N704US

Service difficulty reports · 285

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 = 'N704US' 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.

SDR AALA201807249013Cover · missingEMERGENCY EXIT LIGHT COVER MISSING JUST BELOW LEFT OVERWING EXIT. INSTALLED THE COVER. OK FOR SERVICE.Jul 23, 2018 · N704US · Airbus A319112 · Emergency LightingSDR AALA201805179007Lens · brokenRIGHT OVERWING EMERGENCY EXIT SIGN LENS BROKEN. REPLACED THE LENS IAW AMM 33-51-15.May 16, 2018 · N704US · Airbus A319112 · Emergency LightingSDR AALA201805169016Bottle · low pressureSLIDE BOTTLE LEFT ON CIDS TEST, LOW PRESSURE. MAINTENANCE REPLACED LEFT RESERVOIR BOTTLE IAW AMM 25-62-46, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.May 15, 2018 · N704US · Airbus A319112 · Escape SlideSDR AALA201801249009Power Supply · faultedFORWARD EMERGENCY CABIN POWER SUPPLY FAULTING. REPLACED FORWARD EMERGENCY LIGHT UNIT PER AMM 33-51-38-401.Jan 23, 2018 · N704US · Airbus A319112 · Emergency LightingSDR AALA201712119030Cover · looseAIRCRAFT WAS NOT GROUNDED. 2 LEFT DOOR SLIDE PACK COVER LOOSE. REATTACHED SLIDE COVER PER AMM 25-62-50-400-801C1.Dec 8, 2017 · N704US · Airbus A319112 · Escape SlideSDR AALA201712079025Fan · odorAIRCRAFT WAS NOT GROUNDED. VENT EXTRACT FAULT BURNING SMELL FROM EXTRACT FAN. REPLACED EXTRACT FAN PER AMM REF 21-26-51 P/B 0401. OPERATIONS CHECK NORMALDec 5, 2017 · N704US · Airbus A319112 · Air Distribution FanSDR AALA201712049027Cover · looseAIRCRAFT WAS NOT GROUNDED. SLIDE COVER ON L2 DOOR LOOSE. RESECURED SLIDE COVER (DECORATIVE) ON 2L DOOR PER 25-62-50.Dec 3, 2017 · N704US · Airbus A319112 · Emergency EquipmentSDR AALA201712049013Cover · unsecureAIRCRAFT WAS NOT GROUNDED: SLIDE COVER 2L WOULD NOT STAY ON. RESECURED SLIDE COVER AT 2L AND PERFORMED SUCCESSFUL OPERATIONS CHECK.Dec 1, 2017 · N704US · Airbus A319112 · Emergency EquipmentSDR AALA201710039011Flashlight · inoperativeFLASHLIGHT AT FLIGHT ATTENDANT L2 JUMPSEAT INOPERATIVE. REPLACED THE FLASHLIGHT IAW AMMOct 2, 2017 · N704US · Airbus A319112 · Emergency EquipmentSDR AALA201707319020Battery · dischargedEMERGENCY.EXIT BATTERY AFT LEFT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT BATTTERY .AFT L REF IAW AMM 33-51-38.Jul 30, 2017 · N704US · Airbus A319112 · Emergency LightingSDR AALA201707319060Slide · defectiveWHILE ATTEMPTING SLIDE CHANGE AT THE L2 DOOR, REPLACEMENT SLIDE WAS FOUND TO BE DEFECTIVE FROM STOCK. REINSTALLED L2 DOOR SLIDE IAW JC 26L00025011. SLIDE WAS SENT OUT FOR REPAIR DUE TO BEING UNPACKED, DEPLOYED. VENDOR TESTED AND REPAIRED IAW CMM 25-61-20.Jul 28, 2017 · N704US · Airbus A319112 · Escape SlideSDR AALA201706199030Latch · obstructedEMERGENCY EQUIPMENT DOOR JAMMED. REMOVED DEBRIS FROM DOOR LATCH. OPS CHECKED GOOD.Jun 16, 2017 · N704US · Airbus A319112 · DoorsSDR AALA201706169023Nut · corrodedRIGHT MAIN LANDING GEAR AFT PINTLE PIN, NUT, AND WASHER HAVE PITTING. REMOVED AND REPLACED PIN, NUT AND WASHER.Jun 14, 2017 · N704US · Airbus A319112 · Main Landing Gear Attach SectionSDR AALA201706169001Pin · corrodedRIGHT MAIN LANDING GEAR AFT PINTLE PIN, NUT, AND WASHER HAVE PITTING. REMOVED AND REPLACED PIN, NUT AND WASHER.Jun 14, 2017 · N704US · Airbus A319112 · Main Landing Gear Attach SectionSDR AALA201706159034Fitting · crackedWHILE ACCOMPLISHING WORK CARD 26T14753005 TO INSPECT MLG DOOR KEEL BEAM HINGE AND ACTUATOR FITTINGS, CRACK DETECTED AT LEFT ACTUATOR, AFT FLANGE.KEEL BEAM ATTACH POINT, STRINGER 41L AND FR 42. REPAIRED DOOR ACTUATOR FITTING PER EA # 270779 REVISION A.Jun 12, 2017 · N704US · Airbus A319112 · Fuselage Main, Attach FittingsSDR AALA201706159033Fitting · crackedWHILE ACCOMPLISHING WORK CARD 26T14753005 TO INSPECT MLG DOOR KEEL BEAM HINGE AND ACTUATOR FITTINGS, A CRACK WAS DETECTED AT THE LEFT ACTUATOR, AFT FLANGE.KEEL BEAM ATTACH POINT, STRINGER 41L AND FRAME 42. REPAIRED DOOR ACTUATOR FITTING IAW EA 270779 REVISIOJun 12, 2017 · N704US · Airbus A319112 · Fuselage Main, Attach FittingsSDR AALA201705249006Light · malfunctionedEMERGENCY LIGHTS ON WILL NOT TURN OFF, WHEN SELECTED OFF. EMERGENCY LIGHT SYSTEM CHECKED NORMAL.May 23, 2017 · N704US · Airbus A319112 · Emergency LightingSDR AALA201704059022Lens · missingEMERGENCY LIGHT LENS MISSING AT THE L1 DOOR. REPLACED THE LENS.Apr 4, 2017 · N704US · Airbus A319112 · Emergency LightingSDR AALA201610299004Power Supply · inoperativeAFT CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED CENTER CABIN, RIGHT EMERGENCY POWER SUPPLY UNIT AND AFT CABIN LEFT EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-38.Oct 28, 2016 · N704US · Airbus A319112 · Emergency LightingSDR AALA201610299003Power Supply · inoperativeAFT CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED CENTER CABIN, RIGHT EMERGENCY POWER SUPPLY UNIT AND AFT CENTER CABIN LEFT EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-38.Oct 28, 2016 · N704US · Airbus A319112 · Emergency LightingSDR AALA201610049011Oil System · overservicedFLIGHT CREW REPORTED THAT AN ACID, BURNING RUBBER & MUSTY ODOR CAME ON VERY STRONG RESULTING IN A SLIGHT BURNING IN EYES. DIVERTED WITH NO EMERGENCY WAS DECLARED AND LANDED SAFELY WITH NO FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND THE APOct 1, 2016 · N704US · Airbus A319112 · APU Oil SystemSDR AALA201605129010Lens · missingAIRCRAFT WAS NOT GNDED. EMER LIGHT ABOVE R2 DOOR IS MISSING LENS. INSTALLED NEW LENS IAW AMM 33-51-11-401.May 11, 2016 · N704US · Airbus A319112 · Emergency LightingSDR AALA201603089039Hinge Fitting · excess playAIRCRAFT IN BASE MX. LT ELEVATOR NR 6, HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW AMM 55-16-42.Mar 1, 2016 · N704US · Airbus A319112 · Elevator StructureSDR AALA201603089038Hinge Fitting · excess playAIRCRAFT IN BASE MX. LT ELEVATOR NR 5 HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW AMM 55-16-42.Mar 1, 2016 · N704US · Airbus A319112 · Elevator StructureSDR AALA201602279003Fitting · wornEXCESSIVE PLAY ON BEARING OF FWD FITTING ON LT MLG MAIN DOOR. R & R FWD FITTING ON LT MLG MAIN DOOR IAW CMM 52-81-18.Feb 24, 2016 · N704US · Airbus A319112 · Landing Gear DoorsSDR AALA201602229034Striker · out of adjustAIRCRAFT IN BASE MX. OUT OF ADJUSTMENT DIMENSION A PAX CREW DOOR 842, BETWEEN FINGER & STRIKER LEVER DAMPER MECHANISM. PERFORMED ADJUSTMENT DIMENSION A J2 SENGER CREW DOOR 842, BETWEEN FINGER & STRIKER LEVER DAMPER MECHANISM IAW MM 52-13-14-820-002-A.Feb 21, 2016 · N704US · Airbus A319112 · Passenger/Crew DoorsSDR AALA201603019017Bolt · corrodedAIRCRAFT WAS IN BASE MX. RT WING OTBD FLAP NR 4 TRACK PIVOT BOLT IS CORRODED. REPLACED PIVOT BOLT IAW SRM 51-42-11 & 51-72-11.Feb 20, 2016 · N704US · Airbus A319112 · Trailing Edge FlapsSDR AALA201603159009Skin · delaminatedAIRCRAFT IN BASE MX. RT WING OTBD FLAP HAS DELAMINATION ON THE UPPER SURFACE TE. REPLACED FLAP IAW TASK CARD 26L00027009.Feb 19, 2016 · N704US · Airbus A319112 · Trailing Edge FlapsSDR AALA201602229022Striker · out of adjustAIRCRAFT IN BASE MX. OUT OF ADJUSTMENT DIMENSION A PAX CREW DOOR 841, BETWEEN FINGER & STRIKER LEVER DAMPER MECHANISM. PERFORMED ADJUSTMENT DIMENSION A J2 PAX CREW DOOR 841 IAW AMM 52-11-14-820-002-A.Feb 19, 2016 · N704US · Airbus A319112 · Passenger/Crew DoorsSDR AALA201602229021Slide Raft · deformedDEFORMATION ON SLIDE RAFT PACK ASSEMBLY AT DOOR 841 AT FWD GALLEY AREA. WHEN DOOR IS FULL OPEN, SLIDE & RAFT TOUCH THE FUSELAGE. REPLACED SLIDE.Feb 19, 2016 · N704US · Airbus A319112 · Escape SlideSDR AALA201603089032Access Panel · damagedAIRCRAFT IN BASE MX. LT WING ACCESS PANEL 540HB, HAS AN ELONGATED FASTENER HOLE. REPLACED ACCESS PANEL IAW AMM 57-27-400-002-A.Feb 15, 2016 · N704US · Airbus A319112 · Wing, Plate/SkinSDR AALA201603019023Door Sill · corrodedAIRCRAFT WAS IN BASE MX. CABIN DOOR SILL AT STRINGER 23R IS CORRODED, BETWEEN FRAME 16 & 20. R & R SILL IAW EA 114968.Feb 10, 2016 · N704US · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA201603159003Hinge Fitting · wornAIRCRAFT IN BASE MX. LT WING SPOILER NR 2 CTR HINGE FITTING STOP BOLT WORN. REPAIRED HINGE FITTING IAW SRM 57-70-00 TABLE 202 PARAGRAPH 5 C FIGURE 201.Feb 9, 2016 · N704US · Airbus A319112 · SpoilersSDR AALA201603089041Box Beam · crackedAIRCRAFT IN BASE MX. RT SIDE BOX BEAM FLANGE FASTENER HOLE HAS CRACK INDICATION, AT FRAME 43 & STRINGER 15 RT. REPAIRED BOX BEAM IAW EO 5315Y066.Feb 8, 2016 · N704US · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA201603089040Box Beam · crackedAIRCRAFT IN BASE MX. LT SIDE BOX BEAM FLANGE FASTENER HOLE HAS CRACK INDICATION AT FRAME 43 & STRINGER 15 LT. REPAIRED BOX BEAM IAW EO 5315Y066.Feb 8, 2016 · N704US · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA201603159007Hinge Fitting · excess playAIRCRAFT IN BASE MX. NLG RT AFT DOOR, AFT HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW CMM 52-82-32.Feb 7, 2016 · N704US · Airbus A319112 · Landing Gear DoorsSDR AALA201603159006Hinge Fitting · excess playAIRCRAFT IN BASE MX. NLG RT AFT DOOR, FWD HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW CMM 52-82-32.Feb 7, 2016 · N704US · Airbus A319112 · Landing Gear DoorsSDR AALA201603159002Hinge Fitting · excess playAIRCRAFT IN BASE MX. NLG LT AFT DOOR, FWD HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW CMM 52-82-32.Feb 7, 2016 · N704US · Airbus A319112 · Landing Gear DoorsSDR AALA201603159001Hinge Fitting · excess playAIRCRAFT IN BASE MX. NLG LT AFT DOOR, AFT HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW CMM 52-82-32.Feb 7, 2016 · N704US · Airbus A319112 · Landing Gear DoorsSDR AALA201603019020Hinge Pin · corrodedAIRCRAFT WAS IN BASE MX. NLG TORQUE LINK CTR HINGE PIN IS CORRODED. R & R PIN IAW SRM 51-72-11 & 51-42-11.Feb 7, 2016 · N704US · Airbus A319112 · Nose/Tail Landing Gear Strut/AxleSDR AALA201603159011Skin · saturatedAIRCRAFT IN BASE MX. RT ELEVATOR UPPER SURFACE HAS 5 AREAS WHERE THERE WAS AN INDICATION OF TRAPPED WATER, BETWEEN ELEVATOR STATIONS 131 & 527, & BETWEEN RIB 2 & 9. REPAIRED ELEVATOR IAW SRM 55-21-11-2011.Feb 5, 2016 · N704US · Airbus A319112 · Elevator, Plate/SkinSDR AALA201603159010Skin · saturatedAIRCRAFT IN BASE MX. RT ELEVATOR LOWER SURFACE HAS 1 AREA WHERE TRAPPED WATER WAS INDICATED, BETWEEN ELEVATOR STATIONS 131 - 181 & BETWEEN RIB 1 & 2. REPAIRED ELEVATOR IAW SRM 55-21-11-201-1.Feb 5, 2016 · N704US · Airbus A319112 · Elevator, Plate/SkinSDR AALA201603089034Floor Panel · delaminatedAIRCRAFT IN BASE MX. AFT GALLEY FLOOR PANEL 261DF HAS DELAMINATION. REPLACED FLOOR PANEL IAW SRM 53-02-00-201& IRM 9701 REV G.Feb 5, 2016 · N704US · Airbus A319112 · Fuselage Floor PanelSDR AALA201603049014Floor Panel · delaminatedAIRCRAFT IN BASE MX. AFT GALLEY FLOOR PANEL 261PF HAS DELAMINATION. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701 REV G.Feb 5, 2016 · N704US · Airbus A319112 · Fuselage Floor PanelSDR AALA201603049013Floor Panel · delaminatedAIRCRAFT IN BASE MX. FLOOR PANEL 212EF HAS DELAMINATION. REPLACED FLOOR PANEL IAW SRM 53-12-00 & IRM 9701 REV G.Feb 5, 2016 · N704US · Airbus A319112 · Fuselage Floor PanelSDR AALA201603049008Floor Panel · delaminatedAIRCRAFT IN BASE MX. AFT GALLEY FLOOR PANEL 261BG HAS DELAMINATION. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701 REV G.Feb 5, 2016 · N704US · Airbus A319112 · Fuselage Floor PanelSDR AALA201603049006Floor Panel · delaminatedAIRCRAFT IN BASE MX. AFT GALLEY FLOOR PANEL 261AG HAS DELAMINATION. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701 REV G.Feb 5, 2016 · N704US · Airbus A319112 · Fuselage Floor PanelSDR AALA201603159012Skin · saturatedAIRCRAFT IN BASE MX. LT ELEVATOR UPPER SURFACE HAS 3 AREAS WHERE THERE WAS INDICATION OF TRAPPED WATER, BETWEEN ELEVATOR STATION 131 - 466, & BETWEEN RIB 2 - 9. REPAIRED ELEVATOR IAW SRM 55-21-11-2011.Feb 4, 2016 · N704US · Airbus A319112 · Elevator, Plate/SkinSDR AALA201603159008Skin · saturatedAIRCRAFT IN BASE MX. RUDDER RT SURFACE SKIN HAS 2 AREAS WHERE THERE WAS INDICATION OF TRAPPED WATER, BETWEEN 14.7" & 15.25" FROM THE TE & BETWEEN 17" & 19.5", FROM THE LOWER EDGE & 1 AREA OF DELAMINATION, 14.7" FROM THE TE & 26.47" FROM THE LOWER EDGE. RUDDEFeb 4, 2016 · N704US · Airbus A319112 · Rudder, Plate/SkinSDR AALA201603089037Coupling · damagedAIRCRAFT IN BASE MX. COUPLING AT FRAME 66 & STRINGER 23 RT HAS ELONGATED HOLE. REPLACED COUPLING IAW SRM 51-72-11.Feb 4, 2016 · N704US · Airbus A319112 · Fuselage Miscellaneous Structure
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