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 IPXA10660599Floor Panel · puncturedINSPECTION TYPE:C, MCD STA1425 TO 1522, RBL55 TO RBL77, FLOOR PANEL FND 2 PUNCTURE HOLES AND 8 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & REPLACED IAW AMM 53-01-01.SDR IPXA10660598Floor Panel · puncturedINSPECTION TYPE:C, STA412 TO 544 LBL55 TO 77 MCD FLOOR PANEL FND PUNCTURE HOLES AND 5 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B77-5320-9693-G AND REPLACED IAW AMM 53-01-01.SDR IPXA10660577Floor Panel · damagedINSPECTION TYPE:C, MCD STA540 TO 654+22 LBL11 TO RBL11 FLOOR PANEL FND 6 DAMAGED AND 4 DENT MARKS. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND REPLACED IAW AMM 53-01-01.SDR IPXA10660576Floor Panel · puncturedINSPECTION TYPE:C, MCD STA 972 TO 1112, LBL 11 TO RBL 11, FLOOR PANEL FOUND 3 PUNCTURE HOLES AND TOGETHER WITH 6 DENT MARKS. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND REPLACED IAW AMM 53-01-01.SDR IPXA10660575Floor Panel · damagedINSPECTION TYPE:C, STA1207 TO 1351 RBL11 TO LBL11 FLOOR PANEL FND 3 DAMAGE AND 4 DENT MARKS. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND REPLACED IAW AMM 53-01-01.SDR IPXA10660574Floor Panel · puncturedINSPECTION TYPE:C, MCD STA 1197+22 TO 1207 LBL11 TO RBL11 FLOOR PANEL FND 5 PUNCTURE HOLES AND 5 DENTS. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND REPLACED IAW AMM 53-01-01.SDR IPXA10660573Floor Panel · damagedINSPECTION TYPE:C, MCD STA833 TO 930 RBL11 TO LBL11 FLOOR PANEL FND 6 DAMAGE AND TOGETHER WITH 5 DENT MARKS. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & REPLACED IAW AMM 53-01-01.SDR IPXA10660605Skin · crackedINSPECTION TYPE:C, LT WING NR 4 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT L/B OTBD NOSE SKIN AT OSS641.9 AREA SKIN REPAIRED IAW SRM 57-43-01-22R FIG 201, ORG MATL IS CLAD7075T6-0.063IN, CRK LENGTH 0.244", DAMAGED CUTOUT IS 8.875" X 7.25"SDR IPXA10660579Skin · delaminatedINSPECTION TYPE:C RUDDER SKIN SIDE UPPER AREA DELAMINATION. GRAPHITE FABRIC PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-04, PAR 5K, REV 47.SDR IPXA10660474Stiffener · crackedINSPECTION TYPE:C, FUS MEC COMPT STA 246 FLOORBEAM ATTACH STIFFENER FOUND CRACK AT LBL40". FUS MEC COMPT STA 246 FLOORBEAM ATTACH STIFFENER AT LBL 40" AREA REPAIRED IAW SRM 53-10-51-2R4, FIG 201, REV 47.SDR IPXA10659995Floor Panel · damagedD418763 MCD FLOOR PANEL DAMAGED AT POSITION 10L MFG AND INSTALLED IAW EO B767-4320-9693-G, POS 10L.SDR IPXA09657953Panel · delaminatedVERTICAL STAB AREA OF DELAMINATION, LEFT SIDE, FSS 195.39. REMOVED, REPAIRED AND INSTALLED PER SRM 51-40-02-OG, AND BOEING DWG 175T0000.SDR IPXA09657867Floorboard · damagedFLOORBOARD ON MCD CENTER POS 9 DAMAGED. FABRICATED FLOORBOARD PER EO B767-5320-9693-F.SDR IPXA09657746Floor Panel · damagedMCD FLOOR PANEL DAMAGED POS 9. REPAIRED PER EO B767-5320-9693-F.SDR IPXA09657121Floor Panel · misrepairedINSPECTION TYPE:N/A MCD POS 9 RT OUTBOARD FLOOR PANEL INTERIM REPAIR. FABRICATED FLOOR PANEL PER EO B767-5320-9693-F.SDR IPXA09656709Floor Panel · crackedINSPECTION TYPE:PS D399757 MCD POS 12 RT 2ND FROM O/B FLOOR PANEL INTERIM REPAIR PERMANENT REPAIR AT C-CHECK. REPLACED FLOOR PANEL PER EO B767-5320-9693-F.SDR IPXA09656708Floor Panel · damagedINSPECTION TYPE:PS D399756 MCD POS 9 AND 10 RT 2ND FROM O/B PANEL INTERIM REPAIR 1 HOLE .5 INCH DEEP 1.5 X 1 INCH 2-HOLES WITH CRACKS BOX APPX 1 INCH FWD AREA POS 10 SAME FLOOR PANEL. PERMANENT REPAIR AT C CHECK. REPLACED FLOOR PANEL PER EO B767-5320-9693-F.SDR UPS09654270Wedge · damagedINSPECTION TYPE: N/A INSTALL DOUBLER AND TRIPLER REF RCD 261 TO LWR SURFACE RT WING T/E WEDGE. C/W EO B767-5750-30772B.SDR UPS09654269Wedge · dentedINSPECTION TYPE:N/A RT INBOARD T/E FLAP WEDGE UPPER SURFACE HAS DENT. C/W EO B767-5750-30772B AND B767 SRM 57-53-01-2R TAP CHECK GOOD. PAINTED SEALED MAJOR REPAIR COMPLETE.SDR UPS08653245Seat Track · wornINSPECTION TYPE:C M/D STA 754 RBL 11 SEAT TRACK CROWN WORN. M/D - CARGO TRACK SECTIONAL REPLACED FROM STA 709 TO STA 785 RBL 11 AND REPAIRED AS PER SRM 53-00-52-2R REPAIR 9 FIG 201.SDR UPS08653243Stiffener · crackedINSPECTION TYPE:C FX- INTERNAL AREA STA 246 LBL 50 CABIN FLOORBEAM ATTACHMENT STIFFENER FOUND CRACK. CRACK LENGTH 0.75 INCH. FX- STA 246 LBL 50 CABIN FLOORBEAM ATTACHMENT STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.SDR UPS08652574Structure · damagedFWD PIT DOOR AFT EDGE DAMAGE.SDR UPS08652008Control Panel · defectiveINSPECTION TYPE:ETOP DIVERSION - UNABLE TO MAINTAIN CABIN PRESSURIZATION. REPLACED CABIN PRESSURE SELECTOR PANEL PER AMM 21-31-01-4. AUTO TEST AND MANUAL TEST NORMAL, NO FAULTS AT PRESSURE CONTROLLERS WITH REFERENCE TO FIM 21-31-00.SDR UPS09654402Floor Panel · puncturedINSPECTION TYPE:N/A FLOOR PANEL 3 PUNCTURES. REPAIRED PER EO B767-5320-31943-A.SDR UPS07650391Charger · malfunctionedINSPECTION TYPE:ETOP EICAS MSG MAIN BATTERY CHARGER DISPLAYED. BATTERY DISCHARGE LIGHT DID NOT ILLUMINATE. SWAPPED APU BATTERY CHARGER WITH MAIN BATTERY CHARGER IAW 24-31-02-4 & 24-31-05-4. MAIN BATTERY CHARGER OPS NORMAL.SDR UPS07649936Brake Assy · failedINSPECTION TYPE:ETOP TAXIING INTO EWR RAMP NR 5 BRAKE ASSY INTERNALLY FAILED CAUSING LOW LEVEL HYD FLUID FIRE DUE TO CRACKED PUCK ASSEMBLY. PERFORMED HIGH ENERGY STOP/HEAT DAMAGE CONDITION INSPECTION IAW MM REF 05-51-14-2, NO FIRE DAMAGE NOTED ON ALL ADJACENSDR UPS07649205Engine · bird ingestionINSPECTION TYPE:ETOP TSLV = 4514 - DIVERSION - POSSIBLE BIRD INGESTION THROUGH RIGHT ENGINE. THE CREW NOTICED AN UNUSUAL VIBRATION & REQUESTED TO SPEAK TO ACMX. DIVERTED TO SJO. PERFORMED FIM 71-05-00/101 AND REPLACED FAN BLADES 15-16-34 PER MM 72-00-00-6. SDR UPS06647394Flap · delaminatedFOUND RT I/B AFT FLAP HAS 3.5" DENT WITH DELAMINATED. REPAIRED IAW 51-20-10-2 AND 51-70-10-2R.SDR UPS06646419Window · delaminatedR2 WINDOW HAS 4 INCH AREA OF DELAMINATED ALONG UPPER EDGE. OK PER 767 MM 56-11-00-6 PG 1 ITEM 6F.SDR UPS06646139Fan · odorETOP FWD EQUIP EXHAUST FAN EICAS MSG, ELEC SMELL IN COCKPIT. FOUND CB H21 PANEL P6-4 TRIPPED. RESET CB, TRIPPED AGAIN. A/C RELEASED PER MEL 21-58-4-2-1. FAN ELECTRICALLY DISCONNECTED AND CB TAGGED. LP 532788 FUNCTION CK WAS SATIS. FOUND REMOVAL & INSTALLATIONSDR UPS03641656Door · inoperativeMAIN CABIN DOOR INOPERABLE.SDR UPS02639987Connector · leakingINFLIGHT SHUTDOWN DUE TO FUEL IMBALANCE RT ENGINE SHUT DOWN PER CHECKLIST RETURNED TO LOUISVILLE FUEL LEAKING INTERNALLY IN HMU AND COMING OUT BOTTOM CHANNEL A AND CHANNEL B CANNON PLUG PLATE. REMOVED HMU UP TO STEP 6 IAW M/M REF 73-21-14-4. INSTALLED HMU NRSDR UPS01636194Cap · looseINSPECTION TYPE:N/A INBOUND LOG WRITE UP: CENTER HYDRAULIC QUANTITY DECREASED TO .31. SYSTEM DEPRESSURIZED AND LEAK CONTINUED. SPOILER ACTUATOR PANEL NR 9, FOUND SAFETY WIRE ON CAP, PT 1542661 IPC REF 27-61-02-01 WAS BROKEN AND CAP WAS LOOSE. REMOVED AND SDR UPS00634408Placard · deterioratedINSPECTION TYPE:C, EMERGENCY EXIT MARKINGS OUTSIDE OF FIRST OFFICERS R2 SLIDING WINDOW HAS PULL DECAL DETERIORATED. FAA REQUIRED. INSPECTED DECAL AND FOUND REPLACEMENT DECAL (P/N BAC27N84-0059) ALREADY INSTALLED.SDR UPS97624658Pcu · leakingAIR TURN BACK-LOSS OF HYDRUALIC QUANTITY HYD QTY READS ZERO HYD QTY LGT ILLUM, EICAS MSG DISPLAYED L HYD QTY HYDRAULIC LOW PRESS ON. FOUND BROKEN PACKING ON RT ELEV PCU LEFT SYS. REPLACED PACKING LEAK CK'D RAN LEFT ENG CYCLED FLIGHT CONTROLS ALL SYSTEM'S CK
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