N710UW
Service difficulty reports · 295
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 = 'N710UW' 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 = 'N710UW' 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 AALA201802289024Cover · brokenL1 DOOR ASSIST HANDLE COVER BROKEN. MAINTENANCE REPLACED THE HANDLE COVER AND PERFORMED SATISFACTORY OPERATIONAL CHECK.SDR AALA201710249002Handle · disconnectedR1 DOOR HANDLE, DOOR ASSIST DISCONNECTED. REPLACED R1 DOOR ASSIST COVER, CHECKED OK IAW AMM.SDR AALA201708049013Pin · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION (PITTING) ON RIGHT MAIN GEAR AFT PINTLE PIN. REPLACED PINTLE PIN PER CARD 26T00032001.SDR AALA201708049012Pin · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND MAIN LANDING GEAR REAR PINTLE PIN. REPLACED PINTLE PIN PER JOB CARD 26T00032001.SDR AALA201706159005Computer · faultyVENT SKIN VALVE FAULT. EXTRACT VALVE APPEARS TO BE STUCK OPEN. ACCOMPLISHED AVIONICSE VENTILATION COMPUTER TEST IAW AMM 21-26-00. TEST OK. AIRCRAFT WAS GROUNDED.SDR AALA201702099011Lens · looseAFT LEFT GALLEY EMERGENCY EXIT LIGHT LENS LOOSE. INSTALLED THE LENS.SDR AALA201612179016Flashlight · inoperativeFORWARD FACING JUMPSEAT FLASHLIGHT INOPERATIVE. REPLACED THE FLASHLIGHT.SDR AALA201612019013Girt Bar · out of positionAIRCRAFT WAS GROUNDED. GIRT BAR ON DOOR 2L HAD BROKEN OFF DOOR SLIDE ASSEMBLY. MAINTENANCE FOUND GIRT BAR TO BE OUT OF POSITION (NOT "BROKEN"). REPOSITIONED SURVIVAL KIT LANYARD, RELEASE STRAP AND GIRT BAR PER AMM 26-62-44.SDR AALA201612019011Strap · out of adjustAIRCRAFT WAS GROUNDED. 2L DOOR WILL NOT ARM. MAINTENANCE ADJUSTED STRAPPING ON GIRT/SLIDE ON 2L DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.SDR AALA201611309018Apu · leakingAIR CONDITIONING SYSTEM DISTRIBUTING A "SWEATY SOCK" AROMA. TROUBLESHOOT CABIN AIR QUALITY,26L00021002. APU SMELL IN CABIN AND 26L00021004- DECONTAMINATION OF THE ENVIRONMENTAL CONTROL SYSTEM (ENGINES AND APU). REPLACED APU. THE AIRCRAFT WAS GROUNDED.SDR AALA201611079015Return Line · leakingAIRCRAFT WAS GROUNDED. PASSENGER COMMENTED ON FUMES IN CABIN IN FLIGHT WHILE EXITING A/C AT DESTINATION. FOUND APU TO BE BAD. REPLACED OIL COOLING FAN AND RETURN LINE PER AMM 49-52-51. (EVENT IS A RE-OCCURANCE SEE ORIGINAL AALA201610289011 AND AALA20161104SDR AALA201611049004Cooling Fan · leakingAIRCRAFT WAS GROUNDED. PASSENGER COMMENTED ON FUMES IN CABIN IN FLIGHT WHILE EXITING A/C AT DESTINATION. FOUND APU TO BE BAD. REPLACED OIL COOLING FAN AND RETURN LINE PER AMM 49-52-51. (EVENT IS A RE-OCCURANCE SEE ORIGINAL AALA201610289011 AND AALA20161107SDR AALA201610289011Cooling Fan · leakingAIRCRAFT WAS GROUNDED. FLIGHT ATTENDANTS REPORTED SULFUR SMELL MID CABIN. MAINTENANCE FOUND THE APU OIL LEAKING OIL FROM THE COOLING FAN, INGESTION INTO THE LOAD COMPRESSOR VERIFIED SINCE THE INTAKE AND DIFFUSER WERE OIL SOAKED. REPLACED COOLING FAN AND ACCSDR AALA201609029001Battery · defectiveAIRCRAFT WAS NOT GROUNDED: FORWARD INBD EMERGENCY FLASHLIGHT NEEDS NEW BATTERY. REPLACED BATTERY.SDR AALA201608089011Battery Pack · failedFORWARD LEFT EMERGENCY POWER SUPPLY UNIT FAILS TEST. REPLACED THE BATTERY IN THE POWER SUPPLY AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 33-51-38.SDR AALA201607289013Wire Harness · puncturedRIGHT PYLON IDG ELECTRICAL FEEDER WIRE HARNESS PUNCTURED. REPLACED RIGHT HAND PYLON IDG ELECTRICAL FEEDER WIRE HARNESS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 24-22-02, ESM 20-44-52, AMM 24-41-00-861-002-A02 AND 24-92-00-400-002-A.SDR AALA201607299016Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON NLG LT AFT DOOR AFT HINGE FITTING. REPLACED HINGE FITTING AND ASSOCIATED HARDWARE IAW AMM 32-22-13-410-001-A.SDR AALA201607189025Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON NLG LT AFT DOOR FORWARD HINGE FITTING. REPLACED HINGE FITTING AND ASSOCIATED HARDWARE IAW AMM 32-22-13-410-001-A.SDR AALA201607299017Pin · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT MLG RETRACTION ACTUATOR PIN WORN. REPLACED PIN IAW AMM 32-31-45-400-001-A.SDR AALA201607299036Floor Panel · delaminatedFLOOR PANEL 241JF IS DELAMINATED. FABRICATED AND INSTALLED A REPLACEMENT FLOOR PANEL IAW SRM 53-02-00 PARA.8.H FIG.209 AND IRM 9701 REVISION G.SDR AALA201607299035Floor Panel · delaminatedFLOOR PANEL 241KF IS DELAMINATED. FABRICATED AND INSTALLED A REPLACEMENT FLOOR PANEL IAW SRM 53-02-00 PARA.8.H FIG.209 AND IRM 9701 REVISION G.SDR AALA201607299033Floor Panel · delaminatedFLOOR PANEL 241HF IS DELAMINATED. FABRICATED AND INSTALLED A REPLACEMENT FLOOR PANEL IAW SRM 53-02-00 PARA.8.H FIG.209 AND IRM 9701 REVISION G.SDR AALA201607079001Striker · out of adjustDURING MAINTENANCE, PASSENGER CREW DOOR 841 DIMENSION A (J2) IS OUT OF ADJUSTMENT BETWEEN FINGER AND STRIKER LEVER DAMPER MECHANISM. ADJUSTED PASSENGER CREW DOOR 841 DIMENSION A (J2) PER AMM 52-11-14-020-00-2-A.SDR AALA201607299032Hinge Pin · corrodedOUTBOARD CENTER HINGE PIN ON RIGHT WING SPOILER NR 2 IS CORRODED. REMOVED AND REPLACED THE HINGE PIN IAW AMM 27-64-42-400-001-A.SDR AALA201607299030Hinge Pin · corrodedOUTBOARD CENTER HINGE PIN ON LEFT WING SPOILER NR 2 IS CORRODED. REMOVED AND REPLACED THE HINGE PIN IAW AMM 27-64-42-400-001-A.SDR AALA201607299029Hinge Pin · corrodedINBOARD CENTER HINGE PIN ON LEFT WING SPOILER NR 2 IS CORRODED. REMOVED AND REPLACED THE HINGE PIN IAW AMM 27-64-42-400-001-A.SDR AALA201607299040Deck Plate · crackedCENTER WING BOX PRESSURE DECK PLATE CRACKED AT FRAME 43 AND +Y1650. REPLACED THE DECK PLATE IAW SRM 51-72-11 AND DRAWING 53370500SDR AALA201607299039Floorbeam · crackedFLOORBEAM CRACKED AT FRAME 43 AND -Y1650. REPAIRED THE FLOORBEAM IAW EO 5315Y066.SDR AALA201607299021Pressure Panel · crackedAIRCRAFT IN BASE MAINTENANCE: CENTER WING BOX PRESSURE PLATE CRACKED AT FRAME 43 AND -Y1650. REPLACED PRESSURE PLATE IAW SRM 51-42-11 AND DWG D53370500.SDR AALA201607299009Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT ELEVATOR NR 4 HINGE ARM FITTING BETWEEN RIB 8 AND 9 HAS EXCESSIVE PLAY. REPLACED HINGE ARM FITTING IAW AMM 55-16-42-400-001-A.SDR AALA201607299007Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT ELEVATOR NR 4 HINGE ARM FITTING BETWEEN RIB 8 AND 9 HAS EXCESSIVE PLAY. REPLACED HINGE ARM FITTING IAW AMM 55-16-42-400-001-A.SDR AALA201607299006Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT ELEVATOR NR 1 HINGE ARM FITTING AT RIB 5 HAS EXCESSIVE PLAY. REPLACED HINGE ARM FITTING IAW AMM 55-16-42-400-001-A.SDR AALA201607299005Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT ELEVATOR NR 6 HINGE ARM FITTING AT RIB 13 HAS EXCESSIVE PLAY. REPLACED HINGE ARM FITTING IAW AMM 55-16-42-400-001-A.SDR AALA201607299004Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RT ELEVATOR NR 5 HINGE ARM FITTING AT RIB 10 HAS EXCESSIVE PLAY. REPLACED HINGE ARM FITTING IAW AMM 55-16-42-400-001-A.SDR AALA201607299003Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RT ELEVATOR NR 3 HINGE ARM FITTING BETWEEN RIB 4 AND 13 HAS EXCESSIVE PLAY. REPLACED HINGE ARM FITTING IAW AMM 55-16-42-400-001-A.SDR AALA201607299002Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RT ELEVATOR NR 2 HINGE ARM FITTING BETWEEN RIB 6 AND 7 HAS EXCESSIVE PLAY. REPLACED HINGE ARM FITTING IAW AMM 55-16-42-400-001-A.SDR AALA201607299001Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RT ELEVATOR NR 1 HINGE ARM FITTING AT RIB 5 HAS EXCESSIVE PLAY. REPLACED HINGE ARM FITTING IAW AMM 55-16-42-400-001-A.SDR AALA201607299034Floor Panel · delaminatedFLOOR PANEL 242LF IS DELAMINATED. FABRICATED AND INSTALLED REPLACEMENT FLOOR PANEL IAW SRM 53-02-00 PARA.8.H FIG.209 AND IRM 9701 REVISION G.SDR AALA201607299031Bolt · corrodedLOWER FORWARD BOLT ON RIGHT WING NR 5 SLAT TRACK IS CORRODED. REMOVED AND REPLACED THE BOLT IAW AMM 27-84-67-400-002-A.SDR AALA201607299024Duct · corrodedAIRCRAFT WAS IN BASE MAINTENANCE. AFT AVIONIC COMPARTMENT AIR DUCT BETWEEN FRAMES 21 - 23 FROM STRINGERS 30 - 32L IS CORRODED ON FLANGE. REMOVED AND REPLACED THE AIR DUCT IAW SRM A319 51-72-11 AND DRAWING D53916795.SDR AALA201607299023Door Sill · corrodedAFT CARGO COMPARTMENT DOOR SILL PROFILE PLATE LOCATED BETWEEN FR.58 AND FR.59 AT S38L IS CORRODED. REMOVED AND REPLACED PROFILE PLATE IAW SRM 51-72-11 AND DRAWING NO D53673930.SDR AALA201607299022Fitting · corrodedAIRCRAFT WAS IN BASE MAINTENANCE. CORNER FITTING IN FORWARD GALLEY AREA AT FRAME 20 AND S23R IS CORRODED. R & R FITTING IAW SRM 51-72-11-001 AND DWG D53112109.SDR AALA201607299028Skin · corrodedCORROSION ON UPPER SKIN BETWEEN FR 40 AND F R42 AND BETWEEN RIB1 AND Y1292. REPAIRED SKIN IAW EA 261850.SDR AALA201607299027Structure · corrodedLOWER SILL BETWEEN FRAMES 66 TO 68, STRINGER 23R IS CORRODED. REMOVED AND REPLACED SILL IAW SRM A319 51-72-11, DWG D53474250, D534800009 AND EA 261873.SDR AALA201607299026Structure · corrodedLOWER SILL BETWEEN FRAMES 66 AND 68 LEFT SIDE AT AFT GALLEY IS CORRODED. REMOVED AND REPLACED LOWER SILL IAW SRM A319 51-72-11, DRAWING D53480009. AND EA # 261664..SDR AALA201607299025Floor Support · corrodedCABIN FLOOR SUPPORT AT -Y765 BETWEEN FRAMES 64 - 66 IS CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D53972816.SDR AALA201607289001Floor Panel · delaminatedCABIN FLOOR PANEL 221PF HAS DELAMINATION. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-201. PARAGRAPH 8H AND IRM 9701 REV G.SDR AALA201607299020Trunnion · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING INBD T/E FLAP, FLAP DRIIVE TRUNNION, TORSION FITTING HAS WEAR MARKS. REPLACED FLAP DRIIVE TRUNNION TORSION FITTING IAW CMM 57-52-21.SDR AALA201607299019Coupling · damagedAIRCRAFT IN BASE MAINTENACE: FLOORBEAM COUPLING AT FRAME 66 AND -Y765 HAS ELONGATED HOLE. REPLACED COUPLING IAW SRM 51-72-11 AND DWG D53972816.SDR AALA201607299018Coupling · damagedAIRCRAFT IN BASE MAINTENANCE: R2 DOOR CUTOUT LOWER SILL COUPLING SPLICE HAS ELONGATED HOLE AT FR 66 AND STRINGER 23 RT. REPLACED COUPLING SPLICE IAW SRM 51-72-11 AND DWG D53474250.
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