N755US
Service difficulty reports · 249
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 = 'N755US' 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 = 'N755US' 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 USAA2012092400012Shear Plate · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23L, Y1732. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23L, Y1732 IAW A319 SRM 51-72-11, AIRBUS DRAWING D53474180 & TYPICAL REPAIR TR320-2528-10-0011D.SDR USAA2012092400011Shear Plate · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR64 TO FR70, S23R. REPLACED SHEAR PLATE BETWEEN FR64 TO FR70, S23R IAW A319 SRM 51-72-11, AIRBUS DRAWING D53474180 & TYPICAL REPAIR TR320-2528-10-0011D.SDR USAA2012091700054Coupling · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR64, -Y1292. REPLACED COUPLING AT FR64, -Y1292 IAW A319 SRM 51-72-11.SDR USAA2012091700050Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BEAM BETWEEN FR64 TO FR66, Y765. REPLACED SEAT RAIL BEAM BETWEEN FR64 TO FR66, Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472815.SDR USAA2012091700047Coupling · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR67+15 INCHES, Y1162. REPLACED COUPLING AT FR67+15 INCHES, Y1162 IAW A319 SRM 51-72-11.SDR USAA2012091700046Splice · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING SPLICE AT FR67+15 INCHES, -Y1162. REPLACED COUPLING SPLICE AT FR67+15 INCHES, -Y1162 IAW A319 SRM 51-72-11.SDR USAA2012091700043Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR64 TO FR66, Y1292. REPLACED SEAT RAIL BETWEEN FR64 TO FR66, Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472815.SDR USAA2012091700042Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+15 INCHES & BETWEEN -Y1292 TO -Y1162. REPLACED FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+15 INCHES & BETWEEN -Y1292 TO -Y1162 IAW A319 SRM 51-42-11 & AIRBUS DRAWING D53472780.SDR USAA2012091700053Seat Track · corroded2S CHECK - CABIN SEAT RAIL CORRODED BETWEEN FR 64 AND FR 66 AT Y-1292. REMOVED AND REPLACED SEAT RAIL IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53472816.SDR USAA2012091700052Hinge Fitting · excess play2S CHECK - VERTICAL STABILIZER HINGE FITTING NR 7 AT STATION 561 HAS EXCESSIVE PLAY. REMOVED AND REPLACED HINGE FITTING IAW A319 SRM 51-72-11 AND AMM 55-36-41-0001-A.SDR USAA2012091700048Floorbeam · corroded2S CHECK - CABIN FLOORBEAM CORRODED BETWEEN FR 67 AND FR 69 AT Y1162. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-72-11.SDR USAA2012091700045Floorbeam · corroded2S CHECK - CABIN FLOORBEAM CORRODED BETWEEN FR 67 AND FR 69 AT Y-1162. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D534722780.SDR USAA2012091700041Floorbeam · corroded2S CHECK - FLOORBEAM CORRODED BETWEEN FR 66 AND FR 68 AT Y1162. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53472780.SDR USAA2012091300018Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL BETWEEN FR66 TO FR68, S23L. REPLACED LOWER SILL BETWEEN FR66 TO FR68, S23L IAW A319 SRM 51-72-11, AIRBUS DRAWING D53480505 & EA 502237.SDR USAA2012091200006Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y765. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112812.SDR USAA2012091100042Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC ON FLOORBEAM ASSEMBLY BETWEEN FR67 TO FR70, -Y765. REPLACED FLOORBEAM ASSEMBLY BETWEEN FR67 TO FR70, -Y765 IAW A319 SRM 51-72-11, AIRBUS DRAWING D53472780.SDR USAA2012091100040Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC ON TRACK ASSEMBLY BETWEEN FR12 TO FR24, Y765. REPLACED TRACK ASSEMBLY BETWEEN FR12 TO FR24, Y765 IAW A319 SRM 51-72-11, AIRBUS DRAWING D53112828 & D53110984.SDR USAA2012091100039Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC ON TRACK ASSEMBLY BETWEEN FR12 TO FR24, Y765. REPLACED TRACK ASSEMBLY BETWEEN FR12 TO FR24, Y765 IAW A319 SRM 51-72-11, AIRBUS DRAWING 53112812 & D53110984.SDR USAA2012091100038Web · corroded2S CHECK - LEVEL 2 GALVANIC ON WEB IN PASSENGER CABIN BETWEEN FR20 TO FR24, -Y1700. REPLACED WEB IN PASSENGER CABIN BETWEEN FR20 TO FR24, -Y1700 IAW A319 SRM 51-72-11, AIRBUS DRAWING D53112805 & D53112784.SDR USAA2012091100036Floor Support · corroded2S CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOOR SUPPORT BETWEEN FR12 TO FR24, Y254. REPLACED FLOOR SUPPORT BETWEEN FR12 TO FR24, Y254 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112816.SDR USAA2012091100035Floor Support · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR12 TO FR24, -Y254. REPLACED FLOOR SUPPORT BETWEEN FR12 TO FR24, -Y254 IAW A319 SRM 51-72-11, AIRBUS DRAWING D53111462, D53110984 & D53110920.SDR USAA2012091100032Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y1292 IAW A319 SRM 51-72-11, AIRBUS DRAWING D53918547 & D53112812.SDR USAA2012091100031Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, Y1292 IAW A319 SRM 51-72-11, AIRBUS DRAWING D53112812 & D53918122.SDR USAA2012092400018Skin · worn2S CHECK - WEAR ON RIGHT WING NR 2 SLAT ON INTERNAL SKIN AT LOWER EDGE AT NR 6 SLAT TRACK AT WS 6132. REPAIRED RIGHT WING SLAT NR 2 AT SLAT TRACK NR 6 IAW EA 502936.SDR USAA2012092400017Skin · worn2S CHECK - WEAR ON LEFT WING NR 2 SLAT ON INTERNAL SKIN AT LOWER EDGE AT NR 6 SLAT TRACK AT WS 6132. REPAIRED LEFT WING SLAT NR 2 AT SLAT TRACK NR 6 IAW EA 502942.SDR USAA2012092400016Skin · worn2S CHECK - WEAR ON RIGHT WING NR 1 SLAT ON INTERNAL SKIN AT LOWER EDGE AT NR 1 SLAT TRACK AT WS 700. REPAIRED RIGHT WING SLATNR 1 AT SLAT TRACK NR 1 IAW EA 502936.SDR USAA2012092400015Skin · worn2S CHECK - WEAR ON LEFT WING NR 1 SLAT ON INTERNAL SKIN AT LOWER EDGE AT NR 2 SLAT TRACK. REPAIRED LEFT WING SLAT NR 1 AT SLAT TRACK NR 2 OUTER SKIN TRAILING EDGE IAW EA 502942.SDR USAA2012092400014Skin · worn2S CHECK - WEAR ON LEFT WING NR 1 SLAT ON INTERNAL SKIN AT LOWER EDGE BETWEEN WS 1406 AND WS 1957 AT NR 1 SLAT TRACK. REPAIRED LEFT WING SLAT NR 1 AT SLAT TRACK NR 1 OUTER SKIN TRAILING EDGE IAW EA 502942.SDR USAA2012092400008Frame · cracked2S CHECK - CRACK ON SEGMENT ANGLE FRAME ON EMERGENCY EXIT DOOR 834 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. REPLACED SEGMENT ANGLE FRAME ON EMERGENCY EXIT DOOR 834 IAW EO 5210Y228.SDR USAA2012092400007Frame · cracked2S CHECK - CRACK ON SEGMENT ANGLE FRAME ON EMERGENCY EXIT DOOR 844 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. REPLACED SEGMENT ANGLE FRAME ON EMERGENCY EXIT DOOR 844 IAW EO 5210Y228 & A319 SRM 51-72-11.SDR USAA2012092000011Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON RUDDER HINGE FITTING ASSEMBLY NR 2 BETWEEN RUDDER STA 193 TO STA 228 & BETWEEN RIB 4 TO RIB 5. REPLACED RUDDER HINGE FITTING ASSEMBLY NR 2 IAW A319 SRM 51-72-11.SDR USAA2012091200008Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON NR 5 RUDDER HINGE FITTING AT RUDDER STA 299, RIB 7. REPLACED NR 5 RUDDER HINGE FITTING AT RUDDER STA 299, RIB 7 IAW A319 SRM 51-72-11 & AMM 55-36-41-000-001-A.SDR USAA2010091391983Pin · scoredPIT - TRIPLE GEAR CHANGE - MAJOR REPAIR - RIGHT MAIN LANDING GEAR PINTLE PIN HAS SCOURING. REPLACED RIGHT MAIN LANDING GEAR PINTLE PIN IAW JOB CARD 26T00032001.SDR USAA2010090791935Elevator · saturatedPIT - TRIPLE GEAR CHANGE - MAJOR REPAIR - 5 INCH CIRCUMFERENTIAL AREA INDICATION OF WATER INCLUSION ON LEFT ELEVATOR. ACCOMPLISHED WITNESS HOLE INSPECTION IAW A319 AMM 55-20-00-06. NO WATER EGRESS FOUND. REPAIRED IAW A319 SRM 55-21-11 & 55-21-11.SDR USAA2009110593044Power Supply · dischargedFLT 1607 - PHL - EEL - CEILING EMERGENCY EXIT ROW 10 EXTINGUISHED. MAINTENANCE REPLACED THE POWER SUPPLY UNIT C IAW AIRBUS MAINTENANCE MANUAL 33-51-04.SDR USAA2009082692251Megaphone · unserviceableEMERGENCY EQUIPMENT - FORWARD EMERGENCY MEGAPHONE OUT OF DATE. REMOVED AND REPLACED FORWARD EMERGENCY MEGAPHONE PER MAINTENANCE MANUAL 25-65-51.SDR USAA2009082092189Girt Bar · obstructedFLT 1784 - DURING FLT, L2 DOOR SLIDE APPEARS TO BE ARMED BUT HANDLE IS PULLED OUT .25 INCH JUST ENOUGH TO PREVENT CONTACT CAUSING COCKPIT INDICATION UNARMED AND ALSO ON FLIGHT ATTENDANT CIDS PANEL. DURING DESCENT AND ON GROUND HANDLE IS TIGHT & IN ARMED POSITSDR SA06064Slide · faultyPIT - LOCK WIRE WAS FOUND BROKEN ON DISC AND PAWL OF THE LT MAIN ENTRANCE DOOR ESCAPE SLIDE. MAINTENANCE REPLACED THE LT MAIN ENTRANCE DOOR ESCAPE SLIDE. OK FOR SERVICE.SDR USAA061114Floorbeam · corrodedFOUND FLOORBEAM CORRODED Y1292 FS 66. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72-11; CORROSION TASK JA-260-53500, LEVEL 1 DEFECT SIZE: 2" BY 48" BY .100.SDR USAA061115Floorbeam · corrodedFOUND FLOORBEAM CORRODED Y60 AT C 16. INSTALLED DOUBLER PER SRM 53-00-14 FIG 206; CORROSION TASK JA-220-53500; LEVEL 1 DEFECT SIZE: 3" BY 3" BY .150"SDR USAA061116Sill · corrodedFOUND RT AFT SERVICE DOOR SILL BEAM CORRODED AT FS 66. DEFECTIVE PART REPLACED WITH IDENT PART; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 1" BY 1".SDR USAA061117Sill · corrodedFOUND TOPSIDE OF RT AFT SVC DOOR SILL BEAM 6" FWD OF FS 66. REMOVED AND INSTALLED NEW SILL BEAM PER SRM 52-71-11; CORROSION TASK JA-260-53500; LEVEL 1 DEFECT SIZE: 1" BY 1".SDR USAA061118Floorbeam · corrodedFOUND TOPSIDE OF FLOORBEAM CORRODED AROUND (3) NUTCLIPS -Y1292/-Y1162. REMOVED AND INSTALLED NEW BEAM PER SRM 52-72-11; CORROSION TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1" BY 1".SDR USAA061119Floorbeam · corrodedFOUND CORROSION, TOPSIDE OF BEAM (3" FWD OF FS 68) AROUND NUT PLATE. REMOVED AND INSTALLED NEW BEAM PER SRM 52-72-11; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 1.25" BY 1.25".SDR USAA200507002Skin · cracked2.25 IN CRACK FOUND BETWEEN STA 539 AND 594 STR 36 RT TO 37 RT ON SKIN. REMOVED DAMAGED SKIN AND INSTALLED REPAIR DOUBLER PER EA 81165.SDR SA05023Cushion · contaminatedJAX FLIGHT 175, EN-ROUTE DCA TO JAX - A FUEL ODOR WAS REPORTED DURING FLIGHT, AT SEAT ROW NUMBER 15 ON THE RIGHT HAND SIDE OF THE PLANE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A PETROLEUM ODOR AT SEAT 14F. MAINTENANCE REPLACED THE SEAT CSDR USAASA04085Windshield · crackedMSP - FLT 33 - EN ROUTE PHL-SEA - WHILE IN CRUISE FLIGHT, AT FL350, THE RIGHT WINDSHIELD STARTED ARCING FROM THE LOWER CORNER TO THE UPPER LEFT CORNER. THE CIRCUIT BREAKERS FOR THE WINDSHIELD WERE PULLED, BUT THE ARCING CONTINUED UNTIL THE OUTER LAYER OF WINDSDR USAASA03118Battery · inoperativeDCA - THE LEFT FORWARD EMERGENCY POWER SUPPLY UNIT WAS FOUND INOPERATIVE DURING TESTING. MAINTENANCE REPLACED THE LEFT FORWARD EMERGENCY POWER SUPPLY UNIT BATTERY. OPERATIONALLY CHECKS OK. (M)SDR USAASA03078Battery · inoperativeDURING THE WEEKLY CHECK, THE EMERGENCY LIGHTS TEST FAILED WITH AN 'EPSU BATTERY R' MESSAGE. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY POWER SUPPLY UNIT BATTERY, AND PERFORMED THE EMEGENCY LIGHTS TEST. OPERATIONALLY CHECKED OK. (M)
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