTION TYPE:C, MAIN DECK STA 246 FLOORBEAM ATTACH CLIP FOUND CRACKED AT LBL 50" MAIN DECK STA 246 FLOORBEAM AT LBL50" ATT CLIP REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02.Apr 12, 2010 · N302UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA10659410Stiffener · crackedINSPECTION TYPE:C, WING CTR SECTION FRONT SPAR VERTICAL STIFFENER FOUND CRACKED JUST AT STA785.9 RBL10.94" WING CTR SECTION FRONT SPAR VERT STIFFENER REPAIRED IAW RS R57-00-36703, EO B767-5710-37458 JUST AT STA785.9 RBL10.94" ORG MATL IS BAC1518-749-2024T3511Apr 12, 2010 · N302UP · Boeing 76734AF · Wing Main, Frame StructureSDR IPXA10659389Hinge Fitting · crackedINSPECTION TYPE:C, LT WING INBD MAIN FLAP INBD SUPPORT HINGE FITTING FLANGE FOUND CRACKED. LT WING INBD MAIN FLAP INBD SUPT HINGE FTG REPAIRED IAW SRM 57-53-02-2R1, FIG201, ORG MATL IS 7075T73 FORGING, CRACK LENGTH AT BOTH INBD & OTBD FLANGE ARE 1.5", DAMAGEDApr 12, 2010 · N302UP · Boeing 76734AF · Wing, Control Surface Attach FittingsSDR IPXA10659388Hinge Fitting · crackedRT WING - INBD MAIN FLAP INBD SUPPORT HINGE FITTING FLANGE FOUND CRACKED. RT WING INBD MAIN FLAP INBD SUPT HINGE FTG REPAIRED IAW SRM 57-53-02-2R1, FIG 201, ORG MATL IS 7075T73 FORGING, CRK LENGTH AT BOTH INBD & OTBD FLANGE ARE 1.5", DAMAGED CUTOUT SIZE ARApr 12, 2010 · N302UP · Boeing 76734AF · Wing, Control Surface Attach FittingsSDR IPXA10659365Skin · crackedINSPECTION TYPE:C, LT WING NR 3 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 3 SLAT OTBD NOSE SKIN AT OSS792.5 SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, ORG MATL IS 7075T6-0.063", CRK LEGNTH IS 0.09". DAMAGED CUTOUT IS 8.875" X 7.125" THIS REApr 12, 2010 · N302UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10659364Skin · crackedINSPECTION TYPE:C, RT WING NR 9 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 9 SLAT INBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, JUST AT OSS 572.5, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.08" DAMAGED CUTOUT IS 8.875" X 7.25" THIS IS CApr 12, 2010 · N302UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10659363Skin · crackedINSP TYPE:C, RT WING NR 9 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 9 SLAT OTBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201. JUST AT OSS641.9, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.09" DAMAGED CUTOUT IS 8.875" X 7.125". THIS IS CApr 12, 2010 · N302UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10659362Skin · crackedINSPECTION TYPE:C, LT WING NR 4 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LTW NR4 SLAT INBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201 JUST AT OSS572.5, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.125" DAMAGED CUTOUT IS 8.875" X 7.125" THIS IS CLASSIApr 12, 2010 · N302UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10659361Skin · crackedINSPECTION TYPE:C, LT WING NR 4 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR4 SLAT OTBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, JUST AT OSS641.9, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.25" DAMAGED CUTOUT IS 8.875" X 7" THIS IS CLASSIApr 12, 2010 · N302UP · Boeing 76734AF · Leading Edge Devices
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