N463UA
Registered owner: UNITED AIRLINES INC, IL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| UNITED AIRLINES INC | Operator | 2020-12-23 – 2020-12-23 | Operator named in NTSB report |
| UNITED AIRLINES, INC. (CALA) | Operator | 2020-12-23 – 2020-12-23 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
LOUD STATIC OVER HEADSET, CLEANED INTERPHONE JACK WITH APPLICABLE CLEANER, OPS CHECK NORMAL, NO STATIC FROM HEADSETS GOOD TO CONTINUE.
HYD Y SYS LO LVL ECAM APPEARED AFTER TAKEOFF. CREW STATED THEY LOST YELLOW SYS ON TAKEOFF. SHUT YELLOW HYD ELECT PUMP OFF IMMEDIATELY. FLT WAS JUST OVER A HOUR. CONFIRMED YELLOW SYS EMPTY ON LOWER SERVICE PANEL QTY GAUGE & ON PANEL. MET ACFT ON TAXIWAY, ACFT HAD ZERO HYD FLUID IN YELLOW SYS. NOSE STEERING & CARGO DOORS INOP. INSTALLED GEAR PINS. INSPECTED ACFT , FOUND HYD LEAK UNDER RT ELEVATOR, ALONG WITH A PUDDLE OF FLUID UNDER RT STAB. ACCOMPLISHED STEP K OF AMM 27-34-51-400-001A. ACCOMPLISHED RII INSPECTION OF AMM 27-34-51-400-001A STEP K. CONTINUE THE FROM STEP (D) TO FINISHED OPS CHECKED GOOD AN NO LEAKS IAW AMM 27-34-51-400-001-A. COMPLETED OPS & LEAK CHECKS. SYSTEM OPS NORMAL & NO LEAKS NOTED IAW AMM27-34-51-400-001-A AND GMM09-25-05.
R2 DOOR SILL HAVE EXFOLIATION CORROSION AT FLOOR BOARD FASTENER HOLE JUST FWD OF THE FR68. REPAIRED RR2 DOOR SILL FWD OF THE FR 68 IAW A320 SRM 51-41-14-30 0-001.
Y1292 FWD FLOOR BEAM SEAT TRACK CORRODED @ FR64. REMOVED AND REPLACED FWD FLOOR BEAM SEAT TRACK Y1292 AT FR64 IAW A320 SRM 51-72-11-911-002.
L2 DOOR SILL HAVE EXFOLIATION CORROSION AT FLOORBOARD FASTENER HOLE JUST FWD OF THE FR68. ACCOMPLISHED AFT PASSENGER/CREW DOOR SILL BEAM REPAIR IAW A320 S RM 53-41-14-300-001 AT L2 DOOR.
LEFT AFT SHEAR PLATE @ FR70 CORRODED.
SLIDE PRESSURE GAUGE - VISIBILITY POOR AT DOOR 2L REMOVED L2 DOOR SLIDE. REF AMM 25-62-44 REPLACED L2 DOOR SLIDE. REF AMM 25-62-44. VEREFIED DOOR 2L SLIDE PART NUMBER IS CORRECT REF IPC 25-62-04-02W. VEREFIED PROPER INSTALLATION REF MM 25-62-44-400-006. VERIFIED SAFETY PIN REMOVED AND STOWED WITH SLIDE PACK. GMM 09-25-05.
R/H ELEVATOR TOP SIDE HAS WATER INGRESS AT 123 1/2 IN I/B, 6 IN T/E, 3 IN DIAMETER, "REPAIR PRIOR TO FLIGHT". DRILLED WITNESS HOLES IN R/H ELEVATOR TOP SKIN 123.5 IN FROM I/B 6.IN FROM T/E 1.5IN ON IAW A320 AMM 55-20-00-006-A01 PAR4A(7) FO UND NO LIQUID. REPAIRED AREA IAW A320 SRM 55-21-11-300-004 CAT A REPAIR.
R/H ELEVATOR TOP SIDE HAS WATER INGRESS AT 200 1/2 IN I/B, 4 1/2 IN T/E, 3 IN DIAMETER, "REPAIR PRIOR TO FLIGHT". REPAIRED R/H ELEVATOR TOP SIDE 200 IN I/B 4.5IN FROM T/F 4.5IN B Y 3IN ZONE C IAW A320 SRM 55-21-11-300-005 CAT A REPAIR.
R/H ELEVATOR TOP SIDE HAS WATER INGRESS AT 39IN I/B, 4 1/2IN T/E , 1 1/2IN DIAMETER, "REPAIR PRIOR TO FLIGHT" GEN BY V061632 ON H AECO LCQ NR 9294227/26227
LH FUSELAGE BELLY FAIRING VERTICAL SUPPPORT AT FR35 CRACKED. REMOVED AND REPLACED CRACKED SUPPORT VERT ANGLE AT LH FUSELAGE F R35 IAW A320 SRM 51-72-11-911-001.
PDA 2 UNDERWING REFUEL CAP MISSING REPLACED REFUEL CAP PER AMM. 28-25-41PARTS USED: 31-2825-9-0001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1356663 SN OFF 2456 IPC REFERENCE # 28-25-41-02B
IDG 1 OIL LO PR DISPLAYED ON UPPER ECAM. MEL 2420E REQUESTED, VERIFIED #1 ENG GENERATOR IDG IS STATING (AUTOLAND LIMIT CAT 3 SINGLE) OTBD OF CAPTS PFD. #1 ENG IDG PLACED ON MEL 2420E, MEL DDP C/W. NOTE: PRIOR TO SERVICE, PYLON MOUNTED IDG CONNECTORS MUST BE VISUALLY INSPECTED AD2011-19-01 R1 REQUIREMENTS. C/W DAILY REQUIREMENTS REF MEL 2420E. DAILY REQUIREMENT CW DISCONNECTED, C/W LOAD SHED DDP, AND PLACED 44-0017 PLACARD CLEARING THIS DEFERRED ITEM AND RESTORING INOPERATIVE IDG TO FOR ARCING CONDITIONS (REF. AMM 24-21-43-210-048C1), REF TSM 24-20-00-810-847-A TO ASSIST, T/S NO DEFECTS NOTED. REMOVED ENG #1 IDG REF AMM TASK 24-21-51-000-010-A INSTALLED IDG FEEDER CABLES REF AMM 24-21-51. REQUIRES #1 ENGINE VERIFIED PARTS AND TORQUES OF IDG AND IDG FEEDER. INSPECTION BUYBACK FOR INSTALLATION TORQUE. CABLES,INSPECTED CABLES FOR DAMAGE AND ARCING, PER AMM 24-21-51 REPLACED ENG #1 IDG REF AMM 24-21-51. PERFORMED IDLE RUN LEAK TEST REF 71-00-00 TEST 3. NO LEAKS FOUND. PERFORMED OPS CHECK OF IDG REF AMM 24-21-00-720-042-A. NO FAULTS FOUND OK TO CONTINUE.
G RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN. - HYD DEBRIEFED CREW. CREW STATED THAT AFTER DEPLOYING GEAR, RECEIVED RH RETRACT ACTUATOR HOSE LEAK REMOVED AND REPLACED BOTH RH MLG DOOR ACTUATOR HYD GRN RSVR LO LVL ECAM. CREW CHECKED GREEN QTY INDICATION AND LINES..SERVICED GREEN SYSTEM. REF AMM 32-31-38..STILL NEED LEAK NOTED IT WAS EMPTY. LEAK COMINNG FROM RIGHT WHEEL WELL. GAUGE CK AND OPS CK. AND MORE CLEANING OF THE AREA. PARTS USED: SHOWS SYSTEM EMPTY. 18-3231-3-0081,QTY :1 CLEANED UP AREAS AROUND NEW HOSE REPLACEMENT, AND UNDER BELLY FUSELAGE. SERVICED GREEN HYDRAULIC LEVEL TO TOP. CYCLED GEAR DOORS EIGHT TIMES -- NO AVTIVE LEAKS NOTED. NO ECAM MSG NOTED.
SHOCK ABSORBER FAULT DISPLAYED ON UPPER ECAM SCREEN - L-G L/G SHOCK ABSORBER FAULT AT FL360. AP AND AUTOTHRUST LOST 3 MIN LATER. LIMITS. TARGETS ALSO OUT OF LIMITS AFT OF SENSORS. REPLACED BOTH SENSORS PRECAUTIONARY REF AMM TASK 32-31-73-400-005-A. ADJUSTED GAPS AND TARGET POSITION REF AMM TASK 32-31-73-820-006-A. SENSOR INDUCTANCE CHECKS GOOD REF AMM TASK 32-31-73-820-009-A. LOCKED LOG PAGE DUE TO HISTORY ASSOCIATED MESSAGE ''N LG SHOCK ABSORBER (2526GM)'' SHOWING W/BOTH NEED TO ACCOMPLISH LANDING GEAR BITE TEST REF AMM TASK LGCIU''S AS SOURCE. REF TSM 32-31-00-810-868-A, REFERS TO FAULT 32-69-00-740-001-A FOR REPLACEMENT OF SENSORS. SUGGEST SHOWING FOR ''NLG EXT PROX SNSR 24GA TGT POS''. REF TSM TASK ACCOMPLISH NLG STRUT SERVICE AND GEAR SWING DO TO RECENT HEAVY 32-31-00-810-842-A, FOUND 24GA AND 25GA TARGET GAP OUT OF VISIT. ADD EMP:101154 ITEM UNLOCKED FOR CLEARING ACTION ACCOMPLISHED NOSE GEAR SWING OPS CHECKED, SWITCHES OPERATED OK, NO MSGS NOTED. BITE CHECKED OK.
IN FLIGHT RECEIVEDL/G SHOCK ABSORBERFAULT. DIVERSION ON HVY MX CHK FERRY FLT. NLG SHOCK ABSORBER FAULT ON MM TASK 32-69-00-740-001-A) NO FAULTS. ALSO INSPECTED NLG FOR PFR (24GA). INSPECTED SENSOR AND FOUND CONNECTOR NOT COMPLETELY OBVIOUS DEFECTS, NONE NOTED. SEE PHOTO OF PFR, LLR, AND LGCIU''S LOCKED. CONNECTED SAME AND ALL FAULTS ERASED. CONNECTOR IS NOW LLR. ALL CKS NORMAL AND SYSTEMS RETURNED TO NORMAL. ACFT IS OK SECURELY LOCKED IN PLACE. PERF LGCIU BITE ON BOTH LGCIU''S, (REF FOR SERVICE.
EPSU BATTERY (11WL) TEST FAILED; BATTERY NEEDS TO BE REPLACE. AS NOTED ON LTPR NR# 5001232930-0010. ESPU BATT.(11WL) FAILED ON EMER.LIGHTING BATT.CAPACITY TEST. BATT.REP.OF (11WL) PERFORMED IAW AMM:33-51-38-000/400-002 REV.119. TEST SATIFACTORY. P/N OFF:AD3214-31 S/N OFF:242320 QTY: 1EA P/N:AD3214-3 S/N ON: 273851 QTY:1EA.
EPSU BATTERY 13WL TEST FAILED, BATTERY NEEDS TO BE REPLACE. AS NOTED ON LTPR NR#5001232932-0010. ESPU BATT.(13WL) FAILED ON EMER.LIGHTING BATT.CAPACITY TEST. BATT.REP.OF (13WL) PERFORMED IAW AMM:33-51-38-000/400-002 REV.119. TEST SATIFACTORY. P/N OFF:AD3214-31 S/N OFF:261409 QTY 1EA P/N:AD3214-31 S/N ON: 242257 QTY:1EA.
ESPU BATTERY (12WL) TEST FAILED; BATTERY NEEDS TO BE REPLACE. AS NOTED ON LTPR NR#5001232931-0010. ESPU BATT.(12WL) FAILED ON EMER.LIGHTING BATT.CAPACITY TEST. BATT.REP.OF (12WL) PERFORMED IAW AMM:33-51-38-000/400-002 REV.119. TEST SATIFACTORY. P/N OFF:AD3214-31 S/N OFF:252801 QTY 1EA P/N:AD3214-31 S/N ON: 278854 QTY:1EA.
EPSU BATTERY (10WL) TEST FAILED; BATTERY NEEDS TO BE REPLACE. AS NOTED ON LTPR NR# 5001232929-0010. ESPU BATTERY (10WL) FAILED ON EMERGENCY LIGHTING BATTERY P/N ON:AS3214-31 S/N ON:279092 QTY:1EA WORK ACCOMPLISHED CAPACITY TEST.BATTERY REPLACEMENT OF (10WL) PERFORMED IAW AMM: 5P1122 AND INSPECTED BY 5P0620. 33-51-38-000-002 REV.119 AND AMM:33-51-38-400-002 REV.119. TEST SATISFACTORY. P/N OFF:AD3214-31 S/N OFF:287045 QTY:1EA
PDA 3, AFT LOWER LEFT WING TO BODY FAIRING MISSING SECTION OF SEAL LOWER SERFACE. REPAIRED DAMAGED SEAL PER ECRA 5335-01125. PARTS USED: 18-5335-3-0005.
PDA 3 OPS REPORTS FUEL CAP LANYARD MISSING WAGSTAFF, MARK (V081328)APPLIED CDL 28A. LANYARD MISSING PER CDL DISPATCH DESK: 21 NAME: AL DATE: 16-MAY-22- DEFERRED DIRECTLY BY TOMC UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V081328 PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. CDL 28A MAC RELATED WORK ORDER 000000003044366 AND PRTR WAGSTAFF, MARK (V081328)APPLIED CDL 28A. LANYARD MISSING PER CDL REPLACED DAMAGED CHAIN/ LANYARD AND REINSTALLED CAP REF AMM 28-25-41 OPS CK GOOD
ELEC GEN 1 FAULT ON ECAM WITH NUMEROUS FAILURES UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. CHECKED. WIRING OF THE DISCONECT IDG PER ASM 24-21-01 S 010-009, AND 24-21-51-400-040, PER FAILURE OF THE TDC AC SENSOR ACCPD TSM PERFORMED MSG ELEC GEN 1 FAULT REMAIN , OPEN MEL 2420E OK TO DEFER PER MEL . FOUND OPEN SOLENOID, REPLACED IDG ENG 1 PER AMM 24-21-51-000-040 24-22-00-810-809, REPLACED ENG OIL PRESS RELAY 7XT, AFTER WORK ROTABLE PARTS CHANGE WAS INDICATED - TT # 1111726 SN OFF 9167 ADD EMP:U230133 IPC REFERENCE # 24-21-51 APPROVED FOR MEL2420E ACCOMPLISHED INPECTION CHECK OF IDG REPLACEMENT, ALL STEEPS IAW AMM 24-21-51-000-040. ADDED IDG PLATE PICTURE SIDE OF ENG PYLON REF WD 24-22-01 PG 9, REQUIRES ADDITIONAL OPEN UP TO FURTHER EVAL DAMAGE CHECKED WIRING FROM IDG TO 9XU1 AND FOUND FEEDER T3 SHORTED TO GND, FURTHER T/S FOUND FEEDER CABLES BURNT AT 400VT1 AT GENERATOR, INTE OFF 31-2411-9-0001 9167 ON 31-2411-9-0001 0987 PYLON HARRNESS DG 200.REF AMM 24-21-43,AWM 24-22-01, AND ESPM 20-48-11. REPLACED 400VT1,RETERMINATED CABLES 2422-4504,2422-4505, AND 2422-4506,2422-4507 AT 400VT1.STILL REQUIRES REPLACEMENT OF IDG ADD EMP:U231871 REMOVED AND REPLACED #1 ENGINE IDG FEEDERS ON PYLON, REF AMM 24-92-00-400-001-A
BIRD STRIKE ON CLIMB.8000AGL. 250KIAS.FLAPS UP. PIC ADDED CLEANED BIRD IMPACT AREA AT TOP OF RADOME AND CAPT WINDOW. PERFORMED BIRD STRIKE INSPECTION REF AMM 05-51-14-200-803-A. NO DAMAGE FOUND. OK TO CONTINUE.
COCKPIT WINDOW L3 SHATTERED. 2 SEPERATE TIMES APPROX 14000MSL/26 00 CABIN ALT UP LOAD PHOTOS INFORMATION ONLY FOR L3 WINDOW INFORMATION ONLY BY CAPTAIN NO OVER WEIGHT LANDING. LANDING WAS REMOVED COCKPIT L3 WINDOW REF AMM 56-11-12-000-001-A WINDOW IN POSITION. ORDERED NEW SCREWS SINCE OLD SCREW HEADS INSTALLATION OF NEW WINDOW AMM 56-11-12-400-002-A THRU STEP 4A 1 NORMAL. TOO WORN TO ACHIEVE PROPER TORQUE. CONTINUED INSTALLATION OF L3 WINDOW FROM 56-11-12-000-001-A, STEP 4A1 TO END. OPERATIONAL CHECK GOOD. ADD EMP:U334021
EMER EXIT LIGHT TEST GIVES MESSAGE OF ESPU BATTERY EMERGENCY LIGHT &ESPU BATTERY . RESET BOTH ESPUS, NO HELP. REPLACED THE BATTERY PACK FOR ESPU 11WL & 12WL IAW AMM 33-51-38-000-002-A & 33-51-38-400-002-A, OPS CHECKED OK. ACCOMPLISHED THE INSPECTION OF THE INSTALLATION OF BATTERY PACKS AT 11WL AND 12WL AND OPERATIONAL CHECK.
REF N/R 9024440, RT WING LOWER SURFACE CUTOUT PANEL 640LB FA STENER HOLES IN WING STRUCTURE DAMAGED MULTIPLE LOCATIONS REPAIRED DAMAGED FASTENER HOLES AT RT WING LOWER SURFACE CUTOUT PANEL 640LB IAW SRM 57-27-11-283-002 AND SRM 57-21-11-300-0 03. ACCOMPLISHED ROTO PROBE AND HFEC INSPECTION OF REWORKED HOLES AND ADJACENT AREA, NO CRACKS FOUND, IAW NTM 51-10-01 AND 5 1-10-03. REMOVED AND REPLACED GANG CHANNEL IAW SRM 51-42-11 AND SRM 57-21-11-300-003. THIS IS A CATEGORY "B" REPAIR I 57-21-11-205-037. CURRENT FH IS 62419/ FC 24841. H, SUBSEQUENT INSPECTIONS AT INTERVALS OF 1500 FC/3000 FH IAW SR INSPECTION THRESHOLD FROM AIRCRAFT FIRST FLIGHT 16000 FC/32400 F PANEL 640LB INSTALLED ON CUSTOMER CARD ZONE 640 CLOSE SEQUENCE 2 267 APPROVED DIP FOR REPAIR TO PANEL 640LB FASTENER HOLES PER SRM 57-27-11-283-002 AND SRM 57-21-11-300-003. CAT B REPAIR REQUIRES REINSPECTIONS.
N/R 9023966 (A3NB-53-4-6179, A27-NO DOT) AFT CARGO WASTE SPILL, TOILET PAPER FOUND AT FRAME 63-65 STR 37-39 REMOVED AND INSTALLED INSULATION. CLEANED AFT CARGO WASTE SPILL IAW EC/RA 2011-01000 REV AA AND AMM 25-80-00-000-001-A, AMM 25-80-00-400-001-A, AMM 12-21-12-100-006-A.
AFT CARGO, DOOR SILL TORSION BOX HAS COR ROSION AND DEEP PREVIOUS BLEND OUTS. AAR N/R S/N 9024001 REMOVED CORRODED AFT CARGO DOOR SILL TORSIONBOX IAW A320 SRM 51- TOR SION BOX IAW A320 SRM 51-46-11-001 REMOVED TO F.O.M. AND REI NSTALLED HORSE SHOE TOP PLATE IAW A320 SRM 51-42-11-001. INSTALL ED NEW AFT CARGODOOR SILL TORSION BOX COVER IAW A320 SRM ADD EMP:V919097 42-11-001. LOCATED DRILLED & COUTERSUNK NEW AFT CARGO DOOR SILL 1-001. 51-72-11-911-001. RESTORED PROTECTIVE COATING IAWA32 SRM 51-23-1
L-2 DOOR SILL HAS CORROSION AROUND AFT GIRT BAR FITTINGS. AAR NO NROUTINE 9024224 BLENDED AND REMOVED CORROSION I.A.W A320 SRM 51-74-00. NO CORROS ION ALLOWED I.A.W A320 SRM 53-41-14-283-002 REMOVED AND REPLACED DOOR SILL N L2 I.A.W A320 SRM 51-42-11
R-2 DOOR SILL HAS CORROSION AROUND AFT GIRT BAR FITTINGS. AAR NO NROUTINE 9024225 BLENDED AND REMOVED CORROSION IAW SRM 51-74-00. NO CORROS ION ALLOWED IN AREA I.A.W A320 53-41-14-283-002. REMOVED AND REPL ACED DOOR SILL IAW SRM 51-42-11 ON R2 DOOR
SEAT 2F WHEN PAX HAD DEVICE PLUGGED IN, HAD AN ELECTRICAL ODOR. STOPPED WHEN UNPLUGGED, NO FAULT CONFIRMED, PLUGGED IN DEVICE. NO SMOKE COMING OUT. REMOVED OUTLET. VISUALLY INSPECTED HARNESS CONNECTION TO OUTLET. OUTLET CHECKED GOOD. WORK PERFORMED IAW AMM 25-21-89
EMERGENCY LIGHTS TEST DISPLAYED EPSU BATTERY AFT LEFT RESET SYSTEM. OPS CKS GOOD.
LEFT OVERWING EXIT DOES NOT SHOW ARMED USING RENDER CHECK LIST AND AMM 52-71-00-70-001-A FOUND LT FWD OVER WING EMERGENCY EXIT LATCH PIN OUT OF DETENT. PLACED PIN IN CORRECT POSITION IAW AMM. ALL INDICATIONS NORMAL.
EPSU FWD AND RT BATTERY FAULT LIGHT DURING TEST. REPLACED EMERGENCY BATTERIES PER AMM 33-51-38.
FLIGHT INCURRED YELLOW HYD SYSTEM LOW PRESSURE LIGHT ENROUTE. EMERGENCY DECLARED. REPLACED ORING ON MANIFOLD ASSY IPC 29-13-14-05A ITEM 40. LEAK CHECK AND ENG RUN GOOD.
EXTERIOR FUSELAGE SKIN HAS SCRATCH JUST BELOW AOA VANE MOUNT PLATE. BLENDED SCRATCH ON LT FUSELAGE SKIN, 6.5 INCHES FWD OF FRAME 24 ABOVE SKIN LAP AT STRINGER 28 IAW SRM 51-73-00 PARA F PG 5. HFEC REVEALED NO CRACK INDICATION.
LANDING GEAR SENSOR FAULT ON DESCENT.
AIR EXCHANGER FAULT DISPLAYED ON UPPER ECAM SCREEN, AIR VLV CLOSED ENG 2. IAW TOMC SHUTDOWN ENGINE, RESET A05, Q40, Q07 & F01, NO HELP. REPLACED ACOC MODULATING VLV IAW AMM79-21-51401. TESTED SYS IAW AMM79-21-51-400-010-A PARA 5AB, ALL OPERATIONS & LEAK CHECKED NORMAL. REMOVED ACOC MODULATING VLV MR 79218 DID NOT HAVE A DASH, ONLY SN1384.
BLUE RESERVOIR LOW AIR PRESS DISPLAYED ON UPPER ECAM SCREEN. HYD BLUE SYS HYD RESERVOIR OVER SERVICED. DRAINED & REPLACED YELLOW HYD SYS RESERVOIR DRAIN VALVE, ON ACCOUNT OF STUCK OPEN WHEN DRAINING SYSTEM DUE TO OVER SERVICE.
CAPTAIN`S WINDSHIELD WIPER INOPERATIVE. WIPER MOTOR PCN 565-9005 AMM 30-45-51. SWITCH PCN 565-0615, TSM 30-45-00-810-801. ADJUSTED CAPTAIN`S WIPER BLADE, CYCLED SEVERAL TIMES & OPERATIONS CHECKED NORMAL IAW AMM.
RT WS HT COMPARTMENT 2DG2 AFT CONNECTOR 2DG2 B BACKSHELL BROKEN.
RT WINDOW DISPLAYED ON UPPER ECAM SCREEN, ANTI-ICE. REPLACED RT WHC 2DG2 IAW AMM, OPERATIONS CHECKED OKAY.
RT WS HT COMP 2DG2 AFT CONNECTOR 2DG2 B BACKSHELL BROKEN.
RT WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN, ANTI-ICE. CLEANED & RESET CONNECTOR ON WHC 2. OPERATIONS CHECKED GOOD.
F/O`S SLIDING WINDOW HEATING INOPERATIVE. COLD SPOT ON FWD 1-3 OF WINDOW. RUNS VERTICALLY THE LENGTH OF WINDOW. CONDENSATION AS WELL. REPLACED WINDOW PANE, WINDOW HEAT TESTS OK.
LOOSE SCREW ABOVE COCKPIT DOOR. REPLACED SCREW ON FWD UPPER LT CORNER ON FWD SIDE OF COCKPIT DOOR.
PLASTIC COVER OVER EMERGENCY LIGHT SWITCH ON AFT F/A PANEL MISSING. REPLACED EMERGENCY LIGHT SWITCH COVER. SAFE AND FUNCTIONAL.
PANEL AFT OF DOUBLE DRAINS ON FWD FUSELAGE L/E EXPOSED AND SCREW PULLING THRU-POS DELAMINATED. APPLIED SPEED TAPE IAW MT 53-00-02, PANEL MUST BE REPLACED WITHIN 300 HOURS.
1ST OFFICER'S WINDSHIELD'S VISIBILITY IS AFFECTED BY DEFECTS. CREW COMMENTS: SMALL CREASE IN F/O WINDSHIELD IN DIRECT FIELD OF VISION THAT CAUSES SLIGHT DISTORTION. REMOVED AND REPLACED WINDSHIELD.
CAPTAIN'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). SWAPPED CAPTS OXYGEN MASK SERIAL 94410 WITH SEC OBS SEC OBS MASK SER 71814 NOW IN CAPT POS PER TASK 35-12-41 PAGE BLOCK 0401. OPS CHECK TASK 23-51-00-710-004 -A AND TASK 35-12-41-710-001-A. OPS CHECK GOOD. PLACED SEC OBS SEAT ON DEFERRAL DF472. RPL- :REPLACED O2 MASK. OPS OK.
CABIN EMERGENCY LIGHT CHECK FAILED ON 2 2SVC. REPLACED AFT EPSU BATTERY PER MM,TEST PASSED OPS CHECKS GOOD.
EMERGENCY LIGHT CHECK FAILED ON 2 2SVC. REPLACED AFT EPSU BATTERY, TEST PASSED. OPS CHECKED GOOD.
CAPTAIN'S O2 MASK PRESS TO TEST NOT WORKING. REPLACED CAPTAIN`S 02 BOX.
FOUND ON NR 2 SERVICE LAV SMOKE CHECK, CALL LIGHT FOR LAV F DOES NOT ILLUMINATE (591RH6) ASM23-73-18. ALSO CIDS CLASS 3 FAULTS "PAX CALL LAMP LAV F" FAULTED. SWAPPED LAMPS WITH KNOWN GOOD LAMPS, NO HELP. FOUND WIRES BEHIND LIGHT ASSY NOT CONNECTED. SECURED CONNECTOR AND OP-CHECK SATSFACTORY.
FASTENER MISSING LEFT SIDE FUSELAGE NEAR TRAILING EDGE OF INBOARD FLAP. SAMC TEXT: PANEL 197BB. REPLACED FASTENER LEFT SIDE FUSELAGE AT BLUE HYD SERVICE PANEL.
SLAT SYS 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. - F -CTL. REPLACED SFCC1 AND OP CHECK SATISFACTORY.
AFT CARGO MIX VALVE STAYS FULL COLD EVEN WITH TEMP CONTROL KNOB ROTATED TO FULL HOT. DEFFERED AFT CARGO HEAT HOT AIR PRESS REG VALVE. COMPLETED REQUIREMENTS OF MEL ITEM 2143B. REMOVED AND REPLACED AFT CARGO HEAT PRESS REG VALVE REF AMM 21-43-52, OPS CHECKS GOOD.
NR 1 OUTBOARD PYLON BLOW OUT PANEL 471BL FOUND OPEN AT ARRIVAL. INSPECTED DUCTS AND LEAK CHECKED OK.
EXT FUSELAGE DENTED BETWEEN FR 21 AND 22 AND BETWEEN STR 22L AND 23L. MAJOR REPAIR ACCOMPLISHED: FOUND OUT OF LIMITS. INSTALLED EXT DOUBLER PER SRM.
EXT FUSELAGE DENTED BETWEEN FR 23 AND 24 AND BETWEEN STR 42R AND 43R. FOUND OUT OF LIMITS. INSTALLED EXT DOUBLER PER SRM 53-11-11 FIG 104.
CORROSION AT L2 DOOR THRESHOLD AT AFT INBOARD CORNER. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR PER SRM 53-41-14 FIG 201 ON NR 25483.
LEFT WING SIDESTAY UPPER CARDAN ATTACH FITTING OUTBOARD LUG BORE HAS PITTING CORROSION. BUSHING REMOVED, BORE CLEANED AND BUSHING REPLACED PER SRM.
RIGHT WING SIDESTAY UPPER CARDAN ATTACH FITTING OUTBOARD LUG BORE HAS PITTING CORROSION. BUSHING REMOVED, BORE CLEANED, AND BUSHING REPLACED PER SRM.
LT ENG OIL PRESSURE READS ALMOST FULL SCALE 298PSI ON TAKEOFF, NOTICED MOMENTARY FLUCTUATION. REMOVED AND REPLACED OIL PRESSURE TRANSMITER, PER MM 79-33-15-000-010-A 13,79-33-15-400-0 10-A 13.
L1 DOOR SLIDE SHOWS ARMED WITH DOOR OPEN, ECAM SLIDE MESSAGE ON, WITH DOOR OPEN AND IN DISARMED. REPLACED SDAC-1 PER TSM 52-11-00-810 -804. AND AMM 31-55-34-000-001 MESSAGE CLEARED. OPS CHECKED GOOD
DOOR 1L SLIDE SHOWS ARMED WITH DOOR OPEN. ECAM SLIDE MSG ON WITH DO OR OPEN AND IN DISARMED. REPLACED PROX SWITCH 4WN1 AND RELAY EO245-28AO, NO HELP. REPLACED 1WN1 SLIDE ARMED INDICATOR LIGHT. NO HELP. REPLACED SDAC-1 PER TSM, MESSAGE CLEARED. OPS CHECKS GOOD.
OXYGEN BOTTLE MISSING, USED AT AFT CABIN, FWD CABIN FLIGHT ATTENDANT REPORTED THAT THE OXYGEN BOTTLE WAS FULL BUT FAILED TO PROVIDE OXYGEN TO PASSENGER. REPLACED OXYGEN BOTTLE AT AFT CABIN.
1ST OFFICER'S SLIDING WINDOW'S VISIBILITY IS IMPAIRED. CLEANED WINDOW FOR BETTER FLIGHT VISIBILITY, WINDOW WITHIN LIMITS. BUBBLES DO NOT IMPAIR FLIGHT VISIBILITY.
NR 2 ENG FIRE LOOP A TB 450VT2 NEED OP CHECK AFTER SUPPORT BRACKT INSTALLATION. REPLACED BRACKET AND BURNDY BLOCK. NR 2 ENG STILL HAS "A" LOOP FAULT AFTER ENG START. FIRE LOOP A FAULT DISPLAYED ON UPPER ECAM SCREEN. REPLACED FIRE LOOP, OPS CHECKS GOOD. MESSAGE RETURNED. REPLACED 4000WD1 AND 3WD2. CHKD OK ON ENG RUN AND BITE TEST. FAULT REOCCURED ON TAXI OUT. RING OUT ALL WIRING AND LOOPS ALL CHECK GOOD. WITH ENG BLEED ON FIRE LOOP 'A' FAULTING. WITH APU BLEED ON AND BOOST 1 SELECTED, NR 2 ENG FIRE LOOP 'A' FAULTS. LARGE LEAK FOUND AT OVERPRESSURE VALVE ON NR 2 ENG. REPLACED OVERPRESS VALVE, NO LEAKS. REPLACED FDU PER MM WITH APU BLEED ON, NO FIRE DET FAULTS. RAN ENG FOR 10 MIN WITH BLEED ON, NO FAULTS.
INTERMITTANT DISPLAY OF ECAM ENG 2 FIRE LOOP 'A' FAULT. REPLACED FIRE LOOP 4001WD2. REF AMM 26-12-17. OPS CHECKS GOOD REF. 26-12-00-710-00 1." REOPENED ON 03MAR12 FOR: MESSAGE RETURNED REPLACED LOOPS 4000WD1 & 3WD2, CHK'D OK ON ENG RUN.
FIRE LOOP 'A' FAULT DISPLAYED ON UPPER ECAM SCREEN. -ENG 2. SAMC TEXT: CREW COMPLIED WITH MEL, APPLIED DF STICKER: DEFERRED PER SAMC NO HARD FAULT. REPLACED FIRE LOOP 4001WD2 REF, AMM 26-12-17 OPS CHECKS GOOD. REF AMM26-12-00-710-001", REOPENED ON 03MAR12 FOR: MESSAGE RETURNED.
INTERMITTANT DISPLAY OF ECAM ENG2 FIRE LOOP 'A' FAULT. MEASURED RESISTANCE AT FDC 2 BTWN PIN J AND K, OHMS READ 1510, IS WITHIN LIMIT NEED MORE T-S TIME. NO HARD FAULT. VISUAL INSPECTION OF FIRE LOOPS CHECKS GOOD. REPLACED FIRE LOOP 4001WD2. OPS CHECKS GOOD.
AVIONICS VENT FAULT, FLIGHT DIVERTED. REPLACED AVIONICS EQUIPMENT VENTILATION COMPUTER AND TESTED SEVERAL TIMES WITH NORMAL INDICATION.
ELAC FAULT. REPLACED CAPT'S ROLL SIDE STICK TRANSDUCER 4CE1 REF AMM AND COMPLETED REJECTION FOLLOW-UP #RFU224068.
DURING REMOVAL OF AFT LAV MODULE, FOUND OVERHEAD TURNBUCKLE BRACKET SHEARED OFF. REPLACED OVERHEAD FITTING FOR AFT FWD LAV HOLD ROD.
CABIN EMERGENCY LIGHTS FAILED TEST. SHOWS EPSU BATTERY FWD LT. REPLACED EPSU 10WL BATTERY PACK, OPS NORMAL.
CYCLIC VERTICAL BUMPING-PITCHING FELT AT CRUISE. FLIGHT CONTROL SD SHOWED LT & RT AILERONS MOVING UP & DOWN IN UNISON WITH BUMPING. CONSULTED FMC ELAC 1-2 FAULT, IRREGULAR. TURNED OFF ELAC 1, AILERON MOVEMENT STOPPED. NO FURTHER OCCURRENCE OF BUMPING-PITCHING. PERFORM MM 27-14-00 P.601, AND 613.
AVIONICS SMOKE MSG APPEARED ON LANDING, PER CREW. REPLACED AVIONICS SMOKE DETECTOR 1WA PER MM. OPS NORMAL, MSG GONE.
FIRST OFFICER`S WINDSHIELD HEAT IS INOPERATIVE. REPLACED WHC NR 2 PER AMM. PERFORMED BITE TEST. CHECKED GOOD.
F/O SEAT HAS EXCESSIVE PLAY IN PEDESTAL. REPLACED F/O'S SEAT ASSY, OP'S CHECK GOOD.
OUTER PANE SHATTERED ON 2L SLIDING WINDOW. REMOVED 2L SLIDING WINDOW PER MM. INSTALLED NEW PANEL IN WINDOW FRAME. COMPLETED WINDOW INSTALLATION IAW MM.
LAVATORY WASTE DOOR BENT OR WON'T OPEN-CLOSE FWD CAB LT LAV. FORWARD LAV DOOR WHICH HOLDS THE FIRE EXTINGUISHER FELL OFF. DOOR FALLS OFF BECAUSE THE HOLDER AT THE BOTTOM IS DAMAGED AND DOOR WILL NOT STAY IN PLACE SECURELY. NO TIME ORD. SECURED WITH SAFETY WIRE. SAFTIED LOWER HINGE POINT. DOOR OPERATES NORMALLY.
PACK AIR HAS STRONG SMELL. PACK AIR HAS STRONG SMELL REPEAT ITEM. THE OZONE FILTER IS MOST LIKELY BAD. NONE IN STOCK ORD. REPLACED APU AND RAN PACKS TO BURN OUT SMELL.
LOST NOSE WHEEL STEERING ON LANDING. RED ECAM MESSAGE WITH AUDIBLE DINGS FOR L/G GEAR NOT DOWN LOCKED, WENT AWAY AFTER 10 SEC THEN GOT \NOSE WHEEL STEERING FAULT. NEITHER TILLER HAD INPUT. STEERING DISCONNECT WAS NO HELP. REPLACED 19GA IAW MM. REPLACED SELECTOR VALVE 41GA AND TEST GOOD. REPLACED SAFETY VALVE 2629 GM AND TEST GOOD.
LGCIU FAULT. ON APPCH L/G DID NOT EXTEND ON FIRST ATTEMPT. HAS HISTORY. ACFT IS UP ON JACKS T-S'ING. NEED TO REPLACE PRIORITY VALVE. PRIORITY VALVE REPLACED. ACCOMPLISHED SUCCESSFUL LEAK CHECK. CYCLED GEAR SEVERAL TIMES, OPS OK. NO MESSAGES. ALSO CK'D FREE FALL EXTENSION PRECAUTIONARY. REPLACED BSCU. R & R NLG OPENING 2630G M SAFETY VALVE. WHILE ACFT ON JACKS ALL DOORS AND GEAR OPERATED NORMALLY WITH HYD POWER. REPLACED GREEN SYS LANDING GEAR SAFETY VALVE. 49 GA. VALVE REQUIRES OPS CK. T/S FOUND FAULT WITH NR 1 LGCIU, AND NLG DOOR ACT. REPLACED NR 1 LGCIU, CYCLED GEAR 10 TIMES NO FAULTS, ACP'D MANUAL EXTENSION 6 TIMES, EACH TIME SYS OPERATED NORMAL. REPLACED NLG DOOR ACTUATING CYLINDER.
FA'S HAD A BURNING ODOR IN AFT GALLEY AREA. NOW AFT GALLEY CHILLER MALFUNCTION LIGHT IS ON. CHECKED COFFEEMAKERS, COFFEE WARMERS, FLORESCENT LIGHTS (BALLASTS) OPERATING OK. NO ODOR DETECTED. DEACTIVATED CHILLER C31 (FWD CHILLER FOR AFT GALLEY COMPLEX). RAN CHILLER FOR SEVERAL HRS DID NOT SMELL OR NOTICE ANYTHING BURNING. NFF.
STRONG ODOR IN COCKPIT, RTFL. REMOVED NR 2 ENG INLET CONE AND FAIRING. FOUND OIL IN THE EXTENSION SHAFT. REPLACED BLIND CAP AND SEAL. NEED TO ACP PACK BURN OUT AND REPLACEMENT OF RECIRC FILTER. ACCMP'D PACK BURNOUT. RAN ENGINES AT CLIMB POWER FOR ABOUT 15 MINS. NO OIL SMELL NOTED.
STRONG ELECTRIC BURNING ODOR DETECTED. REPLACED AVIONICS VENT EXT FAN 18HQ SYS. CFDS TEST CHECKED GOOD.
EMERGENCY LIGHT SWITCH COVER FELL OFF. SECURED SWITCH COVER.
GREEN SYSTEM HYD LOSS. REPLACED RIGHT MLG DOOR HYD SWIVEL ELBOW FITTINGS ON DOOR ACTUATOR. REPLACED NR 1 ENG DRIVEN PUMP, REPLACED HP FILTER, REPLACED CASE DRAIN FILTER AND GREEN SYS MAIN FILTER. LEAK AND OPS CKS OKAY.
EMERGENCY LIGHT TEST FAILED FAULTING EPSU BATTERY EMERGENCY RIGHT AND LEFT SIDE. REPLACED RT BATTERY, OPS CHECKS NORMAL REPLACED LT POWER SUPPLY, OPS CHECKS NORMAL.
EMERGENCY AISLE LIGHT AT SEAT 18C IS MISSING LENS. REPLACED SEAT LIGHT. OP CHECKS OKAY.
EPSU INT LOAD EMER R MESSAGE AT CIDS DURING OPERATIONAL TEST OF EMERGENCY CABIN LIGHTS AND SIGN CK. FOUND EPSU FAILED. REPLACED RT O/W EPSU, CHECKS GOOD.
ROW 21 EEL LIGHT INOP. SUPPLEMENTAL DATA UPDATE CAUSE, LAMP INOP. RELAMPED ASSY. OPS CHECKED NORMALLY.
APU FIRE BOTTLE DISCHARGE LIGHT IS ILLUMINATED BLOW OUT DISK IS INTACT LOW PRESSURE. FOUND APU FIRE TEST SWITCH INTERMITTENT STUCK, CAUSED APU BOTTLE DISCHARGE LIGHT PROBLEM. REPLACED ENG, APU FIRE PANEL (1WD) THEN OP-TEST NO FAULT.
AIRCRAFT O2 LOW. SUPPLEMENTAL DATA UPDATE CAUSE: LEAKING FILL PORT ON CREW O2 SERVICING PANEL. REPLACED FILL PORT AND SERVICED CREW O2 TO FULL, NO LEAKS NOTED.
OXYGEN HIGH PRESSURE INDICATION AMBER ON DOOR-OXY SYSTEM ECAM. SERVICED CREW O2 SYSTEM, NO REPEATS.
FLIGHT DIVERTED DUE TO LOUD SQUEAL IN COCKPIT. PRESSURIZED A/C TO 5.7 PSI NO LEAKS, NO SQUEAL DUPLICATED. REPLACED THE FWD LOWER DRAIN. NO REPEATS SINCE ORIGINAL WRITE UP.
CREW OXYGEN PRESSURE IS 1310 PSI ON ECAM. FOUND LEAKING B-NUT AT CAPT LOCATION. TIGHTENED B-NUT AND CHECKED ALL LOCATIONS IN COCKPIT. NO LEAKS NOTED. SERVICED 02 SYSTEM TO FULL.
CABIN EMERGENCY LIGHT CHECK FAILED. 10-19-07 FOUND LT FWD POWER SUPPLY FAULTY. REPLACED LT FWD POWER SUPPLY.
RTFL DUE TO ALL 3 ZONES INDICATING 100F. *S/D* FAULTY ZONE TEMP CONTROLLER. REPLACED ZONE TEMP (150) CONTROLLER. SHOP FINDINGS: NO FAULT FOUND.
LOWER FRONT SIDE OF CAPT SLIDING WINDOW HEAT INOP. WINDOW AREAS COLD AND FOGS UP LIMITING VISIBILITY. REPLACED NR 2 WINDOW
OVEN 105R11 WAS SMOKING IN FLT SHUT OFF POWER AND SMOKE STOPPED. REPLACED OVEN. OPS CHECKED GOOD.
EMERGENCY LIGHTS FAILED TEST. MULTIPLE FWD AND RIGHT SIDE LIGHTS INOPERATIVE. REPLACED BATTERIES FOR 10WL, 12WL, AND TESTED OK.
ENG 2 STALL. TRANSIENT STALL SHORT ECAM THEN ALL PARAMETERS NORMAL AT TOP OF DESCENT. NR 2 ENGINE S/N V10784 HAS ONE HPC 6TH STAGE BLADE MISSING 1/2 AMOUNT OF BLADE. ALL OTHER 6TH STAGE HPC BLADES HAVE NUMEROUS AMOUNTS OF DAMAGE AND MATERIAL LOSS. ENGINE FAILED COMPRESSOR STALL BORESCOPE. REMOVED ENGINE S/N V10784 FROM POSITION 2. INSTALLED ENGINE S/N V10171 AT POSITION 2. HPC DAMAGE CAUSED BY RELEASE OF LINER FOR THE R6 BLADES.
AFT PIT THRESHOLD TORQUE BOX UPPER CAP DAMAGED AT AFT END IB CORNER. MAJOR REPAIR. REPLACED THRESHOLD COVER AND INSPECTED.
L FWD EPSU FAILED ON EMERGENCY LIGHT TEST. REPLACED EPSU AND BATTERY.
DOOR 1R SLIDE FELL OUT OF DOOR.
THE AFT CARGO PIT THRESHOLD TORQUE BOX UPPER CAP AFT END INBOARD CORNER JUST FWD OF FR56 HAS A HOLE DRILLED THRU IT AND SEVERAL NICKS. MAJOR REPAIR: INTERIM REPAIR DOUBLER INSTALLED.
THE AFT CARGO PIT FLOOR CENTERLINE SUPPORT BEAM LOCATED JUST FWD OF FR56 HAS A HOLE DRILLED THRU THE UPPER CAP LEFT FLANGE. MAJOR REPAIR: INTERIM DOUBLER INSTALLED.
EEL LIGHTS ARE OUT AT 6ABC AND 17ABC. REPLACED BAD EEL LIGHTS.
FLIGHT DIVERTED DUE TO SMOKE ODOR IN THE CABIN. FOUND PIN 'A' OF CONNECTOR 400VCA SEVERELY BURNED, ALONG WITH RECEPTICLE. REPLACED IDG POWER CABLE AND PYLON POWER CABLE.
BURNING ELECTRICAL SMELL IN THE COCKPIT ACCOMPANIED BY AIRCRAFT VIBRATION. REPLACED AEVC BLOWER FAN, WHICH HAD EXPERIENCED BEARING FAILURE.
ABORTED TAKEOFF AT 90 KNOTS DUE TO AN AVIONICS VENT MESSAGE. THE AVIONIC EQUIPMENT COOLING COMPUTER WAS RESET AND THE AIRCRAFT FLEW FUTURE FLIGHTS WITH NO INCIDENCE.
FWD LT EMERGENCY POWER SUPPLY UNIT, EMERGENCY LIGHT TEST FAILS. REPLACED EMERGENCY POWER SUPPLY UNIT AND BATTERY, TESTS OK.