N361FR

ATA 2750

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 19,705 hrs · 9,270 cycles

REFERENCE LP 557839 #2 AT ABOUT 4000' MSL, UNCOMMANDED ROLL WHILE GOING FLAPS 1 TO FLAPS 2 WITH SPEED BRAKE DEPLOYED. AUTO PILOT WAS OFF. OBSERVED ON FLIGHT CONTROL. SD PAGE LEFT AIL HALF DOWN, RIGHT AIL HALF UP. FELT REDUCED ROLL AUTHORITY WHILE TURNING. AC WAS GROUNDED. AIRBUS & TECH SERV STATED NO ABNORMALITY. C/W AMM 27-96-00-710-023-A NO FAULTS FOUND. AC RETURNED TO SERVICE.

ATA 5322

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 16,894 hrs · 7,809 cycles

DISCREPANCY: REFERENCE AIRBORNE N/R 16065.0272 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. AFT LH FUSE FR 69-70 SHEAR WEB IS CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED L/H SHEAR WEB AT FR 69-70 IAW A320 NEO SRM 51-72-11. MX ACTION IS ACCEPTABLE. /END/.

ATA 5322

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 16,894 hrs · 7,809 cycles

AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. AFT RH FUSE FR 69-70 SHEAR WEB IS CRACKED. REMOVED AND REPLACED SHEAR WEB R/H BETWEEN FR 69-70 IAW A320 NEO SRM 51-42-11. MX ACTION IS ACCEPTABLE.

ATA 5347

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 16,894 hrs · 7,809 cycles

AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. L1 DOOR O/B SEAT TRACK HAS CORROSION BETWEEN FR 18-20. REMOVED AND REPLACED L1 DOOR O/B SEAT TRACK IAW A320 SRM 51-72-11-911-001. MX ACTION IS ACCEPTABLE.

ATA 2910

Part: FITTING — CRACKED (HYDRAULIC SYSTEM) · airframe 14,753 hrs · 6,654 cycles

ACFT WAS REMOVED FROM SERVICE UNTIL REPAIRS MADE. REFERENCE LP352447 ITEM 1, LOST-YELLOW HYDRAULIC SYSTEM. FOUND PYLON HIGH PRESSURE FITTING CRACKED. REMOVED AND REPLACED FITTING REF.AMM 29-13-49-400-813-A. LEAK CHECK GOOD. OK TO CONTINUE.

ATA 2120

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 12,686 hrs · 5,675 cycles

DISCERPANCY: REFERENCE LP 405902. SDR REPORTABLE EVENT. AFTER LANDING RECEIVED ECAM L/G SHOCK ABSOBER FAULT, ANTI-ICE CAPT TAT, NAV TCAS FAULTS. THESE MSGS DISAPPEARED THEN SHORTLY REAPPEARED FOLLOWED BY SMELL OF SMOKE IN COCKPIT THEN ECAM WARNING ENGINES. CORRECTIVE ACTION: REF LP405902 ITEM 2 DUE TO COCKPIT SMOKE EVENT. PERFORMED TYPE 9 PROCEDURE IN TSM 05-50-00-810-831-A AND ALSO LEVEL A INSPECTION PERFORMED PACK AIR SUPPLY W/ ENGINE 1 AND 2 PER AMM 36-11-00-710-803-A. NO SIGNS OF SMOKE, FUMES, OR ODOR. PERFORMED E&E FWD AND AFT EWIS INSPECTION. NO DEFECTS FOUND TO WIRING, LRUS AND PLUGS. NO SIGNS OF MOISTURE OR WETNESS INSIDE E&E COMPARTMENTS. A/C OK FOR SERVICE. /END/

ATA 3350

Part: BATTERY — DISCHARGED (ZONE 200) · airframe 11,511 hrs · 5,110 cycles

PER HEAVY CHECK T/C PERFORMED OPS TEST OF EMERGENCY LIGHTS VIA MCDU. FAULT BAT/EPSU (11WL) EMERGEN L PERFORMED T/S IAW TSM 33-51-00-810-855-A FOUND BATTERY FOR 11WL NEEDING TO BE REPLACED. REMOVED AND REPLACED BATTERY AT EPSU 11WL IAW AMM 33-51-38-000/400-002-A OPS TEST GOOD VIA MCDU. CIDS POWER UP INTERFACE TEST GOOD. A/C OK FOR SERVICE. (AIRCRAFT WAS RETURNED TO SERVICE)/END/

ATA 2740

Part: RELAY — FAILED (STAB TRIM) · airframe 9,478 hrs · 4,249 cycles

WHEN SETTING TRIM FOR TAKE-OFF, TRIM WHEEL KEEPS MOVING PAST DESIRED SETTING BY ITSELF. WILL MOVE FULL DOWN OR FULL UP IF NOT STOPPED MANUALLY. REMOVED AND REPLACED RELAY 36CE3 IAW AMM 20-46-50-01. OPS CHECK GOOD. A/C OK FOR SERVICE.

ATA 2740

Part: ACTUATOR — FAULTED (TRIM SYSTEM) · airframe 9,478 hrs · 4,249 cycles

DISCREPANCEY: REFERENCE LP 271287 WHEN SETTING TRIM FOR TAKE OFF, TRIM WHEEL KEEPS MOVING PAST DESIRED SETTING BY ITSELF WILL MOVE FULL DOWN OR FULL UP IF NOT STOPPED MANUALLY CORRECTIVE ACTION: REFERENCE LP 271287 W/O MIA-22-1391 REMOVED THSA INSTALLED SERVICEABLE UNIT AND ELSD. INSTALLED IAW 2711-51-400-001-1A, REMOVED IAW 27-41-00-730-001-A.//END//

ATA 2565

Part: SLIDE — NO TEST (L1 DOOR) · airframe 4,365 hrs · 1,911 cycles

L1 ESCAPE SLIDE FAILED EPSU TEST. THIS WAS DURING OVERNIGHT MAINTENANCE. REPLACED L1 ESCAPE SLIDE L1 IAW AMM 25-62-44-400-007-A. T/W F9TAB1763C, CAL DUE 04-2022. TEST OK.