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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR IPXA2014063083445Floor Panel · damagedHOLE IN MAIN CARGO DECK FLOOR PANEL POS 2R. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-H.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR IPXA3680083Floor Panel · puncturedFLOOR PANEL HAS 1.5" X 1" PUNCTURE THRU FACE SHEET. REPAIRED IAW SRM 53-00-50-2R.SDR IPXA3679550Skin · dentedDENT IN FUSELAGE SKIN, BETWEEN STA 1395 - 1417 AND S28-29L. REPAIR IAW EO B767-5330-51604-A.SDR IPXA3679549Intercostal · damagedINTERCOSTAL DAMAGED, BETWEEN BS 1395-1417, S28-29L. FABRICATE IAW EO B767-531051605A.SDR 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.SDR 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 & RSDR 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-SDR 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.SDR 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.SDR 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, ORIGINSDR 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 2024T351-0SDR 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 SDR 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 2024SDR 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 REISDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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-SDR 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.SDR IPXA1670781Floor Panel · damagedMAIN CARGO COMP POS 9/10 L OTBD MOST FLOOR PNL DAMAGED. FABRICATED FLOOR PANEL IAW EO B767-5320-9639.SDR IPXA1670780Floor Panel · damagedMCD FLOOR PANEL POS 4R HAS .25" HOLE RBL 49 STA 662. REPAIRED IAW SRM 53-00-50-2R.SDR IPXA1670779Floor Panel · damagedMCD FLOOR PANEL POS NR 8L HAS .5" HOLE LBL 81 STA 1012. REPAIRED IAW SRM 53-00-50-2R.SDR IPXA1670778Floor Panel · damagedMCD FLOOR PANEL BS 1368 LBL 4.5 HAVE .5" REPAIRED IAW SRM 53-00-50-2R.SDR IPXA1670777Floor Panel · damagedFLOOR PANEL POS NR 14 HAS 1.25" HOLE, RBL 49, BS 1531. REPAIRED IAW SRM 53-00-50-2R.SDR IPXA1670467Floor Panel · damagedMCD FLOOR PANEL POS 9L OTBD HAS HOLE. REPAIRED IAW SRM 53-00-50-2R.SDR IPXA1670466Floor Panel · puncturedMCD FLOOR PANEL POS 2C HAS PUNCTURES. REPAIRED IAW SRM 53-00-50-2R.SDR IPXA1670465Floor Panel · puncturedFLOOR PANEL POS 2C HAS PUNCTURES. REPAIR IAW SRM 53-00-50-2R.SDR IPXA1670464Floor Panel · damagedFLOOR PANEL HAS PUNCTURE, POS 2C REPAIRED IAW SRM 53-00-50-2R.SDR IPXA1670463Floor Panel · damagedDAMAGE TO FLOOR PANEL POS 11R OTBD SIDE. REPAIRED IAW SRM 53-00-50-2R.SDR 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.SDR IPXA1667945Floor Panel · damagedPOS 6R HAS FLOOR PANEL DAMAGED. REPAIRED REF EO B767-5320-9693-H.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.
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