N855UA

Service difficulty reports · 89

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 = 'N855UA' 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 CALA2014063091365Warning System · false indicationCREW REPORTS WHILE ATTEMPTING NR 1 ENG START RECEIVED ENG 1 START FAULT WITH EGT OVER LIMIT. CHECKED EXCEEDANCE PAGE & NO OVERTEMP OCCURRED. CHECKED INLET & EXHAUST, NO DEFECTS NOTED. APU BLEED SYS INOPERATIVE.Jun 29, 2014 · N855UA · Airbus A319131 · Engine EGT/TIT Indicating SystemSDR CALA2014012290209Apu · shutdownECAM MESSAGE APU AUTO SHUTDOWN DISPLAYED ON UPPER ECAM SCREEN APU. NO START 2ND ATTEMPT, CREW ASSISTED BY TRYING ANOTHER APU START, START WAS GOOD. APU IS OPERATING NORMALLY, OK TO CONTINUE.Jan 21, 2014 · N855UA · Airbus A319131 · APU Core EngineSDR CALA2013111492939Acoustic Liner · damagedNR 2 ENG ACOUSTICAL PANEL CHUNK MISSING 6 O'CLOCK WITH ANOTHER SMALLER PIECE LOOSE. INSPECTED FAN CASE ATTRITION LINER IAW MT72-017 REV E. REMOVED LOOSE PIECE OF LINER APPROXIMATELY 0.250 INCH DIAMETER. DAMAGE IS LESS THAN 20% OF PANEL & TO BE REPAIRED WITHNov 13, 2013 · N855UA · Airbus A319131 · Turbine Engine Air Inlet SectionSDR CALA2013082190646Floor Panel · delaminatedAFT CARGO COMPARTMENT. FLOOR PANEL 151VG IS DELAMINATED. DELAMINATED MEASURES APPROX. 4.5 FT LONG X 2.5 FT WIDE, 6 INCHES FROM FWD EDGE, 6 INCHES FROM RT EDGE, ALL THE WAY INCLUDING AFT EDGE. R & R THE AFT CARGO BAY FLOOR PANEL IAW AMM 53-42-14 & ECRA 5342- Aug 21, 2013 · N855UA · Airbus A319131 · Fuselage Floor PanelSDR UALA2013071104854Liner · unsecureNR 1 ENGINE AT APPROX 9 O'CLOCK HAS SECTION OF ATTRITION LINER HAS LIBERATED. AFFECTED AREA IS ACTUALLY A PREVIOUSLY REPAIRED AREA THAT IS LOOSE.Jul 10, 2013 · N855UA · Airbus A319131 · Engine (Turbine/Turboprop)SDR UALA2013061204011Door · unsecureLIGHT AIRFRAME VIBRATION DURING CLIMB THROUGH FL250 AT 302KTS. VIBRATION GONE SLOWING TO 290 KTS. FOLLOW MT 53-005 FOR VIBRATION TROUBLESHOOTING. CHECKED NLG DOORS NO DEFECTS NOTED REF AMM. FOUND ELECTRICAL RECEPTACLE DOOR LOOSE ADJUSTED DOOR REF AMM 52-4Jun 6, 2013 · N855UA · Airbus A319131 · Accessory Compartment DoorsSDR UALA2013021200845Line · leakingHYD LEAK NR 4 BRAKE. LEAK COMING FROM HARD LINE BETWEEN NR 4 BRAKE SERVO VALVE AND BRAKE CONT MODULE ON RIGHT GEAR. LINE APPEARS TO BE PINCHED AT THE AREA THAT IS LEAKING. REPAIRED LINE WITH RYNGLOK REPAIR REF GPM 1-0-13-028. LEAK CHECKS OKAY.Feb 6, 2013 · N855UA · Airbus A319131 · Landing Gear Brake SystemSDR UALA2012121407228Skin · gougedAFT CARGO DOOR LOWER CUTOUT SKIN EDGE HAS GOUGE LOCATED BELOW ROLLER LOCK FITTING NR 2. BLENDED GOUGE PER SRM 53- 41-11, FIG 104 ORIG MAT .236, MAT LOSS .018, MAT REMAINING .218 IS WITHIN LIMITS. THIS GOUGE BLEND OUT PER SRM 53-41-11, FIG 104 WITH MAT LOSS .Dec 13, 2012 · N855UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR UALA2012120406949Servo · out of limitsCREW REPORT: LIGHT AIRFRAME VIBRATION DURING CLIMB. VERY NOTICEABLE IN COCKPIT AND AFT CABIN ALONG VERTICAL ACP CHECK OF THE RUDDER TRAILING PLAY REF AMM. FOUND BLUE SYSTEM SERVO TO BE OUT OF LIMITS, APPROX 14MM OF PLAY, MAX ALLOWED IS 8MM. FOUND YELLOW ANDDec 4, 2012 · N855UA · Airbus A319131 · Rudder Control SystemSDR UALA2012070103498Valve · failedCHRONIC MODERATE AIRFRAME VIBRATION. SLIGHT RUDDER INPUT CEASES VIBRATION. REPLACED BOTH ELEVATOR SERVO CONTROL VALVES PER MM.Jun 27, 2012 · N855UA · Airbus A319131 · Elevator Control SystemSDR UALA2012060503086Computer · malfunctionedFLIGHT DIVERTED FOR FUEL TRANSFER ISSUE. NR 1 FUEL TANK QTY FLUCTUATES BY 1000 LBS. FLUCTUATIONS ARE IN LT WING, INBD TANK. REPLACED 3 QT FQIC IAW AMM, OPS CHECKED OK.Jun 4, 2012 · N855UA · Airbus A319131 · Fuel Indicating SystemSDR UALA2012052202879Unknown · odorF/A REPORTED SLIGHT ODOR NEAR L1 DOOR GALLEY AREA. ODOR DISSIPATED AFTER LDG GEAR EXTENSION. COULD NOT DUPLICATE ODOR ON GROUND.May 21, 2012 · N855UA · Airbus A319131 · Air Distribution SystemSDR UALA2012011600324Sleeve · delaminatedNR 1 THRUST REVERSER SYSTEM INOPERATIVE. SAMC COMMENTS: REVERSER INOPED DUE TO SLEEVE OUTER W ALL ACCOUSTIC MESH DELAMINATED. OPBLM-EMC SAMC TEXT: REVERSER CAN BE REACTIVATED AFTER SLEEVE REPAIR IS ACCOMPLISHED. OPBLM-EMC :LCL MAINT DEACTIVATED ENG 1 THRUSJan 14, 2012 · N855UA · Airbus A319131 · Engine Thrust ReverserSDR UALA2011111406196Light · malfunctionedF/A'S REPORT EMER EXIT LIGHTING CYCLING ON AND OFF INTERMITTENTLY. INBOARD CREW STATED IT DID NOT CYCLE AFTER CYCLING THE SWITCH. TESTED LIGHT NORMAL.Nov 12, 2011 · N855UA · Airbus A319131 · Emergency LightingSDR UALA2011092905276Fmu · malfunctionedREJECTED TAKEOFF AT 100 KNOTS. ACFT YAWED TO THE RIGHT. MAX AUTOBRAKES ENGAGED ACCOMPLISH INSPECTION IAW AMM, INSPECTION AFTER BRAKE EMERGENCY APPLICATION. FOR REFERENCE, THE FLT CREW REPORTED THAT THEY DID NOT SEE ANY BRAKE TEMPS OVER 510. ACCOMPLISHED BRSep 29, 2011 · N855UA · Airbus A319131 · Fuel Controlling SystemSDR UALA2011050302170Seal · missingAFT HALON FIRE EXTINGUISHER SEAL MISSING. REPLACED FIRE EXTINGUISHER.May 3, 2011 · N855UA · Airbus A319131 · Extinguishing SystemSDR UALA2011042702039Valve · failedSMOKE - FIRE FROM TAILPIPE OF THE NR 1 ENGINE AND OIL IN TAILPIPE AFTER ENGINE SHUTDOWN. ACCOMPLISHED INITIAL TBLSHTG PER AMM MT72-022, MT 72-033, NO DEFECTS NOTED. ACCOMPLISHED MT72-022 AND MT72-033 NO COKING FOUND. SCAVENGE PUMP AND NR 4 BEARING SCAVANGEApr 26, 2011 · N855UA · Airbus A319131 · Turbine Engine Oil SystemSDR UALA2011020800670Element · faultedNR 1 ENG BLEED LEAK MESSAGE, RTFL. MECHANIC REPORTED STALL OF NR 1 ENG DURING HIGH POWER RUN WITH ECAM STALL MESSAGE. ACCOMPLISHED TSM FOR NR 1 ENGINE STALL. REPLACED NR 1 ENG 1HF1 OVERHEAT SENSING ELEMENT PER AMM, OPERATIONAL TEST OF THE OVERHEAT DETECTIONFeb 8, 2011 · N855UA · Airbus A319131 · Overheat DetectionSDR UALA2010101103768Servo · faultySPOILER 4 ECAM FAULT, FLIGHT DIVERTED. REPLACED NR 4 RT SERVO. FOUND FAULTY. REPLACED NO. 4 RT SERVO. PER SAMC THE AIRPLANE CAN BE RELEASED BACK TO SVC.Oct 10, 2010 · N855UA · Airbus A319131 · Drag Control SystemSDR UALA2009113003693Battery · no testCABIN EMERGENCY LIGHT BATTERY BITE TEST FAILED ON LT AISLE. SWAPPED BATTERY WITH ONE FROM SPARES. NO HELP. BATTERY AND NEW UNIT ON ORDER. REPLACED BATTERY ON LT OW DOOR. OPS CKD GOOD.Nov 28, 2009 · N855UA · Airbus A319131 · Emergency LightingSDR UALA2009071702114Structure · damagedNR 1 PYLON HAS SUSTAINED DAMAGE. APPLYING UA-EVA 72783B TIME LIMITED REPAIR. RECEIVED LAST FASTENERS FOR THE DOUBLER REPAIR, INSTALLED & SOLD.Jul 17, 2009 · N855UA · Airbus A319131 · Nacelle/Pylon Miscellaneous StructureSDR UALA2009070801971Line · leakingGREEN HYD LO LEVEL ON ECAM QTY ZERO ON HYD PAGE. FOUND 1\ GRN SYS HYD PRESS LINE IN NR 1 PYLON CHAFED THROUGH AT CLAMPING LOCATION.Jul 8, 2009 · N855UA · Airbus A319131 · Hydraulic System, MainSDR 2008UALA05924Smoke Detector · faultyLAVATORY DET FAULT DISPLAYED ON UPPER ECAM SCREEN - SMOKE. REPLACED SMOKE DETECTOR FWD AFT LAVATORY.Sep 28, 2008 · N855UA · Airbus A319131 · Smoke DetectionSDR 2008UALA01827Structure · gougedL2 DOOR GOUGED IN SEVERAL PLACES ALONG BOTTOM OF DOOR. THIS IS A MAJOR REPAIR. BLENDED AREA WITHIN LIMIT REF SRM 52-13-00. NDT NO CRACKS FOUND.Mar 31, 2008 · N855UA · Airbus A319131 · Passenger/Crew DoorsSDR 2008UALA01205Power Supply · no testRT OVERWING EXIT EMERGENCY LIGHT POWER SUPPLY UNIT WILL NOT TEST. REPLACED POWER SUPPLY UNIT.Mar 4, 2008 · N855UA · Airbus A319131 · Emergency LightingSDR 2008UALA01204Battery · failedBATTERY FAULT LIGHT ILLUMINATED ON AFT CABIN EMERGENCY LIGHT POWER SUPPLY UNIT. FOUND THE BATTERY FAILED. REPLACED BATTERY.Mar 4, 2008 · N855UA · Airbus A319131 · Emergency LightingSDR 2008UALA01203Girt Bar · dirtyDOOR 1R AFT GIRT BAR FITTING STOP LEVER MECHANISM STUCK IN DOWN POSITION. FOUND DIRTY FITTING. CLEANED AND LUBED FITTING. OPS CHECKED NORMAL.Mar 4, 2008 · N855UA · Airbus A319131 · Emergency EquipmentSDR 2008UALA00385Proximity Sensor · faultyRTFL DUE TO FWD CARGO DOOR OPEN INDICATION. PROX SNSR 30WV TGT POS ECAM. PROX SENSOR FAILURE. REPLACED PROX SENSOR 30 WV. OPS CHECKED NORMAL. NO REPEATS.Jan 20, 2008 · N855UA · Airbus A319131 · Door Warning SystemSDR 2008UALA00315Proximity Switch · failedRTFL WITH A CARGO DOOR INDICATION PROBLEM. PROX SWITCH 30WV FAILED CAUSING FWD CARGO DOOR ECAM MESSAGE. REPLACED/ADJUSTED PROX SWITCH 30 WV. OPS CHECKED OK.Jan 20, 2008 · N855UA · Airbus A319131 · Door Warning SystemSDR 2007UALA04179Tiller · malfunctionedCAPTAIN'S NOSEWHEEL STEERING TILLER IS OVERLY SENSITIVE TO INPUTS. TOO MUCH TENSION. 10-26-07 ACP FUNCTIONAL CHECK OF NOSE WHEEL STEERING PER AMM -FOUND NO IRREGS. CHECK BSCU FOUND NO FAULTS. TAXI CHECK GOOD. COULD NOT DUPLICATE CONDITION DESCRIBED BY PIOct 12, 2007 · N855UA · Airbus A319131 · Landing Gear Steering SystemSDR 2007UALA01524Battery Pack · faultyCIDS TEST -EPSU BATTERY EMER R- ATA 33-51- 38. REPLACED BATTERY PACK.May 17, 2007 · N855UA · Airbus A319131 · Emergency LightingSDR 2007UALA01468Battery Pack · faultyEMERGENCY LIGHTS EPSU BATTERY EMERGENCY LEFT MESSAGE. REPLACED BATTERY PACK. GROUND CHECKS OKAY.May 10, 2007 · N855UA · Airbus A319131 · Emergency LightingSDR 2007UALA00658Bottle · reads lowDOOR BOTTLE AT 2L REPORTED LOW. [SUP 05-24-07] SERVICED BOTTLE TO PROPER PRESSURE.Mar 3, 2007 · N855UA · Airbus A319131 · Passenger/Crew DoorsSDR 2006UALA02375Cylinder · low pressureLOW PRESSURE ON CYLINDER. WATER BATHED FOR 1 HOUR AND FOUND NO LEAKS. REPLACED VALVE AND REBUILT VALVE.Dec 15, 2006 · N855UA · Airbus A319131 · Escape SlideSDR 2006UALA01760Structure · damagedNR 1 PYLON CANTILEVER STRUCTURE DAMAGED FROM CONTACT WITH JET WAY.Sep 13, 2006 · N855UA · Airbus A319131 · Nacelle/Pylon, Main FrameSDR 2006UALA01006Power Supply · failedEMERGENCY LIGHT TEST FAILS. FAULT MESSAGE EPSU RIGHT EMERGENCY LIGHT. REPLACED RIGHT EMERGENCY POWER SUPPLY AND BATTERY. OPS CHECK GOOD.May 16, 2006 · N855UA · Airbus A319131 · Emergency LightingSDR 2005UALA01425Wire · misinstalledRIGHT AFT DOOR OVER THE DOOR EMERGENCY LIGHT INOP, EXIT SIGN WORKS NORMAL. FOUND LIGHT MISWIRED. ADJ WIRE CONNECTION OPS CHECK GOOD.Dec 8, 2005 · N855UA · Airbus A319131 · Light System WiringSDR 2005UALA00989Warning Light · illuminatedCREW REPORTS SMOKE WARNING FOR AFT CARGO PIT. NTERROGATED SYSTEM AND UNABLE TO VERIFY FAULT FOR AFT CARGO COMPARTMENT SMOKE DETECTION. REPLACED SDU PER AMM 26-17-34. REPLACED AFT CARGO COMPARTMENT SMOKE DETECTOR PER AMM 26-16-15. REPLACED AFT CARGO FIRE Sep 15, 2005 · N855UA · Airbus A319131 · Smoke DetectionSDR 2005UALA00617Bulkhead · cutDAMAGE CUT THROUGH SKIN FWD OF PRESSURE BULKHEAD APPROX 6 INCHES LONG AND 8-9 INCHES WIDE. INSTALLED DOUBLER REPAIR AND SPLICED STRINGER SECTION REF UA EVA-50432 AND SRM53-00-11 FI G 227.Jul 1, 2005 · N855UA · Airbus A319131 · Fuselage Main, Bulkhead
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