N722US

Service difficulty reports · 299

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 = 'N722US' 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 AALA201508049003Power Supply · inoperativeSEVERAL EMER LIGHTS OUT. R & R CABIN EMER POWER SUPPLY & BATTERY. OPERATIONS CHECKED GOOD.Aug 3, 2015 · N722US · Airbus A319112 · Emergency LightingSDR AALA201507209009Carbon Seal · leakingFLIGHT 736 EN-ROUTE, EXCESSIVE OIL CONSUMPTION ON LT ENG, REACHING A PEAK OF 2 QTS PER HOUR. DECLARED AN EMER FOR A STRAIGHT IN APPROACH & LANDED WITHOUT FURTHER INCIDENT. REPLACED STARTER DRIVE PAD CARBON SEAL ON LT ENG IAW AMM 72-63-00-300-002-A6 & SUPPLEMJul 18, 2015 · N722US · Airbus A319112 · Turbine Engine Oil SystemSDR USAA2015010500003Megaphone · inoperativeRON VISIT, AFT CABIN MEGA PHONE INOPERATIVE. REPLACED AFT CABIN MEGA PHONE. OPERATIONS CHECKED GOOD.Jan 3, 2015 · N722US · Airbus A319112 · Emergency EquipmentSDR USAA2014121500001Fan · malfunctionedRETURNED TO GATE FOR SMOKE IN THE COCKPIT. VENT EXTRACT FAULT OCCURRED SHORTLY AFTER ENG START & TAXI STARTED. REPLACED AVIONICS EXTRACT FAN.Dec 12, 2014 · N722US · Airbus A319112 · Air Distribution FanSDR USAA2014110300024Cover · unsecureECAM EMER EXIT DOOR LT COVER CAME OFF DURING FLIGHT. INSTALLED COVER & PERFORMED ADJUSTMENT TEST IAW AMM 52-21-11-400-001A, SUBTASK 700-050-B. OK FOR SERVICE.Oct 31, 2014 · N722US · Airbus A319112 · Emergency ExitsSDR USAA2014103100004Cover · unsecureCOVER FELL OFF LT OVERWING EXIT HANDLE. REINSTALLED OVERWING EXIT PANEL IAW AMM 25-60-00. CHECKED OK.Oct 30, 2014 · N722US · Airbus A319112 · Emergency ExitsSDR USAA2014102700011Cover · unsecureON TAXI IN GOT DOOR LT EMER EXIT ECAM. FLIGHT ATTENDANT SAYS COVER CAME OFF. EXAMINED OVERWING EXIT DOOR HANDLE & COVER MOUNT AREA, ALL CHECKED NORMAL. REINSTALLED COVER, SYS NORMAL.Oct 24, 2014 · N722US · Airbus A319112 · Emergency ExitsSDR USAA2014102000020Floorbeam · corrodedCORROSION ON FLOORBEAM BETWEEN FRAME 67 TO 69 Z-500 -Y1162.5. REPLACED FLOORBEAM BETWEEN FRAME 67 TO 69 Z-500 -Y1162.5 IAW SRM 51-42-11 & 51-72-11.Oct 17, 2014 · N722US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2014102000019Floorbeam · corrodedLEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FRAME 64 TO 66 Z-500 -Y1292. REPLACED FLOORBEAM BETWEEN FRAME 64 TO 66 Z-500 -Y1292 IAW SRM 51-42-12.Oct 17, 2014 · N722US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2014102000018Door Sill · corrodedLEVEL 2 INTERGRANULAR CORROSION ON RT AFT R2 DOOR SILL PLATE BETWEEN FRAME 66 TO 68, Z-500 -Y1589. REPLACED RT AFT R2 DOOR SILL PLATE BETWEEN FRAME 66 TO 68 Z-500 -Y1589 IAW SRM 51-42-11 & DWG 53480505.Oct 17, 2014 · N722US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2014101300015Plate · wrong partWHILE INSTALLING A NEW SERVICEABLE SLIDE FOUND TO HAVE IMPROPER BACKING PLATE. THERE WAS NO SLOTS CUT INTO TOP OF BACKING PLATE TO LET SLIDE COVER BE INSTALLED. FOUND ELEC WIRE EXTENSION WILL NOT ROUTE PROPERLY. RETURNED TO STOCK UNSERVICEABLE.Oct 10, 2014 · N722US · Airbus A319112 · Escape SlideSDR USAA2014072500001Container · faultyWHILE ACCOMPLISHING OPERATIONAL CHECKS OF MANUAL MASK RELEASE IAW AMM 35-23-00-710-001-A, THE AFT RT FLIGHT ATTENDANT OXYGEN CONTAINER & SEAT ROW 16ABC OXYGEN CONTAINER DID NOT OPEN CORRECTLY. REPLACED & REINSTALLED OXYGEN CONTAINERS AT AFT RT FLIGHT ATTENDANJul 24, 2014 · N722US · Airbus A319112 · Crew Oxygen SystemSDR USAA2014062400003Slide · unserviceableTHE 2L SLIDE PACK COVER FALLS OFF EVERY TIME 2L DOOR IS USED. THE 2L DOOR SLIDE ASSEMBLY PACKED WRONG. R & R SLIDE PACK ASSEMBLY IAW JOB CARD 26L00025011, DOOR ESCAPE SLIDE RAFT REPLACEMENT. OPERATIONS CHECKED OK.Jun 24, 2014 · N722US · Airbus A319112 · Escape SlideSDR USAA2014061200015Slide Raft · bulgedWHILE ACCOMPLISHING MOD, 2514Y110 SLIDE RAFT INSPECTION, FOUND R2 SLIDE COVER CONTACTING FUSELAGE. LIGHT ABRASION WAS FOUND. REPLACED DOOR R2 SLIDE RAFT IAW JOB CARD 26L00025011.Jun 12, 2014 · N722US · Airbus A319112 · Escape SlideSDR USAA2014061200014Slide Raft · unserviceableWHILE ACCOMPLISHING MOD, 2514Y110 SLIDE RAFT INSPECTION, FOUND R1 SLIDE COVER CONTACTING FUSELAGE. LIGHT ABRASION WAS FOUND. REPLACED SLIDE RAFT IAW ROUTINE WORK CARD 26L0002501.Jun 12, 2014 · N722US · Airbus A319112 · Escape SlideSDR USAA2014061200013Slide Raft · unserviceableWHILE ACCOMPLISHING MOD, 2514Y110 SLIDE RAFT INSPECTION, FOUND L1 SLIDE COVER CONTACTING FUSELAGE. LIGHT ABRASION WAS FOUND. REPLACED SLIDE RAFT IAW ROUTINE WORK CARD 26L00025011.Jun 12, 2014 · N722US · Airbus A319112 · Escape SlideSDR USAA2014061200012Slide Raft · bulgedWHILE ACCOMPLISHING MOD, 2514Y110 SLIDE RAFT INSPECTION, FOUND L2 SLIDE COVER CONTACTING FUSELAGE. LIGHT ABRASION WAS FOUND. REPLACED L2 DOOR SLIDE RAFT IAW JOB CARD 26L0025011.Jun 12, 2014 · N722US · Airbus A319112 · Escape SlideSDR USAA2014060300005Windshield · crackedEN ROUTE FROM CUN TO PHL, CREW REPORTED THE RT WINDSHIELD HEAT SPARKED & ARCED, THEN CRACKED OUTER PANE. RT WINDSHIELD HEAT INOPERATIVE MEMO ON ECAM. R & R RT WINDSHIELD & RT WINDOW HEAT COMPUTER IAW AMM 56-11-11-000-001-A, 56-11-11-400-001-A, 30-42-34-000-0Jun 2, 2014 · N722US · Airbus A319112 · Flight Compartment WindowsSDR USAA2014021800002Engine · leakingAT CRUISE ALTITUDE FL390, CREW NOTICED NR 2 ENG OIL QTY AT 7.0 QUARTS. LEFT TPA GATE ABOUT AN HOUR PRIOR WITH 18.5 QUARTS ON BOTH ENGS. SOON AFTER, OIL QTY NR 2 CONTINUED TO DECREASE. CREW DECLARED AN EMERGENCY & DIVERTED TO CLT. SHUTDOWN NR 2 ENG AS PRECAFeb 17, 2014 · N722US · Airbus A319112 · Engine (Turbine/Turboprop)SDR USAA2013112100001Light · inoperativeMAINTENANCE REPORTED THE R2 DOOR LOW LEVEL DOOR JAM WALL MOUNTED EMERGENCY LIGHT INOPERATIVE. MX REPLACED R2 DOOR LOW LEVEL DOOR JAM EMERGENCY LIGHT ASSEMBLY AS NECESSARY, OPERATIONS CHECKED OK.Nov 20, 2013 · N722US · Airbus A319112 · Emergency LightingSDR USAA2013100800002Lens · missingSEAT 1C EMERGENCY LIGHTING INOPERATIVE. REPLACED LENS.Oct 7, 2013 · N722US · Airbus A319112 · Emergency LightingSDR USAA2013093000009Control Unit · faultyCREW REPORTED A CLASS II MESSAGE MX SDCU. MX R & R SDCU IAW AMM 26-17-34-400-001-A. BITE TEST AND OPS CHECK GOOD.Sep 27, 2013 · N722US · Airbus A319112 · Smoke DetectionSDR USAA2013090300025Battery · inoperativeAFT EMERGENCY FLASHLIGHT BATTERY PACK INOPERATIVE. REPLACED THE BATTERY PACK ON AFT RT EMERGENCY FLASHLIGHT.Sep 1, 2013 · N722US · Airbus A319112 · Emergency EquipmentSDR USAA2013080500013Cover · unsecureCREW REPORTED THE LT OVERWING EMERGENCY EXIT ECAM ILLUMINATED IN FLIGHT AND CAB OK. MX REINSTALLED LT OVERWING EMERGENCY EXIT DOOR COVER. OPS CHECKS GOOD.Aug 2, 2013 · N722US · Airbus A319112 · Emergency ExitsSDR USAA2013061700027Chiller · faultyCREW REPORTED A MODERATE ELECTRICAL BURNING ODOR IN AFT GALLEY. MX R & R THE AFT CHILLER. OPS CHECK GOOD IAW AMM 25-34-51, PB 401.Jun 14, 2013 · N722US · Airbus A319112 · Buffet/GalleysSDR USAA2013040100025Girt Bar · out of positionMAINTENANCE FOUND THE R1 DOOR HARD TO OPEN. MAINTENANCE FOUND R1 GIRT BAR OUT OF POSITION. REPOSITION GIRT BAR R1 DOOR. OPS CHECK NORMAL PER AMM 52-20-00. R1 DOOR OPS CHECK GOOD.Mar 30, 2013 · N722US · Airbus A319112 · Emergency EquipmentSDR USAA2013010800020Lens · missingMAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY EXIT LIGHT LENS MISSING ON SEATS 6C AND 16C. MAINTENANCE INSTALLED NEW SEAT MOUNTED EMERGENCY EXIT LIGHT LENS ON SEATS 6C AND 16C PER AMM 33-51-18, PB 401.Jan 8, 2013 · N722US · Airbus A319112 · Emergency LightingSDR USAA2012121300009Nut · wornMAINTENANCE REPORTED THE LT OVERWING SLIDE BOTTLE KNURLED NUT SAFETY WIRE HOLE IS WORN. MAINTENANCE REPLACED THE LEFT ESCAPE SLIDE RESERVOIR ASSEMBLY PER AMM 25-62-46-001-A. OPS CHECK GOOD.Dec 13, 2012 · N722US · Airbus A319112 · Escape SlideSDR USAA2012032600034Fcu · malfunctionedELECTRICAL & CHEMICAL ODORS DETECTED ON FLIGHT DECK. REMOVED AND REPLACED FLIGHT CONTROL UNIT PER AMM 22-81-400-001. OPS CHECKED GOOD.Mar 24, 2012 · N722US · Airbus A319112 · Flight ControllerSDR USAA2012012000010Cylinder · low pressureL1 DOOR ASSIST CYLINDER PRESSURE LOW. SERVICED L1 DOOR ASSIST CYLINDER IAW AMM 52-10-11-614-001.Jan 19, 2012 · N722US · Airbus A319112 · Passenger/Crew DoorsSDR USAA2011101900009Stowage Box · defectiveF/O'S OXYGEN PANEL DOES NOT TEST PROPERLY - PRESS TO TEST IS VERY BRIEF AND NO FLOW WITH RED EMERGENCY PRESSED. MAINTENANCE REMOVED AND REPLACED F/O'S OXYGEN PANEL BOX IAW AIRBUS MAINTENANCE MANUAL 35-12-41-000-001, 35-12-41-400-001 AND 35-12-41-710-001.Oct 18, 2011 · N722US · Airbus A319112 · Crew Oxygen SystemSDR USAA2011081800007Girt Bar · out of adjustDOOR R2 ARMING LEVER IS NOT SEATED AGAINST SWITCH. SHOWS DOOR UNARMED IN FLIGHT. FLIGHT ATTENDANT CAN MOVE ARMING LEVER 1/4 INCH TOWARD ARMED POSITION AND SHOWS ARMED OK. ADJUSTED ESCAPE SLIDE GIRT BAR TRAVEL PER AIRBUS MAINTENANCE MANUAL 52-13-22-99-011. Aug 15, 2011 · N722US · Airbus A319112 · Emergency EquipmentSDR USAA2011081500014Unknown · malfunctionedR2 DOOR PRESSURE LIGHT STARTED FLASHING DURING FLIGHT. DOOR SLIDE SHOWED DISARMED ON ECAM. PERFORMED FUNCTIONAL TEST OF VISUAL INDICATOR OF DOOR LOCKING MECHANISM PER AIRBUS MAINTENANCE MANUAL 52-10-720-004 AND TROUBLESHOOTING MANUAL 52-13-00-810-816, NO FAUAug 13, 2011 · N722US · Airbus A319112 · Passenger/Crew DoorsSDR USAA2011081500016Warning System · false activationIN FLIGHT AT 1800 THE LEFT OVERWING EMERGENCY EXIT ILLUMINATED ON ECAM. PRESSURIZATION WAS NORMAL. PERFORMED OPERATIONAL TEST OF THE EMERGENCY EXIT HATCH AND ESCAPE SLIDE ARMING AND DISARMING PER AIRBUS MAINTENANCE MANUAL 52-21-00-710-005, NO FAULTS FOUND.Aug 12, 2011 · N722US · Airbus A319112 · Door Warning SystemSDR USAA2011081200008Skin Panel · corroded2S CHECK - CORROSION ON EXTERNAL FUSELAGE SKIN PANEL AT FR 63+8 INCHES BETWEEN S40L TO S43L. REPAIRED EXTERNAL FUSELAGE SKIN PANEL AT FR 63+8 INCHES BETWEEN S40L TO S43L IAW EA 133741.Aug 10, 2011 · N722US · Airbus A319112 · Fuselage Main, Plate/SkinSDR USAA2011081200007Access Panel · delaminated2S CHECK - DELAMINATION ON ACCESS PANEL 325AL LEFT ON VERTICAL STABILIZER. REPLACED ACCESS PANEL 325AL LEFT ON VERTICAL STABILIZER IAW A319 SRM 53-55-11 & 51-72-11.Aug 2, 2011 · N722US · Airbus A319112 · Vertical Stabilizer, Plate/SkinSDR USAA2011081100009Access Panel · delaminated2S CHECK - DELAMINATION ON ACCESS PANEL 325AR RIGHT ON VERTICAL STABILIZER. REPLACED ACCESS PANEL 325AR RIGHT ON VERTICAL STABILIZER IAW A319 SRM 53-55-11 & 51-72-11.Aug 2, 2011 · N722US · Airbus A319112 · Vertical Stabilizer, Plate/SkinSDR USAA2011080900045Damper · low pressure2S CHECK - DURING OPERATIONAL TEST OF DAMPING FUNCTIONAL & EMERGENCY OPERATION WAS FOUND HARD IMPACT BETWEEN THE BUFFER & FUSELAGE AT PASSENGER/CREW DOOR 842. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT PASSENGER/CREW DOOR 842 IAW AMM 52-13-14-00Jul 23, 2011 · N722US · Airbus A319112 · Passenger/Crew DoorsSDR USAA2011080900044Damper · low pressure2S CHECK - DURING OPERATIONAL TEST OF DAMPING FUNCTIONAL & EMERGENCY OPERATION WAS FOUND HARD IMPACT BETWEEN THE BUFFER & FUSELAGE AT PASSENGER/CREW DOOR 831. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT PASSENGER/CREW DOOR 831 IAW AMM 52-13-14-00Jul 23, 2011 · N722US · Airbus A319112 · Passenger/Crew DoorsSDR USAA2011080900043Damper · low pressure2S CHECK - DURING OPERATIONAL TEST OF DAMPING FUNCTIONAL & EMERGENCY OPERATION WAS FOUND HARD IMPACT BETWEEN THE BUFFER & FUSELAGE AT PASSENGER/CREW DOOR 832. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT PASSENGER/CREW DOOR 832 IAW AMM 52-13-14-00Jul 23, 2011 · N722US · Airbus A319112 · Passenger/Crew DoorsSDR USAA2011080900042Door · out of adjust2S CHECK - OUT ADJUSTMENT DIMENSION "A" BETWEEN STRIKER LEVER & FINGER AT PASSENGER/CREW DOOR 832. ADJUSTMENT CLEARANCE J2 BETWEEN STRIKER LEVER AND FINGER AT PASSENGER/CREW DOOR 832 IAW AMM 52-11-14-0501.Jul 23, 2011 · N722US · Airbus A319112 · Passenger/Crew DoorsSDR USAA2011081100008Bellcrank · out of adjust2S CHECK - OUT ADJUSTMENT TORSION BAR BELLCRANK AT PASSENGER CREW DOOR 842. ADJUSTMENT TORSION BAR BELLCRANK AT PASSENGER/CREW DOOR 842 IAW AMM 52-13-21-0401.Jul 22, 2011 · N722US · Airbus A319112 · Passenger/Crew DoorsSDR USAA2011080900041Door · out of adjust2S CHECK - OUT ADJUSTMENT DIMENSION "A" BETWEEN STRIKER LEVER & FINGER AT PASSENGER/CREW DOOR 842. ADJUSTMENT CLEARANCE J2 BETWEEN STRIKER LEVER AND FINGER AT PASSENGER/CREW DOOR 842 IAW AMM 52-11-14-0501.Jul 22, 2011 · N722US · Airbus A319112 · Passenger/Crew DoorsSDR USAA2011080900039Door · out of adjust2S CHECK - OUT ADJUSTMENT DIMENSION "A" BETWEEN STRIKER LEVER & FINGER AT PASSENGER/CREW DOOR 831. ADJUSTMENT CLEARANCE J2 BETWEEN STRIKER LEVER AND FINGER AT PASSENGER/CREW DOOR 831 IAW AMM 52-11-14-0501.Jul 15, 2011 · N722US · Airbus A319112 · Passenger/Crew DoorsSDR USAA2011080900040Door · out of adjust2S CHECK - OUT ADJUSTMENT DIMENSION "A" BETWEEN STRIKER LEVER & FINGER AT PASSENGER/CREW DOOR 841. ADJUSTMENT CLEARANCE J2 BETWEEN STRIKER LEVER AND FINGER AT PASSENGER/CREW DOOR 841 IAW AMM 52-11-14-0501.Jul 14, 2011 · N722US · Airbus A319112 · Passenger/Crew DoorsSDR USAA2011081100006Hinge Pin · damaged2S CHECK - MISSING PROTECTIVE TREATMENT ON RIGHT WING NR 1 SPOILER HINGE PINS (2EA) BETWEEN WS 3059 TO WS 3758 & BETWEEN RIB 6 TO RIB 7. REPLACED SPOILER HINGE PINS (2EA) IAW EA 133690B.Jul 13, 2011 · N722US · Airbus A319112 · SpoilersSDR USAA2011081000014Hinge Pin · corroded2S CHECK - CORROSION ON 2 EA LT WING SPOILER NR 4 HINGE PINS BETWEEN WS 924 TO WS 970. REPLACED HINGE PINS IAW EA 133690.Jul 13, 2011 · N722US · Airbus A319112 · SpoilersSDR USAA2011081000010Hinge Pin · damaged2S CHECK - MISSING PROTECTIVE PROTECTION ON LEFT AILERON HINGE PINS 1 THRU 5 AT WS 12870 RIB 24. REPLACED LEFT AILERON HINGE PINS 1 THRU 5 IAW A319 AMM 27-14-41 & JOB CARD 26C50027005.Jul 13, 2011 · N722US · Airbus A319112 · AileronsSDR USAA2011080900023Strut · corroded2S CHECK - CORROSION ON INTERNAL AREA OF THE INTERCONNECTING STRUT HOUSING LEFT WING AT WS 4862, RIB 9. REPLACED LEFT WING INTERCONNECTING STRUT IAW JOB CARD 26C57057001.Jul 13, 2011 · N722US · Airbus A319112 · Trailing Edge FlapsSDR USAA2011080900022Strut · corroded2S CHECK - CORROSION ON INTERNAL AREA OF THE INTERCONNECTING STRUT HOUSING RIGHT WING AT WS 4862, RIB 9. REPLACED RIGHT WING INTERCONNECTING STRUT IAW JOB CARD 26C67057001.Jul 13, 2011 · N722US · Airbus A319112 · Trailing Edge Flaps
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