N110UW
Service difficulty reports · 301
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 = 'N110UW' 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 = 'N110UW' 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 AALA201710119019Dummy Rail · corrodedCORROSION ON FORWARD GALLEY DUMMY RAIL AT -Y81, BETWEEN FRAMES 12 AND 16. REPLACED THE DUMMY RAIL IAW SRM 51-72-11, AND DRAWING D53112828.SDR AALA201710119014Seat Track · corrodedCORROSION ON FORWARD GALLEY SEAT TRACK AT -Y765, BETWEEN FRAMES 12 AND 24. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DRAWING D53112812.SDR AALA201710139014Floor Support · corrodedCORROSION ON AFT GALLEY FLOOR SUPPORT BETWEEN FRAMES 64 AND 66, Y1292. REMOVED AND REPLACED THE FLOOR SUPPORT SRM 51-72-11, AND DRAWING D53472090.SDR AALA201710319016Skin · crackedAIRCRAFT IN BASE MAINTENANCE: FUSELAGE SKIN FASTENER HOLE HAS CRACK INDICATION AT FRAME 35 AND STRINGER 30 RIGHT. REPAIRED FUSELAGE SKIN PER EA 273868.SDR AALA201710319015Repair · debondedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING OUTBOARD TRAILING EDGE FLAP UPPER SURFACE EXISTING REPAIR IS DISBONDED AT RIB 10. REPAIRED OUTBOARD TRAILING EDGE FLAP UPPER SURFACE PER EA 274090.SDR AALA201710319011Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON NR 5 RUDDER HINGE FITTING. REPLACED HINGE FITTING PER SRM 51-72-11 AND AMM 55-36-41-400-001-A.SDR AALA201710259010Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON RUDDER TO HINGE ARM NR 1 BEARING AT RIB 2 ON VERTICAL STABILIZER. REPLACED HINGE ARM NR 1 FITTING PER SRM 51-72-11 AND AMM 55-36-41-000-001-A.SDR AALA201710259005Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON RUDDER TO VERTICAL STABILIZER HINGE ARM NR 2 AT RIB 4. REPLACED HINGE ARM FITTING NR 2 PER SRM A320 51-72-11 AND AMM 55-36-41-400-001-A.SDR AALA201710129001Hinge Fitting · excess playEXCESSIVE PLAY ON VERTICAL STABILIZER HINGE ARM NR 7 BEARING. REPLACED THE HINGE FITTING IAW SRM 51-72-11, AND AMM 55-36-41-400-001-A.SDR AALA201710269013Floor Panel · delaminatedAIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED AFT CARGO FLOOR PANEL 151AF BETWEEN FUSELAGE FRAMES 46 TO 50, Y765 TO -Y765. REMOVED AND REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 PARAGRAPH 2 FIGURE 20109 AND IRM 9701 REVISION G.SDR AALA201710269012Floor Panel · delaminatedAIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED FORWARD CARGO FLOOR PANEL 131AF BETWEEN FUSELAGE FRAMES 24 AND 28, Y765 TO -Y765. REMOVED AND REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 PARAGRAPH 2 FIGURE 20109 AND IRM 9701 REVISION G.SDR AALA201710269008Floor Panel · delaminatedAIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED AFT CARGO FLOOR PANEL 151GF BETWEEN FUSELAGE FRAMES 52 AND 59, Y765 TO -Y765. REMOVED AND REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 FIGURE 20109 AND IRM 9701 REVISION G.SDR AALA201708029006Lens · missingSEATS 4C MISSING EMERGENCY LIGHT LENS. INSTALLED A NEW LENS . OK FOR SERVICESDR AALA201707269014Sliding Window · bindingAIRCRAFT WAS GROUNDED. FIRST OFFICER WINDOW IS VERY DIFFICULT TO OPEN AND EVEN MORE DIFFICULT TO CLOSE. REMOVED AND REPLACED WINDOW PER AMM 56-12-11-400-001. LEAK AND OPERATIONAL CHECK GOOD.SDR AALA201705309008Warning Light · defectiveL2 DOOR RED PRESSURE LIGHT ON DURING ENTIRE FLIGHT. THE LIGHT EXTINGUISHED ON LANDING. REPLACED WARNING LIGHT.SDR AALA201705109002Lens · brokenL1 DOOR EMERGENCY EXIT LIGHT HAS A BROKEN LENS. REPLACED THE LIGHT.SDR AALA201703209011Lens · missingEMERGENCY LIGHT AT SEAT 3C IS MISSING IT'S LENS COVER. REPLACED EMERGENCY LIGHT MOUNTING IAW AMM 33-51-19.SDR AALA201703089002Lens · missingCOVER MISSING FROM R2 DOOR EMERGENCY LIGHT. INSTALLED A NEW COVER.SDR AALA201701239015Rotary Actuator · faultyAIRCRAFT WAS GROUNDED: WHILE APPROACHING THE FINAL DESTINATION OF CLT ; THE FLIGHT CREW REPORTED AN ECAM FLAP FAULT - FLAP 1 MESSAGE. THE FLIGHT CREW DECLARED AN EMERGENCY AND LANDED SAFELY AT CLT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT HAND NSDR AALA201701119005Arming Lever · out of adjustAIRCRAFT WAS NOT GROUNDED. 2L DOOR INTERMITTENT SLIDE LIGHT AND CABIN PRESS LIGHT ILLUMINATED. PRESSURE REMAINED NORMAL THROUGHOUT FLIGHT. MAINTENANCE CLEANED GIRT BAR AND GIRT BAR ATTACH JOINTS AND ADJUSTED ARMING LEVER PER AMM 52-10-00.SDR AALA201701049005Box Beam · crackedAIRCRAFT IN BASE MAINTENANCE. CRACK IN LEFT HAND SIDE BOX BEAM UPPER FLANGE AFT 2 FASTENER HOLES AT Y1622 AND FR 43. REPAIRED BOX BEAM PER EO 5315Y066.SDR AALA201701049004Box Beam · crackedAIRCRAFT IN BASE MAINTENANCE. CRACKS ON RIGHT HAND SIDE BOX BEAM UPPER FLANGE AFT 2 FASTENER HOLES AT -Y1622 AND FR 43. REPAIRED SIDE BOX BEAM PER EO 5315Y066.SDR AALA201610139020Plate · out of adjustRT OVERWING SLIDE LOWER STAINLESS PLATE OUT OF POSITION. RE-INSTALLED RT OVERWING SLIDE LOWER STAINLESS PLATE PER AMM CHAP 25-62-42. THE AIRCRAFT WAS NOT GROUNDED.SDR AALA201601129009Door Sill · dirtyAIRCRAFT WAS NOT GNDED. FLIGHT ATTENDANT COULD NOT ARM 2L DOOR. CLEANED DOOR SILL AREA OF TRASH. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE 2L DOOR ARMING SYS.SDR AALA201512069003Sign · detachedAIRCRAFT WAS NOT GNDED. EXIT SIGN BY L1 DOOR FELL OFF. INSTALLED NEW EXIT SIGN BY L1 DOOR.SDR AALA201512029009Coffeemaker · defectiveAIRCRAFT WAS NOT GNDED. RIGHT AFT COFFEE MAKER, RIGHT SMELLS HOT & PULLED BREAKER. SMOKE & SMELL DISSIPATED. REPLACED RIGHT AFT COFFEE MAKER. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 25-35-15.SDR AALA201512029008Outlet · dislodgedAIRCRAFT WAS NOT GNDED. DURING FLIGHT, FLIGHT ATTENDANT REPORTED THE ACRID ODOR OF BURNT WIRING IN THE AFT GALLEY AREA, NO SMOKE WAS DETECTED. COMPLIED WITH JC 23L00021001, TROUBLE SHOT CABIN AIR QUALITY, FOUND AFT GALLEY 115V POWER OUTLET DISLODGED. SECURESDR USAA2015030500009Support Fitting · corrodedC2 CHECK, RT WING MLG SUPPORT FITTING HAS CORROSION AROUND SEVERAL FASTENERS AT RIB 5. REMOVED CORROSION & INSTALLED SHIM WASHERS IAW EA 209459A.SDR USAA2015030500008Support Fitting · corrodedC2 CHECK, LT WING MLG SUPPORT FITTING HAS CORROSION AROUND SEVERAL FASTENERS AT RIB 5. REMOVED CORROSION & INSTALLED SHIM WASHERS IAW EA 209481A.SDR USAA2014102900005Handle · dirtyRIGHT OVERWING EXIT IS NOT SHOWING ARMED. REMOVED DEBRIS IN HATCH HANDLE PANEL FROM RT OVERWING EXIT.SDR USAA2014081800009Skin · saturatedC11 CHECK TRAPPED WATER INDICATION ON UPPER SURFACE OF RT ELEVATOR AT 37, 73 & 81 INCHES FROM OTBD END & 39 INCHES FROM INBD END AT APPROX 3.5 INCHES FROM THE TE. REPLACED RT ELEVATOR IAW AMM 27-34-41.SDR USAA2014081800008Skin · saturatedC11 CHECK TRAPPED WATER INDICATION ON UPPER SURFACE OF LT ELEVATOR AT 18, 25, 60 & 88 INCHES FROM INBD END AT APPROX. 3.5 INCHES FROM THE TE. ALSO TRAPPED WATER INDICATION ON LOWER SURFACE OF LT ELEVATOR AT 88 INCHES FROM INBD AT APPROX. 3.5 INCHES FROM THE TSDR USAA2014081100012Seat Track · corrodedC11 CHECK LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FRAME 16, Y1292. REPLACED SEAT TRACK IAW SRM 53-11-14, 51-42-11 & 51-44-11.SDR USAA2014081100015Floor Panel · delaminatedC11 CHECK DELAMINATION ON FLOOR PANEL 262BG. REPLACED FLOOR PANEL 262BG.SDR USAA2014081100014Floor Panel · delaminatedC11 CHECK DELAMINATION ON FLOOR PANEL 261DF. REPLACED FLOOR PANEL 261DF.SDR USAA2014080800012Floor Panel · delaminatedC11 CHECK CABIN FLOOR PANEL 221DF DELAMINATED. FABRICATED & INSTALLED REPLACEMENT PANEL IAW SRM 53-02-00-201 PARA 8H FIG 209.SDR USAA2014080800011Floor Panel · delaminatedC11 CHECK CABIN FLOOR PANEL 261PF DELAMINATED. FABRICATED & INSTALLED REPLACEMENT PANEL IAW SRM 53-02-00-201 PARA 8H FIG 209.SDR USAA2014080800010Seat Track · corrodedC11 CHECK CABIN FLOOR SEAT RAIL CORRODED AT FRAME 16 & Y 503.2. R & R RAIL IAW SRM 51-42-11 & 51-44-11.SDR USAA2014080800009Shear Plate · crackedC11 CHECK CABIN FLOOR SHEAR PLATE CRACKED AT FRAME 68 & Y 1732. R & R SHEAR PLATE IAW SRM 51-42-11 & 51-44-11.SDR USAA2014080800008Guide Plate · crackedC11 CHECK LT AFT EMER EXIT DOOR GUIDE PLATE CRACKED. R & R GUIDE PLATE IAW SRM 51-42-11-001.SDR USAA2014080800006Guide Plate · crackedC11 CHECK RT FWD EMER EXIT DOOR GUIDE PLATE CRACKED. R & R GUIDE PLATE IAW SRM 51-42-11-001.SDR USAA2014080600014Door Sill · corrodedC11 CHECK LEVEL 2 GALVANIC CORROSION ON R2 DOOR SILL AT FRAME 68, -Y1292. REPAIRED R2 DOOR SILL IAW SRM 53-41-14-101, 53-41-14-201 & 51-44-11.SDR USAA2014061000003Slide · failedSLIDE AT DOOR 2L FAILED OPERATIONAL TEST, TOOK 20 SECONDS TO INFLATE. REPLACED SLIDE AT DOOR 2L.SDR USAA2014050600005Floor Panel · delaminatedWEEKLY CHECK DELAMINATION ON AFT CARGO FLOOR PANEL 151DF BETWEEN FRAME 53 TO FRAME 56 JUST FWD ENTRY DOOR. REPLACED AFT CARGO FLOOR PANEL 151DF IAW AMM 53-47-14-400-001A.SDR USAA2014042500009Actuator · inoperativeFLIGHT CONTROL FLAPS FAULT, WE HAD SLATS FOR LANDING BUT NO FLAPS. REPLACED LT FLAP TRACK ACTUATOR IAW AMM 27-54-49- 400-001A. OPERATIONS CHECK OF FLAPS SYS GOOD IAW AMM 27-54-00-710-001A.SDR USAA2014031300006Cylinder · low pressureL2 DOOR EMERGENCY ASSIST CYLINDER PRESS IS LOW. SERVICED L2 DOOR EMERGENCY ASSIST CYLINDER IAW JOB CARD 26L00005005.SDR USAA2013112500006Connector · dirtyUPON GEAR EXTENSION, CREW REPORTED ECAM DISPLAYED LGCIU 2 FAULT. PERFORMED GO AROUND & CHECK LIST. MESSAGE RETURNED ON 2ND EXTENSION. MESSAGE DISAPPEARED ON POWER CHANGE TO APU POWER. FOUND LGCIU 2 FAULTED PROX SENSOR 29GA. CLEANED 29GA CANON PLUG & SECURESDR USAA2013112000005Control Handle · out of adjustCREW REPORTED THE L1 DOOR WILL NOT OPEN EASILY FROM THE OUTSIDE. MX ADJUSTED CONTROL HANDLE OF L1 DOOR IAW AMM 52-11-00-820-002-A, OPERATIONS CHECKED GOOD.SDR USAA2013052300009Unknown · malfunctionedCLASS II STATUS: EMERGENCY LIGHTS FLASHING, NO CALL BELLS, NO INTERPHONE, NO P/A SYSTEM, OCCURRED 3 TIMES DURING TAXI OUT, TAXI IN, AND AT GATE. CHECKED CIDS SYS IAW TROUBLESHOOTING MANUAL 24-00-00-810-818-A. OPS CHECKS OK, NO FAULTS FOUND VISUALLY OR RECORDSDR USAA2013042900023Damper · defectiveUPON GATE ARRIVAL AGENT HAD HARD TIME OPENING L1 DOOR. REMOVED AND REPLACED L1 DOOR DAMPER IN ACCORDANCE WITH AIRBUS MAINTENANCE MANUAL 52-11-14 AND LUBRICATED DOOR MECHANISM PER AIRBUS MAINTENANCE MANUAL 12-22-52.
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