Aircraft Report for n824ua



Registration History for n824ua







N-Number Make Model Serial Location Description Time
N824UA AIRBUS INDUSTRIE A319-131 0965 CHICAGO, IL Aircraft registered to UNITED AIRLINES INC, airworthiness date 1999-03-15, expiration date 2025-04-30, serial number 0965. 2021-12-02
N824UA AIRBUS INDUSTRIE A319-131 0965 CHICAGO, IL Aircraft registered to UNITED AIRLINES INC, airworthiness date 1999-03-15, expiration date 2022-04-30, serial number 0965. 2019-02-15
N824UA AIRBUS INDUSTRIE A319-131 0965 CHICAGO, IL Aircraft registered to UNITED AIRLINES INC, airworthiness date 1999-03-15, expiration date 2019-04-30, serial number 0965. 2015-12-11
N824UA AIRBUS INDUSTRIE A319-131 965 CHICAGO, IL Aircraft registered to UNITED AIRLINES INC, airworthiness date 1999-03-15, expiration date 2019-04-30, serial number 965. 2015-12-11
N824UA AIRBUS INDUSTRIE A319-131 965 CHICAGO, IL Aircraft registered to UNITED AIRLINES INC, airworthiness date 1999-03-15, expiration date 2016-04-30, serial number 965. 2013-04-01
N824UA AIRBUS INDUSTRIE A319-131 965 CHICAGO, IL Aircraft registered to UNITED AIR LINES INC, airworthiness date 1999-03-15, expiration date 2013-12-31, serial number 965. 2010-09-03

Service Difficulty Reports for n824ua













































































N-Number Make Model Serial Description Time
N824UA AIRBUS A319131 During TAKEOFF - SYS 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. - BRAKES ECAM BRK SYS 2 FAULT ON TO ROLL. REJECTED LESS THAN 30KIAS. RAN QRHRESET. CHECKED GOOD CREW ACCOMPLISHED QRH RESET AND BRAKES SYSTEM 2 FAULT MESSAGE CLEARED. BRAKING AND STEERING NORMALAFTER RESET. NO HITS LAST 10 LEGS 2022-03-10
N824UA AIRBUS A319131 During NOT REPORTED - PDA 2 FUELER REPORTED CAP MISSING. REPLACED CAP AND ATTACHED LANYARD. 2021-02-02
N824UA AIRBUS A319131 During INSP/MAINT - WHILE AT DLH DURING C-2 CHECK, HOLE CRACKS WERE DISCOVERED DURING ACCOMPLISHMENT OF EA5330-05216. OUTSIDE OF CUTOUT AREAAT HOLES 1, 2 & 4 ON LT FRAME 35/36 ACCOMPLISHED REPAIR OF ALL HOLES IAW EC/RA 5331-02412 TO LT FR35-36 PRESSURE PANEL HOLE CRACKS. ACCOMPLISH THE INITIAL INSPECTION REQUIREMENTS AT LT FR35 PRESSURE PANEL PER PART 2 OF ECRA 5331-02412ON OR BEFORE THE AIRCRAFT REACHES 58,983 TOTAL AIRCRAFT FC OR 128,664 TOTAL AIRCRAFT FH, WHICHEVER COMES FIRST. REPEAT THE INSPECTIONS AT NTERVALS NOT TO EXCEED 31,200 THEREAFTER. AIRCRAFT FC OR 62,500 AIRCRAFT FH (WHICHEVER COMES FIRST) APPROVED TO CARRY PER ECRA 5331-02412, ACCOMPLISH THE INITIAL INSPECTION REQUIREMENTS AT LT FR35 PRESSURE PANEL PER PART 2 2019-12-17
N824UA AIRBUS A319131 During INSP/MAINT - (SUPPORT TASK) R2 DOOR HANDLE GEAR BOX HOOK WORN. REFER TO AAR N /R: 9620410. REMOVED AND REPLACED R-2 DOOR HANDLE GEARBOX HOOK IAW CMM 52-13-15. 2019-12-04
N824UA AIRBUS A319131 During INSP/MAINT - R1 DOOR SLIDE PARACHUTE PIN NOT TIED CORRECTLY. PROPERLY TIED THE PARACHUTE PIN ON R1 DOOR SLIDE IAW AMM 25-62- 44-400-802-A, SUBTASK 25-62-44-420-066-A. 2019-11-25
N824UA AIRBUS A319131 During INSP/MAINT - R1 DOOR SLIDE GIRT BAR LANYARD NOT SECURED CORRECTLY. PROPERLY SECURED THE R1 DOOR SLIDE GIRT BAR LANYARD IAW AMM 25-62-44-400-802-A, SUBTASK 25-62-44-420-066-A. 2019-11-25
N824UA AIRBUS A319131 During INSP/MAINT - L2 DOOR SLIDE GIRT BAR LANYARD NOT SECURED CORRECTLY. PROPERLY SECURED L2 DOOR SLIDE GIRT BAR LANYARD IAW A319 AMM 25- 62-44-400-006-A SUBTASK 25-62-44-420-064-A. 2019-11-25
N824UA AIRBUS A319131 During INSP/MAINT - UPON REMOVAL OF SHEAR PLATE TO ACCOMP LISH EA 5346-01001 REV. B OP 003, FOUND SUPPORT FRAME THAT ATTACHES TO BE CORRODED. REMOVED AND REPLACED CORRODED SUPPORT FOR SHEAR PLATE AT FR 69-7 0 R/H IAW SRM 51-72-11-911-001. APPLIED SURFACE PROTECTION IAW ER 5100R01017 REV. F 2019-11-25
N824UA AIRBUS A319131 During INSP/MAINT - L2 DOOR SLIDE CABLE ROUTED INCORRECTLY. PROPERLY ROUTED L2 DOOR SLIDE CABLE IAW AMM 25-62-44-400-00 6-A, SUBTASK 25-62-44-560-051-A. 2019-11-25
N824UA AIRBUS A319131 During INSP/MAINT - ON REMOVAL OF SUPPORT FRAME, FOUND STRINGER SECTION CORRODED AT STR 24 FR 70R. A CORROSION RESULTED IN 100% MATERIAL LOSS OF STRINGER SECTION @ S TR 24 FR70R. REMOVED PART AND MATCHDRILLED, DEBURRED, AND INSTAL LED NEW STRINGER SECTION @ STR 24 FR70R. APPLIED TOP COATING TO FASTENERS IAW SRM 51-72-11-911-001. 2019-11-22
N824UA AIRBUS A319131 During INSP/MAINT - LT FR 68 #1 DOOR STOP FITTING I/B LOWER FASTENER HOLE HAS CRACK INDICATION. REF N/R 9620198. REAMED LT FR68 #1 DOOR STOPFTG I/B LOWER HOLE TO .280". ROTO PROBE PERFORMED, NO CRACK INDICATION. PERFORMED REPAIR IAW SRM 53-41-300-010, SRM 51-44-11-001, NTM 51-10-01. INSP THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT FC 41900, SUBSEQUENT INSP AT INTERVALS OF FC8000. INSP METHOD HFEC IAW SRI 53-41-12- 205-009. REF N/R 9620198. REPAIRED IAW SRM 53-41-300-010, SRM 51-44-11-001, NTM51-10-01. INSP THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT FC 41900, SUBSEQUENT INSP AT INTERVALS OF FC 8000. INSP METHOD HFEC IAW SRI 53-41-12-205-009. REF N/R 9620198. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED QC REVIEWED RECORDS 2019-11-19
N824UA AIRBUS A319131 During INSP/MAINT - LT FR 66 #1 DOOR STOP FITTING I/B LOWER FASTENER HOLE HAS CRACK INDICATION, REF N/R 9620196. REAMED LT FR66 #1 DOOR STOPFTG I/B LOWER HOLE TO .280". ROTO PROBE PERFORMED, NO CRACK INDICATION. PERFORMED REPAIR IAW SRM 53-41-12-300-010, SRM51-44-11-001, NTM 51-10-01. INSP THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT FC 38900, SUBSEQUENT INSP AT INTERVALS OFFC 7300. INSP METHOD HFEC IAW SRI 53-41-12- 205-009. REF N/R 9620196. REPAIRED IAW SRM 53-41-300-010, SRM 51-44-11-001,NTM 51-10-01. INSP THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT FC 38900, SUBSEQUENT INSP AT INTERVALS OF FC 7300. INSPMETHOD HFEC IAW SRI 53-41-12-205-009. REF N/R 9620196. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED QC REVIEWED RECOR 2019-11-19
N824UA AIRBUS A319131 During INSP/MAINT - RT FR 66 #1 DOOR STOP FITTING I/B LOWER FASTENER HOLE HAS CRACK INDICATION. REF N/R 9620197. REAMED RT FR66 #1 DOOR STOPFTG I/B LOWER HOLE TO .280". ROTO PROBE PERFORMED, NO CRACK INDICATION. PERFORMED REPAIR IAW SRM 53-41-12-300-010, SRM51-44-11-001, NTM 51-10-01. INSP THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT FC 38900, SUBSEQUENT INSP AT INTERVALS OFFC 7300. INSP METHOD HFEC IAW SRI 53-41-12-205- 009. REF N/R 9620197. REPAIRED IAW SRM 53-41-300-010, SRM 51-44-11-001,NTM 51-10-01. INSP THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT FC 38900, SUBSEQUENT INSP AT INTERVALS OF FC 7300. INSPMETHOD HFEC IAW SRI 53-41-12-205-009. REF N/R 9620197. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED QC REVIEWED RECOR 2019-11-19
N824UA AIRBUS A319131 During INSP/MAINT - GOUGED FLOOR SUPPORT +Y254 FRAME 70. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001. 2017-08-28
N824UA AIRBUS A319131 During INSP/MAINT - CORROSION ON SEAT TRACK +Y1292 LT SIDE, BETWEEN FRAMES 62 AND 63. BLENDED CORROSION IAW SRM 51-73-00, FIG 00101. REMOVED .040, MAX ALLOWED .028, FOUND TO BE OUT OF LIMITS IAW SRM 53-41-15-283-001, FIG 10101, SHT 1. REMOVED AND REPLACEDTHE SEAT TRACK IAW SRM 51-72-11-911-001. 2017-08-28
N824UA AIRBUS A319131 During INSP/MAINT - CORROSION ON THE AFT FLOORBEAM -Y1292 AT FRAME 68, REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53 -00-14-283-002, FIG 10102, SHEET 1. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11, PAGE 1. 2017-08-24
N824UA AIRBUS A319131 During INSP/MAINT - CORROSION ON THE FLOOR SUPPORT -Y765, FRAME 68. REMOVED & REPLACED THE FLOOR SUPPORT FRAMES 68 - 70 IAW SRM 51-72-11-911-001. RESTORED SURFACE PROTECTION ON THE FLOOR SUPPORT IAW SRM 51-75-12-911-001. 2017-08-24
N824UA AIRBUS A319131 During INSP/MAINT - UNABLE TO SHUT OFF EMERGENCY EXIT LIGHTS. 2017-03-14
N824UA AIRBUS A319131 During CRUISE - CABIN PRESSURE CONTROL 1 AND 2 FAULTED, UNABLE TO PRESSURIZE, CABIN PRESSURE CONTROLLERS 1 AND 2 AND OUTFLOW VALVE FAULTED BEFORE RESET. NO FAULTS NOTED REST OF TESTS. 2016-07-12
N824UA AIRBUS A319131 During INSP/MAINT - EPSU 33-51-38 BATTERY, EMER RT FAULTS ON CIDS DISPLAY DURING TEST. R & R & REINSTALLED BATTERY, FAULT CLEARED, TEST PASSED. 2016-03-18
N824UA AIRBUS A319131 During INSP/MAINT - EMERGENCY LIGHT TEST FAILED ON 2 SERVICE. RESEATED CONNECTOR ON RT EMER LIGHT POWER SUPPLY IAW AMM 33-51-38. EMER LIGHT TEST PASSED. 2015-11-05
N824UA AIRBUS A319131 During INSP/MAINT - SEAT EMERGENCY EXIT LIGHT AT SEAT 22 ABC INOPERATIVE. FOUND BROKEN WIRE. REPAIRED WIRE. OPERATIONS CHECKED NORMAL. 2015-08-12
N824UA AIRBUS A319131 During INSP/MAINT - CORROSION WAS FOUND ON THE LT WING TOP NR 2 PANEL BETWEEN RIB 19 & 20, AT THE MANUAL REFUELING PORT CUT OUT, FROM DF DATED 11 01 2010. BLEND REPAIR WAS ACCOMPLISHED IAW 80263 & EA 319-5721-13-A2032. 2015-07-16
N824UA AIRBUS A319131 During CLIMB - AIRFRAME VIBRATION ONCE AIRBORNE, EMER DECLARED, RETURNED. SECURED & APPLIED TAPE TO FILLET FAIRING ON LT SIDE OF FUSELAGE. COMPLETED INSPECTION OF FUSELAGE, NO DEFECTS FOUND. 2014-12-09
N824UA AIRBUS A319131 During INSP/MAINT - FLIGHT CONTROL SLATS LOCKED. WING TIP BREAKER ON SLAT SYS 2 FAULT CYCLED CB & PERFORMED BITE CHECK. NO FAULTS FOUND, NO MSGS. OPERATIONS CHECKED WITH CREW PRESENT. OPERATIONS CHECKED GOOD IAW AMM 27-51-00. 2014-08-14
N824UA AIRBUS A319131 During INSP/MAINT - SEAT EMERGENCY EXIT LIGHT ON SEAT 29C IS INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY LIGHT AT SEAT 29C IAW AMM 33-51-18, OPERATIONS CHECKED GOOD. 2014-03-11
N824UA AIRBUS A319131 During INSP/MAINT - DOOR SLIDE PRESS GAUGE DOOR 1R NOT VISIBLE. R & R DOOR R1 ESCAPE SLIDE IAW AMM TASKS 25-62-44-00-002-A & 25-62-44-400-006-A. 2014-03-05
N824UA AIRBUS A319131 During INSP/MAINT - AFT PIT FLOOR HAS A DEFECT THAT NEEDS CLARIFICATION. SECURED SIDE WALL PANEL AFT PIT. NO DEFECTS NOTED TO FLOOR. 2014-02-05
N824UA AIRBUS A319131 During INSP/MAINT - AUTO FLIGHT YAW DAMPENER STATUS MESSAGE. TROUBLE SHOT YAW DAMPER 1 MSG. NO ASSOCIATED CFDS MSGS. PERFORMED GROUND SCAN OF THE AFS. TEST FAULTED FAC 1. REPLACED FAC 1 IAW MM, OPERATIONS TEST OF THE AFS FAC 1 TEST PASSED. 2013-12-11
N824UA AIRBUS A319131 During CLIMB - CREW REPORTED EXCESSIVE ACFT PITCH UP. AFTER TAKEOFF ACFT NEEDED FWD STICK PRESSURE. AT CRUISE SPEED CHANGES RESULTEDIN LOSS OR GAIN OF ALTITUDE DUE TO SLOW TRIM RESPONSE. NOTED PITCH UP WAS MORE THAN 2.5 DEGREES PER MIN. AIRMAN SHOWSCFDS MSG "ELAC2 COM OR WIRING FROM ACCLRM 4 12CE4". REPLACED ELAC 2 AND ACCLRM-3 AND ACCLRM-4 REF TSM. ALL TESTED NORMAL PER AMM TASK 27-93-00-710-001-A AND TASK 27-92-16-000-001-A. ACFT OK FOR SERVICE. 2013-09-23
N824UA AIRBUS A319131 During INSP/MAINT - GREEN HYD 0 QTY. FOUND RUPTURED BRAKE HYD FLEX LINE AT TOP OF RT MAIN GEAR, REPLACED REF IPC 32-11-12-04F, ACCOMPLISHED LEAK CHECK OF LINE NO LEAKS NOTED, SERVICE GREEN SYS TO FULL. ACCOMPLISHED AMM 29-00-00-280-006-A-0 1 FOR A POSSIBLECAVITATION OF ENGINE PUMP ALL GOOD CHECK GREEN SYS DPI'S REF AMM, DPI'S NOT POPPED. 2013-09-23
N824UA AIRBUS A319131 During INSP/MAINT - EMERGENCY LIGHTS FAIL SERVICE TEST, DISPLAYS EPSU BATTERY AFT MESSAGE. REPLACED EPSU BATTERY AT AFT EPSU 13WL, OPS NORMAL. 2013-09-18
N824UA AIRBUS A319131 During INSP/MAINT - FIRST OFFICER`S OXYGEN MASK MICROPHONE IS INOPERATIVE. O2 MASK NO HELP, O2 BOX NO HELP, ORIGINAL INSTALLED. REMOVED AND REPLACED AMU, OPS CHECK OKAY. 2013-09-17
N824UA AIRBUS A319131 During NOT REPORTED - FUEL TEMP INDICATION; LEFT INBOARD INOP ON FUEL SYSTEM ECAM PAGE - FUEL COMPLIED WITH MEL. -RDF-P :CFDS MSG FUEL QUANTITY FQIC 3QT MESSAGE ON PFR. RESET FQI CH2 CB AND INDICATION RETURNS TO NORMAL FOR APPROX 2 MINUTES AND THEN GOES TO XX AGAIN. SUSPECT FQIC. RPL- :REMOVED AND REPLACED FQIC COMPUTER. ALL OPS AND TESTS NORMAL. 2013-08-01
N824UA AIRBUS A319131 During INSP/MAINT - FUEL TEMP INDICATION; RIGHT OUTBOARD INOP ON FUEL SYSTEM ECAM PAGE - FUEL. 2013-07-22
N824UA AIRBUS A319131 During INSP/MAINT - INTERIM REPAIRS TO AFT LAV PANEL COMPLETED PER ECRA 534101022. WELDING REPAIR LOOKS GOOD AND MEETS ECRA 534101022. ACPNDT PER 51-10-21 INTERNAL AND EXTERNAL INSPECTION FOUND NO CRACKS. ACP INTERNAL HFEC AND OPEN HOLE INSPECTIONS NO CRACKS FOUND. 2013-06-05
N824UA AIRBUS A319131 During NOT REPORTED - RIGHT WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN. - ANTI ICE. REPLACED NR 2 WHC OP CHECKS GOOD. 2013-05-20
N824UA AIRBUS A319131 During INSP/MAINT - EXTERNAL POWER EGIU CIRCUIT BREAKER TRIPPED. REPLACED EGCIU1 PER MM, CHECKED GOOD. 2013-05-02
N824UA AIRBUS A319131 During INSP/MAINT - FUEL LEAKING FROM RT WING SURGE VENT. REPLACED FUEL PUMP CHECK VALVE IAW MM. 2013-05-02
N824UA AIRBUS A319131 During INSP/MAINT - CANNOT ARM 2L. LEVER IS UP AND CANNOT BE MOVED DOWN. CLEANED DEBRIS FROM DOOR, OPS NORMAL. 2013-05-01
N824UA AIRBUS A319131 During INSP/MAINT - 'ENG FIRE EXTING-SQUIB' LIGHT OF 'AGENT 1' PUSHBUTTON SWITCH IS OFF DURING 'LOOP-SQUIB TEST'. ENG 2 SQUIB LIGHT WON'T TEST. ACCMP'D CHECK PER MEL. PANEL IN A/C LOB. PARTS: 565-9002 MR26123 - PANEL. REPLACED PIN 2 OF 5WE2A, FOUND DAMAGED. OPS CKD OKAY. 2012-11-27
N824UA AIRBUS A319131 During INSP/MAINT - CLEANING FOREMAN REPORTS ON WALK THRU ELECTRICAL WIRES HANGING DOWN BELOW SEAT 32C. TURNED ON THE EMER EXIT LIGHT SWITCH-ALL OTHER LIGHTS WORKING NORMALLY. TAPED AND SECURED WIRING BELOW SEAT 32C. PLACED PLACARD ADJACENT TO THE EMER EXITLIGHT SWITCH IN THE COCKPIT. 2012-06-28
N824UA AIRBUS A319131 During INSP/MAINT - CLEANING FOREMAN REPORTS ON WALK THRU ELECTRICAL WIRES HANGING DOWN BELOW SEAT 32C. FOUND WIRE PULLED OUT OF CONNECTORFOR THE EEL LIGHT ON THE SIDE OF SEAT 32C. TURNED ON THE EMER EXIT LIGHT SWITCH-ALL OTHER LIGHTS WORKING NORMALLY. TAPED AND SECURED WIRING BELOW SEAT 32C. PLACED PLACARD ADJACENT TO THE EMER EXIT LIGHT SWITCH IN THE COCKPIT. SECURED WIRING. OPS NORMAL. 2012-06-20
N824UA AIRBUS A319131 During INSP/MAINT - GALLEY FLOOR SPONGY AT DOOR 2R. DAMAGE IS INBOARD EDGE 5 X 5 AND 10X2 NON PERFORATION. OK TO CF PER SRM. PERM REPAIRWITHIN 350FH. PANEL NUMBER 262FF PCN#110-4657. CURRENT PTT IS 45211:11. TOTAL AREA IS 45 SQ IN., SRM ALLOWS 69.75, 7.087 X 9.843". REPLACED FLOORBOARD AND GALLEY MAT. 2012-05-02
N824UA AIRBUS A319131 During NOT REPORTED - ON CAPTS O2 MASK THE RED TEST BUTTON MIGHT BE MISSING TOP. REPLACED MASK, OPS GOOD PER SUBTASK. 2012-02-16
N824UA AIRBUS A319131 During INSP/MAINT - ECAM CAUTION MESSAGE - RAT FAULT MESSAGE INOP - HYD. CREW COMMENTS: RAT IS DEPLOYED. RAT WAS DEPLOYED ON THE GROUND.STOWED RAT PER MM. 2012-02-15
N824UA AIRBUS A319131 During NOT REPORTED - F/O'S OXYGEN MASK MICROPHONE IS INOPERATIVE. REPLACED F/O O2 OXYGEN MASK STOWAGE BOX PER AMM. 2011-12-19
N824UA AIRBUS A319131 During NOT REPORTED - MASK FELL SEAT 10B. REPACKED O2 MASK AT SEAT 10B. 2011-07-25
N824UA AIRBUS A319131 During INSP/MAINT - F/O OXY MASK MIC INOP. REPLACED F/O'S O2 MASK, OPS CHECK NORMAL. 2011-06-21
N824UA AIRBUS A319131 During INSP/MAINT - EXFOLIATED STR 31R JUST AFT OF FR65, BEHIND OUTFLOW VALVE. MAJOR REPAIR ACCOMPLISHED: REPAIRED CORRODED STR 31R JUST AFT OF FR 65, AFT OF OUTFLOW VALVE. REPAIR ACP ON W-U C6824Q. 2010-11-29
N824UA AIRBUS A319131 During INSP/MAINT - CORROSION FOUND ON EXT SKIN UNDER LT AIRPHONE ANTENNA, BETWEEN FR63 AND FR64 AND STR41L AND 42L. CORROSION WAS BLENDED IAW UA EVA 80261 AND MAE EA319-5341-13-A2031 ON N-R C6070Q. REPAIR HAS RECEIVED A 6 MONTH INTERIM APPROVAL PENDING DTA.AIRBUS MUST ISSUE A NEW RAS SHOWING COMPLIANCE WITH DTA ON OR BEFORE APRIL 29TH 2011. THE ACFT MUST BE REMOVED FROM SERVICE ON APRIL 29TH 2011 UNLESS THE NEW RAS IS RECEIVED. 2010-11-29
N824UA AIRBUS A319131 During INSP/MAINT - CORROSION WAS FOUND ON THE LT WING TOP NR 2 PANEL BETWEEN RIB 19 AND RIB 20, AT MANUAL REFUELING PORT CUTOUT. BLEND REPAIR WAS ACP IAW UA EVA 80263 AND EA 319-5721-13-A2032, ON N-R C6017Q. REPAIR MUST BE INSPECTED AT THRESHOLD OF 200,300FLIGHT HOURS, OR 124,500 FLIGHT CYCLES, WHICHEVER OCCURS FIRST. INSP INTERVALS AND METHOD OF INSP HAVE NOT BEEN DETERMINED. MFG WILL ISSUE A NEW RAS WITH THE INSP INTERVALS AND METHOD BEFORE AC ACCUMULATES ABOVE FH AND FC. 2010-11-29
N824UA AIRBUS A319131 During CRUISE - NR1 ENGINE VIBRATION, FLIGHT DIVERTED. WENT FROM 5.1 TO 8.0, ENGINE VIBRATION COULD BE FELT THROUGH OUT ACFT, FOLLOWEDFM PROCEDURES AND LANDED AT NEAREST SUITABLE AIRPORT. IN DESCENT VIBRATION DECREASED TO 4.3 AT FL 240, AT FL 160 WITH ENGINES AT FLIGHT IDLE, VIB WENT TO ZERO. ALL CHIP DET'S CLEAN. ACP 'D VIBRATION SURVEY REF MM 71-00-00. MAX VIB WAS 1.2ON THE N1 WITH NO SPIKES NOTED. OPS CHECKED ANTI-ICE VALVE. CHECKED OK. OK FOR SERVICE. 2010-08-27
N824UA AIRBUS A319131 During INSP/MAINT - L SIDE FWD OF EMER EXIT BELOW EXIT SIGN IS MISSING A LENS AND BULB. REPLACED LENS COVER. 2010-01-05
N824UA AIRBUS A319131 During CRUISE - ENG1 FUEL CNTRL FAULT ENROUTE. REPLACED NR 1 ENG FMU. ACCOMPLISHED OPERATIONAL TEST AND IDLE LEAK CHECK. OPS NORMAL 2009-12-29
N824UA AIRBUS A319131 During INSP/MAINT - ENG NR2 LOOP A FIRE DETECTOR. HUNG NEW LOOP, NO HELP. SUSPECT FDU BENCH PLUG, SHAKING FDU CLEARS FAULT. SUPPLEMENTAL DATA UPDATE WIRING SHORT IN FAN LOOP HARNESS. REMOVED CONNECTOR PLUG FROM NR2 FDU, WIRE 'A' FROM 450VT PULLED FROM BLOCK.SECURED CONNECTOR PLUG ON NR2 FDU. CONNECTION 458VC 'J' PLUG, INSIDE BOX WIRES, HAS CHAFED COATING ON BOTH WIRES 276, 277, WIRES MARKED WITH TAPE. WIRES REPAIRED. WIRE 2612-276-CF20 PIN A AT 450VT2 DEPINNED FOR TROUBLESHOOTING. INSTALLED PIN. SECURED INSTALLATION. ACCOMPLISHED NR 2 ENG FIRE LOOP TEST IAW 26-12-00. TEST OK. 2009-01-08
N824UA AIRBUS A319131 During INSP/MAINT - CREW O2 PRESSURE IS SHOWING AT 50 PSI. SERVICED BOTTLE TO 1600 PSI AND CHECKED ALL CREW MASKS FOR LEAKS. VERIFIED NO LEAKS AND AFTER 1 HR BOTTLE PRESSURE STILL AT 1600 PSI, ACFT IS OK FOR SERVICE. 2008-09-08
N824UA AIRBUS A319131 During NOT REPORTED - SLAT SYS 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. FOUND FAILURE OF SFCC-2. 22CV. REPLACED SFCC-2. 22CV, OPS TESTED NORMAL. 2008-05-14
N824UA AIRBUS A319131 During TAXI/GRND HDL - ALTERNATE LAW (PROT LOST) DISPLAYED ON UPPER ECAM SCREEN. ECAM SHOWS MOMENTARILY AS FLAPS AND SLATS MOVE OUT TO POSITION. FOUND SLAT/FLAP COMPUTER 22CV FAULTING. REPLACED SLAT AND FLAP CONTROL COMPUTER 22CV 2008-05-07
N824UA AIRBUS A319131 During INSP/MAINT - CAPTAIN'S OXYGEN MASK MICROPHONE IS INOPERATIVE. FOUND WIRE PULLED OUT OF CONNECTOR THAT CONNECTS INSIDE THE BOX. REPLACED THE O2 MASK STOWAGE BOX, OPS CHECKED NORMAL, NO LEAKS NOTED. 2008-04-21
N824UA AIRBUS A319131 During INSP/MAINT - ENG NR 2 LOOP A FIRE DETECTOR. HUNG NEW LOOP, NO HELP. SUSPECT FDU BENCH PLUG, SHAKING FDU CLEARS FAULT. FOUND WIRINGSHORT IN FAN LOOP HARNESS. 2008-03-26
N824UA AIRBUS A319131 During INSP/MAINT - FIRE LOOP A FAULT DISPLAYED ON UPPER ECAM SCREEN ENG 2. FOUND LOOP TOUCHING METAL FRAME IN ENGINE. REPOSITIONED LOOP TO CORRECT POSITION, OPS TESTED NORMAL. 2008-03-06
N824UA AIRBUS A319131 During INSP/MAINT - EEL LIGHT AT 7C INOP. LOOSE CONNECTOR AT SEAT ROW 7. RESECURED LOOSE CONNECTOR, LIGHTS OPS NORMAL. 2008-02-06
N824UA AIRBUS A319131 During CRUISE - FLIGHT DIVERTED DUE TO A FAULTING FMGC. FMGC FAILURE (SHOP FINDINGS NFF). REPLACED FMGC, OPS CHECKED NORMAL. 2008-01-29
N824UA AIRBUS A319131 During INSP/MAINT - EPSU INT LOAD EMER L 33-51-38 FAULT DURING TEST AFTER ESCAPE SLIDE 2L REPLACEMENT. EMERGENCY LIGHT SYS NEEDS REPAIR. FAULTY POWER SUPPLY FOR EMERGENCY LIGHTS (EPSU). REPLACED EPSU, OPS CHECKED GOOD. 2008-01-11
N824UA AIRBUS A319131 During INSP/MAINT - F/A FLASHLIGHT IS NOT FLASHING. *S/D* BATTERY FAILURE. REPLACED BATTERY. 2008-01-09
N824UA AIRBUS A319131 During CRUISE - FLIGHT DIVERTED WITH NR 2 ENGINE EPR MODE FAULT AND NR 2 ENG N1 UNRATED. 2007-12-19
N824UA AIRBUS A319131 During INSP/MAINT - F/O'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). 2007-10-10
N824UA AIRBUS A319131 During INSP/MAINT - SECOND OBS QUICK DONNING MASK INOP. 2007-10-10
N824UA AIRBUS A319131 During TAXI/GRND HDL - NW STEERING FAULT DISPLAYED ON UPPER ECAM SCREEN. WHEEL. [06-26-07] GROUND SCAN OF NR 1 BSCU INDICATED FAULTY STEERING SERVO CONTROL MODULE. REPLACED 6GC STEERING SERVO CONTROL MODULE. ALSO REPLACED BSCU AS A PRECAUTION. 2007-05-24
N824UA AIRBUS A319131 During INSP/MAINT - NR 2 ENGINE FIREX DISCHARGE LINE 4 EA OPENINGS ALL CAPPED WITH FLEX HOSE AND PLUG TEST EQUIPMENT. FIREX LINE IS DIRECTLY ABOVE ENGINE FAN CASE. TEST EQUIPMENT WAS FOUND DURING OPEN UP. [SUP 05-16-07] THE INSTALLED CAPS, FLEX HOSE AND TEST EQUIPMENT ARE USED DURING A PRESSURIZED LEAK TEST OF THE EXTINGUISHER DISCHARGE SYSTEM. THIS TEST WAS LAST PERFORMEDON THE AFFECTED AIRCRAFT DURING A REGULARLY SCHEDULED C-CHECK ON 8/29/2005. AT THAT TIME, THE MECHANICS WHO PERFORMED THE TEST FAILED TO PUT THE DISCHARGE SYSTEM BACK INTO A FLIGHT WORTHY CONDITION AND THE ERROR WAS NOT DISCOVERED TILL THEMOST RECENT C-CHECK WAS PERFORMED ON 1/29/2007. 2007-02-21
N824UA AIRBUS A319131 During INSP/MAINT - SEAT 17ABC EMERGENCY LIGHT INOPERATIVE. RELAMPED SEAT 17 ABC EMERGENCY LIGHT. OPS CHECKS GOOD. 2006-08-16
N824UA AIRBUS A319131 During INSP/MAINT - EMERGENCY ESCAPE PATH LIGHTS INOP AT ROW 20L, 21L. ALSO 17LH AND 18LH HAVE DIM LIGHTS. REPLACED BATTERY POWER SUPPLYPER AMM 33-51-38, TEST NORMAL. 2006-07-10
N824UA AIRBUS A319131 During INSP/MAINT - R2 DOOR SLIDE PRESSURE IN THE RED. REPLACED SLIDE, INSTALLED AT DOOR 2 RIGHT. ACCOMPLISHED INSPECTION OF DOOR 2R SLIDEINSTALLATION. 2006-05-26
N824UA AIRBUS A319131 During CRUISE - LANDED UNDER AMBER ALERT DUE TO GREEN HYDRAULIC SYSTEM LOW PRESSURE MESSAGE. THE SAME MESSAGE CAUSED DIVERSION OF NEXTFLIGHT DUE TO EN ROUTE WEATHER CONDITIONS AND TRADEWINDS AT PLANNED DESTINATION. HYDRAULIC PUMP PRESSURE SWITCH FAILED.REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP PRESSURE SWITCH. RAN BOTH ENGINES FOR SEVERAL MINUTES AND OPERATION OF NR 1ENGINE HYDRAULIC PUMP WAS NORMAL. 2004-06-16
N824UA AIRBUS A319131 During NOT REPORTED - CREW REPORTED LOW QUANTITY WITH GREEN HYDRAULIC SYSTEM. CREW, SAMC, DISPATCH AGREED TO DIVERT TO ORD. AMBER ALERT DECLARED, EQUIPMENT REQUESTED TO MEET AIRCRAFT IN ORD. *S/D* FOUND NR 1 ENGINE HYDRAULIC PRESSURE SWITCH BACKED OUT AND THE O-RING DISPLACED. REPLACED THE O-RING AND SECURED THE SWITCH TO PROPER TORQUE. LEAK CHECKS GOOD ON ENGINE RUN. 2000-10-18

Likely List Price Spread

Historical Listing Counts

Popular Avionics

Explore the Full Dataset

Aviation Datasets Explained


Aircraft Lookup allows anyone to quickly search public datasets published by various aviation administrative services as well as marketplaces and other private aviation data providers in the United States. These datasets provide valuable insight into the history and maintenance record of any aircraft registered in the US. When you provide an N-Number above, we cross reference historical SDR, FAA, and NTSB datasets to identify any relevant records related to that N-Number.

As you may be aware, N-Numbers are not connected to an aircraft for the life of that aircraft - N-Numbers may be deregistered, and re-registered to completely different aircraft. For that reason, please confirm that the details of any search result correspond to the make and model you intended to pull records for.

SDR, FAA, and NTSB databases are provided as follows:

The Service Difficulty Reports (SDR) dataset is defined as "[t]he reports submitted by certificate holders and certificated repair stations, known as service difficulty reports (SDR's), provide the FAA with airworthiness statistical data necessary for planning, directing, controlling, and evaluating certain assigned safety-related programs." This data is, in its raw form, a tab-delimited file with encoded field headers.

The FAA Registration dataset is fairly straightforward - it is a listing of current registrations (along with addresses, aircraft serial number, and other basic metadata) at any point in time. The registration data is a comma delimited file that has named fields at the top of each file. The FAA provides historical data on their site for the previous few years.

The FAA Accident/Incident dataset covers a range of accidents and incidents that may or may not overlap with NTSB data. Typically, more significant crashes are covered by NTSB data while less significant crashes are more comprehensively covered by the FAA Accident/Incident data, which will frequently include minor events like gear-up landings and so forth. The data provided by the FAA is in a tab-delimited file with encoded field headers.

The NTSB investigation dataset is distinct from the FAA dataset. While the number of accidents or incidents they cover are less numerous, the depth at which they are covered is significantly deeper when reported by the NTSB. While each record from the NTSB contains incredible amounts of metadata related to people responsible for the flight, prevailing meteorological conditions at the time of flight, and passengers aboard, this aircraft lookup tool only provides basic summary data. The full dataset is provided as a series of Microsoft access file databases on the NTSB site.