N483UA
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 | 2022-05-25 – 2022-05-25 | Operator named in NTSB report |
| UNITED AIRLINES, INC. (CALA) | Operator | 2022-05-25 – 2022-05-25 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
LVL 2 DUE TO HISTORY OF FWD GALLEY COFFEEMAKER (M11) INOP. REF. L/PS 8694821, 8683565, 86548211. ACP TSM 25-35-00-810-802-A AND CORRECT FAULTS. VERIFY CM M11 (7055MM) GRDS 9007VN & 9008VN REF. AWM'S 25-31-01, 25-31-02 ARE GOOD. UPDATE LOG WITH FINDINGS AND ALL ACTIONS TAKEN. CARRIED BY ELB CHRONIC LVL 2 FOUND PUSHED/BROKEN CONTACT ON M11 COFFEE MAKER TRAY. FOUND PUSHED/BROKEN CONTACT ON M11 COFFEE MAKER TRAY. UNLOCKED REMOVED/REPLACED M11 COFFEE MAKER RAIL ASSEMBLY AIPC 25-31-41-86K AND ACP TSM 25-35-00-810-802-A. INSTALLED COFFEE MAKER REF INSTALLATION OF THE COFFEE MAKER(S) REFERENCE: TASK 25-35-15-400-001-A. OPS CHECKED GOOD.
SHORT FINAL SMELLED SMOK E. AFTER LANDING ECAMS AIR PACK 1 OVERHEAT AND SMOKE DET FAULT. CREW DEBRIEF AND SMOKE. PER CP SMELL WAS DETECTED IN FLIGHT DECK WHICH THEY TOUGHT WAS SOMETHING BURNING IN AN OVEN. LT PACK SHUT DOWN AND FAULT APPEATED. NO SMELL DETECTED BY FAS IN FORWARD CABIN. SLIGHT SMELL DETECTED BY AFT FA FOR A FEW SECONDS WHICH MAY BE UNRELATED. PACK ONE INOP AND HAS HISTORY. MEL 2152Y ITEM REJECTED. NEEDS TSM FOR CABIN ODOR PERFORMED. ITEM LOCKED TO CONFIRM FINDINGS. PERFORMED CABIN TEMP CONTROLLER OPS CHECK AND CABIN PRESSURE CONTROLLER OPS CHECKS. NO FAULTS NOTED REF AMM 21-63-00 AND AMM 21-31-00 REPLACED PACK OUTLET TEMPERATURE SENSOR (13HH) AS PRECAUTIONARY REF AMM 21-61-15/401. REQUIRES OPS. CHECK PER AMM 21-61-15-400-001-A FOUND PACK 1 ACM HAS NO AIRFLOW AT PACK 1 RAM-AIR OUTLET (SEIZED). REMOVED ACM REF AMM 21-52-21-000-001-A. RAN PACKS FOR 1 HOUR COULD NOT DUPLICATE SMELL SMOKE. OPS CHECK GOOD NO LEAK FOUND REF AMM 21-52-21, CABIN TEMP TEST PASSED
NR 1 A/C PACK OVERHEAT WITH A BURNING ODOR OF WOOD OR PAPER, NO SMOKE VISABLE. ODOR DISSIPATED WITH PACKS 1 & 2 OFF. ACFT WAS NOT DEICED PRIOR TO DEPARTURE. PERFORMED IDENTIFICATION OF CABIN ODOR IAW TSM 05-50-00-810-831-A, VERIFIED SOURCE OF ODOR AS NR 1 A/C PACK. PERFORMED VISUAL CHECK OF PACK 1 & RAM AIR INLET, NO DEFECTS NOTED. OPS PACK 1, &PACK BEGAN TO OVERHEAT AGAIN. RAN PACK 2 OFF OF APU TO CLEAR ECS SYS OF ANY POSSIBLE RESIDUAL ODORS. NO DEFECTS NOTED. MEL 2152Y FOR PACK 1 INOP.
FUEL CAP MISSING. APROX 1.2 LBS. APROX 22 SQ INCH. INSTALLED NEW UNDERWING FUEL CAP ASSY IAW AMM 28-25-41-400-007-A, AND AMM 28-25-41-400-006-A. NEW FUEL CAP ASSY IS FLUSH WITH SKIN AND NO LEAKS NOTED FROM THE COUPLING. PLACARD REMOVED.
MISSING RIVET ON NO2 ENG INLET OUTSIDE 11 OCLOCK POS FACING AFT REQUEST CARRY FOR MISSING FASTNER. ONLY 1 MISSING AT THIS TIME. PER SRM DAMAGE IS ZONE K2 AND MAY BE CARRIED FOR 600FH 750FC OR 100 DAYS.
DOOR 2R OPEN ECAM. VERIFIED DOOR 2R CLOSES CORRECTLY, DEFERRED 2R OPEN INDICATION PER MEL 5270AV. REPLACED SENSOR 17WV2. SUGGEST TSM 52-13-00-810-804-A FOR FURTHER ISOLATING THE FAULT. CYCLED R2 DOOR MULTIPLE TIMES AND TEST DOOR INDICATION & WARNING SYSTEM IAW AMM 52-71-00 OPS CHECK GOOD NO FAULT FOUND.
ECAM DOOR R FWD EMER EXIT. CHECKED AND ADJUST FLAP COVER PER AMM 52-11-00. CHECKED AND ADJUST FLAP COVER PER AMM 52-11-00.
AVIATAR REPORTING L/G GEAR NOT DOWNLOCKED, L/G DOOR NOT CLOSED ECAM, CFDS MSG STEERING ELECTRO-HYD MODULE (6GC)- VARGAS TOMC FLAGGED SDR SEE LP 4237214
OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - EPSU BATTERY AFT L FAULT REMOVED AND REPLACED AFT LEFT BATTERY (13WL) PER REF AMM 33-51-38 OPS CHECK GOOD PARTS USED: 18-3351-3-0001,QTY :1
PDA 2 REF LOG 7799106 - RIGHT RETRACTABLE LANDING LIGHT BULB AND RETAINER MISSING (DEPARTED AIRCRAFT). PARTS MISSING ARE BULB, RETAINER & GASKET. REF. IPC 33-42-11-01A ITEMS 20, 30 & 40. RETERMINATED REF. TO AWM 33-42-00 AND ESPM 20-48-19. INSTALLED NEW LANDING LIGHT BULB, REF AMM 33-42-11. OPS CHECK GOOD. OK TO CONTINUE.
DENT FOUND ON EXTERNAL SURFACE OF FWD R1 LOWER AFT EDGE AREA. EVALUATION PERFORMED BY LHT EMP 5T1138 & 5P0052 AS RECORDED ON LTPR NR#5001292157-0010. INSIDE AREA AS PER SRM 52-10-00-283-002. DENT/CRACK DIMENSIONS DOUBLER REPAIR ON FWD DOOR R1 LOWER AFT EDGE AREA AS PER REPAIR REQUIRING REPETITIVE INSPECTION REQUIREMENTS AS PER REPAIR EMBODIMENT 60000FC (FH NOT RELEVANT). SUBSEQUENT AIRCRAFT CURRENT DATA: 67689:30FH/29621FC. WORK ARE: L=20MM, W=1OMM, D=1.57MM, CRACK L=5MM. PERFORMED SRM 52-10-00-300-003. THIS REPAIR IS CLASSIFIED AS MAJOR CAT B SRI 52-10-00-205-022. INSPECTION THRESHOLD FROM TIME OF ADL/ INSPECTIONS AT INTERVALS AND INSPECTION METHOD IS TBD. PERFORMED EXT AND INT DVI SIDE OF DENT ON EXTERNAL SURFACE OF FWD R1 LOWER AFT EDGE AREA, CRACK BEYOND ADL
PDA 2 RH LANDING LIGHT FOUND MISSING ON ARRIVAL FLT 0511-19 IN MSP UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V941601 PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC METER INITIATED FOR WITH VENDOR ID V941601 MAC RELATED WORK ORDER 000000003083672 AND PRTR HUBBARD, ARTHUR (V941601), COMPLIED WITH CDL TAPED UP WIRING AND REMAINING PORTIONS OF RH LANDING LIGHT ASSY PER 33G, STICKER APPLIED HUBBARD, ARTHUR (V941601), COMPLIED WITH CDL TAPED UP WIRING AND REMAINING PORTIONS OF RH LANDING LIGHT ASSY PER 33G, STICKER APPLIED DISPATCH DESK: 37 NAME: BE DATE: 19-AUG-23- DEFERRED DIRECTLY BY TOMC PARTS INFO ADDED LIGHT, RETRACTA OFF 31-3341-9-9001 7316 ON 0000 LIGHT, RETRACTA OFF 31-3341-9-9001 7316 ON 31-3341-9-9001 6909 R/R RH RETRACTABLE LANDING LIGHT. REF. AMM. 33-42-11. NO DEFECTS FOUND, OPS CHECK GOOD. PARTS USED: 31-3341-9-9001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1540087 SN OFF 7316
SMALL PIECE OF ACOUSTIC LINER DELAMINATING INEXHAUST SECTION OF ENG1 FLIGHT DECK LOTO BAG TO KEEP SHIMS WITH AIRCRAFT. PLACING 10 OF 14. REPLACEMENT/REPAIR ON DIP FOR 100 HRS PER ECRA 7811-01400 PAGE FOUND CNA RUB STRIP MISSING PN 740-1027-501 M&E: 18-7811-3-0006. DRILLED OUT RIVETS AND REMOVED SHIMS. PLACED AND LABELD SHIMS IN ADD EMP:U348947 ENGINE 1 CNA RUB BLOCK MISSING AT THE 11 OCLOCK POSITION.. TOMC-APPROVAL FROM SC1ELBYC COMMENT REQUIRES REPLACEMENT WITHIN 100 HRS REF ECRA 7811-01400 ADDING PHOTOTS AND M&L QC RECORDS UPDATE - AP QC REVIEWED. T/A : 100 FH...........AP/U366012 TOMCQC REV PERFORMED INSTALLED NEW RUB BLOCK IAW ECRA 7811-01400
*EMERGENCY* AT FL340 MASTER WARNINGW/ ECAM CABIN PR EXCESS CAB ALT APPEARED FELT CABIN PR CHANGE SEE LOG PAGE 9011036 FOR WORK ACCOMPLISHED. OPS CHECK GOOD PER LP 9011036 . RR OUTFLOW VALVE & PRESSURE CONTROLLER 1 REF. AMM.
*EMERGENCY*G RSVR OVHT DISPLAYED ON UPPER ECAM SCREEN. - HYD LOCKED FOR FIX UNLOCKING FOR UPDATE ON SDAC''S ITEM LOCKED FOR FERRY.TOMC SMITH REPLACED SDAC1 & SDAC2 PER AMM 31-55-34-400-001-A. PERFORMED GND PERFORMED MAINTENANCE TAXI AND ENGINE RUN AT 75% POWER FOR 15 PERFORMED TSM 29-11-00-810-802-A. PERFORMED CONTINUITY CHECK OF SCAN OF CENTRAL WARNING SYS PER AMM 31-50-00-710-001-A. NO MINUTES.. NO INDICATIONS OF G RSVR OVHT MSG. TEMP TRANSM SW 1381GR PIN A/G AND A/K. NO FAULT. MEASURED DC FAULTS. RESISTANCE BETWEEN PINS A/G AND A/K & A/E AND A/F OF TEMP TRANSM ROTABLE PARTS CHANGE WAS INDICATED - TT # 1133746 SN OFF 5495 SW 1381GR. RESISTANCE WITHIN ACCEPTABLE PARAMETERS. TT # 1193575 SN OFF 9886 UNIT, SYSTEM DA OFF 31-3150-9-0006 5495 ON 31-3150-9-0006 5714 UNIT, SYSTEM DA OFF 31-3150-9-0006 9886 ON 31-3150-9-0006 9084 UNLOCKING FOR UPDATE DUPLICATE WRITE UP, SEE LOG PAGES 8544982 AND 8556221 FOR WORK PERFORMED AND SAFETY VALVE REPLACEMENT AND OPS CHECK.
G RSVR OVHT DISPLAYED ON UPPER ECAM SCREEN. - HYD FAULT-OVER HEAT INDICATION EXTINGUISHED AFTER 6 MIN WITH SYSTEM SECURED. ACP TEM 29-11-00-810-802A UP TO UP THROUGH ITEM 3. COULD NOT DUPICATE OVERHEAT. NEED TO ACP ITEM 4D. R/R ENGINE PUMP FIRE -VALVE IAW AMM 29-11-52 PER TCM 29-11-00-810-802-A STEP 4 D, LEAK OPS CHECK SATISFIED PER 29-10-00-720-001-A. ADD EMP:291296 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1196223 SN OFF 9146 VALVE, SHUTOFF, OFF 31-2913-9-9006 9146 ON 31-2913-9-9006 2920
G RSVR OVHT DISPLAYED ON UPPER ECAM SCREEN. - HYD SEE PREVIOUS HISTORY CASE DRAIN FILTER (1084GM). UNLOCKED FOR UPDATE T/S REF TSM 29-11-00-810-802-A. AFTER RUNNING GREEN HYD SYSTEM, FOUND THE PTU EXTREMELY HOT. 40GA, 41GA AND 49GA WERE COOL TO THE TOUCH. SUSPECT PTU IS BYPASSING INTERNALLY. NEED TO REPLACE PTU, LP FILTER (1002GM) HP FILTER (1048GM) AND REMOVED AND REPLACED ABOVE MENTIONED FILTER ELEMENTS WITH NO 29-23-41-400-001-A. CONTAMINATION NOTED, REF AMM 29-11-41, 44 AND 45. REMOVED AND ROTABLE PARTS CHANGE WAS INDICATED - TT # 1837870 SN OFF 1585 REPLACED HYDRAULIC PTU AND PERFORMED ADJ/TEST, OPS CHECK GOOD WITH NO LEAKS NOTED OF PTU OR FILTERS, REF AMM UNIT, TRANSFER OFF 31-2920-9-0001 1585 ON 31-2920-9-0001 0620
PDA 2 UPON MX WALK-AROUND, FOUND RT RETRACTABLE LANDING LIGHT LENS/LAMP MISSING. REF LOG PAGE #7727304. GMM 02-30-95 REQUEST MEL 3340BB FOR RIGHT RETRACTABLE LANDING LIGHT INOP, REF PLACED ON MEL 3340BB PER TOMC. DDP COMPLIED WITH. L/P 7727304. DDP COMPLIED WITH. APPROVED REMOVED AND REPLACED RIGHT RETRACTABLE LANDING LIGHT REF AMM 33-42-11-000-001-A AND AMM 33-42-11-400-003-A. OPS CHECK GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1912000 SN OFF 7393 LIGHT, RETRACTA OFF 31-3341-9-9001 7393 ON 31-3341-9-9001 5977
SKIN VALVE FAULT DISPLAYED ON UPPER ECAM SCREEN. - V ENT REMOVED AND REPLACED SKIN AIR OUTFLOW VALVE OPS CHECKS GOOD REF AMM 21-26-53-400-001-A ROTABLE PARTS CHANGE WAS INDICATED - TT # 1939473 SN OFF 3533 VALVE, SKIN AIR OFF 31-2125-9-0001 3533 ON 31-2125-9-0001 2301
FLIGHT DECK, RH FR 4 UPPER ATTACHMENT, HOLE IN VERTICAL FRAME HA S CRACKE INDIATION AT ATTCHMENT, HOLE IN VERTICAL PRAME HAS CRAC K INDICATION AT JUNCTION OF VER. FRAME AND CORNER FITTINGS, CRAC AIMING PER HAECO LCQ 9298605/24605 GENERATED BY V892422 REPAIRED FLT DECK RH FR4 UPPER ATTACHMENT IAW UAL ECRA 5311-0253 3 ACP INITIAL INSP AT RH FR4 PER PART 2 OF THE LATEST REVISION O F ECRA 5311-02533 ON OR BEFORE THE A/C REACHES 37,026 TOTAL A/C FLT CYCLES. ACP REPEAT INSP AT INTERVALS NOT TO EXCEED 11,000 A/ C FLT CYCLES, THERE AFTER. ACP PERMANENT REPAIR AT RH FR4 ADD EMP:V079319 NSP BY V061671. RE THE A/C REACHES 53,326 TOTAL A/C FLT CYCLES BY MECH V079529 I PER PART 3 OF THE LATEST REVISION OF EC/RA 5311-02533 ON OR BEFO PLEASE NOTE LP''S 6144243 & 6144372 FOR DIP INFO LP REFERENCE FOR 6144372 IS NO LONGER GOOD . NEW LP REF IS 6144601.
FLIGHT DECK, RH FR 4 UPPER ATTACHMENT, HOLE IN VERTICAL FRAME HAS CRACKE INDIATION AT ATTCHMENT, HOLE IN VERTICAL PRAME HAS CRAC K INDICATION AT JUNCTION OF VER. FRAME AND CORNER FITTINGS, CRAC AIMING PER LCQ 9298605/24605. REPAIRED FLT DECK RH FR4 UPPER ATTACHMENT IAW UAL ECRA 5311-0253 3 ACP INITIAL INSP AT RH FR4 PER PART 2 OF THE LATEST REVISION O F ECRA 5311-02533 ON OR BEFORE THE A/C REACHES 37,026 TOTAL A/C FLT CYCLES. ACP REPEAT INSP AT INTERVALS NOT TO EXCEED 11,000 A/ C FLT CYCLES, THERE AFTER. ACP PERMANENT REPAIR AT RH FR4 ADD EMP:V079319 NSP BY V061671. RE THE A/C REACHES 53,326 TOTAL A/C FLT CYCLES PER PART 3 OF THE LATEST REVISION OF EC/RA 5311-02533 ON OR BEFO PLEASE NOTE LP''S 6144243 & 6144372 FOR DIP INFO LP REFERENCE FOR 6144372 IS NO LONGER GOOD . NEW LP REF IS 6144601.
FLIGHT DECK, RH FR 4 UPPER ATTACHMENT, HOLE IN VERTICAL FRAME HA S CRACKE INDIATION AT ATTCHMENT, HOLE IN VERTICAL PRAME HAS CRAC K INDICATION AT JUNCTION OF VER. FRAME AND CORNER FITTINGS, CRAC AIMING PER HAECO LCQ 9298605/24605 GENERATED BY V892422 REPAIRED FLT DECK RH FR4 UPPER ATTACHMENT IAW UAL ECRA 5311-0253 3 ACP INITIAL INSP AT RH FR4 PER PART 2 OF THE LATEST REVISION O F ECRA 5311-02533 ON OR BEFORE THE A/C REACHES 37,026 TOTAL A/C FLT CYCLES. ACP REPEAT INSP AT INTERVALS NOT TO EXCEED 11,000 A/ C FLT CYCLES, THERE AFTER. ACP PERMANENT REPAIR AT RH FR4 ADD EMP:V079319 NSP BY V061671. RE THE A/C REACHES 53,326 TOTAL A/C FLT CYCLES BY MECH V079529 I PER PART 3 OF THE LATEST REVISION OF EC/RA 5311-02533 ON OR BEFO PLEASE NOTE LP''S 6144243 & 6144372 FOR DIP INFO LP REFERENCE FOR 6144372 IS NO LONGER GOOD . NEW LP REF IS 6144601.
L2 DOORSILL CORRODED UNDER GIRT BAR PLATES AT FR66 AND FR68. PER HAECO NR 9298466/24466. GENERATED BY V079529 REMOVED AND REPLACED L2 DOOR SILL AT FR66-FR68 IAW UAL A320 SRM 51-72-11-911-001 BY MECH V914232
AFT INTERNAL FUSELAGE STR31R HAS CORROSION AT FR65, JUST BELOW O UTFLOW VALVE. PER HAECO NR 9298127/24127. REMOVED AND REPLACED STINGER 3/R AT FR64-FR67 IAW A320 SRM 51-72 -11-911-001.
AFT BILGE AREA BETWEEN FR63 AND FR64 STGR42L HAS CORROSION ON ST RG PER HAECO LCQ NON-ROUTINE 24719/9298719 PER MECH V061640 REMOVED AND REPLACED STR42L FR 60-64 IAW A320 SRM 51-42-11 PARA 2E&F & SRM 51-72-11 CAT A REPAIR PER MECH V061640
AFT CARGO COMPARTMENT STR41R WITH FR59 HAS CORROSION. PER HAECO NON-ROUTINE 24667/9298667 BY MECH V061640 REMOVED AND REPLACED STR 41R FR 58-64 IAW A320 SRM 51-42-11 PARA 2E&F. CAT A REPAIR REMOVED DOT E555
AFT CARGO BILGE AREA BETWEEN FR C63 AND C64 STR 41L REMOVED DOT HN-24. PER MECH V061640 REMOVED AND REPLACED STRINGER 41L FR60-694 IAW A320 SRM 51-42-11 PARA LE&F AND SRM 51-72-11 CAT A REPAIR REMOVED DOT HN-29
AFT CARGO BILGE AREA FR C63 STR 41R TO STR 42R HAS CORROSION AND BARE METAL DOT HN-23 PE HAECO NON ROUTINE 24672/9298672 REMOVED AND REPLACED STR 42R IAW A320 SRM 51-42-11 PARA 2E & F, STRINGER 41R WAS REPLACED ON N/R 24667 FR60-64 & SRM 51-72-11. C AT A REPAIR REMOVED DOT HN-23
AFT CABIN AT FR68 DOOR SILL IS CORRODED AT SEVERAL AREAS AND HAS ENLARGED FASTENER HOLE PER HAECO LCQ NON ROUTINE. REMOVED & REPLACED R2 DOOR SILL (FR66-FR68) IAW A320 SRM 51-72-1 1-911-001.
STALL DISPLAYED ON UPPER ECAM SCREEN DURING CLIMB OR CRUISE ACCELERATION. ENGINE NOT SHUTDOWN. ENGINE 2 APPROXIMATELY 3000 FT ON DEPT FELT MINOR THRUST REDUCTION FOLLOWED BY ENG 2 STALL ECAM, ECAM CLEARED AND TH REF TO TSM TASK:71-00-00-810-809-A SURGE OR STALL ON ENGINE 2 -753242 VSV MECH/BLD VLV/LPC2 ON CFDS ALONG WITH 771100 ENGINE 2 STALL FADEC 2 A OR B. AIDES STORED REPORTS DOES NOT HAVE VALID DATA NORMAL W/NO EXCEEDANCES. CFDS HAS NO SCHEDULED MAINT REPORT FOR (TEXT CONT. FROM L/P 5717936) NORMAL IN A FEW SECONDS. ENGINE PARAMETERS FOR MOST OF THE STORED REPORTS EXCEPT "A320 ENGINE GAS PATH ADV REPORT (06)" FROM JAN09 UTC 1409444. TROUBLESHOOTING DATA IN MOMENTARY LOSS OF THRUST AND THEN RECOVERY. CELL 06 RECORDED FAULT PBPSTL. PILOT REPORTED SLIGHT AND PER TSM 71-00-00-810-809-A PAR 4D. FULL TROUBLESHOOTING. NO FOREIGN MATERIAL FOUND, BORESCOPE INSPECTION NOT REQUIRED. BURNER SENSOR TUBE CHECKED GOOD, AND PURGED. FUNCTIONAL CHK OF HPC 7TH STAGE 7A AND 7B SOLENOIDS, SOLENOIDS CHECK GOOD. NEED TO CONTINUE WITH CHECK OF 7TH STAGE BLEED VALVES 7A & 7B, PER AMM FROM 4D 6 ON PAGE 7, TO COMPLETION. 75-32-52-700-011-A. THEN COMPLETION OF TSM 71-00-00-810-809-A ACCOMPLISHED STEPS 5, 6, 7, REF AMM 71-00-00-810-809-A. VSV RIG INSTALLED VSV LINKAGE ON SEPARATE LP. CHECKS GOOD, BLEED VALVES AND LINES GOOD, IP CHECK VALVE GOOD. UNLOCKING FOR MX TO SIGN OFF. ACCOMPLISHED TEST 11 HIGH POWER ASSURANCE. TEST PASSED NR 2 ENGINE REACHED TARGET.
DURING SERVICE CHECK WALK AROUND FOUND DENT ON RIGHT WING INBOARD FLAP 8 INCH FROM WING ROOT. DENT MESURE L= 7 INCH W= 1.25 D= 0.113 PLACING DAMAGE ON A DIP IN REF TO SRM 57-52-00-283-027 FIGURE 1 COLUMN 3 . APPLIED HIGH SPEED TAPE TO THE DAMAGED AREA TO BE REINSPECTED WEEKLY AND A PERMANET REPAIR WITHIN 50 FLIGHT CYCLES REF SRM 57-52-00-283-061, DENT IS LOCATED IN ZONE 2. OK TO DIP DENT PER SRMS 57-52-00-283-021 AND 57-52-00-283-027 FIG 1. INTERIM SPEED TAPE REPAIR MUST BE INSPECTED WEEKLY AND PERMANENT REPAIR ACCOMPLISHED WITHIN 50 FLIGHT CYCLES. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEVED REF LP 4336588 FOR REQUIRED QC RE-INSPECTION PER GMM 06-35-05 QC REVIEWED RECORDS UPDATE TAPE INTACT, DIP REMAINS. RECIEVED AVO 8357A TO ACCOMPLISH REPAIR. FOUND NO ADDITIONAL DAM DAMAGED REF SRM 57-52-00-300-O14 STEP 2A1E. AMT 181277 AGE TO AUXILAIRY SPAR CAP REF AVO OPTION 1 ITEM 1. CUT OUT SKIN CRACK FOUND. ACP''D HFEC AFTER AREA ALREADY CUT OUT. REF NTM 6/51-10-08. NO POTTED HONEYCOMB AREA WITH HIYSOL REF SRM 57-52-00-300-014 ADD EMP:U181277 RECORDS UPDATE MHU359555 BONDED ON REPAIR PER AVO8357.PO# FOR MATERIAL 6342066317 M&E#40- 0604-3-1561. NEEDS FINISH RESTORED. ACP''D INSPECTION ITEM OF PO# VERIFICATION. REPAIRED FLAP PANEL IAW ECRA 5752-01838 VERIFIED RII ITEMS FOR RH IB FLAP TRAILING EDGE REPAIR. REF GMM 09-25-05 TOMCQC REV PERFORMED RIR: 7 DAYS T/A: 50 FC...BK/245861
VENT SKIN VALVE FAULT RESET CBS CFDS TEST PASSED OPS CK MM 21-26-00-710-001 A
EEL FWD LEFT BATTERY FAULT. REPLACED FWD LEFT EEL BATTERY IAW AMM 33-51-38.
FLIGHT ATTENDANTS REPORT SCORCHED PLASTIC SMELL COMING FROM AFT GALLEY OR LAVS. REPLACED WASTE VACUUM GENERATOR PER AMM 38-31-64. OPS CHECKS GOOD, NO BURNING SMELL NOTED.
OPS CHECK OF THE CABIN EMERGENCY LIGHT BATTERY CAPACITY FAILED. REPLACED THE BATTERY PACK, AND TESTED OK.
EXIT SIGN REMAINS ILLUMINATED FOR ENTIRE TIME IN EXIT ROW RESET CIDS. PERFORMED CIDS SYSTEM TEST. NO FAULTS. NO PREVIOUS L EG FAULTS. ACCOMPLISHED OPERATIONAL TEST OF THE EMERGENCY LIGHTS . PER AMM 33-51-00-710-001-A. SYSTEM CHECK NORMAL. OPERATED EMERGENCY LIGHTS FROM FLIGHT DECK AND AFT CABIN. ALL LIGHTS TURN ON AND OFF NORMALLY.
LOW SPEED ABORTED TAKEOFF (70KTS) DUE TO B HYD SYS LOW QTY ECAM. FOUND NR 3 SPOILER ACT LEAKING. R&R AND TESTED PER AMM.
ON FWD FAP HAD MESSAGE FOR EPSU FAIL FWD. ON BATTERY POWER SUPPLY HAD MESSAGE UNIT FAILED. REMOVED AND REPLACED FWD L1 DOOR EMERGENCY LIGHT POWER SUPPLY.
AFTER TAKEOFF CREW LOST BOTH ENG BLEEDS & CROSS BLEED VLV, STARTED APU FOR BLEED, DIVERTED. ACCOMPLISHED BMC BITE CHECKS OK. ACCOMPLISH FAULT CHECK OF CROSS BLEED VLV POSITION CONTROL OK. REPLACED PRESS REGULATOR VLV. OPERATIONS CHECKED GOOD.
RAMP REPORTS BURNING WIRING SMELL IN FWD CARGO BIN. PERFORMED GENERAL VISUAL INSPECTION OF FWD CARGO COMPARTMENT. OPERATED NESTING SYS FULL TRAVEL NO DEFECTS NOTED. NO BURNING SMELL DETECTED.
RIGHT EMER LIGHTS TEST FAIL WITH MSG EPSU EMER RT. REPLACED EPSU & BATTERY AT RT OVERWING DOOR IAW AMM 33-51-38. OPERATIONS CHECKED OK.
HISSING NOISE AT EMER EXIT PLUG DOOR AT 20A. INSPECTED & CLEANED FWD LT HATCH SEAL & SEAL MATING SURFACE & OUTSIDE HANDLE GASKET IAW MT 53-004 & MM 52-21-11-000-001-A. NO SEAL OR GASKET DAMAGE NOTED.
RIGHT OVERWING SLIDE DEPLOYED. REPLACED RT OVERWING SLIDE IAW AMM 25-62-42-400-001-A. REPLACED RT OVERWING INFLATION RESERVOIR IAW AMM 25-62-46-400-001-A. INSTALLED EMER EXIT HATCH IAW AMM 52-21-11-400-001-A.
RUDDER PN 5547100001400 SN TS-1274 WAS FOUND TO HAVE WATER INGRESS & DISBOND DAMAGE. ACCOMPLISHED ALL REPAIRS IAW ECRA 5541-01046 REV A. WORK ACCOMPLISHED ON WU'S 49575, 49576, 49577, 49578, 49579 & 49580. CURRENT PTT 41377 PTC 17871. REPAIR TO RUDDER SIDE SHELL HAS BEEN APPROVED. ACCOMPLISHED CP INITIAL INSPECTION ON OR BEFORE 28MAY2020 REPEAT INSPECTION AT INTERVALS NOT TO EXCEED 6 YEARS THEREAFTER.
FRAME 60 - FRAME 70 CIRCUMFERENTIAL SUPPORT FOUND CORRODED. R & R SUPPORT FRAME D5347112320200 IAW A320 51-72-11.
MAIN CABIN R2 LOWER SILL HAS CORROSION ON FRAME 68. CORROSION FOUND BEYOND OEM LIMITS. FABRICATED & INSTALLED REPAIR PLATE IAW SRM53-41-14 FIG 101 & 201. THIS REPAIR WAS CIR'D & ACCEPTED.
AFT CARGO DOOR AFT ACTUATOR ATTACH FITTING IS CHAFED. BLENDED CHAFED AREA. ORIGINAL THICKNESS WAS 0.200 & REMAINING THICKNESS IS 0.198. MATERIAL LOSS IS 0.002. THIS REPAIR REQUIRES SRI INSP IAW SRI 52-30-00-1-005-00 TABLE 105. FIRST INSPECTION IS DUE AT 60000 FC AFTER REPAIR EMBODIMENT. CURRENT PTT IS 41377 & PTC IS 17871.
LOUD HUMMING SOUND AROUND ROW 22. INSPECTED SEALS ON BOTH LT & RT SIDE, NO DEFECTS FOUND. TAPED FAIRINGS 191DT & 192DT. CREW ON FLIGHT 330 7 REPORTED NO HUMMING.
8 INCH CRACK IN NR 2 ENG EXHAUST CONE ALONG A PREVIOUS WELD. REPLACED EXHAUST CONE.
DENT IN LT SIDE FUSELAGE ALONG CIRCUMFERENTIAL JUST FWD OF WATER SERVICE PANEL AT EYE LEVEL. DENT LOCATED AT FRAME 28L & JUST BELOW STRINGER 34L. DENT IS SMOOTH NO CREASES, APPROXIMATELY 3 IN X 4 IN & .007 DEEP. PERFORMED EXT DVI, NO CRACKS NOTED. DENT IS ALLOWABLE IAW SRM 53-21-11 DIAGRAM 103.
BUILDING HISTORY OF "HOT AIR FAULT" ECAM WARNINGS. RECENT LEG FAULTED "NO ZONE CTL DATA" AT FLT PHASE 4. REPLACE ZONE CONTROLLER, PCN 565-9207, IAW AMM 21-63-34.
NR 1 ENG COWL IS NOT FLUSH JUST AHEAD OF FWD COWL LATCH UNDERSIDE. ADJUSTED COWL & FOUND COWL WITHIN LIMITS.
ELEVATOR SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN, - F -CTL. GOT ECAM DURING FLT CONT CHECK. FLT ATTENDANT REPORTED LOUD CLUNK FROM TAIL COINCIDENTAL W-ECAM PROG TEXT: - ITEM ROLLED FORWARD. REPLACED LT OTBD BLUE ELEVATOR SERVO IAW MM, OPERATIONS CHECKED GOOD.
ELEV SERVO FAULT DISPLAYED, REPEAT. CFDS FAULTING LT G ELEV SERVO VALVE 34CE1. REPLACED LT ELEV SERVO CONTROL VALVE IAW AMMS 27-34-51-000-008-A & 27-34-51-400-003-A. OPERATIONS CHECKED NORMAL ALL MODES NO MESSAGES.
F-CTL ELEV SERVO FAULT. REPLACED NR 2 ELAC IAW MM 27-93-00-710-001-A & TESTED OK. ACCOMPLISHED CAT 3 AUTOLAND TEST IAW MM 22-97-00, CHECKED OKAY.
CUSHION SEAL ONE EACH BOLT SHEARED, RT WING, OTBD FLAP IAW MT-57-008 IPC 57-53-21-05 ITEM 150, SRM 57-53-00 FIG 220 0R 224, IAW CDL 27L REPLACED NEW SCREW
CUSHION SEAL ONE EACH BOLT SHEARED, LT WING OTBD FLAP IAW MT-57-008 IPC57-53-21-05 ITEM 150, SRM57-53-00 FIG 220 OR 224, REPLACED NEW SCREW.
CAPTAINS LT SCREEN IS BLANK. SWAPPED CAPTAIN`S DISPLAY UNIT WITH LOWER ECAM DISPLAY UNIT. CW DDP. ** DL1621 CREATED TO MONITOR. REPLACED LOWER ECAM DISPLAY UNIT, CHECKED GOOD.
ECAM CAUTION MESSAGE, Y RSVR LO LVL MESSAGE INOPERATIVE, HYDRAULIC. FOUND HYDRAULIC LEAK FROM AUTO BRAKE SELECTOR VALVE CENTER B-UNION PIPE. REPLACED O-RING, SERVICED HYDRAULIC TO FULL. LEAK & OPERATIONS CHECKED OK. ECAM MESSAGE CLEARED.
DURING PREFLIGHT, FOUND FUEL DRIP FROM BOTTOM NR 2 NACELLE. FOUND PACKINGS AND HOUSING WORN. R & R IAW AMM 24-21-42-400- 010B13 AND AMM 73-12-41-400-010-B13. RAN ENGINE FOR THREE MINUTES AND OPS AND LEAKS CHECKED GOOD.
SEATS AT ROW 37 ABC, LOOSE. SECURED SEATS AT ROW 37 ABC OK TO CONTINUE.
LEFT MLG MISSING PLASTIC COVER WHERE L-G MEETS AC. REPLACED RUBBER CUP. OK TO CONTINUE.
EMERGENCY LIGHT SYS AFT FAILED TEST. REPLACED BATTERY IAW AMM, OPS CHECKED OK.
FIRST OFFICER SEAT MANUAL UNLATCH STICKS AND BINDS. REPLACED FIRST OFFICER SEAT, OPS GOOD.
CABIN FIRE EXTINGISHER MISSING SEAL. REPLACED FIRE EXTINGISHER.
CABIN EMERGENCY LIGHTING CHECK FAIL. REF A320 3SV STEP 2. CYCLED AND RESET CIDS POWER. CABIN EMERGENCY LIGHT TEST OKAY.
FUEL IMBALANCE OF 1200 LBS. REPLACED FQIC PER MM 28-42-34-400-001-A OPS CHECKED GOOD PER 28-46-00-740-001-A
WHEN TESTING EMERGENCY LIGHTING AFT LT BAT FAULTED. REPLACED POWER SUPPLY AND BATTERY PACK.
DURING VACUUM LOSS INSPECTION (DONE BY AIRBUS) IT WAS NOT POSSIBLE TO APPLY VACUUM TO ONE OF THE INSP HOLES. CHECKS ACP ON PTT SEQUENCE 7962015. REF CF9015 REMOVED RUDDER. NEED TO INSTALL NEW RUDDER. INSTALLED HINGE BOLTS ONLY. BOLTS NOT TORQUED. ACP'D VACUUM CHECK PER AVO 1158 OF NEWLY DRILLED HOLES PER AVO 1158 FIGURE 4. BOTH LWR HOLES FAILED VACUUM LOSS TEST. UPR TWO HOLES OK. ALSO ACP'D THEROMOGRAPHY TEST PER NTM51-10-25, NO WATER FOUND. REPLACED WITH SERVICEABLE RUDDER ASSY. (OFF P/N D544-71025-00, SN 0959). (ON P/N MR55412-3). INSTALLATION TO BE COMPLETED ON SMC4. COMPLETED INSTALLATION OF RUDDER UP TO MM. NEED TO ACCOMPLISH RIG AND OP CHECKS.
FOUND BURNED & BROKEN WIRES 2825-5805 & 2825-5813 IN RT MAIN WHEEL WELL. REPLACED WIRE W2825-5805-20 FROM 10QU-A TO 6793VN. TERMINATED & SECURED WIRE W2825-5813-22 FROM 10QU-A UP TO PRESSURE SEAL 7502VP IN RT WW CEILING REF WD28-25-04 AND HOOK-UP LIST PG 1417. SPLICED W2825-5813-22 WITH ENVIRONMENTAL SPLICE AT PRESSURE SEAL AREA. PERFORMED OPS CHECK IAW MM, FUNCTIONED NORMALLY.
EMERGENCY EXIT LIGHT BULB ON UPPER CONSOLE BURNED OUT. "OFF" LIGHTS WORK DURING LAMP TEST, BUT DO NOT ILLUMINATE WHEN SWITCH IS PLACED "OFF". CHECKED FUSE "F" FOR OPEN CIRCUIT. FOUND BOARD 7LP CAUSING ISSUE. LIGHT WORKS OFF PIN 44 REF ASM. FOUND THAT BOARD 5LP DOES NOT USE PIN 44. SWAPPED BOARDS AND LIGHT NOW WORKS NORMAL.
STEERING INOP WHEN ACFT GOT TO GATE. CYCLED ANTI-SKID NOSE WHEEL STEERING SWITCH SEVERAL TIMES AND STEERING CONTROL RETURNED. REPLACED NOSE WHEEL STEERING ELECTICAL BOX. NO FURTHER ISSUES.
CREW REPORTS A POSSIBLE RUBBER BURNING ODOR OR ELECTRICAL BURNING ODOR IN THE VICINITY OF ROW 24ABC. A NON-REV CREWMAN CHECKED IT OUT AND FOUND THE SMELL HAD DISSIPATED. NO FURTHER PROBLEMS FOUND. SAMC ADVISES THAT UPON ARRIVAL CHECK THE CABIN EMERGENCY EXIT LIGHTS AND THE CABIN LIGHTING IN THE VICINITY. ALSO OPEN THE PASSENGER SERVICE UNITS AND CHECK THE OXYGEN GENERATOR CONDITION AND THE LIGHTING BALLASTS ABOVE THE SEAT ROW. CHECKED THE AREA AT 24ABC INCLUDING THE AFT CARGO PIT. FOR EVIDENCE OF SMOKE OR BURNING SMELL NO DAMAGE NOTED, THE CABIN LIGHTS AND PASSENGER SERVICE UNIT CHECKED GOOD. ALL SYSTEMS WERE NORMAL.
FOUND EPSU BATTERY EMERGENCY R DISPLAYED ON EMERGENCY LIGHT CHECK. FOUND POWER SUPPLY IN FWD CABIN NOT TESTING CORRECTLY. REPLACED IAW MM. ALSO REPLACED BATTERY. OPS CHECKED NORMAL.
FWD ENTRY AREA LIGHTS FLICKER AND CHANGE SETTINGS BY THEMSELVES ACCOMPANIED BY SLIGHT BURNING ODOR AS REPORTED BY F/A. OPENED FWD ENTRY AND FWD GALLEY CEILING PANELS, INSPECTED WIRES AND BALLASTS: NO EVIDENCE OF ARCING OR WHERE SMOKE ODOR ORIGINATED. PULLED- COLLARED CABIN ENTRY LIGHTS CB PRECAUTIONARY. RELAMPED ENTRY LIGHT. ACP OP CKS NORMAL. CYC CIDS SYS.
RED EMERGENCY ESCAPE LIGHT INOP AT SEAT 12C MORE TIME NEEDED TO TROUBLESHOOT. RELAMP NO HELP. ALL OTHER ESCAPE LIGHTS OPERATE NORMAL IN COMPLIANCE WITH MEL 3350C. FOUND WIRES PULLED OUT OF CONNECTOR AT SEAT LIGHT, REPLACED CONNECTOR AND SECURED, OPS CK OF EMERGENCY LIGHTING SYS NORMAL.
EMERGENCY EXIT LIGHTS TEST FAILS EPSU AFT L INTERNAL FAULT. FOUND SHORT UNDER 2ND FROM LAST SEAT ABC, ACCOMPLISHED ENVIRONMENTAL SPLICE, USED POWER SUPPLY FROM ABOVE DOOR 1L TO OP CK. ACCESS PANEL ABOVE 1L REMOVED AND STOWED BEHIND PONY WALL AT 1AB, BAD POWER SUPPLY LOCATED ABOVE 1L DOOR. REPLACED POWER SUPPLY. OP CHECKS ARE NORMAL.
WHEN THE RAMP PRESSED THE LIGHT TEST BUTTON ON THE 108VU, SMOKE STARTED POURING OUT OF THE BACK OF THE PANEL. FOUND ADIRU AND AVNCS VENT LIGHT BODY SHORTED. NEEDS 25HQ BODY AND CAP ASSY TO FIX. NEEDS 25HQ INDICATOR LIGHT BODY AND INDICATOR CAP ASSY TO FIX. REPLACED 25HQ, TEST OKAY.
DOOR 2L SLIDE BOTTLE PRESSURE LOW. SERVICED BOTTLE.
CIDS SYS TEST FAILED DUE TO DOOR 1L SLIDE REPLACEMENT AND RE-INSTALLATION. BATTERY FAULT ON EPSU AT DOOR 1L. REPLACED BATTERY, NO HELP. SWAPPED EPSU FROM CENTER RIGHT AND PROBLEM FOLLOWED. SUSPECT BAD PART FROM STOCK. REPLACED EPSU BACK AT CENTER RIGHT. REPLACED EPSU WITH ANOTHER UNIT. PASSED TEST.
AFT PIT SMOKE DETECTOR DAMAGED. R&R FWD DETECTOR.
LAV SMOKE DETECTOR INOP. REPLACED LAV 'D' SMOKE DETECTOR. AC OK FOR SERVICE.
DOORS 2L & 2R FAILED ARMING SLIDE FORCE TESTS. DIRTY/UNLUBED GIRT FITTING INTERFERENCE. CLEANED AND LUBED GIRT BAR FITTING AND BAR. OPS CHECKED NORMALLY.
CREW COMMENTS: HEARD A BANG, GOT ECAM ENG 2 STALL. NO ABNORMAL ENG INDICATIONS, ENG RUNNING NORMAL SINCE. 11-01-07 FOUND NR 2 ENGINE STALL DUE TO DAMAGED HPC STAGE 6 BLADE- FOUND TORN AND BEYOND DAMAGE TOLERANCES. REPLACED NR 2 ENGINE DUE TO DAMGE OF HPC STG 6 BLADE.
ELAC 2 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN, F-CTL. *S/D* SEC NR 2 AND RELAY 36CE3 FAULT. REPLACED SEC NR 2 AND RELAY 36CE3, OPS CHECK GOOD.
SEAT 1C EEL LIGHT INOP. FOUND 2 WIRES DETACHED UNDER SEAT RAIL. [SUP 06-06-07] REPAIRED EEL LIGHT WIRES UNDER SEAT 1C.
CREW REPORTS, DURING ENG 1 START NO N2 ROTATION WITH GOOD START VALVE OPEN INDICATION. RAMP REPORTED SPARKS FROM STARTER AREA. [06-26-07] REPLACED THE STARTER AND START VALVE. PRESENCE OF SPARKS INDICATES PROBABLE INTERNAL BEARING FAILURE RESULTING IN TURBINE CONTACT WITH HOUSING.
FOUND EMERGENCY EXIT PATHWAY LIGHTS INOP AT SEATS 1C, 8C, & 15C. REPAIRED WIRING AND REPLACED LIGHTS.
FOUND BURNED FEEDER WIRE. TERMINAL ON R3782 AND/OR HARNESS ON R4388. REPLACED APU GENERATOR REF MM 24-23-51.
RECEIVED ECAM AND A FIRE ALARM FOR ENG NR 1. SHUT DOWN ENGINE. NR 1 ENGINE PRESSURE REGULATING VALVE FOR LEAKAGE AROUND SPINDLE SHAFT.
EMERGENCY EXIT AISLE LIGHT INOP AT SEAT 1C. REPLACED BATTERY AND CHARGER 110WL1.