N310UP

Service difficulty reports · 169

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 = 'N310UP' 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 IPXA1667097Floor Panel · puncturedINSPECTION TYPE:C, FLOOR PANEL FOUND 3 PUNCTURES AND 6 DENT MARKS AT STA 1425 TO STA 1540, RBL 55 TO RBL 77. FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.May 26, 2011 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667096Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND 3 PUNCTURES AND 8 DENT MARKS AT STA 412 TO STA 540, LBL 33 TO LBL 55. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.May 26, 2011 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667095Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND 4 PUNCTURES AND 6 DENT MARKS AT STA 654+22 TO STA 690. FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.May 26, 2011 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667094Floor Panel · puncturedINSPECTION TYPE:C, FLOOR PANEL FOUND 4 PUNCTURES AND 4 DENT MARKS AT STA 654+22 TO STA 690 LBL 33 TO LBL 55. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.May 26, 2011 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667049Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND 5 PUNCTURES AND 3 DENT MARKS AT STA 873 TO STA 933, LBL 77 TO LBL 88. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.May 26, 2011 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA0663704Floor Panel · damagedMAIN CARGO FLOOR PANEL REQUIRES FABRICATION IAW EO B767-5320-9693E. THIS IS A MAJOR REPAIR. ACCOMPLISHED FABRICATION OF MAIN CARGO FLOOR PANEL ON NRC 355114 IAW EO B767-5320-9693E.Nov 25, 2010 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA0663686Floor Panel · damagedMAIN DECK FLOOR PANEL, PN 145T5876-68 IS DAMAGED. FABRICATED NEW FLOOR PANEL ON NRC 355114 IAW EO B767-5320-9693-G.Nov 25, 2010 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10660907Floor Panel · damagedMAIN CARGO DECK POSITION 6L, LBL 64 AND LBL 58 TEMP REPAIRED. MFG AND INSTALLED NEW PANEL IAW EO B767-5320-9693 G.Jul 4, 2010 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658998Skin · dented6 SKIN DENTS AT STA 450 JUST FWD OF LWR FWD CARGO DOOR CUTOUT. DENTS ARE IN CLOSE PROX TO EACH OTHER. REPAIRED IAW EO B767-5330-36821-B.Mar 29, 2010 · N310UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA10658991Skin · dented6 SKIN DENTS AT STA 450 JUST FWD OF LWR FWD CARGO DOOR CUTOUT. DENTS ARE IN CLOSE PROX TO ONE ANOTHER. COMPLETED REPAIR IAW EO B767-5330-36821-B.Mar 28, 2010 · N310UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA10658840Floor Panel · damagedPOS 13R OB FWD FLOOR PANEL HAS A .5 DIA HOLE. REPAIRED IAW SRM 767-300F 53-00-50-2R.Mar 14, 2010 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657947Floor Panel · damagedMCD FLOOR PANEL DAMAGED. REPAIRED PER EO B767-53200-9693-F.Nov 17, 2009 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656876Fairing · 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 PAR 5A (1) FIG 5 REV 44. THIS CLASSIFIED AS MAJOR REPAIR WITH REPAIR MATERIAL RESIN EY3804PT AND GLASSFIBER BMS9-3TYH3CJul 22, 2009 · N310UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09656877Skin · dentedINSPECTION TYPE:C CUSTOMER REQUEST - CARRY OUT PERMANENT REPAIR AT FUSELAGE SKIN DENT AREA AT BS 1418 STR 29L-30L AREA. FASTENERS REMOVED & REINSTALLED WITHIN A 2 INCH PERIPHERY OF THE DENT AREA PER HX RS R53-61-36381 REV A, NO DAMAGES OR CRACK WERE FOUND AFTJul 21, 2009 · N310UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA09656858Fairing · delaminatedINSPECTION TYPE:C RT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 44. THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MATERIAL RESIN EY3804PT AND GLASS FIBER BMS 9-3TYHJul 21, 2009 · N310UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09656817Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL AT STA 412 TO 540 RBL 11 TO RBL 33 FOUND GOUGE & DENT MARKS. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED AS PER AMM 53-01-01.Jul 21, 2009 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656816Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL AT STA 283 TO 412, RBL 11 TO RBL 33 FOUND SCORE AND DENT MARKS. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED AS PER AMM 53-01-01.Jul 21, 2009 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656815Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL AT STA 731 TO 833 LBL 11 TO LBL 33 FOUND SCORE & DENT MARKS. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED AS PER AMM 53-01-01.Jul 21, 2009 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656813Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL AT STA 833 TO 930 LBL 55 TO LBL 77 FOUND GOUGE AND DENT MARKS. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED AS PER AMM 53-01-01.Jul 21, 2009 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656863Support Frame · crackedINSPECTION TYPE:C RT WING - I/B AILERON I/B HINGE SUPPORT FRAME AFT UPPER FLANGE FOUND CRACKED, CRACK LENGTH 1 INCH. RT WING I/B AILERON I/B HINGE SUPPORT FRAME AFT UPPER FLANGE REPAIRED AS PER HX RS R57-55-36384 REV A. THIS REPAIR IS CLASSIFIED AS MAJOR REPJul 20, 2009 · N310UP · Boeing 76734AF · AileronsSDR IPXA09656862Wedge · misrepairedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP TRAILING EDGE WEDGE LOWER SURFACE I/B AREA THE EXISTING REPAIR PATCH NON-STANDARD REPAIR. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5G FIG 14 REV 44. THIS IS CLASSIFIED AS MAJOR REPAIR WITHJul 20, 2009 · N310UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09656859Wedge · misrepairedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP T/E WEDGE LOWER SURFACE I/B AREA THE EXISTING REPAIR PATCH NON-STANDARD REPAIR. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5G FIG 14 REV 44. THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MATERJul 20, 2009 · N310UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09656856Attach Fitting · crackedINSPECTION TYPE:C LT WING L/E LES 622 FRONT SPAR ATT CLIP FOUND CRACKED, CRACK LENGTH 1.125 INCH. LT WING L/E LES 622 FRONT SPAR ATT CLIP REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 44.Jul 20, 2009 · N310UP · Boeing 76734AF · Wing SparSDR IPXA09656854Wedge · misrepairedINSPECTION TYPE:N/A LT WING O/B TRAILING EDGE FLAP TRAILING EDGE WEDGE LOWER SURFACE I/B AREA THE EXISTING REPAIR PATCH NON-STANDARD REPAIR. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5G FIG 14 REV 44. THIS REPAIR IS CLASSIFIED AS MAJOR REJul 20, 2009 · N310UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09656836Doubler · delaminatedINSPECTION TYPE:C RT WING NR 7 SPOILER UPPER SURFACE I/B AREA THE EXISTING REPAIR PATCH DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5A (1) FIG 5 REV 44.Jul 20, 2009 · N310UP · Boeing 76734P · SpoilersSDR IPXA09656789Fitting · crackedINSPECTION TYPE:C LT WING I/B MAIN FLAP DRIVE ARM UPPER FITTING LWR FLANGE CRACKED, CRACK AT BOTH I/B & O/B FLANGE. LT WING I/B MAIN FLAP DRIVE ARM UPPER FITTING REPAIRED AS PER SRM 57-53-02-2R1 FIG 201 REV 44, THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR WITH MJul 19, 2009 · N310UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09656860Skin · crackedINSPECTION TYPE:C LT WING NR 4 SLAT I/B NOSE SKIN FASTENER HOLE AREA FOUND CRACKED, CRACK LENGTH 0.125 INCH. LT WING NR 4 SLAT OSS573 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MATERIAL 7075-T6-0.0Jul 18, 2009 · N310UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09656857Skin · crackedINSPECTION TYPE:C RT WING NR 9 SLAT O/B NOSE SKIN FASTENER HOLE AREA FOUND CRACKED, CRACK LENGTH 0.125 INCH. RT WING NR 9 SLAT AT OSS 641.62 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MATERIAL 7075-Jul 18, 2009 · N310UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09656855Skin · crackedINSPECTION TYPE:N/A LT WING NR 4 SLAT O/B NOSE SKIN FASTENER HOLE AREA FOUND CRACKED, CRACK LENGTH 0.125 INCH. LT WING NR 4 SLAT OSS 641.55 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MATERIAL 7075-TJul 18, 2009 · N310UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09656853Skin · crackedINSPECTION TYPE:C LT WING NR 3 SLAT I/B AREA NOSE SKIN FASTENER HOLE AREA FOUND CRACKED, CRACK LENGTH 0.125 INCH. LT WING NR 3 SLAT AT OSS 724.49 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MATERIAL Jul 18, 2009 · N310UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09656819Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL AT STA 246 TO 412 RBL 55 TO RBL 77 FOUND DAMAGED. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED AS PER AMM 53-01-01.Jul 18, 2009 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656818Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL AT STA 690 TO 731, LBL 11 TO RBL 11 FOUND DAMAGED. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED AS PER AMM 53-01-01.Jul 18, 2009 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656814Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL AT STA 412 TO 540 RBL 33 TO RBL 55 FOUND DAMAGED. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED AS PER AMM 53-01-01.Jul 18, 2009 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656812Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL AT STA 936 TO 985 RBL 77 TO RBL 88 FOUND DAMAGED. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED AS PER AMM 53-01-01.Jul 18, 2009 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656811Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL AT STA 412 TO 540, LBL 11 TO RBL 11 FOUND DAMAGED. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED AS PER AMM 53-01-01.Jul 18, 2009 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656810Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL AT STA 833 TO 930, LBL 11 TO LBL 33 FOUND DAMAGED. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED AS PER AMM 53-01-01.Jul 18, 2009 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656809Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL AT STA 1460 TO 1540 LBL 55 TO LBL 77 FOUND DAMAGED. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED AS PER AMM 53-01-01.Jul 18, 2009 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656808Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL AT STA 975 TO 1114, LBL 11 TO RBL 11 FOUND DAMAGED. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED AS PER AMM 53-01-01.Jul 18, 2009 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656807Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL AT STA 412 TO 540, RBL 55 TO RBL 77 FOUND DAMAGED. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED AS PER AMM 53-01-01.Jul 18, 2009 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656806Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL AT STA 1207 TO 1350, LBL 11 TO RBL 11 FOUND DAMAGED. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED AS PER AMM 53-01-01.Jul 18, 2009 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656805Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL AT STA 540 TO 654+22, LBL 11 TO RBL 11 FOUND DAMAGED. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED AS PER AMM 53-01-01.Jul 18, 2009 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656804Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL AT STA 833 TO 930 LBL 11 TO RBL 11 FOUND DAMAGED. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED AS PER AMM 53-01-01.Jul 18, 2009 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656803Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL AT STA 1480 TO 1598 RBL 33 TO RBL 55 FOUND DAMAGED. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED AS PER AMM 53-01-01.Jul 18, 2009 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656802Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL AT STA 985 TO 1087 LBL 75 TO LBL 88 FOUND POOR CONDITION. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED AS PER AMM 53-01-01.Jul 18, 2009 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656801Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL AT STA 654+22 TO 690 LBL 11 TO RBL 11 FOUND DAMAGED. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED AS PER AMM 53-01-01.Jul 18, 2009 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656800Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL AT STA 1480 TO 1598, LBL 11 TO RBL 11 FOUND DAMAGED. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED AS PER AMM 53-01-01.Jul 18, 2009 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656799Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL AT STA 1197 TO 1207 LBL 11 TO RBL 11 FOUND DAMAGED. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED AS PER AMM 53-01-01.Jul 18, 2009 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656798Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL AT STA 833 TO 930, RBL 33 TO RBL 55 FOUND DAMAGE. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jul 18, 2009 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656861Stiffener · crackedINSPECTION TYPE:C FWD CARGO COMPT STA 785.9 WING CENTER SECTION FRONT SPAR STIFFENER FOUND CRACK AT LBL 32.94 WL 194, CRACK LENGTH 1.125 INCH. FWD CARGO COMPT STA 785.9 WING CENTER SECTION FRONT SPAR AT LBL 32.94 STIFFENER REPAIRED PER HX RS R57-10-36376 REV Jul 17, 2009 · N310UP · Boeing 76734AF · Wing, Center BoxSDR IPXA09656835Stiffener · crackedINSPECTION TYPE:C MAIN EQUIPMENT CENTER STA 246 FLOORBEAM STIFFENER FOUND CRACK AT LBL 40, CRACK LENGTH 1.25 INCH. MAIN EQUIPMENT CTR STA 246 LBL 40 FLOORBEAM STIFFENER REPAIRED PER SRM 53-10-51-2R4 FIG 201 REV 44. THIS CLASSIFIED AS MAJOR REPAIR WITH MATERIJul 17, 2009 · N310UP · Boeing 76734AF · Fuselage Main, Floor Beam
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