N722US
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: RIGHT OVERWING EXIT, EMERGENCY EXIT SIGN STAYS ON. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 12WL PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING WITH NO ISSUES NOTED.
AIRCRAFT WAS GROUNDED: BATTERY FAULT FOR LEFT EMERGENCY POWER SUPPLY UNIT DISPLAYED DURING SYSTEM TEST. REPLACED BATTERY PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO FAULTS NOTED.
AIRCRAFT WAS GROUNDED: FAULT FOR FORWARD LEFT EMERGENCY POWER SUPPLY UNIT DISPLAYED DURING SYSTEM TEST. MAINTENANCE REPLACED THE FORWARD LEFT EMERGENCY POWER SUPPLY UNIT (AALA202606290298) AND BATTERY (AALA202606291081) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.
AIRCRAFT WAS GROUNDED: FAULT FOR RIGHT EMERGENCY POWER SUPPLY UNIT DISPLAYED DURING SYSTEM TEST. REPLACED EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO FAULTS NOTED.
AIRCRAFT WAS GROUNDED: FAULT FOR FORWARD LEFT EMERGENCY POWER SUPPLY UNIT DISPLAYED DURING SYSTEM TEST. MAINTENANCE REPLACED THE FORWARD LEFT EMERGENCY POWER SUPPLY UNIT (AALA202606290298) AND BATTERY (AALA202606291081) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.
AIRCRAFT IN BASE MAINTENANCE: R1 DOOR SLIDE RAFT PARACHUTE PIN IS BENT AND PACK SWELLED. REPLACED SLIDE RAFT ASSEMBLY PER JOB CARD 26L00025011.
AIRCRAFT IN BASE MAINTENANCE: RIGHT FORWARD DOOR EMERGENCY ESCAPE SLIDE RED PULL HANDLES ARE NOT ATTACHED TO SLIDE. MAINTENANCE REATTACHED THE HANDLES PER CMM 25-61-20.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON STRINGER AT FR 65 AND S31R. REPLACED STRINGER PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE: LEFT MAIN LANDING GEAR TORQUE LINK APEX PIN SHOWS SIGNS OF WEAR & CORROSION. REPLACED APEX PIN IAW AMM 32-11-29.
AIRCRAFT IN BASE MAINTENANCE: RIGHT AFT PASSENGER DOOR UPPER LOCKING HOOK ROLLER BUSHING SEIZED. MAINTENANCE LUBRICATED ROLLER BUSHING PER AMM 52-13-31.
AIRCRAFT IN BASE MAINTENANCE: LEFT FORWARD DOOR 831 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
AIRCRAFT WAS GROUNDED: BRAKES ARE VERY GRABBY, EXHIBITING WARPED LIKE LURCHING WHEN COLD AT LOW SPEED. MAINTENANCE REPLACED THE YELLOW HYDRAULIC SYSTEM ALTERNATE BRAKING UPPER TRANSDUCER PER AMM 32-44-18. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ISSUES NOTED.
AIRCRAFT WAS NOT GROUNDED: PERFORMED EMERGENCY LIGHT TEST ON PTP PANEL 110 RH AND RECEIVEDNMESSAGE ATA 33-51-38 EPSU BATTERY AFT L. MAINTENANCE REPLACED AFT EPSU BATTERY IAW AMM 33-51-38.
AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT BATTERY DRAINED AT AFT FA JUMPSEAT. MAINTENANCE REPLACE FLASHLIGHT BATTERY IAW AMM 25-65-00.
AIRCRAFT IN BASE MAINTENANCE: L1 DOOR ASSIST BOTTLE PRESSURE BELOW PS LIMIT. MAINTENANCE SERVICED L1 DOOR ASSIST BOTTLE TO PROPER PRESSURE PER AMM 52-10-00.
AIRCRAFT IN BASE MAINTENANCE: ROTO PROBE INDICATES THERE IS A CRACK RIGHT AFT MLG DOOR ACTUATOR FITTING. MAINTENANCE REPLACED RIGHT AFT MLG DOOR ACTUATOIR FITTING IAW EA 365179 & SRM 53-35-11.
AIRCRAFT WAS GROUNDED: AFTER APU BLEED AIR ON, DIRTY SOCKS SMELL IN ENTIRE AIRCRAFT DURING CRUISE. NO INJURIES REPORTED. MAINTENANCE FOUND EVIDENCE OF OIL LEAK AT APU COOLING FAN AND REPLACED APU COOLING FAN IAW AMM 49-52-51.
AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANTS IN AFT SECTION OF THE AIRCRAFT REPORTED FUMES ON DESCENT. MAINTENANCE FOUND THE AIRCRAFT BELLY WAS SOAKED AND DIRTY WITH HYDRAULIC FLUID WHICH MAY HAVE BEEN INGESTED BY THE APU. MAINTENANCE ALSO NOTED THAT HYDRAUILIC FLUID WAS COMING OUT OF THE FUSELAGE DRAINS. MAINTENANCE FOUND THE EMERGENCY GENERATOR LEAKING FROM THE CASE DRAIN AND REPLACED IT PER AMM 24-24-51. (AALA202409239628) MAINTENANCE ALSO FOUND THE FORWARD CARGO DOOR SELECTOR VALVE WAS LEAKING AND REPLACED IT PER AMM 52-36-12. (AALA202409231678) A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANTS IN AFT SECTION OF THE AIRCRAFT REPORTED FUMES ON DESCENT. MAINTENANCE FOUND THE AIRCRAFT BELLY WAS SOAKED AND DIRTY WITH HYDRAULIC FLUID WHICH MAY HAVE BEEN INGESTED BY THE APU. MAINTENANCE ALSO NOTED THAT HYDRAUILIC FLUID WAS COMING OUT OF THE FUSELAGE DRAINS. MAINTENANCE FOUND THE EMERGENCY GENERATOR LEAKING FROM THE CASE DRAIN AND REPLACED IT PER AMM 24-24-51. (AALA202409239628) MAINTENANCE ALSO FOUND THE FORWARD CARGO DOOR SELECTOR VALVE WAS LEAKING AND REPLACED IT PER AMM 52-36-12. (AALA202409231678) A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS GROUNDED: L1 DOOR GUST LOCK WON'T HOLD DOOR OPEN. REPLACED FORWARD L1 DOOR GUST LOCK CONTROL PIN GUIDE PER AMM 52-11-12.
AIRCRAFT WAS GROUNDED: 2R DOOR ARMING LEVER DIFFICULT TO ARM. MAINTENANCE FOUND THE AFT GIRT BAR HITTING THE FLOOR AND NOTED DOOR SAGGING. DURING OPEN UP THE DOOR GIRT BAR HIT THE FLOOR AND THE SLIDE CAME LOOSE FROM THE PACK. MAINTENANCE LUBRICATED THE EMERGENCY ESCAPE SLIDE RELEASE MECHANISM FLEXIABLE CONTROL (AALA202311221601) AND REPLACED THE SLIDE RAFT ASSEMBLY (AALA202311228195) ON THE THE R2 DOOR. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS GROUNDED: 2R DOOR ARMING LEVER DIFFICULT TO ARM. MAINTENANCE FOUND THE AFT GIRT BAR HITTING THE FLOOR AND NOTED DOOR SAGGING. DURING OPEN UP THE DOOR GIRT BAR HIT THE FLOOR AND THE SLIDE CAME LOOSE FROM THE PACK. MAINTENANCE LUBRICATED THE EMERGENCY ESCAPE SLIDE RELEASE MECHANISM FLEXIABLE CONTROL (AALA202311221601) AND REPLACED THE SLIDE RAFT ASSEMBLY (AALA202311228195) ON THE THE R2 DOOR. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS NOT GROUNDED: ARMING LEVER ON DOOR 2R IN AFT IS HARD TO MOVE. LUBED ARMING LEVER AT 2R DOOR
AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT 2L JUMPSEAT FLASHLIGHT NOT FLASHING. REPLACED BATTERY PACK ON 2R FLIGHT ATTENDANT FLASHLIGHT.
AIRCRAFT IN BASE MAINTENANCE: PASSENGER CREW DOOR 841 SLIDE SAFETY PIN HOLES DO NOT NOT ALIGN PREVENTING THE SLIDE FROM BEING DE-ACTIVATED. REPLACED SLIDE RAFT ASSEMBLY PER TASK CARD 26L00025007.
AIRCRAFT IN BASE MAINTENANCE: LEFT HAND MAIN LANDING GEAR DOOR FORWARD HINGE HAS EXCESSIVE PLAY. REPLACED HINGE PER CMM 52-81-18.
AIRCRAFT IN BASE MAINTENANCE: RIGHT PYLON FORWARD SHACKLE AFT ATTCH FITTING WORN. REPLACED ATTACH FITTING PER TASK CARD 26C42554028.
AIRCRAFT IN BASE MAINTENANCE: DEFORMATION OF SLIDE RAFT PASSENGER AT CREW DOOR 832. REPLACED SLIDE RAFT PER JOB CARD 26C83252008.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING PYLON AFT SHACKLE AFT ATTACH FITTING AT PYLON STATION 8293 AND PYLON RIB 10. REPLACED ATTCH FITTING PER AMM 54-51-17.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING FUEL TANK ACCESS PANEL 640KB COUNTERSINK FASTENER HOLE BETWEEN RIBS 15 AND 16. REPLACED ACCESS PANEL PER SRM 57-27-11.
AIRCRAFT IN BASE MAINTENANCE: DON'T PASS OPERATIONAL TEST DAMPER PASSENGER CREW DOOR 842 (DAMPING FUNCTION) AT AFT GALLEY AREA. REPLACED DOOR DAMPER PASSENGER CREW DOOR 842 PER AMM 52-13-14-000-001-B AND AMM 52-13-14-400-001-B AND PERFORMED OPERATIONAL TEST DOOR DAMPING FUNCTION PER AMM 52-10-00-710-001-A TEST IS OK.
AIRCRAFT IN BASE MAINTENANCE FLIGHT DECK WINDSHIELD FRAMING RIGHT HAND CONTINUITY FITTING REPORTED AS CRACKED AND REQUIRES REPLACEMENT AS PART OF THE MAJOR REPAIR BEING ACCOMPLISHED TO THE FLIGHT DECK WINDSHIELD FRAMES PER EA 345442. REPLACED CONTINUITY FITTING PER EA 345442.
AIRCRAFT IN BASE MAINTENANCE FLIGHT DECK WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING REPORTED AS CRACKED AND REQUIRES REPLACEMENT AS PART OF THE MAJOR REPAIR BEING ACCOMPLISHED TO THE FLIGHT DECK WINDSHIELD FRAMES PER EA 345442. REPLACED CONTINUITY FITTING PER EA 345442.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING MAIN LANDING GEAR RETRACTION ACTUATOR ANCHORAGE / JACK FITTING BETWEEN WS 70 AND 141, BETWEEN RIBS 2 AND 3. REPAIRED ANCHORAGE FITTING / JACK FITTING PER SRM 57-26-13-300-025.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK 10 LOWER AFT BOLT BETWEEN WS 11198 AND WS 11664, BETWEEN RIBS 21 AND 22. REPLACED BOLT PER AMM 27-84-66.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #5 UPPER BOLT BETWEEN WS 4862 AND 5512, BETWEEN RIBS 9 AND 10. REPLACED BOLT PER AMM 27-84-64.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #5 LOWER BOLT BETWEEN WS 4862 AND 5512, BETWEEN RIBS 9 AND 10. REPLACED BOLT PER AMM 27-84-64.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK 2 MID AFT BOLT BETWEEN WS 1406 AND WS 1957, BETWEEN RIBS 3 AND 4. REPLACED BOLT PER AMM 27-84-63.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #1 LOWER BOLT BETWEEN WS 700 AND WS 1406, BETWEEN RIBS 2 AND 3. REPLACED BOLT PER TASK CARD 26C51057005.
AIRCRAFT IN BASE MAINTENANCE: DON'T PASS OPERATIONAL TEST PASSENGER CREW DOOR 841 DAMPER (DAMPING FUNCTION) AT FORWARD GALLEY AREA. REPLACED DAMPER PER AMM 52-11-14.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING MAIN LANDING GEAR RETRACTION ACTUATOR ANCHORAGE / JACK FITTING BETWEEN WS 70 AND 141, BETWEEN RIBS 2 AND 3. REPAIRED ANCHORAGE FITTING / JACK FITTING PER SRM 57-26-13-300-025.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #10 LOWER FORWARD BOLT BETWEEN WS 11198 AND WS 11664, BETWEEN RIB 21 AND 22. REPLACED BOLT PER AMM 27-84-66.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #10 LOWER MID BOLT BETWEEN WS 11198 AND WS 11664, BETWEEN RIB 21 AND 22. REPLACED BOLT PER AMM 27-84-66.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #9 LOWER BOLT BETWEEN WS 10204 AND WS 10279, BETWEEN RIB 19 AND 20. REPLACED BOLT PER AMM 27-84-66.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #7 LOWER BOLT BETWEEN WS 7316 AND WS 7792, BETWEEN RIB 13 AND 14. REPLACED BOLT PER AMM 27-84-65.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #5 UPPER BOLT BETWEEN WS 4862 AND WS 5512, BETWEEN RIB 9 AND 10. REPLACED BOLT PER TASK CARD 26C61057005.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #6 LOWER AFT BOLT BETWEEN WS 6132 AND WS 6699, BETWEEN RIB 11 AND 12. REPLACED BOLT PER AMM 27-84-64.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #3 LOWER BOLT BETWEEN WS 1957 AND WS 2580, BETWEEN RIBS 4 AND 5. REPLACED BOLT PER AMM 27-84-63.
AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND MAIN LANDING GEAR DOOR FORWARD HINGE HAS EXCESSIVE PLAY. REPLACED HINGE PER CMM 52-81-18.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL AT FR 68 AND S23R. REPAIRED LOWER SILL PER SRM 53-41-14-300-001.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #2 MID FORWARD BOLT BETWEEN WS 1406 AND WS 1957, BETWEEN RIB 3 AND 4. REPLACED BOLT PER TASK CARD 26C61057005.
AIRCRAFT IN BASE MAINTENANCE: RIGHT WING TRAILING EDGE INBOARD FLAP ATTACH FITTING / BRACKET FOR THE INTERCONNECTING STRUT IS WORN ON THE OUTBOARD SIDE OF THE FLAP BETWEEN RIBS 8 AND 9. REPLACED ATTACH FITTING / BRACKET PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: LEFT WING TRAILING EDGE INBOARD FLAP ATTACH FITTING / BRACKET FOR THE INTERCONNECTING STRUT IS WORN ON THE OUTBOARD SIDE OF THE FLAP BETWEEN RIBS 8 AND 9. REPLACED ATTACH FITTING / BRACKET PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CRACKED LEFT HAND MAIN LANDING GEAR DOOR FORWARD HINGE FITTING ON THE KEETL BEAM BETWEEN FR 42 AND FR 43 AT S36L. REPLACED HINGE FITTING PER EA 347005.
AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND MAIN LANDING GEAR DOOR FORWARD HINGE FITTING FORWARD FACE CRACKED ON THE KEEL BEAM BETWEEN FR 42 AND FR 43 AT S36R. REPLACED HINGE FITTING PER EA 346975.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING #1 SPOILER CENTER HINGE INBOARD PIN. REPLACED INBOARD HINGE PIN PER TASK CARD 26C58227003
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING #1 SPOILER CENTER HINGE OUTBOARD PIN. REPLACED OUTBOARD HINGE PIN PER TASK CARD 26C58227003
AIRCRAFT IN BASE MAINTENACE: CORROSION ON RIGHT WING FUEL ACCESS PANEL 640MB COUNTERSINK FASTENER HOLE BETWEEN RIBS 17 AND 18. REPLACED ACCESS PANEL PER SRM 57-27-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING FUEL TANK ACCESS PANEL 540MB COUNTERSINK FASTENER HOLES. REPLACED ACCESS PANEL 540MB PER SRM 57-27-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING FUEL TANK ACCESS PANEL 640JB COUNTERSINK FASTENER HOLE BETWEEN RIBS 14 AND 15. REPLACED ACCESS PANEL PER SRM 57-27-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING FUEL TANK ACCESS PANEL 640LB COUNTERSUNK FASTENER HOLES BETWEEN RIBS 16 AND 17. REPLACED ACCESS PANEL PER SRM 57-27-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING FUEL TANK ACCESS PANEL 540KB COUNTERSUNK FASTENER HOLES BETWEEN RIBS 15 AND 16. REPLACED ACCESS PANEL PER SRM 57-27-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING FUEL TANK ACCESS PANEL 540LB COUNTERSUNK FASTENER HOLES BETWEEN RIBS 16 AND 17. REPLACED ACCESS PANEL PER SRM 57-27-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING FUEL TANK ACCESS PANEL 540HB COUNTERSUNK FASTENER HOLES BETWEEN RIBS 13 AND 14. REPLACED ACCESS PANEL PER SRM 57-27-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING FUEL TANK ACCESS PANEL / DOOR 540NB COUNTERSINK FASTENER HOLE BETWEEN RIB 18 AND 19. REPLACED LEFT WING FUEL TANK ACCESS PANEL / DOOR 540NB PER SRM 51-72-11
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING REAR SPAR TOP SKIN PANEL #2 LOWER SURFACE AT RIB 16 + 2.700 INCHES AND S17. REPAIRED SKIN PANEL PER EA 345663.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING REAR SPAR TOP SKIN PANEL #2 LOWER SURFACE AT RIB 15 + 8.650 INCHES AND S17. REPAIRED SKIN PANEL PER EA 345663.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING REAR SPAR TOP SKIN PANEL #2 LOWER SURFACE AT RIB 18 + 14.700 INCHES AND S17. REPAIRED SKIN PANEL PER EA 345663.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING REAR SPAR TOP SKIN PANEL #2 LOWER SURFACE AT RIB 15 AND S17. REPAIRED SKIN PANEL PER EA 345663.
AIRCRAFT IN BASE MAINTENANCE: AFT AVIONICS COMPARTMENT RACK 80VU LOWER LEFT LATERAL FORK END WORN AT FR 24 AND S32L. REPLACED FORK END PER EA 345511.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER AFT CORNER SHAPE FITTING AT FR 68 AND S23R. REPLACED AFT CORNER SHAOE FITTING PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE: AFT AVIONICS COMPARTMENT RACK 80VU LOWER RIGHT LATERAL FORK END WORN AT FR 24 AND S32R. REPLACED FORK END PER EA 345511.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING REAR SPAR TOP SKIN PANEL #2 LOWER SURFACE AT RIB 16 AND S17. REPAIRED SKIN PANEL PER EA 345663.
AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE AT FR 69 AND S23L. REPLACED SHEAR PLATE PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT AFT PASSENGER / CREW DOOR CUTOUT LOWER CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23R. REPLACED CENTER SHAPE FITTING PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE AT FR 69 AND S23R. REPLACED SHEAR PLATE PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT DOOR CUTOUT LOWER SILL COVER SHEET BETWEEN FR 55A AND FR 59 AT S38R. REPAIRED COER SHEET PER EA 346203.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUTOUT LOWER AFT CORNER SHAPE FITTING AT FR 68 AND S23L. REPLACED CORNER SHAPE FITTING PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUTOUT LOWER CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23L. REPLACED CENTER SHAPE FITTING PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSSENGER / CREW DOOR CUTOUT LOWER SILL AT FR 66 AND S23R. REPAIRED LOWER SILL PER SRM 53-41-14-300-001.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR SEAT SEAT TRACK AT FR 20 AND +Y1292. REPLACED SEAT TRACK PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR SEAT TRACK AT FR 20 AND -Y765. REPLACED SEAT TRACK PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR DUMMY RAIL BETWEEN FR 12 AND FR 13 AT -Y81. REPLACED DUMMY RAIL PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: DON'T PASS OPERATIONAL TEST PASSENGER CREW DOOR 831 DAMPER (DAMPING FUNCTION) AT FORWARD GALLEY AREA. REPLACED PASSENGER CREW DOOR 831 DAMPER AT FORWARD GALLEY AREA PER AMM 52-11-14-000-001-B AND AMM 52-11-14-400-001-B.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR SEAT TRACK BETWEEN FR 20 AND FR 22 AT -Y1292. REPLACED SEAT TRACK PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT DOOR CUTOUT LOWER THRESHOLD SHEET BETWEEN FR 55A AND FR 59 AT S38R. REPLACED THRESHOLD SHEET PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUTOUT LOWER SILL LEFT AT FR 68 AND S23L. REPLACED LOWER SILL PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT FR 35 AND S30L REPAIRED FRAME PER EA 345336.
AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD FRAME CENTER POST LOWER NODE ATTACTMENT, INTERNAL AREA INBOARD FLANGE. LEFT HAND UPPER TENSION BOLT AT FR 2 AND Y0 LEFT. REPAIRED FRAME PER EA 345442.
AIRCRAFT IN BASE MAINTENANCE: DONT PASS OPERATIONAL TEST DAMPER PASSENGER CREW DOOR 832 IN PASSENGER CABIN. REPLACED PASSENGER CREW DOOR 832 DAMPER AT AFT GALLEY AREA
AIRCRAFT IN BASE MAITENANCE : CRACKED FLIGHT DECK WINDSHIELD FRAME CENTER POST LOWER NODE ATTACTMENT, INTERNAL AREA INBOARD FLANGE RIGHT HAND SIDE, LOWER INBOARD RADIUS AS WELL AS AT THE UPPER TENSION BOLT AT FR 2 AND Y0 RIGHT. REPAIRED FRAME PER EA 345442
AIRCRAFT IN BASE MAINTENANCE: CRACKED FAME WEB AFT FACE HORIZONTAL FLANGE LOWER RADIUS AT FR 68 AND S22L. REPAIRED FRAME PER EA 345466.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING REAR SPAR TOP SKIN PANEL #2 LOWER SURFACE AT RIB 19 AND S11. REPAIRED SKIN PANEL PER EA 345663.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING REAR SPAR TOP SKIN PANEL #2 LOWER SURFACE AT RIB 17 AND S11. REPAIRED SKIN PANEL PER EA 345663.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING REAR SPAR TOP SKIN PANEL #2 LOWER SURFACE AT RIB 13 AND S17. REPAIRED SKIN PANEL PER EA 345663.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING REAR SPAR TOP SKIN PANEL #2 LOWER SURFACE AT RIB 18 AND S17. REPAIRED SKIN PANEL PER EA 345663.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING REAR SPAR TOP SKIN PANEL #2 LOWER SURFACE AT WX3622 AND RIB 7. REPAIRED SKIN PANEL PER EA 345663.
AIRCRAFT WS NOT GROUNDED: L1 DOOR GUST LOCK DOES NOT WORK. MAINTENANCE REMOVED DEBRIS AND LUBED L1 DOOR GUST LOCK MECHANISM PER AMM 52-11-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS GROUNDED: L4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER/ACCUMULATOR PRESSURE LOW. MAINTENANCE SERVICED L4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER/ACCUMULATOR PER AMM 52-10-00.
AIRCRAFT WAS GROUNDED: L4 DOOR ESCAPE SLIDE PRESSURE GAGE NEEDLE READS ON "RED" BAND. MAINTENANCE REPLACED THE ESCAPE SLIDE PER TASK CARD 26L00025011.
AIRCRAFT WAS NOT GROUNDED: AFT CARGO COMPARTMENT FLOOR PANEL AT DOOR PEELING UP. MAINTENANCE REPLACED FLOOR PANEL PER AMM 53-42-14.
AIRCRAFT WAS NOT GROUNDED: DOOR 2L SLIDE DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED L2 DOOR SLIDE DOOR ASSIST BOTTLE PRESSURE PER AMM 52-10-00.
AIRCRAFT WAS GROUNDED: SLIGHT MUSTY ODOR ON DECENT SIMILAR CRAYONS OR WAX THAT WENT AWAY WITH NO ACTION BEING TAKEN BY THE FLIGHT CREW. THE ODOR RETURNED AFTER LANDING DURING TAXI IN AND AT THE GATE. MAINTENANCE FOUND EVIDENCE OF AN OIL LEAK ON THE APU. MAINTENANCE REPLACED THE APU OIL COOLIING FAN THAT WAS LEAKING OIL PER AMM 49-52-51. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ODORS NOTED.
AIRCRAFT WAS GROUNDED: SLIGHT MUSTY ODOR ON DECENT SIMILAR CRAYONS OR WAX THAT WENT AWAY WITH NO ACTION BEING TAKEN BY THE FLIGHT CREW. THE ODOR RETURNED AFTER LANDING DURING TAXI IN AND AT THE GATE. MAINTENANCE FOUND EVIDENCE OF AN OIL LEAK ON THE APU. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR DIFFICULT TO OPEN BOUND UP DEADBOLT. MAINTENANCE ACCOMPLISHED ADJUSTMENT AND TEST OF FLIGHT DECK DOOR PER AMM 52-51-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS GROUNDED: UN-COMMANDED PITCH OSCILLATIONS OF UP TO +400 -200 VV1 AT CRUISE ALT FL210 , AUTOPILOT 1 +2. MAINTENANCE REPLACED ELEVATOR SERVO CONTROL 34CE1 AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER AMM 27-34-51.
AIRCRAFT WAS GROUNDED: AIRCRAFT PITCHED UP AND DOWN EXCESSIVELY AT CRUISE ALTITUDE WITH AUTOPILOT ENGAGED, AUTOPILOT ONE AND TWO. PITCHED OSCILLATION BETWEEN 40 - 100 FPM. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
AIRCRAFT WAS GROUNDED: AIRCRAFT PITCHED UP AND DOWN EXCESSIVELY AT CRUISE ALTITUDE WITH AUTOPILOT ENGAGED, AUTOPILOT ONE AND TWO. PITCHED OSCILLATION BETWEEN 40 - 100 FPM. **SUPPLEMENTAL REPORT FOR AALA202209022146: MAINTENANCE REPLACED SOLENOID VALVE ON LEFT HAND GREEN ELEVATOR SERVO CONTROL ACTUATOR PER AMM 27-34-51. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED. ** (CLOSED)
AIRCRAFT WAS GROUNDED: ELEVATOR FLIGHT CONTROL ISSUE. AIRCRAFT WOULD PITCH UP AND DOWN V/SUP AND DOWN + OR - 100FT. COULD HEAR AND FEEL THE ELEVATOR PITCH UP AND DOWN. OBSERVED ELEVATOR PITCH MOVEMENTS ON FLIGHT CONTROL PAGE. OCCURRED APPROX 15 PLUS TIMES BETWEEN TAKEOFF AT IAH AND LANDING AT LIT. PITCH MOVEMENTS WERE NOTICEABLE BY FLIGHT ATTENDANTS IN BACK. NO ECAM MESSAGE. THE AIRCRAFT DIVERTED TO LIT WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. **SUPPLEMENTAL REPORT FOR AALA202209024347: MAINTENANCE ACCOMPLISHED A GROUND SCAN WHICH SHOWED SEC2 OR WIRING FROM LEFT ELEVATOR POSITION MONITORING TRANSDUCER (49CE1) FAULT. FOUND CANNON PLUG ON TRANSDUCER LOOSE / DISLODGED AND RE-SECURED IT. A SATISFACTORY GROUND SCAN WAS ACCOMPLISHED AND FAULT CLEARED. ** (CLOSED)
AIRCRAFT WAS GROUNDED: ELEVATOR FLIGHT CONTROL ISSUE. AIRCRAFT WOULD PITCH UP AND DOWN V/SUP AND DOWN + OR - 100FT. COULD HEAR AND FEEL THE ELEVATOR PITCH UP AND DOWN. OBSERVED ELEVATOR PITCH MOVEMENTS ON FLIGHT CONTROL PAGE. OCCURRED APPROX 15 PLUS TIMES BETWEEN TAKEOFF AT IAH AND LANDING AT LIT. PITCH MOVEMENTS WERE NOTICEABLE BY FLIGHT ATTENDANTS IN BACK. NO ECAM MESSAGE. THE AIRCRAFT DIVERTED TO LIT WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
AIRCRAFT WAS GROUNDED: L1 DOOR GUST LOCK ENGAGES BUT DOES NOT LOCKS. ALSO, DOOR LACKS SNUBBER EFFECT. REMOVED AND REPLACED WORN GUST LOCK MECHANISM SPRING PER AMM 52-11-12.
AIRCRAFT WAS NOT GROUNDED: STRAP HANGING DOWN FROM SLIDE AT 2L DOOR AND HANGS OUTSIDE AIRCRAFT WHEN DOOR IS CLOSED. SECURED STRAP ON 2L DOOR SLIDE COVER. PER AMM 25-62-50.
AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS 2R DOOR VERY DIFFICULT TO ARM AND OPERATE. CLEANED AND LUBRICATED 2R DOOR GIRT BAR SPRINGS PER AMM 12-22-52.
AIRCRAFT WAS NOT GROUNDED: FIRST OFFICER'S EMERGENCY DESCENT ROPE COVER INOPERATIVE. RE-SECURED ROPE COVER PER AMM 25-13-41.
AIRCRAFT WAS NOT GROUNDED: FORWARD GALLEY OVEN HAS A STRONG BURNT PLASTIC SMELL, AFFECTS FOOD TASTE. REMOVED AND REPLACED FORWARD GALLEY OVEN PER AMM 25-35-19.
AIRCRAFT WAS NOT GROUNDED: DOOR 2R STILL REPORTED AS DIFFICULT TO ARM AND DISARM. STOWED SLIDE RETAINER STRAPS. ARM AND DISARM OPERATIONS CHECK OK.
AIRCRAFT WAS NOT GROUNDED: FLIGHT REPORTS 2R DOOR DISARMING LEVER STICKS. DIFFICULT TO ARM/DISARM. LUBRICATED 2R DOOR ARM/DISARM MECHANISM.
AIRCRAFT WAS NOT GROUNDED: JUMPSEAT FLASHLIGHT BATTERY INOPERATIVE AT 2L DOOR. REMOVED AND REPLACED 2L JUMPSEAT FLASHLIGHT PER AMM 25-65-00.
AIRCRAFT WAS NOT GROUNDED: LEFT HAND AFT JUMPSEAT FLASHLIGHT BATTERY IS DEAD--EXCESS FLIGHT ATTENDANT SEAT. REMOVED AND REPLACED L2 JUMPSEAT FLASHLIGHT IAW AMM 25-65-00.
AIRCRAFT IN BASE MAINTENANCE: SAFETY PIN DIFFICULT TO INSTALL ON L1 DOOR. REMOVED AND REPLACED L1 DOOR SLIDE AS REQUIRED.
AIRCRAFT IN BASE MAINTENANCE. L1 PASSENGER/CREW DOOR FAILED THE OPERATIONAL TEST OF THE DAMPING FUNCTION, PER CARD 296C83152003. REPLACED THE L1 DOOR DAMPER, PER AMM 52-11-14-0401.
AIRCRAFT WAS NOT GROUNDED: ESCAPE PATH LIGHT RED LENS BELOW FWD CLOSET FELL OFF. RESECURED LIGHT LENS.
AIRCAFT WAS GROUNDED: DURING ALL PHASES OF FLIGHT, GEAR UP OR GEAR DOWN, FLAPS 1,2,3 TAKEOFF-LANDING. THE AIRCRAFT PITCH UP WHEN THE CONTROL STICK IS RELEASED. FORWARD STICK IS REQUIRED TO KEEP THE NOSE IN DESIRED ATTITUDE. EMERGENCY DECLARED. ACCOMPLISHED TSM 27-93-00-810-818-A REMOVED AND REPLACED ELAC-2 COMPUTER IAW AMM 27-93-34.
AIRCRAFT IN BASE MAINTENANCE: RIGHT MAIN LANDING GEAR DOOR ACTUATOR FITTING AFT LUG WORN WITH BUSHING MIGRATION. REPLACED FITTING PER EA 302675.
AIRCRAFT WAS GROUNDED: PILOT REPORTS ON DESCENT FLIGHT ATTENDANTS AND PASSENGERS HAD SMELL OF BURNING, PLASTIC. COMPLAINED OF SORE EYES AND HEADACHE. MAINTENANCE REMOVED AND REPLACED APU STARTER MOTOR SEAL IAW AMM 49-42-51. OPS AND LEAK CHECK GOOD.
AFTER ENGINE SHUTDOWN AT THE GATE, AN EICAS MEESSAGE FOR THE NR 1 ENGINE FUEL FILTER CLOG ILLUMINATED. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REMOVED AND REPLACED THE DIFFERENTIAL PRESSURE SWITCH IAW AMM 73-34-15. OPS TESTED GOOD.
FLIGHT ATTENDANT REPORTED AN UNUSUAL ODOR IN THE FORWARD CABIN. THE AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED THE AVIONICS EXTRACT FAN IAW AMM.
AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT REPORTS RED EXIT LIGHT OVER 1L CLOSET DOOR DOESN'T APPEAR TO BE NORMAL. REPLACED 1L CLOSET RED EXIT LIGHT AS REQUIRED. OPERATIONS CHECK GOOD PER AMM 33-51-18.
L2 DOOR SLIDE COVER LOOSE. SECURED THE COVER IAW AMM 25-62-50.
RED EMERGENCY LIGHT LENS IN THE FORWARD GALLEY BROKE OFF. REPLACED THE LENS.
SLIDE COVER CAME OFF THE R2 DOOR. INSTALLED THE SLIDE COVER IAW AMM 25-61-00.
R2 DOOR SLIDE COVER CONTACTS FUSELAGE WHEN DOOR IS OPEN. REPLACED THE HOOK AND LOOP ON THE SLIDE COVER AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.
L1 LAVATORY EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REINSTALLED THE LENS AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 33-20-10.
AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT BATTERY (10WL) WOULD NOT TEST. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY BATTERY (10WL) AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.
AIRCRAFT NOT GROUNDED. 2R SLIDE COVER WON'T STAY ON. REINSTALLED 2R SLIDE COVER. OKAY FOR SERVICE.
AIRCRAFT IN BASE MAINTENANCE. WHILE PERFORMING INSPECTION PER TASK CARD 26T22053004, DETECTED CRACK ON INTERCOSTAL FITTING ATTACHED TO FORWARD SIDE OF L1 DOOR STOP FITTING AT FR 16, LOWER INBOARD HOLE, 1/2 INCH FROM AFT END OF HOLE. REPLACED INTERCOSTAL FITTING PER EA 275345.
AIRCRAFT IN BASE MAINTENANCE. WHILE PERFORMING INSPECTION PER TASK CARD 26T22053004, DETECTED CRACK ON INTERCOSTAL FITTING ATTACHED TO FORWARD SIDE OF R1 DOOR STOP FITTING NR 1 AT FR 16, LOWER INBOARD HOLE, 1/4 INCH TRAVEL DISTANCE INSIDE HOLE. REPAIRED PER EA 275345.
A CRACK INDICATION WAS FOUND ON THE LOWER CORNER OF THE FORWARD R1 DOOR STOP, NR 7 INTERCOSTAL FITTING AT FRAME 16. REPLACED THE INTERCOSTAL FITTING IAW SRM 51-72-11, DRAWING D53112307, AND EA 271592.
L2 DOOR SLIDE HAD DAMAGE TO COVER RELEASE CABLE RETAININING BALL ASSEMBLY.
CRACK ON CENTER WINDOW POST LEFT LOWER CONTINUITY FITTING AT Y50 AND FRAME 2. REPLACED CONTINUITY FITTING IAW EA 270947, REPAIRED IAW DRAWINGS R53112919, AND R53112958.
CRACK ON CENTER WINDOW POST RIGHT LOWER CONTINUITY FITTING AT -Y50 AND FRAME 2. REPLACED CONTINUITY FITTING IAW EA 270947, REPAIR DRAWINGS R53112919, AND R53112958.
AIRCRAFT IN BASE MAINTENANCE. CRACK INDICATION ON L2 DOOR CUTOUT IN RADIUS OF FRAME WEB ON FR 68 AND STRINGER 8L. REPAIRED FRAME WEB PER EA 270837.
CORROSION ON FLOORBEAM UPPER SURFACE AT -Y464 AND FRAME 66. REPLACED THE FLOORBEAM IAW SRM 51-72-11.
WATER INGRESS 27 INCHES FROM INBOARD END OF ELEVATOR AND 19 INCHES FROM TRAILING END. REPAIRED ELEVATOR PER SRM 55-21-11-300-005.
24C EMERGENCY LIGHT HOUSING DETACHED. INSTALLED EMERGENCY LIGHT HOUSING AT 24C.
AIRCRAFT IN BASE MX. RT SIDE BOX BEAM UPPER FLANGE, UPPER HOLE HAS CRACK INDICATION, AT FRAME 43 & -Y1622. REPAIRED BOX BEAM IAW EO 5315Y066.
AIRCRAFT IN BASE MX. LT SIDE BOX BEAM UPPER FLANGE, AFT 2 FASTENER HOLES HAVE CRACK INDICATIONS, AT FRAME 43 & Y1622. REPAIRED BOX BEAM IAW EO 5315Y066.
EMERGENCY EXIT AISLE 8C, LENS COVER OFF & BROKEN. REPLACED EMER EXIT AISLE8C LENS COVER.
RON, DURING R1 DOOR SLIDE CHANGE FOR TIME, NEW SLIDE WAS FOUND TO BE BAD FROM STOCK DUE TO A DETACHED MOORING LINE.
SEVERAL EMER LIGHTS OUT. R & R CABIN EMER POWER SUPPLY & BATTERY. OPERATIONS CHECKED GOOD.
FLIGHT 736 EN-ROUTE, EXCESSIVE OIL CONSUMPTION ON LT ENG, REACHING A PEAK OF 2 QTS PER HOUR. DECLARED AN EMER FOR A STRAIGHT IN APPROACH & LANDED WITHOUT FURTHER INCIDENT. REPLACED STARTER DRIVE PAD CARBON SEAL ON LT ENG IAW AMM 72-63-00-300-002-A6 & SUPPLEMENT 72-63-00-06. STARTER REINSTALLED IAW AMM 80-11-10-400-002. OPERATIONS & LEAK CHECKED OK.
RON VISIT, AFT CABIN MEGA PHONE INOPERATIVE. REPLACED AFT CABIN MEGA PHONE. OPERATIONS CHECKED GOOD.
RETURNED TO GATE FOR SMOKE IN THE COCKPIT. VENT EXTRACT FAULT OCCURRED SHORTLY AFTER ENG START & TAXI STARTED. REPLACED AVIONICS EXTRACT FAN.
ECAM EMER EXIT DOOR LT COVER CAME OFF DURING FLIGHT. INSTALLED COVER & PERFORMED ADJUSTMENT TEST IAW AMM 52-21-11-400-001A, SUBTASK 700-050-B. OK FOR SERVICE.
COVER FELL OFF LT OVERWING EXIT HANDLE. REINSTALLED OVERWING EXIT PANEL IAW AMM 25-60-00. CHECKED OK.
ON TAXI IN GOT DOOR LT EMER EXIT ECAM. FLIGHT ATTENDANT SAYS COVER CAME OFF. EXAMINED OVERWING EXIT DOOR HANDLE & COVER MOUNT AREA, ALL CHECKED NORMAL. REINSTALLED COVER, SYS NORMAL.
LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FRAME 64 TO 66 Z-500 -Y1292. REPLACED FLOORBEAM BETWEEN FRAME 64 TO 66 Z-500 -Y1292 IAW SRM 51-42-12.
CORROSION ON FLOORBEAM BETWEEN FRAME 67 TO 69 Z-500 -Y1162.5. REPLACED FLOORBEAM BETWEEN FRAME 67 TO 69 Z-500 -Y1162.5 IAW SRM 51-42-11 & 51-72-11.
LEVEL 2 INTERGRANULAR CORROSION ON RT AFT R2 DOOR SILL PLATE BETWEEN FRAME 66 TO 68, Z-500 -Y1589. REPLACED RT AFT R2 DOOR SILL PLATE BETWEEN FRAME 66 TO 68 Z-500 -Y1589 IAW SRM 51-42-11 & DWG 53480505.
WHILE INSTALLING A NEW SERVICEABLE SLIDE FOUND TO HAVE IMPROPER BACKING PLATE. THERE WAS NO SLOTS CUT INTO TOP OF BACKING PLATE TO LET SLIDE COVER BE INSTALLED. FOUND ELEC WIRE EXTENSION WILL NOT ROUTE PROPERLY. RETURNED TO STOCK UNSERVICEABLE.
WHILE ACCOMPLISHING OPERATIONAL CHECKS OF MANUAL MASK RELEASE IAW AMM 35-23-00-710-001-A, THE AFT RT FLIGHT ATTENDANT OXYGEN CONTAINER & SEAT ROW 16ABC OXYGEN CONTAINER DID NOT OPEN CORRECTLY. REPLACED & REINSTALLED OXYGEN CONTAINERS AT AFT RT FLIGHT ATTENDANT SEAT & SEAT ROW 16ABC AS REQUIRED IAW 35-21-41-400-001-A. SATISFACTORY OPERATIONS TEST COMPLETED IAW AMM 35-23-00-710-001-A.
THE 2L SLIDE PACK COVER FALLS OFF EVERY TIME 2L DOOR IS USED. THE 2L DOOR SLIDE ASSEMBLY PACKED WRONG. R & R SLIDE PACK ASSEMBLY IAW JOB CARD 26L00025011, DOOR ESCAPE SLIDE RAFT REPLACEMENT. OPERATIONS CHECKED OK.
WHILE ACCOMPLISHING MOD, 2514Y110 SLIDE RAFT INSPECTION, FOUND L1 SLIDE COVER CONTACTING FUSELAGE. LIGHT ABRASION WAS FOUND. REPLACED SLIDE RAFT IAW ROUTINE WORK CARD 26L00025011.
WHILE ACCOMPLISHING MOD, 2514Y110 SLIDE RAFT INSPECTION, FOUND R2 SLIDE COVER CONTACTING FUSELAGE. LIGHT ABRASION WAS FOUND. REPLACED DOOR R2 SLIDE RAFT IAW JOB CARD 26L00025011.
WHILE ACCOMPLISHING MOD, 2514Y110 SLIDE RAFT INSPECTION, FOUND L2 SLIDE COVER CONTACTING FUSELAGE. LIGHT ABRASION WAS FOUND. REPLACED L2 DOOR SLIDE RAFT IAW JOB CARD 26L0025011.
WHILE ACCOMPLISHING MOD, 2514Y110 SLIDE RAFT INSPECTION, FOUND R1 SLIDE COVER CONTACTING FUSELAGE. LIGHT ABRASION WAS FOUND. REPLACED SLIDE RAFT IAW ROUTINE WORK CARD 26L0002501.
EN ROUTE FROM CUN TO PHL, CREW REPORTED THE RT WINDSHIELD HEAT SPARKED & ARCED, THEN CRACKED OUTER PANE. RT WINDSHIELD HEAT INOPERATIVE MEMO ON ECAM. R & R RT WINDSHIELD & RT WINDOW HEAT COMPUTER IAW AMM 56-11-11-000-001-A, 56-11-11-400-001-A, 30-42-34-000-001-A & 30-42-34-400-001-A. OPERATIONS CHECKED OK.
AT CRUISE ALTITUDE FL390, CREW NOTICED NR 2 ENG OIL QTY AT 7.0 QUARTS. LEFT TPA GATE ABOUT AN HOUR PRIOR WITH 18.5 QUARTS ON BOTH ENGS. SOON AFTER, OIL QTY NR 2 CONTINUED TO DECREASE. CREW DECLARED AN EMERGENCY & DIVERTED TO CLT. SHUTDOWN NR 2 ENG AS PRECAUTION WHEN OIL REACHED 3 QUARTS. LANDED SINGLE ENG WITHOUT INCIDENT. TOTAL SINGLE ENG TIME WAS 5 MINUTE. MX ACCOMPLISHED NR 2 ENG CHANGE DUE TO OIL LEAK FROM AFT TURBINE BEARING AREA IAW JOB CARD 26L40071001.
MAINTENANCE REPORTED THE R2 DOOR LOW LEVEL DOOR JAM WALL MOUNTED EMERGENCY LIGHT INOPERATIVE. MX REPLACED R2 DOOR LOW LEVEL DOOR JAM EMERGENCY LIGHT ASSEMBLY AS NECESSARY, OPERATIONS CHECKED OK.
SEAT 1C EMERGENCY LIGHTING INOPERATIVE. REPLACED LENS.
CREW REPORTED A CLASS II MESSAGE MX SDCU. MX R & R SDCU IAW AMM 26-17-34-400-001-A. BITE TEST AND OPS CHECK GOOD.
AFT EMERGENCY FLASHLIGHT BATTERY PACK INOPERATIVE. REPLACED THE BATTERY PACK ON AFT RT EMERGENCY FLASHLIGHT.
CREW REPORTED THE LT OVERWING EMERGENCY EXIT ECAM ILLUMINATED IN FLIGHT AND CAB OK. MX REINSTALLED LT OVERWING EMERGENCY EXIT DOOR COVER. OPS CHECKS GOOD.
CREW REPORTED A MODERATE ELECTRICAL BURNING ODOR IN AFT GALLEY. MX R & R THE AFT CHILLER. OPS CHECK GOOD IAW AMM 25-34-51, PB 401.
MAINTENANCE FOUND THE R1 DOOR HARD TO OPEN. MAINTENANCE FOUND R1 GIRT BAR OUT OF POSITION. REPOSITION GIRT BAR R1 DOOR. OPS CHECK NORMAL PER AMM 52-20-00. R1 DOOR OPS CHECK GOOD.
MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY EXIT LIGHT LENS MISSING ON SEATS 6C AND 16C. MAINTENANCE INSTALLED NEW SEAT MOUNTED EMERGENCY EXIT LIGHT LENS ON SEATS 6C AND 16C PER AMM 33-51-18, PB 401.
MAINTENANCE REPORTED THE LT OVERWING SLIDE BOTTLE KNURLED NUT SAFETY WIRE HOLE IS WORN. MAINTENANCE REPLACED THE LEFT ESCAPE SLIDE RESERVOIR ASSEMBLY PER AMM 25-62-46-001-A. OPS CHECK GOOD.
ELECTRICAL & CHEMICAL ODORS DETECTED ON FLIGHT DECK. REMOVED AND REPLACED FLIGHT CONTROL UNIT PER AMM 22-81-400-001. OPS CHECKED GOOD.
L1 DOOR ASSIST CYLINDER PRESSURE LOW. SERVICED L1 DOOR ASSIST CYLINDER IAW AMM 52-10-11-614-001.
F/O'S OXYGEN PANEL DOES NOT TEST PROPERLY - PRESS TO TEST IS VERY BRIEF AND NO FLOW WITH RED EMERGENCY PRESSED. MAINTENANCE REMOVED AND REPLACED F/O'S OXYGEN PANEL BOX IAW AIRBUS MAINTENANCE MANUAL 35-12-41-000-001, 35-12-41-400-001 AND 35-12-41-710-001.
DOOR R2 ARMING LEVER IS NOT SEATED AGAINST SWITCH. SHOWS DOOR UNARMED IN FLIGHT. FLIGHT ATTENDANT CAN MOVE ARMING LEVER 1/4 INCH TOWARD ARMED POSITION AND SHOWS ARMED OK. ADJUSTED ESCAPE SLIDE GIRT BAR TRAVEL PER AIRBUS MAINTENANCE MANUAL 52-13-22-99-011. OPS CHECK GOOD.
R2 DOOR PRESSURE LIGHT STARTED FLASHING DURING FLIGHT. DOOR SLIDE SHOWED DISARMED ON ECAM. PERFORMED FUNCTIONAL TEST OF VISUAL INDICATOR OF DOOR LOCKING MECHANISM PER AIRBUS MAINTENANCE MANUAL 52-10-720-004 AND TROUBLESHOOTING MANUAL 52-13-00-810-816, NO FAULTS FOUND.
IN FLIGHT AT 1800 THE LEFT OVERWING EMERGENCY EXIT ILLUMINATED ON ECAM. PRESSURIZATION WAS NORMAL. PERFORMED OPERATIONAL TEST OF THE EMERGENCY EXIT HATCH AND ESCAPE SLIDE ARMING AND DISARMING PER AIRBUS MAINTENANCE MANUAL 52-21-00-710-005, NO FAULTS FOUND.
2S CHECK - CORROSION ON EXTERNAL FUSELAGE SKIN PANEL AT FR 63+8 INCHES BETWEEN S40L TO S43L. REPAIRED EXTERNAL FUSELAGE SKIN PANEL AT FR 63+8 INCHES BETWEEN S40L TO S43L IAW EA 133741.
2S CHECK - DELAMINATION ON ACCESS PANEL 325AL LEFT ON VERTICAL STABILIZER. REPLACED ACCESS PANEL 325AL LEFT ON VERTICAL STABILIZER IAW A319 SRM 53-55-11 & 51-72-11.
2S CHECK - DELAMINATION ON ACCESS PANEL 325AR RIGHT ON VERTICAL STABILIZER. REPLACED ACCESS PANEL 325AR RIGHT ON VERTICAL STABILIZER IAW A319 SRM 53-55-11 & 51-72-11.
2S CHECK - DURING OPERATIONAL TEST OF DAMPING FUNCTIONAL & EMERGENCY OPERATION WAS FOUND HARD IMPACT BETWEEN THE BUFFER & FUSELAGE AT PASSENGER/CREW DOOR 832. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT PASSENGER/CREW DOOR 832 IAW AMM 52-13-14-000-001.
2S CHECK - DURING OPERATIONAL TEST OF DAMPING FUNCTIONAL & EMERGENCY OPERATION WAS FOUND HARD IMPACT BETWEEN THE BUFFER & FUSELAGE AT PASSENGER/CREW DOOR 842. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT PASSENGER/CREW DOOR 842 IAW AMM 52-13-14-000-001.
2S CHECK - DURING OPERATIONAL TEST OF DAMPING FUNCTIONAL & EMERGENCY OPERATION WAS FOUND HARD IMPACT BETWEEN THE BUFFER & FUSELAGE AT PASSENGER/CREW DOOR 831. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT PASSENGER/CREW DOOR 831 IAW AMM 52-13-14-000-001.
2S CHECK - OUT ADJUSTMENT DIMENSION "A" BETWEEN STRIKER LEVER & FINGER AT PASSENGER/CREW DOOR 832. ADJUSTMENT CLEARANCE J2 BETWEEN STRIKER LEVER AND FINGER AT PASSENGER/CREW DOOR 832 IAW AMM 52-11-14-0501.
2S CHECK - OUT ADJUSTMENT TORSION BAR BELLCRANK AT PASSENGER CREW DOOR 842. ADJUSTMENT TORSION BAR BELLCRANK AT PASSENGER/CREW DOOR 842 IAW AMM 52-13-21-0401.
2S CHECK - OUT ADJUSTMENT DIMENSION "A" BETWEEN STRIKER LEVER & FINGER AT PASSENGER/CREW DOOR 842. ADJUSTMENT CLEARANCE J2 BETWEEN STRIKER LEVER AND FINGER AT PASSENGER/CREW DOOR 842 IAW AMM 52-11-14-0501.
2S CHECK - OUT ADJUSTMENT DIMENSION "A" BETWEEN STRIKER LEVER & FINGER AT PASSENGER/CREW DOOR 831. ADJUSTMENT CLEARANCE J2 BETWEEN STRIKER LEVER AND FINGER AT PASSENGER/CREW DOOR 831 IAW AMM 52-11-14-0501.
2S CHECK - OUT ADJUSTMENT DIMENSION "A" BETWEEN STRIKER LEVER & FINGER AT PASSENGER/CREW DOOR 841. ADJUSTMENT CLEARANCE J2 BETWEEN STRIKER LEVER AND FINGER AT PASSENGER/CREW DOOR 841 IAW AMM 52-11-14-0501.
2S CHECK - CORROSION ON INTERNAL AREA OF THE INTERCONNECTING STRUT HOUSING LEFT WING AT WS 4862, RIB 9. REPLACED LEFT WING INTERCONNECTING STRUT IAW JOB CARD 26C57057001.
2S CHECK - CORROSION ON INTERNAL AREA OF THE INTERCONNECTING STRUT HOUSING RIGHT WING AT WS 4862, RIB 9. REPLACED RIGHT WING INTERCONNECTING STRUT IAW JOB CARD 26C67057001.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING LOWER FUEL ACCESS PANEL 640HB BETWEEN WS 732 TO WS 779 & BETWEEN RIB 13 TO RIB 14. REPLACED RIGHT WING LOWER FUEL ACCESS PANEL 640HB IAW JOB CARD 26C60057091.
2S CHECK - CORROSION ON 2 EA LT WING SPOILER NR 4 HINGE PINS BETWEEN WS 924 TO WS 970. REPLACED HINGE PINS IAW EA 133690.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON COUNTERSINK HOLES OF RIGHT WING LOWER FUEL ACCESS PANEL 640PB AT WS 9704 BETWEEN RIB 18 TO RIB 19. REPLACED RIGHT WING LOWER FUEL ACCESS PANEL 640PB IAW A319 SRM 57-27-11.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER RIGHT WING COUNTERSINK HOLES OF FUEL ACCESS PANEL 640KB BETWEEN WS 8268 TO WS 8744 & BETWEEN RIB 15 TO RIB 16. REPLACED RIGHT WING FUEL ACCESS PANEL 640KB IAW JOB CARD 26C60057024.
2S CHECK - MISSING PROTECTIVE PROTECTION ON LEFT AILERON HINGE PINS 1 THRU 5 AT WS 12870 RIB 24. REPLACED LEFT AILERON HINGE PINS 1 THRU 5 IAW A319 AMM 27-14-41 & JOB CARD 26C50027005.
2S CHECK - MISSING PROTECTIVE TREATMENT ON RIGHT WING NR 1 SPOILER HINGE PINS (2EA) BETWEEN WS 3059 TO WS 3758 & BETWEEN RIB 6 TO RIB 7. REPLACED SPOILER HINGE PINS (2EA) IAW EA 133690B.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER RIGHT WING COUNTERSINK HOLES OF FUEL ACCESS PANEL 640LB BETWEEN WS 8744 TO WS 9235 & BETWEEN RIB 16 TO RIB 17. REPLACED RIGHT WING FUEL ACCESS PANEL 640LB IAW JOB CARD 26C60057091.
2S CHECK - MULTIPLE CRACKS ON EMERGENCY EXIT DOOR 834 SEGMENT ANGLE BETWEEN FR40 TO FR41 BETWEEN BEAM 1 TO BEAM 4. REPLACED SEGMENT ANGLE ON EMERGENCY EXIT DOOR 834 IAW EO 5210Y228.
2S CHECK - CRACKS ON EMERGENCY EXIT DOOR 844 SEGMENT ANGLE BETWEEN FR40 TO FR41 BETWEEN BEAM 1 TO BEAM 4. REPLACED SEGMENT ANGLE AT EMERGENCY EXIT DOOR 844 IAW EO 5210Y228.
2S CHECK - CRACK ON WEB OF COCKPIT FLOOR STRUCTURE AT FR6, -Y765. REPAIRED WEB AT FR6, -Y765 IAW EA 133717.
2S CHECK - CRACK ON RIGHT WEB BETWEEN FR8 TO FR11, -Y765. REPLACED RIGHT WEB BETWEEN FR8 TO FR11, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING 53113219.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR41 TO FR47, -Y1292. REPLACED SEAT TRACK BETWEEN FR41 TO FR47, -Y1292 IAW A319 SRM 51-72-11AND AIRBUS DRAWING D53371000.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACKS BETWEEN FR36 TO FR40, -Y1292. REPLACED SEAT TRACKS BETWEEN FR36 TO FR40, -Y1292 IAW A319 SRM 51-72-11AND AIRBUS DRAWING D53371000.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, -Y765. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D57130147.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING AT R1 DOOR AT FR18+ 3 INCHES, S23R. REPLACED CENTER FITTING AT R1 DOOR AT FR18+ 7 INCHES, S23R IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112198.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING AT R1 DOOR AT FR18+ 7 INCHES, S23R. REPLACED CENTER FITTING AT R1 DOOR AT FR18+ 7 INCHES, S23R IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112198.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK ASSEMBLY BETWEEN FR35 TO FR36, -Y1292. REPLACED SEAT TRACK ASSEMBLY BETWEEN FR35 TO FR36, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53371024.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR41 TO FR47, Y1292. REPLACED SEAT TRACK BETWEEN FR41 TO FR47, Y1292 IAW A319 SRM 51-72-11.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON WEB FRONT SPAR OF RIGHT OUTBOARD FLAP BETWEEN SUPPORT RIB 13 TO RIB 16, TRACK 4. REPLACED WEB FRONT SPAR OF RIGHT OUTBOARD FLAP IAW A319 SRM 51-72-11 & AIRBUS DRAWING D57571208.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON STRINGER BETWEEN FR68 TO FR69, S23R. REPLACED STRINGER BETWEEN FR68 TO FR69, S23R IAW A319 SRM 51-72-11 & AIRBUS DRAWING D534 80505.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT PYLON SPIGOT RECEPTACLE FITTING BETWEEN PYLON STA 6793 TO STA 7063. REPLACED LEFT PYLON SPIGOT FITTING IAW A319 SRM 54-51-12.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR41 TO FR46, -Y765. REPLACED SEAT TRACK BETWEEN FR41 TO FR46, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53371110.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, -Y1292. REPLACED SEAT TRACK BETWEEN FR24 TO FR35, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53233450.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, -Y765. REPLACED SEAT TRACK BETWEEN FR24 TO FR35, -Y765 IAW A319 SRM 51-72-11 & EA 133697.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, Y1292. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, Y1292 IAW A319 SRM 51-72-11AND AIRBUS DRAWING D57130147.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK RAIL BETWEEN FR47/51 TO FR64, -Y765. REPLACED SEAT TRACK RAIL BETWEEN FR47/51 TO FR64, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53476977.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER CORNER FITTING AT L2 DOOR AT FR66, S23L. REPLACED LOWER CORNER FITTING AT L2 DOOR AT FR66, S23L IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53480505.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK RAIL BETWEEN FR47/51 TO FR64, -Y1292. REPLACED SEAT TRACK RAIL BETWEEN FR47/51 TO FR64, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53476977.
2S CHECK - EXCESS PLAY AT RUDDER HINGE BEARING NR 2 AT VERTICAL STAB STA 1926 / RIB 4. REPLACED RUDDER HINGE FITTING NR 2 IAW A319 SRM 51-42-11.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER CORNER FITTING AT R2 DOOR AT FR66, S23R. REPLACED LOWER CORNER FITTING AT R2 DOOR AT FR66, S23R IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53480505.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON WEB BETWEEN FR24 TO FR24+10 INCHES, -Y1732. REPLACED WEB BETWEEN FR24 TO FR24+10 INCHES, -Y1732 IAW A319 SRM 51-72-11, 51-42-11 & AIRBUS DRAWING D53233414.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER CORNER FITTING AT L2 DOOR AT FR68, S23L. REPLACED LOWER CORNER FITTING AT L2 DOOR AT FR68, S23L IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53480505.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON WEB FRONT SPAR OF LEFT OUTBOARD FLAP BETWEEN SUPPORT RIB 13 TO RIB 16, TRACK 4. REPLACED WEB FRONT SPAR OF LEFT OUTBOARD FLAP IAW A319 SRM 51-72-11 & AIRBUS DRAWING D57571208.
2S CHECK - EXCESSIVE PLAY ON RUDDER HINGE BEARING NR 4 AT VERTICAL STAB RIB 6 & STAB STA 2632. REPLACED RUDDER HINGE FITTING NR 4 AT VERTICAL STAB RIB 6 & STAB STA 2632 IAW A319 SRM 51-72-11.
2S CHECK - LEVEL 2 INTERGRANULAR CORROSION ON INTERNAL CAVITY OF RIGHT PYLON SPIGOT BEARING SLEEVE AT PYLON STA 6465 TO STA 7063 & BETWEEN RIB 3 TO RIB 5. REPLACED RIGHT PYLON SPIGOT BEARING SLEEVE IAW JOB CARD 26C40054035.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SILL AT L2 DOORWAY AT FR67+16 INCHES, S23L. REPLACED LOWER SILL AT L2 DOORWAY AT FR67+16 INCHES, S23L IAW A319 SRM 51-72-11, AIRBUS DRAWING 53480505 & EA 133651.
2S CHECK - EXCESS PLAY AT RUDDER HINGE BEARING NR 1 AT VERTICAL STAB STA 780 / RIB 2. REPLACED RUDDER HINGE FITTING NR 1 IAW A319 SRM 51-42-11.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR47/51 TO FR64, Y765. REPLACED SEAT TRACK BETWEEN FR47/51 TO FR64, Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472831.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON WEB BETWEEN FR24+10 INCHES TO FR25, -Y1732. REPLACED WEB BETWEEN FR24+10 INCHES TO FR25, -Y1732 IAW A319 SRM 51-72-11, 51-42-11 & AIRBUS DRAWING D53233414.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON AFT CARGO DOORWAY THRESHOLD SHEET BETWEEN FR55 TO FR59, S39R. REPLACED AFT CARGO DOORWAY THRESHOLD SHEET IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53477100.
2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT RAIL BETWEEN FR47/51 TO FR64, Y1292. REPLACED SEAT RAIL BETWEEN FR47/51 TO FR64, Y1292 IAW A319 SRM 51-72-11AND AIRBUS DRAWINGS D53476950, D53476977.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY BETWEEN FR12 TO FR16, -Y1379. REPLACED RAIL DUMMY BETWEEN FR12 TO FR16, -Y1379 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112831.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, Y1292 IAW A319 SRM 51-72-11AND AIRBUS DRAWING D53110900.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL SEAT BEAM BETWEEN FR64 TO FR65 PLUS 5", Y765. REPLACED RAIL SEAT BEAM BETWEEN FR64 TO FR65 PLUS 5, Y765 IAW A319 SRM 51-72-11AND AIRBUS DRAWING 53472815.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON DUMMY RAIL BETWEEN FR12 TO FR16, Y503. REPLACED DUMMY RAIL BETWEEN FR12 TO FR16, Y503 IAW A319 SRM 51-72-11.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67+16 INCHES TO FR69, -Y1162. REPLACED FLOORBEAM BETWEEN FR67+16 INCHES TO FR69, -Y1162 IAW A318 SRM 51-72-11 & AIRBUS DRAWING 53472780.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON TRAY BETWEEN FR68 TO FR69, S23R. REPLACED TRAY BETWEEN FR68 TO FR69, S23R IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53480019.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 PLUS 5 INCHES TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR66 PLUS 5 INCHES TO FR70, -Y765 IAW A319 SRM 51-72-11AND AIRBUS DRAWING D534-72780.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR70, -Y160. REPLACED FLOORBEAM BETWEEN FR68 TO FR70, -Y160 IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53472780.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, Y254. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, Y254 IAW A319 SRM 51-72-11 AND AIRBUS DRAWINGS D53472750 AND D53472780.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 PLUS 5 INCHES TO FR70, Y765. REPLACED FLOORBEAM BETWEEN FR66 PLUS 5 INCHES TO FR70, Y765 IAW A319 SRM 51-72-11AND AIRBUS DRAWING 53472780.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23R. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23R IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53474180.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON WEB BETWEEN FR69 TO FR70, S23L. REPLACED WEB BETWEEN FR69 TO FR70, S23L IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53474180.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SILL AT R2 DOORWAY BETWEEN FR66 TO FR68, S23R. REPLACED LOWER SILL AT R2 DOORWAY BETWEEN FR66 TO FR68, S23R IAW A319 SRM 51-72-11, AIRBUS DRAWING 53480505 & EA 133669.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR64 TO FR66 + 5 INCHES, S23R. REPLACED SEAT RAIL BETWEEN FR64 TO FR66 + 5 INCHES, S23R IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472816.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK RAIL BETWEEN FR64 TO FR 66+5 INCHES, Y1292. REPLACED SEAT TRACK RAIL BETWEEN FR64 TO FR 66+5 INCHES, Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D534-72815.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR12 TO FR24, -Y254. REPLACED FLOOR SUPPORT BETWEEN FR12 TO FR24, -Y254 IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53110900.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR20 TO FR24, Y254. REPLACED FLOOR SUPPORT BETWEEN FR20 TO FR24, Y254 IAW A319 SRM 51-72-11 AND AIRBUS DRAWING 53112816.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR65 + 5 INCHES, -Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR65 + 5 INCHES, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D534-72816.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON WEB BETWEEN FR14 TO FR16, Y1612. REPLACED WEB BETWEEN FR14 TO FR16, Y1612 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112570.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR69 TO FR70, S23R. REPLACED FLOOR SUPPORT BETWEEN FR69 TO FR70, S23R IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53474180.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHAPE SILL BETWEEN FR66+5 INCHES TO FR67+15 INCHES, S23L. REPLACED SHAPE SILL BETWEEN FR66+5 INCHES TO FR67+15 INCHES, S23L IAW A319 SRM 51-72-11 & AIRBUS DRAWING 53480505.
2S CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR65 TO FR66, -Y1540. REPLACED FLOORBEAM BETWEEN FR65 TO FR66, -Y1540 IAW A319 SRM 51-72-11.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER AFT CORNER FITTING AT R2 DOOR AT FR68, S23R. REPLACED LOWER AFT CORNER FITTING AT R2 DOOR AT FR68, S23R IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53480505.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23L. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23L IAW A319 SRM 51-72-11 & AIRBUS DRAWING 53474180.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, S23R, -Y765. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, S23R, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112812.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67+10 INCHES, -Y465. REPLACED FLOORBEAM BETWEEN FR64 TO FR67+10 INCHES, -Y465 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D534 72816.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+16 INCHES, -Y1235. REPLACED FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+16 INCHES, -Y1235 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472816.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+16 INCHES, Y1235. REPLACED FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+16 INCHES, Y1235 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D534-72780.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67+16 INCHES TO FR69, Y1162. REPLACED FLOORBEAM BETWEEN FR67+16 INCHES TO FR69, Y1162 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D534-72780.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WEB BETWEEN FR16 TO FR12, -Y1652. REPLACED RIGHT WEB BETWEEN FR16 TO FR12, -Y1652 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53114392.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WEB BETWEEN FR20 TO FR24, Y1652. REPLACED LEFT WEB BETWEEN FR20 TO FR24, Y1652 IAW A319 SRM 51-72-11.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON WEB BETWEEN FR20 TO FR24, -Y1652. REPLACED WEB BETWEEN FR20 TO FR24, -Y1652 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53114392.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67 + 10 INCHES, Y512. REPLACED FLOORBEAM BETWEEN FR64 TO FR67 + 10 INCHES, Y512 IAW A319 SRM 51-72-11.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY BETWEEN FR12 TO FR16, -Y81. REPLACED RAIL DUMMY BETWEEN FR12 TO FR16, -Y81 IAW A319 SRM 51-72-11.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR20 TO FR24, -Y189. REPLACED SEAT TRACK BETWEEN FR20 TO FR24, -Y189 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53111406.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y1292 IAW A319 SRM 51-72-11.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, Y765. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, Y765 IAW A319 SRM 51-72-11.
2S CHECK - BLEND OUT ON EXTERNAL SKIN LOCATED BETWEEN FR29 TO FR30 AND BETWEEN S19L TO S20L UPPER FUSELAGE. REPAIRED FUSELAGE EXTERNAL SKIN BETWEEN FR29 TO FR30 AND BETWEEN S19L TO S20L IAW A319 SRM 53-21-11.
2S CHECK - 4 EA CRACKS ON LEFT PYLON ACCESS PANEL 413DL. REPAIRED LEFT PYLON ACCESS PANEL 413DL IAW EA 133733.
FLT 1982 - CLT-BOS - EMERGENCY LIGHTS - EMERGENCY FLASHLIGHT FORWARD FLIGHT ATTENDANT STATION NO FLASHING RED LIGHT. REMOVED AND REPLACED FORWARD FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT.
PIT - GEAR CHANGE - CORROSION & PITTING ON MAIN LANDING GEAR RIGHT REAR PINTLE PIN. REPLACED MAIN LANDING GEAR RIGHT REAR PINTLE PIN IAW US AIRWAYS TASK CARD 26T00032001.
FLL-DCA-FLT 1712 - CREW RECEIVED A GREEN HYDRAULIC SYSTEM LOW MESSAGE. CREW DIVERTED TO BWI. AS A PRECAUTION, CREW DECLARED AN EMERGENCY. THE LANDING WAS UNEVENTFUL. CREW WAS ABLE TO EXIT THE RUNWAY BY DIFFERENTIAL BRAKING. ACFT WAS TOWED TO THE GATE. MX REPLACED CRACKED LT CASE HYDRAULIC LINE AND CASE DRAIN FILTER. OPERATIONAL TEST WAS GOOD. ACFT WAS RETURNED TO SERVICE. (S)
PIT - FLIGHT ATTENDANT AFT LEFT JUMPSEAT LOWER FLASHLIGHT NOT BLINKING. MAINTENANCE REPLACED THE FLASHLIGHT.
PIT - FLIGHT ATTENDANT AFT LEFT JUMPSEAT LOWER FLASHLIGHT NOT BLINKING. MAINTENANCE REPLACED THE FLASHLIGHT.
MCI FLT 1609 MCI - CLT. A STRONG ODOR WAS NOTED IN THE CABIN. MAINTENANCE ACTION PENDING.
PHL - THE EMERGENCY LIGHTS TEST INDICATED EMERGENCY BATTERY FAULT. MAINTENANCE REPLACED THE MID-CABIN, LEFT EMERGENCY POWER SUPPLY UNIT.
CLT - THE LEFT, MID-CABIN EMERGENCY POWER SUPPLY UNIT BATTERY SHOWS FAULT ON TEST. MAINTENANCE REPLACED THE BATTERY ON THE LEFT, MID-CABIN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.
DCA - THE LEFT HAND, MID-CABIN EMERGENCY EXIT LIGHT BATTERY INDICATED A LOW CHARGE. MAINTENANCE REPLACED THE LEFT HAND, MID-CABIN EMERGENCY EXIT LIGHT BATTERY. OPERATIONALLY CHECKS OK.
BDL - THE EMERGENCY LIGHT SYSTEM FAULTED WITH -EXT LOAD AFT L- MESSAGE DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.
BDL - DURING THE EMERGENCY LIGHTS TEST, RECEIVED -EPSU FWD L- MESSAGE. MAINTENANCE REPLACED THE FORWARD LEFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.
PIT - FOUND BEAM CORRODED 2 INCHES BY 1 INCH, FLOORBEAM FRAME 16, FRAME 16-Y254. REPLACED BEAM PER SRM 51-72-11. (M)
PIT - FOUND FLOOR SUPPORT CORRODED 1 INCH DIAMETER HOLES AROUND NUT PLATES, -Y1200 BETWEEN FRAME 66/69. REPLACED 3 SECTIONS OF FLOORBEAM PER SRM 51-72-11. (M)
FOUND BEAM CORRODED 8 INCHES BY 2 INCHES, BETWEEN FRAME 14 AND 16 Y 503.2. REPLACED BEAM BEAM PER SRM 51-72-11. (M)
PIT - FOUND BEAM CORRODED 10 INCHES BY 2 INCHES, BETWEEN FRAME 16 AND 20 Y254. INSTALLED BEAM PER SRM 51-72-11. (M)
PIT - FOUND FLOORBEAM CORRODED 4 INCHES BY 5 FEET, TOP OF BEAM FRAME 66 THROUGH FRAME 69. REPLACED FLOORBEAM AND A SPLICE PART PER SRM 51-72-11. (M)
IN CRUISE FLT, CABIN CREW REPORTED A RUBBER/ELECTRIC ODOR AROUND ROW 18. THE VIDEO ENTERTAINMENT SYS TURNED OFF. ODOR SUBSIDED, BUT CAME BACK BRIEFLY. ODOR SUBSIDED AGAIN & REMAINED THAT WAY FOR THE REST OF THE FLIGHT. MX COULD NOT DUPLICATE THE ODOR. PLACED THE VIDEO ENTERTAINMENT SYSTEM ON MEL.
THE EMERGENCY EXIT LIGHT WIRING WAS FOUND DISCONNECTED AND THE MAIN ENTRANCE DOOR SLIDE COVER LOOSE. MAINTENANCE INSTALLED THE LOOSE SLIDE COVER AND CONNECTED THE EMERGENCY LIGHT WIRING. OPERATIONALLY CHECKS OK.
THE CABIN CREW REPORTED THAT THE LEFT OVERWING EXIT LIGHT DOES NOT ILLUMINATE WHEN NO PED SWITCH IS TURNED ON. MAINTENANCE ADJUSTED A CONTACT. OPERATIONALLY CHECKS OK.
BDL - THE EMERGENCY LIGHT ON SEAT 8C WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED WIRING AT CONNECTOR ON BOTTOM OF SEAT. OPERATIONALLY CHECKED OK. (M)
PHL - THE LT AND RT OVERWING EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKED OK. (M)
PHX-PHL - FLT 168 - AN ODOR BECAME PRESENT IN THE FORWARD GALLEY AFTER TAKEOFF. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE GALLEY, COFFEEMAKER, CHILLERS, ELECTRICAL DEVICES, AND OTHER EQUIPMENT. ALSO, RAN ENGINE, APU, AND NR 2 PACK. NO ODOR NOTED. OPS CHECKED NORMAL. ALSO, AIR SAMPLES WERE TAKEN BY AN INDUSTRIAL HYGENIST. RESULTS WERE FOUND TO BE NORMAL. (M)