N454UP
Service difficulty reports · 250
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 = 'N454UP' 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 = 'N454UP' 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 IPXA10560089Wedge · chafedINSPECTION TYPE:C4, RT WING NR 8 SLAT T/E WEDGE LOWER SURFACE HAS CHAFING JUST ABOVE OTBD MAIN TRACK (FOUND TO BE OUT OF LIMITS ON CARD NR 861178) REPAIRED RT WING NR 8 SLAT T/E WEDGE LOWER SURFACE IAW SRM 51-70-10-2R
REPAIR 4.SDR IPXA10560067Floorbeam · corrodedINSPECTION TYPE:C4, CORROSION ON UPPER SURFACE OF FLOORBEAM UPPER CHORD COMMON TO 4EA FASTENER HOLES BS 1100 RBL 48 TO RBL 54 WL 207. ENTIRE UPPER CHORD OF BS 1100 TRANVERSER FLOORBEAM WILL BE R & R ON CUST ID NR 861458.SDR IPXA10560066Floorbeam · corrodedINSPECTION TYPE:C4, 6EA NUTPLATES CORRODED ON TRANSVERSE FLOORBEAM AT BS 1100 LBL 45-62. REMOVED 6EA NUTPLATES FROM FLOORBEAM, BLENDED CORROSION., NOTE. THE ENTIRE UPPER CHORD OF BS 1100 TRANVERSE FLOORBEAM WILL BE R & R ON CUST ID 861458.SDR IPXA10560065Floorbeam · corrodedINSPECTION TYPE:C4, TRANSVERSE FLOORBEAM UPPER CHORD FLANGE IS CORRODED AT BS 1100 LBL 0-25, WL 208. ENTIRE UPPER CHORD OF BS 1100 TRANVERSER FLOORBEAM WILL BE R & R ON CUST. ID 861458.SDR IPXA10560036Frame · damagedINSPECTION TYPE:C4, MAIN CARGO DOOR INNER SURFACE, FRAME AT BS 482 BETWEEN STR 14-17 HAS S SCREW START. REMOVED GOUGE, NDI FOUND NO CRACKS, FOUND TO BE WITHIN LIMITS IAW SRM 52-30-02 DETAIL IV ALODINED & PRIMED.SDR IPXA10560010Floorboard · damagedINSPECTION TYPE:C4, MCB FLOORBOARD PANEL DAMAGED BS 1016-1055 LBL 45-62. FABRICATED REPLACEMENT FLOOR PANEL.SDR IPXA10560009Floorboard · damagedINSPECTION TYPE:C4, DAMAGED FLOORBOARD AT 1100-1200 LBL 45-62. FABRICATED REPLACEMENT PANEL.SDR IPXA10560008Floor Panel · corrodedINSPECTION TYPE:C4, MAIN CARGO STA 1681.8 TO STA 1661 FLOOR PANEL HAVE 4 EA INSERTS CORRODED BL 0 TO RBL 24.75. FABRICATED REPLACEMENT PANEL.SDR IPXA10560007Floor Panel · corrodedINSPECTION TYPE:C4, MAIN CARGO STA 1420 TO STA 1540, LBL 45.5 TO LBL 60 FLOOR PANEL HAVE 8 EA INSERTS CORRODED FABRICATED REPLACEMENT PANEL.SDR IPXA10560006Floorboard · dentedINSPECTION TYPE:C4, MCB FLOORBOARD PANEL DENTED BS 900-1016 LBL 45-62. FABRICATED REPLACEMENT PANEL.SDR IPXA10560005Floorboard · damagedINSPECTION TYPE:C4 MCB FLOORBOARD PANEL DAMAGED BS 1055-1100 LBL 45-62. FABRICATED REPLACEMENT PANEL.SDR IPXA10559979Stringer Clip · corrodedINSPECTION TYPE:C4, CORROSION ON STRINGER CLIP B/S 620 STRINGER 5R. FABRICATED AND REPLACED STRINGER CLIP B/S 620, STRINGER 5R.SDR IPXA10560503Stanchion · crackedINSPECTION TYPE:C4, BULK CARGO COMPARTMENT (LT) UPPER SIDEWALL SUPPORT STANCHION IS CRACKED AT UPPER FWD STA 1560. R & R WITH REPLACEMENT PART IAW DWG NR 453N1662.SDR IPXA10560443Frame · damagedINSPECTION TYPE:C4, SCREW STRIKE ON FRAME FLANGE AT BS 418 BETWEEN S-15R AND S-16R. REPAIRED IAW ATS ER 10-2850.SDR IPXA10560440Frame · damagedINSPECTION TYPE:C4, SCREW STRIKE ON FRAME FLANGE AT BS 365.25 BETWEEN S-15L AND S-16L. REPAIRED IAW ATS ER 10-2848.SDR IPXA10560409Frame · damagedINSPECTION TYPE:C4, SCREW STRIKE ON FRAME FLANGE AT BS 365.25 BETWEEN S-15R AND S-16R. BLENDED DAMAGE AND RE-FINISHED IAW ER 10-2846.SDR IPXA10560343Skin · puncturedINSPECTION TYPE:C4, RT WING AILERON LWR SURFACE PUNCTURED JUST INBD OF 2ND FROM OTBD STATIC WICK. RT WING AILERON LWR SURFACE WAS REPLACED IAW SRM 51-70-04 AND SRM 51-60-01-OG.SDR IPXA10560267Support · corrodedINSPECTION TYPE:C4 BULK CARGO BAY FLOOR TO SIDEWALL HAS 4 CORRODED NUT PLATES BETWEEN SPLICE STATION 1410 TO 1530 LBL17 AND 19. SIDE WALL SUPPORT WAS REPLACED IAW SRM 51-40-02-GSDR IPXA10560265Cargo Track · gougedINSPECTION TYPE:C4 THE MAIN CARGO FLOOR TRACK HAS TWO GOUGES AT BS534 AND BS537 LBL62 WL208. FLOOR TRACK SECTION WAS REPLACED PER SRM 51-40-02-GSDR IPXA10560171Support · corrodedINSPECTION TYPE:C4, AFT CARGO BAY; FLOOR TO SIDEWALL SUPPORT HAS CORROSION AROUND CARGO TIE-DOWN FITTING, STA 1320 AND 1340, RBL 20. R & R FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G, SRM 53-60-53-0I, SRM 51-10-02.SDR IPXA10560163Support · corrodedINSPECTION TYPE:C, BULK CARGO BAY; FLOOR TO SIDEWALL SUPPORT HAS CORRODED NUTPLATE. R & R FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-OG, SRM 51-10-02.SDR IPXA10560156Support · corrodedINSPECTION TYPE:C4, AFT CARGO BAY; FLOOR TO SIDE WALL SUPPORT HAS CORROSION AROUND CARGO TIE-DOWN FITTING, STATION 1300, RBL 20. REPLACED FLOOR TO SIDE WALL SUPPORT IAW SRM 51-40-02-0G AND EO B757-5310-32833-A.SDR IPXA10560154Support · corrodedINSPECTION TYPE:C4, AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AROUND NUMEROUS NUTPLATES STA 1340 AND 1380 RBL 19. FOUND TO BE OUT OF REPAIRABLE LIMITS IAW SRM 53-0053-1A1. ENTIRE SECTION OF FLOOR TO SIDEWALL SUPPORT WILL BE REPLACED ON CUSTOMER CASDR IPXA10560119Floorboard · damagedINSPECTION TYPE:C4, CREW COMPARTMENT UPPER FLOORBOARD HAS MULTIPLE AREAS OF DAMAGE ON EDGE, A PUNCTURE, CORROSION ON INSERTS REPLACED IAW EO B757-5320-9692.SDR IPXA10560064Floor Support · corrodedINSPECTION TYPE:C4, BULK CARGO BAY; FLOOR PANEL SUPPORT HAS 2 EA CORRODED NUTPLATES, STA 1469, AND 1470, LBL 16. 10. REMOVE NUTPLATES; REMOVED CORROSION FROM SUPPORT. FOUND TO BE OUT OF LIMITS, ORDERED AND RECEIVED NEW FLOOR SUPPORT LOCATED AND INSTALLED IASDR IPXA10560035Intercostal · corrodedINSPECTION TYPE:C4, CREW ENTRY DOOR AREA INTERCOSTAL BELOW DRAIN PAN HAS CORROSION AT NUTPLATES. REMOVED CORROSION FROM PART - FOUND TO BE WITHIN REPAIRABLE LIMITS IAW SRM 53-00-51. ALODINED & PRIMED REWORK AREA IAW AMM 51-21-04-7.SDR IPXA10560012Support · corrodedINSPECTION TYPE:C4, BULK CARGO COMPARTMENT; CEILING PANEL SUPPORT STRAP IS CORRODED, STA 1623, BL 0. REMOVED AND FABRICATED NEW CEILING PANEL SUPPORT STRAP IAW DWG 453N1802 REV A, AND SRM 51-30-01-0G.SDR IPXA10560511Pan · corrodedINSPECTION TYPE:C4, PLATE ON TOP OF LAV PAN INSIDE FUSELAGE IS CORRODED AT BS354-361 BETWEEN S-21R AND S-23R. REPLACED PART SRM 51-40-02.SDR IPXA10560424Frame · gougedINSPECTION TYPE:C4, MAIN CABIN STA 1540 BETWEEN S-15L TO S16L HAVE FRAME GOUGED 2 EA LOCATION. REPAIRED IAW ATS ER 10-2790.SDR IPXA10560378Frame · gougedINSPECTION TYPE:C4, MAIN CABIN STA 1320 BETWEENS-15L TO S-16L FRAME GOUGED 1EA LOCATION. REPAIR IAW ATS ER 10-2791.SDR IPXA10560370Skin · corrodedINSPECTION TYPE:C4, CORROSION ON NR 1 PYLON SKIN EXTERIOR SURFACE RT SIDE 6" AFT OF NR1 PYLON ACCESS PANEL NR433GR. DAMAGE CLEANUP BEYOND ALLOWABLE LIMITS CUTOUT DAMAGED SKIN AND INSTALLER RE-INFORCEMENT DOUBLER.SDR IPXA10560062Angle · crackedINSPECTION TYPE:C4, WHILE ACCESSING, FOUND UPPER L-ANGLE ON WEB AT BS 483, RBL 10 TO BE CRACKED. REMOVED CRACKED ANGLE. FABRICATED NEW REPLACEMENT ANGLE. AND INSTALLED IAW SRM 51-30-01-0G., SRM 51-40-02-0G.SDR IPXA10560033Stiffener · corrodedINSPECTION TYPE:C4, STIFFENER ABOVE LAV PAN, INSIDE FUSELAGE IS CORRODED AT BS 361 BETWEEN S-21R AND S-23R. R & R STIFFENER IAW SRM 51-40-02-0.SDR IPXA10560032Stiffener · corrodedINSPECTION TYPE:C4, STIFFENER ABOVE LAV PAN, INSIDE FUSELAGE IS CORRODED AT BS 361 BETWEEN S-21R AND S-23R. R & R IAW SRM 51-40-02-0G.SDR IPXA10560011Stringer Clip · gougedINSPECTION TYPE:C4 GOUGE IN STRINGER CLIP STA 1681.8, S-5R, FABRACATED AND REPLACED STRINGER CLIP STA 1681.8, S-5R IAW SRM 51-40-02-0G.SDR IPXA10560270Skin · dentedINSPECTION TYPE:C4 DENT IN LEFT HORIZONTAL STABILIZER SKIN UPPER SURFACE 21.5" AFT OF REMOVEABLE L/E 47" O/B OF FUSELAGE. REPLACED PANEL PER DWG 185N7001 ID 0001 REV CSDR IPXA10560161Spar · gougedINSPECTION TYPE:C4, LT HORIZONTAL STAB AUX SPAR, FWD UPPER CHORD, UPPER SURFACE GOUGED FS STA 186, MARKED. BLENDED DAMAGE AREA, FOUND TO BE OUT OF LIMITS, REPAIRED IAW SRM 55-10-10-1A, ER 10-2748.SDR IPXA10560408Skin · corrodedINSPECTION TYPE:C4, CORROSION ON INNER FUSELAGE SKIN AT BS 1837 TO BS 1848, LBL 11, INSIDE SECTION 48. BLENDED CORROSION AND RESTORED FINISH IAW ATS ER 10-2895.SDR IPXA10560658Skin · damagedINSPECTION TYPE:C4, FUSELAGE LOWER EXTERIOR SKIN HAS A HOLE AT BS 500, LBL 2. REPAIRED IAW ATS ER 10-2761.SDR IPXA10560426Skin · gougedINSPECTION TYPE:C4, EXTERIOR FUSELAGE SKIN IS GOUGED AT BS 480, S14L REPAIRED FUSE SKIN IAW ATS ER10-2746 AND EO B757-5330-38140-A.SDR IPXA09555196Compressor · stalledATB - RT ENG COMPRESSOR STALL AT 1000FT ON DEPARTURE. EMERGENCY DECLARED. REMOVED AND REPLACED RT ENGINE PER ENGINEERING REQUEST PER TC 5001. OPS TEST C/W PER TC 5002. SATISFACTORY AMM 71-00-00-5.SDR UPS07550140Door · stickingINSPECTION TYPE:N/A CABIN ENTRY DOOR STICKS AND DIFFICULT TO OPEN AND CLOSE. PER AMM 12-21-20 LUBRICATED CABIN ENTRY DOOR HANDLE CAM. OPERATION CHECK OK.SDR UPS07549827Guard · looseINSPECTION TYPE:N/A EMERGENCY EXIT LIGHT SWITCH STAYS IN ON POSITION. FOUND EMERGENCY EXIT LIGHT SWITCH GUARD LOOSE AND RESECURED AS REQUIRED. OPS TEST EMERGENCY EXIT LIGHT SYSTEM SATISFACTORY PER AMM 33-51-00-5.SDR UPS06546410Light · weakEMERGENCY LIGHT -UNARMED- LIGHT DIM. RELAMPED, OPS CHECK GOOD.SDR UPS05544287Odor · detectedFLEW THRU HEAVY RAIN, LOTS OF STATIC ELECTRICITY. TEMPORARY EICAS MESSAGES RUDDER RATIO & MACH SPEED TRIM & STRONG ELEC FUMES SMELL. ALL CONDITIONS CLEARED W/IN 5 MIN'S REMAINING FLT NORMAL. LT & RT SAM'S TEST NORMAL PER MM 27-09-00-2, NO FAULTS BALLS DISPLAYESDR UPS04543534Handle · stiffAFTER LANDING ON FIRST LEG, CAPT WINDOW UNLOCK HANDLE BECAME HARD TO MOVE SMOOTHLY. AT THE END OF SECOND LEG, HANDLE REQUIRES EXCESSIVE PRESSURE TO COMPLETELY UNLOCK. IT APPEARS THAT WHEN AIRCRAFT IS PRESSURIZED, IT HELPS BIND THE HANDLE. DEF NR D291605 ASDR UPS04543351Skin · corrodedINSPECTION TYPE-C, CORROSION FWD OF APU INLET BOX BS 1790 4 INCHES IB OF STR6R. REMOVED AND REPLACED STRAP AT APU INLET BOX IAW SRM 51-40-02.SDR UPS03541450Adc · faultyINSPECTION TYPE:N/A F/O'S AIRSPEED DIFFERS BY 20 KNOTS IN FLIGHT ALTERNATE ADC SELECTED CURES INDICATION PROBLEMS. RT ADC SEEMS INACCURATE, ASSOCIATED MACH SPEED TRIM AND RUDDER RATIO EICAS MSGS DISPLAYED. T/S SYSTEM AND REPLACED RIGHT ADC PER FIM 34-12-00 ASDR UPS03541448Adc · malfunctionedINSPECTION TYPE:N/A F/O'S AIRSPEED DIFFERS BY 20KTS IN FLIGHT, ALTERNATE ADC SELECTED CURES ADC INDICATION PROBLEM. RT ADC SEEMS INACCURATE ASSOCIATED MACH TRIM AND RUDDER RATIO EICAS MSGS DISPLAYED. ELEVATOR ASYMMETRY MSG DISPLAYED INFLIGHT AND MILD PITCH VSDR UPS96520206Gear Ind Lght · defectiveCREW HAD ON GEAR DOWN AND LOCKED INDICATION. FOUND THE CAP ASSEMBLY OF THE INDICATOR LIGHT WOULD NOT LOCK INTO THE BASE, THIS CAUSED THE BULB TO NOT WORK. REPLACED NOSE GEAR INDICATION LIGHT ASSEMBLY NR 434-674-1033-2205, CHECKED OP AND OPS OK.
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