N223FR

Part: CHECK VALVE — FAILED (HYD SYSTEM) · airframe 45,247 hrs · 28,679 cycles

LP1229537-1 DISCREPENCY: HYD Y RES OVERHEAT IN FLIGHT FOLLOWED ECAM AND QRH AND RETURNED TO MCO. LP1229537-1 CORRECTIVE ACTION: REF TSM29-13-00-810-802-A. PERFORMED FAULT CONFIRMATION IAW STEP 3B. DETERMINED MORE NOISE THAN USUAL AT CHECK VALVE Y (3083GM). REF STEP 4A, REQUIRES REPLACEMENT AT CHECK VALVE Y (3083GM). DEFECT REMAINS OPEN. REQUIRES FURTHER T/S. REF LP1229537 ITEM 2 FOR FURTHER MAINTENANCE ACTIONS. LP1229537-2 DISCREPENCY: REF LP1229537 ITEM1. "HYD Y RES OVERHEAT IN FLIGHT FOLLOWED ECAM AND QRH AND RETURNED TO MCO" LP1229537-2 CORRECTIVE ACTION: R/R 3083GM CHECK VALVE AND REPLACED LP FILTER 3002GM PRECAUTIONARY AND ALL OPS CHECKS NORMAL AT THIS TIME REF AMM 29-13-44-610-001-A, AMM29-24-21-400-801-A, & TSM 29-13-00-810-802-A. CHECK VALVE WAS CONFIRMED BAD ON VISUAL INSPECTION AFTER REMOVAL/ (3083GM)

Part: GENERATOR — DEFECTIVE (ZONE 100) · airframe 44,170 hrs · 28,214 cycles

DISCREPSNCY LPL 195040 ITEM 3 - OPS TEST OF EMERGENCY GENERATION SYS FAILED. CORRECTIVE ACTION - R+R CONSTANT SPEED MOTOTR GENERATOR REF AMM 24-24-51 PB 401 OPS CHECK GOOD NO LEAKS NOTED ATTHISTIME AC OKTO CONTINUE. T/W ATR0071 DUE 03-05-20.

Part: UNKNOWN — ODOR (CABIN) · airframe 44,104 hrs · 28,184 cycles

DISCREPENCY: LOG PAGE 1195027-ITEM1: FOR THE LAST HOUR OF THE FLIGHT THE CABIN CREW SMELLED A SWEET CHEMICAL SMELL IN THE FRONT THREE ROWS OF THE CABIN. THE SMELL WENT AWAY WHEN THE CABIN DOOR WAS OPENED ON THE GROUND. CORRECTIVE ACTION: LOG PAGE 1195027-ITEM 1: ACCOMPLISHED IDENTIFICATION OF CAUSE CABIN ODORS OR SMOKE. FOUND NO SWEET CHEMICAL SMELL IN THE FRONT THREE ROWS OR FORWARD GALLEY. REF: TSM 05-50-00-810-831.

Part: MANIFOLD — LEAKING (NR 2 ENGINE) · airframe 43,762 hrs · 28,033 cycles

FUME EVENT AFTER NR 2 ENGINE START PASSENGERS & CREW COMPLAINED OF BURNING EYES & NOSE ALONG WITH LIGHT HEADEDNESS FORWARD OF ROW 7 APU WAS RUNNING WITH PACKS NR 1 & 2 ON. INSPECTED AREA & FOUND LEAK FROM YELLOW MANIFOLD, R & R MANIFOLD IAW AMM 29-13-14, OPS CHECK & LEAK CHECK GOOD. ALSO R & R BOTH RECIRCULATION FILTERS IAW AMM 21-21-41& PERFORMED ENGINE RUNS IAW AMM 71-00-00-710-001 LEAK CHECK GOOD, AC OK TO CONTINUE SVC.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,318 hrs · 27,020 cycles

HOLE NR 3 LT ON FR35 STR30 REQUIRES COLD WORK AND FURTHER OVERSIZE PER TECH DISPOSITION 80523626/016/2018#A. REPAIRED FR35 STR 30 LT NR 3 HOLE PER TD/80523626/016/2018#A AND EA A2-53R-3448.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,318 hrs · 27,020 cycles

DISCREPANCY: REFERENCE N/R 2160N285, RHFEC CRACK INDICATIONS, LT FR35, STR30, LWR AFT HOLE (NR 3), 2ND LAYER FROM OUTSIDE, 5 OCLOCK ORIENTATION AS VIEWED FROM OUTBOARD. CORRECTIVE ACTION: REAMED NR 3 HOLE, ON LT FR35 STR 30, LWR AFT HOLE 2ND LAYER FROM OUTBOARD, 5 OCLOCK VIEWED FROM O/B. PERFORMED HFEC, NO INDICATIONS FOUND AT THIS TIME. FINAL HOLE SIZE .215 IAW SRM 51-44-11, NTM 51-10-01 PT 6 & ENGINEERING REST 6609./END/

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,318 hrs · 27,020 cycles

DISCREPANCY: REFERENCE N/R 2160N286, HFEC CRACK INDICATIONS, RT FR35, STR30, LWR AFT HOLE (NR 3), 2ND & 4TH LAYER FROM OUTBOARD, 7 OCLOCK ORIENTATION AS VIEWED FROM OUTBOARD. CORRECTIVE ACTION: REPAIRED RT FR35 STR 30R HOLE NR 3 PER TD/80523626/016/2018#A AND EA A2-53R-34448./END/

Part: LINE — LEAKING (HYD SYSTEM) · airframe 41,278 hrs · 27,000 cycles

DISCREPANCY: REFERENCE LOG PAGE LP1168034 ITEM 3, LOSS OF YELLOW HYDRAULIC SYSTEM IN FLIGHT, PERFORMED ATB. CORRECTIVE ACTION: REMOVED AND REPLACED #2 ENG HCV PIPE. REF AMM 29-13-49-420-091-B, T/W F9TAB1768C DUE 8/19. LEAK AND OPS CHECK GOOD./END/

Part: HELICOIL — PULLED (NR 2 ENGINE) · airframe 40,440 hrs · 26,645 cycles

CREW REPORT ON TAKEOFF/CLIMB ENGINE 2 LOSS OF OIL PRESSURE. PERFORMED ENGINE SHUTDOWN, DECLARED EMERGENCY AND RETURNED TO THE FIELD WITH NO OTHER ISSUES. CREW REPORTED NO PHYSICAL DAMAGED NOTED. MAINTENANCE INVESTIGATED AND FOUND NR 2 ENGINE OIL FILTER HELICOILS PULLED FROM HOUSING AND ENGINE HAD EVACUATED ENGINE OIL. DISPATCHED ROAD CREW AND REPLACED NR 2 ENGINE WITH SERVICEABLE ENGINE SN OFF 577210 SN ON 699851 REF AMM 71-22-11-210-042-B & 71-00-00-400-42-A. ROAD CREW ALSO PLACED OIL FILTERS ON TDI TO BE CHANGED BETWEEN 25-50 FLIGHT HOURS. ALSO COMPLETED SERVICE CHECK REFERENCE FFT-D05100-D0-1. RAN ENGINES OPS CHECK GOOD AND AIRCRAFT RELEASED FOR FLIGHT.

Part: UNKNOWN — ODOR (CABIN) · airframe 40,072 hrs · 26,483 cycles

AT CRUISE, THE FA REPORTED A DIRTY SOCK ODOR IN THE AFT GALLEY, CREW DECLARED AN EMERGENCY AND DONNED OYGEN MASKS AND SMOKE GOGGLES. DIVERTED. AT 12000 FT FLIGHT ATTENDANT REPORTED A CIGARETTE SMOKE ODOR. PERFORMED A 15 MINUTE IDLE RUN OR BOTH ENGINES IAW AMM 71-00-00-710-006. NO SIGNS OF OIL OR SMOKE COMING OUT OF THE FWD SUMP DRAINS DURING ENGINE OPERATION AND NO ODOR OF SMOKE IN THE CABIN IAW AMM 71-00-00-790-002B. NO FUEL OR HYDRAULIC OIL LEAKAGE. PERFORMED GVI OF THE NR 1 & 2 ENGINES, AND BOTH PACKS WITH NO EVEIDENCE OF OIL OR HYD LEAK OR INGESTION. INSPECTED AFT GALLEY LAVATORY AREAS FOR DIRTY SOCK ODOR. NONE NOTED IAW TSM 05-50-00-810-831-A.

Part: FITTING — DAMAGED (RUDDER) · airframe 38,476 hrs · 25,839 cycles

RUDDER BLUE ACTUATOR FITTING DAMAGED FROM BLUE ACTUATOR, DISASSEMBLING ITSELF FROM THE RUDDER SIDE. REMOVED AND REPLACED THE RUDDER IAW AMM 27-21-00. OPS CHECKED GOOD.

Part: SKIN — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 35,271 hrs · 24,622 cycles

CORROSION ON THE LT AFT PASSENGER DOOR CUT OUT SKIN BELOW THE SCUFF PLATE. REPAIRED THE LT AFT PASSENGER DOOR CUT OUT SKIN.

Part: BUSHING — CORRODED (NR 2 PYLON) · corrosion level 2 · airframe 35,271 hrs · 24,622 cycles

NR 2 PYLON TO WING INBD SHACKLE FITTINGS PRESSED BUSHINGS CORRODED. REMOVED THE NR 2 PYLON TO WING INBD SHACKLE FITTING PRESSED BUSHING AND INSTALLED AND LINE HONED NEW FABRICATED BUSHING IAW TD 802729958-006-2017 AND EA A2-57R-33669.

Part: RUDDER — DELAMINATED (ZONE 300) · airframe 35,271 hrs · 24,622 cycles

WATER DETECTED IN RUDDER BETWEEN SCREW 6 AND 7 FROM TOP OF TRAILING EDGE DOWNWARD, AREA OF INDICATION IS 7" X 2.5" FORWARD OF THE TRAILING EDGE. COMPLIED WITH TD/80274197/007/2017A AND EA A2-55R-33666. REPAIR RUDDER BETWEEN SCREWS 6 AND 7 FROM TOP TRAILING EDGE DOWNWARD.

Part: FLOOR SUPPORT — CORRODED (FRAME 68) · corrosion level 2 · airframe 35,271 hrs · 24,622 cycles

FLOOR SUPPORT -Y1292 HAS CORROSION ON UPPER SURFACE AT FRAME 68. REMOVED AND REPLACED THE FLOOR SUPPORT IAW 51-72-11

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 35,271 hrs · 24,622 cycles

FLOOR SUPPORT Y1292 HAS CORROSION ON UPPER SURFACE BETWEEN FRAMES 66 - 68. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,271 hrs · 24,622 cycles

RT FLOORBEAM -Y254 CORRODED AT FR 15. REMOVED AND REPLACED RT FLOORBEAM -Y254 IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,271 hrs · 24,622 cycles

RT FLOORBEAM +Y254 CORRODED AT FR15. REMOVED AND REPLACED RT FLOORBEAM +Y254 IAW SRM 51-42-11.

Part: SKIN — DENTED (FRAME 2) · airframe 35,271 hrs · 24,622 cycles

LEFT FORWARD FUSELAGE RVSM AREA HAD A DENT 3.9 X 4.9, MAX DEPTH .068 LOCATED 13 INCHES BELOW LAP AT LEFT SIDE STRUT JUST FORWARD OF FRAME 2. REPAIRED THE FORWARD FUSELAGE AREA IAW SRM 53-00-11-300-043.