N405UA

Part: HYDRAULIC SYSTEM — LEAKING · airframe 87,532 hrs · 33,769 cycles

ECAM CAUTION MESSAGE - G RSVR LO AIR PR MESSAGE INOP - HYD ON DES INTO ORD 15K CREW DEBRIEF: ON DESCENT THROUGH 15,000, CREW NOTICED ECAM FOR GREEN SYSTEM LOW PRESSURE. THEY LOOKED AT THE HYD PAGE AND QUANTITY WAS NEAR ZERO (ARROW POINTING IN LOWER YELLOW BOX). PUMP. THEY USED THE ALTERNATE GEAR EXTEND PROCEDURES TO DROP THE THEY RAN THE ECAM PAGE AND TURNED OFF PTU AND GREEN HYDRAULIC BACK UP BELOW THE GREEN BAND. GEAR. AFTER LANDING THEY NOTICED GREEN HYDRAULIC SYSTEM ON ECAM LAST LEG ECAM REPORT SHOWS: HYD G RSVR LO LVL, HYD G ENG 1 PUMP FRESH HYD FLUID AROUND GREEN SYSTEM ACCUMULATOR AND ACCUMULATOR INDICATION MATCHING THE EXTERNAL GAUGE. ALL 3 HYDRAULIC LO PR, HYD G SYS LO PR. INITIAL WALK AROUND SHOWS FLIGHT DECK RESERVOIRS HAVE FLUID IN THEM AND ARE CLEAN AND DRY ALL AROUND. FROM THE VENT BELOW ALONG THE RIGHT SIDE OF AIRCRAFT BACK....ALL OTHERS LOOK NORMAL PRESSURE NEAR ZERO. THERE IS A TRAIL OF FRESH HYDRAULIC FLUID ALSO NOTICD STREAK OF WHAT LOOKS LIKE HYD FLUID RUNNDOWN DOWN A VENT BELOW THE TWO FAN COWLS ALL THE WAY BACK ON #1 ENG. SEE ATTACHED IMAGES. HOPE THIS HELPS PRESSURIZED HYDRAULIC SYSTEMS, CYCLED ALL FLIGHT CONTROLS AND TAXI CHECK PERFORMED ON LP 7059430. NO ECAM MESSAGES PRESENT. SEVICED HYDRAULIC SYSTEMS NO LEAKS NOTED REF AMM 12-12-29. ADD EMP:172292

Part: SERVO VALVE — FAILED (MLG BRAKES) · airframe 86,604 hrs · 33,358 cycles

AFTER TOFF AUTO BRAKESAND NORM BRAKES ECAM AFTER LANDING ANTI SKID AND N/W STRG ECAM LOG PAGE LOCKED BY TOMC.BRAKE SERVO VALVE (17GG) WAS REPLACED AND CAT III LAND VERIFY TEST PASSED. AIRCRAFT IS RESTORED TO FULL CAT III STATUS

Part: SENSOR — MALFUNCTIONED (TAT) · airframe 86,125 hrs · 33,149 cycles

LOSS OF ADR 1 AND 3 / .ADR 1 REPLACED TAT SENSOR 11FP1, REF TASK 34-11-18-000-001-A. OPERATIONS CHECK PASS. S/N OFF 0892. S/N ON 8166. TRACKING NR 1182604. ROTABLE PARTS CHANGE WAS INDICATED-TT NR 1182604 SN OFF 0892 IPC REFERENCE 32-11-18-000-001-A SENSOR, TOTAL T OFF 31-4112-9-9001 0892 ON 31-4112-9-9001 8166.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 85,821 hrs · 33,015 cycles

CABIN EMERGENCY LIGHTS OPERATIONAL CHECK. OPERATIONS CHECK FAILED. MULTIPLE ATTEMPTS ALL COME BACK WITH EPSU BATTERY FWD LT FAULT. SEE ATTACHED PHOTO. REPLACED BATTERY AT FWD LT AND MID RT LOCATIONS. EMERGENCY LIGHTS TEST PASSES, REF AMM 33-51-38.

Part: CONNECTOR — BROKEN (EXIT SIGN) · airframe 85,610 hrs · 32,916 cycles

R1 DOOR EMERGENCY EXIT IDENTIFIER LIGHT (LOWER DOOR SURROUND) IS IN OP, INTERMITTENT {A3NB-33-3-6012} - GENERATED BY V061627 ON N/R 9296370 AT HAECO LCQ.

Part: IDG — FAULTED (NR 1 GENERATOR) · airframe 81,518 hrs · 31,069 cycles

GEN 1 FAULT REF TSM TASK 24-20-00-810-803-A, STEP 4 A . INSPECTED POWER FEEDER CONNECTOR AT FIREWALL. NO BURNING/ARCING DAMAGE OR CORROSION. RECONNECTED POWER FEEDER CONNECTOR. VERIFIED NO BURNING/ARCING OR SIGNS OF CORROSION ON POWER FEEDER CONNECTOR AT PYLON PER TSM 24-20-00-810-803-A. VERIFIED INSTALLATION OF PER FEEDER CONNECTOR TO PYLON. REMOVED AND REPLACED #1 IDG UP TO AND INCLUDING STEPS 4. F. (16) PER AMM 24-21-51 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1163111 SN OFF 0232 GENERATOR, INTE OFF 31-2411-9-0001 0232 ON 31-2411-9-0001 1041 FINISHED INSTALLATION OF #1 ENGINE IDG REF MM 24-21-51. OPS AND LEAK CHECKED GOOD. COMPLIED WITH INSPECTION PORTION OF NUMBER ONE ENGINE IDG ENGINE INSTALLATION REF 24-21-51 AND GMM 09-10-05

Part: SKIN — GOUGED (FUSELAGE) · airframe 80,793 hrs · 30,754 cycles

3 EA GOUGES BETWEEN FR51-52 AND STR 38- 39 FROM CONTACT WITH WTB FAIRING 198GB. INSTALLED REPAIR INTERNAL DOUBLER AT FR 51-52, STR 38-39 IAW SRM 53-41-11-300-010 FIG 20109 SHEET 2. ORIGINAL MATERIAL .016.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 80,793 hrs · 30,754 cycles

R-1 DOOR FRAME 16 NR 7 DOOR STOP INBD LOWER HOLE PRODUCES REJECTABLE INDICATIONS DURING RHFEC BOLT INSPECTION AD -2017-22-03. REPAIRED R1 DOOR FRAME BY REMOVE AND REPLACE NR 7 INTERCOSTAL IAW SRM 51-42-11 AND DWG B53114223000.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 80,793 hrs · 30,754 cycles

L-1 DOOR FRAME 16 NR 7 DOOR STOP INBD UPPER HOLE PRODUCES REJECTABLE INDICATIONS DURING RHFEC BOLT INSPECTION AD- 2017-22-03. UPON FURTHER EVALUATION FR16 NR 7 INTERCOSTAL FITTING HAD REJECTABLE INDICATIONS. REMOVED AND REPLACED INTERCOSTAL FITTING IAW AMM 52-11-31-400-002-A, SRM 51-42-11 PARA E AND DWG B53114 236.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 80,793 hrs · 30,754 cycles

L1 DOOR FRAME 16 NR 1 DOOR STOP INBD LOWER HOLE PRODUCES REJECTABLE INDICATIONS DURING RHFEC BOLT HOLE INSPECTION ON LCQ REF 9292176 SPEC A3NB-53-4-6304 AD 2017-22-03. R&R INTERCOASTAL ON FRAME 16 LT AT DOOR STOP NUMBER ONE IAW SRM 51-42-11.

Part: COMPUTER — FAULTY (SLAT SYSTEM) · airframe 76,418 hrs · 28,789 cycles

FLAP SYS 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. EMERGENCY DECLARED. REPLACED THE NR 1 SLAT FLAP CONTROL COMPUTER IAW AMM 27-51-34-400-001 AND OPS CHECKED GOOD IAW AMM 27-54-00-710-002

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 76,271 hrs · 28,718 cycles

LEFT WING OTBD FLAP LEADING EDGE HAS CORROSION ON FWD SPAR FWD FACE AROUND FASTENER HOLE JUST ABOVE FLAP TRACK NR 3 INSIDE PANEL NR 2. REMOVED CORROSION LT WING OTBD SPAR WEB AND FOUND TO BE OUT OF LIMITS, IAW SRM 51-74-00. REMOVED AND REPLACED THE SPAR WEB IAW SRM 57-53-20 PG 229-231.

Part: DOOR FRAME — CORRODED (EMERGENCY HATCH) · corrosion level 2 · airframe 76,271 hrs · 28,718 cycles

LEFT FWD EMERGENCY HATCH HAS CORROSION ON INNER STRUCTURE FITTING AFT LOWER CORNER. REMOVED CORROSION AT LH FWD EMERGENCY HATCH T SECTION LOWER FRAME. NO ALLOWABLE DAMAGE LIMITS IN SRM. R & R T SECTION, CURVED EDGE FRAME, SEAL RETAINER IAW SRM 51-42-11,PAR.6,5,3. 51- 49-60, TABLE 11. 51-73-00, PAR.5. 52-20-00. 51-72-11, PAR.4,5.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,271 hrs · 28,718 cycles

AFT CARGO AT FR62 STR40R HAS CORROSION. REMOVED AND REPLACED STR4 0 FROM FR58 TO FR64 IAW SRM 51-42-11 PARA 6 AND 7.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 76,271 hrs · 28,718 cycles

AFT CARGO COMPARTMENT FR54-55 STR43L HAS CORROSION. REMOVED AND REPLACED STR43L FROM FR54-60 IAW SRM 51-42-11 PARA 6 AN 7.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,271 hrs · 28,718 cycles

L2 DOOR SILL IS CORRODED UNDER FWD AND AFT GIRT BAR PLATE FITTINGS FR66-FR68. REPLACED L2 DOOR SILL IAW A320 SRM 51-42-11.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,271 hrs · 28,718 cycles

FWD CARGO CLEAT FR32 STR40R-41R CLEAT HAS CORROSION. :REPLACED CLEAT AT FR32 ST R40R-41R IAW A320 SRM 51-42-11.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 76,271 hrs · 28,718 cycles

LT AFT CABIN SHEAR WEB FR68-69 IS CRACKED. REMOVED & REPLACED CRACKED SHEAR WEB LT SIDE FR68-69 IAW SRM 51-42-11 PN D5348002069601.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,271 hrs · 28,718 cycles

LT AFT CABIN SHEAR WEB AT FR69-70 HAS CORROSION ON LOWER SURFACE FR69-70, STR23L-STR22L. BLENDED CORR ON SHEAR WEB SUPPORT, OUT OF LIMITS. INSTALLED NEW SHEAR WEB SUPPORT PN D53 47112320200 IAW 51-42-11.

Part: SHEAR TIE — CORRODED (FRAME 33) · corrosion level 2 · airframe 76,271 hrs · 28,718 cycles

FWD CARGO FRAME 33 STRINGERS 41 - 42L SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE.

Part: SHEAR TIE — CORRODED (FRAME 31) · corrosion level 2 · airframe 76,271 hrs · 28,718 cycles

FWD CARGO FRAME 31 STRINGERS 41 - 42R SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE.

Part: SHEAR TIE — CORRODED (FRAME 33) · corrosion level 2 · airframe 76,271 hrs · 28,718 cycles

FWD CARGO FRAME 33 STRINGERS 41 - 42R SHEAR TIE HAS CORROSION :REMOVED AND REPLACED THE SHEAR TIE.

Part: SHEAR TIE — CORRODED (FRAME 32) · corrosion level 2 · airframe 76,271 hrs · 28,718 cycles

FWD CARGO FRAME 32 STRINGERS 41 - 42L SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE.

Part: SHEAR TIE — CORRODED (FRAME 32) · corrosion level 2 · airframe 76,271 hrs · 28,718 cycles

FWD CARGO FRAME 32 STRINGER 39-40R SHEAR TIE HAS CORROSION :REMOVED AND REPLACED THE SHEAR TIE.

Part: SHEAR TIE — CORRODED (FRAME 33) · corrosion level 2 · airframe 76,271 hrs · 28,718 cycles

FWD CARGO FRAME 33 STRINGERS 40 - 41R SHEAR TIE HAS CORROSION :REMOVED AND REPLACED THE SHEAR TIE.

Part: SHEAR TIE — CORRODED (FRAME 32) · corrosion level 2 · airframe 76,271 hrs · 28,718 cycles

FWD CARGO FRAME 32 STRINGERS 41 - 42R SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE.

Part: SHEAR TIE — CORRODED (FRAME 32) · corrosion level 2 · airframe 76,271 hrs · 28,718 cycles

FWD CARGO BAY FRAME 32 STRINGERS 42 - 43L SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE.

Part: SHEAR TIE — CORRODED (FRAME 32) · corrosion level 2 · airframe 76,271 hrs · 28,718 cycles

FWD CARGO FRAME 32 STRINGERS 40 - 41L SHEAR TIE HAS CORROSION :REMOVED AND REPLACED THE SHEAR TIE.

Part: SHEAR TIE — CORRODED (FRAME 34) · corrosion level 2 · airframe 76,271 hrs · 28,718 cycles

FWD CARGO FRAME 34 STRINGERS 41 - 42L SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE.

Part: DOOR SILL — CORRODED (FRAME 68) · corrosion level 2 · airframe 76,271 hrs · 28,718 cycles

R2 DOOR SILL HAS CORROSION ON FRAME 68 STRINGERS 22 - 23R. REPAIRED THE DOOR SILL IAW SRM 53-41-14.

Part: STRINGER — CORRODED (FRAME 34) · corrosion level 2 · airframe 76,271 hrs · 28,718 cycles

FWD CARGO STRINGER 41R HAS CORROSION FRAME 34. REMOVED AND REPLACED THE STRINGER IAW SRM 53-21-13

Part: WIRE — DAMAGED (EEC) · airframe 75,035 hrs · 28,151 cycles

DURING CLIMB, NR 1 ENGINE AMBER EGT INDICATION ILLUMINATED. LOOKED AT EGT & NOTICED IT WAS OVER 600 DEG FOR 5 SECS, BUT COULD NOT GIVE AN EXACT TEMP TO MX. R & R FOUR WIRES THAT WERE FOUND DAMAGED THAT GOES FROM HPC STAGE SOLENOID TO EEC. PERFORMED POWER RUNS & OPERATIONS CHECKS IAW MM 71-00-00-860-010 -B13 & ENG OVERTEMP CONDITIONS EGT 2-4-52.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 71,606 hrs · 26,680 cycles

L2 DOOR FRAME 68 STOP FITTING NR 7 MOUNT HOLE HAS A CRACK INDICATION. REPAIRED WITH FREEZE PLUG IAW SRM 53- 41-12 PARA 5E FIG 204.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 71,606 hrs · 26,680 cycles

AFT RT PAX DOOR FRAME 68 RT NR 7 FITTING LOWER OTBD HOLE HAS CRACK INDICATION. CLEANED UP HOLE & NDT INSP HFEC IAW NTM 51-10-08 & NO CRACK FOUND. FABRICATED FREEZE PLUG & REPAIR FITTING FOR AFT END & INSTALLED IAW SRM 53-41-12.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 71,606 hrs · 26,680 cycles

L2 DOOR FRAME 66 STOP FITTING 1IB UPPER MOUNT HOLE HAS A CRACK INDICATION. REPAIRED WITH A FREEZE PLUG IAW SRM 53-41-12 PARA 5E FIG 204.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,606 hrs · 26,680 cycles

R2 DOOR SILL FRAME 68 INBD & FWD OF AFT GIRT BAR FITTING, CORROSION AT 7 LOCATIONS. R & R R2 DOOR SILL IAW SRM 51-42-11.

Part: SKIN — GOUGED (FUSELAGE) · airframe 71,606 hrs · 26,680 cycles

THREE EACH SKIN GOUGES BETWEEN FRAME 51 - 52 & STRINGER 38 -39R FROM CONTACT WITH WTB FAIRING 198GB. BLENDED GOUGES IAW SRM 53-41-11 F105. NOMINAL SKIN THICKNESS IS .157" IAW SRM 53-41-11 PAGE 15. IAW NTM 51-10-04 PB4 MINIMUM MATERIAL REMAINING OF 3 AREAS ARE .143", .136" & .134". MAX MAT LOSS OF .023" & WITHIN SRM 53-41-11 FIG 105 SHEET 2 LIMIT. THIS SRM REFERS TO SRI 53-41-11-1-010-00 TABLE 123 TO INSPECT EVERY 2300C SINCE 16400C THRESHOLD HAS PASSED.

Part: SKIN — GOUGED (FUSELAGE) · airframe 71,606 hrs · 26,680 cycles

THREE EA SKIN GOUGES BETWEEN FRAME 51 - 52 & STRINGER 38 - 39R FROM CONTACT WITH WTB FAIRING 198GB. BLENDED GOUGES IAW SRM 53-41-11 F105. NOMINAL SKIN THICKNESS IS .157" IAW SRM 53-41-11 PG 15.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,606 hrs · 26,680 cycles

R2 DOOR SILL FRAME 68 INBD & FWD OF AFT GIRT BAR FITTING CORROSION AT 7 LOCATIONS. R & R R2 DOOR SILL IAW SRM 51-42-11.

Part: FRAME — CORRODED (FUSELAGE) · airframe 71,606 hrs · 26,680 cycles

RIGHT FRAME 68 FWD FACE JUST ABOVE FLOOR LEVEL IS CORRODED. ORIGINAL THICKNESS .098 INCHES, MATERIAL LOSS OF .035 INCHES IS OUT OF LIMITS IAW SRM 53-41-12 FIG 102. REPAIRED IAW SRM 53-41-12 PAR 5A FIG 201. DOUBLER INSTALLED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,270 hrs · 25,351 cycles

SEAT ROW 37 ABC, EMERGENCY EXIT LIGHT INOPERATIVE. TERMINATED CONNECTOR EMERGENCY EXIT LIGHT AT SEAT ROW 37 ABC, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,270 hrs · 25,351 cycles

SEAT ROW 27 ABC, EMERGENCY EXIT LIGHT INOPERATIVE. TERMINATED CONNECTOR AT EMERGENCY EXIT LIGHT SEAT ROW 27 ABC, OPERATIONS CHECKED GOOD.

Part: CONNECTOR — UNSECURE (AUTOPILOT SYS) · airframe 67,829 hrs · 25,169 cycles

AUTO FLIGHT 'RUDDER TRIM 1 FAULT' DISPLAYED ON UPPER ECAM SCREEN. PLACED RUDDER TRIM 1 ON M EL IAW MEL 2722A DF128. CAT STATUS DOWNGRADED TO AUTO LAND LIMITS CAT 3 SINGLE, AC OK TO CONTINUE. SECURED FAC NR 1 BENCH PLUG, CHECKED GOOD. RETURNED ACFT TO CAT 3 STATUS.

Part: SEAT BELT — DETACHED (CABIN) · airframe 67,312 hrs · 24,980 cycles

SEAT BELT AT 25D BECAME DETACHED. ATTACHMENT POINT BROKEN.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 67,251 hrs · 24,954 cycles

CAPTAIN`S 02 MASK INOPERATIVE, CAN HEAR SQUEAL FROM MIC.

Part: OXYGEN BOX — FAULTY (COCKPIT) · airframe 67,247 hrs · 24,951 cycles

CAPTAIN`S 02 MASK INOPERATIVE, CAN HEAR SQUEAL FROM MIC. SWAPPED FIRST OBSERVER`S OXYGEN BOX WITH CAPTAINS, MIKE WORKS NORMALLY AT CAPTAIN'S POSITION. FIRST OBSERVER`S O2 MIKE INOPERATIVE, BUT O2 MASK OTHERWISE WORKS FOR O2. STICKER APPLIED IAW MEL 2511S. PARTS: 649-0375, MR35114 MASK

Part: AMU — FAULTY (COCKPIT) · airframe 67,244 hrs · 24,950 cycles

CAPTAIN'S OXYGEN MASK MICROPHONE IS INOPERATIVE. REPLACED CAPTAIN'S O2 MASK IAW AMM, NO HELP. REPLACED CAPTAIN'S AUDIO PANEL IAW AMM, NO HELP. REPLACED AUDIO MANAGEMENT UNIT PN AMU2790CB04 - SERIAL 131. OPERATIONS CHECKED GOOD.

Part: SKIN — DAMAGED (LT WING) · airframe 66,715 hrs · 24,746 cycles

LEFT WING SKIN FUEL LANDING FOR ACCESS PANEL 540RB HAS 1 DAMAGED SCREW HOLE. HOLE WAS REPAIRED IAW ECRA 5720-0243 5 AND REO-L01409, REV 1R.

Part: SKIN — DENTED (FUSELAGE) · airframe 66,715 hrs · 24,746 cycles

DENT ON FUSELAGE, LT NOSE NEAR NOSE UNDER LT SIDE STBY STATIC AREA. DENT IS AT FRAME 5, STR 31LT 1FT AFT OF THE FWD LWR EE DR. MEAS 2 AND 1-2" BY 1 AND 3-4TH .015" DEEP. ACCOMPLISHED VISUAL INSPECTION IAW SRM 53-11-11, DIG 103 PGS 137-138 NO CRACKS NOTED. REPAIRED DENT IAW SRM 53-00-11 FIG 240.

Part: SENSOR — FAULTY (EQ COOLING DUCT) · airframe 66,711 hrs · 24,744 cycles

VENT BLOWER FAULT DURING CLIMB OUT. REPLACED DUCT TEMP SENSOR IAW 21-26-12-400-001-A, NO FAULTS NOTED, SYS OPS CHECKED GOOD ON GROUND.

Part: VALVE — FAILED (CABIN PRESSURE) · airframe 51,787 hrs · 20,833 cycles

CREW REPORTED LOSING CABIN PRESSURE ON DESCENT. FAULT INDICATED CABIN PRESSURE SAFETY VALVE HAS FAILED OPEN ON ECAM.

Part: STRUCTURE — DAMAGED (RT WING) · airframe 66,121 hrs · 24,506 cycles

REMOVED RT WING FENCE DUE TO DAMAGE. REPLACED RT WING TIP FENCE IAW AMM.

Part: SHOCK ABSORBER — LOW (MLG) · airframe 66,121 hrs · 24,506 cycles

LANDING GEAR SYSTEM DISAGREE MSG, RTFL. LG SYS DISAGREE MESSAGE DISPLAYED AND UNABLE TO RAISE LANDING GEAR AFTER TAKEOFF. CREW CYCLED GEAR THRU SEVERAL CYCLES AND NO HELP. LOUD BANGING NOISE HEARD AFTER GEAR CYCLING ATTEMPT. ACFT ALSO SHOWS IN FLT PHASE 8 WHILE STILL AIRBORNE. SERVICED LT & RT MLG SHOCK ABSORBERS PER AMM AND PERFORMED FUNCTIONAL TEST PER AMM, OPS TEST NORMAL.PERFORMED FUNCTIONAL TEST OF THE NORMAL EXTENSION AND RETRACTION OF THE LANDING GEAR PER AMM, OPS CHK NORMAL.

Part: CONTROL MODULE — MALFUNCTIONED (MLG HANDLE) · airframe 66,041 hrs · 24,466 cycles

GEAR HANDLE STICKS WHEN TRYING TO DROP GEAR, PERFORMED SEVERAL ATTEMPTS REQUIRED. REPLACED LANDING GEAR CONTROL LEVER MODULE PER MM.

Part: BRACKET — MISINSTALLED (CARGO BAY) · airframe 65,877 hrs · 24,407 cycles

FORWARD CARGO NESTING SYSTEM CENTER BAY WILL NOT LOCK. FOUND BOTH AFT ANGLE STOP BRACKETS INSTALLED UPSIDE DOWN. REPOSITIONED BOTH ANGLE STOP BRACKETS. RESET BOTH C/B'S. OPS CHECK GOOD. DF971 REMOVED.

Part: ENGINE — SHUTDOWN (NR 2) · airframe 65,831 hrs · 24,391 cycles

INFLT SHUTDOWN, FLIGHT DIVERTED. MULTIPLE FAILURES IN FLIGHT. ACP INSPECTION. FOUND MASTER MCD HEAVILY COVERED WITH METAL. REPLACED ENGINE.

Part: STRIKER — DAMAGED (COCKPIT DOOR) · airframe 65,744 hrs · 24,360 cycles

COCKPIT DOOR 'FAULT' LIGHT AND DOOR CONTROLLER 'TOP STRIKE' OR 'LOWER STRIKE' LIGHT IS ON. BOTTOM FLT LIGHT ON. BOTTOM LATCH NOT LATCHING. REPLACED LWR DOOR STRIKE ASSEMBLY, OPS CHECKED GOOD.

Part: BOLT — SHEARED (TOW LUG) · airframe 65,709 hrs · 24,347 cycles

ON PUSHBACK, NLG LUG BOLTS SHEARED. REPLACED NLG TOWING ATTACHMENT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,149 hrs · 24,125 cycles

CEILING LIGHTS INOPERATIVE. NO CIDS 1 DATA INTERMITTENT. PFR SHOWED CIDS 1 AS INTERMITTANT. CIDS 1 WILL NOT GO INTO BITE. REPLACED CIDS 1 CONTROLLER. BITE TEST IS GOOD. ALL INDICATIONS NOW NORMAL. REPLACED ACARS MU PER AMM, OPS CHECKED OKAY.

Part: SWITCH — FAULTY (COCKPIT) · airframe 64,915 hrs · 24,038 cycles

AIRCRAFT EMERGENCY EVAC HORN GOES OFF IN FLIGHT. DUE TO CONTINUED EVAC HORN GOING OF IN FLIGHT. REPLACE EVAC PUSH BUTTON SWITCH (3WP) SEE IPC 25-63-08-01 FOR PARTS. REPLACED PB SWITCH, 3WP, TESTED NORMAL.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 64,104 hrs · 23,701 cycles

02 MASK AT SEAT 27ABC DEPLOYED. SECURED MASK. DROP TEST OKAY.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 64,104 hrs · 23,701 cycles

THE 02 MASK AT SEAT 27ABC DEPLOYED. SECURED MASK. DROP TEST OKAY.

Part: PAINT — PEELING (RT AILERON) · airframe 63,957 hrs · 23,640 cycles

AT DEPARTURE TIME, RAMP REPORTED PEELING ON TOP OF RIGHT AILERON. REPAIRED AND APPLIED PRIMER, STILL NEEDS TOP COAT PAINT.

Part: INDICATOR — LEAKING (HYDRAULIC SYS) · airframe 63,860 hrs · 23,603 cycles

CREW REPORTS GREEN HYD RESERVOIR QTY LOSS. REPLACED GREEN SYSYEM DIFF PRESS INDICATOR ON THE BRAKE FILTER MOD. ALSO REPLACED FILTER ASSY. LEAK CHECKS GOOD, CLEANED FUSELAGE AND WHEEL WELL AREA.

Part: EIU — MALFUNCTIONED (NR 2 ENGINE) · airframe 63,831 hrs · 23,592 cycles

DURING ENGINE TEST, NR 2 ENGINE STALL. NR 2 ENGINE FADEC 2A DOES NOT INTERFACE WITH BOTH CDU'S. REPLACED NR 2 EIU. ACP OPS CHK REF MM. CHKS OK.

Part: CAP — MISSING (RT WING TE FLAP) · airframe 63,428 hrs · 23,447 cycles

RT INBD FLAP RT INBD CANOE MISSING CAP. BOLT AND BUSHING MIGRATED OUT.

Part: ACTUATOR — FAULTED (NR 1) · airframe 63,401 hrs · 23,436 cycles

AUTO FLT 'YAW DAMPER 1' DISPLAYED ON UPPER ECAM SCREEN. NR 1 YAW DAMPER INOPERATIVE. REPLACED ACTUATOR.

Part: CAP — MISSING (TE FLAP) · airframe 63,197 hrs · 23,349 cycles

RIGHT INBOARD FLAP CANOE MISSING CAP. BOLT AND BUSHING MIGRATED OUT. REMOVED SAFETY WIRE ON BOLT. REF IPC 57-51-33-2B, ITEM 70, PCN 110-3208, AND ITEM 90, P-N D5754055520000, ITEM 95, P-N D575405462000, NEEDED FOR REPAIR. 1 OF EA. CDL 27AA COMPLIED WITH. ACP REACTIVATION OF THE FLAP TRACK FAIRING PROCEDURE WHEN FAIRING IS REPLACED (REF MM 57-55-00-401) REPLACED & INSTALLED RIGHT INBOARD FLAP CANOE PER MM.

Part: HANDLE — OUT OF ADJUST (DOOR SLIDE) · airframe 62,538 hrs · 23,101 cycles

L2 DOOR HANDLE RIDES UP IN FLIGHT DISARMING DOOR SLIDE. ADJUSTED DOOR ESCAPE SLIDE MECHANISM PER AMM. PRESSURIZED ACFT & CHECK DOOR HANDLE ALL INDICATIONS & DOOR HANDLE CHECKS NORMAL.

Part: STRAP — LOOSE (EVAC SLIDE) · airframe 62,517 hrs · 23,093 cycles

DOOR 2L SLIDE ARMING HANDLE IS NOT FLUSH WHEN IN THE ARMED POSITION. SECURED LOOSE SLIDE COVER STRAPS. ARMING HANDLE OPERATES NORMAL.

Part: BOLT — BACKED OUT (NR 2 EXHAUST) · airframe 62,436 hrs · 23,065 cycles

ENG 2 - TAIL CONE HAS 7 (OF 13) ATTACH BOLTS BACKED OUT AS FOLLOWS (CLOCK POSITION, DISTANCE BACKED OUT): 2:45, 3-16": 3:30, 1-8": 4:30, 1-8": 5:30, 3-16": 6:30, 1-8": 7:30, 7-32": 9:15, 5-32". FROM BASE WRITE-UP U5015K. CHECK TURBINE EXH CASE SHANK NUTS AND REPAIRED IF FOUND DAMAGED OR LOOSE.

Part: ROD END — EXCESS PLAY (RUDDER) · airframe 62,322 hrs · 23,023 cycles

VIBRATION-NOISE ENCOUNTERED IN FLIGHT. REF FLT MANUAL 12.20.1 NEED TO COMPLETE VIBRATION REPORTING CHECKLIST AND DEBRIEF MAINTENANCE (SAMC) ON ARRIVAL TO DESTINATION STATION. CREW COMMENTS: LIGHT VIBRATION ABOVE FL200+ 300 KNOTS. STOPPED FL300+ BELOW 290 KNOTS. FELT IN ALL AREAS. ACP RUDDER SERVO CONTROL EXCESSIVE PLAY CK PER MM. FOUND BLUE SERVO CONTROL ROD END WITH EXCESSIVE PLAY. REPLACED ROD END PER MM. RECHECK FOUND WITHIN LIMITS.

Part: SLIDE — UNSECURE (L2 DOOR) · airframe 62,171 hrs · 22,968 cycles

ON LANDING, SLIDE AT L2 DOOR CAME LOOSE FROM DOOR. TO REPLACED L2 DOOR SLIDE PER AMM. RIG AND OPS CHECKED IAW AMM. REF ICS GROUP NR 1 OP AND INDICATION NORMAL.

Part: DRAIN LINE — LEAKING (GALLEY) · airframe 62,071 hrs · 22,937 cycles

FWD GALLEY DRAIN LINE HAS LEAK. CLEAN UP BELLY AREA OF WATER. LEAK ONLY COMES FROM FWD GALLEY SINK. LEAK IS COMING FROM PREVIOUS REPAIR ON FITTING BELOW FLOOR BOARD FEW INCHES FROM FUSELAGE SKIN. REPLACED DRAIN LINE ABOVE GALLEY FLOORBOARD PER IPC, LEAK CHK OKAY.

Part: OXYGEN MASK — FAILED (COCKPIT) · airframe 61,725 hrs · 22,826 cycles

1ST OBSERVER O2 MASK FREEFLOWS. REPLACED MASK, OPS OKAY.

Part: SWITCH — STICKING (TOILET) · airframe 61,366 hrs · 22,701 cycles

AFT LAVATORY DOESN’T STOP FLUSHING, THE PROBLEM IS THE FLUSH BUTTON, IT STICKS IN THE 'ON' POSITION, RESET TOILET VACUUM SYS CIRCUIT BREAKER, OPS CHECKED OKAY.

Part: BOLT — DEFECTIVE (EVAC SLIDE) · airframe 60,669 hrs · 22,375 cycles

DOOR 1L-GUST LOCK STICKS-HARD TO RELEASE DOOR TO CLOSE. REPLACED UPPER FWD ATTACH BOLT FOR SLIDE. OPERATES NORMALLY. ACCOMPLISHED RII INSPECTION AS REQUIRED REF MM. SLIDE PIN REMOVED AND STOWED PIN, VERIFIED BY MGMT.

Part: FIRE BOTTLE — EMPTY (CABIN) · airframe 60,634 hrs · 22,357 cycles

AFT CABIN, FWD LAV, FIRE EXT BOTTLE PRESSURE EMPTY IN LAV WASTE BIN AREA. REPLACED FIRE EXTINGUISHER BOTTLE OFF S/N 28651 AND ON S/N 48498.

Part: SENSOR — FAULTY (TAT) · airframe 60,634 hrs · 22,357 cycles

ADR 1 ECAM, FLIGHT DIVERTED. SAMC TEXT: *UPDATE* CFDS SHOWS TAT SENSOR 11FP1 FAULT SEEN BY BOTH ADR1 AND ADR3. SENSOR PCN 484- 0084. REPLACED TAT SENSOR 1, REF TSM 34-11-00-810-863 AND AMM-34-11-18. ACP SENSOR TEST. NO FAULTS. CONCURRED WITH OPBLM.

Part: BOTTLE — DISCHARGED (L1 DOOR) · airframe 60,514 hrs · 22,311 cycles

DOOR 1L EMERGENCY CYLINDER PRESSURE LOW. SERVICED DOOR EMERGENCY ACCUMULATOR.

Part: ACTUATOR — FAILED (HORIZ STAB) · airframe 60,086 hrs · 22,153 cycles

ELAC 1 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. - F-CTL. SAMC TEXT: ECAM FAULT 27-00 ELAC2 PITCH FAULT IN CONJUNCTION WITH CFDS 27-44-51 (06) THS ACTR POS ERROR 9CE OF ELAC2 ID: EFCS1 AND 27-44-51 (06) THS POS ACTR POS ERR 9CE OF ELAC1 ID:EFCS1 REF TSM FAILURE OF THE THS ACTUATOR. REPLACED THS ACTUATOR.

Part: ACTUATOR — FAULTY (HORIZ STAB) · airframe 60,056 hrs · 22,139 cycles

ECAM ELAC 1 AND 2 FAULT. ACP'D TSM AND FOUND ELAC 1 & SEC 1 SERVO MOTOR NOT WORKING. REPLACED PITCH TRIM ACT ON THS PER AMM, TESTS OKAY PER AMM. ACCOMPLISHED CAT III TEST PER AMM, CHECKS OKAY.

Part: SINK — MALFUNCTIONED (LAVATORY) · airframe 59,998 hrs · 22,114 cycles

FWD LAVATORY SINK WILL NOT STOP FLUSHING. SHUT OFF WATER SUPPLY TO FWD LAV SINK AND APPLIED MEL. WATER SHUT OFF PER MEL.

Part: CONE — CRACKED (NR 2 EXHAUST) · airframe 59,939 hrs · 22,091 cycles

NR 2 ENGINE EXHAUST CONE HAS SEVERAL CRACKS AT FWD END BY MOUNT BOLTS. REPLACED EXHAUST CONE PER AMM.

Part: BLADE — BIRD INGESTION (LT ENGINE) · airframe 59,295 hrs · 21,845 cycles

LEFT ENGINE BIRD STRIKE. CONFERRED WITH ENGINE DESK. ENGINE WILL NEED TO BE REPLACED. REPLACED NR 1 ENGINE ACCT ONE 6TH STG HPC BLADE HAS A TEAR IN A BLADE TIP CURL. RPL'D ENGINE PER MT71-01

Part: ACTUATOR — SEIZED (TE FLAPS) · airframe 57,889 hrs · 21,244 cycles

FLAPS JAMMED ON EXTENSION TO FULL. WORKED NORMAL AFTER CYCLING. FOUND TORQUE LIMITER ON LT WING NR 1 FLAP ROTARY ACTUATOR. RESET LIMITER, DID NOT TRIP AFTER FLAP TEST. CALLS OUT TO REPLACE NR 1 ROTARY ACTUATOR AS A PRECAUTION. REPLACED LEFT WING NR 1 ROTARY ACTUATOR.

Part: CABLE — OUT OF ADJUST (GIRT BAR) · airframe 57,331 hrs · 20,952 cycles

RT AFT SLIDE INDICATION INOP ON DOOR-OXY SYS E CAM PAGE - DOOR-OXY. VERIFIED DOOR 2R ARMS AND DISARMS AND GIRT BAR ENGAGES AND DISENGAGES NORMALLY. ECAM DOOR PAGE DOOR SLIDE INDICATION INTERMITTENT.28AUG SFO CQT-:VERIFIED DOOR LOCKED AND ARMED PRIOR TO DEPT FLT 202. DOOR GIRT BAR ARMS NORMALLY, WHEN ARMING LEVER IS WIGGLED, ECAM ARM INDICATION IS INTERMITTENT. SUSPECT TARGET NEED ADJUSTMENT. ADJUSTED ARMING CABLE REF MM52-13-22. OPS AND INDICATION NORMAL.

Part: ANTENNA — CORRODED (AIRPHONE) · airframe 57,177 hrs · 20,888 cycles

RT SIDE AIRPHONE ANTENNA FOUND DAMAGED. ANTENNA IS CRACKED ALONG THE ENTIRE LENGTH OF THE BASE. REPLACED ANTENNA. ANTENNA WAS CORRODED.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,833 hrs · 20,736 cycles

SEAT 15C EMERGENCY EXIT LIGHT INOP. FOUND CONNECTOR REMOVED. REINSTALLED. LIGHT OPS NORMAL 15C.

Part: STARTER — FAULTY (NR 2 ENGINE) · airframe 56,481 hrs · 20,555 cycles

RAMP AND PILOT REPORTS SPARKS COMING FROM NR 2 ENGINE DURING START. REPLACED STARTER ASSY AND STARTER VALVE. OPERATED STARTER, OPS CHECKED NORMAL.

Part: ELECTRICAL BOX — FAULTY (NLG STEERING) · airframe 56,439 hrs · 20,541 cycles

NW STRNG DISCNT MSG NOT DISPLAYED WITH PIN IN. REPLACED ELECTRICAL BOX NOSE NOSE WHEEL STEERING. OPS NORMAL.

Part: LIMIT SWITCH — FAULTY (RAT) · airframe 55,388 hrs · 20,115 cycles

RAT FAULT ON UPPER ECAM, FOUND JACK EJECTION 2454GE STOWED LIMIT SWITCH AT FAULT. RAT DEPLOYMENT OPERATION NORMAL MANUAL AND AUTOMATIC JUST STOWAGE AND ECAM DISPLAY FAULT DUE TO LIMIT SW. REPLACED EJECTION JACK, LEAK CK'D & OPS CK'D OKAY.

Part: STRUT — UNDERSERVICED (NLG) · airframe 55,192 hrs · 20,023 cycles

L/G SHOCK ABSORBER FAULT, RTFL. PFR FAULTING PROX SENSORS 24GA AND 25GA, NLG EXTEND SENSORS. FOUND NOSE STRUT LOW. NECESSARY TO SWING NLG DUE TO SENSOR FAULT AND STRUT SERVICE. REPLACED ASSOCIATED HARDWARE FOR BARREL FITTING ACCT BOLTS WERE WORN. CYCLED GEAR SEVERAL TIMES. SWUNG GEAR CHECKS OKAY.

Part: ENGINE — VIBRATION (NR 2) · airframe 53,865 hrs · 19,422 cycles

WHILE FLYING THROUGH TURBULENCE, NOTICED HIGH N1 VIBES FOR ENG 2. FLIGHT DIVERTED. CHECKED CHIP DETECTORS, NO METAL FOUND. ACP'D BOROSCOPE, NO LIMITING DEFECTS NOTED. ACCMP'D GENERAL VISUAL INSPECTION OF ENG 2 INLET & EXHAUST LOOK FOR METAL IN THE TAILPIPE. NO METAL IN THE TAILPIPE. CHK'D CFDS FOR VIBRATION RELATED FAULTS & ACCOMPLISHED EVMU TEST. NO FAULTS ON POST FLIGHT REPORT, NOTHING ON LAST LEG REPORT, EVMU TEST PASSED, NO CLASS 3 FAULT RELATED TO EVMU. RECHECKED CHIP DETECTORS ACCOMPLISHED VIBRATION SURVEY TEST NR 8 MAX N1 VIBRATION WAS 2.1 UNITS AT 82 PERCENT N1. CONFIRMED FINDINGS WITH OPBLM. A/C CLEARED FOR SERVICE.

Part: BLEED VALVE — FAILED (NR 1 ENGINE) · airframe 52,274 hrs · 18,820 cycles

APU BLEED FAULT. RTFL. REPLACED NR1 ENG HP BLEED VALVE. ALL CKS NORMAL AFTER HP VALVE REPLACEMENT.

Part: PLATE — CORRODED (FUSELAGE) · airframe 52,053 hrs · 18,744 cycles

ONE EA FLOORBOARD CONNECTOR PLATE CORRODED AT FRAME 68. MAJOR REPAIR ACCOMPLISHED. REPLACED PLATE AT FRAME 68.

Part: BEAM — CORRODED (FUSELAGE) · airframe 52,053 hrs · 18,744 cycles

BEAM 200 HAS SEVERAL PLACES CORRODED. MAJOR REPAIR ACCOMPLISHED. CONNECTED NEW BEAM 200 TO NEW BEAM 205. INSTALLED BEAM 200 IN ACFT.

Part: BEAM — CORRODED (FUSELAGE) · airframe 52,053 hrs · 18,744 cycles

BEAM 205 HAS 1EA HOLE CORRODED. MAJOR REPAIR ACCOMPLISHED. CONNECTED NEW BEAM 205 TO NEW BEAM 200 AND INSTALLED GALLEY HOLD DOWN NUTS IN RETAINERS. INSTALLED BEAM 205.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 52,053 hrs · 18,744 cycles

AFT RT SIDE TRIANGULAR SHEAR PLATE HAS CORROSION AT FASTENER HOLES. REMOVED 4EA LOCK FASTENERS AT SHEAR PLATE AND BEAM 205. REMOVED PLATE, DRILLED NEW PLATE, NEEDS INSTALL. INSTALLED 5 EA LOCK AND BLIND FASTENERS. COMPLETED INSTALLATION OF FRAME AND SHEAR PLATE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,053 hrs · 18,744 cycles

AFT TRIANGLE SHEAR PLATE ATTACH FRAME TO FUSELAGE CORRODED. REMOVED FRAME, DRILLED NEW FRAME NEEDS INSTALL. FRAME AND PLATE REPLACED COMPLETE. INSPECTED INSTALLATION AFT RT TRIANGLE TO FUSELAGE SHEAR PLATE SUPPORT FRAME.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,053 hrs · 18,744 cycles

BEAM 165 HAS 2EA HOLE CORRODED. REMOVED BEAM 165 AND TRANSFERRED BRACKETS TO NEW BEAM. JOINED BEAM BS 200 TO 165. INSTALLED BEAM 165 IN ACFT.

Part: SILL — CORRODED (FUSELAGE) · airframe 52,053 hrs · 18,744 cycles

DOOR 2R SILL PLATE HAS CORROSION IN SEVERAL PLACES. REMOVED SILL PLATE. REPLACED DOOR 2R SILL.

Part: BEAM — DAMAGED (FUSELAGE) · airframe 52,053 hrs · 18,744 cycles

BEAM 210 NEEDS REPLACED. STARTED REMOVAL OF BEAM. INSTALLED NEW BEAM.

Part: BEAM — CORRODED (FUSELAGE) · airframe 52,053 hrs · 18,744 cycles

BEAM 95 HAS CORROSION. INSTALLED NEW BEAM.

Part: MECHANISM — JAMMED (EMERGENCY EXIT) · airframe 51,401 hrs · 18,482 cycles

LEFT OVERWING EXIT IS NOT ARMED. FOUND DEBRIS IN MECHANISM. UNJAMMED OVERWING EXIT DOOR ARMED IND MECHANISM.

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO DOOR) · airframe 51,352 hrs · 18,459 cycles

FWD CARGO DOOR ECAM. ABORTED T/O AT 100 KNOTS. CYCLED DOOR ALL WINDOW SHOWED GREEN CREW REPORTS MESSAGE CLEARED.

Part: SLIDE — DAMAGED (L1 DOOR) · airframe 49,884 hrs · 17,948 cycles

DOOR 1L SLIDE-RAFT GIRT RUBS ON FLOOR AFTER INSTALLATION AND GIRT IS FRAYED. FOUND WEAR AND IMPROPER LANYARD INSTALLATION. REPLACED SLIDE.

Part: GIRT BAR — DIRTY (R1 DOOR) · airframe 49,767 hrs · 17,907 cycles

DOOR 1R SLIDE ARM LEVER BINDS ON ARMING AND DOES NOT STAY FLUSH. FOUND DEBRIS UNDER GIRT BAR FITTING. REMOVED DEBRIS FROM GIRT BAR FITTING. OPS CHECKED NORMAL.

Part: STRAP — UNSECURE (AFT GALLEY DOOR) · airframe 49,686 hrs · 17,881 cycles

AFT GALLEY DOOR WON'T ARM PROPERLY. FOUND LOOSE STRAP AROUND DOOR 2R GIRT BAR PREVENTING FULL MOVEMENT. RESECURED STRAP, CYCLED DOOR AND ARMED TWICE. NORMAL COCKPIT INDICATIONS, NO FURTHER JAMMING NOTED.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 48,794 hrs · 17,588 cycles

DOOR 1L EMERGENCY CYLINDER PRESSURE GAUGE READS ZERO. SERVICED CYLINDER TO FULL. NO REPEATS.

Part: SENSOR — FAULTY (NR 2 BLEED TEMP) · airframe 48,464 hrs · 17,469 cycles

RTFL DUE TO NR 2 ENGINE AIR BLEED FAULT. FOUND RT HEAT EXCHANGER OUTLET TEMP SENSOR FAULTY. REPLACED THE RT HEAT EXCHANGER OUTLET TEMP SENSOR AND REPLACE NR 2 FAN AIR VALVE CONTROL THERMOSTAT DUE TO NR 2 BLEED AIR OVERHEAT.

Part: SLIDE — FAULTY (DOOR 2L) · airframe 47,995 hrs · 17,290 cycles

DOOR 2L SLIDE WILL NOT ARM. ATTACH POINTS WERE FOUND DISLODGED. REPLACED BOTH ATTACH (UPPER) ASSYS.

Part: BOTTLE — LOW (L1 DOOR) · airframe 46,592 hrs · 16,763 cycles

FOUND DOOR 1L BOTTLE AT 1500 PSI READS LOW. SERVICED DOOR ASSIST SYSTEM TO PROPER PRESSURE.

Part: STRAP — OUT OF ADJUST (L2 DOOR) · airframe 46,424 hrs · 16,691 cycles

DOOR 2L HARD TO ARM.

Part: CONNECTOR — LOOSE (FWD CARGO DOOR) · airframe 45,414 hrs · 16,315 cycles

CREW REPORTS FWD CARGO DOOR ECAM ON CLIMB. FOUND A LOOSE CONNECTOR ON DOOR SWITCH. RESECURED, INDICATES OKAY.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 45,220 hrs · 16,242 cycles

CREW REPORTED SMOKE/SMELL IN CABIN & COCKPIT FOLLOWED BY A EXTRACT FAN FAULT. [SUP 05-08-07] VERIFIED THAT AVIONICS AIR EXTRACT FAN WAS FAULTY AND WAS REPLACED. SMOKE/ELECTRICAL SMELL DUE TO BEARING FAILURE.

Part: HYDRAULIC SYSTEM — FAILED · airframe 45,188 hrs · 16,230 cycles

YELLOW HYDRAULIC SYSTEM FAILURE. ECAM CAUTION MESSAGE - Y SYS LO PR MESSAGE INOP - HYD. CREW COMMENTS: YELLOW HYDRAULIC SYSTEM LOW QTY WARNING ECAM. FOUND ENGINE 2 HYDRAULIC FLEX HOSE, JUST ABOVE PRESSURE SWITCH, ON LEFT SIDE APROX 3 O'CLOCK POSITION LEAKING. REPLACED LINE AND ACCOMPLISHED ENGINE RUN LEAK CHECKS. HYDRAULIC RESERVISED TO FULL AS NECESSARY. OPS AND LEAK CHECKS GOOD. AS PRECAUTIONARY ACCOMPLISHED HYDRAULIC YELLOW SYSTEM CHECKS AND PUMP OPS CHECK AS REQUIRED FOR POSSIBLE CAVITATION. ALL CHECKS NORMAL.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 45,026 hrs · 16,169 cycles

RTFL WITH A HYDRAULIC SYSTEM PROBLEM. BLUE HYDDRAULIC PUMP OVER HEAT DURING FLIGHT. PUMP TURNED OFF. REPLACED PUMP.

Part: SLIDE — MISMANUFACTURED (RIGHT) · airframe 44,574 hrs · 16,017 cycles

NR 2 RIGHT MED SLIDE CAME IN WITHOUT THE POWER CABLE HOOKED UP. ELECTRICAL POWER CABLE CONNECTED.

Part: LIGHT — BURNED OUT (ROW 24ABC) · airframe 43,821 hrs · 15,752 cycles

EMERGENCY PATH LIGHT ON ROW 24ABC BURNED OUT. REPLACED LIGHT, TEST OK.

Part: BATTERY — FAILED (CABIN) · airframe 43,233 hrs · 15,547 cycles

AFT L EMERGENCY BATTERY FAILED EMERGENCY TEST.

Part: LIGHT — INOPERATIVE (ROW 20 ABC) · airframe 40,446 hrs · 14,551 cycles

EMERGENCY LIGHT AT SEAT ROW 20 ABC INOPERATIVE. REPLACED HARNESS.

Part: MOUNT — CRACKED (CARGO DOOR) · airframe 39,973 hrs · 14,391 cycles

AFT CARGO DOOR HANDLE MOUNT PLATE WHERE IT ATTACHES TO DOOR FRAME IS CRACKED.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 39,973 hrs · 14,391 cycles

FWD CARGO DOOR INNER SKIN IS CRACKED AT LWR AFT CORNER.

Part: MOUNT — CRACKED (CARGO DOOR HANDL) · airframe 39,973 hrs · 14,391 cycles

FWD CARGO DOOR HANDLE MOUNT PLATE WHERE IT ATTACHES TO THE DOOR FRAME IS CRACKED AT THE FRAME.

Part: ENGINE — STALLED (NR 1) · airframe 39,145 hrs · 14,122 cycles

NR 1 ENGINE EXPERIENCED TWO COMPRESSOR STALLS, ONE IN CRUISE AND ONE AT TOP OF DESCENT. ENGINE WAS CHANGED AND AIRCRAFT CONTINUED FLYING AFTERWARDS WITHOUT FURTHER INCIDENT. COMPRESSOR STALL WAS CAUSED BY HIGH-PRESSURE COMPRESSOR (HPC) BLADE DAMAGE PRIMARILY IN THE 6TH STAGE (R6), WHICH WAS CAUSED BY F.O.D. INGESTION.

Part: WARNING LIGHT — ILLUMINATED (GREEN HYD SYS) · airframe 35,990 hrs · 13,076 cycles

GREEN RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN. EMERGENCY DECLARED. LOST NOSE WHEEL STEERING. TOWED TO GATE. FOUND GREEN SYSTEM YAW DAMPER SERVO ACTUATOR LEAKING. YAW DAMPER SERVO ACTUATOR WAS REPLACED.

Part: SILL — CORRODED (FUSELAGE) · airframe 33,716 hrs · 12,264 cycles

R-2 DOOR SILL PLATE CORRODED. MAJOR REPAIR ACCOMPLISHED. AREA REPAIRED PER EVA IMC 30161 AND MAE EA 20-5341-13-A1060.

Part: STRUCTURE — CONTAMINATED (LT ELEVATOR) · airframe 33,716 hrs · 12,264 cycles

LT ELEVATOR HAD 3 AREAS OF WATER INGRESS. ALL AREAS ABOUT 1 INCH BY 1 INCH IN SIZE. TWO AREAS ON UPPER SURFACE: 1 LOCATED 98 INCHES FROM I/B EDGE & 2.5 INCHES FROM T/E, & 1 AT 177 INCHES FROM T/E & 10.5 INCHES FROM T/E, ONE AREA ON LWR SKIN 53 INCHES FROM I/B EDGE, & 4 INCHES FROM T/E. MAJOR REPAIR ACCOMPLISHED. REPAIRED PER SRM 55-21-11 REP 5E, PG 226, FIG 205, SHEET 3 & 4.

Part: SENSOR — DAMAGED (29GA) · airframe 30,529 hrs · 11,057 cycles

RETURNED TO FIELD DUE TO LEFT MAIN GEAR DOOR NOT UPLOCKED AFTER GEAR RETRACTION. SUPPLEMENTAL DATA UPDATE FOUND LH MAIN GEAR DOOR PROXIMITY SENSOR (29GA) AND CONNECTOR DAMAGED. REPLACED SENSOR AND CONNECTOR. ALSO DETERMINED LH MAIN LANDING GEAR UPLOCK ASSEMBLY NOT WORKING CORRECTLY. REPLACED UPLOCK ASSEMBLY.

Part: LANYARD — DETACHED (RT SERVICE DOOR)

AFT RIGHT DOOR LIFE RAFT LANYARD NEEDS TO BE RESTOWED. IT IS INHIBITING ARMING THE DOOR. LANYARD WAS PULLED FROM ITS ATTACHMENT POINT ON THE GIRT BAR TRIGGER BY A F/A. MAINTENANCE SUBSEQUENTLY REATTACHED THE LANYARD TO ITS PROPER LOCATION ON THE GIRT BAR TRIGGER.

Part: SEAT — CRACKED (CABIN)

DURING THE FIRST HEAVY MAINTENANCE VISIT (HMV-1) FOR THIS AIRCRAFT, VIRTUALLY 100 PERCENT OF THE COACH PASSENGER SEAT PANS WERE FOUND CRACKED. THESE SEAT PANS ARE INSTALLED ON RECARO MODEL 3410, 720 SERIES SEATS INSTALLED IN A-320-232 AIRCRAFT. THESE CRACKS ARE OCCURRING AT THE FORWARD EDGE OF THE SEAT PAN ADJACENT TO THE MOUNTING HOLES WHERE THE PAN IS ATTACHED TO THE SEAT FRAME. THE SEAT MANUFACTURER DESIGNATES THE SEAT PAN TO BE PRIMARY STRUCTURE.

Part: LGICU — FAILED (LANDING GEAR)

LANDING GEAR FAILED TO RETRACT. NR 1 LGICU FAULT. RETURNED TO ATL. NORMAL LANDING. *S/D* FOUND TARGET FOR PROX SENSOR 24GA LOOSE OR MISSING. RETORQUED BOLT AT BRACKET, OP CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

ESCAPE PATH LIGHTING IN FIRST CLASS AND FIRST TWO ROWS IN COACH INOP. REPLACED FWD PWR SUPPLY AND INSTALLED NEW BATTERY PACK, OPS CHECKED OK.

Part: BRAKES — SMOKING (RT MLG)

ON LANDING TOWER REPORTED SMOKING FROM RIGHT MAIN GEAR.

Part: DISCONNECT BOX — MIS INSTALLED (CABIN)

FOUND LOCALIZED HEAT DAMAGE AT THE WALL DISCONNECT BOX OF THE PASSENGER ENTERTAINMENT SYSTEM. *S/D* THE DAMAGE WAS CAUSED BY IMPROPER INSTALLATION OF ONE CONNECTOR AND MOISTURE FROM CONDENSATION. THE WALL DISCONNECT BOX WAS REPLACED AND OPERATED NORMALLY.

Part: EEL — INOPERATIVE (CABIN)

CABIN EMERGENCY LIGHT CHECK FAILED TEST.