N311UP

Service difficulty reports · 171

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 = 'N311UP' 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 IPXA1668528Floor Panel · dentedINSPECTION TYPE:8C, MCD FLOOR PANEL FOUND 8 DENTS AND 7 PUNCTURES AT STA 1197+22 TO STA 1207 LBL11 TO RBL11. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM53-01-01.Jul 29, 2011 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1668505Fairing · delaminatedINSPECTION TYPE:C, LT WING OTBD T/E FLAP INBD L/E FAIRING DELAMINATED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A (1) FIG 5, REV 50.Jul 29, 2011 · N311UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA1668504Fairing · delaminatedINSPECTION TYPE:C, LT WING INBD MAIN FLAP OTBD L/E FAIRING FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A(1) FIG 5, REV 50.Jul 29, 2011 · N311UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA1668495Failsafe · damagedINSPECTION TYPE:C, FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FITTING, FAIL SAFE STRAP AREA, SUSPECT CRACK FOUND, REMOVED FASTENER FOR CRACK CONFIRMATION FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP ATT MOST LOWER BOLT REMOVED AND REIJul 29, 2011 · N311UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA1668491Failsafe · crackedINSPECTION TYPE:C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FTG FAIL SAFE STRAP AREA , SUSPECT CRACK FOUND, REMOVE FASTENER FOR CRACK CONFIRMATION. FUSELAGE LT BS 955, REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP ATT MOST LOWER BOLT. REMOVED AND REINSTALJul 29, 2011 · N311UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA11666523Skin · dentedDENT NR 1 D449024 AND DENT NR 2 D449025 LT WING INBD AFT FLAP T/E WEDGE LWR SURFACE DENTS. REPAIRED BOTH DENTS USING ONE REPAIR IAW SRM 51-70-10-2R AND EO B767-5 750-41819-B.May 8, 2011 · N311UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA11666522Skin · dentedD449026 DENT NR 3 LT WING INBD AFT FLAP T/E WEDGE LWR SKIN DENT REPAIR. REPAIRED IAW SRM 51-70-10-2R AND EO B767-5750-42592-A.May 8, 2011 · N311UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA11666521Skin · dentedDENT 4 LT WING INBD AFT FLAP T/E WEDGE LWR SKIN REPAIR. REPAIRED IAW SRM 51-70-10-2R AND EO B767-5750-42593-A.May 8, 2011 · N311UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA1665844Detection Sys · inoperativeINSPECTION TYPE:E, TOP -LT DUCT LIGHT CAME ON WITH EICAS MSG. RAN CHECKLIST. LT DUCT LEAK DETECTION SYS DEFERRED INOP IAW MEL 26-18-1-1-4. STICKER INSTALLED. ETOPS REPORT FILED OPEN. INSPECTED LT PNEUMATIC MANIFOLD FOR LEAKS IN THE PYLON, WING AND AIR CONDIApr 3, 2011 · N311UP · Boeing 76734AF · Overheat DetectionSDR IPXA10661444Floor Panel · damagedPOS 4L HAS DAMAGE ON THE FWD END JUST AFT OF THE BALL MAT 1" DIA DAMAGE IS LOCATED 41" FROM AFT ED AND 8" FROM L/E EDGE. REPAIRED IAW SRM53-00-50-2R.Aug 2, 2010 · N311UP · Boeing 767300 · Fuselage Floor PanelSDR IPXA10659683Eec · faultyDURING ENGINE START ON NR 2 EGT DID NOT RISE. ON SECOND START WITH ENG 2 START SELECTOR IN BOTH. NORMAL START. T/S C/O IAW FIM 74-00-00 FIG, 107 SH2. R & R ENG NR 2 EEC IAW AMM 73-21-15-4 . REPLACED BOTH IGNITOR PLUGS IAW AMM 74-21-02-4. C/O TEST IAW AMM 74-May 6, 2010 · N311UP · Boeing 76734AF · Engine ControlsSDR IPXA10658726Seal · deformedATB - STATUS MESSAGE LANDING GEAR MONITOR APPEARED DURING CLIMB-OUT. RETURNED TO MIA. C/W FIM 32-61-00 FIG 104. FOUND PSEU FAULT CODE 234 AND 235. FOUND LONGITUDINAL SEALS ON BOTH DOORS DEFORMED AND INTERFERING WITH DOOR CLOSING. ACCOMPLISHED BLOCK 1 OF FMar 5, 2010 · N311UP · Boeing 76734AF · Landing Gear DoorsSDR IPXA10658412Floor Panel · damagedMAIN DECK FLOOR PANEL POS 9L HAS DAMAGE 3/4" BY 1/2" GOUGE THROUGH UPPER SKIN ONLY. REPAIRED IAW EO B767-5320-9693-G.Feb 6, 2010 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657910Wedge · damagedLEFT O/B FLAP T/E WEDGE DAMAGED. REPAIRED PER EO B767-5750-35546-A.Nov 9, 2009 · N311UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09657321Fairing · delaminatedINSPECTION TYPE:C RT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.Sep 7, 2009 · N311UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09657382Fitting · crackedINSPECTION TYPE:C LT WING L/E LES 548 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP FOUND CRACK. CRACK LENGTH 0.375 INCH. LT WING L/E LES 548 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-4Sep 4, 2009 · N311UP · Boeing 76734AF · Wing SparSDR IPXA09657334Attach Fitting · crackedINSPECTION TYPE:C NR 1 PYLON MID SPAR ATTACH CLIP AT RT NAC STA 285.45 FOUND CRACK. CRACK LENGTH 0.5 INCH. NR 1 PYLON MID SPAR ATTACH CLIP AT RT NAC STA 285.45 REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.Sep 4, 2009 · N311UP · Boeing 76734AF · Nacelle/Pylon, Frame/Spar/RibSDR IPXA09657333Wedge · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP TRAILING EDGE WEDGE I/B AREA UPPER SURFACE, THE EXISTING REPAIR DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5A (1) FIG 9 REV 45.Sep 4, 2009 · N311UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09657332Wedge · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP TRAILING EDGE WEDGE I/B AREA LOWER SURFACE THE EXISTING REPAIR DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5G FIG 14 REV 45.Sep 4, 2009 · N311UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09657305Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGE AT STA 975 TO 1114, LBL 55 TO LBL 77. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 4, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657390Angle · crackedINSPECTION TYPE:C RT WING LT LES 155 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR ANGLE FOUND CRACK. CRACK LENGTH 1 INCH. RT WING - LT LES 155 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-Sep 3, 2009 · N311UP · Boeing 76734AF · Wing SparSDR IPXA09657361Support Fitting · crackedINSPECTION TYPE:C AFT CARGO STA 1087 LBL 25 FLOOR PANEL SUPPORT CLIP FOUND CRACK. CRACK LENGTH 1 INCH. AFT CARGO STA 1087 LBL 25 FLOOR PANEL SUPPORT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.Sep 3, 2009 · N311UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657360Support Fitting · crackedINSPECTION TYPE:C AFT CARGO COMPT STA 1087 RBL 25 FLOOR PNL SUPPORT CLIP FOUND CRACK. CRACK LENGTH 1 INCH. AFT CARGO STA 1087 RBL 25 FLOOR PANEL SUPPORT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.Sep 3, 2009 · N311UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657338Attach Angle · crackedINSPECTION TYPE:C MAIN DECK STA 1581 LEFT O/B FLOOR PANEL SUPPORT ATTACH ANGLE FOUND CRACK. CRACK LENGTH 1 INCH. MAIN DECK STA 1581 LEFT O/B FLOOR PANEL SUPPORT ATTACH ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.Sep 3, 2009 · N311UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657322Fairing · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP O/B LEADING EDGE FAIRING DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.Sep 3, 2009 · N311UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09657312Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 283 TO 412 , LBL 11 TO RBL 11. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 3, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657311Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 412 TO 540, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 3, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657310Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGE AT STA 412 TO 540 LBL 11 TO LBL 33. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 3, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657309Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 654+22 TO 690 LBL 77 TO LBL 88. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 3, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657308Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 731 TO 833 LBL 55 TO LBL 77. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 3, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657307Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 875 TO 932, LBL 77 TO LBL 88. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 3, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657306Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1480 TO 1598, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 3, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657381Angle · crackedINSPECTION TYPE:C LT WING L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR ANGLE FOUND CRACK. CRACK LENGTH 0.5 INCH. LT WING L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-4Sep 2, 2009 · N311UP · Boeing 76734AF · Wing SparSDR IPXA09657380Skin · misrepairedINSPECTION TYPE:C SURVEY SEQ 311-W3-01 LT WING NR 4 SLAT OUTER SKIN L/E 42 INCHES FROM O/B EDGE EXISTING REPAIR DOES NOT CORRELATED TO A SRM. LEFT WING NR 4 SLAT NOSE SKIN BETWEEN OSS 638 TO OSS 645 REPAIRED AS PER UPS EO B767-5750-34944-A AND HX RS R57-43-36Sep 2, 2009 · N311UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657368Skin · misrepairedINSPECTION TYPE:C SURVEY SEQ 311-F1-02 FX SKIN REPAIR BETWEEN BS 1836 TO 1850 LBL 7 TO LBL 15 AREA. EXISTING REPAIR DOES NOT CORRELATE TO A SRM. FX SKIN REPAIR BETWEEN BS 1836-1850 LBL 7 TO LBL 15 AREA INCORRECT TYPE OF FASTENERS REPAIRED (REPLACED) PER HX RSep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA09657337Angle · crackedINSPECTION TYPE:C MEC COMPT FLOORBEAM STA 246 ANGLE FOUND CRACKED AT LBL 25. CRACK LENGTH 0.75 INCH. MEC COMPT FLOORBEAM STA 246 ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45 JUST AT LBL 25.Sep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657336Fitting · crackedINSPECTION TYPE:C MEC COMPT STA 246 FLOORBEAM CLIP FOUND CRACK AT RBL 10. CRACK LENGTH 1.5 INCH. MEC COMPT STA 246 FLOORBEAM CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45 JUST AT RBL 10.Sep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657335Fitting · crackedINSPECTION TYPE:C MEC COMPT STA 246 FLOORBEAM CLIP FOUND CRACK JUST AT LBL 50. CRACK LENGTH 1 INCH. MEC COMPT STA 246 FLOORBEAM CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45 JUST AT LBL 50.Sep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657320Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 540 TO 654+22, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657319Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 833 TO 930 LBL 11 TO RBL 11. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657318Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 412 TO 550 LBL 77 TO LBL 88. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657317Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1344 TO 1480, LBL 33 TO LBL 55. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657316Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1425 TO 1540, LBL 55 TO LBL 77. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657315Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1480 TO 1598 , RBL 11 TO RBL 33. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657314Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1207 TO 1344, RBL 33 TO RBL 55. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657313Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 731 TO 833, LBL 33 TO LBL 55. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Sep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657304Skin · crackedINSPECTION TYPE:C LT WING - NR 4 SLAT I/B NOSE SKIN AT I/B SUPPORT WEB RIVET HOLE FOUND CRACK. CRACK LENGTH 0.125 INCH. LT WING - NR 4 SLAT I/B NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45 JUST AT OSS 573.25. THIS IS CLASSIFIED A MAJOR REPAIR WSep 2, 2009 · N311UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657303Skin · crackedINSPECTION TYPE:C RT WING - NR 9 SLAT O/B NOSE SKIN AFT O/B SUPPORT WEB RIVET HOLE FOUND CRACKED. CRACK LENGTH 0.125 INCH. RT WING - NR 9 SLAT O/B NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45 JUST AT OSS 641.62 INCH. THIS IS CLASSIFIED AS A MAJSep 2, 2009 · N311UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657302Skin · crackedINSPECTION TYPE:C RT WING - NR 9 SLAT I/B NOSE SKIN AT I/B SUPPORT WEB RIVET HOLE FOUND CRACKED (CRACK LENGTH 0.125 INCH). RT WING NR 9 SLAT I/B NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45 JUST AT OSS573.25". THIS IS CLASSIFIED A MAJOR REPAIR WSep 2, 2009 · N311UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657298Stiffener · crackedINSPECTION TYPE:C MEC COMPT STA 246 FLOORBEAM STIFFENER FOUND CRACK AT LBL 40 ( CRACK LENGTH 1.125" ). MEC COMPT STA 246 FLOORBEAM STIFFENER REPAIRED AS PER SRM 53-10-51- 2R4 FIG 201 AT LBL 40. THIS IS CLASSIFIED A MAJOR REPAIR WITH MATERIAL 7075T6-0063. RESep 2, 2009 · N311UP · Boeing 76734AF · Fuselage Main, Floor Beam
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