Aircraft Report for n828ua



Registration History for n828ua







N-Number Make Model Serial Location Description Time
N828UA AIRBUS INDUSTRIE A319-131 1031 CHICAGO, IL Aircraft registered to UNITED AIRLINES INC, airworthiness date 1999-06-25, expiration date 2025-04-30, serial number 1031. 2021-12-02
N828UA AIRBUS INDUSTRIE A319-131 1031 CHICAGO, IL Aircraft registered to UNITED AIRLINES INC, airworthiness date 1999-06-25, expiration date 2022-04-30, serial number 1031. 2019-01-09
N828UA AIRBUS INDUSTRIE A319-131 1031 CHICAGO, IL Aircraft registered to UNITED AIRLINES INC, airworthiness date 1999-06-25, expiration date 2019-04-30, serial number 1031. 2015-12-11
N828UA AIRBUS INDUSTRIE A319-131 1031 CHICAGO, IL Aircraft registered to UNITED AIRLINES INC, airworthiness date 1999-06-25, expiration date 2019-04-30, serial number 1031. 2015-12-11
N828UA AIRBUS INDUSTRIE A319-131 1031 CHICAGO, IL Aircraft registered to UNITED AIRLINES INC, airworthiness date 1999-06-25, expiration date 2016-04-30, serial number 1031. 2013-04-01
N828UA AIRBUS INDUSTRIE A319-131 1031 CHICAGO, IL Aircraft registered to UNITED AIR LINES INC, airworthiness date 1999-06-25, expiration date 2014-07-31, serial number 1031. 2011-07-27

Service Difficulty Reports for n828ua









































































N-Number Make Model Serial Description Time
N828UA AIRBUS A300* During UNKNOWN - HYD Y RSVR LOHYD Y RSRV OVHT INSP AC FOUND LEAK AT PRIORITY VALVE ON POWER TRANSFER UNIT MANIFOLD ON AFT WALL ABOVE KEELBEEM. REMOVED AND REPLACED YELLOW HYDRAULIC PRIORITY VALVE REF AMM.29-11-33-000/400-0001-A. OPERATED YELLOW HYDRAULIC. NO LEAKS FOUND. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1865545 SN OFF 3451 IPC REFERENCE # 28-13-33-01 VALVE, HYDRAULI OFF 31-2910-9-9001 3451 ON 31-2910-9-9001 2595 2022-08-31
N828UA AIRBUS A319131 During UNKNOWN - PDA 3 OPS REPORTS FUEL CAP LANYARD MISSING CURRAN, MICHAEL (V921870)APPLIED CDL 28A. NO LEAKS NOTED. REMOVED REMAINING PORTION OF LANYARD. DISPATCH DESK: 31 NAME: AM DATE: 14-APR-22- DEFERRED DIRECTLY BY TOMC UPDATED MAACODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V921870 PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. APPLY CDL 28A MAC RELATED WORK ORDER 000000003041435 AND PRTR CURRAN, MICHAEL (V921870)APPLIED CDL 28A. NOLEAKS NOTED. REMOVED REMAINING PORTION OF LANYARD. FOUND FUEL CAP LANYARD PRESENT,SECURE, AND FUNCTIONING PRPERLY. 2022-04-18
N828UA AIRBUS A319131 During CRUISE - LEFT BRAKE SHOWS 2000PSI ON GAUGE INFLIGHT R&R''D TRIPPLE INDICATOR AMM 32-44-21 PERFORMED BOTH OP''S CK''S ALL TESTS PASSED. PART ENTRY UPDATE. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1937450 SN OFF 3816 IPC REFERENCE # 32-44-08-01ITEM 50 2021-04-01
N828UA AIRBUS A319131 During INSP/MAINT - PDA 2 RIGHT ENG INBD T-R TO PYLON FLEX SEAL (SECOND FROM AFT) IS CRACKED AND MISSING SEGMENT. PARTS UPDATE IPC 54-57-22-07A REMOVED AND REPLACED FLEX SEAL - REF ECRA 5450-02357 REV-B. 2020-03-05
N828UA AIRBUS A319131 During NOT REPORTED - FWD AVIONICS DISPLAYED ON UPPER ECAM SCREEN. - DOOR IINDICATION WAS RIGHT FORWARD DOOR. APPROVED FOR MEL 5270CB COMPLIEDTHE PROXIMITY SENSOR OF RH FWD AVIONICS DOOR WAS REPLACED IAW AMM 52-71-14-000-001-A REMOVAL, AMM 52-71-14-400-001-A INSTALLATION, OP TEST OK. 2019-12-17
N828UA AIRBUS A319131 During INSP/MAINT - (SUPPORT TASK) L-58 NO DOT; THE EMER LIGHT TEST FAILS WITH THE MESSAGE ''EPSU UNIT FWD L'' ATA 33-51-38. REMOVED AND FWDEPSU(10WL) AND FWD EPSU BATTERY IAW AMM 33- 51-38-000-002-A, 33-51-38-000-001-A, 33-51-38-400-001-A AND 33-5 1-38-400-002-A. OPS CHK GOOD IAW AMM 33-51-00-710-001-A. REMOVED AND REINSTALLED CEILING PANEL 221BC IAW A319 AMM 25-23-42- 000-001-A, AND 25-23-42-400-001-A IDT ROTABLE PARTS CHANGE WAS INDICATED - TT # 1249140 SN OFF 8099 POWER SUPPLY, C OFF 31-3350-9-9001 8099 ON 31-3350-9-9001 8228. 2019-10-11
N828UA AIRBUS A319131 During INSP/MAINT - RT AIRPHONE SYSTEM ANTENNA MOUNT SKIN HOLES HAVE ELEVEN HOLES THAT ARE DAMAGE/OUT OF ROUND/CORROSION AS MARKED ON EXTERIOR OF SKIN (SUPPORT TASK) AT REF. NR 9294752. REPAIRED RT AIRFONE SYSTEM ANTENNA MOUNT IAW EC/RA 5331-02272. DTA DIP LOGPAGE ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF EC/ RA 5331-02272 ON OR BEFORE APRIL 04,2019. PERMANENT REPAIR TO B ADD PART 3 - PERMANENT REPAIR, TO BE DETERMINED BY ENGINEERING PLANNING TO CONTACT ENGINEERING AFTER MARCH 14, 2019 BUT BEFORE MARCH 24, 2019 REF EC/RA 5331-02272 ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF EC/ RA 5331-02272 ON OR BEFORE APRIL 04, 2019. DIP APPROVED PER ECRA 5331-02272 TOMC-APPROVAL FROM SC1ELBYC COMMENT QC RECORDS UPDATE QC REVIEWED INIT: &GT 2019-07-05
N828UA AIRBUS A319131 During INSP/MAINT - AD RELATED 2017-22-03 A3NB-53-4-6304 ABHEC SCAN REAVEALED CRACK OF 2EA IB HOLES OF NR 7 STOP FITTING AT FR 16 OF R1 DOORGENERATED BY V892444 UPON FURTHER EVALUATION FOUND CRACKS TO BE IN INTERCOSTAL ONLY REMOVED AND REPLACED INTERCOSTAL ATNR 7 STOP FITTING LOCATION BETWEEN FR15-16 IAW SRM 51-42-11. 2019-07-01
N828UA AIRBUS A319131 During INSP/MAINT - L-1 DOOR CUTOUT FRAME 16 STOP FITTING LOCATION 7 HAS TWO CRACKED HOLES. UPPER INBOARD HOLE IN INTERCOSTAL AT 6:00 AND LOWER INB OARD HOLE IN WEB AT 4:00 A3NB-53-4-6304 GENERATED BY V061633 REMOVED AND REPLACED INTERCOSTAL AT FR16 STOP FITTING NO. 7 IAW A319 SRM 51-42-11 2D,2E,2F REMOVED DOT E246 BY MECH V922369 INSP BY LC-81 2019-06-28
N828UA AIRBUS A319131 During INSP/MAINT - AFT CABIN L2 DOOR SILL AT FR68 HAS BROKEN NUT PLATE HOLE. REPAIRED AFT CABIN L2 DOOR SILL AT FR68 IAW SRM 53-41-14-30 0-001 FIG 20101 PRINCIPLE 5 REPAIR CATEGORY A. 2019-06-18
N828UA AIRBUS A319131 During INSP/MAINT - REAR AVIONICS COMPARTMENT ACCESS DOOR 824 HAS MULTIPLE DENTS. REWORKED DENTS & INSTALLED REPAIR DOUBLER AT REAR AVIONICSCOMPT ACCESS DOOR 824 PER SRM 51-73-00 PARA 7(A) & SRM 52-41-00- 300-001 PG 4 STEP 3(R). 2018-10-15
N828UA AIRBUS A319131 During INSP/MAINT - LT AIRPHONE SYSTEM ANTENNA MOUNT SKIN HOLES HAVE SEVEN (7) HOLES THAT ARE DAMAGED /OUT OF ROUND/ CORROSION AS MARKED ONEXTERIOR OF SKIN. CUT OUT DAMAGE AT LT AIRPHONE ANTENNA MOUNT BETWEEN FR 63 AND 64 AND STR 42 LT AND 43 LT IAW SRM 53-00-11-300-002. CUTOUT DIMENSIONS LENGTH = 4.6" AND WIDTH = 1.8". DOUBLER REPAIR ACP IAW SRM 53-00-11-300-002. 2018-10-15
N828UA AIRBUS A319131 During INSP/MAINT - RT AIRPHONE SYSTEM ANTENNA MOUNT SKIN HOLES HAVE ELEVEN HOLES THAT ARE DAMAGE/OUT OF ROUND/CORROSION AS MARKED ON EXTERIOR OF SKIN. REPAIRED RT AIRFONE SYSTEM ANTENNA MOUNT IAW EC/RA 5331-02272. 2018-10-15
N828UA AIRBUS A319131 During INSP/MAINT - DURING A SERVICE CHECK, FOUND EPSU FOR THE EMERGENCY LIGHT BATTERY LT FAULT MESSAGE ON CIDS DISPLAY. REPLACED THE EPSU BATTERY AND OP CHECKED GOOD IAW AMM 33-51-39. 2018-06-11
N828UA AIRBUS A319131 During CRUISE - F/O FWD WINDSCREEN OUTER PANE SHATTERED. EMERGENCY DECLARED. REMOVED & REPLACED THE WINDSHIELD IAW MM 56-11-00 & 56-11-11. 2017-05-23
N828UA AIRBUS A319131 During CRUISE - L/G SHOCK ABSORBER FAULT. EMERGENCY DECLARED. CLEARED ITSELF DURING DESCENT AT 11000 FEET. WHILE SPEAKING TO THE PILOTIN FLIGHT HE ALSO OBSERVED THE FOLLOWING WARNINGS: AUTO FLT AP OFF AUTO FLT A/THR OFF ANTI ICE STBY PITOT L/G SHOCK ABSORBER FAULT L/G RETRACT. INSTALLED SERVICEABLE FLIGHT GROUND SENSING MECHANISM PER ECRA3220-01757 AND AMM 32-21-45-400-801. ADJUSTED DIMENSION X ON SENSORS 24GA AND 25GA WITH SHIMS AT ROD AND LEVER CLEVIS MOUNT BOLT ON FLIGHT/GROUND SENSINGMECHANISM. PROX SENSOR 24GA AND 24GA INDUCTANCE CHECK FOR ON GROUND AND IN FLIGHT ARE WITHIN LIMITS AS PER DATA CHARTS REF:32-31-73-0501. OPS CHECK FOR FLIGHT SENSING AND WEIGHT ON GROUND CHECKED GOOD. 2017-04-17
N828UA AIRBUS A319131 During CRUISE - AUTO FLT ''AP OFF'' AND ''A-THR OFF'' DISPLAYED ON UPPER ECAM SCREEN. EMERGENCY DECLARED. SUSPECTED LGCU 1 FAULT PERFORMED BITE TEST ON LGCU1 TEST OK MESSAGE CLEARED. 2017-04-11
N828UA AIRBUS A319131 During INSP/MAINT - BATTERY EMERG POWER SUPPLY FOUND INOP AT FWD LT CABIN. REPLACED BATTERY EMERG POWER SUPPLY LT FWD IAW AMM 33-51-38-000-002A AND 33-51-38-400-002A, OPS CK GOOD. 2017-01-10
N828UA AIRBUS A319131 During INSP/MAINT - CIDS MESSAGE, EPSU BATTERY AFT LEFT. CYCLED CIDS, TESTED GOOD IAW AMM. 2016-08-23
N828UA AIRBUS A319131 During INSP/MAINT - CIDS MESSAGE, EPSU BATTERY FORWARD LEFT. CYCLED CIDS, TESTED GOOD IAW AMM. 2016-08-23
N828UA AIRBUS A319131 During INSP/MAINT - FORWARD LT EPSU BATTERY INOPERATIVE. REPLACED BATTERY PACK FWD LT. OPERATIONS CHECKED GOOD IAW AMM 33-51-38-400-002. 2015-09-01
N828UA AIRBUS A319131 During INSP/MAINT - EPSU MID LT INOPERATIVE. REPLACED EPSU & BATTERY PACK OPERATION CHECKS GOOD IAW AMM 33-51-38-400-001 & 33-51-38-400-002. 2015-09-01
N828UA AIRBUS A319131 During INSP/MAINT - 11WL EPSU BATTERY FAILED. REPLACED BATTERY IAW AMM 33-51-38. 2015-02-03
N828UA AIRBUS A319131 During INSP/MAINT - SDCU MESSAGES REPEAT LEVEL 1 CHRONIC SDCU NO DATA MESSAGES. PROBLEM STARTED AFTER THE LAST SDCU WAS INSTALLED, OCCURS ON ENG START. REPLACED THE SDCU PCN 565-9019 IPC 26-17-08-02-130E AMM 26-17-34-401, SYSTEM CHECKED OK. 2014-02-11
N828UA AIRBUS A319131 During INSP/MAINT - ONE RT MED DAMPER CYLINDER STRIKER ASSEMBLY IS CRACKED AT ATTACH FLANGE. GENERATED C-CHECK WU M7739I. REPLACED CYLINDER ON WU M7739I. 2014-01-23
N828UA AIRBUS A319131 During INSP/MAINT - CAPTS LT PFD SCREEN IS BLURRY, EVEN SWITCHING DISPLAY THE LT SCREEN IS FUZZY. R & R LOWER ECAM DU IAW TASK 31-63-22, OPERATIONS CHECKED GOOD. ALSO PERFORMED TASK 2 4-25-00-710-001-A ESS-GEN SWITCHING TESTED GOOD. 2014-01-14
N828UA AIRBUS A319131 During NOT REPORTED - 20A EXIT DOOR PANEL FELL OFF. RESECURED LOOSE PANEL INTO PLACE. ACFT OK FOR SERVICE. 2013-10-29
N828UA AIRBUS A319131 During INSP/MAINT - DURING TWO SERVICE EMERGENCY LIGHT CHECK HAD EPSU EMERGENCY LIGHT MESSAGE. REPLACED EPSU IAW AMM 33- 51-38 & EPSU BATTERY IAW AMM 33-51-38. BITE TESTED GOOD ON EPSU & EMERGENCY LIGHT CHECKED GOOD AT DOOR 1L. 2013-09-24
N828UA AIRBUS A319131 During INSP/MAINT - FORWARD LAVATORY HAS A LARGE WATER LEAK. REPLACED TOILET ASSY. 2013-09-05
N828UA AIRBUS A319131 During INSP/MAINT - NR 1 ENGINE I/B SIDE OF UPPER PEN NIB MISSING 1 EACH RIVET. REPAIRED PER AMM MT78-001 PARA M. INSTALLED 1 MISSING RIVET AND REPLACED 15 LOOSE RIVETS ON INBD AND OUTBD AREAS. 2013-08-01
N828UA AIRBUS A319131 During INSP/MAINT - ON NR 1 ENGINE NOSE CONE ON CIRCULAR RETAINER WITH 6 BOLTS. METAL AROUND A BOLT HAS CRACK. PLACED ON CF PER AMM 72-38-11-200-010-B13. MUST BE INSPECTED PRIOR TO EACH DEPARTURE. MUST BE REPAIRED BY "C" CHECK. INF- : REPLACE SPINNER FAIRING 1ST AVAILABLE PCN 222-0379. (PARTS: 222-0379 5A1834 - FAIRING) REPLACED PER AMM 72-38-11-200-010-B13 AND AMM. 2013-05-30
N828UA AIRBUS A319131 During NOT REPORTED - FUEL MIGRATING TO CTR TANK. FOUND FUEL IN LEFT SURGE TANK. WILL REPLACE JET PUMP AND CHECK VALVE. FUEL FILLING SURGETANK JET PUMP 66QM AND CHECK VALVE 3 7QM. REPLACED 37QM CHECK VALVE PER MM AND REMOVED JET PUMP NOZZLE 66QM FOUND DEBRIS BLOCKING JET PUMP AND ORING CUT. REPLACED JET NOZZLE. ALSO FOUND CHECK VALVE WITH DEBRIS HOLDING IT OPEN. ALL OPS CKS GOOD. 2012-11-16
N828UA AIRBUS A319131 During INSP/MAINT - SEAT ROW 1AB, 23ABC AND 29DEF FAILED OXYGEN DROP TEST PSU'S DID NOT OPEN. ADJUSTED CONTAINER DOOR ACTUATORS AND REPACKING PROPERLY O2 MASK PER MT 35-003 AND PERFORMED OPERATIONAL TEST ALL OKAY. 2012-07-12
N828UA AIRBUS A319131 During INSP/MAINT - DURING THE HMV3 6 HOLES LOCATED BETWEEN FR27 & FR28 AT S39L & S42L WERE INADVERTENTLY OVERSIZED. CLEANED HOLES REF PEMCO EA PT19-53-004 & ECRA # 5320-02056. ACP NDT FOR CRACKS REF NTM. FABRICATED & INSTALLED COUNTERSINK BUSH FOR SKIN & PROTRUDING BUSH FOR INTERNAL STRINGER (FREEZE PLUGS). 2012-05-17
N828UA AIRBUS A319131 During INSP/MAINT - LEFT WING NR 2 SPOILER FAILS FREE PLAY CHECK. REMOVED & REPLACED THE NR 2 SPOILER ASSY. PERFORMED FREEPLAY CHECKS REFAMM. ALL CHECKS GOOD. 2012-05-16
N828UA AIRBUS A319131 During INSP/MAINT - FORWARD CARGO COMP STRINGER 41R CORRODED BTWN FRAMES 30-31. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION & FOUND MATERIAL LOSS OUT OF LIMITS. REMOVED DAMAGE REF SRM 53-21-13. FABRICATED & INSTALLED ANGLE & FILLER REPAIR REF SRM 53-00-13FIG 201. THIS REPAIR REQUIRES RE-INSPECTION REF SRI 53-00-13-2-001-00 TABLE 203 AT 60000 FLT CYCLES AFTER EMBODIMENT OF REPAIR. 2012-05-16
N828UA AIRBUS A319131 During INSP/MAINT - FORWARD CARGO COMPARTMENT STRINGER & RIVET BUCKTAILS CORRODED BETWEEN FRAME 30-34 AT STRINGER 42R. MAJOR REPAIR ACCOMPLISHED. RMV'D RIVETS & RMV'D CORROSION TO STRINGER. FOUND MATERIAL LOSS OUT OF LIMITS OF SRM. ACP NDT FOR CRACKS REF PEMCO EA PT 19-53-003 & ECRA 5320-02054. REMOVED EXISTING JOINT ANGLE NEAR FRAME 34. FABRICATED & INSTALLED EXTENDED JOINT ANGLE REF EA & ECRA TO CAPTURE DAMAGED STRINGER SECTION. 2012-05-16
N828UA AIRBUS A319131 During INSP/MAINT - DOOR 1L DAMAGED DUE TO JETWAY CONTACT. AUTO LEVEL SYSTEM FAULT OR NOT BEING SELECTED ON AFTER DOOR OPENED ON ARRIVAL.DOOR WILL NOT FULLY CLOSE. REPLACED UPPER HINGE ARM. 2012-05-01
N828UA AIRBUS A319131 During CRUISE - SELECTED FLAP RETRACTION AND RECEIVED A VENT VALVE FAULT FIXED WHEN BLOWER OFF. RTF. ACCOMPLISHED CHECK OF AEVC CLASS3 FAULTS AND FOUND AIR OUTLET VALVE 22HQ AND SMOKE DET 1W A DISPLAYED, ACCOMPLISHED WIRING CHECK OF VALVE 22HQ TO AEVC10HQ FOUND NO SHORTS TO GROUND OR OPENS WDM 21-26-10. 2012-02-27
N828UA AIRBUS A319131 During INSP/MAINT - EXTERNAL FUSE SKIN IS DENTED AT FRAME 25+ 13 BETWEEN STR 39-40LT. ACP'D MAJOR RPR AT C-04 VISIT. DAMAGE WAS REMOVED &A DOUBLER WAS INSTALLED PER SRM. 2011-10-24
N828UA AIRBUS A319131 During INSP/MAINT - NR 2 ENGINE N1 VIBRATION AT 6.2 WHEN ABOVE IDLE. AT IDLE VIBRATION 5.0. DEBRIEF CREW FOR CONDITIONS AND IF VIBRATIONS FELT. VISUALLY ACCOMPLISHED A VISUAL INSPECTION OF INLET AND EXHAUST AND NO APPARENT DAMAGE NOTED. MASTER CHIP DETECTORFOUND CLEAN. ACCOMPLISHED VIBRATION SURVEY REF MM. ALL PHASES MAX VIB N1 RECORDED. 1 UNITS. PERFORMED POWER ASSURANCERUN JRH 2-40-35. ALL PARAMETERS NORMAL. 2011-08-25
N828UA AIRBUS A319131 During NOT REPORTED - CAPT O2 MASK INTERCOM APPEARS INOP. REPLACED CAPTAINS QUICK DONNING OXYGEN MASK ASSY PER AMM, OPERATIONAL TEST NORMAL. 2011-08-15
N828UA AIRBUS A319131 During INSP/MAINT - DAMAGE NOTED ON PANEL 621EB TRAILING EDGE. DAMAGED ON OUTBOARD SECTION NEAR ENG 2. REPLACED PANEL 621EB RT WING. 2011-08-02
N828UA AIRBUS A319131 During CRUISE - WX RADAR SYSTEM INOP, FLIGHT DIVERTED. SYSTEM CHECKS NORMAL WHILE AT THE GATE. NO FAULTS FOUND. A/C RETURNED TO SERVICE. 2011-07-06
N828UA AIRBUS A319131 During INSP/MAINT - SEAT ROW 10ABC LIGHT LENS IS WRONG COLOR. SHOULD BE RED. REPLACED LENS PER AMM. REMOVED WHITE AND REPLACED WITH RED (P/N BR9644-22) REF WU C7622L. 2011-05-09
N828UA AIRBUS A319131 During INSP/MAINT - NR 1 ENGINE NOSE COWL AT 6 O'CLOCK POSITION HAS A CRACK RUNNING BETWEEN 3 BLIND RIVETS AND TERMINATING BETWEEN THE 2 ROWS OF RADIAL RIVETS. CRACK LENGTH 2.75 INCHES LONG. STOP DRILL CRACK IAW SRM IN PREPARATION FOR TYPE 2 MX FERRY. NR 1ENGINE NOSE COWL AT 6 O'CLOCK HAS 3 EACH BLIND RIVETS HEADS SHEARED OFF THAT ARE ADJACENT TO EACH OTHER. RIVETS ARE TOBE REPLACED WITHIN 10 HRS. REPLACED NR 1 NOSE COWL IAW MM 71-11-11. 2011-03-24
N828UA AIRBUS A319131 During INSP/MAINT - AVIONICS SMOKE DISPLAYED ON UPPER ECAM SCREEN-SMOKE. ECAM RIGHT AFTER ENG SHUTDOWN AT GATE. PERFORMED ECAM STEPS AND INDICATION VANISHED AFTER. REPLACED BLOWER FAN. 2011-03-03
N828UA AIRBUS A319131 During NOT REPORTED - EMERGENCY LIGHT TEST FAILED. EPSU BATTERY AFT LT FAULTED. REPLACED AFT LT BATTERY IAW MM, CHECKED GOOD. 2011-02-17
N828UA AIRBUS A319131 During CRUISE - EXTRACT FAN FAULT ECAM MESSAGE APPEARED IN CRUISE. FOLLOWED FM PROCEDURE, PUT EXTRACT FAN IN OVRD. ACRID SMELL REMAINSTHROUGHOUT CABIN, IAW CREW. FAN IS BAD. COMPLIED WITH MEL. (FILTER, PCN 565-2066 AND 10HQ AEVC PCN 482-9059). REPLACED EXHAUST FAN AND BOTH AVIONICS FILTERS, ALL CHECKED NORMAL. 2011-01-19
N828UA AIRBUS A319131 During INSP/MAINT - RT WING OTBD FLAP LOWER SKIN DELAMINATED AND SEPARATED FROM FWD SPAR AT RIB 10. DAMAGE IS APPROX 7 AND 1-2 INCHES LONGAND 3 INCHES WIDE. LOCATION IS FROM 1 AND 1-2 INCHES INBD OF RIB 10, EXTENDING 6 INCHES OTBD OF RIB 10 AND IS 3 INCHESFROM LOWER SKIN FWD EDGE EXTENDING AFT. STARTED REMOVAL OF RIGHT FLAP, INTERCONNECTING STRUT DISCONNECTED, ACTUATOR DRIVE LEVERS DISCONNECTED, NEED EXTRACTOR TOOL TO REMOVED PIN FROM FLAP CARRIAGE AND FLAP. SLING INSTALLED. 2010-12-28
N828UA AIRBUS A319131 During INSP/MAINT - 15B LIFEVEST POUCH UNDER SEAT TORN. MADE INTERIM REPAIR WITH TAPE. LIFEVEST IS SECURE IN POUCH AND AVAIL FOR PASS. IFNEEDED. LIFEVEST CONTAINER TO BE REPLACED AT FIRST MAINT. REPLACED POUCH. 2010-12-23
N828UA AIRBUS A319131 During NOT REPORTED - NR 1 ENGINE INLET COWL LIP SKIN HAS A CRACK ACROSS 7 RIVETS. DAMAGED AREA IS LOCATED IN ZONE "J". REPLACED NOSE COWL. 2010-07-19
N828UA AIRBUS A319131 During CLIMB - SMOKE IN CABINS, RTFL. NO VISIBLE SMOKE ONLY PLASTIC BURNING SMELL. NO SMELL IN FIRST CLASS. NO FIRE NOTED AND SMELL WAS COMPLETELY GONE AFTER LANDING. RAN BOTH ENGINES WITH PACKS ON HOT AND COLD. RAN OVEN'S, COFFEEMAKERS, HOT PLATES ANDCHILLERS. CKD CABIN LIGHTS, READING LIGHTS AND EMERGENCY LIGHTS. CKD PCU(S) AND VIDEO SYS. CK E&E COMPT'S. COULD NOT DUPLICATE. 2010-06-16
N828UA AIRBUS A319131 During INSP/MAINT - EXTERNAL FUSELAGE SKIN IS DENTED FRAME 20 PLUS 6", 18" ABOVE CABIN FLOOR, JUST AFT OF DOOR 1R. TEMPORARY REPAIR ACCOMPLISHED PER SRM. PERMANENT REPAIR MUST BE ACCOMPLISHED WITHIN 3000 FLIGHT CYCLES. DAMAGE REMOVED, AREA IS FREE OF CRACKS AND TEMP REPAIR ACCOMPLISHED. 2010-01-26
N828UA AIRBUS A319131 During INSP/MAINT - SUSPECTED CRACK IN FWD CORNER OF UPPER COVER PLATE OF DOOR 2L. FOUND CRACKS IN BOTH UPPER CORNERS. HFEC PERFORMED TO VERIFY LENGTH OF CRACK. REMOVED UPPER COVER FROM DOOR 2L. FABRICATED REPAIR DOUBLERS IAW EVA. NEED TO BE COUNTERSUNK (EXCEPT FOR SCREW HOLES), PRIMED AND INSTALLED. COMPLETED INSTALLATION OF REPAIR DOUBLERS AND INSTALLED NEW RUB STRIPS IAWUA-EVA-73160. PARTS ON WORK ST (PARTIAL). ACP REPAIR DOUBLER REPAIR. DOOR SEAL INSTALLED AND AREA PRIMED AND PAINTED. 2010-01-04
N828UA AIRBUS A319131 During UNKNOWN - ELEC BURNING ODOR NOTED VICINITY OF SEATS 6 D, E, F. ODOR UNDER SEATS 2ABC. ISOLATED TO SEB AT 2ABC. REPLACED PER MM23-33-46. 2008-12-30
N828UA AIRBUS A319131 During INSP/MAINT - CARGO SMOKE TEST FAILS. CYCLE SYSTEM CB'S - ALL TESTED NORMAL AFTER. 2008-03-07
N828UA AIRBUS A319131 During NOT REPORTED - FIRE LOOP B-FAULT DISPLAYED ON UPPER ECAM SCREEN ENG 2. LAST MTC WAS A FDU CHANGE ON 10/24/07. NO REPEATS SINCE THEN.FOUND 2 BAD SPLICES IN 'B' LOOP HARNESS ON PREVIOUS MONTHS REPORTS AND REPAIRED THOSE SLICES. 2007-05-09
N828UA AIRBUS A319131 During INSP/MAINT - BATTERY 2 FAULT ON GROUND. REPLACED NR 2 BATTERY AND BATTERY CHARGER. BATTERY OPS CHECKED NORMAL. 2007-02-07
N828UA AIRBUS A319131 During INSP/MAINT - EMERGENCY LIGHT TEST FAILED EPSU COMM AFT L. REPLACED AFT EPSU. TESTED OK. 2006-10-18
N828UA AIRBUS A319131 During CRUISE - COCKPIT HALON FIRE EXTINGUISHER STARTED LEAKING AT SEAL ON TOP. BOTTLE NOW MOSTLY EMPTY. REPLACED COCKPIT HALON FIRE EXTINGUISHER BOTTLE. 2006-09-08
N828UA AIRBUS A319131 During NOT REPORTED - BURNING ELECTRICAL ODOR COMING FROM ROW 6. FLIGHT ATTENDANT NOTED ELECTRICAL SMELL WHEN AIDING PASSENGER STOW BAGGAGEIN OVERHEAD BIN AT ROW 6. ACCOMPLISHED INSPECTION OF CABIN INTERIOR. PERFORMED MULTIPLE TESTS ON CIDS. REPLACED SIDEWALL LIGHT AT ROW 6L AND SEVERAL READING LIGHTS PRECAUTIONARY. RAN PACKS FOR BURN OUT. INSPECTED GALLEY OVENS, COFFEEPOTS, COFFEE HEATERS, CHECKED WATER HEATERS, AND OVERHEAD CB PANELS. NO SMELL NOTED. 2006-08-23
N828UA AIRBUS A319131 During INSP/MAINT - DOOR 1R SLIDE ELECTRICAL WIRING ROUTED AROUND AFT SIDE OF SLIDE. PER AMIS 1632001 ON 4/10/2006 IN ORD, THE 1R DOOR SLIDE MR25611-205 WAS REPLACED WITH SLIDE MR25611-1112 PER AMM 25-62-44 DUE TO MR TIME SET TO EXPIRE 4/14/2006. AMIS ITEM 1632001, THE SUBJECT OF THIS SDR, NOTES THAT THE SLIDE ELECTRICAL WIRING WAS NOT PROPERLY ROUTED. THE SLIDE ELECTRICAL WIRING WAS REROUTED PER AMM 25-62-44. 2006-05-30
N828UA AIRBUS A319131 During INSP/MAINT - FUSELAGE STRUCK BY JETWAY AFT OF DOOR 1L. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH SRM 53-00-11, FIGURE 203. 2006-04-03
N828UA AIRBUS A319131 During CRUISE - UNWANTED FUEL TRANSFER IN FLIGHT FROM LEFT MAIN TO CENTER TANK. ACCOMPLISHED FAULT ISOLATION PROCEDURE PER MM 28-12-00-818-801 AND RESULTS WERE *NO FAULTS FOUND*. ACCOMPLISHED VISUAL STATIC CHECK OF CENTER FUEL TANK RESULTING IN -NO DEFECTS-. TRANSFERED APPROXIMATELY 2000 LBS OF FUEL INTO CENTER TANK AND VERIFIED DRIPSTICK READINGS IN RELATION TO FUEL INDICATIONS RESULTING IN -DRIPSTICK READINGS AND FUEL QUANTITY INDICATIONS CORRECT-. ENGINEERING WILL CONTINUE TO MONITORAND TO DATE NO ISSUES REGARDING UNWANTED FUEL TRANSFER. 2006-01-30
N828UA AIRBUS A319131 During INSP/MAINT - FWD LT EMERGENCY POWER SUPPLY AND BATTERY FAILS TEST. REPLACED POWER SUPPLY AND BATTERY. 2005-09-14
N828UA AIRBUS A319131 During CLIMB - ELECTRICAL SMELL OBSERVED IN THE FLIGHT DECK. NSPECTED GALLEY AREAS AS WELL AS AVIONICS COOLING FANS. FLIGHT CREW HAD NO OTHER ABNORMAL INDICATIONS OR SYSTEM MALFUNCTIONS. ACCOMPLISHED POWER RUNS AND REPLACED AEVC FILTER CARTRIDGE AS PRECAUTINARY MEASURES. NO TRIPPED BREAKERS FOUND. CAUSE UNDETERMINED. 2005-01-26
N828UA AIRBUS A319131 During INSP/MAINT - EMERGENCY SEAT TRACK LIGHTING INOPERATIVE AT ROWS 15, 16, 19, 20, 23 AND 24. WIRE HARNESS WAS INOPERABLE. REPAIRED WIREHARNESS 350WL10 FOUND UNDER SEATS 23AND 24 ABC. 2004-09-07
N828UA AIRBUS A319131 During CLIMB - NUMBER 1 OIL QUANTITY INDICATOR INOP. SUPPLEMENTAL DATA UPDATE FOUND LOOSE PIN ON OIL QUANTITY TRANSMITTER CONNECTOR. TRANSMITTER WAS ALSO REPLACED. 2001-01-11
N828UA AIRBUS A319131 During TAXI/GRND HDL - CREW REPORTS NOSE STEERING DISCONNECT MESSAGE COMES AND GOES. WHEN MESSAGE APPEARS UNABLE TO STEER ACFT. NECESSARY TOCHECK AND CORRECT. *S/D* REPLACED NOSE WHEEL STEERING ELECTRICAL BOX. 2000-10-16
N828UA AIRBUS A319131 During TAKEOFF - ON TAKEOFF CREW HEARD A LOUD BANG AND ANOTHER AIRCRAFT OBSERVED DEBRIS DEPARTING AIRCRAFT. SAN AIRPORT RECOVERED TIRE DEBRIS FROM RUNWAY. LEFT NOSE LANDING GEAR TIRE TREAD SEPARATED ON DEPARTURE. FLIGHT DIVERTED TO LAX UNDER AMBER ALERT.*S/D* LT NLG TIRE TREAD SEPARATED ON DEPARTURE. LEFT NOSE TIRE ON ARRIVAL FOUND TREAD MISSING. REPLACED LEFT NOSE AND RIGHT NOSE TIRE PER MM 32-41-12. 1999-09-17
N828UA DOUG DC1010 During CLIMB - AIRCRAFT DEPARTED SFO. ON TAKEOFF CLIMB (1820Z), NR 2 ENGINE EXPERIENCED A FIRE WARNING INDICATION. ENGINE WAS SHUTDOWNAND EMERGENCY CHECKLIST PROCEDURES WERE ENACTED. AIRCRAFT RETURNED TO SFO. UPON TROUBLESHOOTING, MAINTENANCE FOUND TWO BROKEN LOOP CONNECTORS. CONNECTORS WERE REPLACED AND AN OPERATIONAL CHECK WAS PERFORMED. OPS CHECK WAS GOOD AND AIRCRAFTWAS RETURNED TO SERVICE. 1986-08-15

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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.