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 IPXA2016022299695Floor Panel · damagedFLOOR PANEL BS 536 TO 632 DAMAGE. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693I.Feb 22, 2016 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2016022199678Floor Panel · not reportedFLOOR PANEL BS 6382 - 684. FABRICATED A NEW FLOOR PANEL IAW EOB767-5320-9693-I.Feb 21, 2016 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2015063090674Container · tornLIFE VEST BAG IS TORN ON RT SUPERNUMERY SEAT POSITION. INSTALLED A NEW VEST IN RT SUPERNUMERY POSITION IAW MM 25-62-00-001.Jun 30, 2015 · N310UP · Boeing 76734AF · Life JacketSDR IPXA2015063090673Life Vest · damagedLIFE VEST BAG IS TORN ON LT SUPERNUMERY SEAT POSITION INSTALLED NEW VEST IN LT SUPERNUMERY POSITION, PN OFF P01074-101, REF M/M 25-62-00-001.Jun 30, 2015 · N310UP · Boeing 76734AF · Life JacketSDR IPXA2015050988864Skin · crackedINSPECTION TYPE: C10, 1.8" CRACK WAS FOUND ON INBD SIDE SKIN AND DOUBLER OF NR 2 ENG PYLON BETWEEN NAC 221 TO 237. REPAIR IAW SR 3-3241385369 AND EO B767-5430-57387-A.Apr 30, 2015 · N310UP · Boeing 76734AF · Nacelle/Pylon, Plate/SkinSDR IPXA2015050988870Skin · debondedINSPECTION TYPE: C10, DISBOND DAMAGE ON RT WING INBD AFT FLAP UPPER SKIN, AT IFS 112 REPAIR IAW SRM 57-53-01-2R-1, REPAIR 1 AND SRM 51-70-10-2R-4, REPAIR 4.Apr 30, 2015 · N310UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA2015050988869Skin · debondedINSPECTION TYPE: C10, DISBOND DAMAGE ON LT WING INBD AFT FLAP UPPER SKIN AT IFS 107. REPAIR IAW SRM 57-53-01-2R-1, REPAIR 1 AND SRM 51-70-10-2R-4, REPAIR 4.Apr 30, 2015 · N310UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA2015051088891Stringer · crackedINSPECTION TYPE: C10, A ONE INCH CRACK WAS FOUND ON THE STR 20L AT STA 1550. REPAIR IAW SR : 3-3241205710 AND EO B767-5310-57364-A.Apr 27, 2015 · N310UP · Boeing 76734AF · Fuselage Main, Longeron/StringerSDR IPXA2015051088890Stringer · crackedINSPECTION TYPE: C10, CRACK FOUR INCH WAS FOUND ON THE STR 20R AT FS 1550. REPAIR IAW SR3-3239361352 AND EO B767-5310-57363-A.Apr 27, 2015 · N310UP · Boeing 76734AF · Fuselage Main, Longeron/StringerSDR IPXA2014112184911Actuator · leakingMAIN CONTROLLER QTY DECREASE .12, SYSTEM DEPRESSURIZED. FLUID LOSS OF CONTROLLER HYDRAULIC SYS, LEAK STOPPED. R & R RT LCCA. OPS CHECK GOOD IAW AMM 22-13-03-004-035 AND 22-13-03-404-046. MCDP GROUND TEST, 07 CHECKS GOOD IAW AMM 22-00-02-201.Nov 20, 2014 · N310UP · Boeing 76734AF · Hydraulic System, MainSDR IPXA2014102984727Transceiver · inoperativeINAUDIBLE TO TRANSMIT ON BOTH HF RADIOS. MIC SELECTORS WOULD NOT WORK AT ALL PILOT STATIONS AND OBSERVER SEAT. REPLACED LT HF TRANCEIVER IAW AMM 23-11-03-401. SYS OPS CHECKED NORMAL IAW AMM 23-11-00.Oct 28, 2014 · N310UP · Boeing 76734AF · HF Communications SystemSDR IPXA2014091784310Channel · damagedESCAPE AFT RETENSION CHANNEL DISTORTED AND DAMAGED. REPLACED CHANNEL.Sep 15, 2014 · N310UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2014082084023O-Ring · leakingC HYD QTY EICAS MESSAGE FOLLOWED BY A C HYD PRESSURE EICAS MESSAGE. PERFORMED CHECKLIST AND RETURNED TO DEPARTURE FOR A FLAPS 20 LANDING. EMERGENCY DECLARED. SERVICED CTR SYS HYD. PERFORMED LEAK CHECK ON CTR SYS HYD. FOUND LEAKING AT THE LCCA FILTER COVER.Aug 18, 2014 · N310UP · Boeing 76734AF · Hydraulic System, MainSDR IPXA2013100900517Spring · brokenDUE TO ABNORMAL PITCH RESPONSE VS CONTROL INPUT. ROUND SPRINGS 690, IAW CMM 27-31-09, BROKEN ON EICU FEEL UNIT. R &R SPRING IAW CMM. SYS TEST CHECKED GOOD IAW AMM 27-31-00-825-060, PAR 3, STEP B.Oct 6, 2013 · N310UP · Boeing 76734AF · Elevator Control SystemSDR IPXA3680409Skin · dentedNR 3 SLAT T/E SKIN DENTED 144 INCHES FROM OTBD EDGE. REPAIR IAW EO B767-5750-52263-A.Sep 29, 2013 · N310UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA3680402Skin · damagedNR 5 SLAT DENTED ON T/E WEDGE LOCATED 84 INCHES FROM OTBD EDGE AND 4.5 INCHES FROM T/E. REPAIRED IAW SRM 51-70-10-2R.Sep 29, 2013 · N310UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA3680399Skin · damagedNR 1 L/E SLAT HAS 1" CUTOUT IN UPPER SKIN OF T/E WEDGE LOCATED 83.25" FROM INBD EDGE 7.5" FROM T/E REPAIRED IAW EO-B767-5750-52279-A.Sep 29, 2013 · N310UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA3680184Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.Sep 9, 2013 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA13677934Floor Panel · damagedINSPECTION TYPE:C9, FOUND TWO HOLES ON MAIN DECK CARGO FLOOR PANEL AT BS 453, RBL 83.5. REPAIRED IAW EO NR B767-5320-9693-H.Apr 18, 2013 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA13677933Floor Panel · damagedINSPECTION TYPE:C9, FOUND TWO HOLES ON MAIN DECK CARGO FLOOR PANEL AT BS 630, RBL 83.5. REPAIRED IAW EO NR B767-5320-9693-H.Apr 18, 2013 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA13673310Wedge · dentedLT INBD AFT FLAP T/E WEDGE DENTED.Jan 6, 2013 · N310UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA13676609Skin · damagedRT OTBD ELEVATOR T/E HAS DAMAGE.Jan 6, 2013 · N310UP · Boeing 76734AF · Elevator, Plate/SkinSDR IPXA2676465Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL 12R DAMAGED. REPAIRED IAW SRM 53-00-50-2R.Dec 15, 2012 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2676464Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL POS8 DAMAGED. REPAIRED IAW SRM53-00-50-2R.Dec 15, 2012 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2676413Floor Panel · dentedMAIN CARGO DECK FLOOR PANEL POS NR 2R DAMAGED. FABRICATED NEW PANEL IAW EO 767-5320-9693-H.Dec 9, 2012 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2676412Floor Panel · damagedPOS NR 14 FLOOR PANEL HAS .250" PUNCTURE 146T5869-43. REPAIRED IAW SRM 53-000-50-2R.Dec 9, 2012 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2676411Floor Panel · damagedPOS NR 10 MAIN CARGO DECK FLOOR PANEL BS 1210 HAS .250" PUNCTURE 146T5869-52. REPAIR IAW SRM 53-00-50-2R.Dec 9, 2012 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2676410Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL POS 11L FWD 3RD FROM OTBD HAS HOLE. REPAIRED REF SRM 53-00-50-2R.Dec 9, 2012 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA12676227Floorboard · puncturedMAIN DECK FLOORBOARD DAMAGED AT POS 3R OTBD. FABRICATED NEW FLOORBOARD IAW B767-5320-9693-H.Nov 12, 2012 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA12676226Floorboard · puncturedMAIN DECK FLOORBOARD DAMAGED. FABRICATE NEW FLOORBOARD IAW SREO B767-5320-9693-H-B.Nov 12, 2012 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2675127Floor Panel · damagedFLOOR PANEL POS 9R FWD HAS HOLE LESS 3 IN PANEL IS FROM POS 9R, FABRICATED REPLACMENT FLOOR PANEL IAW EO B767-5320-9693H.Sep 1, 2012 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2675126Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL AT POS 10R FWD OTBD HAS 2 GOUGES AND DENTS. FABRICATED REPLACMENT FLOOR PANEL IAW EO B767-5320-9693H.Sep 1, 2012 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2675125Floor Panel · gougedMAIN CARGO DECK FLOOR PANEL AT POS 14 SECOND PANEL FROM L/E LT HAS 2 GOUGES. FABRICATED REPLACEMENT FLOOR PANEL IAW EO B767-5320-9693H.Sep 1, 2012 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2675124Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL AT POS 8, LT OTBD HAS A HOLE IDENTIFED PANEL FROM POS 8 LT OTBD. FABRICATED REPLACMENT FLOOR PANEL IAW EO B767-5320-9693H.Sep 1, 2012 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2673923Floor Panel · damagedMAIN CARGO FLOOR PANEL DAMAGED. FABRICATED FLOOR PANEL IAW EO B767-5320-96930H AND REPLACED.Jun 10, 2012 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2673922Floor Panel · damagedMAIN CARGO FLOOR PANEL DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H AND REPLACED.Jun 10, 2012 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11667216Failsafe · crackedINSPECTION TYPE:8C, FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP CRACK FOUND RUNNING FWD AND AFT. FX BS 955 RHS REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP REPAIR IAW EO B767-5350-17922-H, APP D, ORG MATERIAL IS 2024T351-0.750" MACHIJun 1, 2011 · N310UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA11667215Failsafe · damagedINSPECTION TYPE:8C, DURING ACCOMPLISH EO B767-5350-17922-H, BS 955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP INSPECTION, A FASTENER HOLE WAS FOUND WHICH LARGER THAN EO CALL OUT AT LT SIDE. FX BS955 LT SIDE NEAR STR-23L REAR SPAR BULKHEAD SIDE FITTING FAJun 1, 2011 · N310UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA11667214Tee Fitting · crackedINSPECTION TYPE:8C, FUSELAGE LT BS 955 REAR SPAR B/H SIDE FITTING, TEE FITTING FOUND CRACKED. FUSELAGE LT BS 955, REAR SPAR B/H SIDE FITTING, TEE FITTING REPLACED AND INSTALLED IAW EO B767-5350-17922-H, APP C, ORG MATERIAL IS 7075-T73 DIE FORGING, THIS REPAIRJun 1, 2011 · N310UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA11667213Tee Fitting · crackedFUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FITTING, TEE FITTING FOUND CRACKED. FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FITTING, TEE FITTING REPLACED AND INSTALLED IAW EO B767-5350-17922-H, APPEND D, ORG. MATERIAL IS 7075-T73 DIE FORGING, THIS REPAIR IS CLJun 1, 2011 · N310UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA11667209Skin · corrodedINSPECTION TYPE:8C, FUSELAGE LT BS 955 BULKHEAD SIDE FTG - A SLIGHT CORROSION IS FOUND AFTER FAIL SAFE STRAP TRIMMED OFF AT THE INTERNAL SURFACE OF THE SKIN IN THE AREA WHERE THE TEE FITTING TO THE FAIL SAFE STRAP AREA. FX LT BS 955 BULKHEAD SIDE FITTING, A SJun 1, 2011 · N310UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA11667208Bulkhead · corrodedINSPECTION TYPE:8C, FUSELAGE RT BS 955 BULKHEAD SIDE FITTING - A SLIGHTLY CORROSION IS FOUND AFTER FAIL SAFE STRAP TRIMMED OFF AT THE INTERNAL SURFACE OF THE SKIN IN THE AREA WHERE THE T-FITTING TO FAIL SAFE STRAP AREA. REMOVED IAW SRM 51-10-02 & REPROTECTED Jun 1, 2011 · N310UP · Boeing 76734AF · Fuselage Main, BulkheadSDR IPXA1667089Fairing · delaminatedINSPECTION TYPE:C, RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION AT MID AREA. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A (1) FIG 5, REV 50.Jun 1, 2011 · N310UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA1667093Fairing · delaminatedINSPECTION TYPE:C, RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION AT OTBD AREA. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A(1) FIG 5, REV 50.May 30, 2011 · N310UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA1667092Wedge · crackedINSPECTION TYPE:C, LT WING OTBD T/E FLAP T/E WEDGE INBD END CAP CRACKED FIBERGLASS. WET LAY UP REPAIR CARRIED OUT IAW RS NR R-57-50-37100 REV A, REFER EO NR B767-5750-42998-A.May 30, 2011 · N310UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA1667090Fairing · delaminatedINSPECTION TYPE:C, LT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A(1) FIG 5, REV 50.May 30, 2011 · N310UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA11667147Wedge · damagedINSPECTION TYPE:8C, RT WING - NR 8 SLAT UPPER WEDGE, LWR SURFACE AT MID AREA FOUND DAMAGED. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 200, SHEET 8, REV 50.May 29, 2011 · N310UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA11667148Panel · delaminatedINSPECTION TYPE:8C, VERTICAL STAB LT FSS 11.787 TO 92.250 FIXED PANEL FOUND DELAMINATION. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 202, SHEET 3, REV 50.May 27, 2011 · N310UP · Boeing 76734AF · Vertical Stabilizer, Plate/SkinSDR IPXA11667120Panel · crackedINSPECTION TYPE:C, RT WING NR 7 SLAT LWR CLOSURE PANEL CRACKED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW ARM 51-70-07, PAR 5H, FIG 15, REV 50.May 27, 2011 · N310UP · Boeing 767300 · Leading Edge DevicesSDR IPXA1667067Floor Panel · crackedINSPECTION TYPE:8C, MCD FLOOR PANEL FOUND 2 CRACKS AND 5 DENT MARKS AT STA 1041 TO STA 1114, LBL 33 TO LBL 55. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALL IAW AMM 53-01-06.May 27, 2011 · N310UP · Boeing 76734AF · Fuselage Floor Panel
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