N705UW
Registered owner: BANK OF UTAH TRUSTEE, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO PIT DUE TO THE FLIGHT CREW REPORTING THAT DURING CRUISE LOST YELLOW HYDRAULIC SYSTEM FLUID ALONG WITH A HYDRAULIC YELLOW LOW LEVEL ECAM. THE FLIGHT CREW ACCOMPLISHED THE CHECK LIST AND LANDED SAFELY AT PIT WHERE THE AIRCRAFT TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE FOUND UNION ON PTU YELLOW SYSTEM MANIFOLD LOOSE AND LEAKING. REPLACED PACKING ON UNION AND REINSTALLED PER AMM 29-13-15. A SATISFACTORY LEACK / OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ISSUES NOTED.
AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTS 1R SLIDE HANDLE POPS UP. MAINTENANCE RE-FOLDED SLIDE GIRT IN CORRECT POSITION PER AMM 25-62-44. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS NOT GROUNDED: CEILING EMERGENCY LIGHT AT ROW 12 INOP RELAMP NO HELP. MAINTENANCE RE-CONNECTED LIGHT ASSEMBLY PER AMM 33-50-00
AIRCRAFT WAS GROUNDED: STRONG ODOR IN THE ENTIRE CABIN. MAINTENANCE FOUND APU OIL COOLING FAN LEAKING. REPLACED O-RING IAW AMM 49-52-51. LEAK CHECK GOOD.
AIRCRAFT WAS NOT GROUNDED: REF MIC# 7309412. DURING THE INSTALLATION OF THE R1 EMERGENCY SLIDE PACK IAW WORKCARD # 26L00025011 MAINTENANCE FOUND GIRT BAR R/H SIDE WILL NOT STAY SEATED. MAINTENANCE REPLACED R1 DOOR AFT GIRT BAR FLOOR FITTING IAW A/C MM52-13- 31.
AIRCRAFT WAS GROUNDED: CLIMBING THROUGH 35,000', A LOUD HUMMING SQUEAL WAS HEARD FROM DOOR 1R. DECESION MADE TO DIVERT TO LAX. NO EMERGENCY DECLARED AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE EXTRUDER SEAL PER AMM 52-11-18 AND PERFORMED LEAK CHECK PER AMM 05-53-78-1-A01.
AIRCRAFT IN BASE MAINTENANCE: R1 DOOR SLIDE NEEDS TO BE REPLACED BECAUSE IT UNWRAPPED. MAINTENANCE REMOVED AND REPLACED SLIDE ON ROUTINE JOB CARD 26L00025011.
AIRCRAFT IN BASE MAINTENANCE: LH AFT PASSENGER DOOR OPEN ASSIST PRESSURE LOW. MAINTENANCE SERVICED L2 DOOR DAMPER/EMERGENCY OPERATION CYLINDER PER AMM 52-10-00-614-001-A.
AIRCRAFT IN BASE MAINTENANCE: CRACK ON FRAME 68 AT STRG 22 RIGHT. MAINTENANCE CUT OUT DAMAGE AND WEBS AT STR21R TO STR22R AND INSTALLED NESTED REINFORCING REPAIR IAW EA 365506 DRAWING R5342228 & AIRBUS TD/80566481/023/2021#A.
AIRCRAFT IN BASE MAINTENANCE: L/H AFT PAX DOOR TOP ROLLER ON AIR FRAME STIFF. MAINTENANCE INSTALLED ALL NEW RELATED HARDWARE IPC 53-46-04-80B FOR L2 DOOR UPPER HOOK, ROLLER, PER AMM 20-21-11 PAGEBLOCK 0201.
AIRCRAFT WAS NOT GROUNDED: 11C FLOOR EMERGENCY ESCAPE MARKER LIGHT INOP. MAITNENANCE RESECURED 11ABC LIGHTING CANNON PLUG IAW CMM 25-22-52. OPS CHECKGOOD.
AIRCRAFT WAS NOT GROUNDED: CRACK ON INNER PANE OF WINDSHIELD. CAPTAIN'S FORWARD FACING WINDSHIELD. AS A PRECATION AIRCRAFTE DDIVERTED TO SYR AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RESIDUE ON CAPTAIN WINDOW .CLEANED AND ACCOMPLISHED WINDOW INSPECTION AS PER AMM 56-11-12. ALL CHECKS NORMAL, NO CRACKOR DEFECT NOTED.
AIRCRAFT WAS GROUNDED: CATERING REPORTS UNABLE TO OPEN 1R SERVICE DOOR COMPLETELY. MAINTENANCE REPLACED #1 DOOR EMERGENCY OPERATION CYLINDER IAW AMM 52-11-14.
AIRCRAFT WAS GROUNDED: CATERING REPORTS UNABLE TO OPEN 1R SERVICE DOOR COMPLETELY. MAINTENANCE REPLACED #1 R DOOR DAMPER IAW AMM 52-11-14.
AIRCRAFT WAS NOT GROUNDED: DOOR 1R WILL NOT OPEN FULLY. CATERING COULD NOT OPEN. TRIED TO OPEN AND IT FEELS LIKE SOMETHING IS NOT ALLOWING IT TO OPEN FULLY. LOOKED AND COULD NOT SEE ANYTHING. TRIED A COUPLE TIMES. LUBED TELESCOPIC ACTUATOR IAW 12-22-52 OPERATIONAL CHECK OF DOOR NORMAL.
AIRCRAFT WAS NOT GROUNDED: LEFT FORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTEDANT FLASHLIGHT AT L2 SEAT INOPERATIVE. REPLACED L2 FLASHLIGHT
AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXTERNAL LOAD FAULT ON CIDS OPS CHECK. REMOVED AND REPLACED CABIN EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-38. OPS CHECK GOOD.
AIRCRAFT WAS GROUNDED: THE AIRCRAFT RETURNED TO LAX DUE TO THE FLIGHT CREW REPORTING THAT ON CLIMB OUT PASSING 2000 FT. UPPER EICAS DISPLAYED FUEL CTR TANK TRANSFER FAULT. CENTER TANK SHOWED EMPTY. THE FLIGHT CREW FOLLOWED PROCEDURES AND THE FUEL ON BOARD TOTALIZER ON THE FUEL PAGE FLASHED YELLOW AND THE FLIGHT CREW PLACED THE CENTER TANK MODE SELECTION IN MANUAL AND TURNED THE CENTER TANK PUMPS OFF. THE AIRCRAFT LANDED SAFELY AT LAX WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED CENTER TANK FUEL QUANTITY PROBE 39QT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO FAULTS NOTED.
AIRCRAFT WAS NOT GROUNDED: MAINTENANCE FOUND EMERGENCY LIGHT AT SEAT ROW 11 INOPERATIVE DURING SYSTEM TEST OF THE EMERGENCY LIGHTING SYSTEM. MAINTENANCE REPLACED EMERGENCY LIGHT CONNECTOR AT SEAT ROW 11 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT PATH LIGHTS INOP AT ROWS 11, 20, AND 21. FOUND CONNECTOR AT ROW 20/21 DISCONNECTED. RECONNECTED CANON PLUG AT ROW 20/21.
AIRCRAFT WAS NOT GROUNDED: FORWARD AND AFT PASSENGER AND CREW DOOR EMERGENCY ACCUMULATOR NEED SERVICE. SERVICED FORWARD PASSENGER AND CREW DOOR EMERGENCY ACCUMULATOR.
AIRCRAFT WAS NOT GROUNDED: FORWARD AND AFT PASSENGER AND CREW DOOR EMERGENCY ACCUMULATOR NEED SERVICE. SERVICED AFT PASSENGER AND CREW DOOR EMERGENCY ACCUMULATOR.
AIRCRAFT WAS GROUNDED: CLIMBING ABOVE FL 320 FLIGHT CREW REPORTED HEARING A SQUEAL BELIEVED TO BE FROM PRESSURIZATION. COULD NOT IDENTIFY THE SOURCE, BUT POSSIBLY FROM EITHER THE CAPTAIN OR FIRST OFFICERS SLIDING WINDOW. DESCENDED FROM FL 360 BACK TO FL 320 AND THE SQUEAL WENT AWAY AT FL32.1. FL360 DELTA P 8.0 CABIN ALT 7150, FL 340 DELTA P 7.9 CABIN ALT 6500. FL 320 DELTA P 7.9 CABIN ALT 5750. MAINTENANCE REPLACED THE LEFT HAND SLIDING WINDOW (AALA202402263489) AND THE RIGHT HAND SLIDING WINDOW (AALA202402260800) PER TASK CARD 26L21156001. A SATISFACTORY LEAK CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS GROUNDED: CLIMBING ABOVE FL 320 FLIGHT CREW REPORTED HEARING A SQUEAL BELIEVED TO BE FROM PRESSURIZATION. COULD NOT IDENTIFY THE SOURCE, BUT POSSIBLY FROM EITHER THE CAPTAIN OR FIRST OFFICERS SLIDING WINDOW. DESCENDED FROM FL 360 BACK TO FL 320 AND THE SQUEAL WENT AWAY AT FL32.1. FL360 DELTA P 8.0 CABIN ALT 7150, FL 340 DELTA P 7.9 CABIN ALT 6500. FL 320 DELTA P 7.9 CABIN ALT 5750. MAINTENANCE REPLACED THE LEFT HAND SLIDING WINDOW (AALA202402263489) AND THE RIGHT HAND SLIDING WINDOW (AALA202402260800) PER TASK CARD 26L21156001. A SATISFACTORY LEAK CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS GROUNDED: R1 CABIN DOOR WILL NOT OPEN ALL THE WAY. REPOSITION BONDING STRAP.
AIRCRAFT WAS GROUNDED: 1R DOOR NOT FULLY OPENING. FOUND TELESCOPIC ARM STICKING OUT. LUBED.
AIRCRAFT WAS GROUNDED: FLIGHT DECK DOOR WILL NOT OPEN FROM THE FLIGHT ATTENDANT KEY PAD, LIGHT IN FLIGHT DECK WILL NOT SHOW UNLOCK WITH TOGGLE SWITCH UNLOCK. FLIGHT DECK DOOR MID STRIKE ELECTRICAL CONNECTOR PIN WAS FOUND LOOSE AND WAS RESECURED PER ESPM 20-44-00. A SATISFACTORY OPERATIONAL CHECK OF THE FLIGHT DECK DOOR LOCKING SYSTEM WAS ACCOMPLISHED PER AMM 52-51-00.
AIRCRAFT WAS NOT GROUNDED: FIRST FLIGHT ATTENDANT FLASHLIGHT NOT BLINKING. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT IN BASE MAINTENANCE: FORWARD LAVATORY ENTRY DOOR HANDLE IS LOOSE. DOOR HARD TO OPEN OR CLOSE. ADJUSTED FORWARD LAVATORY ENTRY DOOR HANDLE PER CMM 25-41-51.
AIRCRAFT WAS NOT GROUNDED: L2 DOOR DAMPER CYLINDER REQUIRES SERVICED. SERVICED L2 DOOR DAMPER CYLINDER PER AMM 52-10-00.
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO MID DUE TO #1 ADR FAULT, NO FAULT LIGHTS AUTO PILOT / AUTO THROTTLE LOST, CAPTAINS INSTRUMENTS LOST. AIR DATA SWITCH TO CAPTAINS DID NOT BRING BACK CAPTAINS INSTRUMENTS. ALSO #3 IRS / GPS OFF 22 MILES THEN BLANK, CHECK IRS 03/FM POSITION. THE AIRCRAFT LANDED SAFELY AT MID. MAINTENANCE REPLACED THE #1 (AALA202211166964) AND #3 (AALA202211164644) ADIRU PER AMM 34-12-34. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO MID DUE TO #1 ADR FAULT, NO FAULT LIGHTS AUTO PILOT / AUTO THROTTLE LOST, CAPTAINS INSTRUMENTS LOST. AIR DATA SWITCH TO CAPTAINS DID NOT BRING BACK CAPTAINS INSTRUMENTS. ALSO #3 IRS / GPS OFF 22 MILES THEN BLANK, CHECK IRS 03/FM POSITION. THE AIRCRAFT LANDED SAFELY AT MID. MAINTENANCE REPLACED THE #1 AND #3 ADIRU PER AMM 34-12-34. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS NOT GROUNDED: GROUND CREW SPOTTED SAFETY STRAP ON 2L DOOR STICKING OUT ON WALK AROUND. FOUND BUSTLE COVER STRAP HANGING DOWN , RE POSITIONED STRAP ON BUSTLE AS REQUIRED DOOR OPERATES PROPERLY.
AIRCRAFT WAS GROUNDED: ON TAKEOFF #1 ADVANCED TO 87% #2 ONLY ADVANCED TO 71% AND A REJECTED TAKE OFF WAS ACCOMPLISHED AT 60 KNOTS. CREW ATTEMPTED TO TAKE OFF FOR A SECOND TIME WITH THE SAME RESULTS AND ACCOMPLISHED A SECOND REJECTED TAKE OFF AT 60 KNOTS. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
AIRCRAFT WAS GROUNDED: ON TAKEOFF #1 ADVANCED TO 87% #2 ONLY ADVANCED TO 71% AND A REJECTED TAKE OFF WAS ACCOMPLISHED AT 60 KNOTS. CREW ATTEMPTED TO TAKE OFF FOR A SECOND TIME WITH THE SAME RESULTS AND ACCOMPLISHED A SECOND REJECTED TAKE OFF AT 60 KNOTS. **ORIGINAL REPORT WAS AALA202204208340** REPLACED #2 ENGINE FUEL PUMP PER AMM 73-11-10 AND REPLACED THE #2 ENGINE HYDRO MECHANICAL UNIT (HMU) PER TASK CARD 26L40073007 (AALA202204276660) A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS GROUNDED: ON TAKEOFF #1 ADVANCED TO 87% #2 ONLY ADVANCED TO 71% AND A REJECTED TAKE OFF WAS ACCOMPLISHED AT 60 KNOTS. CREW ATTEMPTED TO TAKE OFF FOR A SECOND TIME WITH THE SAME RESULTS AND ACCOMPLISHED A SECOND REJECTED TAKE OFF AT 60 KNOTS. **SUPPLEMENTAL REPORT FOR AALA202204208340: REPLACED #2 ENGINE FUEL PUMP PER AMM 73-11-10 AND REPLACED THE #2 ENGINE HYDRO MECHANICAL UNIT (HMU) PER TASK CARD 26L40073007 (AALA202204276660) A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED** (CLOSED)
AIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIT PATH LIGHT ON LAVATORY D LOOSE/ LANDING ON WIRES. CORRECTLY INSTALLED EMERGENCY EXIT PATH LIGHT ON LAVATORY D PER AMM 33-51-18-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: CAPTAINS SLIDING WINDOW HANDLE CRACKED. REPLACED SLIDING WINDOW HANDLE PER AMM 56-12-11-400-001-A02.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON SPIGOT NUT. REPLACED SPIGOT NUT PER TASK CARD 26C41554031.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON SPIGOT NUT. REPLACED SPIGOT NUT PER TASK CARD 26C42554031.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TOP SKIN PANEL #2 LOWER SURFACE AT THE TRAILING EDGE REAR SPAR BETWEEN WMRX5621,977 AND WMRX5855,6, BETWEEN RIB 15 AND RIB 16. REPAIRED SKIN PANEL PER EA 332921.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING UPPER SKIN PANEL #2 LOWER SURFACE BETWEEN WMRX4390 AND WMRX6415, BETWEEN RIB 13 NAD RIB 14. REPAIRED SKIN PANEL PER EA 332921.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE FLAP PIVOT BOLT. REPLACED PIVOT BOLT PER TASK CARD 26L0002709.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING #2 TRAILING EDGE FLAP TRACK PIVOT BOLT BETWEEN RIB 9 AND RIB 10. REPLACED PIVOT BOLT PER TASK CARD 26C58057015.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FRAME LOCATED AT FR 43 FROM S18R TO S24R. REPLACED FRAME PER EA 332514 AND DWG R533-70232 REV. C.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON STRINGER BETWEEN FR 64 AND FR 67 AT S31R. REPLACED STRINGER PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE FLAP TRACK #4 PENDULUM ASSEMBLY. REPLACED PENDULUM ASSEMBLY PER CMM 57-53-21-400-809-C01 AND SRM A319 57-72-11-911-001.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON SPIGOT SLEEVE. REPLACED PYLON SPIGOT SLEEVE PER TASK CARD 26C42554031.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON SPIGOT SLEEVE. REPLACED PYLON SPIGOT SLEEVE PER TASK CARD 26C41554031.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT #3 LOWER AFT BOLT. REPLACED BOLT PER AMM 27-84-65-400-002-A.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT #1 , TRACK #2 FORWARD LOWER BOLT. REPLACED BOLT PER AMM 27-84-61-200-001-A AND AMM 27-84-63-400-002-A
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE #1 SLAT, TRACK #3 ECCENTRIC BOLT . REPLACED BOLT PER AMM 27-84-61-200-001-A AND AMM 27-84-63-400-002-A.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL AT FR 68 AND S23L. REPAIRED LOWER SILL PER SRM 53-41-14-300-001.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL AT FR 68 AND S23R. REPAIRED LOWER SILL PER SRM 53-41-14-300-001.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SHEAR TIE AT FR 65 BETWEEN S29R AND S31R. REPLACED SHEAR TIE PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM AT FR 66 AND +Y765. REPLACED FLOOR BEAM PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: AFT GALLEY AREA CRACKED SHEAR PLATE LOCATED FROM FR 69 TO FR 70 AND S23R. REPLACED SHEAR PLATE PER SRM 51-42-11-801 AND DWG D53470100.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM BETWEEN FR 12 AND FR 24 AT -Y765. REPLACED FLOOR BEAM PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR WEB BETWEEN FR 69 AND FR 70 AT S23R. REPLACED FLOOR WEB PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING OUT BOARD FLAP OUTER DOUBLER BETWEEN RIB 14 AND RIB 15 AND S7 AND S10. REPLACED FLAP TASK CARD 26L00027009.
AIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD TRAILING EDGE FLAP LOWER SURFACE DELAMINATED BETWEEN RIB 6 AND RIB 8. REPAIRED FLAP PER SRM 57-52-00-300-094.
AIRCRAFT IN BASE MAINTENANCE: CRACKED FITTING AT FR 65 BETWEEN S9L AND S10L. REPLACED FITTING PER SRM 51-42-11.
AIRCRAFT WAS GROUNDED: AFTER 2 HRS 30 MIN AT 390 DURING DESCENT AT APPROX. 11K' ENGINE #1 COMPRESSOR VANE WITH AVOID RAPID THRUST ECAM , EVERY THROTTLE MOVEMENT UNTIL 4K' LIGHT CAME BACK ON , LANDING NORMAL / IDLE LOVER. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
AIRCRAFT WAS GROUNDED: AFTER 2 HRS 30 MIN AT 390 DURING DESCENT AT APPROX. 11K' ENGINE #1 COMPRESSOR VANE WITH AVOID RAPID THRUST ECAM, EVERY THROTTLE MOVEMENT UNTIL 4K' LIGHT CAME BACK ON, LANDING NORMAL / IDLE LOWER. **ORIGINAL REPORT WAS AALA202111126521** REPLACED ENGINE 1 BLEED VALVE STOP MECHANISM PER AMM 75-31-20. REPLACED ENGINE 1 BLEED VALVE FUEL MOTOR ASSEMBLY PER AMM 75-31-10 (AALA202111156257). A SATISFACTORY LEAK /OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS GROUNDED: AFTER 2 HRS 30 MIN AT 390 DURING DESCENT AT APPROX. 11K' ENGINE #1 COMPRESSOR VANE WITH AVOID RAPID THRUST ECAM, EVERY THROTTLE MOVEMENT UNTIL 4K' LIGHT CAME BACK ON, LANDING NORMAL / IDLE LOWER. **SUPPLEMENTAL REPORT FOR AALA202111126521: REPLACED ENGINE 1 BLEED VALVE STOP MECHANISM PER AMM 75-31-20. REPLACED ENGINE 1 BLEED VALVE FUEL MOTOR ASSEMBLY PER AMM 75-31-10 (AALA202111156257). A SATISFACTORY LEAK /OPERATIONAL CHECK WAS ACCOMPLISHED. ** (CLOSED)
AIRCRAFT WAS GROUNDED: WHILE ACCOMPLISHING SERVICE CHECK WALK AROUND, FOUND CRACK ON L1 DOOR COVER PLATE 3.25 INCHES FROM TOP. CRACK IS ON TOP DOOR SEAL CHANNEL AFT SIDE UPPER. REPLACED COVER PLATE PER SRM 51-23-31.
AIRCRAFT WAS GROUNDED: APU AGENT DISCHARGE LIGHT ILLUMINATED. REPLACED APU FIRE BOTTLE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 26-22-41.
AIRCRAFT WAS GROUNDED: RIGHT MAIN LANDING GEAR LEG FIXED FAIRING ASSEMBLY MOUNT BRACKET AND BUSHINGS ON GEARSIDE WORN. REPLACED MOUNT BRACKET PER CMM 32-12-25 AND AMM 32-12-14.
AIRCRAFT WAS GROUNDED: LEFT MAIN LANDING GEAR LEG FIXED FAIRING ASSEMBLY MOUNT BRACKET AND BUSHINGS ON GEARSIDE WORN. REPLACED MOUNT BRACKET PER CMM 32-12-25 AND AMM 32-12-14.
AIRCRAFT WAS GROUNDED RIGHT HAND SIDE OVER WING SLIDE CONTAINER HOUSING IS DELAMINATED ON THE UPPER TRAILING EDGE. REPLACED SLIDE PER J/C 26L0025014.
AIRCRAFT GROUNDED - ECAM MESSAGE: ELEC BATTER 1 FAULT, FUMES IN FORWARD CABIN AND COCKPIT. PERFORMED JOB CARD 26L00021001 - SMOKE, ODOR, FUMES INITIAL TROUBLESHOOTING, FOUND BATTERY NR 1 TO BE SOURCE OF ODOR. REMOVED AND REPLACED BATTERY NR 1 PER AMM 24-38-51, OKAY FOR SERVICE.
AIRCRAFT WAS GROUNDED: AT CRUISE FLT 34000 RECIECVED ECAM NR 2 ENGINE BLEED FAULT WITH ACCOMPANYING CABIN ALTTUDE LINE MAKES CABIN ALTITUDE 9000. (NR 1 ENGINE BLEED ON EXISTING MEL PLACARD). AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO CLE WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. REPLACED OVERPRESSURE VALVE PER AMM 36-11.
AIRCRAFT WAS NOT GROUNDED: AFT CARGO SMOKE WARNING DISPLAYED. MAINTENANCE ACCOMPLISHED CIRCUIT BREAKER RESET PER TSM 24-00-00-810-818 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS GROUNDED: PILOT REPORTS AFTER THE "80" CALL CAPTAIN'S AIRSPEED INDICATION WAS INDICATING ZERO. REJECT WAS MADE BELOW 100KTS. MAINTENANCE REPLACED CAPT'S PITOT PROBE (9DA1) IAW AMM 34-11-15 PGBLOCK 0401. (DEBRIS FOUND IN PITOT PROBE) FLUSHED LINE AND PERFORMED SATISFACTORY FUNCTIONAL TEST OF AIRSPEED AND ALTITUDE DATA IAW AMM 34-13-00-720-009-B.
AIRCRAFT WAS NOT GROUNDED: SMOKE AFT CARGO SMOKE MESSAGE DISPLAYED. MAINTENANCE ACCOMPLISHED AFT CARGO HEAT RESET PER TSM 24-00-00 AND PEFORMED SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT IN BASE VISIT: RH ELEVATOR HAS 1.5" AREA OF WATER INGRESS 4.75IN FORWARD OF TE, TOP SKIN. CUT OUT DAMAGED CORE, INSTALLED NEW CORE AND REPAIR PLIES AND RESTORED PAINT IAW SRM 55-21-11-300-005, SRM 51-75-12.
AIRCRAFT IN BASE VISIT: RH ELEVATOR HAS AREA OF WATER INGRESS 1.5" DIA. 5.0IN FROM TE ON TOP SKIN. CUT OUT DAMAGED CORE, INSTALLED NEW CORE AND REPAIR PLIES AND RESTORED PAINT IAW SRM 55-21-11-300-005, SRM 51-75-11.
R2 DOOR SLIDE COVER SIGHT GLASS CRACKED. MAINTENANCE REPLACED THE SIGHT GLASS AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
RIGHT OVERWING SLIDE PANEL DOOR ASSEMBLY HAD DELAMINATION AND OVERWING SLIDE DOOR RETAINER PANEL HAD A 7505 MM CRACK AT THE LOWER AFT CORNER. REPLACED THE RIGHT OVERWING SLIDE IAW J/C 26L20025014.
THE NR 2 ENGINE INBOARD THRUST REVERSER J-RING HAS PITTING CORROSION ON RUB STRIP. THE AIRCRAFT WAS GROUNDED. REPLACED THE J-RING IAW CMM 78-32-36.
THE NR 2 ENGINE OUTBOARD THRUST REVERSER J-RING HAD PITTING CORROSION ON THE RUB STRIP. THE AIRCRAFT WAS GROUNDED. REPLACED THE J-RING IAW CMM 78-32-36.
EXIT LIGHT ABOVE THE AFT SERVICE DOOR, THE LENS WAS MISSING. INSTALLED A NEW LENS. OK FOR SERVICE.
AIRCRAFT IN BASE MAINTENANCE: EMERGENCY DECLARED. RETURNED TO CLT ON ACCOUNT OF PRESSURE LOSS IN YELLOW HYDRAULIC SYSTEM. MAINTENANCE ACCOMPLISHED INSPECTION FOR POSSIBLE HYDRAULIC CONTAMINATION/OVERHEAT/ CAVITATION PER AMM 29-00-00-280-006-A01. MAINTENANCE ALSO REPLACED HYDRAULIC LINE GOING TO HYDRAULIC CONTROL UNIT PER IPC 29-13-06 AND REPLACED MAIN SUPPLY FUEL HOSE PER AMM 73-11-11 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
RIGHT FUEL TANK PUMP 1 LOW IAW ECAM MESSAGE. MAINTENANCE REPLACED THE RIGHT WING PUMP SWITCH 14QA IAW ESPM 20-45-11, AND PERFORMED A SATISFACTORY OPS CHECK IAW AMM 28-21-51.
RIGHT OVERWING EXIT SLIDE DOESN'T SHOW ARMED. PERFORMED EMERGENCY EXIT ADJUSTMENT AND TEST IAW AMM 52-21-11.
LEFT OVERWING EMERGENCY EXIT DOOR INDICATES UNARMED ON ECAM DOOR PAGE. RESET TO ARM LEFT OVERWING EMERGENCY EXIT DOOR IAW AMM 52-21-00-0001.
AIRCRAFT WAS NOT GROUNDED: L2 DOOR WILL NOT ARM. MAINTENANCE LUBED L2 DOOR LOCKING MECHANISM AND SLIDE BAR AND PERFORMED SATISFACTORY TEST PER AMM 52-13-21.
L1 DOOR WAS DIFFICULT TO OPEN. PLASTIC COVER ON TOP OF DOOR WOULD DROP DOWN CAUSING DOOR TO BIND, RESTRICTING DOOR MOVEMENT. MAINTENANCE ADJUSTED THE DOOR TRIM PANEL AND PERFORMED A SUCCESSFUL OPS CHECK IAW AMM 52-20-00.
FORWARD L1 DOOR, RIGHT ASSIST HANDLE IS LOOSE AND PINCHES FINGERS WHEN USED. REPLACED FORWARD THE L1 DOOR HANDGRIP COVER IAW AMM 25-23-46.
EMERGENCY EXIT SIGNS AT ROW 14 RIGHT, WILL NOT EXTINGUISH. ACCOMPLISHED A WIRING CHECK FROM 4WL TO 12WL IAW AWM 33-51-03. FOUND W3351-1014 PIN D AT 12WLA INTERMITTENT. SECURED IAW ESPM 20-44-11. ACCOMPLISHED OPERATIONAL TEST IAW AMM 33-51-00, TESTED GOOD. AIRCRAFT WAS GROUNDED.
RIGHT OVERWING EXIT SLIDE DISARMED. SLIDE ARM INDICATION LIGHT 2W HAS BEEN REPLACED IAW AMM.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT MAIN LANDING GEAR REAR PINTLE PIN. REPLACED PINTLE PIN ASSEMBLY PER JOB CARD NO 26T00032001.
AFTER PUSHING THRUST LEVERS FORWARD FOR TAKE OFF, ECAM MESSAGE FOR FLT CONTROL ELAC 1 FAULT MESSAGE ON ECAM. ABORTED TAKEOFF AT 5 KTS. RETURNED TO GATE FOR MAINTENANCE. ACCOMPLISHED OPERATION TEST OF THE ELAC 1 IAW TSM 27-93-00-710-001-A NO FAULTS NOTED.
CENTER FUEL PUMP NR 1 FAULT, AFT TAKE OFF ECAM PROCEDURE PERFORMED. REPLACED CONTROL PUMP PRESSURE SWITCH IAW TSM 28-21-00-810-813.
RIGHT OVERWING SLIDE COVER IS CRACKED, APROXIMATELY 6 INCHES AFT SIDE. REMOVED AND REPLACED THE SLIDE ASSEMBLY. AIRCRAFT WAS GROUNDED.
OVERWING EXIT LEFT SIDE SIGN DAMAGED. REPLACED THE LENS.
POST FLIGHT INSPECTION FOUND BULGING CRACK IN FUSELAGE AFT OF THE TRAILING EDGED OF THE RIGHT WING, SLIDE ENCLOSURE DAMAGED. REPAIRED DAMAGE AND REPLACED ESCAPE SLIDE. AIRCRAFT WAS GROUNDED.
AIRCRAFT WAS NOT GROUNDED. AFT CENTER FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT INOPERABLE. REPLACED BATTERY PER AMM 25-65-00.
AFT 2L DOOR EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
LEFT EMERGENCY POWER SUPPLY UNIT BATTERY FAULTED. REPLACED LEFT EMERGENCY POWER SUPPLY UNIT BATTERY AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 33-51-38-000-002-A.
AFT LEFT EXIT EMER EXIT LIGHT MISSING COVER. REPLACED LENS/ COVERS REQUIRED. OK FOR SERVICE. THE AIRCRAFT WAS NOT GROUNDED.
FORWARD ENTRY BULKHEAD EMERGENCY LIGHT IS LOOSE. REINSTALLED LIGHT FIXTURE INTO WALL SOCKET PER AMM 33-51-18.
IN FLIGHT, HAD A LAVATORY SMOKE ECAM. FLIGHT ATTENDANT REPORTED IT WAS THE FORWARD LAVATORY RESET ITSELF IN ABOUT 5 SECONDS. FIGHT ATTENDANT REPORTED THAT THERE WAS NO SMOKE IN THE FORWARD LAVATORY. MAINTENANCE PERFORMED SYSTEM RESET IAW TSM TASK 26-15-00-810-804A. NO FAULTS NOTED.
AIRCRAFT WAS NOT GNDED. DESCENDING THROUGH 12000 LOUD HOWLING NOISE STOPPED, FOLLOWED BY CLASS 1 ECAM VENT BLOW FAULT. FLIGHT CREW FOLLOWED ECAM ACTIONS, VENT OVERRIDE OFF. THIS WAS FOLLOWED BY ELEC SMELL IN COCKPIT & FWD CABIN. REPLACED THE AVIONICS BLOWER FAN & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 21-26-51.
AIRCRAFT IN BASE MX. COCKPIT WINDSHIELD CUT OUT FRAME, UPPER STIFFENER HAS CRACK INDICATION AT FRAME 4 RT. REPAIRED FRAME STIFFENER IAW EA 256984.
AIRCRAFT IN BASE MX. AFT CARGO COMPARTMENT FLOOR PANEL 151VG DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.
AIRCRAFT IN BASE MX. PAX CREW DOOR 832, L2, SLIDE RAFT CONTACTS FUSELAGE WHEN DOOR IS FULLY OPEN. REPLACED PAX L2, SLIDE RAFT IAW JC 26C83252008.
AIRCRAFT IN BASE MX. WINDSHIELD CTR FRAME HAS CRACK INDICATION AT FRAME 4 RT. REPLACED IAW EA 256933 & 256736.
AIRCRAFT IN BASE MX. WINDSHIELD CTR FRAME, UPPER FASTENER HOLE AT FRAME 4 LT HAS CRACK INDICATION. REPLACED FRAME IAW EA 256933 & 256736.
AIRCRAFT IN BASE MX. LT WING FUEL ACCESS PANEL 540JB WORN AT SEVERAL COUNTERSINK FASTENER HOLES. REPLACED ACCESS PANEL 540JB IAW TASK CARD 26C54057007.
AIRCRAFT IN BASE MX. LT WING ACCESS PANEL 540KB, WORN AT SEVERAL FASTENER COUNTERSINK HOLES. REPLACED ACCESS PANEL 540KB IAW TASK CARD 26T50057039.
AIRCRAFT IN BASE MX. LT WING NR 2 SPOILER, CTR HINGE FITTING BOLT STOP WORN. DIMENSION T REPAIRED IAW SRM 57-70-00-201 PARAGRAPH 5C FIGURE 201 SHEET 2.
AIRCRAFT WAS IN BASE MX. PERFORM SPECIAL INSPECTION FOR CRACK ON HANDLE SLIDING WINDOW, FIRST OFFICER SIDE IN COCKPIT. R & R HANDLE SLIDING WINDOW, FIRST OFFICER SIDE IN COCKPIT IAW AMM 56-12-12-400-003-A.
AIRCRAFT IN BASE MX. RUDDER HINGE ARM NR 2 AT RIB 4 HAS EXCESSIVE PLAY. REPLACED HINGE IAW AMM 55-36-41-0401.
AIRCRAFT IN BASE MX. RUDDER HINGE ARM NR 1 AT RIB 2 HAS EXCESSIVE PLAY. REPLACED HINGE IAW AMM 55-36-41-0401.
AIRCRAFT IN BASE MX. RUDDER FITTING AT RUDDER STATION 4132 & RIB 9 HAS EXCESSIVE PLAY. REPLACED FITTING IAW AMM 55-36-41.
AIRCRAFT IN BASE MX. CORROSION ON CORNER FITTING AT FRAME 68 & STRINGER 23R. REPLACED FITTING IAW SRM 51-72-11.
AIRCRAFT IN BASE MX. CORROSION ON L2 DOOR CUT OUT LOWER SILL, CTR SHAPE SILL FITTING, BETWEEN FRAME 66 & 68 AT STRINGER 23L. REPLACED FITTING IAW SRM 51-72-11.
AIRCRAFT IN BASE MX. CORROSION ON CORNER FITTING AT FRAME 68 & STRINGER 23L. REPLACED FITTING IAW SRM 51-72-11.
AIRCRAFT IN BASE MX. CABIN FLOOR PANEL 231XG DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.
AIRCRAFT IN BASE MX. RT RUDDER SKIN HAS 4 AREAS OF TRAPPED WATER INDICATION, BETWEEN RUDDER STATION 120 - 389, 2.45" & 29.5" FROM THE TE & 33.25" & 104" FROM THE LOWER EDGE. REPAIRED RUDDER SKIN IAW EA 256820.
AIRCRAFT IN BASE MX. RT SIDE BOX BEAM FLANGE HAS CRACK INDICATION AT FRAME 43 & -Y1651. REPAIRED IAW EO 5315Y066.
AIRCRAFT IN BASE MX. LT SIDE PRESS PLATE HAS CRACK INDICATION AT FRAME 43 & Y1292. REPLACED PRESS PLATE IAW SRM 51-42-11.
AIRCRAFT IN BASE MX. RT WING NR 3 SPOILER, CTR HINGE FITTING BOLT STOP WORN. DIMENSION T REPAIRED IAW SRM 57-70-00-201 PARAGRAPH 5C FIGURE 201 SHEET 2.
AIRCRAFT IN BASE MX. CORROSION ON RT MLG DOOR HINGE FITTING. REPLACED FITTING IAW CMM 52-81-18.
AIRCRAFT IN BASE MX. LT WING NR 4 SPOILER CTR HINGE FITTING WORN AT THE BOLT STOP AREA. REPAIRED FITTING IAW SRM 57-70-00-201 PARAGRAPH 5C FIGURE 201 SHEET 2.
AIRCRAFT IN BASE MX. LT WING NR 3 SPOILER, CTR HINGE FITTING BOLT STOP WORN. REPAIRED IAW SRM 57-70-00-201 PARAGRAPH 5C FIGURE 201 SHEET 2.
AIRCRAFT IN BASE MX. RT WING NR 2 SPOILER, CTR HINGE FITTING WORN AT THE BOLT STOP AREA. REPAIRED FITTING IAW SRM 57-70-00-201 PARAGRAPH 5C FIGURE 201 SHEET 2.
AIRCRAFT IN BASE MX. AFT GALLEY FLOOR PANEL 261DF DELAMINATED. REPLACED IAW AMM 53-42-12-400-002-A.
AIRCRAFT IN BASE MX. FWD GALLEY FLOOR PANEL 232DF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.
AIRCRAFT IN HEAVY MX. FWD GALLEY FLOOR PANEL 221LF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.
AIRCRAFT IN HEAVY MX. AFT GALLEY FLOOR PANEL 261PF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.
AIRCRAFT IN BASE MX. FWD GALLEY FLOOR PANEL 222EF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.
AIRCRAFT IN BASE MX. FWD GALLEY FLOOR PANEL 221DF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.
AIRCRAFT IN BASE MX. AFT GALLEY FLOOR PANEL 261AG DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.
AIRCRAFT WAS IN BASE MX. EXCESSIVE PLAY ON LT ELEVATOR NR 1 HINGE ARM. R & R HINGE ARM FITTING IAW AMM 55-16-42.
AIRCRAFT WAS IN BASE MX. EXCESSIVE PLAY ON LT ELEVATOR NR 5 HINGE ARM. R & R HINGE ARM FITTING IAW AMM 55-16-42.
AIRCRAFT WAS IN BASE MX. EXCESSIVE PLAY ON LT ELEVATOR NR 2 HINGE ARM. R & R HINGE ARM FITTING IAW AMM 55-16-42.
AIRCRAFT WAS IN BASE MX. EXCESSIVE PLAY ON LT ELEVATOR NR 6 HINGE ARM. R & R HINGE ARM FITTING IAW AMM 55-16-42.
AIRCRAFT IN HEAVY MX. FWD GALLEY FLOOR PANEL 231FF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.
AIRCRAFT IN BASE MX. AFT GALLEY FLOOR PANEL 261BG DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.
AIRCRAFT IN BASE MX. AFT GALLEY FLOOR PANEL 262BG DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.
AIRCRAFT IN BASE MX. SEAT TRACK INBD LOWER COUPLING AT FRAME 66 & -Y1292, HAS ELONGATED HOLE. REPLACED COUPLING IAW SRM 51-42-11.
AIRCRAFT IN BASE MX. CORROSION ON SEAT TRACK, BETWEEN FRAME 62 & 64 AT -Y1292. REPAIRED SEAT TRACK IAW SRM 53-41-15.
AIRCRAFT IN BASE MX. LT EMER EXIT DOOR SEGMENT, FRAME CRACKED AT BEAM 4. REPLACED SEGMENT FRAME IAW SRM 51-72-11.
AIRCRAFT IN BASE MX. SEAT TRACK INBD UPPER COUPLING AT FRAME 64 & -Y1292, HAS ELONGATED HOLE. REPLACED COUPLING IAW SRM 51-42-11.
AIRCRAFT IN BASE MX. CORROSION ON CTR WING BOX, UPPER SURFACE SKIN, BETWEEN FRAME 41 & 42 AT +Y1292. REPAIRED IAW EA 256738.
AIRCRAFT IN BASE MX. COUPLING AT FRAME 68 & -Y1162 HAS ELONGATED HOLE DIAMETER. REPLACED COUPLING IAW SRM 51-72-11.
AIRCRAFT IN BASE MX. CORROSION ON SEAT TRACK, BETWEEN FRAME 64 & 66 + 5" AT -Y1292. REPLACED SEAT TRACK IAW SRM 51-42-11.
AIRCRAFT IN BASE MX. CORROSION ON JOINT COVER, BETWEEN FRAME 12 & 16 AT -Y81. REPLACED JOINT COVER IAW SRM 51-72-11.
AIRCRAFT IN BASE MX. CABIN FLOOR PANEL 242MF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.
AIRCRAFT IN BASE MX. CORROSION ON FLOORBEAM, BETWEEN FRAME 66 + 5" & 67 + 15" AT +Y1225. REPLACED FLOORBEAM IAW SRM 51-72-11.
AIRCRAFT IN BASE MX. CORROSION ON FLOORBEAM, BETWEEN FRAME 66 + 5" & 67 + 15" AT -Y1225. REPLACED FLOORBEAM IAW SRM 51-72-11.
AIRCRAFT IN BASE MX. CORROSION ON FLOORBEAM, BETWEEN FRAME 67 + 15" & 69 AT -Y1162. REPLACED FLOORBEAM IAW SRM 51-72-11.
AIRCRAFT IN BASE MX. CORROSION ON L2 DOOR CUT OUT LOWER SILL, BETWEEN FRAME 66 & 68 AT STRINGER 23L. REPLACED LOWER SILL IAW SRM 51-72-11.
AIRCRAFT IN BASE MX. CORROSION ON FLOOR STRUCTURE BEAM, BETWEEN FRAME 66 AT -Y1732. REPLACED BEAM IAW SRM 51-72-11.
AIRCRAFT IN BASE MX. COUPLING AT FRAME 65 & -Y1589 HAS ELONGATED HOLE. REPLACED COUPLING IAW SRM 51-42-11.
AIRCRAFT IN BASE MX. CORROSION ON FLOORBEAM, BETWEEN FRAME 67 + 15" & 69 AT +Y1162. REPLACED FLOORBEAM IAW SRM 51-72-11.
AIRCRAFT IN BASE MX. CORROSION ON COUPLING AT FRAME 68 & -Y1162. REPLACED COUPLING IAW SRM 51-72-11.
AIRCRAFT IN BASE MX. SPLICE AT FRAME 24 & -Y254 HAS ELONGATED HOLE. REPLACED SPLICE IAW SRM 51-42-11.
AIRCRAFT IN BASE MX. AFT CARGO COMPARTMENT FLOOR PANEL 151ZG DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.
AIRCRAFT IN BASE MX. CORROSION ON WEB AT FRAME 16 & STRINGER 23R. REPLACED WEB IAW SRM 51-42-11 & 51-72-11.
AIRCRAFT IN BASE MX. CORROSION ON SEAT TRACK, BETWEEN FRAME 64 & 66 + 5" AT +Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11.
AIRCRAFT IN BASE MX. CORROSION ON WEB AT FRAME 20 & STRINGER 23R. REPLACED WEB IAW SRM 51-72-11 & 51-42-11.
AIRCRAFT IN BASE MX. CORROSION ON SEAT TRACK, BETWEEN FRAME 12 & 24 AT -Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11 & 51-42-11.
AIRCRAFT IN BASE MX. CORROSION ON SEAT TRACK, AT FRAME 64 & 66 + 5" AT -Y765. REPLACED SEAT TRACK IAW SRM 51-72-11.
AIRCRAFT WAS IN BASE MX. CABIN SEAT RAIL AT Y -81 CORRODED, BETWEEN FRAME 12 & 16. R & R SEAT RAIL IAW SRM 51-72-11 & DWG 53112829.
CABIN FLOOR SEAT TRACK CORRODED, BETWEEN FRAME 12 & 16, AT Y 503.2. R & R THE SEAT TRACK IAW SRM 51-72-11.
AIRCRAFT IN BASE MX. LT ELEVATOR UPPER SKIN PANEL HAS TRAPPED WATER INDICATION 9.5" INBD OF RIB 4 & 10.5" FROM THE TE. REPAIRED ELEVATOR UPPER SKIN PANEL IAW SRM 55-21-11 & 51-77-13.
AIRCRAFT IN BASE MX. LT ELEVATOR UPPER SKIN PANEL HAS TRAPPED WATER INDICATION. 5" OTBD OF RIB 1 & 15.5" FROM THE TE. REPAIRED ELEVATOR UPPER SKIN PANEL IAW SRM 55-21-11 & 51-77-13.
AIRCRAFT IN BASE MX. RUDDER HINGE ARM NR 7 AT RIB 11 HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW AMM 55-36-41-0401.
AIRCRAFT IN BASE MX. RUDDER HINGE ARM NR 4 AT RIB 6 HAS EXCESSIVE PLAY. REPLACED HINGE IAW AMM 55-36-41-0401.
AIRCRAFT IN BASE MX. RUDDER HINGE ARM NR 5 AT RIB 7 HAS EXCESSIVE PLAY. REPLACED HINGE IAW AMM 55-36-41-0401.
AIRCRAFT IN BASE MX. LT ELEVATOR UPPER SURFACE SKIN HAS 3 AREA OF TRAPPED WATER INDICATION, BETWEEN ELEVATOR RIB 1 & 6, BETWEEN 10" & 12.2" FROM THE TE. REPAIRED ELEVATOR SKIN IAW SRM 51-77-13-001 & 55-21-11-201.
AIRCRAFT IN BASE MX. RUDDER HINGE ARM NR 3 HAS EXCESSIVE PLAY. REPLACED HINGE ARM IAW AMM 27-21-00-720-003-A.
AFTER LANDING, LT AFT WINDSHIELD CRACKED. R & R LT AFT WINDSHIELD IAW AMM 56-11-12-0401.
LEFT OVERWING EMER EXIT SIGN WILL NOT ILLUMINATE. REPLACED BATTERY IAW AMM 33-51-38-000-001-A. OPERATIONS CHECKED NORMAL. OK FOR SERVICE.
ARM & DISARM LEVER ON 2R DOOR IS VERY HARD TO OPERATE. LUBRICATED ARMING MECHANISM AT GIRT FLOOR & REMOVED DEBRIS IAW AMM 52-13-00-820-062 & 52-13-00-820-063. OPERATIONS NORMAL.
L1 DOOR FWD RETAINING CLIP OF GIRT BAR ATTACHMENT NOT SPRINGING BACK TO NORMAL POSITION. CLEANED & LUBRICATED FWD RETAINING CLIP OF GIRT BAR. NO FAULT NOTED AT THIS TIME.
EN ROUTE, FLIGHT ATTENDANTS REPORTED AN ODOR AROUND ROW 21. TEN MINUTES LATER, A SIMILAR ODOR WAS SMELLED IN COCKPIT. DECLARED AN EMER, DIVERTED & FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLE SHOT CABIN AIR QUALITY PER JOB CARDS 26L00021001, 26L00021005 AND 26L00021004. NO ODOR NOTED AT THIS TIME. FOUND APU OIL OVERSERVICED. DRAINED TO PROPER LEVEL. RAN APU AND BOTH ENGINES WITH LEFT AND RIGHT PACKS. OPS CHECK NORMAL. ALSO, FOUND AFT GALLEY AND ALL THREE LAV EXTRACTION FAN VENT FILTERS CLOGGED. REMOVED AND REPLACED FILTERS PER STANDARD PRACTICES.
THE FIRST OFFICER'S SEATBACK RECLINE FAILS TO RETURN TO UPRIGHT POSITION. REPLACED BOTH SEATBACK RECLINE RETURN CYLINDERS IAW CMM 25-11-31.
THE CAPTAIN'S SEATBACK RETURN SPRING INOPERATIVE. SEATBACK FLOPS BACK & WILL NOT RETURN UPRIGHT UNLESS MANUALLY BROUGHT UPRIGHT. R & R CYLINDER WITH NO HELP. REPLACED CAPTAIN'S SEAT IAW AMM 25-11-51-0401. OPERATIONS CHECKED GOOD.
THE RT OVERWING SLIDE LOWER STAINLESS PLATE OUT OF POSITION. REPOSITIONED & INSTALLED PLATE IAW AMM 53-35-11-400-001-A.
THE LT OVERWING SLIDE LOWER STAINLESS PLATE OUT OF POSITION. REPOSITIONED & INSTALLED PLATE IAW 53-35-11-400-001-A.
CREW REPORTED THE FWD MEGAPHONE INOPERATIVE. BATTERIES DEAD IN MEGAPHONE. FOUND SERVICEABLE DATE NEAR EXPIRATION, REPLACED MEGAPHONE.
MAINTENANCE REPORTED SEAT 1A EMERGENCY LIGHT LENS MISSING FROM SEAT. MAINTENANCE REPLACED MISSING LENS ON SEAT 1A. OPS CHECKED GOOD.
CREW REPORTED A DIRTY SOCKS ODOR, APU OFF, FUMES IN COCKPIT. THERE WAS A QUICK ODOR DURING DESCENT AND THEN A CONTINUOUS ODOR IN FWD CABIN AND COCKPIT DURING LAST 5,000 FT OF DESCENT AND APPROACH. FLIGHT CREW WENT ON OXYGEN. MX ACCOMPLISHED CABIN AIR QUALITY J/C 26L00021001. NO ODOR NOTED. ACCOMPLISHED SATISFACTORY TEST FLIGHT. ACFT OK FOR SERVICE.
CREW REPORTED THE L2 DOOR SLIDE ARMING HANDLE DIFFICULT TO ENGAGE AND DISENGAGE. MX LUBED GIRT BAR ON SLIDE AREAS. OPS CHECKED OK.
"C" F/A EMERGENCY LIGHT FLASHLIGHT NOT SHOWING CHARGE. MX REPLACED BATTERY. CHECKS OK IAW 25-60-00.
C11 CHECK - 2 CRACKS IN LT EMERGENCY EXIT DOOR SEGMENT BEAM BETWEEN FR40 TO FR41. REPLACED LT EMERGENCY EXIT DOOR SEGMENT BEAM BETWEEN FR40 TO FR41 IAW EO 5210Y228.
C11, CHECK-SEVERAL CRACKS IN RT EMERGENCY EXIT DOOR SEGMENT BEAM BETWEEN FR40 TO FR41. REPLACED RIGHT EMERGENCY EXIT DOOR SEGMENT BEAM BETWEEN FR40 TO FR41 IAW EO 5210Y228.
C11 CHECK - WATER INGRESS AT 9 SEPARATE LOCATIONS ALONG THE ENTIRE LENGTH OF THE RT ELEVATOR UPPER SURFACE. REPLACED RT ELEVATOR IAW EO 5511Y295.
CREW REPORTED THE 2R EMERGENCY EXIT DOOR SMALL LENS COVER NEEDS TO BE RE-ATTACHED, NOT THE EMERGENCY EXIT SIGN. MAINTENANCE RESET 2R EMERGENCY LIGHT COVER (LOWER). CHECKS OK.
MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 1L, 4L AND OVERHEAD PANELS AT ROW 1 AND ROW 5 ARE INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT AND EMERGENCY BATTERY PACK AT L1 DOOR IAW AMM 33-51-38. OPS CHECK GOOD.
CREW REPORTED THE 1R DOOR WILL NOT ARM. MAINTENANCE REMOVED DEBRIS FROM GIRT BAR FLOOR FITTINGS. ALSO, LUBED ARMING LEVER. OPS CHECK GOOD.
DURING ALL PHASES OF FLIGHT (FLT 1665, CLT-STL), CREW REPORTED THE AIR HAD A MUSTY/OILY ODOR. SWITCHED PACKS OFF ALTERNATELY - AIR SEEMED TO IMPROVE WITH PACK 2 OFF. FLIGHT CONTINUED ONTO DESTINATION TO STL. MAINTENANCE PLACED THE APU ON MEL 49-10-01A. SUBSEQUENTLY, THE NEXT FLIGHT (FLT 1053, STL-CLT) THE FOLLOWING MORNING, THE CREW REPORTED A MUSTY/OILY ODOR EMITTING FROM VENTS DURING ALL PHASES OF FLIGHT. FLIGHT CONTINUED ONTO DESTINATION TO CLT. MAINTENANCE REMOVED AND REPLACED THE APU PER J/C 26L31049003. LEAK AND OPS TEST OK. ACCOMPLISHED J/C 26L00021001 - T/S CABIN AIR QUALITY, J/C 26L00021002 - APU SMELL IN CABIN AND J/C 26L00021004 - DECONTAMINATION OF THE ECS A319/A320/A321 (ENGINES AND APU). CLEARED MEL 49-10-01A.
FORWARD ENTRY DOOR L1 SLIDE WHITE LANYARD ROUTED INCORRECTLY. RE-ROUTED FORWARD ENTRY DOOR L1 SLIDE LANYARD.
EMERGENCY LIGHTS INOPERATIVE AT FORWARD ENTRY, FORWARD GALLEY, AND FORWARD CABIN. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (10WL) PER AMM 33-51-38-044-001. OPS CHECKED GOOD.
HYDRAULIC GREEN SYSTEM LOW PRESSURE FAULT. SYSTEM SHOWS 2950 PSI. BUT WE HAD AMBER ILLUMINATED ON GREEN SYSTEM. FLIGHT CONTROL PAGE SHOWED AMBER ON ALL GREEN ITEMS. BSCU-1 FAULT SHOWN. REMOVED AND REPLACED BSCU AS PER AMM 32-42-34-400-001-A , SYSTEM OPS CKECKED GOOD.
ON LANDING GEAR RETRACTION AFTER TAKEOFF, LANDING GEAR REMAINED UNLOCKED. ECAM MESSAGE GENERATED AFTER APPROXIMATELY 3 MINUTES. LANDING GEAR RETRACTED. ECAM PROCEDURE HAD NOT YET BEEN ACCOMPLISHED. WHEN UNLOCKED, NOISE OF GEAR DOORS OPEN WAS HEARD. REMOVED AND REPLACED LANDING GEAR CONTROL INTERFACE UNIT (LGCIU). OPS CHECKED GOOD.
FORWARD LEFT EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER AMM 25-65-53. OPS CHECKED GOOD.
FLT 2049 - BOS-DCA - EMERGENCY LIGHTS - SEAT 20 ABC HAS BROKEN WIRE AT CONNECTOR FOR EMERGENCY LIGHTNING. ACCOMPLISHED SERVICEABLE REPAIR PER ESPM 20-44-00. OPERATIONAL CHECK GOOD.
DOOR R2 F/A FLASHLIGHT BATTERY BURNED OUT. R & R FLASHLIGHT BATTERY. OPS CHECK WAS GOOD.
FLT 1761 - BOS - EEL - AFT GALLEY EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY.
PIT - S4 - MAJOR REPAIR - CRACK ON LEFT WING NR 3 SLAT NR 7 TRACK ANTI-ROTATION STOP OUTBOARD LUG. REPAIRED LEFT WING NR 3 SLAT NR 7 TRACK ANTI-ROTATION STOP IAW EA 114368.
LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR20, -Y1292. REPLACED FLOORBEAM AT FR20, -Y1292 IAW A319 SRM 51-72-11.
PIT - S4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR23, Y1292. REPLACED FLOORBEAM AT FR23, Y1292 IAW A319 51-72-11.
LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR 22, -Y765. REPLACED SEAT TRACK FLOORBEAM AT FR 22, -Y765 IAW A319 SRM 51-72-11.
LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR 20 TO FR 21, -Y189. REPLACED FLOORBEAM BETWEEN FR 20 TO FR21, -Y189 IAW A319 SRM 51-72-11.
LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR24, -Y1292. REPAIRED SEAT TRACK AT FR24, -Y1292 IAW A319 SRM 53-21-15.
PIT - S4 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM BETWEEN FR65 TO FR66, S23L, Y1732. REPLACED FLOORBEAM BETWEEN FR65 TO FR66, S23L, Y1732 IAW A319 SRM 51-72-11.
PIT - S4 - MAJOR REPAIR - NR 26C26053005/007 - LEVEL 2 CORROSION ON FLOORBEAM BETWEEN FR 65 TO FR 66, S23L, Y1732. REPLACED FLOORBEAM BETWEN FR 65 TO FR 66, S23L, Y1732 IAW A319 SRM 51-72-11.
LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR 65 TO FR 69, Y1292. REPLACED FLOORBEAM BETWEEN FR 65 TO FR 69, Y1292 IAW A319 SRM 51-42-11.
LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR 65 TO FR 69, Y1292. REPLACED FLOORBEAM BETWEEN FR 65 TO FR 69, Y1292 IAW A319 SRM 51-42-11.
PIT - S4 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM AT FR20, S23R, -Y254. REPAIRED FLOORBEAM AT FR20, S23R, -Y254 IAW A319 SRM 53-00-14.
PIT - S4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, -Y1292. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, -Y1292 IAW A319 SRM 51-72-11 & 51-42-00.
PIT - S4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM SEGMENT BETWEEN FR66 TO FR68, & BETWEEN -Y1167 TO Y1292. REPLACED FLOORBEAM SEGMENT BETWEEN FR66 TO FR68, & BETWEEN -Y1167 TO Y1292 IAW A319 SRM 51-72-11 & 51-42-00.
PIT - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 TO FR67, -Y464. REPLACED FLOORBEAM BETWEEN FR66 TO FR67, -Y464 IAW A319 SRM 51-72-11.
PIT - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOOR BEAM BETWEEN FR66 TO FR67, Y512. REPLACED FLOORBEAM BETWEEN FR66 TO FR67, Y512 IAW A319 SRM 51-72-11.
PIT - S4 - MAJOR REPAIR - CORROSION ON SHEAR WEB BETWEEN FR68 TO FR69, -Y1162.5, S23L. REPAIRED SHEAR WEB BETWEEN FR68 TO FR69, -Y1162.5, S23L IAW A319 SRM 51-42-11.
LEVEL 2 GALVANIC CORROSION ON R-2 DOOR SILL FLOORBEAM AT FR 66, S23R. REPLACED R-2 DOOR SILL FLOORBEAM AT FR 66, S23R IAW A319 SRM 53-41-14.
PIT - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SILL BEAM AT FR66, S23R. REPLACED SILL BEAM AT FR66, S23R IAW A319 SRM 53-41-14.
SHEER WEB CRACKED BETWEEN FR 68 TO FR 69, -Y1162.5, S23R. REPLACED SHEER WEB BETWEEN FR 68 TO FR 69, -Y1162.5, S23R IAW A319 SRM 51-42-11.
CLT - S4 - MAJOR REPAIR - UPPER SURFACE OF CENTER CABIN FLOOR PANEL 232LF DAMAGED. REPLACED CENTER CABIN FLOOR PANEL 232LF.
PIT - S4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR20 TO FR21, Y254. REPLACED FLOORBEAM BETWEEN FR20 TO FR21, Y254 IAW A319 SRM 51-42-11.
CLT - S4 - MAJOR REPAIR - AREA DISBONDED ON RIGHT WING AILERON OUTBOARD LOWER SKIN AT TRAILING EDGE WEDGE. REPAIRED RIGHT WING AILERON OUTBOARD LOWER SKIN AT TRAILING EDGE WEDGE IAW A319 SRM 57-61-21.
PIT - S4 - MAJOR REPAIR - LEVEL 2 FILIFORM CORROSION ON SHEER PLATE BETWEEN FR69 TO FR70, -Y1162.5. REPLACED SHEER PLATE BETWEEN FR69 TO FR70, -Y1162.5 IAW A319 SRM 51-22-00.
LEVEL 2 FILIFORM CORROSION ON SHEER PLATE BETWEEN FR 69 TO FR 70, -Y1162.5, S23R. REPLACED SHEER PLATE BETWEEN FR 69 TO FR 70, -Y1162.5, S23R IAW A319 SRM 51-22-00.
PIT - S2 - MAJOR REPAIR - LEVEL 2 FILIFORM CORROSION ON SHEAR PLATE AT FR70 RIGHT SIDE. REPLACED SHEAR PLATE AT FR70 RIGHT SIDE IAW A319 SRM 51-22-00.
LEVEL 2 CORROSION ON FLOORBEAM AT FR 16, Y505, S23L. REPLACED FLOORBEAM AT FR16, Y505, S23L IAW A319 SRM 51-72-11.
FLT 880 - PHL-BOS - EMERGENCY LIGHTS - EXIT COVER LENS BY 2L DOOR MISSING. REPLACED EXIT COVER LENS AT 2L DOOR.
FLT 1692 - CLT - EEL - FORWARD GALLEY FLASHLIGHT NOT BLINKING. MAINTENANCE INSTALLED NEW BATTERY.
FLT 1660 - CLT-BNA - AIR TURNBACK - CAPTAIN WINDSHIELD ARCED AND THEN CRACKED SHORTLY AFTER TAKEOFF. WINDSHIELD SHATTERED IMMEDIATELY. REPLACED CAPTAIN WINDSHIELD. OPERATIONAL CHECK WAS GOOD.
DCA - THE TEST OF THE EMERGENCY EXIT LIGHT SYSTEM FAILED, FAULTING EPSU EXT LOAD L ON THE FORWARD CIDS PANEL. MAINTENANCE REPLACED THE AFT LEFT EMERGENCY POWER SUPPLY BATTERY, WHICH DID NOT FIX THE PROBLEM. THE AIRCRAFT WAS RELEASED ON MEL. SUBSEQUENTLY, MAINTENANCE FOUND AND CORRECTED A BENT PIN IN THE AFT, RIGHT SLIDE ELECTRICAL HARNESS. OK FOR SERVICE.
SAN - FLT 91 - EN-ROUTE PHL - SAN, THE RIGHT REAR COCKPIT WINDOW CRACKED DURING FLIGHT. THE AIRCRAFT CONTINUED TO SAN AND LANDED WITHOUT FURTHER INCIDENT.
BFM - FOUND FLOOR PANEL CORRODED 3 INCHES LONG BY 2 INCHES WIDE BY .02 INCH DEEP, MAIN DECK FLOOR PANEL 262FF. REMOVED AND REPLACED FLOOR PANEL PER SRM 51-72-11 AND 51-42-11. (M)
MAIN DECK SEAL ANGLES AT PNL 262GF AND 262EG CRACKED AT WELDS. REMOVED AND REPLACED SEAL ANGLES PER SRM 51-72-11 AND 51-42-11. (M)
BFM - FOUND FLOOR PANEL CORRODED 5 INCHES LONG BY 3 INCHES WIDE BY .02 INCH DEEP AREA, MAIN CABIN 261FF. REMOVED AND REPLACED FLOOR PANEL PER SRM 51-72-11 AND 51-42-11. (M)
BFM - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH BY .02 AND .03, TWO AREAS, FS 66-68, Y1292, -Z240. REMOVED AND REPLACED FLOORBEAM PER SRM 53-00-14, 51-74-00 AND 51-42-11. REMOVED AND REPLACED BEAM PER SRM 53-00-14, 51-74-00 AND 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. REMOVED AND REPLACED BEAM PER SRM 53-00-14, 51-74-00 AND 51-42-11. (M)
BFM - FOUND PLATE ASSEMBLY CORRODED 5 INCHES BY 1.6 INCHES BY .020 INCH AREA, FRAME 20, -Z240, -Y765. REMOVED AND REPLACED PLATE ASSEMBLY PER SRM 53-11-14 AND 51-72-11. CORROSION LEVEL 2, TASK NR JA-220-53500. (M)
BFM - FOUND FLOOR PANEL CORRODED 1 INCH WIDE BY .015 DEEP ENTIRE LENGTH, MAIN CABIN, PNI 222FF. REPLACED WITH NEW PANEL PER SRM 51-72-11. (M)
BFM - FOUND BEAM CORRODED 1 INCH BY 1 INCH BY .039 INCH DEEP, FRAME 68, Y1162, -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)
BFM - FOUND FLOOR PANEL CORRODED 1 INCH BY 1 INCH WIDE BY .02 INCHES DEEP AREA, MAIN CABIN, PANEL 221FF. REPLACED WITH NEW PANEL PER SRM 51-72-11. (M)
BFM - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH BY .048D AREA, FRAME 68 Y 1292 -Z240. REMOVED AND REPLACED FLOORBEAM PER SRM 51-74-00, 53-00-14 AND 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)
BFM - FOUND SEAT TRACK/BEAM ASSEMBLY CORRODED 1 INCH LONG BY .040 INCH WIDE BY .119 INCH DEEP, FRAME 24, -Y 1292, -Z 240. INSTALLED SEAT TRACK SPLICE/DOUBLER REPAIR PER SRM 53-00-15 AND SRM 42-11, 53-43-1. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)
BFM - FOUND SILL CORRODED .110 INCH BY .190 INCH BY .070 INCH DEEP, FRAME 68, Y1420, -Z240. REMOVED AND REPLACED SILL PER SRM 51-41-14. CORRODED LEVEL 2, TASK NR JA 260-53500. (M)
BFM - FOUND FLOORBEAM CORRODED 3 INCHES BY 1 INCH BY .050 INCH AREA, FRAME 68-69, -Y1210, -Z2240. REMOVED AND REPLACED FLOORBEAM PER SRM 53-00-14, 51-74-00, 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)
BFM - FOUND SILL CORRODED 2 INCHES BY 1.3 INCHES BY .070 INCH DEEP, FRAME 66, Y 1502, -Z240. REMOVED AND REPLACED SILL PER SRM 53-41-14. CORROSION LEVEL 2, TASK NR JA 260-53500. (M)
BFM - FOUND PLATE CORRODED 2 INCHES BY 1 INCH BY .17 INCH DEEP, FS 69-70, -Y1292, -Z240. REMOVED AND REPLACED SHEAR PLATE PER SRM 53-41-17, 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)
BFM - FOUND PLATE ASSEMBLY CORRODED 1.2 INCHES BY .8 INCHES BY .020 INCH AREA, FRAME 68, Y1502, -Z240. REMOVED AND REPLACED PLATE ASSEMBLY PER SRM 51-74-00, 51-42-11, 53-41-49. CORROSION LEVEL 2, TASK NR JA-160-53500. (M)
BFM - FOUND BEAM CORRODED 1.8 INCHES BY 1.4 INCHES BY .060 INCH AREA, FRAME 66-68, -Y1220, -Z240. REMOVED AND REPLACED BEAM PER SRM 53-00-14, 51-74-00, 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)
BFM - FOUND BEAM CORRODED 1.8 INCHES BY 1.4 INCHES BY .060 INCH AREA, FRAME 64, -Y1270, -Z240. REMOVED AND REPLACED BEAM. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)
BFM - FOUND SILL SHAPE CORRODED 2 INCHES BY .50 INCH BY .02 INCH AREA, BETWEEN FRAME 66 AND 68, Y +1732, -Z240. REMOVED AND REPLACED SILL SHAPE PER SRM 51-74-00 AND 53-41-79. (M)
BFM - FOUND SCUFF PLATE SUPPORT CORRODED .57 INCH DEEP BY .70 INCH WIDE BY 3 INCHES LONG, FS 68, Z=-240, Y=-1420. REMOVED AND REPLACED SCUFF PLATE SUPPORT PER SRM 51-74-00 AND 53-41-69. (M)
PIT - FOUND SHEAR PLATE WORN/CHAFED 1 INCH BY 1 INCH IN FOUR AREAS, FRAME 69-70 Y1292, Z-240. REPLACED SHEAR PLATE PER SRM 53-41-17 AND 51-42-11. LEVEL 2, TASK NR JA-260-53500. (M)
BFM - FOUND FLOORBEAM CORRODED 1 INCH IN DIAMETER BY .030 INCH DEEP, LAV E MOUNTHOLE, -Y720, 10 INCHES AFT OF FRAME 64 ON BEAM ASSEMBLY. REMOVED AND REPLACED FLOORBEAM PER SRM 53-00-14, 51-42-11. (M)
FOUND FLOORBEAMBEAM WORN 1 INCH BY 1 INCH BY .070 INCH, FRAME 66 Y-254, -Z240. REMOVED AND REPLACED BEAM PER SRM 53-00-14, 51-42-11. (M)
BFM - FOUND TRACK CORRODED 1.6 INCHES LONG BY 1.0 INCH WIDE BY .068 INCH DEEP AREA, BETWEEN FRAME 12-24 BL Y765. REMOVED AND REPLACED SEAT TRACK PER SRM 51-42-11, 51-74-00, 53-11-14. CORROSION LEVEL 2 TASK NR JA-220-53500. (M)
BFM - FOUND TRACK CORRODED 1.3 INCHES BY 1.1 INCHES BY .043 INCH AREA, MAIN DECK SEAT TRACK, FRAME 16, Y 1252, -Z240. REMOVED AND REPLACED SEAT TRACK PER SRM 51-42-11, SRM 53-11-14. CORROSION LEVEL 2, TASK NR JA-220-53500. (M)
BFM - FOUND SEAT TRACK ASSEMBLY CORRODED .1 INCH BY 1 INCH BY .49 INCH DEEP, FS 66 Y765, -Z35. REMOVED AND REPLACED SEAT TRACK ASSEMBLY PER SRM 51-74-00, 53-00-14, 51-42-00 AND 51-23-01. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)
BFM - FOUND LONGITUDINAL FLOOR SUPPORT CORRODED 2.3 INCHES LONG BY 1.7 INCHES WIDE BY .070 INCH DEEP AREA, BETWEEN FRAME 66/70, -Y 800MM. REPLACED LONGITUDINAL FLOOR SUPPORT PER SRM 51-42-11, SRM 53-00-14 AND SRM 51-74-00. CORRODED LEVEL 2, TASK NR JA-260-53500. (M)
BFM - FOUND TRACK CORRODED 2.7 INCHES BY 1.1 INCH BY .053 INCH DEEP, FRAME 15, Y=503.2, Z=-240. REMOVED AND REPLACED TRACK PER SRM 53-11-14, FIG 106, 51-42-11, 51-74-00. CORROSION LEVEL 2, TASK NR JA-220-53500. (M)
AT APPROX FL260, DURING DESCENT, NR 2 ENG STALLED & LOST POWER. FELT A VIBRATION AS N1 DECREASED FROM 90 TO 50 PERCENT. THROTTLE PULL BACK STOPPED VIBRATION. COMMAND INDICATED APPROX 40 PERCENT, BUT ENGINE THRUST INDICATED 20 PERCENT. THROTTLE ADVANCED SLOWLY, NO RESPONSE RECEIVED FROM OTHER INDICATIONS. RECEIVED A 'ENG 2 STALL' ECAM MESSAGE. SHUTDOWN NR 2 ENG. FLT CONTINUED & LANDED WITHOUT INCIDENT. TOTAL SINGLE ENG TIME 15 MINS. MX REPLACED NR 2 ENG IP CHECK VALVE. INSPECT NR 2 ENG MAG CHIP DETECT FOR METAL, DUE TO POPPED CHIP DETECTOR. NO METAL FOUND. RESET CHIP DETECTOR. PERFORMED AN ENG BORESCOPE. NO FAULTS FOUND. RAN ENG & OPS CHECKED BLEED SYSTEM. OK FOR SERVICE. (M)
PIT - AN 'EPSU BATT EMER R' MESSAGE CAME ON DURING THE EMERGENCY LIGHTS TEST. REPLACED RIGHT EMERGENCY POWER SUPPLY UNIT BATTERY. OPERATIONALLY CHECKED OK. (M)
PIT-SAN - FLT 89 - AFTER DEPARTING PIT, AND CLIMBING THROUGH FL160, AND ELECTRICAL ODOR WAS REPORTED IN THE COCKPIT. THE FLIGHT RETURNED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE RAN THE AIR CONDITIONING PACKS WITH BOTH THE APU AND ENGINES. CHECKS OK FOR SERVICE. (M)
DEN/PHL - FLT 140 - AFTER TAKEOFF, FLIGHT CREW WAS ALERTED TO A LEFT ENGINE N2 OVERSPEED. THE LEFT ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO THE FIELD. 28 MINUTES SINGLE ENGINE TIME. MAINTENANCE REPLACED THE LEFT ENGINE.