N320UP

Service difficulty reports · 185

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 = 'N320UP' 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 IPXA2014063083445Floor Panel · damagedHOLE IN MAIN CARGO DECK FLOOR PANEL POS 2R. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-H.Jun 29, 2014 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2014052383020Clamp · looseRT ENGINE BLEED DUCT LEAK. TIGHTENED NR 2 BLEED INTERCONNECT DUCT CLAMPS IAW AMM 36-11-01-401, TASK 424-019-001, PAR F, SUB PAR 4. PERFORMED ENGINE GRAD RUN, N1=50 PERCENT, N2=88.4 PERCENT. NO DUCT LEAK INDICATION, LIGHT AND EICAS, OK FOR SERVICE.May 20, 2014 · N320UP · Boeing 76734AF · Engine Bleed Air SystemSDR IPXA2014051282925Skin · dentedDURING A C09 INSPECTION, FOUND A DENT ON LT SIDE FUSELAGE SKIN, BETWEEN BS 1491-1505, S29-30L. REPAIRED IAW SRM 53-00-01, REPAIR 14, REV 59.00.May 11, 2014 · N320UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA4682919Floor Panel · dentedDURING C09 INSPECTION, FOUND A DENT CARGO BAY FLOOR PANEL 231GFF, BETWEEN BS 533-654+22, LBL 11-33. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO 5320-9693-H.May 10, 2014 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2014051282924Floor Panel · scratchedDURING A C09 INSPECTION, FOUND A SCRATCH ON CARGO FLOOR PANEL 232LFF, BETWEEN BS 654+22-687, RBL 33-54.78. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO 5320-9693-H.May 10, 2014 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2014051282923Floor Panel · crackedDURING A C09 INSPECTION, FOUND A CRACK IN CARGO FLOOR PANEL 222DFF, BETWEEN BS 285-412, RBL 77.5-88.5. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO 5320-9693-H.May 10, 2014 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2014051282922Floor Panel · crackedDURING A C09 INSPECTION, FOUND A CRACK IN CARGO FLOOR PANEL 232SFF BETWEEN BS 687-764, RBL 77-88. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO NR 532-9693-H.May 10, 2014 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2014051282921Floor Panel · crackedDURING A C09 INSPECTION, FOUND A CRACK IN THE CARGO FLOOR PANEL 231HFF, BETWEEN BS 533-654+22, LBL 33-55. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO NR B767-5320-9693-H.May 10, 2014 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2014051282920Floor Panel · dentedDURING A C09 INSPECTION, CARGO FLOOR PANEL 251MFF FOUND DENTED BETWEEN BS 1208-1318, LBL 11- 33. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO 5320-9693-H.May 10, 2014 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2014051282918Floor Panel · scratchedDURING C09 INSPECTION, FOUND A SCRATCH ON CARGO FLOOR PANEL 251XFF BETWEEN LBL 54.75- 77. 50. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO NR 5320-9693-H.May 10, 2014 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2014051282917Floor Panel · dentedDURING C09 INSPECTION, CARGO FLOOR PANEL 251AGF FOUND DENTED BETWEEN BS 1480-1598.97 LBL 33-55. FABRICATED THE REPLACEMENT FLOOR PANEL IAW EO 5320-9693-H.May 10, 2014 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA3680083Floor Panel · puncturedFLOOR PANEL HAS 1.5" X 1" PUNCTURE THRU FACE SHEET. REPAIRED IAW SRM 53-00-50-2R.Sep 2, 2013 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA3679550Skin · dentedDENT IN FUSELAGE SKIN, BETWEEN STA 1395 - 1417 AND S28-29L. REPAIR IAW EO B767-5330-51604-A.Jul 30, 2013 · N320UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA3679549Intercostal · damagedINTERCOSTAL DAMAGED, BETWEEN BS 1395-1417, S28-29L. FABRICATE IAW EO B767-531051605A.Jul 30, 2013 · N320UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA12673071Skin · wornINSPECTION TYPE: 8C, EMPENNAGE RT LOWER AIR GATE FAIRING FWD CUTOUT FAIRING SKIN PANELS FOUND WORN. RT LOWER AIR GATE FAIRING FWD CUTOUT PANELS REPAIRED SRM 53-80-012R3 FIG 201, REV 52.Apr 13, 2012 · N320UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA2673135Skin · corrodedINSPECTION TYPE: 8C, FUSELAGE RT BS 955 BULKHEAD SIDE FITTING. SLIGHT CORROSION IS FOUND AFTER FAIL-SAFE STRAP TRIMMED OFF AT THE INTERNAL SURFACE OF THE SKIN IN THE AREA WHERE THE T-FITTING TO THE FAIL-SAFE STRAP AREA. CORROSION REMOVED IAW SRM 51-10-02 & RApr 12, 2012 · N320UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA2673130Fitting · corrodedINSPECTION TYPE: 8C, FUSELAGE LT 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 THE FAIL SAFE STRAP AREA. CORROSION REMOVED IAW SRM 51-10-Apr 12, 2012 · N320UP · Boeing 76734AF · Fuselage Main, BulkheadSDR IPXA12673052Hinge Fitting · crackedINSPECTION TYPE: 8C, RT WING INBD MAIN FLAP, INBD HINGE ARM FITTING FOUND CRACKED. RT WING INBD MAIN FLAP INBD HINGE ARM FITTING REPAIRED IAW SRM 57-53-02-2 REPAIR 1 FIG 201, REV 52.Apr 11, 2012 · N320UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA2673154Battery Pack · failedINSPECTION TYPE: 8C, EMERGENCY LIGHT DID NOT STAY ON FOR 15 MINS. EMERGENCY LIGHT BATTERY PACK REPLACED AND OPS TEST CARRIED OUT NORMAL, REF AMM 33-51-07.Apr 9, 2012 · N320UP · Boeing 76734AF · Emergency LightingSDR IPXA2673133Tee Fitting · crackedINSPECTION TYPE: 8C, FUSELAGE BS 955, S22AR CRACK WAS FOUND AT RT SIDE TEE FITTING AT 9 O`CLOCK POSITION .0625" APPROX. FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FITTING AREA TEE FITTING REPLACED AND INSTALLED IAW EO B767-5350-17922-J APPROX D, FIG 6, ORIGINApr 9, 2012 · N320UP · Boeing 76734AF · Fuselage Main, BulkheadSDR IPXA2673132Failsafe · crackedINSPECTION TYPE: 8C, FUSELAGE BS 955 S22AR CRACK WAS FOUND AT RT SIDE FAIL SAFE STRAP AT 9 O/C POSITION 0937" APPROX. FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FTG FAIL SAFE STRAP IS REPAIRED IAW EO B767-5350-17922-J APPX 'D', ORIGINAL MATERIAL IS 2024T351-0Apr 9, 2012 · N320UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA2673128Tee Fitting · crackedINSPECTION TYPE: 8C, FUSELAGE BS 955, S22LA CRACK WAS FOUND AT LT SIDE TEE FITTING AT 2 O/C POSITION 3/32" APPROX FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FTG AREA T-FITTING. REPLACED AND INSTALLED IAW EO B767-5350-17922-J APPX 'C' FIG 6, ORIGINAL MATERIAL Apr 9, 2012 · N320UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2673127Failsafe · crackedINSPECTION TYPE: 8C, FUSELAGE BS 955, S22LA CRACK WAS FOUND AT LT SIDE FAILSAFE STRAP AT 8 O`CLOCK POSITION .0937" APPROX. FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FTG FAIL SAFE STRAP IS REPAIRED IAW EO B767-5350-17922-J, APPROX C, ORIGINAL MATERIAL IS 2024Apr 9, 2012 · N320UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA2673126Bulkhead · crackedINSPECTION TYPE: 8C, FX - LT BS 955 REAR SPAR BULKHEAD SIDE FITTING 1 EA FASTENER HOLE FOUND CRACK INDICATION BY ULTRASONIC METHOD FURTHER INVESTIGATION REQUIRED. FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FITTING AT THE LOWER 3 FASTENERS ARE REMOVED AND REIApr 9, 2012 · N320UP · Boeing 76734AF · Fuselage Main, BulkheadSDR IPXA12673070Floor Panel · damagedINSPECTION TYPE: 8C, MAIN CARGO DECK FLOOR PANEL HAS NINE DENTS AND TWELVE PUNCTURES AT BS 412 TO 530, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.Apr 9, 2012 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA12673012Skin · crackedINSPECTION TYPE: 8C, RIGHT WING NR 8 SLAT SKIN CRACKED. REPAIRED IAW SRM 57-43-01-2R2, REPAIR 2, FIG 201, REV 52. REPAIR CLASSIFIED AS MAJOR.Apr 9, 2012 · N320UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA12673011Skin · crackedINSPECTION TYPE: 8C, LEFT WING NR 5 SLAT SKIN CRACKED. REPAIRED IAW SRM 57-43-01-2R2, REPAIR 2, FIG 201, REV 52. REPAIR CLASSIFIED AS MAJOR.Apr 9, 2012 · N320UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA12673010Skin · crackedINSPECTION TYPE: 8C, LEFT WING NR 4 SLAT SKIN CRACKED. REPAIRED IAW SRM 57-43-01-2R2, REPAIR 2, FIG 201, REV 52. REPAIR CLASSIFIED AS MAJOR.Apr 9, 2012 · N320UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA12673009Skin · crackedINSPECTION TYPE: 8C, LEFT WING NR 3 SLAT INBD NOSE SKIN CRACKED. REPAIRED IAW SRM 57-43-01-2R2. REPAIR 2, FIG 201, REV 52. REPAIR CLASSIFIED MAJOR.Apr 9, 2012 · N320UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA2673131Fitting · crackedINSPECTION TYPE: 8C, RT BS 955 REAR SPAR BULKHEAD SIDE FITTING 1 EA FASTENER HOLE FOUND CRACK INDICATION BY ULTRASONIC METHOD FURTHER INVESTIGATION REQUIRED. FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FITTING AT THE LOWER 3 FASTENERS ARE R & R IAW EO NO B767-Apr 8, 2012 · N320UP · Boeing 76734AF · Fuselage Main, BulkheadSDR IPXA2671283Bracket · inoperativeCAPT NR 2 SLIDING WINDOW LATCH HANDLE WILL NOT OPERATE WITHOUT DEPRESSING LATCH RELEASE BUTTON. R & R AFT STRIKER BRACKET ON CAPT NR 2 WINDOW IAW AMM 56-11-02-6. OPS CK OK.Jan 28, 2012 · N320UP · Boeing 76734AF · Flight Compartment WindowsSDR IPXA1670781Floor Panel · damagedMAIN CARGO COMP POS 9/10 L OTBD MOST FLOOR PNL DAMAGED. FABRICATED FLOOR PANEL IAW EO B767-5320-9639.Dec 25, 2011 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1670780Floor Panel · damagedMCD FLOOR PANEL POS 4R HAS .25" HOLE RBL 49 STA 662. REPAIRED IAW SRM 53-00-50-2R.Dec 25, 2011 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1670779Floor Panel · damagedMCD FLOOR PANEL POS NR 8L HAS .5" HOLE LBL 81 STA 1012. REPAIRED IAW SRM 53-00-50-2R.Dec 25, 2011 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1670778Floor Panel · damagedMCD FLOOR PANEL BS 1368 LBL 4.5 HAVE .5" REPAIRED IAW SRM 53-00-50-2R.Dec 25, 2011 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1670777Floor Panel · damagedFLOOR PANEL POS NR 14 HAS 1.25" HOLE, RBL 49, BS 1531. REPAIRED IAW SRM 53-00-50-2R.Dec 25, 2011 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1670467Floor Panel · damagedMCD FLOOR PANEL POS 9L OTBD HAS HOLE. REPAIRED IAW SRM 53-00-50-2R.Nov 27, 2011 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1670466Floor Panel · puncturedMCD FLOOR PANEL POS 2C HAS PUNCTURES. REPAIRED IAW SRM 53-00-50-2R.Nov 27, 2011 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1670465Floor Panel · puncturedFLOOR PANEL POS 2C HAS PUNCTURES. REPAIR IAW SRM 53-00-50-2R.Nov 27, 2011 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1670464Floor Panel · damagedFLOOR PANEL HAS PUNCTURE, POS 2C REPAIRED IAW SRM 53-00-50-2R.Nov 27, 2011 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1670463Floor Panel · damagedDAMAGE TO FLOOR PANEL POS 11R OTBD SIDE. REPAIRED IAW SRM 53-00-50-2R.Nov 27, 2011 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1670460Floor Panel · puncturedDECK FLOOR PANEL BS 749, RBL 39.0 HAS A 1.5 DIA DENT WITH PUNCTURE IN TO CORE. DAMAGE IS 1.5" DIA. REPAIRED IAW SRM 53-00-50-2R, 4D.Nov 27, 2011 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667945Floor Panel · damagedPOS 6R HAS FLOOR PANEL DAMAGED. REPAIRED REF EO B767-5320-9693-H.Jul 17, 2011 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667709Actuator · inoperativeRUDDER TRIM WOULD NOT MOVE RT WITH RUDDER TRIM KNOB. TRIM AT 1.5 LT FOR LANDING-AIR TURN BACK TO DEPARTURE T/S IAW FIM 27-21-00/101, FIG 100, FOUND RUDDER TRIM ACTUATOR WOULD NOT MOVE. R & R RUDDER TRIM ACTUATOR AND SYS OPS CHECK NORMAL IAW AMM 27-21-11-2.Jul 5, 2011 · N320UP · Boeing 76734AF · Rudder Tab Control SystemSDR IPXA10660572Floor Panel · puncturedINSPECTION TYPE:C, MCD STA 1114 TO 1197+22 LBL 11" TO 33" FLOOR PANEL 3 PUNCTURE AND TOGETHER WITH 7 DENT MARKS. MCD FLOOR PANEL FABRICTED IAW EO B767-5320-9693-G AND REPLACED IAW AMM 53-01-01.Jun 14, 2010 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10660604Fairing · delaminatedINSPECTION TYPE:C, RT 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 47.Jun 9, 2010 · N320UP · Boeing 76734AF · Wing Miscellaneous StructureSDR IPXA10660600Wedge · crackedINSPECTION TYPE:C, LT WING OTBD T/E FLAP T/E WEDGE INBD AREA LWR SURFACE CRACKED. FIBERGLASS PREPREG LAYUP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5G, FIG 14, REV 47.Jun 9, 2010 · N320UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10660607Floor Panel · puncturedINSPECTION TYPE:C, MCD STA412 TO 544 LBL 77 TO LBL 88 FLOOR PANEL FOUND 4 PUNCTURE HOLES TOGETHER WITH 6 DENT. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND REPLACED IAW AMM 53-01-01.Jun 8, 2010 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10660606Wedge · delaminatedINSPECTION TYPE:C, LT WING OTBD FLAP T/E LWR SURFACE AT 54.5" FROM OTBD EDGE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1) FIG 9, REV 47.Jun 8, 2010 · N320UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10660601Wedge · delaminatedINSPECTION TYPE:C, LT WING OTBD FLAP T/E LWR SURFACE AT 127" FROM OTBD EDGE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A (1) FIG 9, REV 47.Jun 8, 2010 · N320UP · Boeing 76734AF · Trailing Edge Flaps
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