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 USAA2014111000006Lens · missingSEAT EMER LIGHT LENS MISSING AT SEAT ROWS 3L & 4L. INSTALLED SEAT EMER LIGHT LENS AT SEAT ROWS 3L & 4L.SDR USAA2014071400012Tachometer · faultyA BRAKES AUTO BRAKE FAULT BRAKE RELEASED MSG ON ECAM. FLIGHT RETURNED TO FIELD & LANDED WITHOUT INCIDENT. R & R NR 3 BRAKE TACHOMETER.SDR USAA2014062300039Floor Panel · delaminatedRON VISIT DELAMINATION ON FLOOR PANEL 151VG BETWEEN FRAME 53 TO 56 & BETWEEN STRINGER 39L TO 39R. REPLACED FLOOR PANEL 151VG IAW AMM 53-42-14.SDR USAA2014062300016Sign · inoperativeTHE EXIT SIGN AT L3 DOOR HAS BURNED BULBS. REPLACED EXIT SIGN AT L3 DOOR.SDR USAA2014061000006Battery · dischargedBOTH EMER AFT FLIGHT ATTENDANT FLASHLIGHTS NOT BLINKING. REPLACED BATTERIES IN BOTH FLASHLIGHTS, OK FOR SERVICE.SDR USAA2014012700035Hinge Fitting · wornCREW REPORTED THE 1L DOOR IS DIFFICULT TO DISARM. R & R THE UPPER HINGE ARM FITTING.SDR USAA2013123100008Duct · collapsedON CLIMB OUT FROM PBI, CREW REPORTED THEY HEARD A POP & A LOSS OF SOME PRESSURIZATION. FLIGHT DIVERTED TO MCO, LANDED WITHOUT FURTHER INCIDENT & TAXIED TO THE GATE. REPLACED EXTRACTION DUCTS DUE TO INFLIGHT COLLAPSE. PERFORMED OPERATIONS TEST 21-26-00-710-0SDR USAA2013121600007Slide · out of adjustTHE FWD CABIN DOOR 1L DIFFICULT TO DISARM AFTER PRESSURIZATION CYCLE. FOUND GIRT BAR ENGAGEMENT CAUSING THE PROBLEM. CLEANED GIRT BAR ENGAGEMENT AREA. FOUND GIRT BAR SLIDE MATERIAL FOLDED INCORRECTLY, CORRECTED FOLD, SLIDE WAS NOT REMOVED. ARMING & DISARMISDR USAA2013120900016Lever · bindsCREW REPORTED DOOR 1L DISARMING LEVER IS BINDING, SLIGHTLY, WHEN DISARMING. DISARMED LEVER, OPERATIONS NORMAL IAW AMM 52-10-00.SDR USAA2013110700006Girt Bar · out of positionCREW REPORTED THE MAIN CABIN DOOR SLIDE DISARM HANDLE IS DIFFICULT TO OPERATE. INDICATING CIRCLE NOT LINED UP CORRECTLY. TO DISARM DOOR, TOOK TWO HANDS TO OPERATE HANDLE. MAINTENANCE TROUBLESHOT TO L1 MAIN DOOR GIRT BAR OUT OF POSITION. REPOSITIONED GIRT BASDR USAA2013102400013Door · dirtyF/A REPORTED L1 DOOR DIFFICULT TO OPEN. MAINTENANCE CLEANED DEBRIS FROM DOOR FLOOR AREA. DOOR CHECKS OK.SDR USAA2013091300020Oil System · overservicedCREW REPORTED AN ODOR IN CABIN. MX ACCOMPLISHED JC 26L00021001. SOURCE WAS FOUND TO BE APU OVERSERVICED. SERVICED APU OIL TO CORRECT LEVEL. ALSO, ACCOMPLISHED JC 26L00021002 AND FOUND VALVE, FIN 2577GM, LEAKING FROM FITTING. REPLACED PACKING IAW AMM 32-43-SDR USAA2013051300010Cover · unsecureCREW REPORTED THE EMERGENCY EXIT LIGHT COVER FOR EXIT LIGHT ADJACENT TO 2R DOOR FELL OFF AND IS NOW LOCATED IN COCKPIT. MAINTENANCE INSTALLED COVER FOR EXIT LIGHT ADJACENT TO 2R DOOR EMERGENCY LIGHT.SDR USAA2013020400022Lens · wrong partMAINTENANCE REPORTED AN INCORRECT EXIT MARKING SIGN LENS INSTALLED ABOVE L2 DOOR (INCORRECT LEGEND). MAINTENANCE INSTALLED CORRECT EXIT MARKING LENS AT L2 DOOR SIGN 45WL. EMERGENCY LIGHTING OPERATION CHECKS SATISFACTORY. REF 33-51-00-710-009.SDR USAA2012092400019Skin · worn2S CHECK - WEAR ON RIGHT WING NR 1 SLAT ON INTERNAL SKIN AT LOWER EDGE AT NR 2 SLAT TRACK AT WS 1406. REPAIRED RIGHT WING SLAT NR 1 AT SLAT TRACK NR 2 IAW EA 502936.SDR USAA2012092000012Support · excess play2S CHECK - EXCESSIVE PLAY AT LEFT WING AILERON NR 3 HINGE SUPPORT FRAME ASSEMBLY BETWEEN WS 1287 TO WS 1346 & BETWEEN RIB 24 TO RIB 25 WING AILERON NR 3 HINGE SUPPORT FRAME ASSEMBLY IAW A319 AMM 57-51-31 & SRM 51-72-11.SDR USAA2012092000010Support · excess play2S CHECK - EXCESSIVE PLAY AT LEFT WING AILERON NR 1 HINGE SUPPORT FRAME ASSEMBLY BETWEEN WS 1228 TO WS 1287 & BETWEEN RIB 23 TO RIB 24. REPLACED LEFT WING AILERON NR 1 HINGE SUPPORT FRAME ASSEMBLY IAW A319 AMM 57-51-31 & SRM 51-72-11.SDR USAA2012090400017Slide · out of adjust2S CHECK - DURING VISUAL INSPECTION OF THE LEFT OFF WING SLIDE ENCLOSURE DOOR FOUND DOOR IS NOT FLUSH WITH THE OUTER SURFACE OF THE LEFT OFF WING SLIDE ENCLOSURE. REPACKED LEFT OFF WING SLIDE IAW CMM 25-60-58 REV 19 AND FOLDING PROCEDURE P-11907 REV R.SDR USAA2012091300020Strut · corroded2S CHECK - CORROSION ON INTERNAL HOUSING OF RIGHT WING INTERCONNETING STRUT BETWEEN WS 407 TO WS 486 ALSO BETWEEN RIB 8 TO RIB 9. REPLACED RIGHT WING INTERCONNETING STRUT IAW A319 AMM 27-51-44 & JOB CARD 26C67057001.SDR USAA2012091200002Strut · corroded2S CHECK - CORROSION ON INTERNAL AREA AT HOUSING OF LEFT WING INTERCONNECTING STRUT BETWEEN WS 4067 TO WS 4862 & BETWEEN RIB 8 TO RIB 9. REPLACED LEFT WING INTERCONNECTING STRUT IAW JOB CARD 26C57057001.SDR USAA2012091300021Support Frame · corroded2S CHECK - CORROSION ON SUPPORT FRAME BETWEEN FR69 TO FR70, S23L. REPLACED SUPPORT FRAME BETWEEN FR69 TO FR70, S23L IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53171180.SDR USAA2012091300019Support Frame · corroded2S CHECK - CORROSION ON SUPPORT FRAME BETWEEN FR69 TO FR70, S23R. REPLACED SUPPORT FRAME BETWEEN FR69 TO FR70, S23R IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53171180.SDR USAA2012091100030Hinge Pin · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING NR 1 SPOILER OUTBOARD HINGE PIN THREADS BETWEEN WS 3059 TO WS 3758 & BETWEEN RIB 6 TO RIB 7. REPLACED LEFT WING NR 1 SPOILER OUTBOARD HINGE PIN IAW A319 AMM 27-64-41.SDR USAA2012091100029Hinge Pin · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING NR 5 SPOILER OUTBOARD HINGE PIN THREADS BETWEEN WS 10729 TO WS 11198 & BETWEEN RIB 20 TO RIB 21. REPLACED LEFT WING NR 5 SPOILER OUTBOARD HINGE PIN IAW A319 AMM 27-64-45.SDR USAA2012091100028Hinge Pin · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING NR 3 SPOILER INBOARD HINGE PIN THREADS BETWEEN WS 7792 TO WS 8268 & BETWEEN RIB 14 TO RIB 15. REPLACED LEFT WING NR 3 SPOILER INBOARD HINGE PIN IAW A319 AMM 27-64-43.SDR USAA2012091100027Hinge Pin · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING NR 3 SPOILER OUTBOARD HINGE PIN THREADS BETWEEN WS 7792 TO WS 8268 & BETWEEN RIB 14 TO RIB 15. REPLACED LEFT WING NR 3 SPOILER OUTBOARD HINGE PIN IAW A319 AMM 27-64-43.SDR USAA2012091100026Hinge Pin · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING NR 2 SPOILER INBOARD HINGE PIN THREADS BETWEEN WS 6132 TO WS 6699 & BETWEEN RIB 11 TO RIB 12. REPLACED LEFT WING NR 2 SPOILER INBOARD HINGE PIN IAW A319 AMM 27-64-42.SDR USAA2012091100025Hinge Pin · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING NR 2 SPOILER INBOARD HINGE PIN THREADS BETWEEN WS 6132 TO WS 6699 & BETWEEN RIB 11 TO RIB 12. REPLACED RIGHT WING NR 2 SPOILER INBOARD HINGE PIN IAW A319 AMM 27-64-42.SDR USAA2012091100024Hinge Pin · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING NR 1 SPOILER INBOARD HINGE PIN THREADS BETWEEN WS 3059 TO WS 3758 & BETWEEN RIB 6 TO RIB 7. REPLACED LEFT WING NR 1 SPOILER INBOARD HINGE PIN IAW A319 AMM 27-64-41.SDR USAA2012091100023Hinge Pin · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING NR 5 SPOILER INBOARD HINGE PIN THREADS BETWEEN WS 10729 TO WS 11198 & BETWEEN RIB 20 TO RIB 21. REPLACED LEFT WING NR 5 SPOILER INBOARD HINGE PIN IAW A319 AMM 27-64-45.SDR USAA2012091100022Hinge Pin · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING NR 5 SPOILER INBOARD HINGE PIN THREADS BETWEEN WS 10729 TO WS 11198 & BETWEEN RIB 20 TO RIB 21. REPLACED RIGHT WING NR 5 SPOILER INBOARD HINGE PIN IAW A319 AMM 27-64-45.SDR USAA2012092400022Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FITTING AT INTERNAL AREA OF LEFT OUTBOARD FLAP, INBOARD SIDE OF FRONT SPAR AT RIB 14. REPLACED LEFT OUTBOARD FLAP IAW JOB CARD 26L00027009.SDR USAA2012092400010Skin Panel · corroded2S CHECK - CORROSION ON SKIN PANEL BETWEEN FR63 TO FR64 & BETWEEN S41L TO S42L. REPAIRED SKIN PANEL BETWEEN FR63 TO FR64 & BETWEEN S41L TO S42L IAW EA 502245.SDR USAA2012092400009Skin Panel · corroded2S CHECK - CORROSION ON SKIN PANEL BETWEEN FR63 TO FR64 & BETWEEN S41R TO S42R. REPAIRED SKIN PANEL BETWEEN FR63 TO FR64 & BETWEEN S41R TO S42R IAW EA 502902.SDR USAA2012091700051Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR60+11 INCHES TO FR64, -Y765. REPLACED SEAT RAIL BETWEEN FR60+11 INCHES TO FR64, -Y765 IAW A319 SRM 53-41-15.SDR USAA2012091100037Web · cracked2S CHECK - CRACK ON WEB OF FLIGHT COMPARTMENT FLOOR STRUCTURE BETWEEN FR8 TO FR11, -Y765. REPLACED WEB BETWEEN FR8 TO FR11, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53113378.SDR USAA2012091700040Fitting · corroded2S CHECK - FLOORBEAM FITTING CORRODED BETWEEN FR 16 AND FR 20 AT S23R. REMOVED AND REPLACED FITTING IAW A319 SRM 51-72-11 AND AIRBUS DRAWINGG D53112109.SDR USAA2012091700049Hinge Fitting · excess play2S CHECK - VERTICAL STABILIZER HINGE FITTING NR 4 AT STATION 263 HAS EXCESSIVE PLAY. REMOVED AND REPLACED HINGE FITTING IAW A319 SRM 51-72-11 AND A319 AMM 55-36-41-000-001-A.SDR USAA2012091200009Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER AFT CORNER FITTING AT FR68, S23R. REPLACED LOWER AFT CORNER FITTING AT FR68, S23R IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53480505.SDR USAA2012091200007Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON NR 1 RUDDER HINGE FITTING AT RUDDER STA 78, RIB 2. REPLACED NR 1 RUDDER HINGE FITTING AT RUDDER STA 78, RIB 2 IAW A319 SRM 51-72-11 & AMM 55-36-41-000-001-A.SDR USAA2012091100041Sill · corroded2S CHECK - LEVEL 2 GALVANIC ON LEFT CENTER SHAPE SILL BETWEEN FR66 TO FR68, S23L. REPLACED LEFT CENTER SHAPE SILL BETWEEN FR66 TO FR68, S23L IAW A319 SRM 51-72-11, AIRBUS DRAWING D53480505.SDR USAA2012091100034Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER CENTER FITTING BETWEEN FR66 TO FR68, S23R, -Y1500. REPLACED LOWER CENTER FITTING BETWEEN FR66 TO FR68, S23R, -Y1500 IAW A319 SRM 51-72-11, AIRBUS DRAWING D53480505.SDR USAA2012091100033Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON AFT LOWER CORNER FITTING AT FR68, S23L. REPLACED AFT LOWER CORNER FITTING AT FR68, S23L IAW A319 SRM 51-72-11, AIRBUS DRAWING D53480505.SDR USAA2012092400020Floor Panel · missing2S CHECK - MISSING MATERIAL ON FLOOR PANEL 262BG BETWEEN FR64 TO FR66 & BETWEEN -Y1292 TO -Y254. REPLACED FLOOR PANEL 262BG IAW A319 SRM 53-02-00, IRM 9701 REV G & EA 502946.SDR USAA2012091700055Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, -Y1292. REPLACED SEAT TRACK BETWEEN FR24 TO FR35, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53233450.SDR USAA2012091300017Splice · worn2S CHECK - WEAR ON SEAT TRACK BRACKET SPLICE AT FR35, Y1292. REPLACED SEAT TRACK BRACKET SPLICE AT FR35, Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53371020.SDR USAA2012091200005Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, Y1292. REPLACED SEAT TRACK BETWEEN FR24 TO FR35, Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53233450.SDR USAA2012091200004Floor Panel · damaged2S CHECK - MATERIAL MISSING ON FLOOR PANEL 261PF BETWEEN FR65 TO FR70 & BETWEEN -Y1292 TO Y1292. REPLACED FLOOR PANEL 261PF IAW A319 SRM SUPPLEMENTAL INF 53-02-00-201 & IRM 9701 REV G.SDR USAA2012091200003Floor Panel · damaged2S CHECK - MATERIAL MISSING ON FLOOR PANEL 261BG BETWEEN FR66 TO FR64 & BETWEEN Y765 TO Y1732. REPLACED FLOOR PANEL 261BG IAW A319 SRM SUPPLEMENTAL INF 53-02-00-201 & IRM 9701 REV G.SDR USAA2012092400021Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON R2 DOOR CUTOUT LOWER SILL BETWEEN FR66 TO FR68, S23R. REPLACED R2 DOOR CUTOUT LOWER SILL BETWEEN FR66 TO FR68, S23R IAW EA 502911.
Back to N755US