N235NV

Part: LENS — CRACKED (ZONE 200) · airframe 69,386 hrs · 28,658 cycles

(AIRCRAFT NOT GROUNDED) DURING EMERGENCY EQUIPMENT CHECK, FOUND R2 DOOR FLOOR EMERGENCY EXIT LIGHT LENSE CRACKED. / REPLACED EXIT MARKER AT R2 DOOR IAW AMM 33-51-13-000-001-A AND 33-51-13-400-001-A. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 69,091 hrs · 28,515 cycles

(AIRCRAFT NOT GROUNDED) L2 AND R2 LOWER WALL MOUNTED EXIT MARKING SIGN INOP, REF TSM 33-51-00-810-814-A, PERFORMED AN OPERATIONAL TEST OF CABIN EMERGENCY LIGHTS AND SIGNS IAW MM 33-51-00-710-009-A. BOTH LOWER DOORS L2 AND R2 WALL MOUNTED EXIT SIGNS DID NOT COME ON. DUE TO BOT NOT ILLUMINATING TSM RECOMMENDS REPLACEMENT OF POWER SUPPLY UNIT 110WL3. ORIGNINAL PROBLEM REMAINS FUTHER T/S REQUIRED.

Part: OIL SYSTEM — LEAKING (APU) · airframe 68,349 hrs · 28,194 cycles

(AIRCRAFT NOT GROUNDED) FA'S STATE ""DIRTY SOCK SMELL"" FROM TAXI UNTIL APPROX 10,000FT / PERFORMED TC 21-00-002. NO DISCREPENCIES FOUND. PER TC 21-00-002 THIS CLEARS MEL 49-10-01-A MDDR# 211203. INOP PLACARDS REMOVED. NO 'M' PROCEDURES. M313 BEING GENERATED FOR TC 21-00-003. (RESOLVED ON W/O: 519752 TASKCARD: NR-00003 ) C/W TC A32X-21-000-003 AS REQUIRED. DURING A32X-21-000-002 TASK CARD, APU FOUND TO BE LEAKING. APU WAS REMOVED AND REPLACED ON TSR-1681 TC 21-000-003 WAS ACCOMPLISHED ASWELL THIS CLEARS MDDR# 211374 INOP PLACARDS REMOVED."

Part: BELLOWS — FAILED (CONDENSER) · airframe 67,372 hrs · 27,747 cycles

(AIRCRAFT NOT GROUNDED) AFT FLIGHT ATTENDENT REPORTED A DIRTY SOCK ODER DURING DESCENT THROUGH 9000 FEET. MID CABIN THROUGH AFT GALLEY / LH OZONE FILTER REMOVED, RH OZONE FILTER REMOVED, REPLACED SLEEVE (BELLOWS) ON CONDENSER W/REF AMM 21-52-32-400-001-A. (RESOLVED ON W/O: 507086 TASKCARD: NR-00001 ) C/W PHASE 3 T/C 21-000-003.ITEM: 1C/W PHASE 3 T/C 21-000-003.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,273 hrs · 26,729 cycles

ALL EMERGENCY LIGHT EXIT LOCATION SIGNS HAVE MULTIPLE LIGHTS INOP. / REMOVED AND REPLACED ALL INOP LAMPS IN CABIN EMERGENCY EXIT LOCATION SIGNS REF AMM 33-51-17-000-001-A AND 33-51-17-400-001-A"

Part: EPSU — UNKNOWN (UNKNOWN) · airframe 65,074 hrs · 26,641 cycles

FOUND LOWER EMERGENCY EXIT LIGHTS ON BOTH SIDES OF CABIN INTERIOR WOULD NOT ILLUMINATE. / REMOVED AND REPLACED L/H CABIN EPSU BATTERY 11WL0 IAW AMM 33-51-38-000-002-A & AMM 33-51-38-400-002-A. EMERGENCY EXIT LIGHT CHECK GOOD."

Part: EPSU — UNKNOWN (UNKNOWN) · airframe 65,005 hrs · 26,609 cycles

FWD & RH CABIN EMERGENCY LIGHTING BATTERY FAILED CABIN EMERGENCY LIGHTING TEST. / REMOVED AND REPLACED FWD & RH CABIN EMERGENCY LIGHTING BATTERY IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A. OPS CHECK SATISFACTORY."

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 64,388 hrs · 26,308 cycles

(EMERGENCY DECLARED) F/CTL FLAPS FAULT ECAM WHEN SELECTING FLAPS 2 ON BASE. ECAM AND CHECKLIST WERE ACCOMPLISHED.LANDING AND ROLL OUT WAS NORMAL, BRAKES GOT TO 500 DEG C AFTER LANDING, NO ISSUES DURING COOLING // PERFORMED A BITE TEST OF SFCC1/2 IAW AMM 27-51-00-740-002-A, NO FAULTS DETECTED, PERFORMED OPERATIONAL CHECK OF THE FLAP SYSTEM IAW AMM 27-54-00-710-001-A, OPS CHECK NORMAL, AC OK FOR SERVICE."

Part: CONTROLLER — FAULTED (CABIN PRESSURE) · airframe 60,457 hrs · 24,376 cycles

CAB PR2 FAULT, ECAM PROC FOLLOWED. / R & R #2 CABIN PRESSURE CONTROLLER & OP TEST OK W/REF TSM 21-31-00-810-827A."

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 60,042 hrs · 24,133 cycles

EMERG BATT FIN 12WL FAILED CAP TEST / REMOVED AND REPLACED EMERG BATT, OPS CHECK GOOD IAW AMM 33-51-38 PB 401"

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 60,042 hrs · 24,133 cycles

EMERG BATT FIN 10WL FAILED CAP TEST / REMOVED AND REPLACED EMERG BATTER FIN 10WL IAW A320 AMM 33-51-38 OPS CHECK GOOD"

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 60,042 hrs · 24,133 cycles

EMERG BATT FIN 11WL FAILED CAP TEST / REMOVED AND REPLACED EMERG BATT FIN 11WL IAW A320 33-51-38 OPS CHECK GOOD"

Part: NONE — NONE · airframe 61,500 hrs · 24,907 cycles

NRC 5000-0042: 1237-31. LH MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHEMENT FITTING FOUND CORRODED ON LOWER SURFACE ARROUND THE BUSHING. / LH MLG RETRACTION, JACK ANCHORAGE FITTING REPAIRED IAW SRM 57-26-13-300-008. SEE AWS FOR REPAIR DETAILS. REPAIR CATEGORY C, REPAIR LIFE LIMIT OF 35000FC FROM REPAIR EMBODIEMENT IAW SRM 57-26-13-300-008 TABLE 001. REPAIR ACCOMPLISHED AT 24064 FC. ANCHORAGE FITTING TO BE REPLACED OR AIRBUS MUST BE CONTACTED NLT 59064FC."

Part: NONE — NONE · airframe 47,260 hrs · 34,951 cycles

NRC 6000-0004: 211-2 R/H WING, HYDRAULIC PRESSURE LINE FEED THROUGH THE LOWER WING SKIN AT RIB 8 FWD OF FALSE SPAR HAS ELONGATED HOLE ELONGATED / R/H WING, PYLON MOUNTING PLATE BTW RIBS 7 AND 8 FWD OF FALSE SPAR PERMANENTLY REPAIRED IAW SRM 57-21-11-300-005. REPAIR CATEGORY A, NO FURTHER ACTION REQUIRED. ALUMINIUM: 2024T3 0.125IN PO:1622190. SEE NRC 4001444-6000-0078 FOR MECANIC ACCESS."

Part: NONE — NONE · airframe 32,152 hrs · 23,794 cycles

NRC 2000-0001: (274-2) JUST FWD OF R/H WINDSHIELD, BTWN FR3-4, DENT FOUND. / JUST FWD OF R/H WINDSHIELD BTW FR 3-4, DENT FOUND WITHIN LIMITS IAW SRM 53-00-11-283-005. REPAIR CATEGORY B, SEE SRI 53-00-11-205-050 FOR INSPECTION REQUIREMENTS. INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT: 60000FC/120000FH, SUBSEQUENT INSPECTION AT INTERVALS OF: TBD, INSPECTION METHOD: TBD. DENT DIMENSIONS: LENGTH: 2.900IN, WIDTH: 1.300IN, DEPTH: 0.032IN, A: 0.660IN, SKIN THICKNESS: 0.079IN, D/A 0.1? 0.032 0.066. SEE AWS FOR DETAIL."

Part: NONE — NONE · airframe 32,152 hrs · 23,794 cycles

NRC 1000-0110: 633-19 BULK CARGO DOOR CUTOUT LOWER SILL BEAM FR61 AND 62, NUT PLATE AREAS, CORROSION FOUND. / BULK CARGO DOOR CUTOUT LOWER SILL BEAM BTW FR 61 AND FR 62 AT NUT PLATES AREAS (QTY.2) PERMANENTLY REPAIRED IAW SRM 53-41-49-300-003. REPAIR CATEGORY B SEE SRM TASK SRI 53-41-49-205-003 FOR INSPECTION REQUIREMENTS: INSPECTION THRESHOLD FROM TIME OF REPAIR EMBODIMENT: 60000FC/120000FH, SUBSEQUENT INSPECTION INTERVALS: TBD FC/FH, INSPECTION METHOD: TBD. ALUMINIUM: 2024T3 0.090IN PO:1578507"

Part: DOOR SILL — CORRODED (FRMS 19-20) · airframe 59,936 hrs · 24,064 cycles

DURING THE S1 CHECK OF FWD LH PASSENGER/CREW DOOR CUTOUT LOWER SILL, CORROSION FOUND ON BRACKET BTW FR 19-20 / REPLACED BRACKET BTW FR 19-20 ON FWD LH PASSENGER/CREW DOOR CUTOUT LOWER SILL PER SRM 51-42-11."

Part: DUMMY RAIL — CORRODED (FRM 16) · airframe 59,936 hrs · 24,064 cycles

DURING THE S1 CHECK OF PASSENGER CABIN FLOOR STRUCTURE, CORROSION FOUND ON TRACK HARD POINT AT FR 16 AND Y503.2. / REPLACED PASSENGER CABIN FLOOR STRUCTURE DUMMY RAIL BEAM FR12- 16, Y503.2 PER IAW SRM 51-72-11-911-001."

Part: FLOOR SUPPORT — CORRODED (FRM 66) · airframe 59,936 hrs · 24,064 cycles

DURING THE S1 CHECK OF PASSENGER CABIN FLOOR STRUCTURE, FOUND CORROSION LOCATED ON LONGITUDINAL BEAM Y122 AT FR 66 AREA / REPLACED LONGITUDINAL BEAM BTW FR 64 - 66 AND Y122 PER SRM 51-72-11."

Part: EPSU — NO TEST (EMERGENCY LIGHTS) · airframe 59,449 hrs · 23,833 cycles

CABIN EMERGENCY LIGHTING EPSU SYS TEST 10WL,11WL,12WL AND 13WL FAILED TEST /REMOVED AND REPLACED EMERGENY BATTERY PACK 10WL,11WL,12WL AND 13WL W/REF TO AMM 33-51-38 PB 401 OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 58,055 hrs · 23,161 cycles

LT OVER WING EMERGENCY EXIT LIGHT INOP. REPLACED OVER WING EMERGENCY EXIT LIGHT.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 57,839 hrs · 23,031 cycles

(EMERGENCY DECLARED) CAB PR SYS 1 FAULT AT CRUISE / REPLACED CABIN PRESS CONTROL UNIT "

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 57,839 hrs · 23,031 cycles

(EMERGENCY DECLARED) CAB PR SYS 1 FAULT AT CRUISE / REPLACED CABIN PRESS CONTROL UNIT "

Part: COMPUTER — MALFUNCTIONED (FLAP SYSTEM) · airframe 57,767 hrs · 22,996 cycles

(EMERGENCY DECLARED) FLAP/CTL FLAPS FAULT ECAM MESSAGE FLAPS FAILED TO EXTEND /REPLACED SFCC #1. OPS CHECK GOOD."

Part: REGULATOR — MALFUNCTIONED (CREW OXYGEN)

(EMERGENCY DECLARED) IN CRUISE RECEIVED UNCOMMANDED O2 FLOW FROM FIRST OFFICERS MASK AT EXCESSIVE RATE. BLINKER LIGHTS ACTIVATED ON ALL OTHER MASKS O2 DEPLETED / REMOVED AND REPLACED PRESSURE REGULATOR"