N421UA

Part: FITTING — CRACKED (FR4) · airframe 89,401 hrs · 35,145 cycles

FLIGHT DECK FR4 CENTER POST CONTINUITY FITTING INSPECTION PRODUCED A CRACK INDICATION ON THE L/H SIDE FITTING DURING HFEC INSPEC TION. LOCATION WITHOUT REMOVAL OF THE FASTENER, BUSH AND WASHER. PART 3 TOTAL AIRCRAFT FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTIONS AT I PART 2 INSPECTION REQUIREMENTS: AT LH AND RH FRONT WINDSHIELD F PERMANENT REPAIR: TO BE DETERMINED BY ENGINEERING PRIOR TO THE NOTED THRESHOLD. NOTE TO ENGINEERING: SB 53-1331 IS IMPACTED ACCOMPLISHED INTERIM REPAIR IAW ECRA 5310-08179 AT HAECO - LCQ O N HAECO NR# 9298197. AN INITIAL INSPECTION IS REQUIRED PER PART OKAY TO DIP TO ACCOMPLISH INITIAL INSPECTION PER PART 2 OF THE TOMC-APPROVAL FROM SC1ELBYC COMMENT LATEST REVISION OF ECRA 5310-08179 ON OR BEFORE 40,745 TOTAL AIRCRAFT FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTION AT INTERVALS NOT TO EXCEED 5,600 AIRCRAFT FLIGHT CYCLES, THEREAFTER REF ECRA 5310-08179 PERFORM HFEC INSPECTION PER NTM 51-10-08 AT LH AND RH FRONT WIND BY THE REPAIR WITH AN ALTERNATIVE INSPECTION PROGRAM DEFINED QC SHIELD FRAME AREAS SHOWN IN FIGURE A. WHEN ACCOMPLISHING INSPEC ABOVE WITHIN ECRA 5310-08179. TION AT THE REPAIRED FASTENER HOLE LOCATION, HFEC INSPECTION NEE DS TO BE PERFORMED AROUND THE INSTALLED WASHER AT THE REPAIRED L RECORDS UPDATE....HC QC REVIEWED INIT :

Part: STRINGER — CORRODED (FR65) · airframe 89,401 hrs · 35,145 cycles

STRINGER 31R HAS EXFOLIATING CORROSION AT FR65 REQUIRES REPAIR/R EPLACE PER HAECO LCQ NR 9298009/28009 GENERATED BY V061673 REMOVED & REPLACED CORRODED STRINGER 31R @ FR65 IAW A320 SRM 51- 72-11-911-002 MECH V061673 INSP V921755

Part: HANDLE — FAULTY (AFT CARGO DOOR) · airframe 87,819 hrs · 34,380 cycles

**REJECTED TAKEOFF** AFT CARGO DOOR OPEN INDICATION AT JUST UNDER 100 KTS. FOUND CANNON PLUG ON PROX SWITCH 32WV LOOSE WITH NO SAFETY WIRE. RECONNECTED CANNON PLUG AND WIRED CLAMP TO SWITCH REF MT52-019. WILL NEED GAP CHECK AFTER REPLACEMENT OF DOOR HANDLE. AFT CARGO DOOR HANDLE REPLACED. PROX SWITCH BACKSHELL REPLACED. PROX SWITCH GAP CHECKED GOOD. ECAM CARGO DOOR INDICATIONS NORMAL. ACP RII INSPECTION OF HANDLE INSTALLATION AND OPERATIONAL CHECKS GOOD.

Part: DOOR — NONE (AFT) · airframe 85,086 hrs · 33,060 cycles

AFT CARGO DOOR SHOWSOPEN IN FLIGHT. REMOVED AND REPLACED PROX SWITCH 32WV PER AMM 52-71-12-000-002-A. OPS CHECK GOOD, NO FAULTS NOTED AT THIS TIME.

Part: DOOR ACTUATOR — NONE (AFT) · airframe 85,036 hrs · 33,038 cycles

AFT CARGO DOOR ECAMON DEPT NORMAL PRESSURIZATION VERIFIED DOOR WAS CLOSED AT ARRIVAL GATE AFTER AIR RETURN. AFT COMPLIED WITH MEL. CARGO DOOR CLOSED INDICATION INOP.PLACED ON MEL. NOC DESK: 320 NAME: MF DATE: 19-NOV-21- APPROVED FOR MEL 5270D, AFT CARGO DOOR INDICATION INOP, VARGAS TOMC. FURTHER DETAILS AWAITED

Part: OXYGEN MASK — NO TEST (20 RT) · airframe 84,539 hrs · 32,808 cycles

ON O2MASK DROP TEST, UNIT AT 20 RIGHT DID NOT DEPLOY. FOUND DISCONNECTED WIRE RUNNING TO UNIT. SECURED WIRE. UNIT TESTED PROPERLY THRICE.

Part: SKIN — CORRODED (FR68-70) · airframe 83,560 hrs · 32,346 cycles

CORROSION FOUND AT LAV VENT HOLE DOUBLER REPAIR AT FR68-70 & STR 30RH-34RH REF LP 3570424 AND ECRA 5341-01071 USED FOR INITIAL RE PAIR. REMOVED EXISTING REPAIR, INSTALLED NEW DOUBLER RPR IAW NEW ECRA 5330-06822. DIP CREATED IAW ECRA 5330-06822 REQUIREMENTS ACCOMPLISH INSPECTI ON REQUIREMENTS IAW PART 2 OF ECRA 5330-06822 ON OR BEFORE THE ACFT REACHING 62269 TTL FLT CYC. CURRENT ACFT CYCLES 32346 REPAIR ACCOMPLISHED

Part: SKIN — CORRODED (LAV VENT HOLE) · airframe 83,560 hrs · 32,346 cycles

CORROSION FOUND AT LAV VENT HOLE DOUBLER REPAIR AT FR68-70 & STR 30RH-34RH REF LP 3570424 AND ECRA 5341-01071 USED FOR INITIAL RE PAIR. REMOVED EXISTING REPAIR, INSTALLED NEW DOUBLER RPR IAW NEW ECRA 5330-06822. DIP CREATED IAW ECRA 5330-06822 REQUIREMENTS ACCOMPLISH INSPECTI ON REQUIREMENTS IAW PART 2 OF ECRA 5330-06822 ON OR BEFORE THE ACFT REACHING 62269 TTL FLT CYC. CURRENT ACFT CYCLES 32346 REPAIR ACCOMPLISHED BY BQN TECH 5H0883 & 5H0318 AND INSPECTED BY 5H0619. NOTE: PLANNING TO CONTACT ENGINEERING AFTER 57000 TTL ACFT CYCLES BUT BEFORE 58000 TTL FLT CYCLES FOR ECRA 5330-06822 PART 2 INSPECTION REQUIREMENTS. DIP CREATED IAW ECRA 5330-06822 REQUIREMENTS ACCOMPLISH INSPECTI ON REQUIREMENTS IAW PART 2 OF ECRA 5330-06822 ON OR BEFORE THE ACFT REACHING 62269 TTL FLT CYC. CURRENT ACFT CYCLES 32346. OPBLM CHRISTIANSEN TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED RECORDS UPDATE..KJB QC REVIEWED INIT:>57000<58000 TAFC (PLN TO CONTACT ENG) T/A: 62269 TAFC..KJB U372999

Part: ACTUATOR — INOPERATIVE (L2 DOOR) · airframe 81,299 hrs · 31,349 cycles

CATERING REPORTED NR 2 DOOR WOULD NOT OPEN ALL THE WAY. NEEDS CYLINDER DOOR DAMPER (ACTUATOR). REPLACED THE L2 DOOR DAMPNER IAW AMM 52-13-14, OPS CHECKED GOOD.

Part: LIGHT — MISSING (EXTERIOR) · airframe 79,965 hrs · 30,793 cycles

R SIDE LANDING LIGHT ASSEMBLY MISSING FROM A/C. CORRECT LOG SHOULD READ RIGHT LANDING LIGHT RETAINING RING, LAMP AND LUGS MISSING. NOT ASSY. RETERMINATED WIRES, RELAMPED AND REPLACED RING. CHECKS OK. ALSO REF L/P 9063476 FOR CATEGORY 2 PARTS DEPARTING A/C.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 78,129 hrs · 29,974 cycles

L2 DOOR SILL HAS SURFACE CORROSION. REPAIRED L2 DOOR SILL IAW SRM 53-41-14-300-001 FIG 20101, REPAIR PRINCIPLE NR 11 CAT A REPAIR, NO SRI REQUIRED.

Part: WEB — DAMAGED (FUSELAGE) · airframe 78,129 hrs · 29,974 cycles

FWD CARGO WEB FR33-FR34 RT STR38 HAS AN ELONGATED HOLE. REMOVED AND REPLACED WEB AT STR 38R BETWEEN FR33 AND FR34 IAW SRM 51-42-11 PARA 2E.

Part: BUSHING — ROTATED (LT MLG) · airframe 78,129 hrs · 29,974 cycles

LT MLG UPPER SIDE STAY BUSHING ROTATED. LT WING MLG SIDE STAY FITTING INBOARD AND OUTBOARD LUGS REPAIRED BY OVERSIZING AND INSTALLING NEW BUSHINGS IAW SRM 57-26-13-300- 006.

Part: BUSHING — ROTATED (RT MLG) · airframe 78,129 hrs · 29,974 cycles

RT MLG UPPER SIDESTAY BUSHING IS ROTATED. RT WING MLG SIDE STAY FITTING INBOARD AND OUTBOARD LUGS REPAIRED IAW ECRA 5308-01127 BY OVERSIZING AND INSTALLING NEW BUSHINGS PER PART 1 INTERIM REPAIR INSTRUCTIONS.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 78,129 hrs · 29,974 cycles

LEFT FORWARD PASSENGER DOOR CUTOUT FR16, STOP FITTING NR 1 HOLE NR 3 IS CRACKED FOUND BY ROTORY HFEC INSP REQUIRES REPAIR AND REINSPECT PRIOR FLIGHT. REPAIRED LT FR16 NR 1 DOOR STOP NR 3 HOLE IAW ECRA 5311-01970.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,129 hrs · 29,974 cycles

FORWARD CARGO COMPARTMENT FRAME 29 BETWEEN STRINGER 43 AND 44 LEFT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR29 STR44-43L NOMINAL THICKNESS .055" MATERIAL LOSS .007" REMAINING MATERIAL .048" ALLOWABLE LOSS .004", FOUND TO BE OUT OF LIMITS IAW SRM 51-73-11. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-42-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,129 hrs · 29,974 cycles

FORWARD CARGO COMPARTMENT FRAME 32 BETWEEN STRINGER 42 AND 4 3 LEFT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE ON FR32 STR42-43 NOMINAL THICKNESS .055" MATERIAL LOSS .007" REMAINING MATERIAL .048" ALLOWABLE LOSS .004", FOUND TO BE OUT OF LIMITS IAW SM ASNA3042. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-72-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,129 hrs · 29,974 cycles

FORWARD CARGO COMPARTMENT FRAME 31 BETWEEN STRINGER 43 AND 44 LEFT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR31 STR43-44L NOMINAL THICKNESS .055" MATERIAL LOSS .009" REMAINING MATERIAL .046" ALLOWABLE LOSS .004" IAW SM ASNA3042. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-72-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,129 hrs · 29,974 cycles

FORWARD CARGO COMPARTMENT FRAME 30 BETWEEN STRINGER 42 AND 4 3 LEFT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR30 STR42-43L NOMINAL THICKNESS .055" MATERIAL LOSS .006" REMAINING MATERIAL .049" ALLOWABLE LOSS .004", FOUND TO BE OUT OF LIMITS IAW SM ASNA3042. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-71-11 PARA 2A3 & 4.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,129 hrs · 29,974 cycles

FORWARD CARGO COMPARTMENT FRAME 26 BETWEEN STRINGER 42 AND 4 3 LEFT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR26 STR42-43L NOMINAL THICKNESS .055" MATERIAL LOSS .005" REMAINING MATERIAL .49" ALLOWABLE LOSS .004" FOUND TO BE OUT OF LIMITS IAW SM ASNA3042 REMOVED AND REPLACED SHEAR TIE IAW 51-42-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,129 hrs · 29,974 cycles

FORWARD C ARGO COMPARTMENT FRAME 30 BETWEEN STRINGER 41 AND 42 LEFT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR30 STR41-42L NOMINAL THICKNESS .055" MATERIAL LOSS .013" REMAINING MATERIAL .042" ALLOWABLE LOSS .004", FOUND TO BE OUT OF LIMITS IAW SM ASNA3042. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-72-11 PARA 2A2.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,129 hrs · 29,974 cycles

FORWARD CARGO COMPARTMENT FRAME 32 BETWEEN STRINGER 43 AND 44 LEFT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR32 STR43-44L NOMINAL THICKNE SS .055" MATERIAL LOSS .008" REMAINING MATERIAL .047" ALLOWABLE LOSS .004" FOUND TO BE OUT OF LIMITS IAW SM ASNA3042 REMOVED AND REPLACED SHEAR TIE IAW A320 SRM 51-72-11 PARA 2A34.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,129 hrs · 29,974 cycles

FORWARD CARGO COMPARTMENT FRAME 32 BETWEEN STRINGER 41 AND 4 2 LEFT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE FR32 STR41-42L ORIG THICKNESS .05 5 LOSS. 007 REMAINING .048 ALLOWABLE LOSS .004 OUT OF LIMITS IAW SM ASNA3042. REMOVED AND REPLACED SHEAR TIE IAW SRM 5 1-72-11 PAR 2A3&4.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,129 hrs · 29,974 cycles

FORWARD CARGO COMPARTMENT FRAME 32 BETWEEN STRINGER 41 AND 4 2 RIGHT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR32 STR41-42R .055" NOMINAL THICKNESS MATERIAL LOSS .010" REMAINING MATERIAL .045" ALLOWABLE REMAINING MINIMUM THICKNESS .051", FOUND TO BE OUT OF LIMITS IAW SM ASNA3042. REMOVED AND REPLACED SHEAR TIE IAW SRM 51- 42-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,129 hrs · 29,974 cycles

FORWARD CARGO COMPARTMENT FRAME 29 BETWEEN STRINGER 40 AND STRINGER 41 LEFT CORRODED SHEAR TIE. BLENDED CORROSION ON SHEAR TIE FR29 STR40-41L NOMINAL THICKNESS .055" MATERIAL LOSS .006" REMAINING MATERIAL .040" ALLOWABLE LOSS .004", FOUND TO BE OUT OF LIMITS IAW SM ASNA3042. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-72-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,129 hrs · 29,974 cycles

FORWARD CARGO COMPARTMENT FRAME 29 BETWEEN STRINGER 42 AND 4 3 LEFT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR29 STR42-43L NOMINAL THICKNESS .055" MATERIAL LOSS .015" REMAINING .040" ALLOWABLE LOSS .004", FOUND TO BE OUT OF LIMITS IAW SM ASNA3042. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-42-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,129 hrs · 29,974 cycles

FORWARD CARGO COMPARTMENT FRAME 31 BETWEEN 42 AND 43 LEFT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR31 STR42-43L NOMINAL THICKNESS .055" MATERIAL LOSS .008" REMAINING MATERIAL .047" ALLOWABLE LOSS .004", FOUND TO BE OUT OF LIMITS IAW SM ASNA3042. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-72-11 PARA 1A3 & 4.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,129 hrs · 29,974 cycles

FORWARD CARGO COMPARTMENT FRAME 26 BETWEEN STRINGER 42 AND 4 3 SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR26 STR44-43R NOMINAL THICKNESS .055" MATERIAL LOSS .018" REMAINING MATERIAL .037" ALLOWABLE LOSS .004", FOUND TO BE OUT OF LIMITS IAW SM ASNA3042. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-72-11 PARA 2A3 &4.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,129 hrs · 29,974 cycles

FORWARD CARGO COMPARTMENT FRAME 32 BETWEEN STRINGER 40 AND 41 RIGHT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE FR32 STR40-41R NOMINAL THICKNESS .055" MATERIAL LOSS .005" REMAINING MATERIAL .050" ALLOWABLE LOSS .004", FOUND TO BE OUT OF LIMITS IAW SM ASNA3042. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-72-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,129 hrs · 29,974 cycles

FORWARD CARGO COMPARTMENT FRAME 33 BETWEEN STRINGER 41 AND 42 LEFT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR33 STR41-42L NOMINAL THICKNESS .055" MATERIAL LOSS .006" REMAINING MATERIAL .049" ALLOWABLE LOSS .004", FOUND TO BE OUT OF LIMITS IAW SM ASNA3042. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-72-11 PARA 2A3 & 4.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,129 hrs · 29,974 cycles

FORWARD CARGO COMP FRAME 31 BETWEEN STRINGER 39 AND 40 RIGHT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR31 STR39-40R NOMINAL THICKNESS .055" MATERIAL LOSS .020" REMAINING MATERIAL .055 ALLOWABLE MINIMUM REMAINING THICKNESS .039" FOUND TO BE OUT OF LIMITS IAW SRM 51-73-00. REMOVED AND REPLACED SHEAR TIE IAW SRM 51- 42-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,129 hrs · 29,974 cycles

FORWARD CARGO COMPARTMENT FRAME 30 BETWEEN STRINGER 40 AND 41 LEFT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR30 STR40-41L NOMINAL THICKNESS .055" MATERIAL LOSS .008" REMAINING MATERIAL .047", ALLOWABLE LESS .004" FOUND TO BE OUT OF LIMITS IAW SM ASNA3042. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-72-11 PARA 2A3 & 4.

Part: STRINGER — CORRODED (FRAMES 58-59) · airframe 78,129 hrs · 29,974 cycles

DURING INSPECTION OF THE AFT CARGO STRINGER 43L, FOUND CORROSION BETWEEN FRAMES 58 - 59. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-11-001.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 76,252 hrs · 29,138 cycles

EMERGENCY LIGHT LENS FOUND BROKEN AT SEAT 21C. REPLACED THE LENS.

Part: DISPLAY — FAULTY (CAPTAIN'S) · airframe 75,205 hrs · 28,674 cycles

CAPTAIN`S ND WENT BLANK SHORTLY AFTER TAKEOFF. HAD ELECTRICAL ODOR AND WENT AWAY. REMOVED AND REPLACED THE CAPTAIN`S ND IAW AMM 31-63-22-000-001-A & 31-63-22-400-001-A. OPS CHECKED NORMAL.

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 74,421 hrs · 28,352 cycles

EMERGENCY LIGHTS WILL NOT GO OUT. CREW CYCLED THE EMERGENCY LIGHT SWITCH IN THE COCKPIT AND CABIN. LIGHTS NOW OPS NORMAL.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS)

DURING TEST, MESSAGE FOR LT FWD BATTERY. REPLACED POWER SUPPLY UNIT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,128 hrs · 27,754 cycles

AFT LEFT EMERGENCY POWER SUPPLY BATTERY FAULT LIGHT ILLUMINATED. R & R THE BATTERY PACK IAW AMM , TESTED OK

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,903 hrs · 26,763 cycles

LAVATORY BLOWER VENT HAS AREA OF SHEET METAL DAMAGE & CORROSION TO ACFT SKIN. INSTALLED INTERIM REPAIR IAW ECRA & 5341-01071 PART 1.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,903 hrs · 26,763 cycles

LAVATORY BLOWER VENT HAS AREA OF SHEET METAL DAMAGE & CORROSION TO ACFT SKIN. INSTALLED INTERIM REPAIR IAW ECRA 5341-01071 PART 1. TIME LIMITED REPAIR, REMOVE ACFT FROM SERVICE ON APRIL 23 2016, UNLESS A NEW RDAS IS RECEIVED.

Part: FLUID — LOW (NLG SHOCK) · airframe 69,803 hrs · 26,277 cycles

SHOCK ABSORBER FAULT, DISPLAYED ON UPPER ECAM SCREEN. DISPLAYED AFTER GEAR RETRACTION. FOUND NLG SHOCK FLUID & PRESS LOW. FOUND NLG PROX SENSORS 24GA, 25GA OUT OF RAND. ADJUSTED FLUID & PRESS IN NLG IAW AMM 12-12-32-610. ADJUSTED NLG PROX SENSORS IAW 32-31-73-200-002.

Part: ENGINE — VIBRATION (NR 2 ENGINE) · airframe 68,948 hrs · 25,923 cycles

AT CLIMB POWER ENG 2 N1 VIB 2.7 WITH ENG 1 AT 0.4. ALSO ENG 2 EGT 570 DEGREES & ENG 1 AT 519 DEGREES. ACCOMPLISHED ON SHOT TRIM BALANCE IAW MT71-010, MM 72-31-11 & MM 71-00-00. TESTED NR 8. ALL INDICATIONS NORMAL, MAX N1 VIBE WAS 0.4 AT 85%.

Part: SWITCH — UNSECURE (LANDING LIGHT) · airframe 67,492 hrs · 25,345 cycles

RIGHT RETRACTABLE LAND LIGHT SWITCH NEEDS SECURING. SECURED RT RETRACTABLE LANDING LIGHT SWITCH. OPERATIONS CHECKED OK.

Part: OXYGEN SYSTEM — LOW (CREW O2) · airframe 67,492 hrs · 25,345 cycles

CREW OXYGEN SYS LOW. SERVICED CREW OXYGEN IAW AMM 12-14-35-0301. OPERATIONS & LEAK CHECKED OK. PRESS PRIOR TO SERVICING 1250PSI.

Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 65,989 hrs · 24,748 cycles

LT HAND HORIZONTAL STABILIZER LE HAS A HOLE APPROXIMATELY 4 INCHES FROM FUSELAGE DIMENSIONS ARE 1 - 2 INCHES LONGERONS 1-8 INCHES WIDE. LACED ON CF INSTALLED INTERIM REPAIR IAW SRM 51-77-12, PAR 2A.

Part: UNKNOWN — FAULTY (HYDRAULIC SYS) · airframe 65,469 hrs · 24,548 cycles

LT MLG UNSAFE SUSPECT PRIORITY VLV AT PTU. REPLACED PRIORITY VLV ASSEMBLY IAW AMM 29-11-33-000-001-A, NO HELP. LT MLG STILL SLOW TO FULL DOWN & LOCK.

Part: INDICATION SYS — ACTIVATED (COCKPIT) · airframe 65,469 hrs · 24,548 cycles

GEAR UNSAFE INDICATION.

Part: MICROPHONE — FAULTY (COCKPIT) · airframe 65,411 hrs · 24,523 cycles

CAPT BOOM MIKE VERY GARBLED, HAND MIKE WORKS OK. REPLACED CAPTS BOOM MIKE.

Part: LANDING GEAR — OUT OF LIMITS (MAIN) · airframe 65,364 hrs · 24,502 cycles

MOMENTARY LG UNLOCKED ECAM AFTER GEAR EXTENSION FOR 10 SEC WHICH CLEARED ITSELF. FOUND LT MAIN GEAR & RT MAIN GEAR OUT OF LIMITS IAW MM 12-12-32-611-010-A. LT UPPER CHAMBER APPROXIMATELY 1150PSI, LOWER CHAMBER 1100, H DIMENSION 5 INCHES. RT GEAR UPPER CHAMBER APPROXIMATELY 1150, LOWER 1150PSI, H DIMENSION APPROXIMATELY 5 INCHES. CHECKED BOTH NR 1 & NR 2 LGICU BOTH TESTED OK, NO FAULTS. BOTH MAIN GEAR SVCD IAW MM 32-12-12-PG 661-010-A.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 65,039 hrs · 24,380 cycles

SCRATCH ON FS BETWEEN FR21 & FR23 AROUND STRINGER 20. DAMAGED AREA HAS BEEN REWORKED BUT NOT DOCUMENTED. DAMAGE MEASURES 1"LONG & .100" WIDE & 0.019" MATERIAL REMOVED. DAMAGE IS UNDER 25% OF ORIGINAL SKIN THICKNESS OF 0.079".

Part: DISPLAY — DEFECTIVE (COCKPIT) · airframe 64,886 hrs · 24,322 cycles

LOWER ECAM DISPLAY UNIT INOPERATIVE EIS FLASHES WITH DIAGONAL WHITE LINE. REPLACED LOWER ECAM DISPLAY, TESTED OKAY.

Part: FASTENER — MISSING (LT WING) · airframe 64,853 hrs · 24,312 cycles

INBOUND PAX SAY RIVETS MISSING AT ENGINE 1 CONNECTION TO WING. SKIN OF WING LIFTS UP. REPLACED MISSING FASTENERS.

Part: FAIRING — CRACKED (NR 2 NOSE CONE) · airframe 64,354 hrs · 24,119 cycles

NOSE CONE NR 2 ENGINE CRACKED. CRACK IN FAIRING ASSY. FROM 1 BOLT HOLE ALL THE WAY THRU TO THE REAR EDGE, OUT OF LIMITS IAW AMM. REPLACED INLET CONE FAIRING IAW AMM.

Part: LIGHT — NO TEST (CABIN) · airframe 63,865 hrs · 23,917 cycles

DURING EMERGENCY LIGHT TEST, MESSAGE BATTERY EMERGENCY. TESTED IAW MM 33-51-38 TESTED OKAY.

Part: CONTROL UNIT — FAULTY (LAVATORY) · airframe 63,727 hrs · 23,861 cycles

H2O POURING OUT FWD LAV INTO COCKPIT. REMOVED AND REPLACED FLUSH CONTROL UNIT REF AMM 38-31-12. REMOVED AND REPLACED RINSE VALVE FWD LAV 'A'. OPS AND LEAKS CHECK GOOD. NO FURTHER CLEAN UP IS REQUIRED.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 63,570 hrs · 23,803 cycles

DURING WALKAROUND FOUND MISSING FASTENER ON EXTERIOR PANEL, CORNER, LEFT FUSELAGE FILLET PANEL.

Part: SUPPORT — CRACKED (AFT CARGO DOOR) · airframe 62,913 hrs · 23,552 cycles

AFT CARGO DOOR HAS DAMAGE AT SUPPORT. SUPPORT IS CRACKED. AREA IS NEAR AFT ROLLER LATCH. REMOVED FITTING, NO FURTHER DAMAGE NOTED IN AREA. NEW FITTING ON AOG. CONT OF AMIS ITEM 9132006. REPLACED FITTING.

Part: RADAR — INOPERATIVE (WX SYS) · airframe 62,648 hrs · 23,445 cycles

WEATHER RADAR SYSTEM INOPERATIVE, NO RADAR SWEEP DISPLAYED WITH RADAR ON. ALSO WEATHER RADAR RT DISPLAYED ON WITH RADAR SYS SWITCH ON. REPLACED THE WEATHER RADAR TRANSCEIVER. IAW TSM 34-41-00-810-812 AND 34-41-00-810-818. PLACED WEATHER RADAR ON DF IAW 3441 A. DFF 338. TRIED NEW RT AND CONTROL PANEL. REPLACED WEATHER RADAR CONTROL PANEL. STILL SHOWS R SLASH T ON CAPT AND FIRST OFFICER ND DISPLAY.

Part: ACTUATOR — FAILED (NR 1 ENGINE) · airframe 61,456 hrs · 22,950 cycles

ECAM REPORTS NR 1 ENGINE FADEC B FAULT. NR 1 ENGINE STALL. STEADY STATE CLIMB, 8 MINUTES AFTER TAKEOFF. REPLACED NR 1 ENGINE LPC BLEED SLAVE ACTUATOR. REPLACED LOW PRESSURE COMPRESSOR BLEED MASTER ACTUATOR, REF EM3454-1. REPLACED ACTUATOR IAW AMM.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 61,336 hrs · 22,905 cycles

RAPID CABIN DEPRESS AT 7000 FT, OUTFLOW VALVE WENT FULL OPEN. REPLACED CABIN PRESSURE CONTROLLER NR 1 PER MM. SYSTEM OPS NORMAL. NO FAULTS FOUND.

Part: CONTAINER — WRONG PART (OXYGEN MASK) · airframe 61,325 hrs · 22,899 cycles

DURING DROP TEST FOR CF-225 FOUND OXYGEN MASK CONTAINER ABOVE AFT FLIGHT ATTENDANTS SEATS HAS WRONG EFFECTIVITY TEST BUTTON. INTERCHANGE ABILITY SUPPORTED BY SIL35-007 PG32.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 1 EF) · airframe 61,325 hrs · 22,899 cycles

ON CLIMB OUT PASS O2 MASKS IN SEATS 1EF DEPLOYED. MASKS HAD TO BE SECURED WITH DUCT TAPE. REPACKED MASK PER AMM. PERFORMED. ACCOMPLISHED DROP TEST.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 61,223 hrs · 22,862 cycles

PER 3 SVC ACFT FAILS EMERGENCY LIGHT TEST FOR FWD LEFT BATTERY. REPLACED LEFT FWD EMERGENCY LIGHT BATTERY. TEST OP CHECKED OKAY.

Part: EXHAUST DUCT — CRACKED (NR 2 ENGINE) · airframe 61,154 hrs · 22,833 cycles

NR 2 ENGINE EXHAUST CONE HAS A 2-3 INCH CRACK AT THE SIX O'CLOCK POSITION. SUPPLEMENTAL DATA UPDATE, CRACK RUNS ALONG SEAM OF WELD REPAIR AT 6 0'CLOCK POS APPROX 5 INCHES LONG. ACCOMPLISHED REPAIR BY STOP DRILLING PER MM.

Part: WINDSHIELD — FAULTY (COCKPIT) · airframe 60,780 hrs · 22,676 cycles

RIGHT WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN, ANTI ICE. RT WINDSHIELD SENSOR ON CFDS. COMPLIED WITH MAINTENANCE TIP 30-003 .WHC2 TESTS OK. JUMPER INSTALLED ON RT WINDSHIELD SENSOR. REPLACED FIRST OFFICERS WINDSHIELD REF AMM. WINDOW HEAT OP CHECKED NORMAL.

Part: RUB STRIP — DEBONDED (R2 DOOR) · airframe 60,106 hrs · 22,399 cycles

THERE IS A SQUEAL AT DOOR 2R INFLIGHT. FOUND UPPER COVER PLATE RUB DIS-BONDED. REMOVED TEFLON AND ACCOMPLISHED INTERIM REPAIR. REPLACED RUBSTRIPS AS REQUIRED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 59,632 hrs · 22,182 cycles

TWO EXTERNAL SKIN DOUBLERS INSTALLED AT FR63 - 64 AT FORMER L-BAND ANTENNA LOCATIONS PER COA40795C AND SRM 53-00-11 FIG 238. MAJOR REPAIR ACCOMPLISHED. DOUBLERS INSTALLED PER JC 97954010 BY 396114 AND LC-09. PER SRI 53-00-11 TABLE 219 DOUBLERS REQUIRE FIRST INITIAL RE-INSPECTION AT 48,000 CYC OR 84,000 HRS FROM REPAIR EMBODIMENT WITH SUBSEQUENT INSPECTIONS EVERY 3300 CYC OR 5775 HRS AFTER FIRST INSPECTION. CURRENT PTC IS 22182.

Part: STRUCTURE — OUT OF LIMITS (FUSELAGE) · airframe 59,632 hrs · 22,182 cycles

FUSELAGE DENT FR 57-58 STR 25R-26R. FOUND TO BE OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR IAW SRM. WORKED ON W-U V0931J.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,571 hrs · 22,153 cycles

EMERGENCY LIGHT INOP AT SEAT 10 ABC. REMOVED AND REPLACED BULB SUSPECT WIRING ISSUE.

Part: SILL — CORRODED (FUSELAGE) · airframe 58,339 hrs · 21,594 cycles

CORROSION ON L2 DOOR SILL AT FRAME 68. REMOVED CORROSION AND INSTALLED REPAIR STRAP.

Part: RECEPTACLE — DAMAGED (OXYGEN SYSTEM) · airframe 58,072 hrs · 21,478 cycles

OXYGEN FILL PORT THREADS STRIPPED AND DESTROYED. REPLACED FILL PORT.

Part: ACTUATOR — MALFUNCTIONED (MLG DOOR) · airframe 67,437 hrs · 25,199 cycles

MAIN LANDING GEAR DID NOT EXTEND USING ALTERNATE GEAR SWITCH. ON 2ND ATTEMPT HAD RT MAIN BUT STILL NO LEFT. REPLACED LT MLG DOOR ACTUATOR IAW MM. LEAK AND OPS CHECK GOOD IAW MM. PERFORMED ALTERATE EXTENSION SYSTEM TEST IAW MM. TEST GOOD.

Part: LIGHT — FAILED (EXTERIOR) · airframe 57,188 hrs · 21,102 cycles

EMERGENCY LIGHT TEST FAILED. FAULT IS EXT LOADS EMER L. LT AFT OVERWING EXTERIOR LIGHT FWD LIGHT IS INOP. RELAMPED, NO HELP, NEEDS NEW LIGHT ASSY. REPLACED AFT LEFT OVERWING EXTERIOR LIGHT ASSY, OPS CHK GOOD.

Part: CONNECTOR — FAULTY (EMERGENCY LIGHT) · airframe 56,818 hrs · 20,920 cycles

"ATA 33-51-38 EXT LOADS EMER L" DISPLAYED DURING EMERGENCY LIGHT TEST. IAW TSM PERFORMED OPS TEST OF EMERGENCY LIGHTS NOT WITH CIDS TASK 33-51-00-710-006 FAULT ON POWER SUPPLY IS EXTERNAL LIGHTS REPLACED AFT EMERGENCY LIGHTS ON WING AFT LIGHTS NOW FLASH DURING TEST FWD LIGHTS DO NOT FLASH. IRREGULARITY NOT FLAGGED. THIS ENTRY MADE TO FLAG ENTRY. FOUND LIGHT ASSY 63WL BAD. REPLACED CONNECTOR AND BACKSHELL ASSY ON AFT OVERWING EMERGENCY EXIT LIGHT ASSY 63WL. EMERGENCY LIGHT SYS TEST NORMAL WITH NO FAULTS DISPLAYED.

Part: STRUCTURE — DAMAGED (RT WING TE FLAP) · airframe 56,412 hrs · 20,727 cycles

RT INBD FLAP DAMAGED NEAR T/E (ZONE 2) OTBD OF FAIRING. REPAIRED RT INBD AFT FLAP.

Part: ACTUATOR — FAULTY (O2 MASKS) · airframe 56,236 hrs · 20,648 cycles

O2 MASKS FAILED TO DEPLOY WHEN TESTED. TEST REQUIRED FOR DF726 6ABC TEST. REPLACED ACTUATOR AT 3AB. TESTS OK.

Part: ACTUATOR — FAILED (OXYGEN MASKS) · airframe 56,236 hrs · 20,648 cycles

O2 MASKS FAILED TO DEPLOY WHEN MANUALLY TESTED FOR DF726 6ABC. RESTOWED MASKS AT 22DEF. TESTS OK.

Part: BOTTLE — READS LOW (EXTINGUISHER) · airframe 55,144 hrs · 20,110 cycles

NR 2 ENG FWD FIRE BOTTLE IS REMOVED BECAUSE OF LOW PRESSURE. REPLACED BOTTLE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,027 hrs · 20,063 cycles

CABIN EMERGENCY LIGHTS FAILED TEST DURING (3) SERVICE. EXT LOADS EMERGENCY LIGHT RELAMPED LT EXT, EMERGENCY LIGHTS, NO HELP. REPLACED LT EPSU AND BATTERY, NO HELP. FAILS MSG SHOWS EXT EMERGENCY LOADS L. ACCOMPLISHED TSM, DID OPS TEST OF LT OVERWING EPSU, EXT. LT. FAULT, RELAMPED AFT LT OVERWING ESCAPE LIGHT, EMERGENCY LIGHTING SYS OPS.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 54,343 hrs · 19,759 cycles

LEFT OVERWING EMERGENCY LIGHT INOP. FOUND CONNECTOR OFF LIGHT ASSY. CORRECTED, CLEANED CONNECTION AT CHARGER IN DADO PANEL. OP CHK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,047 hrs · 19,618 cycles

EEL LIGHTS INOP AT SEAT ROWS 16C AND 25C. WILL NEED 2 EA LIGHT ASSY'S. REPLACED LAMP ASSEMBLIES OKAY.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 53,309 hrs · 19,258 cycles

EMERGENCY LIGHTING TEST FAILS, FAULTS AFT BATTERY. REPLACED BATTERY. OPS CHECKED GOOD.

Part: PROBE — FAULTY (TAT) · airframe 53,260 hrs · 19,236 cycles

LOST BOTH AUTOPILOT AND AUTOTHROTTLES, FLIGHT DIVERTED. REPLACED RIGHT STATIC PRESSURE AIR DATA MODULE NUMBER 19FP4 (PRECAUTIONARY). CURRENT STATUS NO FAULTS. NR 2 TAT PROBE READS LOW, REPLACED PROBE. RPLC'D ADRIU 3 (P/N HG1150AC06-18, POSITION 3). ACCMP'D CAT III TEST. ACFT OPS NORMAL.

Part: SKIN — DENTED (LE SLAT) · airframe 51,381 hrs · 18,431 cycles

LEFT WING NR 5 SLAT HAS TWO DENTS IN UPPER SKIN. REPLACED NR 5 LT SLAT.

Part: RELAY — FAILED (ELECTRICAL SYS) · airframe 47,795 hrs · 16,984 cycles

EMERGENCY GENERATOR DOES NOT COME ON WHEN EMER GEN SW IS SELECTED. TRIED RELAY 12XE AND CONTROL UNIT 1XE, NO HELP. CK'D FOR VOLTAGE AT HYD FLOW SOLENOID ON TOP OF EMER GEN 8XE, NO VOLTAGE PRESENT. *S/D* RAT EXT INHIB COND RELAY BAD. REPLACED RAT EXT INHIB CONDITION RELAY 20XE, CKS GOOD PER MM.

Part: LAMP — FAILED (EMERGENCY LIGHTS) · airframe 46,687 hrs · 16,624 cycles

LEFT OVERWING EMERGENCY LT. TEST FAILED EXTERNAL LOADS. SUPPLEMENTAL DATA UPDATE CAUSE: SEVERAL LAMPS FAILED IN LIGHT ASSY. CORRECTIVE ACTION: RELAMPED ASSY, OPS CHECK OK.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 46,180 hrs · 16,446 cycles

EMERGENCY LIGHT TEST FAILED, SHOWING EXTERNAL FAULT LEFT. FOUND BULB BURNED OUT. RELAMPED AND TEST PASSES.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,067 hrs · 16,413 cycles

EMERGENCY LIGHT TEST FAILS WITH MESSAGE EXT LOAD. FOUND SEVERAL LAMPS BURNT OUT ON O/W EXITS (EXTERIOR). RELAMPED ASSYS- SYSTEM TESTED NORMALLY.

Part: LANYARD — OUT OF POSITION (L2 DOOR) · airframe 45,941 hrs · 16,364 cycles

CREW REPORT: DOOR 2L HAS GREEN CHORD HANGING OUT BELOW SLIDE PACK. RESECURED MOORING LINE BACK INTO SLIDE PACK. NO REPEATS.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 45,662 hrs · 16,270 cycles

EMERGENCY LIGHT TEST FAILED ON 3SVC. FOUND LAMPS AT OVER WING LOCATION WERE OUT AND BATTERY FAILED AT FWD LOCATION. REPLACED BATTERY AT FWD MED AND RELAMPED EMER LIGHTS ON OVER WING EXIT.

Part: ROD END — WORN (ELE SERVO CONTRL) · airframe 45,124 hrs · 16,064 cycles

MODERATE AIRFRAME VIBRATION DURING CLIMB 320KT - 14000 STOPPED AT 300. *S/D* ELEVATOR SERVO CONTROL ROD END (LT) OUT OF RIG. REPLACED BOTH ELEVATOR SERVO ROD ENDS AND PERFORMED ELEV FREEPLAY CHECK. ALL NORMAL, NO REPEATS SINCE ORIGINAL.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 44,501 hrs · 15,849 cycles

EMERGENCY LIGHTS TEST FAILS, -EPSU EXT LOADS EMER L- MESSAGE DISPLAYED. REPLACED POWER SUPPLY AND BATTERY.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHT) · airframe 44,165 hrs · 15,730 cycles

EMERGENCY LIGHT TEST FAILS WITH FAULT EXTERNAL LOAD L. [07-03-07] REPLACED OVER WING LIGHT BULBS (EXTERIOR) AND REPLACED EPSU PER MM 33-51-38. EMERGENCY LIGHT TEST PASSED ON GND.

Part: CONNECTOR — DAMAGED (FUEL INDICATOR) · airframe 44,058 hrs · 15,692 cycles

RIGHT INBOARD AND OUTBOARD FUEL QTY IND 2 AMBER DASHES ON FUEL PAGE. UNRELIABLE DATA. [06-26-07] FAULT TRACING FOUND FAULTY FUEL BOOST PUMP FUSE CONNECTOR. REPLACED 4044VCA FUSE CONNECTOR.

Part: A/C PACK — FAILED (NR 2) · airframe 43,955 hrs · 15,660 cycles

RTFL DUE TO NR 2 PACK FAILURE & NR 1 PACK'S CURRENT DEFERRAL. AFTER ATB, ON GROUND TESTING INDICATING NORMAL SINGLE PACK OPS-PERFORMED PACK TEMP CONTROL TEST- OK, REPLACED TURBINE BYPASS VALVE - ALL OPS TESTS ARE NORMAL- NO REPEATS SINCE ORIGINAL.

Part: CONNECTOR — DISCONNECTED (CABIN SEATS 3AB,) · airframe 43,354 hrs · 15,450 cycles

CABIN SEATS 3AB, 3CD, 17ABC FAILED O2 MASK RELEASE CHECK. [SUP 05-29-07] ADJUSTED THE OXYGEN CONTAINER DOOR SPACERS AND REPLACED THE RELEASE SOLENOIDS AS A PRECAUTIONARY MEASURE. AT SEATS 17ABC, FOUND THE ELECTRICAL CONNECTOR DISCONNECTED. RECONNECTED & PERFORMED DROP TEST. TESTS OKAY.

Part: BLEED VALVE — FAULTY (NR 1 ENGINE) · airframe 43,352 hrs · 15,449 cycles

A 'THUD' NOISE NOTED ON TAKEOFF, DEADHEADING CAPT ON 23A NOTICED WHAT APPEARED TO BE A FIREBALL FROM ENG 1 EXHAUST. CREW REPORTED NO ABNORMAL PARAMETERS. NO DEBRIS FOUND ON RUNWAY. SUPPLEMENTAL DATA UPDATE CHECKED FOR EVIDENCE OF COMPRESSOR FAILURE WITH NO FINDINGS FOUND. FURTHER TROUBLESHOOTING FOUND THE 7TH AND 10TH STAGE BLEED VALVES SOLENOIDS TO BE FAULTY AND WERE REPLACED. ALSO PERFORMED A VARIABLE STATOR VANE SYSTEM LUBE AS A PRECAUTIONARY MEASURE. REPLACED ENGINE.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHT) · airframe 41,892 hrs · 14,919 cycles

EMERGENCY LIGHT TEST FAILS WITH DOOR LEFT POWER SUPPLY MESSAGE. REPLACED EPSU. OPS TESTED NORMAL.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 41,678 hrs · 14,829 cycles

FOUND EMERGENCY LIGHT TEST FAILED WITH FAULTS, INT LOADS EMER L, INT LOADS AFT L AND COMM EMER L, AFT L. REPLACED EPSU'S 11WL AND 13WL INCLUDING BATTERY PACKS. OPS CHECKS NORMAL.

Part: WARNING LIGHT — ILLUMINATED (CARGO DOOR) · airframe 40,901 hrs · 14,551 cycles

RETURNED TO FIELD DUE TO FWD CARGO DOOR INDICATION.

Part: BATTERY — MALFUNCTIONED (CABIN) · airframe 25,479 hrs · 9,072 cycles

EPSU COMM FWD LT MESSAGE DURING EMERGENCY BATTERY SYS TEST. REPLACED BATTERY PACK AT DOOR 1 LEFT,

Part: LIGHT — BURNED OUT (CABIN) · airframe 38,258 hrs · 13,561 cycles

ONE LIGHT OF THE EMERGENCY LIGHTING PATH IS BURNED OUT ROW 15.

Part: STRINGER — CORRODED (FS 57-58) · airframe 37,911 hrs · 13,434 cycles

CORROSION ON STR 43L BETWEEN FS 57 AND FS 58. BUSINESS DECISION TO REPLACE STRINGER RATHER THAN REPAIR.

Part: STRINGER — CORRODED (FR 54-55) · airframe 37,911 hrs · 13,434 cycles

STRINGER 43L HAS CORROSION BETWEEN FS 54 AND FS 55.

Part: ACTUATOR — OUT OF LIMITS (SLATS) · airframe 31,702 hrs · 11,199 cycles

SLATS FAILED TO DEPLOY, S-CTRL FAULT ILLUMINATED. THE TORQUE LIMITER OF THE LT NR 2 SLAT OUTBOARD ACTUATOR WAS FOUND TRIPPED. THE SLAT STOP TO FWD ROLLER DIMENSION WAS ALSO FOUND OUT OF LIMIT. REPLACEMENT OF THE FAULTY SLAT ACTUATOR AND SUBSEQUENT ADJUSTMENT OF THE SLAT RIG WERE ACCOMPLISHED WITHOUT FURTHER ANOMALY.

Part: DOOR — LEAKING (CARGO)

ACFT EN ROUTE TO ORD, ECAM FWD CARGO DOOR, PRESSURIZATION FLUX. PATCH WITH SAM. FLT CONTINUED TO ORD AT 10 THOUSAND FT.

Part: SELECTOR VALVE — LEAKING (HYDRAULIC SYS) · airframe 19,630 hrs

YELLOW SYSTEM LO QTY IN FLIGHT. TURNED OFF PUMP PER ECAM. *S/D* FOUND LEAK AT AUTO BRAKE SELECTOR. REPLACED PACKING. SERVICED YELLOW SYSTEM TO FULL.

Part: OUTFLOW VALVE — BROKEN (CABIN)

PASSING 9000' GOT CABIN PRESSURE ECAM & MASTER WARNING. VERTICAL SPEED WAS UP TO 500+ AND DOWN TO -1200 FPM. CABIN TEMP WENT FROM WARM TO COLD SEVERAL TIMES BEFORE LANDING. RETURNED TO DEN. *S/D* FOUND BROKEN BACKSHELL ON ACTUATOR ELECTRONIC 1, 10HLA OF OUTFLOW VALVE. BROKEN BACKSHELL WAS CHAFING NUMEROUS WIRES. PROTECTED EACH WIRE IN CONNECTOR WITH HEAT SHRINK, REPLACED BACKSHELL AND SECURED.

Part: LIGHT — INOP (SEAT 3B)

EMERGENCY LIGHTS INOP AT SEAT 3B.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

CABIN EMERGENCY LIGHTING CHECK FAILS TEST. POWER SUPPLY INOPERATIVE. REPLACED POWER SUPPLY AT DOOR 1L.

Part: LAMPS — FAILED (CABIN)

EMERGENCY LIGHT SYSTEM FAILED TEST AT FORWARD FLIGHT ATTENDANT PANEL. *S/D* FOUND LAMPS FAILED. REPLACED AND OPERATIONALLY CHECKED NORMAL.

Part: WINDOW — LOOSE (RT COCKPIT)

CABIN DEPRESSURIZED DURING LANDING. FIRST OFFICERS WINDOW WAS THE SOURCE OF AIR LOSS. WINDOW IS LOOSE. WINDOW STARTED LEAKING ON DESCENT AND MOVED INWARD RELEASING CABIN PRESSURE ON TOUCH DOWN.