N411UA

Part: CONTROL UNIT — WEAK (90VU) · airframe 92,159 hrs · 36,041 cycles

N LG SHOCK ABSORBER(2526GM)/IDLGCIU 2 WITH FAILURE MSG N LG EXTPROX SNSR(24GA)TGT POS /IDLGCIU 1 LOCKING LOG FOR POSITIVE FIX. OK TO UNLOCK TO CLEAR UNIT, LGCIU VK0 OFF 31-3260-9-0001 9224 ON 0000 UNIT, LGCIU VK0 OFF 31-3260-9-0001 9224 ON 31-3231-9-0002 0261 LGCIU-1 LAST LEG REPORT SHOWED: 527112: AFT CARGO DR SAFETY MECH PROX SNSR(32WV) TGT POS; 323173: N LG EXT PROX SNSR(24GA) TGT POS; 322113: NLG SHOCK ABSORBER . FAULTS ON PHASE 6 (CRUISE). T/S IAW TSM 32-31-00-810-842-A. INSPECTED NLG EXT SENSORS 24GA & 25GA, NO FAULTS NOTED. CONNECTORS 24GA_A, 25GA_A PIN RETENTION CHKD GOOD, BACKSHELL & WIRES CHKD NORMAL. FOUND LGCIU-1 NORMAL C/B, 1GA, WEAK. REPLACED C/B. ALSO REPLACED LGCIU-1 IAW AMM 32-31-71-400-001-A. PERFORMED LGCIU BITE IAW AMM 32-69-00-740-001-A. NO FAULTS NOTED. ALSO PERFORMED BITES ON AFT CARGO DOOR SWITCH, ADIRU-3, STBY PITOT ANTI-ICE WHICH WERE CAUSED BY LGCIU-1 FAULT. NO FAULTS NOTED. FAULT DISPLAYED ON UPPER ECAM SCREEN. - F -CTL UPDATED MAA CODE. SFCC-2 FLAP LAST LEG REPORTS SHOWED 31-12-34: NO CFDIU DATA, CHECK WIRING TO FLP 2. CLEANED CONNECTORS ON SFCC-1 &-2, CFDIU. SCFCC-2 STATUS & ON GND FAULTS CHKD GOOD. RAN FLAPS, NO FAULTS NOTED. DURING OTHER T/S ON A DIFFERENT SYSTEM, SFCC-2 GLITCHED. WHEN RECOVERED, IT SHOWED NO FAULTS. SUSPECT SFCC-2. SFCC 2 REP

Part: EPSU — FAILED (13WL) · airframe 92,146 hrs · 36,036 cycles

EPSU BATTERY 13WL FAILED OPERATIONAL TEST. REPLACED EPSU 13WL IAW AMM 33-51-38-400-002. OPS CKC NORMAL.

Part: EPSU — FAILED (11WL) · airframe 92,146 hrs · 36,036 cycles

EPSU BATTERY 11WL FAILED OPERATIONAL TEST. REPLACED EPSU 11WL IAW AMM 33-51-38-400-002. OPS CKC NORMAL.

Part: EPSU — FAILED (12WL) · airframe 92,146 hrs · 36,036 cycles

EPSU BATTERY 12WL FAILED OPERATIONAL TEST. REPLACED EPSU 12WL IAW AMM 33-51-38-400-002. OPS CKC NORMAL. B

Part: EPSU — FAILED (10WL) · airframe 92,146 hrs · 36,036 cycles

EPSU BATTERY 10WL FAILED OPERATIONAL TEST. REPLACED EPSU 10WL IAW AMM 33-51-38-400-002. OPS CKC NORMAL. BY LHT TECH 5P1115 AND INSP 5H0086.

Part: EPSU — FAILED (13WL) · airframe 92,146 hrs · 36,036 cycles

CABIN LIGHTS EMERGENCY CAPACITY TEST FAILED. REPLACEMENT OF EPSU BATTERY 10WL IS REQUIRED. A3NB-33-3-6013 SEQ:633 ZONE:200 EPSU BATTERY 13WL FAILED ON EMERGENCY LIGHTING BATTERY CAPACITY TEST AND REQUIRE REPLACEMENT. PERFORMED EPSU BATTERY REPLACEMENT 13WL, IAW AMM: 33-51-38-400-002/ 33-51-3800-002 REV. 122 TEST SATIFACTORY.

Part: EPSU — FAILED (10WL) · airframe 92,146 hrs · 36,036 cycles

CABIN LIGHTS EMERGENCY LIGHTING BATTERY CAPACITY TEST FAILED. REPLACEMENT OF EPSU BATTERY 10WL IS REQUIRED. A3NB-33-3-6013 SEQ.:633 ZONE:200 EPSU BATTERY 10WL FAILED ON EMERGENCY LIGHTING BATTERY CAPACITY TEST AND REQUIRE REPLACEMENT. PERFORMED EPSU BATTERY REPLACEMENT 10WL, IAW AMM:33-51-38-000-002/ 33-51-38-400-002 REV. 122. TEST SATIFACTORY.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 92,146 hrs · 36,036 cycles

CABIN LIGHTS EMERGENCY CAPACITY TEST FAILED. REPALCEMENT OF EPSU BATTERY. (10WL) IS REQUIRED. (A3NB-33-3-6013) SEQ:633 ZONE:200 EPSU BATTERY (11WL) FAILED ON EMERGENCY LIGHTING BATTERY. WORK RECORDED ON UAL LOGPAGE CAPACITY TEST AND REQUIRE REPLACEMENT. PREFORMED EPSU BATTERY REPLACEMENT (11WL), IAW AMM:33-51-000-002/ 33-51-38-400-002 REV 122. TEST SATISFACTORY.

Part: EPSU — FAILED (12WL) · airframe 92,146 hrs · 36,036 cycles

CABIN LIGHTS EMERGENCY LIGHTING CAPACITY TEST FAILED. REPLACEMENT OF EPSU BATTERY. 10WL IS REQUIRED. A3MB-33-3-6013 SEQ: 633 ZONE:200 EPSU BATTERY 12WL FAILED ON EMERGENCY LIGHTING BATTERY CAPACITY TEST AND REQUIRE REPLACEMENT. PERFORMED EPSU BATTERY REPLACEMENT 12WL, IAW AMM:33-51-38-000-002/ WORK RECORDED ON UAL LOGPAGE# 6111818 33-51-38-400-002 REV. 122. TEST SATIFACTORY.

Part: FITTING — CRACKED (LH ELEVATOR) · airframe 92,146 hrs · 36,036 cycles

LH ELEVATOR INBD SERVO CONTROL HINGE FITTING BOLT ANTI ROTATION FOUND WITH CRACK, REQUIRES FURTHER EVALUATION. TASK PERFORMED BY LHT EMP 5P0722 & INSP BY LHT EMP 5H0619 AS RECORDED ON LTPR NR# 5001264906-0020. DURING INSPECTION OF LH ELEVATOR, FOUND CRACK ON LOCKING LUG OF LH ELEVETOR ACTUATOR FITTING. PREFORMED REPAIR ON DAMAGE LUG AS PER SRM TASK 55-26-47-300-001 REV. THE REPAIR IS CATEGORY A WORK ACCOMP BY V933327.

Part: LANYARD — LOOSE (ACCESS PANEL) · airframe 90,070 hrs · 35,051 cycles

SEAL DANGLING ON A/C BELLY. RESECURED LOOSE LANYARD STRAP ON LH ACCESS BELLY PANEL.

Part: NONE — NONE (ALL LAVS) · airframe 89,314 hrs · 34,674 cycles

ALL LAVS INOP/WILL NOT FLUSH ON ARRIVAL FOUND FAP INOP LIGHT ON AND WASTE TANK INDICATION PRECHARGE OF 5 GALLONS AND TANK READ 15% AT FAP PANEL. ALLOWED FULL 100%. HAD LAV SERVICE DRAIN AND FLUSH TANK. TANK READ OVER 15% WITH 3 GALLONS. ALL 20% EMPTY. HAD LAV SERVICE FILL WITH 20 GALLONS AND FLUSHED ICE LAVS FLUSH NORMAL. AND VINEGAR DOWN EACH TOILET. LAV SERVICE DUMPED AND PUT IN

Part: FILTER — ODOR (EE BAY) · airframe 87,896 hrs · 34,027 cycles

EXHAUST FUMES IN COCKPIT SMOKE ODOR FORM PICTURES. CARTRIDGES. REF. AMM-21-21-41/401 CONFIG 00. ACCOMPLISHED REMOVAL/INSTALLATION OF BOTH RECIRCULATION FILTER CARTRIDGES. REF. AMM-21-21-41/401 CONFIG 00. ACPLISHED TASK CARD 05-50-00-810-831-A NO ODOR NOTED

Part: BATTERY PACK — NONE (R2 DOOR (M33098)) · airframe 86,846 hrs · 33,511 cycles

BRAKE 2 OVERHEATED ONCLIMB DEN THEN ONPARKING SLC WAS 420..BRAKE 1 350 UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. REF MT 32-001 FOR POSSIBLE DRAGGING BRAKES , PLEASE JACK ACFT UP AND ATTEMPT TO ROTATE IF YOU FEEL ANY GRABBING PLEASE REPLACE BRAKE OR DEFER REF MEL 3242D AND DEACTIVATE BRAKE CONTRACT TECHNICIAN SEAN V920011 CONFIRMED BRAKE IS GRABBING REF MT 32-001 ADD EMP:V920011 E UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN E E UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V907926 MAC RELATED WORK ORDER 000000003020338 AND PRTR MARTIN, ERIC (V907926), FOUND BRAKE LOCKING UP DEACTIVATED PER MEL 3242G AND AMM 32-42-00. FOR GREEN SYS SEE LOGPAGE # 7109334 FOR YELLOW SYS MARTIN, ERIC (V907926), FOUND BRAKE LOCKING UP DEACTIVATED PER MEL 3242G AND AMM 32-42-00. FOR GREEN SYS SEE LOGPAGE # 7109334 FOR YELLOW SYS DISPATCH DESK: 12 NAME: KA DATE: 23-SEP-21- DEFERRED DIRECTLY BY TOMC

Part: CONNECTOR — DAMAGED (OXYGEN BOTTLE) · airframe 83,124 hrs · 31,841 cycles

CREW REPORTS O2 BOTTLE HAS DAMAGED CONNECTOR UPDATED MAA CODE CRW USING VENDOR MAA SCREEN WORKING ITEM WITH CREW BOTTLE CONSIDERED INOP. NEEDS NEW MASK ASSY. BOTTLE IS IN PLACE AND PLACARDED. BOTTLE LOCATED AFT CABIN NOC DATE: 31-OCT-19- MEL APPROVED BOTTLE PLACRDED PER MEL R/R AFT GALLEY PORTABLE O2 BOTTLE IAW AMM 35-30-00 LEAK CHECK GOOD. NEW MASK INSTALLED.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 83,022 hrs · 31,798 cycles

EPSU L AND R FAIL P TP SYSTEM LIGHT CHECK REMOVED AND REPLACED LEFT AND RIGHT EPSU''S (11WL AND 12WL) AND L EFT AND RIGHT EPSU BATTERIES IAW AMM 33-51-38-000-001-A, 33 -51-38-400-001-A, 33-51-38-000-002-A, AND 33-51-38-400-002-A. PE RFORMED OPS CHECK OF THE EMERGENCY SUPPLY UNITS BY BITE CHECK IAW A320 AMM 33-51-00-710-001-A. OPS CHECK GOOD.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 77,946 hrs · 29,540 cycles

EMERGENCY L MSG ON EMERGENCY BATT TEST AT CIDS PANEL. REMOVED AND REPLACED EMERGENCY BATT PACK 11WL REF AMM 33-51-38 OPS CHECK GOOD.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHT) · airframe 77,578 hrs · 29,360 cycles

OVERWING EPSU FAULT ILLUMINATED DURING AN EMERGENCY LIGHT TEST. REPLACED LEFT OVERWING EPSU. REPLACED THE RT OVERWING EXIT SIGNS AND OVERWING CENTER EXIT SIGN IAW AMM 33-51-38-400-001-A, SYSTEM CHECKED GOOD.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 77,335 hrs · 29,235 cycles

L1 DOOR DAMPER EMERGENCY OPERATION CYLINDER FOUND WITH LOW PRESSURE AND DISARM LEVER STICKING. REMOVED AND REPLACED THE CYLINDER IAW AMM 52-11-14-400-001-A , CHECKED OK.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 77,335 hrs · 29,235 cycles

EMERGENCY POWER SUPPLY UNIT AT THE L1 DOOR, FAULTED ON CIDS. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33=51-38, OPS CHECKED NORMAL.

Part: PIN — DAMAGED (CONNECTOR) · airframe 77,236 hrs · 29,180 cycles

EMERGENCY LIGHTS TEST FAILED FOR AFT LT EXTERIOR LOADS. R & R THE EPSU 13WL. R & R THE BATTERY 13WL. R & R THE AFT R2 DOOR SLIDE. REPAIRED THEWIRING AT LAVATORY D, AFT EMERGENCY LIGHTS PIN E ON CONNECTOR 7202VC & FLOOR LIGHT EQNVR1, WIRE 4106-A20. EPSU & BATTERY AT 13WL CHECKED GOOD. EMERGENCY LIGHTS CHECKED GOOD IAW TSM 33-51-00, AWM 33- 51-08, AWM 25-43-01, AMM 33-51-38-002-A, 000-001-A, 400-002-A, 4 00-001-A, 25-62-44-000-804-A, 860-078-A, 020-087-A, 400-803-A, AND 33-51-00-710-001-A,

Part: RETAINER — BROKEN (L1 DOOR SLIDE) · airframe 77,236 hrs · 29,180 cycles

L1 DOOR SLIDE HAS BROKEN RETAINING CLIP FOR THE DECORATIVE COVER. REMOVED AND REPLACED TH EL1 DOOR SLIDE IAW AMM 52-62-44-40 0-007-A, AND 52-62-44-000-007-A.

Part: EPSU — FAULTY (EMERGENCY LIGHTS) · airframe 77,236 hrs · 29,180 cycles

EPSU 11WL FAULTED. R & R THE EPSU.

Part: BUCKLE — BROKEN (L1 DOOR SLIDE) · airframe 77,236 hrs · 29,180 cycles

L1 DOOR SLIDE HAS A BROKEN BUCKLE. REPLACED THE DOOR SLIDE ASSY.

Part: SKIN — CORRODED (FRAMES 27-28) · airframe 77,236 hrs · 29,180 cycles

FORWARD CARGO BAY INNER SKIN FRAMES 27 TO 28 BETWEEN STRINGERS 38L TO 38R HAS FASTENERS WITH CORROSION. REMOVED AND REPLACED THE FASTENERS ON THE SKIN AND REMOVED AND REPLACED ONE SHEAR TIE FRAME 28 BETWEEN STRINGERS 39 AND 40L IAW SRM 53-21-12-001, 51-44-11, AND 51-42-11. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-42-11 PAR 2E.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 77,236 hrs · 29,180 cycles

FWD CARGO PIT HAS A CORRODED SHEAR TIE FR 28 BETWEEN STR 40R-41R, FWD CARGO CLEAT AT FR28 STR40R-41R FOUND TO BE OUT OF LIMITS IAW SRM 51-73-11-001. REMOVED AND REPLACED CLEAT IAW A320 SRM 5 1-42-11-001.

Part: SHEAR TIE — CORRODED (FRAME 30) · airframe 77,236 hrs · 29,180 cycles

FWD CARGO COMPARTMENT INNER BOTTOM SKIN BETWEEN STRINGERS R40-R41 AND FR30 , HAS SHEAR TIE WITH CORROSION. UPON INSPECTION OF FR30 STR 40R-41R IT WAS FOUND THAT THE SHEAR TIE WAS CORRODED IAW A320 SRM 51-73-11-001 AND WAS REMOVED A320 SRM 51-42-11-001 PG 1 FIG 00109 AND REPLACED WITH NEW SHEAR TIE ON FR30R IAW A320 SRM 51-42-11-001 PG 6 PART 2.

Part: SHEAR TIE — CORRODED (FRAME 34) · airframe 77,236 hrs · 29,180 cycles

FWD CARGO BAY HAS A CORRODED SHEAR TIE FRAME 34 BETWEEN STRINGERS 41 - 42R. REMOVED CORROSION FROM SHEAR TIE, ORIGINAL THICKNESS .055", MINIMUM ALLOWABLE REMAINING THICKNESS .051", ACTUAL REMAING THICKNESS .045" FOUND TO BE OUT OF LIMITS IAW A320 S RM 51-73-11 AND AIRBUS DWG D53230513. REMOVED AND REPLACED SHEAR TIE IAW A320 SRM 51-42-11.

Part: FITTING — CORRODED (FUSELAGE) · airframe 77,236 hrs · 29,180 cycles

AFT CABIN R2 DOOR SILL FWD CORNER FITTING AT FR 66 HAS CORROSION. REMOVED & REPLACED AFT CABIN R2 DOOR SILL FWD CORNER FITTING AT FR66 IAW SRM 51-72-11-911-001 PARA 2.

Part: FITTING — CORRODED (FUSELAGE) · airframe 77,236 hrs · 29,180 cycles

AFT CABIN R2 DOOR SILL AFT CORNER FITTING AT FR 68 HAS CORROSION. REMOVED & REPLACED AFT CABIN R2 DOOR SILL AFT CORNER FITTING IAW SRM 51-72-11-911-001 PARA 2.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 77,236 hrs · 29,180 cycles

AFT PIT SKIN/STRAP CORRODED AFT SIDE OF FR64, STR43L-SRT43R. REMOVED AND REPLACED BUTT-STRAP AT FR64 STR 42R-32L IAW SRM 51-42-11.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,236 hrs · 29,180 cycles

AFT CARGO UNDER FLOOR AREA, SURFACE CORROSION ON STRINGER 38R BETWEEN FR59-60. REMOVED AND REPLACED STR 38R FR58-64 IAW SRM 51-42-11.

Part: FITTING — CRACKED (FRAME 68) · airframe 77,236 hrs · 29,180 cycles

RIGHT AFT PASSENGER DOOR CUTOUT FRAME 68 DOOR STOP FITTING NR 1 OTBD LOWER HOLE CRACKED AT 6:00. REPAIRED IAW SRM 53-41-12-300-001.

Part: DOOR — DELAMINATED (RT OVRWNG SLIDE) · airframe 77,236 hrs · 29,180 cycles

RIGHT OVERWING SLIDE DOOR IS DELAMINATED.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,236 hrs · 29,180 cycles

AFT CARGO UNDER FLOOR AREA, SURFACE CORROSION ON STRINGER 43L BETWEEN FR54-60. REMOVED AND REPLACED SECTION OF STR 43L BTW FR54-60 IAW SRM 51-72-11, 51-42-11 AND 53-41-13-001.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,236 hrs · 29,180 cycles

AFT CARGO UNDER FLOOR AREA, THREE SPOTS OF SURFACE CORROSION STRINGER 42L BETWEEN FR57-58. REMOVED AND REPLACED 42L AFT SPLICE AND CLEAT AT FR 59. ALSO REPLACED 42L STRINGER IAW SRM 51-42-11.

Part: DOOR SILL — CORRODED (FRAME 68) · airframe 77,236 hrs · 29,180 cycles

FRAME 68 FWD FACE AT DOOR SILL STRINGER 23R HAS CORROSION. INSTALLED A REPAIR IAW SRM 53-41-12-300-002.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 77,236 hrs · 29,180 cycles

FWD CARGO UNDER FLOOR AREA, SHEAR TIE, FRAME 32, BETWEEN STRINGERS 41 - 42L HAS A SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51 -42-11-001, PG 1, FIGURE 00109 AND SRM 51-73-11-001.

Part: ATTACH ANGLE — CORRODED (FRAME 70) · airframe 77,236 hrs · 29,180 cycles

AFT CABIN RT AFT SHEAR WEB ATTACH ANGLE HAS CORROSION ON BOTTOM SIDE AT FRAME 70. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-72-11-911- 001, PARA 2.

Part: DOOR SILL — CORRODED (FWD CARGO) · airframe 77,236 hrs · 29,180 cycles

FWD CARGO DOOR SILL HAS CORROSION SPOTS ON UPPER FACE. REMOVED AND REPLACED FWD CARGO DOOR SILL IAW A320 SR M 51-42-11.

Part: STRINGER — CORRODED (FRAMES 31-32) · airframe 77,236 hrs · 29,180 cycles

FWD CARGO COMPARTMENT INNER BOTTOM STRINGER 43R BETWEEN FRAMES 31 - 32 HAS CORROSION, REMOVED & REPLACED THE STRINGER IAW SRM 5 1-42-11, REV 119.

Part: DOOR SILL — CORRODED (R2 DOOR) · airframe 77,236 hrs · 29,180 cycles

AFT CABIN R2 DOOR SILL HAS CORROSION. REMOVED AND REPLACED THE R2 DOOR SILL IAW SRM 51-42- 11, PARA 2E.

Part: DOOR SILL — CORRODED (AFT CABIN) · airframe 77,236 hrs · 29,180 cycles

AFT CABIN, R2 DOOR SILL HAS MULTIPLE AREAS OF CORROSION AT FRAMES 66 & 68. REMOVED & REPLACED AFT THE DOOR SILL IAW SRM 51-42-11- 001.

Part: SHEAR TIE — CORRODED (FRAME 30) · airframe 77,236 hrs · 29,180 cycles

SHEAR TIE CORRODED BEYOND LIMITS 50% MATERIAL LOSS AT FRAME 30, STRINGER 41-42R. REMOVED AND REPLACED THE SHEAR TIE IAW 51-42-11-001, REV 119, AND SRM 51-44-11-001.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 77,236 hrs · 29,180 cycles

FWD CARGO UNDER FLOOR AREA, SHEAR TIE, FRAME 32 BETWEEN STRINGERS 40 - 41L HAS A SURFACE CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-42-11-001 AND SRM 5 1-44-11-001, REV 119.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 77,236 hrs · 29,180 cycles

FWD CARGO, SHEAR TIE, FRAME 32 BETWEEN STRINGERS 42 - 43L HAS A SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-42-11-001, REV 119, AND SRM 51-44-11-001, REV 119.

Part: SHEAR TIE — CORRODED (FRAME 26) · airframe 77,236 hrs · 29,180 cycles

FORWARD CARGO COMPARTMENT INNER SKIN FRAME 26 BETWEEN STRINGERS 41 TO 42R. SHEAR TIE CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-42-11-001.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 77,236 hrs · 29,180 cycles

FWD CARGO BAY INNER BOTTOM SHEAR TIE CORRODED AT FRAME 32 BETWEEN STRINGERS 41 - 42R. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-42-11-001, AND SRM 51-44-11-001, REV 119.

Part: FITTING — CORRODED (FRAME 69) · airframe 77,236 hrs · 29,180 cycles

AFT CABIN L2 DOOR SILL AFT CORNER FITTING HAS CORROSION FRAME 69. REMOVED AND REPLACED THE FITTING IAW SRM 53-41-79-001, ITEM 355, AND 51-77-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 77,236 hrs · 29,180 cycles

FWD CARGO SKIN AT FRAME 31, BETWEEN STRINGERS 41- 42R, SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-42-11-001, AND SRM 51-44-11-001.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 77,236 hrs · 29,180 cycles

FWD CARGO BAY INNER BOTTOM SKIN AT FRAME 31 AND BETWEEN STRINGERS 40 - 41R, SHEAR TIE HAS CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-42-11-001-A, AND SRM 51-44-11-001, REV 119.

Part: DOOR SILL — CORRODED (FRAME 68) · airframe 77,236 hrs · 29,180 cycles

AFT CORNER FITTING OF L2 DOOR CORROSION IS PRESENT IN AREA OF FRAME 68. REMOVED AND REPLACED DOOR SILL IAW SRM 53-41-14-001, ITEM 18, AND 51-72-11-911-00

Part: SHEAR TIE — CORRODED (FRAME 27) · airframe 77,236 hrs · 29,180 cycles

FWD CARGO, SHEAR TIE FRAME 27 BETWEEN STRINGERS 42 - 43R HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW 320 SRM 51-42-11-001, REV 119.

Part: SHEAR TIE — CORRODED (FRAME 29) · airframe 77,236 hrs · 29,180 cycles

SHEAR TIE FRAME 29 BETWEEN STRINGERS 42 - 43R HAS A SURFACE CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 51-73 -11, AND DRAWING D53230398. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51- 42-11 PAR 2E.

Part: SHEAR WEB — CRACKED (FRAME 68) · airframe 77,236 hrs · 29,180 cycles

AFT CABIN RT AFT SHEAR WEB IS CRACKED AT FRAME 68 ON BOTTOM SIDE. REMOVED AND REPLACED THE SHEAR WEB IAW SRM 51-72-11-911-001, PARA 2.

Part: DOOR SILL — CORRODED (L2 DOOR) · airframe 77,236 hrs · 29,180 cycles

AFT CABIN L2 DOOR SILL HAS CORROSION AT AFT END. DOOR SILL BEYOND LIMITS, 50 PERCENT MATERIAL LOSS. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-73-11-0 01, AND 51-72-11-911-001.

Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 76,701 hrs · 28,946 cycles

EMERG EXIT LIGHTS CYCLING CABIN WITH CABIN ALT WARNINGS NORMAL. OPS TEST OF EMERG LIGHTS TEST GOOD REF AMM 33-51-00-710-001-A.

Part: COFFEEMAKER — INOPERATIVE (GALLEY) · airframe 76,273 hrs · 28,747 cycles

FA REPORTS FWD COFFEEMAKER INOP. NO CB POP BUT REPORTED POSSIBLE ELEC SMELL PRIOR . REPLACED COFFEEMAKER.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 75,864 hrs · 28,567 cycles

EMERG PWR SUPPLY 10WL FAILED TEST. REPLACED POWER SUPPLY 10WL REF AMM 33-51-38.

Part: CONTROL VALVE — FAILED (HYD SYSTEM) · airframe 74,189 hrs · 27,811 cycles

LEVEL CRUISE FLIGHT AT FL360, HYD RESERVOIR LOW LEVEL ECAM DISPLAYED. SECURED THE HYD SYSTEM, DECLARED EMERGENCY AND DIVERTED. R & R THE NR 2 THRUST REVERSER HYDRAULIC CONTROL VALVE AND ENGINE HYDRAULIC PUMP. CHANGED CASE DRAIN FILTER WITH NO DEBRI NOTED.

Part: SKIN — DENTED (CARGO DOOR) · airframe 72,398 hrs · 26,996 cycles

FORWARD CARGO DOOR OUTER SKIN SURFACE FRAME 27 & RIB 3 - 4 HAS DENT. DENT ON FWD CARGO DOOR OUTER SKIN SURFACE WAS OUT OF LIMITS IAW SRM 52-30-00 PARA 4 E FIG 105. REPAIRED INSTALLING A REPAIR DOUBLER IAW SRM 52-31-00 PARA 5 I FIG 209.

Part: SKIN — DENTED (CARGO DOOR) · airframe 72,398 hrs · 26,996 cycles

FORWARD CARGO DOOR, OUTER SKIN SURFACE, FRAME 25A & RIB 4 - 5 HAS DENT. DENT ON FWD CARGO DOOR OUTER SKIN SURFACE OUT OF LIMITS IAW SRM 52-30-00 PARA 4 E FIG 105. REPAIRED INSTALLING A REPAIR DOUBLER IAW SRM 52-31-00 PARA 5 I FIG 209.

Part: FLAP — FAULTED (WING) · airframe 67,505 hrs · 25,044 cycles

FLAP CONTROL FLAPS LOCKED ALIGNMENT FAULT ON ECAM.

Part: STRUT — OUT OF RIG (TE FLAP) · airframe 67,481 hrs · 25,034 cycles

AIR RETURN DUE TO INABILITY TO RETRACT FLAPS AFTER TAKEOFF IAW TSM27-51-00-810, PERFORMED STEP 6 PG 3. LT & RT INTERCONNECTING STRUTS TO BE OUT OF RIG. RIGGED IAW MM27-51-44-820-001-A. ALL CHECKED NORMAL.

Part: ATTACH BOLT — CORRODED (NLG) · airframe 67,042 hrs · 24,870 cycles

NLG LEG ASSEMBLY DOOR LONG ATTACH BOLT CORRODED. NEW BOLT COMES FROM THE VENDER TEMP INSTALLED IN GEAR LEG.

Part: OIL SYSTEM — LEAKING (LT ENGINE) · airframe 66,992 hrs · 24,849 cycles

OIL STREAK RUNNING FROM BENEATH DRAIN MAST ON INSIDE SIDE OF LT ENG. RESIDUAL OIL FROM THE COWLING VENT AREA, SMALL AMOUNT. OIL QTY CHECKED AT TANK, TANK IS FULL. REVIEW OF PLENOIL, ENG IS OPERATING AT 0.03 QTS PER HR WELL WITHIN LIMITS. CLEANED AREA, OK TO CONTINUE.

Part: STRIKER — FAULTY (COCKPIT DOOR) · airframe 66,498 hrs · 24,646 cycles

COCKPIT DOOR 'FAULT' LIGHT & DOOR CONTROLLER 'MID STRIKE' LIGHT IS ON. REPLACED MID STRIKER & TESTED IAW MM 52-51-12-400, ALL NORMAL.

Part: ACTUATOR — FAULTY (NR 2 ENGINE) · airframe 66,141 hrs · 24,510 cycles

COMPRESSOR VANE DISPLAYED ON UPPER ECAM SCREEN. ENG PARAMETERS ABNORMAL, ENG NR 2. REPLACED NR 2 ENG VSV ACTUATOR IAW AMM.

Part: STRAP — OUT OF POSITION (DOOR) · airframe 66,074 hrs · 24,487 cycles

ALL FOUR DOORS, COULD NOT LOCATE SURVIVAL PACK ATTACH POINT STRAP. REPOSITIONED STRAPS AROUND TRIGGER MECH.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 66,032 hrs · 24,469 cycles

FIRST OFFICER`S OXYGEN MASK HAS LEAK & DOESN'T EXPAND FOR PROPER FIT AROUND HEAD. SWAPPED FIRST OFFICER`S WITH FIRST OBSERVER`S. FIRST OFFICERS` OPERATIONS CHECKED GOOD. DEFERRED STICKER FIRST OBSERVER`S SEAT INOPERATIVE. REPLACED FIRST OBSERVER`S MASK IAW MM.

Part: LINER — DETACHED (THRUST REVERSER) · airframe 65,857 hrs · 24,405 cycles

NR ENGINE INNER LINER OF FAN CASE IS DETACHED, 4 O'CLOCK POSITION VIEWED FROM REAR. TAPED DELAMINATED SECTION OF LINER WITH SPEED TAPE IAW MT 78-010 PAR 3.

Part: A/C PACK — LOW PRESSURE · airframe 65,590 hrs · 24,304 cycles

CONT TEMP IS COLD BUT LOW AIRFLOW MAKES COCKPIT VERY HOT. EXTERNAL AIR IS ALSO VERY LOW FLOW.

Part: CONTROLLER — INOPERATIVE (PACK TEMP) · airframe 65,586 hrs · 24,302 cycles

PACK LOW FLOW. UNACCEPTABLE TEMP, COCKPIT TEMP 89 DEGREES, CABIN TEMP 82 IN CLIMB. LT PACK OUT TEMP RUNNING +5 DEG. RT 10, R & R NR 1 PACK TEMP AND ZONE TEMP CONTROL IAW AMM. OPS CHECKED GOOD.

Part: CONTROLLER — FAILED (WINDSHIELD HEAT) · airframe 65,311 hrs · 24,193 cycles

RT WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN. REPLACED NR 2 WINDSHIELD HEAT CONTROLLER , OPS OK.

Part: FAN — NOISY (CARGO BAY) · airframe 65,261 hrs · 24,174 cycles

AFT CARGO EXTRACTION FAN MAKING VERY LOUD NOISE. DEACTIVATED AFT CARGO EXTRACTION FAN BY PULLING OPEN CB AFT CARGO VENT & HEATING CONTROL CB ON PANEL 122VU S22. PARTS: 565-9012, MR21270. (FAN)

Part: MANIFOLD — LEAKING (HYD SYSTEM) · airframe 65,047 hrs · 24,095 cycles

GREEN SYS QTY WAY BELOW MINIMUM. FOUND LEAK AT MANIFOLD GROUND SERVICE VALVE. REMOVED GROUND LEAKAGE MEASUREMENT MANIFOLD OF GREEN HYD SYS IAW MM. INSTALLED GROUND LEAKAGE MEASUREMENT MANIFOLD OF THE GREEN HYD SYS IAW MM, OPS AND LEAK CHECKED GOOD.

Part: WINDSHIELD WIPER — MALFUNCTIONED · airframe 64,910 hrs · 24,041 cycles

CAPTAIN`S WINDSHIELD WIPER WHEN SELECTED ON STICKS THEN JUMPS ON. ADJUSTED CAPTAIN`S WIPER ARM OK.

Part: FAN — FAILED (AVIONICS BAY) · airframe 64,610 hrs · 23,926 cycles

AVONICS SYSTEM FAULT DISPLAYED ON UPPER ECAM SCREEN. REPLACED VENT BLOWER FAN.

Part: COMPUTER — ODOR (AVIONICS) · airframe 64,610 hrs · 23,926 cycles

AVIONIC VENT ECAM WENT TO OVERRIDE, AN ODOR ELECTRICAL BURNING FROM VENT. REPLACED AEVC COMPUTER IAW AMM 21-26-34-401, CHECKED GOOD.

Part: KNOB — BINDING (AUTOFLIGHT) · airframe 64,329 hrs · 23,819 cycles

FCU ALTITUDE CONTROL KNOB VERY DIFFICULT TO PULL FOR OPEN DESCENT. LUBRICATED KNOB AND EXERCISED IN ALL DIRECTIONS. NO DIFFICULTIES IN MOVEMENT.

Part: STRUCTURE — DELAMINATED (RT ELEVATOR) · airframe 63,780 hrs · 23,601 cycles

CREW AND RAMP REPORT: RIGHT SIDE ELEVATOR TRAILING EDGE-LOWER-DELAMINATION OF FILLER MATERIAL EVIDENT-APPROX 1.5" BY .750" PIECE. TEMPORARY REPAIRED WITH SPEED TAPE REF 51-77-12 PAGE 4 AND 55-21-11. CF REF: SRM 51-77-12 P4. RCF-T :REINSPECTED TEMPORARY REP AIRE, NO PROGRESSION NOTED, TAPE SECURED.

Part: LEVER — BROKEN (O2 STOWAGE BOX) · airframe 63,308 hrs · 23,420 cycles

F/O OXYGEN MASK STOWAGE CONTAINER PRESS TO TEST LEVER BROKEN OFF. REPLACED F/O O2 MASK BOX PER MM. OPS AND LEAK CHECKED OK.

Part: SEAT BELT — DEFECTIVE (COCKPIT) · airframe 63,302 hrs · 23,418 cycles

CAPTAINS SEAT BELT WILL NOT LATCH. REPLACED CAPTAIN'S SEAT BELT.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 63,058 hrs · 23,331 cycles

SYSTEM 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. - CAB PR. CAB PR 1 SAMC TEXT: CFDS FAULTS OUTFLOW VALVE: 644-4602, REPLACE PER AMM. REMOVED AND REPLACED PRESSURIZATION OUTFLOW VALVE IAW AMM 21-31-51. CHECKS OK, NO FAULTS. ATA CHANGED TO SHOW HISTORY IN CHAPTER 21.

Part: COMPUTER — MALFUNCTIONED (NR 2) · airframe 62,654 hrs · 23,168 cycles

ELAC 2 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. F-CTL CREW COMMENTS: ATTEMPTED RESET ECAM MESSAGE RETURNED SAMC TEXT: CFDS SHOWS "27-44-00 THS ACTR POS ERROR 9CE OF ELAC 2" AT FLT PHASE 5. OPBLM SEE TSM 27-93-00-810-836A. REPLACED ELAC 2 & TESTED PER MM 27-27-00, CHECK'S OK. ACP CAT III AUTOLAND AND AFS TEST PER MM 22-97-00, TESTED OKAY.

Part: COMPUTER — FAULTY (ELAC) · airframe 62,567 hrs · 23,129 cycles

ELAC 1 FAULT. REPLACED NR 1 ELAC AND TEST AND TESTED OKAY.

Part: OUTFLOW VALVE — FAULTED (CABIN PRESSURE) · airframe 62,242 hrs · 23,009 cycles

HEARD & FELT LOW FREQUENCY RUMBLE. NO PRESSURE DIFFERENCES OFF ENGINE BLEED AIR. CPC 2 SYS IN CHARGE. REPLACED AVIONICS DUCT PER AMM. PRESSURIZED ALL DUCTS AND CHECKED FOR ADDITIONAL LEAKS -NONE FOUND. PERFORMED AVIONICS EQUIPMENT VENTILATION ADJUSTMENT AND TEST PER AMM, OPS CHECKED GOOD.

Part: TRANSCEIVER — WEAK (VHF COMM) · airframe 59,969 hrs · 22,174 cycles

VHF1 TRANSMIT WEAK AND UNREADABLE FROM BOTH CAPT AND F/O SIDES. VHF2 PERFECT. REPLACED NR 1 VHF TX PER AMM.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 59,566 hrs · 22,004 cycles

PANEL 191AB REMOVED FOR REPAIR. SECURED PANEL 191AB ON AIRCRAFT.

Part: SWITCH — OUT OF ADJUST (RAT) · airframe 59,428 hrs · 21,952 cycles

RAT WILL NOT STOW, AFTER OPS CHECK. ADJUSTED RAT LEG POSITION SWITCH. OPS NORMAL.

Part: FITTING — OUT OF ADJUST (CABIN) · airframe 59,157 hrs · 21,829 cycles

RIGHT AFT SLIDE INDICATION INOP ON DOOR-OXY SYSTEM ECAM PAGE - DOOR-OXY. CREW COMMENTS: AFT DOOR ARMING HANDLE DOES NOT REMAIN INCORRECT POSITION-INTMT SLIDE NOT ARMED INDICATION - (DEFERRED). ADJUSTED FWD AND AFT GIRT BAR FLOOR FITTING. ARM AND DISARMED OPERATION NORMAL. INSPECTED INSTALLATION PER METHOD NR 4. INDICATIONS AND OPERATION NORMAL.

Part: TRIGGER — LACK OF LUBE (R2 DOOR) · airframe 58,996 hrs · 21,766 cycles

DOOR 2R SHOWING DISARMED IN FLT. F/A PUSHED ON ARMING LEVER AND SHOWING OKAY. REPEAT FROM 14 JUL. LUBED DOOR ARMING SLIDING TRIGGER ASSY PER AMM, OPS NORMAL.

Part: CONTROL PANEL — FAULTED (AUDIO) · airframe 58,393 hrs · 21,523 cycles

F/O ACP TRANSMISSION BUTTON GREEN LIGHTS DO NOT ILLUM. LIGHT UP WHEN TESTED. REPLACED F/O'S ACP. TESTS OK.

Part: SLIDE — CRACKED (OVERWING EXIT) · airframe 58,106 hrs · 21,406 cycles

ON PRE-DEPARTURE RT OVERWING ESCAPE SLIDE AFT EDGE HAS 8.5 INCH CRACK, OUT OF LIMITS. NOTE CRACK IS IN AREA 2. REPLACED RT SLIDE PER MM. INSP AND FORMAN PRESENT. ELEC CONNECTOR AND HOSE INSTALLED.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 57,489 hrs · 21,148 cycles

EMERGENCY LIGHT CHECK FAILED INT LOADS AFT L 33-51-38. T/S FOUND WIRING UNDER SEAT 19ABC DAMAGED. REPAIRED WIRING, EMERGENCY LIGHT PASS 3 SERVICE TEST FROM FWD F/A PANEL.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,785 hrs · 20,855 cycles

AFT FUSELAGE BILGE FRAME 67 AT CTR LINE AREA CORRODED. MAJOR REPAIR ACCOMPLISHED: REMOVED ANGLE, FABRICATED NEW PART, REF DWG D53480212236. INSTALLED IAW SRM.

Part: STRINGER — CORRODED (CARGO BAY) · airframe 56,785 hrs · 20,855 cycles

AFT PIT BILGE FROM FR 53 - 60, STR 42L IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED STR SECTION. LOCATED, DRILLED, AND INSTALLED NEW SECTION IAW SRM.

Part: STRINGER — CORRODED (S43L) · airframe 56,785 hrs · 20,855 cycles

AFT PIT STRINGER 43L CORRODED BETWEEN FR54 AND FR60. MAJOR REPAIR ACCOMPLISHED: R & R CORRODED SECTION OF STR 43L, FROM FR54 TO FR60. WORK ACP ON NR B0246A BY MAE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,785 hrs · 20,855 cycles

AFT PIT STRINGER 44 IS CORRODED JUST FWD OF FR64. MAJOR REPAIR ACCOMPLISHED: SPLICED IN NEW SECTION OF STRINGER FROM FR 62 TO FR 64 PER SRM. WORK ACP ON NR B9845Z.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 56,678 hrs · 20,804 cycles

F/O RT REAR WINDOW DELAMINATED ON LWR EDG-APPEARS MILKY LIKE AN ELEC ARC MARK. REPLACED F/O RT REAR WINDOW.

Part: LATCH — OBSTRUCTED (SEAT 10C) · airframe 54,249 hrs · 19,774 cycles

LATCH ON EMERGENCY EQUIPMENT COMPARTMENT ABOVE SEAT 10C IS DEFECTIVE. REPOSITIONED ESCAPE ROPE IN COMPARMENT TO RELIEVE INTERFERENCE. LATCH OK.

Part: LANYARD — MISROUTED (R2 DOOR SLIDE) · airframe 54,068 hrs · 19,681 cycles

DOOR 2R WHITE SURVIVAL KIT LANYARD ROUTED THROUGH GIRT. SHOULD READ DOOR 2R. SECURED SURVIVAL KIT LANYARD.

Part: SLIDE — FRAYED (R1 DOOR) · airframe 54,068 hrs · 19,681 cycles

1R SLIDE SURVIVAL KIT LANYARD FRAYED AND MISSING ATTACHING VELCRO. DOOR 1R SLIDE REMOVED FOR REPLACEMENT. NEED SLIDE RAFT. NOT STOCKED. REMOVED OLD SLIDE, NEW SLIDE BAD, OUT OF STOCK WITH FRAYED LACING ON GIRT BAR AND SURVIVAL KIT LANYARD, NO OTHER SLIDE AT ORD. SLIDE ON AOG S1839. REPLACED SLIDE.

Part: CYLINDER — UNDERSERVICED (DOOR ASSIST) · airframe 53,930 hrs · 19,623 cycles

MED NR 2 LT DOOR EMERGENCY CYCL, ACCUMULATOR PRESS WAS FOUND TO BE LOW (READING 1500...SHOULD BE 1740 MIN). SVC'D BOTTLE TO PROPER PRESSURE.

Part: CYLINDER — LEAKING (CREW O2) · airframe 52,098 hrs · 18,807 cycles

CREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. CREW COMMENTS: CHRONIC AND LONG HISTORY - CREW OXYGEN PRESSURE LEAK 200 PSI LOSS IN 2.7 HRS. FOUND LEAK ON HIGH PRESS SIDE OF O2 SYSTEM. REPLACED O2 CYLINDER AND O2 TRANSMITTER AND PRESS REGULATOR. NO LEAKS NOTED AT THIS TIME.

Part: SEAL — LEAKING (BLEED AIR SYS) · airframe 50,903 hrs · 18,349 cycles

L WING LEAK DISPLAYED. FLIGHT DIVERTED. FOUND L WING BLD DUCT SEALS LEAKING INBOARD ON NR 1 PYLON, REF IPC 36-11-05-11B ITEM 220. REPLACED SEALS, NO LEAKS WITH APU BLEED ON, NO FAULTS, BMC1&2 GND TEST PASSED.

Part: FIRE BOTTLE — LOW (AFT LAV) · airframe 49,642 hrs · 17,840 cycles

AFT LAV FIRE BOTTLE IS SHOWING RED BAND. REPLACED AFT LAV FIRE BOTTLE. OKAY FOR SERVICE.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 49,322 hrs · 17,716 cycles

PRESSURIZATION PROBLEMS. FLIGHT DIVERTED. FOUND PFR FAULTING OUTFLOW VALVE 81. REPLACED OUTFLOW VALVE. OPS CHECKED GOOD.

Part: GIRT LACING — INADEQUATE (LT DOOR SLIDE) · airframe 49,320 hrs · 17,715 cycles

LT AFT DOOR SLIDE GIRT LACING. *S/D* SLIDE GIRT LACING INADEQUATE. NEW SLIDE INSTALLED.

Part: COMPUTER — FAILED (NR 2 ELAC) · airframe 48,942 hrs · 17,578 cycles

ELEVATOR - AILERON COMPUTER (ELAC) 2 INOP. CHANNEL 4 CPU FAILURE (INTERNAL) ON ELAC 2. REPLACED ELAC 2, OPS CHECKED GOOD.

Part: HYDRAULIC LINE — LEAKING (NR 2 ENGINE) · airframe 48,938 hrs · 17,577 cycles

YELLOW SYSTEM PRESSURE & QTY LOSS IN CRUISE. FLIGHT DIVERTED. LEAK ON HYD LINE ON NR 2 ENGINE. FOUND HYDRAULIC LINE ON ENGINE LEAKING. REPLACED LINE. ALSO, REPLACED NR 2 ENGINE HYDRAULIC PUMP, CHECKED HYDRAULIC CONTROL UNIT FILTER, CASE DRAIN FILTRT AND HP FILTER. ALL HAD NO PARTICLES. REPLACED FILTERS PRECAUTIONARY.

Part: OXYGEN SYSTEM — LOW PRESSURE (CREW O2) · airframe 48,931 hrs · 17,574 cycles

CREW OXYGEN SYSTEM LOW. RECORD PRESSURE PRIOR TO SERVICING. CREW COMMENTS: O2 IS 1480 PSI. SERVICED CREW O2 TO FULL, NO LEAKS WERE NOTED AT TIME OF SERVICE.

Part: LINE — LEAKING (OIL SYSTEM) · airframe 48,506 hrs · 17,417 cycles

A/C LOSING OIL QUANTITY. FLIGHT DIVERTED. OIL SUPPLY PRESSURE TUBE FOUND DAMAGED AND LEAKING. TUBE REPLACED CORRECT THIS CONDITION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,376 hrs · 17,369 cycles

SEAT MOUNTED FLOOR PROXIMITY EMERGENCY ESCAPE PATH LIGHT OUT AT SEAT 2B. REPLACED AFT LIGHT ASSY.

Part: WIRE — SHORTED (OXYGEN MASK) · airframe 48,312 hrs · 17,345 cycles

F/O'S OXYGEN MASK MICROPHONE IS INOPERATIVE. FOUND INTERNAL SHORT. REPLACED FO MASK.

Part: DISK — DISLODGED (APU FIRE BOTTLE) · airframe 48,285 hrs · 17,337 cycles

APU FIRE BOTTLE DISK DISLODGED. SUPPLEMENTAL DATA UPDATE, CAUSE, DISK WAS DETERIORATED. REPLACED FIRE BOTTLE DISK.

Part: OXYGEN SYSTEM — LOW (CREW O2) · airframe 47,189 hrs · 16,987 cycles

THE O2 LOW. SERVICED CREW O2 TO FULL.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 46,335 hrs · 16,678 cycles

FOUND CABIN EMERGENCY LIGHTS CHECK FAILED BATTERY PACK FWD LT. 10-19-07 REPLACED BATTERY PACK.

Part: DOOR — DAMAGED (RT MLG) · airframe 45,437 hrs · 16,342 cycles

RIGHT MLG MAIN DOOR & UPPER SIDE DOOR FOUND DAMAGED UPON ARRIVAL. REPLACED RT MLG FIXED AND SECONDARY HINGED FAIRINGS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,159 hrs · 16,242 cycles

EMERGENCY EXIT LIGHTS AT BOTH OVERWING CENTER AISLE LOCATIONS AND LT OVERWING EXIT HAVE INOP LAMPS. RELAMPED, OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,159 hrs · 16,242 cycles

EMERGENCY LIGHTS AT SEATS 3B, 12C AND 16C HAVE INOPERATIVE LAMPS. RELAMPED, OPS NORMAL.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 44,753 hrs · 16,088 cycles

LOWER KEEL BEAM FAIRING SUPPORT ANGLE RIGHT SIDE AT FRAME 46 IS CRACKED. MAJOR REPAIR ACCOMPLISHED: REPLACED ANGLE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 44,753 hrs · 16,088 cycles

LOWER KEEL BEAM FRAME 47 FAIRING ATTACH ANGLE LEFT SIDE IS CRACKED. MAJOR REPAIR ACCOMPLISHED: REPLACED ANGLE.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 44,339 hrs · 15,938 cycles

NR 2 ENGINE HAD A COMPRESSOR STALL WITH AN AUDIBLE BANG. [SUP 06-01-07] INSPECTED ENGINE PER AMM TASK FOR STALL CONDITION AND FOUND NO DEFECTS. LUBED VARIABLE STATOR VALVE MECHANISM AND PERFORMED IDLE RUN CHECK. NO FURTHER IRREGULARITIES NOTED.

Part: EXTINGUISHER — MISINSTALLED (NR 1 ENGINE) · airframe 44,188 hrs · 15,886 cycles

NR 1 ENGINE FWD FIRE EXTINGUISHER BOTTLE SAFETY RELIEF VALVE FOUND WITH A METAL CAP STILL INSTALLED. [SUP 05-27-07] REMOVED METAL CAP AND REINSTALLED FIRE EXTINGUISHER BOTTLE. AT THE PREVIOUS C-CHECK ON 9/13/2005, THE NR 1 ENGINE FWD BOTTLE WAS ACCIDENTALLY DISCHARGED AND REPLACED WITH A NEW ONE. INSPECTION OF THE NEW BOTTLE WAS INADEQUATE, ALLOWING THE AIRCRAFT TO RETURN TO SERVICE WITH THE METAL CAP LEFT ON THE RELIEF VALVE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 44,007 hrs · 15,825 cycles

RTFL DUE TO A MAIN LANDING GEAR INDICATION. [SUP 05-16-07] ALL DOOR INDICATORS WERE AMBER. ALL INDICATORS GREEN AFTER SECOND ATTEMPT. CREW STATED THAT IT SEEMED THAT ALL GEAR RETRACTED BUT DOORS REMAINED OPEN SUPPLEMENTAL DATA UPDATE FAULT TRACED TO OUT OF ADJUSTMENT NOSE LANDING GEAR PROXIMITY SENSOR. MAIN LANDING GEAR PROXIMITY SENSORS WERE CHECKED AS A PRECAUTION WITH NO FAULTS FOUND. ADJUSTED NOSE GEAR PROXIMITY SENSOR TO PROPER CLEARANCES.

Part: CHARGER — FAILED (CABIN) · airframe 44,007 hrs · 15,824 cycles

EMERGENCY LIGHTS CHARGER UNIT AT DOOR 1L HAS FAILED. REPLACED CHARGER.

Part: FITTING — INOPERATIVE (GIRT BAR) · airframe 43,364 hrs · 15,594 cycles

FOUND MED 2L EMERGENCY SLIDE GIRT BAR AFT ATTACH POINT TO AC INOPERABLE, SPRING POSSIBLY BROKEN. REPLACED AFT FLOOR FITTING.

Part: LIGHT — BROKEN (CABIN) · airframe 42,586 hrs · 15,331 cycles

RED EMERGENCY LIGHT PATH BROKEN AT AISLE 10 RIGHT. REPLACED EMERGENCY PATH LIGHT. OPS CHECKS OK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,327 hrs · 14,865 cycles

CABIN EMERGENCY LIGHTS FAILED ON CIDS PANEL. REPLACED FWD LEFT AND RIGHT BATTERY. OPS CHECKS NORMAL.

Part: LIGHT — NO TEST (CABIN) · airframe 41,075 hrs · 14,770 cycles

"FWD L UNIT" DISPLAYED AFTER EMERGENCY LIGHTS TEST. REPLACED EPSU AND BATTERY AT 1L "TEST OK".

Part: SPRING — BROKEN (GIRT BAR FITTING) · airframe 40,156 hrs · 14,444 cycles

DOOR 2L FWD GIRT BAR FITTING SPRING LOADED LEVER HAS SPRING BROKEN. LEVER WILL NOT STAY UP. GIRT BAR SPRING FITTING CHANGED. THIS IS THE SUBJECT OF AD 2005-23-05 WHICH IS COVERED BY UNITED COA 405130. COA ASSIGNMENT TO BE MADE.

Part: GENERATOR — MALFUNCTIONED (NR 2) · airframe 39,226 hrs · 14,116 cycles

F/A REPORTS INTERMITTENT BURNING SMELL AT ROW 15, SMELLS LIKE BURNT RUBBER. CREW SHUT DOWN & SECURED GEN 2. NR 2 ENG IDG PYLON CONNECTOR FOUND WITH EVIDENCE OF FRETTING, ARCING AND BLACK SOCKETS WITH SOME PITTING. NR 2 ENG IDG HARNESS REPLACED.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 38,636 hrs · 13,904 cycles

LEFT EMERGENCY BATTERY WON'T PASS TEST. REPLACED BATTERY.

Part: ENGINE — FAILED (NR 1) · airframe 37,680 hrs · 13,600 cycles

LOUD BANG ON CLIMBOUT FROM NR 1 ENGINE. OIL QUANTITY AND PRESSURE WENT TO ZERO, EGT RED LINED. ENGINE WAS REPLACED AND AIRCRAFT CONTINUED FUTHER FLYING WITHOUT INCIDENT. THE ENGINE FAILURE WAS CONFIRMED AS A HIGH PRESSURE COMPRESSOR 3RD STAGE BLADE (R3 BLADE) FAILURE. THIS IS AN INDUSTRY-WIDE AND KNOWN ISSUE, WITH BOTH A SHORT-TERM AND LONG-TERM FLEET MANAGEMENT PLAN: SHORT TERM IS BORESCOPE MONITORING OF FLEET FOR C3 MID-SPAN CONDITION. LONGER TERM IS UPGRADING OF C3 BLADE TO MORE ROBUST DESIGN..

Part: SLIDE — TORN (GAUGE & BAG)

PREDEPLOYED, FOUND BOTTLE GAUGE BROKEN AND BAG TORN. ASPIRATOR BENT. ALL FLANGABLE LINKS POPPED A HOLE IN THE TOP TUBE, BLOWN OUT SEAM AND TORN FABRIC. DEFECTS REPORTED BY THE OSV SHOP (WINSLOW) ARE OF A SLIDE/RAFT PREVIOUSLY INADVERTENTLY DEPLOYED BY CREW ON 12/17/2004 (IAD). THERE WAS NO REPORTED ABNORMALITY DURING SLIDE DEPLOYMENT, HENCE THE REPORTED MULTIPLE DAMAGE ON THE SLIDE/RAFT ASSY FOUND IN THE SHOP ARE PROBABLY DUE TO MISHANDLING DURING SLIDE REMOVAL AND/OR TRANSPORTATION.

Part: ASPIRATOR — DAMAGED (CABIN)

LOWER CHAMBER ASPIRATOR (60322-105) CRUSHED AND RENDERED UNREPAIRABLE. PACKBOARD DAMAGED AT BOTH OUTBOARD CORNERS AND BOTTOM SHAFT SUPPORTS DAMAGED FROM SERVICE HANDLING. ASPIRATORS APPEAR DAMAGED FROM LAST PACKING. REPLACED THE ASPIRATORS AND PACKBOARD.

Part: CABLE — BROKEN (ESCAPE SLIDE) · airframe 35,622 hrs · 12,920 cycles

DOOR 2R WILL NOT ARM. THE CABLE AT BOTTOM OF SLIDE/RAFT ASSY WAS FOUND BROKEN WHICH DISRUPTED THE NORMAL FUNCTION OF EMERGENCY SELECTOR MECHANISM. THE SLIDE RAFT CABLE SYSTEM IN THE SLIDE LOWER LACING COVER IS A SENSITIVE DESIGN. RELEASING THE CABLE SYSTEM WOULD DROP THE SLIDE PACK FOR DEPLOYMENT. IN-SERVICE ABUSE, SUCH AS INADVERTENT IMPACT BY FOOD CARTS, ETC OR BY SOMEONE SITTING ON THE SLIDE BUSTLE COULD TRIGGER THIS UNWANTED RESULT. REPLACED 2R DOOR SLIDE.

Part: ENGINE — FAILED (NR 2) · airframe 34,358 hrs · 12,477 cycles

ON TAKEOFF ROLL, APPROX 20 TO 30 KTS, HEARD LOUD POP & RT YAW. TAKEOFF ABORTED. ANOTHER AIRPLANE REPORTED NR 2 ENGINE WAS ON FIRE. SHUTDOWN NR 2 ENGINE AND FIRED THE BOTTLE. 3RD STAGE COMPRESSOR BLADE FAILED DUE TO PREVIOUS FOD. REPLACED NR 2 ENGINE. OPERATIONS CHECK NORMAL. OEM IS WORKING ON A REDESIGN OF THIS BLADE AND ITS MID-SPAN SHROUD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 33,435 hrs · 12,157 cycles

AFT CABIN FLOORBOARD SUPPORT STRUCTURE AT RBL 46 IS CORRODED AT 2 LOCATIONS BETWEEN FRAMES 69 & 70. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW SUPPORT STRUCTURE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 33,435 hrs · 12,157 cycles

STRINGER 43L CORRODED FROM FRAME 58 TO 59. MAJOR REPAIR ACCOMPLISHED. INSTALLED NESTED ANGLE REPAIR.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 33,435 hrs · 12,157 cycles

STRINGER 42L CORRODED FROM FRAME 53 TO FRAME 59. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER, INSTALLED ATTACHING HARDWARE AND RESTORED FINISH.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 33,435 hrs · 12,157 cycles

STRINGER 43L CORRODED FROM FRAME 54 TO 55. MAJOR REPAIR ACCOMPLISHED. INSTALLED NESTED ANGLE REPAIR.

Part: RUB STRIP — DEBONDED (NR 2 ENGINE) · airframe 27,595 hrs · 9,867 cycles

NR 2 ENGINE EXPERIENCED A MAJOR COMPRESSOR STALL. THE THROTTLE WAS RETARDED TO IDLE SPEED. REPLACED ENGINE. CORRECTIVE ACTION FOR MAJOR CAUSE IS INCORPORATION OF UPGRADED HIGH PRESSURE COMPRESSOR (HPC) RUBSTRIP MATERIAL THAT IS MUCH MORE RESISTANT TO DISBONDING.

Part: IDG — FAILED (NR 2 ENGINE) · airframe 21,228 hrs · 7,629 cycles

AT 80 KNOTS ON T/O ROLL ECAM IDG2 LO OIL PRESS. ABORTED THE TAKEOFF PRIOR TO 100 KTS AND COMPLETED ECAM PROCEDURE DISCONNECTING IDG. *S/D* REMOVED AND REPLACED ENGINE 2 INTEGRATED DRIVE GENERATOR PER AMM 24-21-51-401.

Part: BATTERY — DISCHARGED (EMERGENCY EXIT)

CABIN EMERGENCY SYSTEM TEST FAIL. *S/D* BAD BATTERY WAS FOUND ON LEFT OVERWING POWER SUPPLY UNIT. BATTERY WAS REPLACED.

Part: REGULATOR — LEAKING (COCKPIT)

FLIGHT DIVERTED TO DEN WHEN SUPPLEMENTAL OXYGEN WAS LOST. WHILE SEARCHING FOR O2 LEAK FOUND CREW O2 REGULATOR TRANSMITTER ASSY LEAKING MASSIVLY. LEAK IS AT THE BACK OF THE TRANSMITTER HOUSING. REPLACED REGULATOR ASSY. LEAK CHECKED REGULATOR. NO LEAKS NOTED.

Part: FAN — OVERHEATED (COCKPIT)

FLIGHT CREW ADVISED DISPATCH OF FUMES IN THE COCKPIT (POSSIBLY DUE TO AN EXTRACT FAN OVERHEAT). CREW ON OXYGEN. DECLARED EMERGENCY FOR EXPEDITED LANDING AT ORD ON 14L. EXTRACT FAN OVERHEATED. NO REPORTED APU PROBLEMS. EXTRACT FAN REPLACED PER MM 21-26-51. REPLACEMENT FAN OPERATES OK.

Part: CIRCUIT BREAKER — TRIPPED (NR 1 & 2 FMGC)

MCDU NR 1 & 2 BLACKED OUT SEVERAL TIMES FOR SEVERAL MINUTES INDEPENDENTLY AND CAME BACK ON THEIR OWN. NR 2 FLIGHT DIRECTOR SEEMED TO WANDER BOTH VERTICALLY AND LATERALLY 300 FEET. *S/D* RESET FMGC 1 AND 2 CB'S, OPS CHECKS NORMAL. NO ADDITIONAL PROBLEMS HAVE BEEN IDENTIFIED.

Part: ACTUATOR — FAILED (NR 1 ENGINE)

NR 1 COMPRESSOR STALL. ENGINE SHUT DOWN. *S/D* COMPRESSOR STALL WAS CAUSED BY A VSV ACTUATOR WITH A FAULTY POSITION FEEDBACK SIGNAL. COA R90290 HAS BEEN ACCOMPLISHED ON APPROXIMATELY 80 PERCENT OF THE V2500 ENGINE FLEET. ACCOMPLISHMENT HAS BEEN ACCELERATED TO COMPLETE THE REMAINING 20 PERCENT. THIS MODIFICATION WILL PREVENT THIS TYPE OF EVENT FROM HAPPENING IN THE FUTURE.

Part: GALLEY — SMOKING (AFT CABIN)

AIRCRAFT RETURNED TO GATE AFTER FLIGHT ATTENDANT NOTICED SMOKE FROM AFT GALLEY AREA.

Part: HYD FLUID — LOSS (GREEN HYD SYST)

AFTER DEPARTURE CREW REPORTS INDICATED LOSS OF GREEN HYDRAULIC SYSTEM FLUID QUANTITY WITHOUT ASSOCIATED ECAM MESSAGE. TWO HOURS LATER ECAM RSVR LO AIR PRESSURE MESSAGE RECEIVED AND FLT DIVERTED FOR PRECAUTIONARY LANDING.

Part: HYD FLUID — LOSS (GREEN HYD SYST)

CREW REPORTS, LOSS OF GREEN HYDRAULIC SYSTEM FLUID QUANTITY WITH ASSOCIATED ECAM MESSAGE RSVR LO AIR PRESSURE.

Part: FAN — OVERHEATED (E/E COMPT)

BLOWER FAN MESSAGE ACCOMPANIED BY ELECTRICAL BURNING ODOR. *S/D* AVIONICS EQUIPMENT VENTILATION COMPUTER BLOWER FAN MOTOR OVERHEATED. REPLACED AEVC BLOWER FAN.

Part: SMOKE ALARM — MALFUNCTIONED (COCKPIT)

CREW REPORTED, ELECTRONIC CENTRALIZED AIRCRAFT MONITORING MESSAGE CARGO SMOKE DISCHARGE AGENT 2. *S/D* RECYCLED AIRCRAFT POWER AND THE MESSAGE CLEARED. NO FURTHER MESSAGES ENCOUNTERED.

Part: ASSIST BOTTLE — DISCHARGED (NR 2R DOOR)

WHILE PERFORMING OPERATIONAL CHECK OF NR 2 AFT RIGHT DOOR AFTER SLIDE REPLACEMENT, THE DOOR ASSIST BOTTLE DISCHARGED AND DOOR WAS UNABLE TO OPEN.